A UNITED STATES DEPARTMENT OF COMMERCE PUBLICATION

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U.S. DEPARTMENT OF COMMERCE

National Oceanic and Atmospheric Administration

COLLECTED REPRINTS-1971

Volume II

ATLANTIC OCEANOGRAPHIC ND METEOROLOGICAL LABORATORIES

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'WENT O^

U.S. DEPARTMENT OF COMMERCE Peter G. Peterson, Secretary

NATIONAL OCEANIC AND ATMOSPHERIC ADMINISTRATION Robert M. White, Administrator ENVIRONMENTAL RESEARCH LABORATORIES Wilmot N. Hess, Director

Collected Reprints— 1971

Volume II

ATLANTIC OCEANOGRAPHIC

AND METEOROLOGICAL LABORATORIES

ISSUED JULY 1972

T,

o

Atlantic Oceanographic and Meteorological Laboratories Miami, Florida 33149

For sale by the Superintendent of Documents, U. S. Government Printing Office, Washington, D. C. 20402

■•

FOREWORD

An increased understanding of the ocean and its processes, of the underlying geological and geophysical structures, and of the overlying atmosphere and its interactions with the sea will result in man's increased ability to deal intelligently with the problems of this environment.

The scientific and technical accomplishments of the National Oceanic and Atmospheric Administration's Environmental Re- search Laboratories are contributing to this understanding. Be- cause the published results of the Atlantic Oceanographic and Meteorological Laboratories are broadly scattered through the literature, they are being brought together in a series of annual publications. These provide a convenient summary of the results of the work of these laboratories for researchers and interested laymen alike.

This volume, the sixth in the series, contains the published results of NOAA's Atlantic Oceanographic and Meteorological Laboratories for the year 1971.

Director, Atlantic Oceanographic and Meteorological Laboratories

Digitized by the Internet Archive

in 2012 with funding from

LYRASIS Members and Sloan Foundation

http://archive.org/details/collectedreprintv2atla

CONTENTS

VOLUME

General

Ape 1 , John R .

Wave Interactions in Solid State Plasmas: Book Review. Physics Today 2_4, No. 2, p. 47.

Stewart, Harris B. Jr.

CICAR - An International Ocea nog rap h i c Program in the Caribbean: Oceanic Citation Journal 8_, No. 5, 2-5-

S tewa rt, Harris B. Jr.

Ecological Aspects of Industrial Development: Muse News _M_> No. 12, 411-413-

Stewart, Harris B. Jr.

Exploring America's Mediterranean: NOAA 1, No. 2, 9-11.

Stewart, Harris B. Jr.

Man and the Sea: Book Review. Bulletin of the American Meteorological Society 5_2_, No. 8, 739-740.

Stewart, Harris B. Jr.

Non-Food Resources as Viewed by: Federal Oceanog raph i c Research: Third Proceedings of the Third Sea Grant Conference, sponsored by Oregon State University, March 1970, 47-48.

S tewa rt, Harris B. Jr.

Ocean Symposium: AAAS Symposia Annual Meeting: Phila- delphia. Science 1 74 , No. 4012, 964-965.

Staff

Satellite Data Requirements of Atlantic Oceanog raph i c and Meteorological Laboratories for Studies of Ocean Physics and Solid Earth. NOAA TR ERL 225-AOML 5-

Physical Oceanography

9. Chew, Frank, and G. A. Berber ion

A Determination of Horizontal Divergence in the Gulf Stream Off Cape Lookout: Journal of Physical Oceanog- raphy J_, No. 1 , 13-kk .

1 0 . Hansen , Dona Id V .

Oceanography for the 1970's. The Science Teacher 38 , No . 1 .

11. Hansen, Donald V.

Oceans from Space: Book Review. Bulletin of the American Meteorological Society 5_2_, No. 8, 738-739-

12. Low, James K., and George A. Maul

Precise Two-Point STD Calibrations: Marine Technology Society Journal 5_, No. 5, 22-33.

13. Zet 1 e r , Bernard D .

Earth Tides. McGraw-Hill Yearbook of Science Tech no 1 ogy , 174-177-

\h. Zetler, Bernard D., and George A. Maul

Precision Requirements for a Spacecraft Tide Program: Journal of Geophysical Research 7_6_, No. 27, 6601-6605-

1 5 - Zet 1 er , Berna rd D .

Radiational Ocean Tides Along the Coasts of the United States: Journal of Physical Oceanography ]_, No. 1, 34-38.

16. Zetler, Bernard D., D. Cartwright, and W. Munk

Tidal Constants Derived from Response Admittances: Sixth International Symposium on Earth Tides, Stras- bourg 1 969 , 1 -4 .

17- Zetler, Bernard D .

Tide: Encyclopedia Americana, 7 3 1 ~ 7 3 5

18. Zet ler , Bernard D .

Tsunamis and the Seismic Sea Wave Warning System: Man and the Sea, American Museum of Natural History, 301 -306.

Meteorology

19- Anthes , R i chard A .

A Numerical Model of the Slowly Varying Tropical Cyclone in Isotropic Coordinates: Monthly Weather Review 99 , No. 8, 617-635.

20 . Anthes , Richard A .

Iterative Solutions to the Steady-State Ax i symme t r i c Bounda ry- Laye r Equations under an Intense Pressure Gradient: Monthly Weather Review 99_, No. 4, 261-268.

2 1. Anthes , R i cha rd A .

Numerical Experiments with a Slowly Varying Model of the Tropical Cyclone: Monthly Weather Review 99 , No. 8, 636-643.

22 . Anthes , R i cha rd A .

The Development of Asymmetries in a Th r ee-D i men s i ona 1 Numerical Model of the Tropical Cyclone: NOAA Tech Memo ERL NHRL-94 .

23 Anthes , R i chard A .

The Response of a Three-Level Axisymmetric Hurricane Model to Artificial Redistribution of the Convective Heat Release: NOAA Tech Memo ERL NHRL-92.

24. Anthes, Richard A., Stanley L. Rosenthal, and James W. Trout

Preliminary Results from an Asymmetric Model of the Tropical Cyclone: Monthly Weather Review 9_9.» No. 10, 744-758.

25. Anthes, Richard A., James W. Trout, and Stellan S. Ostlund

Three-Dimensional Particle Trajectories in a Model Hurricane: Weatherwjse 2_4, No. 4, 174-178.

26. Anthes, Richard A., James W. Trout, and Stanley L. Rosenthal

Comparisons of Tropical Cyclone Simulations With and Without the Assumption of Circular Symmetry: Monthly Weather Review 99, No. 10, 7 59 - 766 .

27 Bl ack , Peter G .

Cumulonimbus Modification of Tropical Nature: Bulletin of the American Meteorological Society 52, No. 7, 562- 565.

28. Black, Peter G., and Richard A. Anthes

On the Asymmetric Structure of the Tropical Cyclone Outflow Layer: Journal of Atmospheric Sciences 28, No. 8, 13^8-1366.

29 . Carl son , Toby N .

A Detailed Analysis of Some African Disturbances: NOAA Tech Memo ERL NHRL-90.

30. Carl son , Toby N.

Weather Note: An Apparent Relationship Between the

Sea-Surface Temperature of the Tropical Atlantic and

the Development of African Disturbances into Tropical

Storms: Monthly Weather Review 99., No. k, 309 - 3 1 0 .

31. Carlson, Toby N., and Robert C. Sheets

Comparison of Draft Scale Vertical Velocities Computed from Gust Probe and Conventional Data Collected by a DC-6 Aircraft: NOAA Tech Memo ERL NHRL-91.

32 . Gentry , R . Cec i 1

To Tame a Hurricane: Science Journal, 49 ~ 5 5 .

33- Koss, Walter James

Numerical Integration Experiments with Variable-Reso- lution Two- D i men s i ona 1 Cartesian Grids Using the Box Method: Monthly Weather Review 99., No. 10, 725~ 738 .

3^. Rosenthal, Stanley L.

The Response of a Tropical Cyclone Model to Variations in Boundary Layer Parameters, Initial Conditions, Lateral Boundary Conditions and Domain Size: Monthly Weather Review 99, No. 10, 767~ 777 .

35- Rosenthal, Stanley L., and Michael S. Moss

Numerical Experiments of Relevance to Project Stormfury NOAA Tech Memo ERL NHRL-95.

36. Rosenthal, Stanley L., and Michael S. Moss

The Responses of a Tropical Cyclone Model to Radical Changes in Data Fields During the Mature Stage: NOAA Tech Memo ERL NHRL-96.

37 . Scott , Wi 1 1 iam D .

Aerosol Sampling and Data Analysis with the NCAR Coun- ter: The Second International Workshop on Condensation and Ice Nuclei sponsored by National Science Foundation, August 1970, 49-52.

38. Scott, William D., Robert K . Cunningham, Robert G. Knollenberg, and William R. Cotton

Symposium on the Measurements of Cloud Elements: Bulletin of the American Meteorological Society 52 , No. 9, 889-890.

39- Sugg, Arnold L., Leonard G. Pardue, and Robert L. Carrodus

Memorable Hurricanes of the United States Since 1873: NOAA Tech Memo NWS SR-56.

Vo 1 ume I I

Meteorology (continued)

40. Staff

Project Stormfury 1970 Annual Report.

41. Trout, James W., and Richard A. Anthes

Horizontal Asymmetries in a Numerical Model of a Hur ricane: NOAA Tech Memo ERL NHRL-93-

42 . Barday , Robert J .

Free-Air Gravity Anomalies South of Panama and Costa Rica (NOAA Ship Oceanog raphye r - August 1969) : NOAA Tech Memo ERL A0ML-14.

43

44

Bassinger, B. G

R

N. Harbison, and L. Austin Weeks

Marine Geophysical Study Northeast of Trinidad-Tobago The American Association of Petroleum Geologists Bulletin 55_, No. 10, 1730-1740.

Bennett, Richard H., and Douglas N. Lambert

Rapid and Reliable Technique for Determining Unit Weight and Porosity of Deep-Sea Sediments: Marine Geology 11, 201 -207-

45. Bennett, Richard H., Douglas N. Lambert, and Paul J. Grim

Tables for Determining Unit Weight of Deep-Sea Sedi- ments from Water Content and Average Grain Density Measurements: NOAA Tech Memo ERL AOML-13.

46 . D ietz , Robert S .

North Atlantic-Geology and Continental Drift (A Sympo- sium): Marine Technology Society Journal 5, No. 5, 33

47 . D i etz , Robert S .

Shatter Cones (Shock Fractures) in Astroblemes: Mete- or i tics 6, No. 4, 258-259.

48 . D ie tz , Robert S .

Sudbury Astrobleme: A Review. Meteorftics 6_, No. 4, 259-260.

49 . D i etz , Robert S .

The Sea: Ideas and Observations on Progress in the Study of the Seas. Book Review American Scientist 59 , No. 5, 627.

50 . D i etz , Robert S .

Those Shifty Continents 204-21 2.

Sea Frontiers 17, No. 4,

Dietz, Robert S., and K. D.

Portrait of a Scientist: Rev iews 7 , No. 1 , A9~A1 5

Erne ry Francis Shepa rd

Earth-Science

52. Dietz, Robert S,, and John C. Holden

Pre-Mesozoic Oceanic Crust in the Eastern Indian Ocean (Wharton Basin): Nature 229, No. 5283, 309-312.

53. Dietz, Robert S., John C. Holden, and Walter P. Sproll

Geotectonic Evolution and Subsidence of Bahama Platform Reply. Geological Society of America Bulletin 82 , 811-814.

54. Dietz, Robert S., and Harley J. Knebel

Trou Sans Fond Submarine Canyon: Ivory Coast, Africa: Deep Sea Research 18, 441-447.

55- Freeland, George L., and Robert S. Dietz

Plate Tectonic Evolution of Caribbean - Gulf of Mexico Region: Nature 232 , 20-23.

56. Keller, George H.

Engineering Properties of North Atlantic Deep-Sea Sediments: Interocean '70 2_, 6 5 ~ 7 1 -

57 Ke 1 1 er , George H .

Mass Properties of the Sea Floor in a Selected Deposi- tional Environment: Proceedings Civil Engineering in the Oceans II, Miami Beach, December 1969, 857-877-

58 . La 1 1 imore , R

62

63

6k

K

L. Austin Weeks, and L. W. Mordock

Marine Geophysical Reconnaissance of Continental Margin North of Paria Peninsula, Venezuela: The American Association of Petroleum Geologists Bulletin 55., No. 10, 1719-1729.

59- Peter, George and Omar E. DeWald

Deformation of the Sea Floor off the North-west Coast of the United States: Nature Physical Science 232 , No. 31 , 97-98.

60. Peter, George, Barrett H. Erickson, and Paul J. Grim

Magnetic Structure of the Aleutian Trench and Northeast Pacific Basin (I968): The Sea, Ed. A. E. Maxwell, Pub- lished by Wi 1 ey- I n terse i ence , k, pt. 2, 191-222, 1971. John Wiley & Sons, Inc., 1971.

6 1 . Rona , Peter A .

Bathymetry Off Central Northwest Africa Research 18, 321-327.

Deep Sea

Rona , Peter A .

Deep Sea Salt Diapirs: Letter to editor Geotimes, p. 8

Rona , Peter A .

Depth Distribution in Ocean Basins and Plate Tectonics: Nature 2_3J_, 179-180.

Starr, Robert B., and Robert G. Bassinger

Marine Geophysical Observations of the Eastern Puerto Rico-Virgin Islands Region: Trans-Fifth Caribbean Geo- logical Conference, Geology Bulletin No. 5, Queens Col 1 ege Press , 25-29-

65

66

Weeks, L. Austin, and Robert K. Lattimore

Continental Terrace and Deep Plain Offshore Central California: Marine Geophysical Research 1, 145-161.

Weeks, L. Austin, R. K. Lattimore, R B. G. Bassinger, and G. F. Merrill

N . Harbison,

Structureal Relations Among Lesser Antilles, Venezuela, and Tr i n i dad -Tobago : The American Association of Petroleum Geologists Bulletin 55, No. 10, 1741-1752.

67

68

69

70

71

72

Sea-Air Interaction

Hanson, K i r by J .

Studies of Cloud and Satellite Parameterization of Solar Irradiance at the Earth's Surface: Proceedings of the Miami Workshop on Remote Sensing March 29-31, 1971 , M iami , Florida , 133-148.

McAl i s ter , E

William McLeish, and Ernst A. Corduan

Airborne Measurements of the Total Heat Flux from the Sea during BOMEX: Journal of Geophysical Research 76 , No. 18, 4172-4180.

Nordbert, W., J. Conway, Duncan B. Ross, and T. Wilheit

Measurements of Microwave Emission from a Foam- Covered Wind-Driven Sea: Journal of Atmospheric Sciences 2_8_, No. 3, 429-435-

Ostapof f , F .

Introductory Remarks - Sea-Air Interaction Instrumen- tation: IEEE Transactions on Geoscience Electronics GE-9, No. 4, 197-198.

Ostapoff, F.

Ocean-Atmosphere Interaction in the Caribbean Sea: Viewed from the Ocea nog ra phe r Side: Proceedings Sym- posium on Investigations and Resources of the Caribbean Sea and Adjacent Regions, 1 3 7 - 1 4 5 .

Shinners, W i 1 lard W., Gerald E. Putland, and Peter B. Connors

Tests of Modified Radiosonde Hygristor Duct: NOAA Tech Memo ERL A0ML-15.

U.S. DEPARTMENT OF THE NAVY J. H. CHAFEE, Secretary

Naval Weather Service Command W. J. KOTSCH, Rear Admiral, USN, Commander

40

U. S. DEPARTMENT OF COMMERCE M. H. STANS, Secretary

National Oceanic and Atmospheric Administration R. M. WHITE, Administrator

PROJECT STORMFURY

ANNUAL REPORT

1970

MIAMI, FLORIDA MAY 1971

Project STORMFURY was established by an Interdepartmental agreement between the Department of Commerce and the Department of Defense, signed July 30, 1962. Additional support has been provided by the National Science Foundation under Grant NSF-G-17993

This report is the ninth of a series of annual reports to be prepared by the Office of the Director in accordance with the Project STORMFURY interdepartmental agreement.

Additional copies of this report may be obtained from:

U. S. Naval Weather Service Command Department of the Navy Washington Navy Yard Washington, D. C. 20390

or

National Hurricane Research Laboratory

P. 0. Box 8265, University of Miami Branch

Coral Gables, Florida 3312A.

NOTICE

The National Hurricane Research Laboratory and the Naval Weather Service Command, do not approve, recommend, or endorse any proprietary product or proprietary material mentioned in this publication. No reference shall be made to either or- ganization or to this publication in any advertising or sales promotion which would indicate or imply that the National Hur- ricane Research Laboratory or the Naval Weather Service Com- mand approves, recommends, or endorses any proprietary product or material mentioned herein, or which has as its purpose an intent to cause directly or indirectly the advertised product to be used or purchased because of this publication.

TABLE OF CONTENTS

INTRODUCTION

HISTORY AND ORGANIZATION

PROJECT STORMFURY ADVISORY PANEL

PUBLIC AFFAIRS

PYROTECHNIC DEVICES - SILVER IODIDE

AREAS OF OPERATIONS

PLANS FOR FIELD OPERATIONS - 1970

FIELD OPERATIONS

RESEARCH ACTIVITIES

OPERATIONAL AND RESEARCH DATA COLLECTION

OUTLOOK FOR 1971

REFERENCES AND SPECIAL REPORTS

APPENDIX A. Report On Meeting Of Project Advisory Panel

APPENDIX B. A Hypothesis For Modification Of Hurricanes

APPENDIX C.

APPENDIX D.

APPENDIX E.

APPENDIX F.

APPENDIX G.

APPENDIX H.

APPENDIX I.

APPENDIX J.

H u r r i H u r r i

Summa Asymm

Respo To Ag Sol ut

Measu Eyewa

An Es Tropi

Ice-P Cumul

Use 0 Activ

Use 0 H u r r i

cane Model ing At T cane Research Labo

ry Of Prel i mi nary etric Model Of The

nse of STORMFURY C I And Agl-Nal Ice ion-Combustion Gen

he National ratory (1970)

Results From An Tropical Cyclone

loudline Cumuli Nuclei From A era tor

1 Motion In The Hurricane Debbie

rements Of Vertica 11 Cloud Region Of

timate Of The Fraction Ice In cal Storms

hase Modification us Clouds In Hurri

Potential Of canes

f Light Aircraft In STORMFURY i t i e s

f Echo Velocities cane Modification

To Evaluate Experiments

Page

1

2

3

4

4

5

5

8 10 12 13 14

A-l

B-l

C-l D-l

E-l F-l G-l H-l 1-1 J-l

1 1 1

APPENDIX K. APPENDIX L.

A Summary Of Radar Precipitation Echo Heights In Hurricanes

Project STORMFURY Experimental Eligibility In The Western North Pacific

Page K-l

L-l

1 v

PROJECT STORMFURY ANNUAL REPORT

1970

INTRODUCTION

The apparently successful seeding operations on Hurri- cane Debbie in 1969 made it most urgent that similar experi- ments be carried out on a 1970 storm to provide further eval- uation of the effectiveness of the technique. The 1970 hurricane season, however, produced no tropical cyclones which were eligible for seeding experiments. In spite of this, or perhaps because of it, the 1970 season was undoubt- edly the most productive research period for Project STORMFURY to date.

forces line ex Storm D the Nav 24 July e x e r c i s forces on 1 9 A a h u r r i not i n t ment, s FURY mo c i e n 1 1 y to Puer weaken e r a t i o n needed

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With the lack of eligible storms in 1970, the hurri- cane research efforts were intensified and carried out with- out operational interruptions. The results of these various research activities are extremely interesting particularly as they relate to future STORMFURY operations, and the more significant results are given in the Appendices to this re- port. Of special interest in this connection is Appendix B which details a new and better explanation for the apparent success of the 1969 "Debbie" experiments than was possible with the pre-existing hypothesis.

The optimism generated by the "Debbie" work also re- sulted in increased emphasis being placed on the Project by the Government. In 1970 Project STORMFURY was designated a National Pilot Project by the Interdepartmental Committee for Atmospheric Science (ICAS), and some additional STORMFURY funding was made available in the FY-1971 budget of the Department of Commerce.

HISTORY AND ORGANIZATION

Project STORMFURY is a joint Department of Commerce (NOAA) -Department of Defense (Navy) program of scientific ex- periments designed to explore the structure and dynamics of tropical cyclones and their potential for modification. The Project which was formally established in 1962 has as its principal objective experimentation directed towards changing the hurricane's energy exchange by strategic seeding from aircraft with silver iodide crystals. The crystals are dis- pensed from pyrotechnic devices developed by the U.S. Navy. The hypothesis calls for a measurable decrease in the maximum wind velocities near the center of the storm. Navy and NOAA scientists and aircraft, supplemented by those of the U.S. Air Force, have cooperated in STORMFURY experimental opera- tions since 1961 when the first informal agreement was pro- posed. To date, the experiments conducted by the Project consist of:

Hurricane Esther Hurricane Beulah Tropical Cumulus Tropical Cumulus

- seeded in 1961 - Single seeding

- seeded in 1963 - Single seeding Cloud Seedings - 1963

Cloud Seedings - 1965

Tropical Cloudline Seedings - 1968

Tropical Cloudline Seedings - 1969

Hurricane Debbie Seedings - 1969 - Multiple seeding

Tropical Cloudline Seedings - 1970.

Since 1962, only two hurricanes have been seeded1. The results of the Hurricane Debbie multiple seeding experiments conducted on 18 and 20 August 1969, were extremely encour- aging in that a decrease in the maximum wind velocity of the hurricane was observed on both days. Although by no means conclusive, these observations coupled with radar and other meteorological data strongly suggest that a modification to Hurricane Debbie was achieved. The exact amount of effect caused by seeding is still s/ery difficult to determine due to the natural fluctuations which occur in each tropical cy- cl one.

The initial 1962 Project STORMFURY agreement between the Department of Commerce and the Department of the Navy covered 3 years and was renewed annually from 1965 to 1968. The 1969 renewal was extended to cover a 3 year period.

1 See Project STORMFURY Annual Reports 1963 through 1969.

Dr. Robert M. White, NOAA Administrator, and Rear Admiral W. J. Kotsch, U.S. Navy, Commander Naval Weather Service Command, had overall responsibility for the coopera- tively administered project.

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I I i n g e r Director tor.

PROJECT STORMFURY ADVISORY PANEL

The Advisory Panel of five members is representative of the scientific community and provides guidance through its consideration of various scientific and technical problems involved with the project. Their recommendations have proved to be of great value to the project since its inception.

The Panel reviews results from previous experiments, proposals for new experiments and their priorities, and makes recommendations concerning the effectiveness of data collec- tion and evaluation, eligibility criteria for storms to be seeded, and other items as applicable.

During 1970, the Advisory Panel consisted of the fol- lowing prominent scientists: Professor Noel E. LaSuer, Chairman (Florida State University), Professor Jerome Spar (Department of Meteorology and Oceanography, New York Uni- versity), Professor Edward Lorenz (Department of Meteorology, Massachusetts Institute of Technology), Professor Charles L. Hosier (Dean, College of Earth and Mineral Sciences, Pennsyl- vania State University), and Professor James E. McDonald (Institute of Atmospheric Sciences, University of Arizona).

The Panel met in Miami on 29 and 30 September 1970 to discuss numerical hurricane modeling research and the simula- ted seeding experiments with the hurricane models conducted by Dr. S. L. Rosenthal and his group at NHRL.

The Panel again met in Washington, D.C., on 28-30 January 1971. The first day, the Panel members participated in a briefing to NOAA about research on "Decision Analysis of Hurricane Modification" done at the Stanford Research Insti- tute. The Panel meeting on 29 and 30 January was attended by representatives from cooperating agencies and included full discussions of research on past experiments and future plans for the Project. Professor Lorenz resigned from the Panel in October due to the pressure of other work in which he is engaged. He was replaced by Professor Norman A. Phillips (Department of Meteorology, Massachusetts Institute of Tech- nology). Recommendations from the Panel meetings in Miami, Florida, and Washington, D.C., are included in this report as Appendix A.

PUBLIC AFFAIRS

A coordinated press release and fact sheet for STORM- FURY were distributed to the media prior to the experimental season. Although no hurricane seeding opportunities occur- red, the public affairs team was prepared to operate with a plan similar to that used during the "Debbie" experiments of 1969. Two seats on the Project aircraft were to be made available on a pool basis to media representatives. One seat was to go to a reporter and the other to a cameraman repre- senting TV networks. Additional seats for the media may be possible for future operations if sufficient interest for additional coverage becomes apparent.

PYROTECHNIC DEVICES - SILVER IODIDE

The pyrotechnics prepared for the 1970 season were similar to the STORMFURY I unit used in the 1969 seeding experiments, but incorporated several improvements that made them safer to handle. This new unit, developed under the leadership of Dr. Pierre St. Amand of the Naval Weapons Cen- ter, China Lake, California, was provisionally designated WMU-2(XCL-1 )/B.

The new unit is fired from the same type of rack and cartridge case as is the STORMFURY I round. Its pyrotechnic grain is also similar in composition and performance to that of the earlier unit, but it incorporates pressure relief, bore-safety, and time delay functions that will permit it to be certified for general use in all appropriate racks and aircraft without special supervision.

More details of the pyrotechnics used can be found in Appendix D of the 1969 Project STORMFURY Annual Report.

AREAS OF OPERATIONS

Eligible areas for experimentation in 1970 were the Gulf of Mexico, the Caribbean Sea, and the southwestern North Atlantic region.

Operations in these areas were limited by the following guideline: A tropical cyclone was considered eligible for seeding as long as there was only a small probability (10 percent or less) of the hurricane center coming within 50 miles of a populated land area within 18 hours after seeding.

There are two primary reasons for not seeding a storm near land. First, a storm seeded further at sea will have reverted to its natural state prior to affecting a land area. Second, large changes in the hurricane structure occur when it passes over land. These land- induced modifications would obscure the short period effects expected to be produced by the seeding experiments and greatly complicate the scientific evaluation of the results.

PLANS FOR FIELD OPERATIONS - 1970

The period 20 July to 31 October was established for STORMFURY operations in 1970. The following aircraft were planned as STORMFURY forces during the season:

1. Navy Weather Reconnaissance Squadron Four

Four WC-121N's

2. Marine All-Weather Attack Squadron Two Two Four

Four A-6 Intruders

3. NOAA Research Flight Facility

Two DC-6's

One B-57

One C-54 (replaced by a C-130 during the season)

4. Air Force 53rd Weather Reconnaissance Squadron

Two WC-130's

5. Air Force 55th Weather Reconnaissance Squadron

One WC-135

6. Air Force 58th Weather Reconnaissance Squadron

One RB-57F

7. Naval Air Test Center

One P3

8. Naval Weapons Center One Cessna 401 .

The plan also provided for a series of fall-back re- search missions to be used when no eligible hurricane was available for seeding after deployment of project forces. These research missions are primarily data gathering or storm monitoring missions in unseeded cloud systems or storms

As recommended by the STORMFURY Advisory Panel, first priority was given to the eyewal 1 experiment in order to gain additional data which could be correlated with those collected during the 1969 "Debbie" seeding experiments.

This multiple seeding of the clouds in the annulus radially outward from the maximum hurricane winds calls for five seedings at 2-hour intervals. Each seeding consists of dropping 208 pyrotechnic units along a radially outward flight path, starting just outside the radius of maximum winds. The hypothesis in 1969 and early 1970 stated that the introduction of freezing nuclei (silver iodide crystals produced by the pyrotechnics) into the clouds in and around the eyewal 1 should cause a chain of events that includes the release of latent heat, warming of the air outside the central core, changes in temperature and pressure gradients, and a reduction in maxi- mum winds. Data from several experiments and individual cases are needed before definite conclusions regarding the validity of this hypotehsis can be assumed.

Because the magnitude of natural variations in hurri- canes is sometimes as large as the hypothesized artificially induced changes, it is frequently difficult to distinguish between the two.

Second priority was given to the rai to the rainband experiments. The rainsecto designed to test whether some of the latent air flowing toward the center of the hurric cepted and released while it is still betwe miles from the center. If successful, this result in the dispersal of the energy over rather than concentration near the center, degree sector between 50 and 75 miles radiu stimulate growth. This sector is selected area where an abundance of warm moist tropi carried by the low-level winds toward the c center of the storm. If cloud growth in th moist air to ascend to the outflow layer at large radius, some of the energy normally r center of the storm would be released at gr could result in a reduction in the storms'

nsector and third r experiment is

energy in the ane can be inter- en 50 and 100

experiment should a 1 arger area

Clouds in a 4 5- s are seeded to because it is an cal air is being louds nearer the is sector causes

a relatively el eased near the eater radi us and wind maxi ma .

All suitable clouds in the designated sector are seeded while monitoring aircraft continue to collect data to document changes in storm structure or intensity. The seed- ings are made in four periods of 50 minutes each, separated by non-seeding periods of 50 minutes.

The Rainband Experiment has the same objectives as does the Rainsector Experiment and, in addition, should per- mit the opportunity to study the interaction of seeded clouds with other clouds in the same and nearby rainbands. Clouds are seeded along a rainband (a line of clouds spiraling a- round and toward the center of the storm) at 50 to 150 miles from the storm center. Seeding of such a rainband may pro- duce a dispersion of the energy of the hurricane over a larger area and should provide information and data needed to improve the design of other modification experiments. The rainband experiment provides data needed for studies of cloud inter- actions. A rainband can be selected that is well removed from the central vortex area and not obscured by the main cloud system of the hurricane. This selection facilitates visual observations.

The Advisory Panel has recommended that cloudline ex- periments continue to be conducted in order to collect data vital to the understanding of the dynamics of clouds organized into systems such as rainbands. These experiments can be con- ducted when there are no hurricanes and should provide addi- tional opportunities for evaluation of seeding effects. Dur- ing these experiments, tests of various seeding agents and dispersing techniques can also be conducted. Cloudline ex- periments were scheduled for 24-31 July 1970, in the military operational areas near Puerto Rico.

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FIELD OPERATIONS

Dry-runs were conducted from the Naval Station Roose- velt Roads, Puerto Rico, on 21 and 23 July, following a gen- eral briefing on 20 July. Participating in the dry-runs were aircraft from the Navy Weather Reconnaissance Squadron FOUR (VW-4), NAS Jacksonville, Florida; NOAA's Research Flight Facility, Miami, Florida; Marine All-Weather Attack Squadron Two Two Four ( VMA-AW-224 ) , MCAS Cherry Point, North Carolina; Air Force 53rd Weather Reconnaissance Squadron, Ramey AFB, Puerto Rico; and the 55th Weather Reconnaissance Squadron, McClellan AFB, Sacramento, California.

Also taking part were scientists from the Naval Weather Service Command Headquarters, Washington, D.C.; Naval Weapons Center, China Lake, California; Fleet Weather Facility, Jacksonville, Florida; Navy Weather Research Facility, Norfolk Virginia; University of Miami, Coral Gables, Florida; and NOAA's National Hurricane Research Laboratory, Coral Gables, Florida.

Dry-run exercises for the STORMFURY eyewal 1 experiment were conducted on 21 July and for the rai nsector/ rai nband ex- periment on 23 July. Extensive individual debriefs of each flight were made followed by a general critique covering the total operations after each experiment.

A series of cloudline type experiments were carried out at the conclusion of the dry-runs with a portion of the forces. (The Marine A-6 aircraft, the Air Force WC-135, and two of the Navy WC-121N's were released.) Flight opera- tions were carried out on 24, 27, 28, 29, 30, and 31 July, utilizing three types of seeding aircraft (Cessna 401, DC-6, B-57). See appendix I for report on the Cessna 401 opera- tions.

The DC-6 was used on the last three operating days to

seed with various silver iodide compositions generated from

a burner attached to the wing. A report on these operations is included as appendix E.

On 19 August, Tropical Storm Dorothy developed east of the Caribbean Sea and was predicted to move into the Car- ibbean on the 20th. In anticipation that the storm would either intensify into a hurricane or remain stable enough in intensity as a tropical storm to serve as a fit subject for a STORMFURY monitoring mission, the forces (with the exception of seeder aircraft) were requested to deploy to Puerto Rico on 20 August. The monitoring mission was to include the flight patterns used to monitor a seeded hurri- cane. These data collected in an unseeded storm were to be used for comparison purposes and for research on the natural variability of storms.

The Research Flight Facility flew a three-plane mis- sion of the monitoring type on 21 August, and the other pro- ject aircraft (less seeders) arrived for the major effort on Saturday, 22 August.

After crossing Marti slowly. On Friday, the 21s culation, but the Research difficulty orienting their weak center. By Saturday, to a tropical wave with max STORMFURY monitoring missio research flight mission whi on a tropical wave. These able for studying the struc of this type have been extr

nique, Dorothy started weakening t, there was still a closed cir- Flight Facility aircraft had flight patterns about the broad the 22nd, the storm had reverted imum winds of about 45 knots. The n was then changed to a fall-back ch collects data at several levels data should prove to be \/ery val u- ture of easterly waves, for data emely rare in the past.

Forces performed in an outstanding manner throughout the dry-run exercises, the cloudline experiments, and the Tropical Storm Dorothy operations. The fall-back exercise gave the first opportunity to work with all three of the Air Force participants (WC-130, WC-135, RB57F) . Several problems were found in data collection and were resolved as a result of experience gained during these operations.

RESEARCH ACTIVITIES

Progress in the hurricane modification work was quite considerable in 1970 even though nature did not provide a suitable hurricane for a field experiment. This progress was due to the efforts of the research workers, and their find- ings provide a much broader and firmer base for the future work of the Project. This research took place primarily at the National Hurricane Research Laboratory, Coral Gables, Florida; the Navy Weather Research Facility, Norfolk, Vir- ginia; and at cooperating Universities. Appendices B through L are reports on some of these STORMFURY research efforts.

Appendix B "A hypothesis for modification of hurri- canes," by Drs. R. C. Gentry and H. F. Hawkins, explains the new hypothesis on hurricane modification experiments that was developed this year. The article summarizes the evolu- tion of ideas concerning the use of freezing nuclei for mod- ifying hurricanes, explains how the new hypothesis accounts for the apparently favorable results from the experiments on Hurricanes Esther (1961), Beulah (1963), and Debbie (1969), and discusses some of the questions concerning hurricane modification which still need to be answered either by the theoretical investigations or by the field experiments.

Appendix C "Hurricane modeling at the National Hurri- cane Research Laboratory, 1970," by Dr. S. L. Rosenthal, re- views the NHRL's more significant achievements in the general area of time-dependent hurricane modeling. Dr. Rosenthal dis- cusses the specific problem of modeling a Debbie-like field experiment and summarizes efforts less directly related to the development of time-dependent models. He also outlines inves- tigations planned by this group for the next few years.

Appendix D "Summary of the preliminary results from an asymmetric model of the tropical cyclone," by Dr. R. A. Anthes, Dr. S. L. Rosenthal, and J. W. Trout, shows that the asymmetri- cal hurricane model reproduces many observed features of the three-dimensional tropical cyclone. Realistic portrayals of

10

spiral rainbands and the strongly asymmetric structure of the outflow layer are obtained. The kinetic energy budget of the model compares favorably with empirical estimates and also shows the loss of kinetic energy by truncation errors to be s/ery small. Large-scale horizontal asymmetries in the out- flow are found to play a significant role in the radial trans- port of vorticity during the mature stage and are of the same magnitude as the transport by the mean circulation. In agree- ment with empirical studies, the outflow layer of the model storm shows substantial areas of negative absolute vorticity and anomalous winds.

Appendix E "Response of STORMFURY cloudline cumuli to Agl and Ag I N a I ice nuclei from a solution-combustion genera- tor," by E. E. Hindman, II., Dr. S. D. Elliott, Jr., Dr. W. G. Finnegan, and B. T. Patton, studies the responses of cumulus clouds to silver iodide seedings during the 1970 STORMFURY cloudline operations and compares the effectiveness of two different silver iodide solutions burned in a solution- combustion generator.

Appendix F "Measurements of vertical motion in the eyewall cloud region of Hurricane Debbie," by Dr. T. N. Carlson discusses the estimates of cumulus cloud vertical motions re- corded by an RFF DC-6 aircraft while flying in Hurricane Debbie. The accuracy of the vertical motions obtained is dis- cussed, and various factors which may affect the accuracy are explained.

Appendix H "Ice phase modification potential of cumulus clouds in hurricanes," by D. A. Matthews, presents an examina- tion of ice-phase modification potential of cumulus clouds. Predicted results of modification potential by a one-dimensional steady-state cumulus model are used to test the suggestion (Gentry, 1971) that an important effect on hurricanes may be realized by seeding the less fully developed cumulus cells that are located slightly outward from the mammoth clouds in the inner eyewall. Mr. Matthews's paper also describes the decreases in surface pressure, the increases in rainfall, and the increases in cloud top height as derived from model simu- lation of the ice-phase modification. In the calculations, he uses 87 temperature soundings observed within 100 n miles of hurricane eyes and five average hurricane soundings pre- pared by Sheets (1969) .

11

Appendix I "Use of light aircraft in STORMFURY activi- ties," by Dr. S. D. Elliott, Jr., and Dr. W. G. Finnegan, describes the use of contractor-operated light aircraft in Project STORMFURY dry-run and cloudline experiments and offers conclusions and recommendations involving the use of light aircraft in future STORMFURY activities.

Appendix J "Use of echo velocities to evaluate hurri- cane modification experiments," by P. G. Black, examines radar echo velocities computed over the entire storm for six time intervals before and during the seeding of Hurricane Debbie on 20 August 1969. He finds that mean echo speeds equaled or exceeded cycl os trophi c winds computed from 12,000- ft D-value data as well as measured 12,000-ft winds after a correction for water motion was applied to the original "Doppler winds." Mr. Black further examines mean echo cross- ing angles to determine their variations and angular rotation in relation to the storm's major and minor axes.

Appendix K "A summary of radar precipitation echo heights in hurricanes," by H. V. Senn, surveys radar height data and hurricane case histories to determine likely occur- rence of clouds that can be significantly modified in various sectors of a hurricane. This information suggests that clouds exist in hurricanes of the type that the new hypothesis (app. B) suggests are needed in the hurricane modification work.

Appendix L "Project STORMFURY experimental eligibility in the Western North Pacific," by W. D. Mallinger, updates and reviews numbers of typhoons eligible for Pacific STORMFURY experiments. This study strongly indicates that both Guam and Okinawa must be available as bases for Project forces in order to expect a profitable number of experimental storms during a 3-month operation.

OPERATIONAL AND RESEARCH DATA COLLECTION

Data collection procedures appeared adequate for the Project. While problems with radar still existed on some of the Project aircraft, continuous efforts were made during the season to improve these observational tools.

Two special Polaroid cameras (CU-5) were purchased and modified for use on the Air Force WC-130 aircraft radar. Al- though automatic time-lapse radar cameras are preferred, the Polaroid cameras produced good research data where none had been previously available from these aircraft.

12

The Research Flight Facility conducted several research missions in tropical circulations, but the 1970 hurricane sea- son was generally one in which few good data collection op- portunities occurred.

A one-plane mission was flown into Hurricane Ella in the far southwest Gulf of Mexico on 11 September.

A three-plane, five-level mission was flown into Trop- ical Storm Felice on 15 September. Felice was almost up to minimal hurricane force, and wind gusts as high as 64 knots were noted as it passed to the south of the Mississippi Delta regi on .

A three-plane, five-level mission on 2 October and a two-plane mission on 3 October were flown in Tropical Depres- sion No. 14 as it passed through the eastern Caribbean.

Processing of STORMFURY films was again accomplished at a commercial firm in Miami. Some experiments in reducing costs by obtaining work prints to satisfy requirements for duplicates were attempted, but technical difficulties in processing were encountered. These difficulties are now be- lieved to be surmounted, and a modified version of this pro- cedure will be tried during the 1971 STORMFURY season.

OUTLOOK FOR 1971

Project STORMFURY operations are expected to be \/ery similar to those planned for 1970. It is likely that the dry-run exercises will be conducted from the Naval Station Roosevelt Roads, Puerto Rico, followed by a series of cloud- line experiments with forces based at Barbados.

Continued emphasis will be placed on repeating the "Debbie" type experiment and conducting monitoring missions in unseeded storms for comparisons purposes.

Project aircraft will be essentially the same as in 1970, except that a WP-3 weather reconnaissance aircraft be- longing to Navy Weather Reconnaissance Squadron FOUR (VW-4) is expected to participate in STORMFURY missions for data collection and for additional use and evaluation as a seeder aircraft.

13

REFERENCES AND SPECIAL REPORTS

Anthes, R. A., S. L. Rosenthal, and J. W. Trout (1970): Num- erical simulation of a hurricane. Proceedings of the Meteorological Technical Exchange Conference t 21-24 September, Annapolis, Md., U.S. Naval Weather Service Command.

Anthes, R. A. (1971): The response of a 3-level axisymmetric hurricane model to aritificial redistribution of con- vective heat release. Technical Memorandum ERLTM-NHRL No. 92, NOAA, Dept. of Commerce, NHRL , Miami.

Black, P. G. , and T

T. Fuji ta Debbie as

of Hurricane Debbie as reve ocities from airborne radar

Proceedings of the 14th Ann

(1970): In- and outflow field evealed by echo and cloud vel- dar and ATS - 1 1 1 pictures.

Annunl. P. nrt ■?£>. Y>an r> a nn 'Rnrlny

al Conference on Radar

Black,

Meteorology , Tucson, Ariz. November, pp. 353-358.

P. G., H. V. Senn, and C. L. Courtright (1971): Some airborne radar observations of precipitation tilt, bright band distribution, and eye configuration changes during the 1969 multiple seeding experiments in Hurri- cane Debbie. Submitted for publication in the Monthly Weather Review.

Carlson, T. N., and R. C. Sheets (1971): Comparison of draft scale vertical velocities computed from gust probe and conventional data collected by a DC-6 aircraft. Tech- nical Memorandum ERLTM-NHRL No . 91, NOAA, U.S. Dept. of Commerce, NHRL, Miami, Fla.

Gentry, R. C. (1970): Progress on hurricane modification re- search - October 1969 to October 1970. Presented at

the Twelfth Interagency Conference on Weather Modifi- cation;, October 28-30, Virginia Beach, Va.

Gentry, R. C. (1970): Hurricane modification - Experiments and prospects. Presented at Hurricane Foresight Con- ference,, New Orleans, La., April 30, and distributed by the New Orleans States-Item.

Gentry, R. C. (1970): Modification experiments on Hurricane

Debbie, August 1969. Proceedings of the Second National Conference on Weather Modification^ American Meteorolo- gical Society, pp. 205-208.

Gentry, R. C. (19 70): The hurricane modification project:

Past results and future prospects. Proceedings of the Seventh Space Congress^ April 22-24, Cocoa Beach, Fla.

14

Gentry, R. C. (1970): Modifying the great storm on earth --

the hurricane. Underwater Science and Technology Jour- nal, December, pp. 204-214.

Gentry, R. C. (1971): To tame a hurricane. Science Journal, 7, (1), January, pp. 49-55.

Gentry, R. C. (1971): Hurricane. McGraw-Hill Yearbook of Science and Technology , pp. 232-234.

Hawkins, H. F. (1971): Modifying the hurricane. Submitted

for publication in UMSCHAU (German publication), April.

Hawkins, H. F. (1971): Comparison of results of the Hurricane Debbie (1969) modification experiments with those from Rosenthal's numerical model simulation experiments.

Monthly Weather Review, 99, (5), May, pp. 427-434.

Mallinger, W. D. (1970): Project STORMFURY operations and plans. Mariners Weather Log, 14, (5), September, pp. 262-266.

Underwood, L. J. (1970): Project STORMFURY operations 1970.

Presented at the Twelfth Interagency Conference on

Weather Modification, October 28-30, Virginia Beach, Va.

15

APPENDIX A

REPORT ON MEETING OF PROJECT STORMFURY ADVISORY PANEL

Miami, Florida

29-30 September 1970

INTRODUCTION

In response to the recognition of the increasing im- portance of computer simulation of both "natural" and "seeded" hurricanes to the interpretation and design of Project STORM- FURY field experiments, the Advisory Panel met at NHRL on 29-30 September to undertake a more intensive evaluation of models developed by Rosenthal and colleagues at NHRL. From this assessment, several conclusions and recommendations emerged .

EVALUATION OF HURRICANE MODELING

Results of computer simulations of natural hurricanes were available from two models: the improved symmetric (two- dimensional) model with explicit water cycle and air-sea en- ergy exchanges and better horizontal resolution of 10 km, as well as preliminary results from a simplified asymmetrical (three-dimensional) model which neglects interaction with the environment, has constant Coriolis parameter, and rather coarse vertical and horizontal resolution. Simulation of seeded hurricanes was carried out solely with the use of the symmetrical model. Varying augmented heating rates were applied at different radial increments both continuously and intermittently for 10 hours in an attempt to simulate the multiple eyewall experiment of Project STORMFURY.

From a study of these results the Panel reached the following conclusions:

(1) Within the limitations imposed by symmetry and convective parameterization, the simulation of the natural hurricane is impressively realistic. The distributions of temperature, pressure, and horizontal and vertical motion of the model storm compare favorable with those observed in typical mature hurricanes in nature.

(2) Within the limitations of the simple asymme model given above, plus the recognition tha asymmetry is introduced artificially by rou errors and boundary geometry, an asymmetric structure develops in a manner and with a s that is not unrealistic. When averaged in azimuthal direction, the structure is suffi similar to the symmetrical analog to give i confidence in the validity of the symmetric The favorable comparison of model storm str with observation lends credence to the simu of seeded hurricane structure. In spite of realistic simulation of hurricane structure Panel noted that neither the symmetrical no asymmetrical model is able to give any info on the effects of internal or external infl on the motion of natural or seeded hurrican

(3) The essential result which emerges from the ing simulation is the formation ot a new wi imum and zone of strongest upward motion at greater radius than those existing in the n model storm if the augmented heating rate i outside these pre-existing maxima. Only mi differences in this essential result appear experiments with different augmented heatin at di f f eren t radi i .

(4) This new wind maximum which forms in the se storm is weaker than the model control by a 10 percent. Larger reductions of wind spee at the radius of maximum wind of the contro and smaller increases occur at radii beyond new maximum. The decreases in wind speed a sociated with decreased horizontal temperat gradients in the upper and middle troposphe weakened surface pressure gradients togethe the fact that inflowing air rises at a grea radius, thus acquiring smaller tangential r momentum. The augmented heating also incre the static stability which is associated wi smaller rates of release of latent heat and version of available potential to kinetic e

(5) Evidence from available simulations has, so always indicated that seeding at radii outs the original wind maximum results in reduct the maximum winds. However, the augmented associated with the simulated seeding resul an increase in the total kinetic energy of hurricane winds by about 20 percent. Since could result in a significant increase in t

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ci rcumstances , ing rates used

RECOMMENDATIONS

Based upon the above conclusions, the Advisory Panel makes the following recommendations with regard to Project STORMFURY:

Recommendation ONE: More detailed diagnostic studies of existing simulations of seeding should be carried out to verify the tentative conclusions reached above as to the mech- inisms of the seeding influences. In particular, other quan- tities than those now available should be studied with greater time resolution.

Reasons: It is essential to understand the seeding simulations in as great detail as possible to gain confidence in the results and for comparison with field experimental re- sults.

Recommendation TWO: Development of the asymmetrical (three-dimensional) model should be continued with the ulti- mate objective of modeling the nons tationary hurricane as it moves through and interacts with the larger scale environment. When this has been achieved for natural storms, simulation of seeding should be carried out.

Reasons: Only with such a model it is possible to in- vestigate interactions between the hurricane and its environ- ment and remove the constraint of axial symmetry. Furthermore, simulation of seeding in only one sector of the storm will be possible, as well as investigating the possible effects of seeding on the motion of hurricanes.

A-3

Recommendation THREE: Further simulations of seeding should be made with the symmetrical (two-dimensional) model to supplement the diagnostic studies of existing seeding simulations recommended above.

Reasons: Additional information on varying augmented heating rates and radii of seeding is needed. It is also anticipated that the diagnostic studies will reveal points in need of further clarification.

Recommendation FOUR: The resources of the computer simulation group under Dr. Rosenthal at NHRL should be aug- mented by: (a) two Ph.D. level scientists with appropriate qualifications, and (b) computer facilities of greater speed and capacity.

Reasons: Although excellent progress has been made by this group in the past 2 years, the experiments recommended above will require additional personnel and computer facili- ties to accelerate this rate of progress in the next 2 years.

Recommendation FIVE: Available radar data should be studied in an attempt to verify the existence of convective clouds just outside existing eyewalls with a structure sus- ceptible to enhanced growth through seeding. Results from Hurricane Debbie should be reviewed once more from this point of view.

Reasons: If verified, the existence of such clouds and their enhan cement by seeding would provide a sounder hypothesis for STORMFURY field experiments.

Recommendation SIX: Radar and cloud physics instru- mentation on the research aircraft should be further improved to give more quantitative information on the distribution of convective and other clouds and all phases of water in the hurricane.

Reasons: The essence of possible modification of hur- ricanes rests in the questions of influencing the intensity and organization of convection and the associated phase changes of water. Unless more and better data can be acquired on these questions, residual doubt will always remain in the interpretation of experimental results.

Professor Noel E. LaSeur, Chairman Dean Charl es L . Hosl er Professor James E. McDonald Professor Edward N. Lorenz Professor Jerome Spar

10 November 1970

A-4

RECOMMENDATIONS OF THE ADVISORY PANEL FOR PROJECT STORMFURY

Washington. D.C. February, 1971

INTRODUCTION

In the course of the meeting of the Advisory Panel for Project STORMFURY held in Washington, D.C, 28-30 January 1971, two aspects of Project activities emerged which need immediate action if necessary planning is to be accomplished. These are: the proposed operations of Project STORMFURY in the Pacific during the summer of 1972; and the acquisition, outfitting, and testing of alternate seeding aircraft. Be- cause of the immediacy of these problems, the Advisory Panel is issuing these recommendations; further recommendations on other aspects of Project activities discussed will be forth- coming.

pri a the ci a t typh s umm

expe quen ocea to m reas Paci cane

R

te a f i na ed w oon er o R ri me cy o ni c ove on t fie s .

eaomme g e n c i e n c i a 1 , i th pr region f 1972 easons n ts to f Paci regi on Pro jec o be 1 i typhoo

ndation ONE: The Panel re s of the government intens

logistic, diplomatic, and oposed operations of Proje

of the Western North Paci

The increased opportuni be expected from the typi

fie typhoons in a large, s fully justify the expense

t operations to that area.

eve that experimental resu

ns will be completely vali

commends that appro- i fy efforts to sol ve other problems asso ct STORMFURY in the fie Ocean during the

ties for STORMFURY cal ly greater fre- parsely populated and effort requi red There is every Its obtained in d for Atlantic hurri

Recommendation TWO: The Panel recommends that Project STORMFURY continue efforts to acquire, outfit, and test alter- nate seeding aircraft with the following capabilities: in- creased capacity to carry Project personnel and seeding pyrotechnics; increased range and time "on-station" in the storm; and capability to seed at levels in the range from 25,000 ft to 30,000 ft or at lower levels if suitable temp- eratures for seedings exist.

Reasons: The Panel considers it undesirable for the Project to have to rely on seeder aircraft from external units. In the past, available aircraft have lacked capacity for Project personnel to fly on-board, and thus provide better

A-5

control of the time and place of seeding. They have also lacked range, capability for mulitple seeding without refueling, and were limited to high altitudes. Acquisition by the Pro- ject of aircraft with the recommended capabilities could eliminate significant uncertainties inherent in the presently available planes.-

Professor Noel E. LaSeur, Chairman Dean Charles L. Hosier Professor James E. McDonald Professor Jerome Spar

A-6

APPENDIX B

A HYPOTHESIS FOR MODIFICATION OF HURRICANES

R. Cecil Gentry and Harry F. Hawkins National Hurricane Research Laboratory

INTRODUCTION

The encouraging results from the Hurricane Debbie mod- ification experiments of August, 1969 (Gentry, 1970a) have stimulated research on many problems related to hurricane modification experiments. One of the more interesting devel- opments during 1970 was a new hypothesis which accounted for results from the "Debbie" experiments and offered a more ac- ceptable rationale that details how seeding a hurricane can cause a reduction in its maximum intensity.

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the c was an tic mo tint ng eff pothes age re

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ef fee del , h he sto ects c ized t ducti o

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1 aten atures lid on cul ate ght be be con his wo the ma

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1 developed by S. L, Rosenthal periments relative to the mod- 69). In these experiments, ted by assuming that the seed- ting of the seeded clouds ture at the rate of 2°C per h eeding was simulated by in-

a specified volume of the dded at 500 mb and 300 mb ,

artificial freezing nuclei zing of significant amounts n made with the model to

determine in which portion of the storm addition of heat would most likely result in reduction of the maximum winds; in an: (1) annular band radially inward from the maximum winds, (2) annular band spanning the radius of maximum winds, or (3) an- nular band radially outward from the radius of maximum winds. The answer from the model was that reductions were most likely when the heat was added radially outward from the maximum wi nds .

Based on these experiments with the model, crude as they were, the seeding pattern for the experiment was rede- signed. Formerly, the seeding aircraft crossed the eye of the hurricane and started dropping the pyrotechnic silver iodide generators at the inner edge of the eyewall. The run continued radially outward for 15 to 25 miles (Simpson and Malkus, 1964a). Prior to the 1969 hurricane season, this pattern was altered to have the run start about 3 miles radi- ally outward from the inner edge of the eyewall (past the ring of maximum winds) and continue on for 15-25 miles. This meant a relatively small change in the annular band seeded be- cause there was about an 85 percent overlap in this pattern and the one used in the earlier seeding runs on hurricanes.

Debbie was seeded five times at 2-hour intervals on 18 August 1969, and again on 20 August (Gentry, 1970b). The operational plan called for the seeding runs to be from the radius of maximum wind outward for 15-25 miles (the spread was somewhat a function of the reaction time of the man in the seeder aircraft and the turbulence encountered). When operations are conducted, it is frequently difficult for the Project Director in the command-control aircraft to know the exact location of the radius of maximum winds, but he does have a good radar picture of the hurricane. R. Sheets, Na- tional Hurricane Research Laboratory, has studied the flight data collected by the Research Flight Facility and the Na- tional Hurricane Research Laboratory during the last 14 years, and has concluded that in mature hurricanes the most likely radius for the maximum winds was 2 or 3 miles radially out- ward from the inner edge of the eyewall (as seen by radar)1.

By the time of the Debbie experiments, S. L. Rosen- thal had made several improvements in the hurricane model. The encouraging results from the field experiments put much greater emphasis on all phases of the research effort, and a new series of experiments simulating the modification effects were made with the more sophisticated model (Rosenthal, 1970).

Personal communication

B-2

The new experiments also simulated the modification experiment by assuming that seeding would add heat to the clouds. It was again found that a reduction in maximum winds was most likely if the heat was added radially outward from the radius of maximum winds. Several variations were run in which changes were made in the intensity of the enhanced heat- ing function, in the radial bands at which it was applied, and in the length of time of application. There were also experiments to consider whether the heating should be applied continuously or in pulses to simulate the multiple seeding ex- periments conducted on Debbie.

In general, the results showed that a reduction in maximum winds was most likely if the heat were added radially outward from the radius of maximum winds. They also showed that there was little difference in the reactions between heat added continuously and heat added in pulses. Larger amounts of enhanced heating caused quicker responses in the wind field, but eventually the reduction in maximum winds became about the same. There did seem to be a lower limit to the rate at which heat should be added below which no sig- nificant change in the maximum winds occurred within 10 to 20 hours (Rosenthal , 1971 ) .

During the 1968, 1969, and 1970 seasons, the National Hurricane Research Laboratory with the assistance of the Re- search Flight Facility of NOAA made some measurements of the liquid- and solid-water content of hurricane clouds (Sheets, 1969).

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was con- ed water to account 1 runs t is e x - cts of ti on ti mes , runs

B-3

When the multiple seedings were considered, however, there appeared to be too little supercooled water for the latent heat of fusion to be an adequate sole heat source. Once the liquid in the clouds has been frozen, one cannot keep refreezing it to get more heat. Only by introducing fresh supercooled water into the clouds can one get the addi- tional heat by this mechanism. Simple calculations suggest that heating rates through the release of latent heat of fusion would be 1 to 2 orders of magnitude less than the a- mount calculations with Rosenthal's hurricane model suggest is needed if one is to get significant reductions in the max- imum winds within 4 to 10 hours. In further view of the fact that there appears to be a lower limit below which the heat- ing has no apparent effect, this limited small heat source gave serious concern to the scientists involved.

A new hypothesis for the source of the enhanced heat- ing has been developed. We have reviewed the seeding proce- dures used in the Hurricane Esther, 1969 (Simpson et al . , 1963), Hurricane Beulah, 1963 (Simpson and Malkus, 1964a), and Hurricane Debbie, 1969 (Gentry, 1970a, b) experiments and believe that the changes observed in each of these storms may be accounted for much more reasonably by the new hypothesis than by the original hypothesis. It provides for an improved interpretation of the Debbie results without requiring any drastic revision of the seeding patterns used in the hurri- cane experiments. If this hypothesis is confirmed, however, it will permit changes in the seeding patterns and seeding altitudes to allow more efficient use of the Project aircraft that are likely to be available in future years.

A NEW SEEDING HYPOTHESIS

The new explanation reemphasi zes that the seeding should be done radially outward beyond the tallest clouds in the eyewall and at radii greater than that of either the greatest ascending motion or the maximum winds. The first goal of the seeding with silver iodide crystals is to cause freezing of supercooled water droplets in towering cumulus with tops at temperatures of -5 to -20°C and to release the latent heat of fusion. In the old explanation, the latter was the main reaction expected. In the new explanation, it is the initiation of a bigger reaction, i.e., the trigger that sets off a chain reaction. The latent heat of fusion is expected to increase the buoyancy of the towers to cause greater growth of the ascending plumes in the clouds, and ultimately to result in condensation or sublimation of extra water vapor at the radii of the seeding. Either of the latter

B-4

two processes can release many times as much heat as would be released by merely freezing the supercooled water droplets in the clouds. The stimulation of cloud growth at these radii accomplishes two ends: it allows the clouds to grow verti- cally up into the outflow layer so that air "circulating through this duct" never penetrates to smaller radii, and at the same time it increases the heat release at the radii of seeding. Obviously, air which is thus diverted upward never spirals on into the eyewall and is therefore unable to contri- bute its heat and angular momentum to maintaining the old ring of maximum wi nds .

Thus, one purpose of seeding the clouds outside the old eyewall is to develop a "new eyewall" at a greater radius. If this is accomplished, and most of the air flowing inward ascends at a larger radius, lower maximum wind speeds should result simply from conservation of angular momentum. H. Sundqvist (1970), who has also developed a hurricane model, recently expressed this same idea when he wrote, "Regarding the radial distribution of heating by condensation, we can conclude that the farther from the centre the maximum is, the farther from the centre will the maximum radial wind occur. And from absolute angular momentum considerations it is clear that the earlier (coming from the outside) the inflow ceases the less will the tangential wind be."

A first reaction to this proposal may be, "Hurricane clouds already extend to great heights. How can one make them grow taller?" In the eyewall this may indeed be diffi- cult, but in all other regions it may be quite practical. H. V. Senn (app. K) studied RHI (vertical profiles of radar targets) radar pictures of hurricanes. He found many echoes whose tops were between 20,000 and 30,000 ft. Such clouds occupied much of the outer portions of the hurricane, and there were many even within 5 n miles outward from the inner edge of the eyewall. His data show that more than 50 percent of the echoes within 30 n miles of the center have tops in this range. These data are not adequate support for any strong conclusions, but Senn found nothing to indicate that most echoes in the vital annular ring naturally grew to the top of the troposphere. Thus, current radar data suggest it is possible to make the cumuliform clouds grow sufficiently to cause extra condensation (sublimation) of water vapor in the region where the simulation experiment with the Rosenthal model indicates that application of the enhanced heating function results in the greatest reduction in maximum winds.

Scientists in the Naval Weapons Center at China Lake, California (St. Amand, 1970; Schleusener et al . , 1970), the Experimental Meteorology Laboratory of N0AA (Simpson and Woodley, 1971), Pennsylvania State University (Davis, 1966;

B-5

Davis et al . , 1968) and other groups have all sively that under certain conditions, cumulus ing those in the tropics, can be made to grow and horizontally by seeding and in some cases grow expl os i vely .

shown concl u- clouds, includ- both vertically can be made to

The cloud environment in a hurricane is different from the mean tropical atmosphere, but there are reasons for be- lieving that clouds outside the eyewall in a hurricane also can be made to grow by seeding. R. Sheets (1969a) using the cloud model developed at the Experimental Meteorology Labora- tory (Simpson and Wiggert, 1969) has made computations as to the seedability of hurricane clouds using the mean soundings he developed for different radii (surface pressure) in hurri- canes. Using assumptions considered reasonable, he calculated that cumuliform clouds similar to those found beyond the eye- wall of hurricanes might be expected to grow considerably more than 5000 additional feet after being seeded. D. A. Matthews obtained similar results using a different cloud model ( app . H ) .

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The left side of figure B-2 illustrates the basic fac- tors considered in simulating the modification experiment with Rosenthal's model (1970b). The enhanced heating function was such as to change the temperature at the rate of 4°C hour-1 and was applied at 300 mb and 500 mb . The temperatures do not actually change this much because the extra heat is rap- idly dispersed to other portions of the storm. Considering the levels used in the model and interpolations between levels, this means that the enhanced heating affects the layer between 600 mb and 250 mb or a layer 350 mb thick.

B-6

■x*v,

M rM

,«Jr •«»-'♦♦ »-«»-«- ».#•*><#> »

*** «MI * %** ~|

v^iar#l 'I * "** s*

Figure B-l. Photo of the rainbands and southern eyewall of Hurricane Debbie, 20 August 1969, taken by the APS-45 (X- Band) radar operating in RHI mode on U.S. Navy Reconnais- sance aircraft . The white line shows 20,000 ft elevation. The tallest echo (about 40 n miles from aircraft) is the eyewa 11 .

Consi t e n d i f unct In th the c The s 5.5 g rel ea cl oud 2000 then woul d

der any ng thro ion c a 1 e repro ol umn ( p e c i f i c

kg"1 o se of 1

buoyan a d d i t i o be 4.5

be sub

vertical column 1 cm2 in cross section and ex- ugh a depth of 350 mb. Then the enhanced heating Is for adding 0.0934 cal sec-1 to this column, duct ion of the radar band just to the right of fig. B-2), some potential for growth is suggested

humidity at the top of the radar echo was about f air. If by seeding, one could initiate the atent heat of fusion and sufficient increase in cy to cause the ascending column to rise about nal feet, the specific humidity at the top would g kg-1. That is, 1 extra gram of water vapor limated or condensed and would release up to

B-7

r(lOOmb)

SIMULATING A HURRICANE MODIFICATION EXPERIMENT

-<200mb)

-(SOOmb)

HURRICANE "DEBBIE" AUGUST 20,1969

AH-.0934 cal./ttc.

AH- H(4*C/hr)

-(SOOfflb)

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AH»L,qj

-4 q "i.37 xlO qmtJfc

Wj-180 cm./»tc.

-(1000 mb

f _ r 50 40 SO 20 iO 0

NAUTICAL MILES from AIRCRAFT

Figure B-2. Radar echoes from the original picture reproduced in Fig. 1 are in the right side of the diagram . The center of Hurricane Debbie was about 50 n miles north-northwest of the aircraft . The eyewall (40 n miles from aircraft) ex- tended higher than 403000 ft (limit of the radars cope) . The left portion refers to calculations of amount of heat that can be released by seeding and to the amount of heat required for modification of a hurricane in the simulation experiment with a theoretical model (see text).

B-8

made of the divergence fields in hurricanes. Obviously up- drafts will be stronger in the clouds in order for the aver- age vertical velocity to be 180 cm sec"1. Since we do not have accurate estimates of the percentage of the area that is covered by the active convective towers, we cannot state pre- cisely what the average updraft speeds will be, but order of magnitude type calculations again suggest values that are in line with observations. Thus, it seems reasonable that the amount of heat required under the assumption of an enhanced heating function sufficient to cause temperature change at rates of 4°C hour-1 can be provided by the latent heat of sublimation (or condensation) if the seeding will cause the clouds to grow an additional few thousand feet.

The U.S. Air Force Air Weather Service will make spe- cial efforts in 1971 to release dropsondes at radii outside the eyewall of tropical cyclones to provide data needed to make more reliable computations of the seedability (differ- ence in height of seeded cloud and expected natural growth of the same cloud) of hurricane clouds outside the eyewall.

Qualitative support is provided by Rosenthal's model- ing results to the idea that adding heat above the freezing level and outside the eyewall can cause a new eyewall to develop at a greater radius. In part of the volume in the model where the enhanced heating was applied, "natural fac- tors" started operating and 13 times as much heat was re- leased in the model computations as was added due to the artificial enhancement of the heating function. For the volume as a whole, the natural enhancement as represented by the increases in enthalphy was approximately 10 times as great as that added by the enhanced heating function (Rosen- thal, 1971). This is further evidence that there is a latent instability present which can be triggered by properly ap- plied heating.

The increased "natural" heating in the model is ex- d by what happened to the vertical motion in the "mod- model hurricane. Initially, the maximum updraft vel- s were located between the 15 and 25 km radii. After hanced heating was applied between radii of 25-45 km, maxima of vertical motion developed there, and within han 10 hours, the original maxima had disappeared. The to the radii of enhanced heating resulted in much r condensation at those radii. Since the total volume

annulus increases when its radii increases, the same al velocity results in a larger total rainfall for the ed storm. A detailed analysis of the vertical motion revealed two maxima for a short period, one at the of the original maximum, and the other at the radii

p 1 a i n e if ied" o c i t i e the en a new less t shift greate of the verti c modi f i fields radi us

B-9

of the enhanced heating function. Eventually the latter be- came the larger, and a new eyewall (or at least the maximum vertical velocity) developed at the greater radii. Once the inflowing air at the low levels started ascending at the lar- ger radii, the calculations with the model indicated a reduc- tion in maximum winds. Winds at the new maximum wind radius were stronger than the old winds at that radius but less than the old maximum winds.

h u r r i c a n Beulah ( i n rough cases , t wall and outwa rd extended about 20 i n g run ward fro 15 to 30 the radi changes p e r i m e n t

xami na es tha 1963) , ly the he see

i n De from t

r a d i a

n mil shoul d m the

n mil i from from t s to t

t i o n of t t have be

and Debb

same rad ding run b b i e star he inner 1 1 y outwa es . The

start at inner e d g e s . This

those us he s e e d i n hose of t

he see en see ie (19 i a 1 b a s tarte ted at edge o rd 14 new hy

a poi e of t

const ed i n g radi he Deb

di ng ded, 69), nd or d at

a po f the to 30 pothe nt ab he ey i t u t e the D i use bi e e

runs that re ve ann the i nt eye n m s i s out ewal s an ebbi d fo xper

made is, E als th ul us . inner about wal 1 . i 1 e s a sugges 5 n mi 1 and even e expe r the i men t .

in the v s ther ( 1 ey were

In the edge of 3 n mile

All see nd most ts that 1 e s radi go outwa smal 1 er ri ment t 1961 and

an ous 961),

al 1 seeded earl i e r the eye- s radially ding runs extended the seed- ally out- rd for change in nan the 1963 ex-

The present plans for the seeding and those used in the Debbie experiment call for the pyrotechnics to produce a curtain of silver iodide crystals from about 33,000 ft down to the freezing level. If the new hypothesis is correct, the seeding might be equally effective if the silver iodide gene- rators produced the crystals from some lower level, for ex- ample, 27,000 ft, down to the freezing level.

QUESTIONS NEEDING BETTER ANSWERS

While the new hypothesis does suggest better answers to some of the questions that have been asked by critics of the hurricane modification experiments, there are still sev- eral questions which have not been adequately answered. A few of these are discussed in the following paragraphs:

(1) The basic question, of course, is, will the modi- fication experiment work and, if so, under what conditions? Thus far we have been seeking answers to this question from the modeling experiments with back-up from information derived from the Hurricane Debbie experiments. While the latest version of the hurricane model does simulate many

B-10

features of hurricanes very well ( Ro developer says it is still in some r crude model. It should not be depen authoritative, and quantitative answ suits to expect from a modification actual hurricane. More experience w sophisticated models is needed.

(2) How do we get the freezing nuclei in they are most likely to produce resu problems here. The first involves g airplane to the right position to pu into the clouds. While pilots are v flying aircraft through hurricanes, them to identify and fly to the port having the strongest updraft and to dide without encountering hazardous The second question is what happens freezing nuclei that are released in ascending current. Presumably, they the storm by the winds. Are they en updraft that they pass or do they sk et al . (1971) and Hawkins and Rubsam data about the radar bright band whi are already many naturally created i hurricane clouds outside of the acti the artificial freezing nuclei that updrafts initially may be mixed with crystals and have little influence o

(3) The most difficult question we have Debbie and earlier experiments is ho results. It is comparatively simple the storm weakens or intensifies. I learn whether the seeding caused the the change was a result of natural f planation for why the seeding should tunities, however, for answering thi a sequence of events which should oc convective clouds present which cont and relatively few natural freezing clouds do not extend to the top of t Seeding these clouds with silver iod grow. (d) When the clouds grow, the creases slightly in the area of the eyewall starts to develop in that ar craft currently assigned to the Proj monitor the clouds and record change the seeded band for several hours to proper times and at rates expected t seeding. If changes occur in con for thesis, this would be very convincin seeding contributed to these changes changes in the wind speed.

senthal , 1970) , i ts espects a rather ded upon for f i nal , ers about what re- experiment on an i th this and more

to the clouds where 1 ts ? There are two etting the seeder t freezi ng nucl ei ery experienced in it is difficult for ion of the cloud drop the silver i o- f 1 i gh t condi ti ons . to the si 1 ver i odi de

a cloud without an

are swept around trained into the next irt around it? Senn

(1968) have presented ch suggest that there ce crys tal s in the ve updrafts . I f so , do not get into the

the natural ice n later developments, had to answer in the w to eval uate the

to determine whether t is difficult to

change or whether orces. The new ex- work offers oppor- s ques ti on . We have cur : ( a ) There are ain supercooled water nuclei. (b) These he hurricane. (c) ide causes them to

temperature in- seeding, (e) A new ea . The radar on ai r- ect can be used to s in the clouds in

see if they grow at o resul t from the mance with the hypo- g evidence that the

and to simultaneous

B-ll

(4) Where does water vapor come from that is (or sublimated) to provide the heat requi the new hypothesis? In the simulation ex made with the Rosenthal model, it was ass the enhanced heat came from releasing the heat of fusion from water already in the In the new version of the hypothesis, we count for new supplies of water vapor bei densed in greater quantities at greater r and this vapor must come either from the the low atmospheric levels, or from some portion of the storm. Anthes (1971) has gated this problem and concluded that the in the maximum winds that the model sugge take place varies greatly depending on th of the water vapor that goes into the gro seeded clouds. S. L. Rosenthal discusses dix C, another method of simulating the s the modeling experiments. Perhaps these peri men ts he is planning will answer this In any case, this is a problem that will much more research on both the hurricane scales of motion and their interactions.

(5) As has already been mentioned, there is a know more about the seedability of hurric That is, can they be made to grow taller by seeding? How numerous are they, how h they grow, what volumes of low-level air divert?

conden red in perime umed t

1 aten vol ume must a ng con ad i i , ocean , m i d - 1 e i nvest

reduc s t s w i e o r i g wing

in ap e e d i n g new ex

quest r e q u i r and cl

sed

nt

hat

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pen- in

ion .

e

oud

need to ane clouds and larger i g h should might they

FUTURE PLANS

The Air Weather Service (USAF) has already issued in- structions to the hurricane hunter squadrons in the Atlantic and Pacific to make special efforts to get dropsonde data from the 300-mb level in tropical cyclones in the annulus, 5 to 40 miles radially outward from the inner edge of the eyewall. These data will make possible more definitive com- putations of the seedability of the hurricane clouds.

The Navy, NOAA, and Air Force aircraft will make extra efforts to get consistent radar coverage not only of experi- mental hurricanes, but also of nonexperimental hurricanes. The latter data will be used for establishing a range of nat- ural variability that can be compared with the changes occur- ring in experimental hurricanes following seedings. The Navy aircraft have radar especially wel 1 -designed for this task. The radar data should also provide more information about the number and location of clouds that have seedability.

B-12

The Research Flight Facility and the National Hurri- cane Research Laboratory will continue their efforts to get more information about the amount and distribution of the liquid- and solid-water contents of the hurricane clouds.

As outlined in appendix C, greatly increased efforts will be devoted to improving the theoretical models of hurri- canes .

Finally, ewery effort will be made to conduct addi- tional modification experiments on hurricanes. These are necessary. No matter how the theoretical models are improved, and no matter how much cloud physics, radar, and other data are accumulated, they in themselves will be insufficient (for the foreseeable future) to determine whether we can modify hurricanes. The final answer will have to come from experi- ments on real storms.

ACKNOWLEDGEMENTS

Many people have contributed to the development of the new hypothesis. Some of these have been referenced in this paper. The first presentation of a preliminary version of the new hypothesis was made by the senior author at a meeting of the STORMFURY Advisory Panel on 29 September 1970. Many improvements in the hypothesis were suggested at that time. Among those participating were Professor Noel E. LaSeur, Pro- fessor Charles Hosier, Professor Edward Lorenz, Professor James E. McDonald, Professor Jerome Spar, Dr. Stanley Rosenthal, Dr. Harry F. Hawkins, Dr. Richard Anthes, Mr. William Mallinger, Mr. Peter Black, and Dr. William Cotton.

This presentation of the hypothesis is the work of the writers and any deficiencies should be attributed to them. If, however, the hypothesis proves to have great merit, credits should be shared with the ones listed above and the many people whose research has been referenced herein.

In addition, credit should be given to the scientists and technicians of the National Hurricane Research Labora- tory (NOAA), Research Flight Facility (NOAA), Navy Weather Research Facility, and the Navy and Air Force Hurricane Hunter Squadrons who collected, processed, and analyzed the data needed to support the new ideas.

B-13

REFERENCES

Anthes, R. A. (1971): The response of a 3-level axi symmetri c hurricane model to artificial redistribution of con- vective heat release. Technical Memorandum ERLTM-NHRL No. 92, NOAA, Dept. of Commerce, NHRL, Miami, Fl a .

Davis, L. G. (1966): Alternation of buoyancy in cumuli. Ph.D Thesis, The Pennsylvania State University, University Park , Penn .

Davis, L. G., J. I. Kelley, A. Weinstein, and H. Nicholson

(1968): Weather modification experiments in Arizona. NSF Report 1 2A and Final Report NSF GA-777, Department of Meteorology, The Pennsylvania State University, University Park, Penn. 129 pp.

Gentry, R. C. (1969): Project STORMFURY. AMS Bulletin, 50, (6) , June, pp. 404-409.

Gentry, R. C. (1970a): Hurricane Debbie modification experi- ments, August, 1969. Science, 1683 pp. 473-475.

Gentry, R. C. (1970b): The hurricane modification project: Past results and future prospects. Project STORMFURY Annual Report 1969, U.S. Department of Navy and U.S. Department of Commerce, Appendix B.

Rosenthal, S. L. (1970a): A circularly symmetric primitive equation model of tropical cyclone development con- taining an explicit water vapor cycle. Monthly

Weather Review, 98, (9) September, pp. 643-663.

Rosenthal, S. L. (1970b): A circularly symmetric, primitive equation model of tropical cyclones and its response to artificial enhancement of the convective heating functions. Monthly Weather Review, 99, (5), May, pp. 414-426.

Schleusener, R. A., P. St. Amand, W. Sand, and J. A. Donnan

(1970): Pyrotechnic production of nucleants for cloud modification. Journal of Weather Modification, 2, (4), May, pp. 98-117.

Sheets, R. C. (1969): Computations of the seedability of

clouds in a hurricane environment. Project STORMFURY Annual Report 1968, U.S. Department of Navy and U.S. Department of Commerce, Appendix E.

B-14

Sheets, R. C. (1969): Preliminary analysis of cloud physics data collected in hurricane Gladys, 1968. Project STOEMFURY Annual Report 1968, U.S. Department of Navy and U.S. Department of Commerce, Appendix D.

Simpson, J., and V. Wiggert (1969): Models of precipitation cumulus towers. Monthly Weather Review, 97 , (7), July, pp. 471-489.

Simpson, J., and W. L. Woodley (1971): Seeding cumulus in Florida--New 1970 results. Science, 17 2, (3979), April 9, pp. 117-126.

Simpson, R. H., M. R. Ahrens , and R. D. Decker (1963): A cloud seeding experiment in Hurricane Esther, 1961.

National Hurricane Research Project Report No. 60, Weather Bureau, U.S. Department of Commerce, Washing- ton , D. C. , 30 pp .

Simpson, R. H., and J. S. Mai kus (1964a): A cloud seeding

experiment in Hurricane Beulah, 1963. Project STORM- FURY Annual Report 1963, U.S. Department of Navy and U.S. Department of Commerce, Appendix E.

Simpson, R. H., and J. S. Malkus (1964b): Experiments in hurricane modification. Scientific American, 211, pp. 27-37.

Simpson, R. H., and J. S. Malkus (1965): Hurricane modifica- tion: Progress and prospects, 1964. Project STORMFURY Annual Report 1964. U.S. Department of Navy and U.S. Department of Commerce, Appendix A.

St. Am and, P. (1970): Techniques for seeding tropical cumu- lus clouds. AMS Second National Conference on Weather Modification, April, Santa Barbara, Cal .

Sundqvist, H. (1970): Numerical simulation of the develop- ment of tropical cyclones with a ten-level model. Part I. Tellus, XXII, Nov. 4, pp. 359-390.

B-15

APPENDIX C

HURRICANE MODELING AT THE NATIONAL HURRICANE RESEARCH LABORATORY (1970)

Stanley L. Rosenthal National Hurricane Research Laboratory

INTRODUCTION

The major achievement of this period has been the de- velopment of a working, asymmetric model of the hurricane (app. D). Substantial progress has, however, also been made in other areas. Brief summaries of these efforts will be given in later sections of this appendix.

Section 2 reviews our more significant achievements in the general area of time-dependent hurricane modeling. Sec- tion 3 reviews the specific problem of modeling a Debbie- like field experiment. Section 4 summarizes efforts less directly related to the development of time-dependent models. Section 5 outlines investigations planned by the group for the next few years .

TIME-DEPENDENT MODELS

(a) The Asymmetric Model: As already noted, progress with this model has been sufficient to warrant a separate discussion (app. D) in this year's annual report. An expanded version of appendix D (Anthes, Rosenthal, Trout, 1970) will appear in the Monthly Weather* Review. A second paper which compares results of the asymmetric model with a symmetric analog of equivalent vertical resolution has also been ac- cepted for publication (Anthes, Trout, and Rosenthal, 1970).

Computing economics dictate rather coarse vertical and horizontal resolution for the asymmetric model. The atmo- sphere's vertical structure is represented by only three layers and horizontal spacing of grid points is 30 km. The radial extent of the computational domain is approximately 435 km. The version used to obtain the results shown in appendix D did not contain an explicit water vapor cycle. Although the model allows azimuthal variations, the hurricane

remains an isolated, stationary vortex on an f-plane similar in fashion to the circularly symmetric models. Like the cir- cularly symmetric models, this model is a theoretical tool with no potential for dealing skillfully with real data.

Despite obvious deficiencies due to the lack of ade- quate resolution, the model reproduces many of the observed asymmetrical features of the hurricane. Realistic portrayals of spiral rainbands are obtained. The anticyclonic eddies of the upper troposphere are reproduced as are the observed areas of negative absolute vorticity and anomalous winds.

Since the preparation of appendix D, the asymmetric model has been generalized to include an explicit water vapor cycle and has been recoded for a staggered horizontal grid. The latter reduces local truncation error without either in- creasing the number of grid points or reducing the spacing between them. A number of experiments have been conducted with the revised model and results even more promising than those described in appendix D have been obtained. These data are now undergoing careful study.

Despite the realism of the creased accuracy obtained through variables, the model continues to quate resolution. Improvement of appears to be economically beyond poss ibi 1 i ty , on at least in the

results and despite the in horizontal staggering of suffer from a lack of ade- the vertical resolution our reach. There is a the other hand, that horizontal resolution, inner core of the hurricane, may be improved

through the use of horizontally variable grids

NHRL

f o rm

spac

This

size

at t

(b)

tran

(c)

fami

asso

i s m

(e)

othe

1 i ne

sour

Tw . On ati on e to syst of a he ce Since sf orm In th liar c i a t e i n i m u The m r han arte ce of

o such g e of the

from a an ortho em posse

gri d el nter of

the var a t i o n , t e 1 i m i t i two-di me d with t m at the a c h i n e p d , the t rms than

d i f f i c u

ri d se ( non- gona sses emen the iabl he d ng c ns io he n

cen rogr rans

the lty

syste Anthe ortho 1 con

the t var array e gri egree ase , nal , on-or ter a ammi n forme

ori g i n ve

ms h s , 1 gona stan foil i es

to d i s

of the squa thog nd m g is d eq i nal ry 1

a ve b 970a) 1 , va t mes owi ng smoot a max

deri v a r i a v a r i a re gr o n a 1 i a x i m u

rel a uati o

equa ong i

een des

is an r i a b 1 e h i n a

charac hly fro i m u m a 1 ved fro bill ty b 1 e gri id. (d ty of t m al ong t i v e 1 y ns do c t i o n s w ntegrat

i g n e d analyt mesh i comput t e r i s t m a mi ong th m an a is e a s d coll ) The he var the b s i mpl e o n t a i n h i c h m ions.

and te i c a 1 t n phys a tiona i cs : n i m u m e boun n a 1 y t i i 1 y c h apses d i s t o r i a b 1 e oundar . On more ay be

sted at rans - i cal 1 space (a) The val ue dary . cal

anged . to the tion grid i es . the non- a

C-2

pose

surr

larg

grid

"tel

wi th

Howe

grid

tral

The

na te

addi

tion

gral

the

form

appe

extr

The s d of a c ounded b er size, s . A de escope"

ref eren v e r , o t h squares core , s advantag s are us t i o n a 1 n s . A fu s are pr equation a t i o n co ar. The emely 1 a

econd typ entral co y ' square The con generate grid w h i c ce to loc er member

increase eem to be es of Kos ed and , h o n 1 i n e a r rther adv eserved t s are exp eff i ci ent

major d i borious .

e of v re of annul struct member h has al for soft rathe more s ' s ap ence , terms antage o with ressed s ( s i m sadvan

a r i a b equal i ' of ion d

of t been ecas t he fa r gra s u i t a proac n e i t h appea

i s t in t i

in f i 1 ar tage

1 e g r i area squar e f i n e s he fam discus ing by mily , dual ly ble fo h are er tra r i n t hat ma me dif 1 ux fo to map is t h a

d (Ko squar e gri

a fa i 1 y i sed i

nume in wh

outw r the that nsf or he hy ss an f eren rm an -seal t mac

ss, 197 e grid d eleme mily of s the f n the 1 ri cal m i c h the ard fro hurr i c C a r t e s i mati on drodyna d momen c i n g e r d v a r i a e facto h i n e c o

0) is el erne nts o

vari ami 1 i i tera ethod

size m the ane p an co terms mi c e turn i rors ble c rs ) d ding

com- nts

f even abl e a r

ture s . s of

cen- robl em o r d i -

nor qua- nte- since rans - o not i s

Numerical tests (Anthes, 1970a; Koss, 1970) indicate that both types of variable grids show promise for the hur- ricane problem. Further tests are planned for both systems.

Two other studies related to the asymmetric model are in progress. It has been suggested that the vertical stag- gering of variables (see app. D) may severely distort the basic C I S K mechanism which drives the model hurricane. While the realism of the results counteracts this suggestion, we are investigating the matter through a linear analysis. The analysis requires solution of a ninth order characteristic equation with complex coefficients. Results are not yet available.

ami ne i nsi g With the c ti me . proce ci rcu 4 and the a all o and 2 bound cul ar wave

Out d i n h t in c i r c u al cul

Asy dure 1 ar . , to symme f the . An ary w vari numbe

put da detai 1 to the 1 arly a t i o n mmetri and by

Both a less tri c s c i r c u excep here w ance n r 4 , o

ta from in an asymme symmetr shoul d es are

the fa of thes er exte tage of 1 ar var tion to ave num ear the ver-al 1

the a attemp tri c s i c in i remai n i ntrod ct tha e ef f e nt , wa

the n i a n c e

this ber 4

bound , is r

symme t to truct ti al

ci re uced t the cts t ve nu umeri is co occur i s mo ary i a ther

trie mo gain gr ure of and bou ul arly through

bounda end to mber 8. cal i n t ntai ned s qui te st sign s quite

i n s i g n

del are b eater phy the model ndary con symme tri c

the i n i t

ries are

excite w a

However

egrati on ,

in wave

cl ose to i f i cant .

smal 1 an i f i c a n t .

ei ng si ca

sto d i t i

for i a 1 i not ve n , du

vi r numb

the

The d, h

ex- 1

rm. ons ,

all zation qui te umber ring tual ly ers 1

outer

ci r- ence ,

C-3

While the growth of the symmetric part of the systems is understandable from earlier work with symmetric models, and while the dominance of wave numbers 1 and 2 over higher wave numbers is empirically reasonable, we would like to know more about the physical mechanisms involved. The investiga- tion involves a program of harmonic analysis in an attempt to understand the behavior of the governing equations in the spectral domain.

(b) The Seven-Level Symmetric Model: The basic de- sign of this model, as well as typical results to be expected, were documented in three reports which appeared during the year (Rosenthal, 1970a, 1970b, 1970c).

The only significant revisions during the past year (and since the experiments discussed in the papers cited a- bove) are concerned with the boundary layer formulation. Whereas air-sea exchanges of sensible and latent heat had been simulated by some rather pragmatic constraints on the Ekman layer temperatures and humidities, these energy ex- changes are now computed explicitly through the bulk aerody- namic method. The constant drag coefficient used in previous experiments has been replaced with Deacon's empirical rela- tionship.

The revised model was used for a number of experiments (Rosenthal, 1970d) in which boundary layer parameters, initial conditions, lateral boundary conditions, and computational domain size were varied.

When the drag coefficient is varied during the imma- ture stage, the response of the model follows linear theory, and growth is more rapid with larger drag coefficients. How- ever, the ultimate intensity reached by model storms varies inversely with drag coefficient. In the mature stage, small decreases of drag coefficient lead to stronger peak winds; but when the drag coefficient is reduced by large amounts, peak winds diminish. In the latter situation, there is in- sufficient low-level convergence to sustain convection in the storm core.

Oceanic evaporation was found to be an essential in- gredient without which immature storms would not develop and mature storms could not sustain themselves. The air-sea ex- change of sensible heat was of lesser importance and only small changes occurred when this energy source was completely suppressed. The relative importance of the air-sea exchanges of sensible and latent heat can be explained rather easily (Rosenthal , 1970d) .

C-4

Comparisons between experiments with open and mechani- cally closed lateral boundaries show these boundary conditions to be extremely important. For computational domains of 2000 km or less, model storms with closed lateral boundaries are less intense than their counterparts with open lateral bound- aries. The intensity of closed systems increases markedly with domain size, while that of open systems varies only slowly with domain size. The experiments indicate that dif- ferences due to lateral boundary conditions might be mini- mized if the computational domain exceeded 2000 km.

Experiments conducted with open lateral boundaries revealed that the structure and intensity of the mature stage of the model cyclone is relatively insensitive to variations in the scale and intensity of the initial perturbation. The time required to reach the mature stage is, however, quite sensitive to these factors.

MODELING AND GUIDANCE FOR PROJECT ST0RMFURY (1970)

Appendix C of the 1969 Project ST0RMFURY Annual Report summarized a number of calculations performed with the seven- level symmetric model in which extremely crude attempts were made to simulate a Debbie-like field experiment. (A revised version of that summary appears in the Monthly Weather Review (Rosenthal, 1970e).) Additional calculations of this type have been carried out during the last few months and provide results which differ in varying degrees from those reported on last year.

Before proceeding with a discussion of these differ- ences, some words of caution are in order. These comments arise from having an additional year of thought and discus- sion devoted to the simulation problem. Rosenthal (1970e) pointed out that the assumption of circular symmetry pre- cluded direct comparisons between model calculations and specific real tropical cyclones. It was our feeling at that time, and it continues to be our feeling, that the model should only be considered representative of some sort of "average" hurricane. We pointed out that real hurricanes are strongly influenced by interactions with neighboring synoptic systems and that these interactions may vary mark- edly in character from storm to storm and cannot realisti- cally be modeled with a symmetric, isolated vortex.

C-5

The calculations discussed in Rosenthal ( additional questions concerning certain aspects In previous reports (Rosenthal, 1970e, for examp shown the model to yield a highly realistic stor during the mature stage. However, since the mod and cannot be tested using real observations as ditions, we cannot examine the model's realism w the time required for it to pass through a serie sients as it proceeds from one slowly varying st Furthermore, Rosenthal (1970d) showed that the t for a model storm to reach its mature stage vari days according to the values of several rather a rameters (see discussion in Time Dependent Model

1970d), raise of the model . le) we have m structure el has not initial c o n - ith regard to s of tran- ate to another ime required ed by several rbi trary pa- s p. C-l).

Both the field experiments and the model simulations involve adding a small perturbation to a mature hurricane with the hope that it will be unstable. Since no clear-cut theoretical path for establishing the model's credibility with regard to small perturbations is at hand, and since we cannot be entirely certain that Debbie's changes were pro- duced by the seeding, the realism of the model's response to artificial enhancement of the heating functions must also remain an open question. This will be discussed later in this section.

A major difficulty with regard to interpretation of model simulations is related to the so-called "new hypothesis" (discussed elsewhere in this report, see app. B). The arti- ficial enhancement of the model heating functions, which was designed on the basis of the old hypothesis, appears, from a conceptual point of view, to be inconsistent with the new hypo the si s .

Under the old hypothesis, the source of this additional heat was attributed to the freezing of supercooled water in the upper tropospheric portions of tall Cb. In the model calculations, this was represented by adding a fixed amount of heat to the upper troposphere over periods of several hours. While valid arguments could be raised concerning the reality of the magnitude of this heat source and the length of time over which it was added, we could at least visualize a clear relationship between the model procedure and the pos- tulated real atmospheric process.

The hurricane could be pictured as a system which con- tinually generates new Cb whose upper tropospheric positions consist of supercooled water. The seeding operation could then be visualized as a process in which this newly generated supercooled water is continually frozen through artificial nucleation. With this view of the field experiment, it is

C-6

not unreasonable to attempt a simulation by adding fixed amounts of heat (intended to be the released heat of fusion) to the upper troposphere at each time step for some period of time .

Under the new hypothesis, however, heat of fusion re- leased through silver iodide nucleation is considered only as a stimulus for increasing the buoyancy of Cb (outward from the main eyewall) which by natural processes would reach only to middle tropospheric levels. Under this hypothesis, the major source of energy for modification purposes is sought in the additional condensation and/or sublimation heating re- leased as the seeded clouds grow to upper tropospheric levels.

The difficulty with a simulation relevant to the new hypothesis is that all model Cb which originate in the bound- ary layer reach upper tropospheric levels by natural proces- ses. This stems from the fact that the model Cb are comprised of undilute ascent. Entrainment is not taken into account. Wit.h the current version of the model, therefore, the eyewall region differs from other regions of the storm in cloud con- centration but not in cloud depth.

vi sua! One ca new hy 1 arger of the moi stu field t i v e 1 y paragr c e i v a b concen this p convec

Si mu ized n , ho po the

than

boun re an exper

shor aph. 1 e an tvati oi nt ti on

1 ati on unl ess wever , sis is

that dary 1 d angu iment , t cl ou

In th al ogue on of of vie is s t i

of th

one a

argue

the s

of the

ayer i

1 ar mo

this ds to e mode to th tall c w has mul ate

e new hypo d o p t s a hi

as fol 1 ow t i m u 1 a t i o n

eyewal 1 i nflow thus mentum to is to be a become tal 1 , where a e field ex 1 ouds at t been accep d becomes

thesis is then not easily ghly philosophical attitude, s. The basic feature of the

of tall convection at radii n the hope of diverting some

reducing the supply of the eyewall region. In the ccomplished by causing rela-

I as described in a previous

II clouds are tall, a con- periment is to increase the he corresponding radii. Once ted, the means by which model rather arbitrary.

The addition of a fixed amount of heat as in Rosenthal (1970e) is only one of many possibilities. Others include arbitrary changes of boundary layer convergence, changes of the humidity patterns, and changes in static stability. Of course, these alterations can also be made in various combi- nations.

While calculations of the Rosenthal (1970e) type can still provide helpful information for Project STORMFURY if properly interpreted, clearly literal comparisons between the calculations and the Debbie experiment are unwarranted. Aside from the arbitrary procedures used to simulate seeding,

C-7

the questions concerning the response time of the model raised earlier in this section must be considered as must the lack of interaction with other synoptic features.

It is abundantly clear that we must strive to provide more direct numerical tests of the new hypothesis. To achieve this end, it will be essential to include entrainment and some simple representation of the more significant mi crophys i cal processes. It may also be necessary to make improvements in the modeling of the interactions between the Cb and hurricane scales. This will be a high priority item for the next year.

I t i n u e . mat ion w di f f eren 1 a t i o n s months . to a rev This rev c o e f f i c i (see d i s dependen reached the diff i n g e n h a series o aspect o

n the These hen c ces o repor Some i s i o n i s i o n ent ( c u s s i ce on until erenc nceme f con f the

meant have ompare f vary ted on of th of th consi 3 x 10 on in wind wi nds es may nt is trol 1 e probl

l me , c and w i d a g a i i ng de

1 ast e s e d i e mode sted o "3) by Sectio speed , appro wel 1 depend d expe em.

al cu 11 c ns t gree year f fer 1 du f re

Dea n 2)

and ach be t ent rime

1 ati ons onti nue each ot have a and th ences a ring t h pi aceme con ' s e . The val ues 50 m se hat mod on the n t s is

of t to p her . ri sen ose p re pr e i nt nt of mpi ri 1 a tte of 3 c-1.1 el re i n i t i pi ann

he ol d rovi de

As not

betwee erforme obably erveni n

the co cal rel r gives

x 10-3

A sec

sponse

al cond

ed to s

type usef u ed ea n the din a 1 1 r i g per ns tan ation a li are ond s to th i t i o n tudy

wi 1 1 con' 1 infor- rl i er ,

cal cu- recent butabl e iod. t drag ship near not

ource of e heat- s. A this

presen the fo i ncrea ing) , ( extre radi al e x p e r i The se 20 km. the he i mum. was at add he radii peri me the ey

To ma ted in rmer a sed at 3 kj-t me hea

i nter

ments )

a-1 eve

Henc

at was

The c

25 km at fro experi nts we ewal 1

ke m

the re b

500 on- l ting val s

and 1 wi e, i

app ente

rad m th ment re a cent

e a n i n g f u

1969 re

riefly s

and 300

sec"1 (

) for 10

sel ecte

35, 45,

nd maxim

n both t

lied at

r of the

i u s . T h

e eyewal

s do not

lso cond

er inwar

1 compa port an ummari z

mb by large h -hour i d were

and 55 urn for he smal radii b

eyewal e small 1 cente

add he ucted i d.

r i s o n s be d those o ed below. 1 kj-ton" eating) , hterval s 25, 35, a

km ( larg the contr I and lav eyond the 1 for the

radii ca r outward at at the n which h

tween t

b t a i n e d

H e a t i

1 sec" 1

and 9 k

at v a r i

nd 45 k

e radii

ol expe

ge radi

sea-1 e

contro

1 c u 1 a t i

wherea

eyewal

eat was

he res

more ng rat

( norm j-ton" ous ra m ( sma

exper riment i expe vel wi 1 expe ons , t s the 1 cent

added

ul ts

recently , es were al heat-

I sec- 1

d i i . The

II radii i ments ) .

was at ri ments , nd max- ri ment herefore , large er. Ex-

f rom

For a discussion of the effect of this change on the typical results to be expected from the model, the reader is referred to Rosentha 1 ( 1 970d) .

C-8

Small and large radii experiments were consistent in showing the development of a new eyewall at 35 km and destruc tion of the original eyewall. A new surface-wind maximum was consistently formed at a radius of 40 km, and the original maximum (at 20 km) was eventually destroyed. In general, the newly formed maximum was about 5 m sec-1 less intense than the original.

for

hour

wi th

howe

wind

trem

lati

gave

al so

radi

2 ho

es ta

face

sec

trem

i n s

arti

stat

tras

stab

arti

- i

With normal heating at small radii3 the time required the new wind maximum to become established was about 8 s. Differences between small and large radii experiments

normal heating were minor. In both of these experiments, ver, prior to the development of the new wind maximum, s stronger than the control were found at all radii. Ex- e heating experiments differed from normal heating calcu- ons only in response time. Extreme heating at large radii

results which differed from extreme heating at small radii

only in response time. With extreme heating at large ij the new surface-wind maximum was established within urs. Extreme heating at small radii required 4 hours to blish the new velocity maximum. Prior to this time, sur-

winds in the modified calculation were as large as 5 m greater than in the control. Application of the ex- e heating rate inside the radius of maximum wind resulted urface wind increases of 3 m sec-1. However, when the ficial heating was terminated, the system recovered to a e close to that of the control within 4 hours. In con- t, the large and small radii experiments reached rather le configurations which were maintained even after the ficial heating was terminated.

While the general evolution of the sea-level winds in the experiments described above was in the sense predicted by either the "old" or the "new" hypothesis, the model's behavior at 700 mb raised some questions. The sense of the 700 mb changes was more or less similar to those changes at sea level. However, the 700 mb responses were more rapid and extreme. The early intensification found at the surface was even more pronounced at 700 mb. The new wind maximum, when formed at 700 mb, was generally more intense than the origi- nal maximum until after termination of the enhanced heating

C-9

original maximum. In the old calculations the displacement was 20 km. In the old calculations, with the normal heating rate, the magnitude and timing of the response were similar for both large and small radii experiments. In the new cal- culations, normal heating at large radii generates the new sea-level wind maximum about 6 hours earlier than does normal heating at small radii. Calculations with the k the normal heating rate at small radii shows an ultimate effect similar to that obtained for the experiments with normal heating. However, approximately 2h days of enhanced heating are re- quired to obtain the effect.

Despite the differences which have been emphasized in the last few paragraphs, the experiments do show a consistent pattern which is useful for the design of field experiments. Enhancement of the upper tropospheric heating functions for a sufficiently long period at radii greater than the eyewall center and surface wind maximum will ultimately produce a new eyewall and a new, less intense, sea-level wind maximum at radii greater than those of the "naturally" occurring features The time required to produce these changes is reduced as the rate of heating enhancement is increased. Application of enhanced, heating from the eyewall center inward or only at the eyewall center will result in stronger winds at sea level. In this case, the eyewall and the wind maximum will remain at the natural locations.

OTHER INVESTIGATIONS

Anthes (1970b) examined the role of azimuthal asymme- tries in satisfying the mean angular momentum budget for the steady-state hurricane.

Anthes (1970c) developed a circularly symmetric model in isentropic coordinates to study the effects of differen- tial heating on the dynamics and energetics of the steady- state tropical cyclone. From specified heating functions, he obtained nearly steady-state solutions for the mass and momentum fields. These solutions were then used to evaluate the available potential energy cycle for the theoretical hur- ricane. The major results of this investigation will appear in the Monthly Weather Review (Anthes, 1970d, 1970e).

Anthes (1970f) examined the problem of truncation error in the calculation of vertical motions at the top of the Ekman layer under an imposed hurricane-like, circularly symmetric press ure field.

C-10

Black and Anthes (1971) constructed detailed wind anal- yses of the outflow layer for four hurricanes and one tropical storm. Harmonic analysis of these data, together with that of the composite storms of Miller and Izawa, shows wave numbers 1 and 2 to account for most of the circular variance in the momentum and kinetic energy fields.

FUTURE PLANS

High priority will be given the development of a more sophisticated cloud representation to be used with the seven- level, circularly symmetric hurricane model so that closer simulations of the "new" STORMFURY hypothesis may be per- formed .

Simulations of hurricane seeding will be carried out with the asymmetric hurricane model during the next year.

Horizontal resolution in the central portions of the asymmetric hurricane model may be improved through recoding for one of the variable mesh systems discussed in Section 2. Beyond this, the next logical step would seem to be removal of the stationary, isolated vortex assumptions. This will be a major step and will increase our computing requirements by an order of magnitude.

We envision a model in which a fine mesh moves with the hurricane center through a coarse mesh on which the large- scale synoptic patterns are forecast. This type of model will not only serve as a theoretical tool but also will have the potential for real hurricane forecasting. Whether or not this potential will ever be realized will, to a major extent, be dependent upon the development of real time observational techniques for providing adequate high resolution initial data (-10 km horizontal resolution) in the hurricane vortex.

To develop such a model, important background investi- gations will be required. The mathematical and physical con- siderations for linking a moving fine mesh with a stationary coarse mesh in the framework of a primitive equation model will require extensive research. The problem of hurricane displacement forecasting by dynamic methods must be reexam- ined. It is not clear whether the characteristic errors of the existing filtered (primarily barotropic) models are pri- marily a result of erroneous initial data or physical simpli- fications.

C-ll

While these problems must ultimately be faced in the real data context, it is our feeling that the most promising start lies with the use of hypothetical initial data and a philosophical attitude similar to that adopted for our earlier work .

REFERENCES

Anthes, R. A. (1970a): Numerical experiments with a two- dimensional horizontal variable grid. Monthly Weather Review* 983 (11), November, pp. 810-822.

Anthes, R. A. (1970b): The role of large-scale asymmetries and internal mixing in computing meridional circula- tions associated with steady-state hurricanes. Monthly Weather Review, 98* (7), July, pp. 521-529.

Anthes, R. Z. (1970c): A diagnostic model of the tropical

cyclone in isentropic coordinates. ERLTM-NHRL Techni- cal Memorandum No. 89, ESSA, U.S. Dept. of Commerce, NHRL, Miami , Fla. , 147 pp.

Anthes, R. A. ( 1 9 7 0 d ) : A numerical model of the steady-state tropical cyclone in isentropic coordinates. Paper accepted for publication in the Monthly Weather Review.

Anthes, R. A. (1970e): Numerical experiments with a steady- state model of the tropical cyclone. Paper accepted for publication in the Monthly Weather Review.

Anthes, R. A. (1970f): Iterative solutions to the steady- state axisymmetric boundary layer equations under an intense pressure gradient. Paper accepted for publi- cation in the Monthly Weather Review.

Anthes, R. A., S. L. Rosenthal, and J. W. Trout (1970): Pre- liminary results from an asymmetric model of the tropical cyclone. Accepted for publication in the

Monthly Weather Review.

Anthes, R. A., J. W. Trout, and S. L. Rosenthal (1970): Com- parisons of tropical cyclone simulations with and without the assumption of circular symmetry. Accepted for publication in the Monthly Weather Review.

C-12

Black, P. G., and R. A. Anthes (1971): On the asymmetric structure of the tropical cyclone outflow layer. Paper submitted to the Monthly Weather Review.

Koss, W. J. (1970): Numerical integration experiments with variable resolution two-dimensional Cartesian grids using the box method. Accepted for publication in

the Monthly Weather Review.

Rosenthal, S. L. (1970a): A survey of experimental results obtained from a numerical model designed to simulate tropical cyclone development. ERLTM-NHRL Technical Memorandum No. 88, ESSA, U.S. Dept. of Commerce, NHRL, Miami, Fl a . , 78 pp .

Rosenthal, S. L. (1970b): Experiments with a numerical model of tropical cyclone development. Some effects of radial resolution. Monthly Weather Review, 98, (2), February, pp. 106-120.

Rosenthal, S. L. (1970c): A circularly symmetric primitive equation model of tropical cyclone development con- taining an explicit water vapor cycle. Monthly Weather Review, 98, (9), September, pp. 643-663.

Rosenthal, S. L. ( 1 9 7 0 d ) : The response of a tropical cyclone model to variations in boundary layer parameters, ini- tial conditions, lateral boundary conditions, and domain size. Accepted for publication in the Monthly Weather Review.

Rosenthal, S. L. (1970e): A circularly symmetric, primitive equation model of tropical cyclones and its response to aritificial enhancement of the convective heating functions. Monthly Weather Review, 99, (5), May, pp. 414-426.

C-13

APPENDIX D

SUMMARY OF PRELIMINARY RESULTS FROM AN ASYMMETRIC MODEL OF THE TROPICAL CYCLONE1

Richard A. Anthes, Stanley L. Rosenthal, and James W. Trout National Hurricane Research Laboratory

The results show that the model reproduces many ob- served features of the three-dimensional tropical cyclone. Realistic portrayals of spiral rainbands and the strongly asymmetric structure of the outflow layer are obtained. The kinetic energy budget of the model compares favorably with empirical estimates and also shows the loss of kinetic energy to truncation errors to be very small.

Large scale horizontal asymmetries in the outflow are found to play a significant role in the radial transport of vorticity during the mature stage and are of the same magni- tude as the transport by the circulation.

In agreement with empirical studies, the outflow layer of the model storm shows substantial areas of negative abso- lute vorticity and anomalous winds.

This report summarizes a more complete version to be pub lished in the Monthly Weather Review in 1971.

INTRODUCTION

cycle o (Ooyama They ha i c s , en the 1 at With th b i 1 i ty , metri c these a h u r r i c a and nea

Axi symme tr f tropical , 1969; Ya v e also y i e r g e t i c s , ent heat r is backgro it is not features o re the upp ne motion, rby synopt

ic numerical models have simulated the life

cyclones with a large degree of realism masaki, 1968a, 1968b; Rosenthal, 1970b). elded valuable insight into hurricane dynam- and the important problem of parameterizing eleased in organized cumulus convection, und, and with ever increasing computer capa-

premature to begin the study of the asym- f the hurricane. Among the more notable of er tropospheric outflow layer, the rainbands

and the interactions between the hurricane ic systems.

To incorporate all of these features in a single nu- merical model is an extremely ambitious goal that will require further investigation. The model developed here represents an isolated stationary vortex and appears to be the logical first step beyond the axisymmetric models. For computational economy, we have limited the model to three vertical levels, a coarse horizontal resolution of 30 km, and a relatively small domain of radius 435 km.

DESIGN OF MODEL

The equations of motion are written in a coordinates (Phillips, 1957) on an f-plane, where f, the Coriolis param- eter, is appropriate to approximately 20°N (5 x 10"5 sec-1)- The equations of motion, continuity equation, thermodynamic equation, and hydrostatic equation are identical to those employed by Smagorinsky et al . (1965) for general circulation studies. The basic equations are given in Anthes et al. (1971a), hereafter referred to as I, and are not repeated here .

STRUCTURE OF THE MODEL

The vertical structure of the model is shown by figure D-la. The atmosphere is divided into upper and lower layers of equal pressure depth and a thinner Ekman boundary layer. The information levels for the dynamic and thermodynamic var- iables (fig. D-la) are staggered according to the scheme used by Kurihara and Holloway (1967).

D-2

The horizontal mesh (fig. vertical structure

D-lb) is rectangular with a uniform spacing of 30 km. The

lateral boundary points approx- °-=o ' ' ' ' ' < ' ' < < ' < < ' imate a circle, and all bound- ary points are contained be- tween radii of 450 and 435 km. CT-* - - *™

All variables are defined at all grid points on the a-sur- faces .

VARIABLE K P(mb)

V.T iv2 225

V,T 2V, 675

THE FINITE DIFFERENCE EQUATIONS

O".* 3 900

V,T 3V2 9575

<t>--v-Q 4 1015

(a) HORIZONTAL STRUCTURE - Northwest Section

«-E»tenor Boundary Point

o-lntenor Boundary Point

-Interior Point

>

The finite difference « > ° ° ° 0 o legend

analogs to the horizontal der- ,11°.°.'.'.

ivatives are similar to those ... °. '.'.'. '.

in Grammel tvedt ' s (1969) scheme * 4 center of end

"B". The vertical portion of \ I '.'.'.'.'.'.'. '.

the differencing scheme is i-

dentical to that of Kurihara « . ! ! .' ! .' '. '.'.'.'.

and Holloway (1967) with the < .

exception that potential temp- ". ° ."!!'.!'.!!! !

erature rather than tempera- . . ......... '.

ture is interpolated where (b)

needed. The details are given _. _ . > . ,. 7. t 3 F%guve D-l. (a) Vertical in-

formation levels; (b) North- For adiabatic, inviscid west quadrant of the hori- flow in a laterally closed do- zontal grid. main with a = 0 at a = 0 and 1,

Kurihara and Holloway showed this system to conserve the fi- nite difference analog to

/ / /V fd + "2 \ VH dadydx. (D.l) x y o L v J

VERTICAL DIFFUSION OF MOMENTUM

Although vertical transport of horizontal momentum by the cumulus-scale motions has been shown to 'be an important element in maintaining the observed structure of hurricanes (Gray, 1967; Rosenthal, 1970b), this effect is not included in the preliminary calculations reported on here. Therefore,

D-3

vertical diffusive and "frictional" effects in this experiment are due to the vertical transports of horizontal momentum by subgrid scale eddies smaller than the cumulus scale. The most important aspect of these terms is the surface drag which produces frictional convergence in the cyclone boundary layer and, therefore, a water vapor supply which controls the param- eterized cumulus convection (Charney and Eliassen, 1964; Ooyama, 1969; Rosenthal, 1970b).

The surface drag is modeled using the well-known quad- ratic stress law, and a constant value of 3 x 10~3 was adop- ted for C[). For the remaining o-levels we use the Austausch formulation with the Rossby-Montgomery formulation adopted for the vertical kinematic coefficient of eddy viscosity, Kz (Smogorinsky et al . , 1965). The details are given in I.

LATERAL MIXING TERMS

After Smagorinsky et al . (1965), the lateral exchange of horizontal momentum by subgrid scale eddies is written

FH<V> =j;

(D.2)

where V

sure

is the horizontal vector velocity, and K|-| is the horizontal coefficient

of

is surface pres eddy vi scosi ty

The formulation ultimately adopted was

Ku = Ci V + C

(D.3)

where Ci = 103 and C2 = 5 x

103m2

sec

_ i

D-4

While this selection was based primarily on the results of numerical tests, the form was suggested by the encouraging results obtained from symmetrical models (Rosenthal, 1970b; Yamasaki , 1968b) which employed upstream differencing of ad- vection terms with forward time steps. This scheme introduces a computational viscosity (Molenkamp, 1968) which is similar to the variable portion of (D.3).

Although (D.3) is not terribly satisfying from a phys- ical point of view, it does afford a useful interim represen- tation of the statistical effect of horizontal interactions between the momentum fields of the cumuli and macroscale. More satisfying formulations are dependent on the success of future theoretical and observational studies of these inter- actions.

The preliminary tests also indicated that adequate results can be obtained if the lateral diffusion of heat is computed with a constant thermal diffusivity (Kj) of 5 x 101* m2 sec-1. The lateral mixing term in the thermodynamic equation was, therefore, expressed in the form

FH(T)

p*K-

/ill + ill\

\3x2 8y2/

(D.4)

where T is temperature.

TIME INTEGRATION

of s

made

Wend

(196

di ab

supe

base

suit

due

this

f req

grav

heat

effe

A elect

betw rof f 6) si ati c rior d on s. P to i t

mode uency i ty w ing. ct.

numbe ing a een t schem mul at ef fee to th i n t u i resum s sev 1 has

i ner ave)

The

r of

meth he us e (Ri ed fo ts in e oth ti ve ably, ere d very t i a - g are p Matsu

experi me o d of t i ual leap ch tmyer rward-ba cl uded , er schem meteorol

the sup a m p i n g o

limited ravi ty w robably no dampi

nts we me i n t -frog and Mo ckward the Ma es tes o g i c a 1 e r i o r i f high v e r t i aves ( overly ng may

re cond eg rati o method , rton, 1

scheme tsuno t ted. T

i n s p e c ty of t

tempor cal res p a r t i c u

exci te , then,

ucted n . Co

the t 967), . Wit e c h n i q his co t i o n o he Mat al f re o 1 u t i o larly , d by t

compe

for th mpari s wo-ste and th h vi sc ue was ncl us i f the suno s q u e n c i n , the the e he d i a nsa te

e purpose ons were p Lax- e Matsuno ous and

cl early on was test re- cheme is e s . Since

high- xternal b a t i c for this

D-5

LATERAL BOUNDARY CONDITIONS

The small domain size and the irregular boundary make the choice of lateral boundary conditions extremely important. Preliminary experimentation showed that realistic results could be obtained for steady-state pressure and temperature on the boundary and a variable momentum based on extrapolation out- ward from the interior of the domain.

LATENT HEAT RELEASED IN ORGANIZED CUMULUS CONVECTION

ment

The basic characteristics of this convective adjust- are summarized as follows:

1. Convection occurs only in the presence of low-level convergence and conditional instability for air parcels rising from the surface.

2. All the water vapor that converges in the boundary layer rises in convective clouds, condenses, and falls out as precipitation.

3. All the latent heat thus released able to the macroscale flow.

4. The vertical distribution of this that the macroscale lapse rate is the pseudo-adi abat appropriate to surface .

Empirical justfication for these characteristics

is made avail- heating is such adjusted towards ascent from the

by Rosenthal (1969)

is presented

The convective adjustment, described above, applies only when the atmosphere is conditionally unstable; i.e., the cloud temperature, Tc, exceeds the environmental temperature, T. In mature hurricanes, however, prolonged and intense cumulus convection substantially reduces parcel buoyancy and lapse rates approach the moist adiabatic. Under these circum- stances, significant amounts of nonconvecti ve precipitation (and, hence, latent heat release) may occur (Hawkins and Rubsam, 1968). Since, in this experiment, water vapor is not explicitly forecast, it is necessary to parameterize this effect

D-6

The parameterization of nonconvecti ve latent heat re- lease under nearly moist adiabatic conditions proceeds as follows. Whenever (Tc - T) < 0.5°C in the middle or upper tropospheric layers, this quantity is arbitrarily set to 0.5°C. Under a nearly moist adiabatic lapse rate, therefore, Tc - T = 0.5°C at both levels, and the latent heat is partitioned equally between the upper and lower troposphere. Therefore, latent heat is released in the column as long as a water vapor supply from the boundary layer is present.

The value of specific humidity, q, in the boundary layer, needed for the evaluation of the moisture convergence, is assumed to be given by

q = mi

nimum <

(0.

90

020

(D.5)

where qs is the saturation specific humidity. The upper boundary of 0.020 avoids excessive moisture values at points close to the storm center in the late stages of development when warm temperatures associated with an "eye" appear.

Finally, the surface humidity and temperature are re- quired to establish the pseudoadi abat appropriate to parcel ascent from the surface.

The surface temperature, T*, is computed by a downward extrapolation from the temperature at level k = 7/2 assuming a constant lapse rate between the dry and moist adiabatic rates. The surface specific humidity, q*, is obtained from q through the assumption that the relative humidity is con- stant in the boundary layer.

AIR-SEA EXCHANGE OF SENSIBLE HEAT

The sensible heat flux at the air-sea interface is as sumed to obey the bulk aerodynamic relationship. It is fur- ther assumed that the heat flux decreases linearly with a until it reaches a value of zero at the k = 3 level. This gives

1 gcpcEi \/[ P

■*(T -T*)

v sea '

e*Qk=7/2 =

, T, >T* sea

T <T* sea-

CD. 6)

D-7

h7^7;

where

time a

to Cd (0.003)

cussed below.

s the sensible heat added per unit mass and / 2 . The exchange coefficient Cf: is taken equal

sea

= 302°K is used for the experiment dis-

INITIAL CONDITIONS

The initial conditions consist of an a xi symmetric vor- tex in gradient balance. The minimum pressure is 1011 mb and the environmental pressure on the lateral boundaries is 1015

mb, yielding a maximum gradient wind of 18 of 240 km.

msec

_ i

at a radius

EXPERIMENTAL RESULTS

The history of the cyclone is summarized by figure D-2 which shows the evolution of the minimum surface pressure and the maximum wind speed in the boundary layer (k = 7/2). Due

P(mb) 1020

MINIMUM SURFACE PRESSURE

1000 -

980 -

960

i i 1

■SYMMETRIC STAGE-

20 40 60 80 100 120 140 160 180 200 220 MAXIMUM SURFACE WIND SPEED

240 260

(a)

r

100 120 140 160

TIME(HOURS)

240 260

(b)

Figure D-2. Time variation of the minimum surface pressure and the maximum surface wind speed.

D-8

to the q a n i z a i ntens bout 4 mai ns poi nt , mum wi of the devel o f 1 ow r

nents versio

subs t i o n a i f i c a 0 hou i n a

a se nd ev

stor pment egi on

Fi gu of th n of

tanti 1 pha tion rs an quasi cond entua m dur of p ). T

re D- e kin poten

al st se" o begi n d, th -stea perio lly e ing t ronou hese

3 sho eti c tial

rength f only s. Hu ereaft dy sta d of i xceeds his pe need a asymme

ws the energy to kin

of the initial vortex, a short "or- 12 hours is needed before steady rricane force winds appear at a- er, the relatively weak storm re- te until about 120 hours. At this ntensi fi cation begins and the maxi-

60 m sec"1. The unsteady nature riod seems to be related to the symmetries (especially in the out- tries are discussed in detail later.

temporal variations of the compo- budget. The sum of, (1) the con- etic energy (C(K)), (b) the flux

10

5 -

' I ' I ' I ' I ' I ' I ' I ' I ' I ' I ' I ' I ' I ' I I I ' I ' I ' I I I ' I ' I i I '

KINETIC ENERGY CHANGE

~ TRUNCATION ERROR

,swg*igacsgBggggw

S5>"

at

ANALYTIC TENDENCY

AK At

OBSERVED TENDENCY

I , i , i , I i

I I I l

i i i i i i i i i i i i i i

0 12 24 36 48 60 72 84 96 108 120 132 144 156 162 174 186 198 210 222 234 246 258 270

TIME(HOURS)

40 -

20-

<

9

^ -20

-40-

-60

I I i I ' I ' I i I i I i I ' I i I ' I i I ' I i I ' I ' I ' I ' I i I i I XJ ' I i I i COMPONENTS OF ENERGY BUDGET

i.i.

12 24

' ' ' '

I ' I

I ' ' ' , l i I i I i l

-V(mix)

'.'.'.'.'

36 48 60 72 84 96 108 120 132 144 156 162 174 186 192 210 222 234 246 258 270 TIME(HOURS)

Figure D-3. (a) Time variation of the observed kinetic energy (Lk/Lt) and the change computed from the kinetic energy equa- tion (dk/dt): (b) Time variation of individual components of the kinetic energy tendency: C(k) is the conversion of poten- tial to kinetic energy 3 B(k) is the flow of kinetic energy through the lateral boundary, H(mix) is the loss of kinetic energy through lateral eddy viscosity , V(mix) is the^ loss of kinetic energy through vertical eddy viscosity and includes the effect of surface drag friction.

D-9

of kinetic energy across the lateral boundary (B(K)), (3) the dissipation due to lateral mixing (H(mix)), and (4) the dis- sipation due to vertical mixing (V(mix)) equals the ''analytic" kinetic energy tendency (3k/9t). Also shown by figure D-3 are the observed rates of change of kinetic energy (Ak/At). The difference between 3 k/ 9 1 and Ak/At is a measure of the trun- cation error and, as figure D-4 shows, this difference is quite small. Furthermore, the individual components of the budget are reasonable when compared to empirical estimates (Hawkins and Rubsam, 1968; Miller, 1962; Pal men and Riehl, 1957; and Riehl and Malkus, 1961).

For purposes of discussion, it is convenient to divide the history of the storm into two stages. From the initial instant until about 120 hours, all features are quite sym- metric with respect to the storm center. During this period, there is neither evidence of a banded structure in the rain- fall (analogous to rainbands in real hurricanes) nor does the

20

o ■** --40

MINIMUM

r r

RELATIVE VORTICITY

SYMMETRIC STAGE-

T

ASYMMETRIC STAGE

-CORIOLIS PARAMETER ( 5X1Q-3 SEC"*)

ll>

20 40 60 80 100 120 140 160 180 200 220

MAXIMUM TEMPERATURE ANOMALY

240 260

o 5 -

UJ

120 140

TIME (HOURS)

160

260

Figure D-4. (a) Time variation of the minimum relative vorti- oity in upper troposphere (level lh) ; (b) Time variation of the maximum temperature anomaly (departure of temperature from the steady-state value at the lateral boundary ) in the upper troposphere (level lh) .

D-10

upper tropospheric outflow show any preference for particular quadrants. We refer to this interval as the "early symmetric stage." After 120 hours, the upper outflow is quite asymmet- ric while the rainfall and vertical motions show distinct pat- terns analogous to the spiral rainbands found in real storms. We refer to this period as the "asymmetric stage." The "sym- metric" and "asymmetric" stages refer to the model calculation only, and, because of the arbitrary nature of the initial con- ditions, are not meant to have direct counterparts in natural storms .

EARLY, SYMMETRIC STAGE OF THE MODEL STORM

A representative view of the structure during this per iod is provided by the data at 84 hours. The region of hur- ricane force winds is \/ery small, extending only about 75 km from the center. Gale force winds extend outward to 150 km. The maximum tangential and radial winds are 34.0 m sec"1 and -19.4 m sec"1, respectively, yielding an inflow angle of a- bout 29 degrees .

^h)

The circulation in the upper troposphere (level shows a fairly symmetric outflow pattern. Cyclonic outflow occurs inside a radius of about 200 km. Beyond 200 km, the circulation is anti cycl oni c , reaching a maximum velocity of about 6 m sec"1 around the outer boundary. The figures are shown in I.

Dynamic (or inert ial) instability of the upper tropo- spheric outflow has been suggested by Alaka (1961, 1962, 1963) and others as a contributory factor in the intensification of tropical cyclones. An approximate necessary condition for this instability is given by

(^H

< o

(D.7)

where | V | is the wind speed, R is the radius of curvature of the streamlines, and ca is the absolute vorticity.

Strictly speaking, this criterion for instability re- fers to horizontal parcel displacements normal, to a stream- line and is derived under the assumption that the velocity and pressure fields are invariant along the streamline. A

D-ll

necessary criterion for a closely related instability is

/8V.

\3r

")GH

< 0

(D.8)

The criterion (D.8) relates to the instability of horizontal symmetric fluid ring displacement in a symmetric vortex.

A third type of dynamic instability is governed by the necessary condition that the radial gradient of the absolute vorticity of the tangential flow have at least one zero. That is, the condition

_9_ 8r

dv

8r

+ f

}••

(D.9)

is satisfied somewhere i.n the fluid system. This is a neces- sary condition for asymmetric (azimuthally varying) horizontal perturbations to be unstable.

metri

Since

s t a b i

t i o n .

i n i t i

cl ose

(maxi

appro

like

waves

round

tial

cl ear

is be

eddy

At t c and

the i

1 i t i e s

On t

al dat

to th mum of xima te pertur

of th -off d symmet

that i n g co vi scos

he in tange n i t i a

do n he ot a sin e cen

an ti ly 34 b a t i o is ty i f fer ry i s the i unter ity.

i ti al nti al 1 dat o t co her h ce th ter o cycl o 5 km. ns in pe ar ences reta nstab acted

i nst , (D. a sat ntri b and , ere i f the ni c r Th i

the e pre , and i ned i 1 i ty

by o

ant, wh 7) and isfy ne ute to (D.9) 1 s a max

storm e 1 a t i v e s shoul azimuth sent in

since, for the

is e i t ther ef

en th

(D.8)

i t h e r

the v

s sat

imum

and a

vort

d fav

al di

the

as a

f i rs

her q

fects

e flow i

become

c o n d i t i

ery earl

i s f i e d e

of cyclo

vorti ci

icity) a

or the g

recti on .

initial

1 ready n

t 120 ho

uite we a

such as

s ne equi on , y in ven ni c ty m t a rowt Si data oted urs , k or tho

arly val en these tensi in th vorti i n i m u r a d i u h of nee w due , sub it i that se du

sym- t.

i n- f i c a e

ci ty m

s of wave- eak to

s tan- s

it e to

Figure D-4 shows the time evolution of the minimum value of relative vorticity in the upper level within 350 km of the storm center. During the initial deepening stage the minimum value of absolute vorticity becomes slightly nega- tive. However, this occurs after the intensification and only over a small region.

D-12

The term (2|V|/R + f) was also evaluated for several times during the first 120 hours. These calculations revealed only small patches of anomalous winds. We, therefore, also feel that the instabilities represented by (D.7) and (D.8) played no significant role in the early symmetric stage of the model storm.

Azimuthally averaged vertical cross sections provide an adequate description of the storm structure during the early symmetric stage. Mean cross sections2 for the tangen- tial wind, radial wind, and the temperature departure at 84 hours are shown by figure D-5. These cross sections reveal a structure \/ery typical of that of a weak hurricane (Hawkins and Rubsam, 1968).

MEAN VERTICAL CROSS SECTION

84 HOURS

TANGENTIAL WIND (M./SEC.)

435

405 435

J I I L

i05 135 165 195 225 255 285 315 RADIUS (KM.)

375 405 435

Figure D-5. Azimuthal mean vertical cross sections for the tangential wind, the radial wind, and the temperature anom- aly at 84 hours. Isotherms are labeled in °C; isotachs are labeled in m sec'1.

The circular averages were computed through linear interpc lation of gridpoint values to a polar grid with a radial in- crement of 30 km and an angular increment of 22.5 degrees.

D-13

The vertical 84 hours shows a nea extends from the cen about -140 mb hour-1 the center. Weak su 180 km. The stronge troposphere (level 5 sec" * ) . These val ue 30 km interval of a

conv the wi th cane ti me i cal fall

time surf vi de The a ma (Col shap wel 1 (Fie

iod

1 ows

deve

a qu

i n w

ly r

The

symm

i n t

a na

ward

outf

beyo

abso

f 1 ow

i n s

pres

lies

comp

ergy

for

The a e r s i o n o e q u i v a 1 e the est Daisy ( is 5.0 es ti mat pattern

F i g u r s along ace i s o b

an adeq minimum x i m u m w i on, 1963 es of th

with ob tcher, 1

The e may be s . After 1 opment asi -stea hi ch the esembl es c i r c u 1 a t e t r i c . he low 1 rrow ri n

in the low beco nd 200 k 1 ute vor

layer i mall are sure, te , rainfa onents o

budget a weak h

verage r f the to nt water i mates m 1958). x ^0lk W es (Anth at 84 h

e D-6 sh one r a d i ars are uate des val ue at nd of 32 ) . The e profil s e r v a t i o 955; Mil

arly sym ummari ze a short (about 2 dy state model s a weak ion is n Air s p i r evel s , a g , and f upper le mes anti m. Howe t i c i ty i s p o s i t i as. The mperatur 1 1 rates f the ki are all u r r i c a n e

motion a rly circ ter to a

(about bsi dence st upwar II) and s appear weak hur

ai nfal 1 tal rele

depth , ade by R The tota . This es and J ours sho

ows surf us from very nea c r i p t i o n 84 hour m sec" l general es agree ns ler, 196

metric p d as fol

period 4 hours)

is reac torm clo h u r r i c a n early ax al s i nwa scends i lows out vel s . T cycl onic ver, the n the ou ve excep

central e anoma- , and th n e t i c en reasonab

t th ul ar bout 0.4

occ d ve reac

rea ri ca

over ase i s 6 iehl 1 re al so ohns ws n

e top regio 180 k m sec" u r s in 1 o c i t i h -230 sonabl ne (Ca

the i of lat 5 cm d

and M 1 ease

compa on, 19 o e v i d

of the n of u m. Ma 1 ) occ

the e es occ

mb ho e for rl son

nner 1 ent he ay"1 w al kus of lat res fa 68) . ence o

ace pressure pro the center of th rly circular, th

of the surface s (995 mb) is qu

boun pward xi mum ur i n nvi ro ur in ur" 1 avera and S

00 km at i n hi ch (1961 ent h vorab Fi nal f spi

f i les e gri ese p press i te r

dary mot vel a r

nmen the

(abo

ges

heet

, CO a c i s c ) fo eat ly w

ly, ral

laye ion t

0 c i t i ing n t bey

mi dd ut 0. over s, 19

mpute

01 umn ompar r Hur at th i th e the r bands

r at

hat

es of

ear

ond

le

7 m

a

71).

d by

to able ri - i s

mpi r- ain-

for various d. Since the rofiles pro- ure field, ealistic for

1030

1020

1010

3). er-

of

>

ned~iooo se-

e . -

Q. 1 "

rd

n

he

t- t

990

980

970 -

960

"I 1 1 1 1 1 1 1 P

RADIAL PROFILES OF SURFACE PRESSURE

84 HOURS 156 HOURS 192 HOURS

J 1 1 1 I I I I

100

200 300 R (KM.)

400

500

le

Figure D-6. Radial profiles of surface pressure along an east-west axis at 843 1563 and 192 hours.

D-14

ASYMMETRIC STAGE OF THE MODEL

and ma begi ns The lo but sh maxi mu extend averag

i n a h occurs about i s typ 1963) .

As sh xi mum

a sec w-1 eve ows an m wind

outwa e angl

In co i g h 1 y

i n tw the ma i c a 1 o

own by th temperatu ond perio 1 inflow i ncrease speed is rd to 80 e of i n f 1

ntrast to asymmetri o quadran in center f many hu

e central press re anomaly (fig d of in ten si fie at 156 hours is d intensity ove now 46 m sec"1 km, and gale fo ow has increase

the symmetric

c fashion (figs

ts, and several

This asymmet

r r i canes (e.g.,

ure, ma s. D-3 a t i o n a

still r that , h u r r i rce win d to 38

inflow, . D-7 a

smal 1 ric nat

Alaka,

ximum w and D-4 t about fai rly at 84 h cane fo ds to 2 degree

the ou nd D-8) eddies ure of

1961 ,

i n d speed, ) , the storm

120 hours, symmetri c , ours. The rce winds 10 km. The s .

tflow occurs

Outflow are located the outflow 1962; Miller,

The vorticity ative absolute vortic sec-1. This is in co hours. These regions in various sectors of havior of the outflow oscillations in the c during the latter por is noted that negativ ture of hurricane out feature of composite

The presence o ticity suggests the p dynamic instability d Since the condition ( since (D.9) is satisf able effect, atte^ntio The quantity, 2|V|/R, In contrast to the ea to coy^er substantial of 2 | V | / R exceed 40 x winds in hurricane ou

at 1 e i ty , ntras are the i s p entra t i o n s e abs f 1 ow mean

f lar resen i s c u s D.8) i ed i n was was rly s areas

io-5

tflow

vel 3/2 shows large regions of neg- with minimum values about -30 x 10~5 t with the vorticity pattern at 84 transient. They form and reform outflow level. This unsteady be- robably related closely to the 1 pressure and maximum surface wind of the computation (fig. D-2). It olute vorticity is an observed fea- (Alaka, 1962) and even appears as a storms ( Izawa , 1 964 ) .

ge va

ce of

sed i

refer

n the

focu

compu

tages

of t

sec

has

_ i

lues of negative absolute vor- one or more of the types of

n the previous subsection.

s to symmetric instability and initial data without notice-

sed on the condition (D.7).

ted for level 3/2 at 156 hours.

, anomalous winds are found

he domain and negative values The presence of anomalous

been documented by Alaka (1961)

The role of dynamic instability in the development of tropical cyclones has been subjected to prolonged debate and will not be discussed in detail here. We merely note that the second period of intensification in this model calcula- tion appears to be related to the development of areas of dynamic instability. If we refer to figure D-9, we note that the minimum vorticity in the outflow layer shows a sudden de- crease at about 100 hours. The second period of deepening (as measured by central pressure and maximum winds) follows this decrease in absolute vorticity by about 20 hours.

D-15

STREAMLINES

LEVEL

156 HOURS

Figure D-7.

Streamline analysis for the upper troposphere (level lh) at 156 hours.

Coincident with the formation of asymmetries in the outflow is the appearance of spiral bands of rising motion which closely resemble hurricane rainbands. The vertical motion pattern at level 2h (fig- D-9) shows two bands of upward motion which begin at the edge of the domain and spiral inward toward the primary ring of upward motion near the center. The maximum vertical velocity near the center is -440 mb hour-1 (about 1.5 m sec-1).

The precipitation pattern, shown in figure D-10, re- sembles a radar picture of a mature hurricane (e.g., Colon, 1962; Colo et al . , 1961). Strong convection occurs near the center in an irregular circle corresponding to an "eyewall."

D-16

ISOTACHS (M./SEC.) LEVEL lV2

156 HOURS

Figure D-8. Isotaoh analysis for the upper troposphere (level lh) at 156 hours. Isopheths are labeled in m see-1.

Maximum rainfall rates in this region are over 100 cm day-1. Two bands of weaker convection spiral in toward the center. The rainfall rates in the spiral bands are much less than those near the center of the storm, averaging only about 3 cm day" 1 .

The fact that the spiral bands do not appear in the model calculation until the symmetry of the outflow pattern has been destroyed suggests that the generation of the bands and the breakdown of the outflow pattern may be related. As we have noted above, the loss of symmetry in the outflow ap- pears to be associated with dynamic instability. It should

D-17

OMEGA M(CBVHOUR)

LEVEL 3%

156 HOURS

F%gure D-9 . for level 3-2 of ob hour~ 1

Individual rate of change of pressure ( L^-dp/dt) at 156 hours. Isophleths are labeled in units

be emphasized, however, that this linkage is merely specula- tion at this time and will be pursued further when we have had the opportunity to perform experiments with greater hor- izontal resolution.

In a recent paper, Anthes (1970) hypothesized that large scale asymmetries between radii of 400 and 1000 km from the hurricane center may play an important role in satisfying the angular momentum budget of the mature hurricane. The mean radial flux of vorticity may be written

A _

A e v' c' + v,

A A

(D.10)

D-18

RAINFALL RATES

(CM./DAY)

156 HOURS

LEGEND © 1 < R < 10 © 10 < R < 100 100 < R

Figure D-10. Rainfall rates (em day~l) computed from the total release of latent heat at 156 hours. Isopheths are labeled in units of cm day-1.

X

where the ( ) operator refers to the azimuthal mean at a given radius and ( )' refers to departures from this mean.

,. , \ A A

Figure D-ll shows the radial profiles of v 5' and v^ z,

r a r a

computed for the model storm at 192 hours. Both mean and eddy transports of vorticity are positive inside 200 km. Be- yond 200 km, however, where the vertical motion is small, there is a negative correlation between outflow and absolute vorticity, and the eddy flux \/ery nearly balances the mean flux from there to the limit of the domain.

D-19

Although the maximum value of v' c' in figure D-ll is j r a

-70 x 10_lt cm sec-2, which is about half the maximum value

found by Anthes (1970), the qualitative agreement is good.

Figure D-12 shows the azimuthally averaged vertical

cross sections at 156 hours.

circulations are more intense

The temperature section shows

anomaly from 2.5 to 4.1°C and

cold core maximum from -1.5°C

level cold region located between 105 and

has disappeared by 156 hours.

The mean tangential and radial than at 84 hours (see fig. D-5) an increase in mean temperature in the low-level The weak middle- 225 km at 84 hours

a reduction to -1 .0°C.

In summary, beginning at about 100 hours, substantial areas of negative absolute vor- ticity appear in the upper level and the outflow pattern becomes asymmetric. Rainbands appear during this asymmetric stage. The storm is consider- ably less steady than during the earlier, symmetric stage, and the central pressure and maximum winds oscillate with a period of about 6 hours. This unsteady behavior appears to be related to the transient behavior of the regions of negative vorticity in the out- flow layer.

1000

From ance of the hours , more

the time of appear- asymmetries at 120 or less continuous deepening occurs until the storm reaches a maximum inten- sity at about 2 30 hours (see fig. D-3) . At this time the storm corresponds to a strong hurricane, with a central pres sure of 963 mb and a maximum wind speed of 65 m sec-1. The lapse rate in the inner region is wery nearly pseudoadi aba ti c at this time. After 230 hours the storm begins to slowly fill and the calculation is terminated at 260 hours.

-200

J i L

j_

JL.

100

200 300 R(KM.)

Figure

D-ll X

Azimuthal and eddy

(v '

r

400

mean A

500

(vr Ca j r 'a

horizontal vortioity flux in the upper troposphere (level lh) at 192 hours.

D-20

MEAN VERTICAL CROSS SECTION 156 HOURS

TANGENTIAL WIND (M./SEC.)

500 -20

CD

S- 1000

a:

15 45

0

75 105 135 165 195 225 255 285 315 345 375 405 435 RADIAL WIND (M./SEC.)

<

1000

15 45 75 105 135 165 195 225 255 285 315 345 375 405 435

TEMPERATURE DEPARTURE (°C)

1000

15 45 75 105 135 165 195 225 255 285 315 345 375 405 435

RADIUS (KM.)

Figure D-12. Asimuthal mean-vertical cross sections for the tangential wind, the radial wind, and the temperature anom- ally at 156 hours. Isotherms are labeled in °C. Isotachs are labeled in m sec'1.

SUMMARY AND CONCLUSIONS

Preliminary results show that the model is capable of reproducing many observed features of the three-dimensional tropical cyclone. Rather realistic simulations of spiral rainbands and the strongly asymmetric structure of the outflow are obtained.

Despite a relatively coarse horizontal resolution of 30 km, the model produces a storm with maximum winds exceeding 65 m sec"1 and a kinetic energy budget which compares favor- ably with empirical estimates.

D-21

In the mature, asymmetric stage of the storm, substan- tial regions of negative absolute vorticity, anomalous winds, and dynamic instability are present in the upper troposphere. There is a suggestion that the breakdown of the early symmetry of the flow as well as the deepening which takes place during the asymmetric stage are related to the dynamic instability. Large scale, horizontal asymmetries in the outflow are found to play a significant role in the transport of vorticity dur- ing the mature stage. Beyond 200 km, the eddy transport of vorticity is opposite in sign and nearly equal in magnitude to the mean transport.

REFERENCES

Alaka, M. A. (1961): The occurrence of anomalous winds and their significance. National Hurricane Research Pro- ject Report No. 45, U.S. Weather Bureau, Washington, D. C. , June , 25 pp .

Al aka,

M. A. (1962): On the occurrence of dynamic ity in incipient and developing hurricanes.

Hurricane Research Project Report No. 50, U Bureau, Washington, D.C., March, pp. 51-56.

i n s t a b i 1 -

National S. Weather

Alaka

M. A. (1963): Instability aspects of hurricane gene- sis. National Hurricane Research Project Report No. 64, U.S. Weather Bureau, Washington, D.C., June, 23 pp

Anthes, R. A., and D. R. Johnson (1968): Generation of avail able potential energy in Hurricane Hilda (1964).

Monthly Weather Review, 96, (5) May, pp. 291-302.

Anthes, R. A. (1970): The role of large-scale asymmetries and internal mixing in computing meridional circula- tions associated with steady-state hurricanes.

Monthly Weather Review, 98, (7) July, pp. 521-529.

Anthes, R. A., S. L. Rosenthal, and J. W. Trout (1971): Pre- liminary results from an asymmetric model of the trop- ical cyclone. Accepted for publication in the Monthly Weather Review.

Anthes, R. A., J. W. Trout, and S. L. Rosenthal (1971): Com- parisons of tropical cyclone simulations with and without the assumption of circular symmetry. Accepted for publication in the Monthly Weather Review.

D-22

Carlson, T. C, and R. C. Sheets (1971): Comparison of draft scale vertical velocities computed from gust probe and conventional data collected by a DC-6 aircraft. Tech- nical Memorandum ERLTM-NHRL No. 91, NOAA, U.S. Dept. of Commerce, Miami, Fla.

Charney, J. G., and A. Eliassen (1964): On the growth of the hurricane depression. Journal of the Atmospheric Sciences 3 21 3 (1), January, pp. 68-75.

Colon, J. A., and Staff NHRL (1961): On the structure of Hurricane Daisy, 1958. National Hurricane Research Project Report No. 463 U.S. Weather Bureau, Washington, D.C. , October, 102 pp.

Colon, J. A. (1962): Changes in the eye properties during the life cycle of tropical hurricanes. National Hurricane Research Project Report No. 503 U.S. Weather Bureau, Washington, D.C, March, pp. 341-354.

Col on

J. A. (1963): On the evolution of the wmiu ing the life cycle of tropical cyclones. N

Hurricane Research Project Report No. 653 U Bureau, Washington, D.C, November, 36 pp.

wind field dur-

National S . Weather

Fletcher, R. D. (1955): Computation of maximum surface winds in hurricanes. Bulletin of the American Meteorologi- cal Society* 363 (6), June, pp. 247-250.

Grammel tvedt , A. (1969): A survey of finite-difference schemes for the primative equations. Monthly Weather Review, 97 3 (5) , May, pp. 384-404.

Gray, W. M. (1967): The mutual variation of wind, shear, and barocl i ni ci ty in the cumulus convective atmosphere of the hurricane. Monthly Weather Review* 953 (5), February, pp. 55-73.

Hawkins, H. F., and D. T. Rubsam (1968): Hurricane Hilda, 1963 II: Structure and budgets of the hurricane on October 1, 1964. Monthly Weather Review* 963 (9), September, pp. 617-636.

Izawa, T. (1964) : On Technical Note Meteorologi cal March, 19 pp.

the mean wind structure of typhoon No. 23 Typhoon Research Laboratory Research Institute, Tokyo, Japan,

D-23

Kuo, H. L. (1965): On formation and intensification of trop- ical cyclones through latent heat release of cumulus convection. Journal of the Atmospheric Sciences 3 22, (1), January, pp. 40-63.

Kurihara, Y., and J. L. Holloway (1967): Numerican integra- tion of a nine-level global primitive equation model formulated by the box method. Monthly Weather Review, 95, (8), August, pp. 509-530.

Matsuno, T. (1966): Numerical integrations of the primitive equations by a simulated backward difference method.

Journal of the Meteorological Society of Japan, 44, (1), February, pp. 76-83.

Miller, B. I. (1962): On the momentum and energy balance of Hurricane Helene (1958). National Hurricane Research Project Report No. 53, U.S. Weather Bureau, Washington, D.C. , April , 19 pp.

Miller, B. I. (1963): On the filling of tropical cyclones

over land. National Hurricane Research Project Report No. 66, U.S. Weather Bureau, Washington, D.C, Decem- ber, 82 pp.

Molenkamp, C. R. (1968): Accuracy of finite difference methods applied to the advection equation. Journal of Applied Meteorology, 7, (2), April, pp. 160-167.

Ogura, Y. (1964): Frictionally controlled, thermally driven circulations in a circular vortex with application to tropical cyclones. Journal of the Atmospheric Sciences , 21, (6), November, pp. 610-621.

Ooyama, K. (1969): Numerical simulation of the life cycle of

tropical cyclones. Journal of the Atmospheric Sciences , 26, (1), January, pp. 3-40.

Palmen, E., and H. Riehl (1957): Budget of angular momentum and kinetic energy in tropical cyclones. Journal of Meteorology , 14, (2), March, pp. 150-159.

Phillips, N. A. (1957): A coordinate system having some

special advantages for numerical forecasting. Journal of Meteorology, 14, (2), April, pp. 184-185.

Richtmyer, R. D. , and K. W. Morton (1967): Difference methods for i ni ti al -val ue problems. Second edition, Inter- science, New York, 405 pp.

D-24

Riehl, H., and J. S. Malkus (1961): Some aspects of Hurricane Daisy, 1958. Tellus, 139 (2), May, pp. 181-213.

Rosenthal, S. L. (1969): Numerical experiments with a multi- level primitive equation model designed to simulate the development of tropical cyclones: Experiment I. Tech- nical Memorandum ERLTM-NHRL No. 82, ESSA, U.S. Dept. of Commerce, Miami, Fla., January, 33 pp.

Rosenthal, S. L. (1970): A circularly symmetric, primitive equation model of tropical cyclone development con- taining an explicit water vapor cycle. Monthly Weather Review, 98, (9), September, pp. 643-663.

Smagorinsky, J., S. Manabe, and J. L. Holloway, Jr. (1965): Numerical results from a nine-level general circula- tion model of the atmosphere. Monthly Weather Review, 93, (12), December, pp. 727-768.

Syono, S., and M. Yamasaki (1966): Stability of symmetrical motions driven by latent heat release by cumulus con- vection under the existence of surface friction.

Journal of the Meteorological Society of Japan, Ser. 2, 44, (6), December, pp. 353-375.

Yamasaki, M. (1968a): A tropical cyclone model with param- eterized vertical partition of released latent heat.

Journal of the Meteorological Society of Japan, 46, (3), June, pp. 202-214.

Yamasaki, M. (1968b): Detailed analysis of a tropical cyclone simulated with a 13-layer model. Papers in Meteorology and Geophysics , 19, (4), December, pp. 559-585.

D-25

APPENDIX E

RESPONSE OF STORMFURY CLOUDLINE CUMULI TO Agl AND Agl-Nal ICE NUCLEI FROM A SOLUTION-COMBUSTION GENERATOR

Edward E. Hindman, II Navy Weather Research Facility

Shelden D. Elliott, Jr., and William G. Finnegan Naval Weapons Center

and

Bradley T. Patton Research Flight Facility

INTRODUCTION

The existing basis for reducing destructive hurricane winds has been the seeding of eyewall cumulus clouds with silver iodide ice nuclei (Simpson and Malkus, 1964; Gentry, 1970). Recent investigations (Woodley, 1970; Gentry, 1971) suggest that less fully developed cumuli at slightly greater distances outward from the present eyewall seeding location may be more responsive to seeding than eyewall cumulus clouds, The responses of such cumuli to silver iodide seedings were studied during the 1970 STORMFURY cloudline operation.

In addition, at the suggestion of Naval Weapons Center, China Lake, California, a special experiment to compare the effectiveness of two different silver iodide solutions was conducted during the 1970 STORMFURY cloudline operation. Sil- ver iodide-sodium iodide-acetone and silver iodide-ammonium iodide-acetone solutions were burned in the solution-combustion generator designed by Patton (1970). Vonnegut (1949, 1950) discovered that combustion products from both solutions were effective ice nuclei. Recent evidence (Finnegan et al., 1971) suggests that the sodium solution produces complexed nuclei (AgI*NaI), and the ammonium solution produces uncomplexed nuclei (Agl). Laboratory and field evidence (Donnan et al . , 1970; Auer and Veal, 1970) have shown that this difference in nucleus structure affects the nucleus activation; the Agl nuclei become active at -5°C and the Agl'Nal nuclei become active at -10°C when both nuclei are released in the warmer- than-f reezi ng regions of cumulus clouds. Furthermore, when both nuclei are released in clouds at -5°C the Agl nuclei are the more active.

PROCEDURE

A NOAA-Research Flight Facility (RFF) DC-6 aircraft was utilized for both seeding the cloudline cumuli and monitoring the effects of seeding. The NOAA-RFF solution-combustion gen- erator (Patton, 1970) was used to produce the ice nuclei (see fig. E-l). The nuclei delivery rate was nearly equivalent to

the rate (~1 g sec"1) of the WMU-2 pyrotechnic flares presently used in hurricane seedings.

The cloud response to the nuclei was indicated by simul- taneous in-cloud measurements of vertical motions and liquid- water contents (LWC) and ice-water contents (IWC). N0AA- National Hurricane Research Laboratory (NHRL) derived the ver- tical-motion values from the DC-6 aircraft pitch-angle and

Figure E-l. The NOAA-Besearch Flight Facility solution-

Qombustion ice nuclei generator is pictured mounted on the NOAA-RFF DC-6 (N85S9C). The seeding solution is contained in the tank and the solution is burned in the two cylindri- cal chambers . The resulting ice nuclei exhaust from the rear of the chambers .

E-2

radio-altimeter data (Carlson and Sheets, 1971). The LWC and IWC of the precipitation size particles (dia > 200 ym) were determined by Navy Weather Research Facility (WEARSCHFAC) from NOAA-NHRL foil inpactor data (Hindman, 1970)(see fig. E-2). The water contents of the cloud size particles (dia < 200 ym) can be reduced from simultaneously gathered formvar replicator data in a manner similar to the analysis of foil impactor data and will be accomplished at a later data. Results will be de- scribed in a subsequent report. These results should provide an important follow-on to previous studies of IWC increases in cumulus clouds that were attributed to seeding (Todd, 1965; Sax, 1969; and Weinstein and Takeuchi, 1970).

Figure E-2. The Mete- orology Research > Inc.; foil impactor is ■pic- tured mounted on the NOAA-RFF DC-6(N8539C) . The particle impres- sions from this im- pactor are analyzed by Navy Weather Re- search Facility to produce liquid-water and ice-water contents and liquid and ice particle size-distri- bution.

E-3

The water-content values were computed from particle size-distributions which were reduced from foil impactor data using a CALMA 302 digitizer, a UNIVAC 1107 computer, and a Calcomp plotter. The digitizer was used to code particle sizes and type onto magnetic tapes which were processed on the computer. The resulting water-contents and size-distributions were displayed by means of the plotter. The verti cal -motion values were retrived from data cards provided by NOAA-NHRL.

The procedure of seeding and monitoring 1970 STORMFURY cloudline cumuli is illustrated in figure E-3. Seeding was conducted at +5°C in the Cloud I experiment and monitoring penetrations were made at 0 and -5°C, 14 and 27 minutes after seeding, respectively. Immediately following the -5°C moni- toring penetration in Cloud I, seeding was conducted on the first -5°C penetration of the Cloud II experiment. Subse- quently, two monitoring penetrations were made through Cloud II, both at -5°C at intervals of 15 and 30 minutes after seed- ing, respe.cti vely .

The Agl nuclei were tested on 29 and 30 July, and the Agl-Nal nuclei were tested on 31 July. The procedure outlined in figure E-3 was followed on all 3 days. The flight path in the Cloud I experiment tested the effectiveness of both nuc- lei when released in the warmer-than-f reezi ng cloud region. The flight path in the Cloud II experiment tested both nuc- lei when released in the subcooled region of the clouds.

CLOUD I

cloud n

mlJpt

j&fi/tt/si/f/

Figure E-3. Procedure for seeding and monitoring STORMFURY oloudline cumuli 3 29 3 30 3 31 July 1970. Seeding was done at + 5°C in Cloud I and monitoring passes were made at 0°C and -5°C. Seeding was done on the first pass at -5°C in Cloud II. Two counter-clockwise monitoring passes then were made at -5°C in Cloud II. Cloud I tested warm-cloud release of ice nuclei and Cloud II tested cold-cloud re- lease of ice nuclei.

E-4

RESULTS

An example of the average liquid and ice particle size- distributions computed from the foil impactor data gathered in Cloud I is given in figure E-4. The largest particles were ice suggesting that ice particle growth by accretion was more effective than liquid particle growth by coalescence.

Simultaneous foil impactor were gathered on each penetration An example of the water-content and verti cal -motion results from these data is presented in figure E-5. The average LWC and IWC for the precipitation size particles (dia > 200 ym) are plotted along with the ver- ticle-motion values. Positive water-content deviations indi- ; cate the precipitation core within the cloud. The verti- cal-motion values are studied to diagnose the extent of the interaction of cloud dynamical and micro physical processes. Similar results from Cloud II are not presented because the analysis of these data has not been completed.

The average LWC and IWC of the precipitation-size par- ticles were computed from the water-content data gathered during the 0°C and -5°C moni- toring passes of the Cloud I experiment on 29 and 31 July. The values are presented in table E-l. The IWC was greater than the LWC on all passes.

All precipitation mea- surements (total, LWC and IWC) were considerably larger on the 29 July Cloud I experiment than in the 31 July experiment.

and verti cal- mot ion data

of Cloud I on 29 and 31 July.

FLIGHT 700729-A , CLOUD I , PASS 2

INITIAL TIME 160731Z TEMPERATURE + 1°C ALT 15.000FT

_i>

is

CC

LU Q.

ce

100r

2 3

iAMETER (mm)

Figure E-4. Liquid and iae par- ticle size-distribution aver- aged along the 0°C monitoring pass of Cloud I, 29 July 1970 are shown. The unknown parti- ales (u) and small particles (s) contain both ice and liq- uid particles but are too small to differentiate between either ice or water.

E-5

FLIGHT 7700729-A , CLOUD I , PASS 2

INITIAL TIME 160731Z TEMPERATURE + 1°C ALT 15.000FT.

Figure E-5. Navy Weather Re- search Facility water- content deviations about the average water-content value are plot- ted with the simultaneously observed NOAA-NHEL vertical- motion values. The data are from the 0°C monitoring-pass of Cloud I on 29 July 1970. The initial time is the time the aircraft entered the cloud. The aircraft flew at 100 m sec'1; as a result } 10 sec on the time equals 1 km. The average LWC and IWC val- ues are 0.715 and 0.958 g m~ 3 j respectively .

0 10 20 30 40 TIME FROM INITIAL TIME (sec)

On both days, however, the absolute precipitation amounts (total, LWC and IWC) at the lower level (0°C) were from five fold to an order of magnitude greater than at the upper level (-5°C), and the percentage of liquid content with res- pect to ice content was greater at the lower level. These figures indicate that the layer between 0°C and -5°C was an active precipitation formation region and that the increases in both the LWC and the IWC between -5°C and 0°C may indicate significant contributions from both coalescence and accretion

The ratio of the LWC to the IWC at the 0°C level was approximately the same on both days but was somewhat lower at the -5°C level for the Agl experiment, suggesting effects of seeding which will be discussed in more detail.

While these results are quite useful, their re analysis in conjunction with cloud particle distributions from the formvar replicator data should contribute to improved under- standing and improved parameterization of microphysi cal pro- cesses in numerical simulation models.

E-6

Table E-l. Average Liquid-Water and lee-Water Content of Precipitation (g m~z).

CLOUD I Experiment*

Test Day Nuclei

0°C

Monitoring Level

-5°C

LWC

IWC LWC/IWC LWC IWC LWC/IWC

2?97(jly AgI °-715 0.958 0.75 0.074 0.188

3197Qly A9I#NaI 0-078 0.106 0.74 0.010 0.022

0.39 0.45

* Cloud II Experiment data not reduced yet

The average vertical motions were computed and the maximum updrafts were isolated from the verti cal -motion data gathered on all passes in the Cloud I and Cloud II experi- ments on 29 and 31 July. The values are presented in table E-2. The maximum positive verti cal -motion and updrafts for all passes occurred during the seeding pass and then tapered off during the monitoring passes.

Table E-2. Observed Average Vertical Motion/Observed Maximum Updrafts (m sec~l).

Test Day

u c 1 e i

CLOUD I

Experiment

Seed Monitor

+5°C 0°C -5°C

CLOUD II

Seed

-5°C -5°C

Mom* tor

-5°C

29 July 1970

31 July 1970

AgI

Agl-Nal

3.0/ 9.3

1.5/ 7.5

0.5/ 3.5

0.7/ 5.2

1 .0/ 4.0

0.2/ 2.5

1 .0/ 6.2

2.7/ 8.2

0.3/ 2.6

2.7/ 5.7

0.8/ 4.0

■0.3/ 2.1

DISCUSSION

E-7

aircraft reached the and -5° levels 14 and 27 minutes after seeding, respectively. Hence, it is likely that most of the seeding material had been carried up and through these levels prior to the aircraft penetration.

Th have been The media observed cles were minutes i LWC) (Hin ci ty af te than the from the Agl nucl e passed -5 ice parti the time

e preci observ n mass at -5°C e s t i m a n the o dman an r 17 mi updraf t rising i are a °C, the cles is it took

p i t a t i ed at di a met was a ted to bserve d John nutes , thus s e e d i n c t i v a t n the 7 mi n the a

on resu the -5° er of t pproxi m

grow f d i n - c 1 son , 1 9 of grow

permi t g regio e d in 3 total t

+ 3 mi i r c r a f t

1 ti ng C 1 eve he i ce ately r o m i c oud co 70). th was ting t n. As

m i n u t ime fr n + 17

to re

from seed 1 in Clou

preci pi t 1.5 mm . e nuclei n d i t i o n s The parti

estimate he p a r t i c suming th es after o m s e e d i n

min = 27 ach the -

i ng , however , may d I on 29 July, ati on parti cl es These ice parti- to 1.5 mm in 17 (-5°C, 1 g m"3 cles' fa 1 1 vel o- d to be faster les to settle at a majority of the seeded region g to grow 1 . 5 mm

minutes which is 5°C level .

The LWC/IWC ratio illustrated in table E-l shows that the 0°C passes in Cloud I on 29 and 31 July had similar LWC/ IWC ratios. The -5°C passes, however (which presumably mea- sure the seeding effects on the precipitation), had a lower ratio on the 29th (0.39) than on the 31st (0.45). The higher relative ice content of the Agl-seeded cloud (29th) at -5°C compared to that of the Agl »NaI-seeded cloud (31st) suggests that the aircraft may have intercepted the ice precipitation particles settling from the region of the cloud affected by the Agl .

Random interpretation error of approximately ±19 per- cent has been estimated when differentiating between ice and water particle impressions from the foil sampler. The dif- ference in the LWC/IWC ratio is slightly greater than the possible random error, therefore the difference is considered real .

settl woul d -10°C the - and t that serve regi o becau falli the o

It w i n g f r be in and p 5°C le he mon preci p d on r n. Th se a 4 ng fro bserva

oul d om th terce robab vel i i tori i t a t i adar i s re m se m the ti on

not be expected that the ice precipitation e region of Cloud I affected by the Agl-Nal pted. These particles formed at and below ly did not overcome the updraft to reach n the 27-minute interval between seeding ng passes. Simpson (1970) recently showed on assumed to result from seeding was ob- within 10 minutes at 6 km below the seeded markably short period of time was possible c-1 downdraft assisted the precipitation in

formation level (6-7 km above cloud base) to level (1 km above cloud base).

E-8

Significant decreases in the average vertical motion after seeding were measured in both the Agl and Agl-Nal ex- periments in Cloud II (see table E-2). An unexpected reduc- tion was registered in the Agl-seeded cloud on the first monitoring pass followed by a restoration trend on the second monitoring pass. In contrast, the Agl «NaI-seeded cloud showed a slight decrease during the first monitoring pass but a more significant reduction during the second monitoring pass.

Admittedly the vertical motion values constitute a limited sample and the magnitudes are near the data's noise level. If these observations are considered somewhat credi- ble, they still present a paradox and suggest certain weaknes- ses in current parcel and bubble theories of convection. The theories may not adequately explain the paradoxical decrease in updrafts following seeding. A more rigorous application of the hydrodynamic and thermodynamic equations integrated with a more realistic mi crophys i cal parameterization may be required for adequate simulation of cumulus convective pro- cesses. Such a formulation is currently being considered at WEARSCHFAC which would explain the sequence of events in the Cloud II experiments according to the suggested processes bel ow.

vel oci f i c i a 1 in u p d effect updraf i ncrea this r of the the se active drafts the fi gan to updraf rel eas higher are 1 e drafts of val

For ties

nucl rafts s of ts in sing e g i o n

late e d i n g

at -

woul rs t m

dimi ts in e of

1 eve ss ac

woul ues s

both were e i in

foil s e e d i

and the s . In nt he

and 5°C. d be oni to ni sh creas the 1 Is th ti ve d be hown

s e e d i measu creas owi ng ng de above tabil

the at of s e n s i

Henc n o t i c ring by th ed. atent an in than del ay in th

ngs l n red bel ed natu

these crease

the in i ty and Agl exp

fusion ng leve e the s ed rath penetra e time In the

heat o

the Ag the Agl e d , w h i e CI oud

Cloud ow th ral g seedi the s creas

supp eri me

woul 1 s be uppre er qu t i o n , of th Agl -N f fus I exp

nucl ch is

II e

II, e reg 1 a c i a ngs s tabil ed gl res si nt th d tak cause s s i n g i c k 1 y

and e sec al ex ion w eri me ei .

cons x p e r i

the av ion in tion . uggest i ty an a c i a t i ng the e i n c r e pi ac these ef fee Sue perhap ond pa peri me oul d t nt bee The i m i stent ment i

erage

whi c

The

that

d i nc

on re

updr

eased

e di r

nucl

ts on

h was

s the

ss be

nt , t

ake p

ause

pact

with n tab

v e r t i h the decrea

the i rease gi on w afts b

rel ea ectly ei bee

the u

the c

ef fee cause he i n c 1 ace a the Ag on the

the t le E-2

cal

a r t i -

ses

n i t i a 1

the

hile

el ow

se

above

ome

P-

ase on

t be-

the

reased

t

I-Nal

up- rend

These processes suggest the following cycle of events which may occur after a cumulus cloud is seeded:

a. The seeding material will be carried upward with increased glaciation taking place at the level according to the activation of the seeding material

E-9

and will be followed by increased condensation and increased precipitation.

b. Initially, the increased release of latent heat will augment the updrafts in and above the in- creased glaciation level and suppress updrafts bel ow this 1 eve! .

c. Subsequently, the net effect of the whole process will warm the cloud core as well as create a divergent outflow in the upper levels. The warming and outflow will decrease the surface pressure which will cause an increased inflow at the lower levels and produce a general increase in upward motion throughout the cloud.

This cycle suggests prospects of developing a ration- ale for increasing cloud growth by successive pulsed seedings Empirical evidence compiled by St. Amand (1969) indicates that pulsed seedings may increase cloud growth and merge in- dividual clouds into cloud systems. While the cycle is not properly reflected in current simple cloud models, its phys- ical reasoning is qualitatively consistent.

1 ce

figu

were

Matt

crea

gl ac

clou

than

grow

woul

The

beca

1 eve

1 eve

An

nuclei

re E-6

s i m u 1

hews i

se to

iate a

d seed

6.3 k

to ro

d i ncr

cl oud

use th

1 . Th

1 i t w

advan rath . II ated n thi zero t -25 ed wi m. T ughly ease seede ese n is gl oul d

tage er th 1 ustr wi th s rep at 6. °C, i th Ag he cl the na tur d wit ucl ei a c i a t have

of gl an Ag ated a num ort ( 3 km n d i c a I-Nal oud r -10°C al gl h Agl i ncr ion b grown

aci ati I-Nal

are cl e r i c a 1 app . H for th ting a

ice n eached

1 evel a c i a t i

ice n eased oosted

to na

ng tr ice n oud v

cumu )• T e nat

cl ou u c 1 e i

the

befo on an u c 1 e i natur

the tural

0 p i c a 1

u c 1 e i i erti cal

1 us mod he vert ural cl d top a

also d -6°C le re the d incre , howev al gl ac cloud p

cumul s ill moti el de i cal oud a t 6.3 i d no vel b Agl-N ase c er, g i a t i o as t t

i wit ustra ons t scrib moti o ssume

km . t gro ut ne al i c 1 oud rew t n at he 6.

h Agl ted in hat ed by ns de- d to The w more eded to e nuclei growth . o 1 1 km the -5°C 3 km

CONCLUSIONS

Ice-water content data and verti cal -motion data from two cloudline cumuli seeded with Agl ice nuclei tentatively indicate that the cumuli began to glaciate at approximately -5°C. Similar data from two other cloudline cumuli seeded with Agl'Nal indicate that the cumuli began to glaciate at a colder temperature, possibly -10°C. These tentative con- clusions are in agreement with previous laboratory results

E-10

Donnan et al . (1970) and field results of Auer and Veal (1970). This agreement suggests that given a choice of acetone solu- tions to burn in a solution- combustion generator, the Ag I - NH4-acetone solution would be the choice if glaciation at temperatures near -5°C is de- sired.

Vertical- motion data from two cloudline cumuli seeded and monitored at the -5°C level sug- gest that the initial effects of seeding may have suppressed the updrafts below the regions of increased glaciation and heating

Further testing, however, is needed to confirm these pre- liminary conclusions. The ex- tremely limited number of seeded clouds prevented a statistically significant sample. Furthermore the lack of control clouds pre- vented objective comparisons of the seeded clouds with those developing naturally.

The operational data gathered from the NOAA-RFF solution-combustion generator indicated that the device can be used routinely to seed STORMFURY cloudline cumuli.

Figure E- on updr aloud i onment 3 Matthew dimensi Cloud b sumed t pheric aloud g was fro sure re

6. Effect afts in a n a hurrio as simula s (1971) u onal oumul ase diamet o be 3 km. sounding > rowth was m the 996- gion of a

of seeding cumulus ane envir- ted by sing a one- us model, er was as-

The atmos- from which simulated^ 999 mb pres- hurricane .

E

UJ

>

LU -I

< LU (/)

LU > O CD <

I CD

LU

I

I

Ag I SEEDING (Active at -5C )

- -35

- -30

-25 -20 -15

NATURAL SEEDING (Active at - 25 C )

Agl Nal SEEDING

(Active of -IOC )

J I I L

io L

LU CE

h- <

5 *

J LU

a.

LU

I-

LU

15

20

5 10

W ( m sec"1)

o

LU

E-ll

RECOMMENDATIONS

1 . C o n c 1 u s i STORMFURY cloudline by the prel i mi nary n experiments should b tial effect of seedi pression of updrafts

2. The need i ng and moni tori ng p above the seeding le

3. The diff rapid succession and indicates the desira within the core and the seeded updraft. 2-32 sai 1 pi ane ( Schr requi rements . This of the rising air an Resul ts from such f 1 seeding is glaciatin vide a measure of th tions. These result provement in the par numerical cloud mode

ons derived from data presented i n ature of the expe e more extensive ng tropical cloud

the evaluation of 1970

the report are limited ri merits. Subsequent to determine if the ini line cumuli is the sup-

for s asses vel su i cul ty

moni t bil i ty rise a

The c i bner , a i rcra d cont i g h t s g the e ef fe s shou ame ter Is.

horte

and t

ggest

i n e

0 r i n g of h

t app loud

1966 ft wo i n u o u woul d avail cts o

1 d co i z a t i

r time he nee

a dua xecut i

passe avi ng roxi ma physi c ) i s s ul d be sly mo

i 1 1 u s able s f seed n t r i b u on of

-sepa d for 1 -air ng mo s abo an ai tely s ins ui ted abl e ni tor trate uperc i ng o te to seedi

rati o

moni

craft

n i t o r

ve th

rcraf

the s

trume

for

to s

the

how

ool ed

n ver

a mu

ng ef

n bet t o r i n

expe i ng p e see t tha ame s nted these eed t seedi thoro

wate t i c a 1 ch ne fects

ween g pas r i m e n asses ding t can peed NCAR

flig he co ng ef ughly r and

acce eded

i n

seed-

ses

t.

i n 1 evel

stay as SGS ht re fects

the

pro- 1 era- i m-

REFERENCES

Auer, A. H., Jr. and D. Veal (1970): Evaluation of cloud seeding devices in an outdoor laboratory. Project Report, Naval Weapons Center Contract N6 600 1- 70-C-O 639 November, (on file, Naval Weapons Center (code 602), China Lake, California).

Carlson, T. N., and R. C. Sheets (1971): Comparison of draft scale vertical velocities computed from gust probe and conventional data collected by a DC-6 aircraft. Technical Memorandum ERLTM-NHRL No. 91, NOAA, Dept. of Commerce, NHRL, Miami, Fla.

Donnan, J. A., D. N. Blair, W. G. Finnegan and P. St. Amand

(1970): Nucleation efficiencies of A g I - N H4 1 and A g I Nai-Acetone solutions and pyrotechnic generators as a function of LWC and generator flame temperature. A Preliminary Report. The Journal of Weather Modifi- cation, 2, pp. 155-164.

E-12

Finnegan, W. G., P. St. Amand and L. A. Burkardt (1971): An

evaluation of ice nuclei generator systems. Submitted

to Science .

Gentry, R. C. (1970): Hurricane Debbie modification experi- ments, August 1969. Science, 164, pp. 473-475.

Gentry, R. C. (1971): Progress on hurricane modification

research-October 1969 to October 1970. Presented at

Twelfth Interagency Conference on Weather Modification , October 28-30, Virginia Beach, Va.

Hindman, E. E., II (1970): Cloud particle samples and water contents from a 1969 STORMFURY cloudline cumulus.

Project STORMFURY Annual Report 1969, U.S. Dept. of Navy and U.S. Dept. of Commerce, Appendix F.

Hindman, E. E., II and D. B. Johnson (1970): Numerical simu- lation of ice hydrometeor development. Preprints -

Conference on Cloud Physics. American Meteorological Society, Boston, Mass., pp. 63-64.

Patton, B. T. (1970): Preliminary report on the Patton mark series generators. On file at N0AA-RFF, Miami, Fla., 5 pp.

Sax, R. I. (1969): The importance of natural glaciation of

the modification of tropical maritime cumuli by silver

iodide seeding. Journal of Applied Meteorology , 8, pp. 92-104.

Schribner, K. (1966): The explorer. Journal Soaring Society of America, pp. 12-13.

Simpson, J. (1970): On the radar-measured increase in precip- itation within ten minutes following seeding. Journal of Applied Meteorology , 9, pp. '318-320.

Simpson, R. H., and J. S. Malkus (1964): Experiments in hur- ricane modification. Scientific American, 211, p. 27.

St. Amand, P. (1969): Weather modification techniques devel- opment. Appears in "A Summary of the U.S. Navy Pro- gram and FY - 1 969 Progress in Weather Modification and Control." WEARSCHFAC Technical Paper No. 26-69, pp. 38-39.

Todd, C. J. (1965): Ice crystal development in a seeded cum- ulus cloud. Journal of Atmospheric Science, 4, pp. 70-78

E-13

Vonnegut, B. (1949): Nucleation of supercooled water clouds by silver iodide smokes. Chemical Review, 44, pp. 277' 289.

Vonnegut, B. (1950): Techniques for generating silver iodide smoke. Journal of Colloid. Sciences 3 S3 p. 377.

Weinstein, A. I., and D. M. Takeuchi (1970): Observation of ice crystals in a cumulus cloud seeded by vertical- fall pyrotechnics. Journal of Applied Meteorology , 93 pp. 265-268.

Woodley, W. L. (1970): Precipitation results from a pyrotech nic cumulus seeding experiment. Journal of Applied Meteorology 3 93 pp. 242-257.

E-14

APPENDIX F

MEASUREMENTS OF VERTICAL MOTION IN THE EYEWALL CLOUD REGION OF HURRICANE DEBBIE

Toby N . Carl son National Hurricane Research Laboratory

INTRODUCTION

Vertical motions on a cumulus cloud scale (1 to 100 km) can be estimated using various parameters recorded by the RFF DC-6 aircraft (Carlson and Sheets, 1971). The formula used to obtain the drift scale vertical velocity, W, is

W = V+ (a.

) + W,

(F.l)

where V. is the true air speed, a, and 0. are the angle of attack and pitch angle of the aircraft with respect to the equilibrium values of these angles, and Wp is the aircraft vertical velocity. In the DC-6 aircraft, the latter is de- termined by differentiating the radio-altimeter values to give change in aircraft height with time. The true airspeed and pitch angle are directly measured; the equilibrium value of the pitch angle must be continuously determined since it is found to drift slowly with time.

The equilibrium pitch angle suming that the mean vertical moti straight line pass is zero for sho clouds; in longer passes, such as through hurricanes, it is assumed over a longer interval, L, (-50 to is thereby determined at the mid-p length L which will be shorter tha Inspection of the vertical motion vertical velocity averaged over L case the zero vertical velocity ax eye; for example, if the values fa undisturbed environment of a cumul of the hurricane eye. The angle o but is computed indirectly from th aircraft lift. In practice during

» oe , on thr rt pas strai g that W

75 mi oi nt o n the trace need n is sho il to us cl o f atta e equa

fligh

is deter oughout ses thro h t line

is zero 1 es ) ; a f a slid length o may indi ot be ze uld be a approach u d or in c k is no t i o n of ts in hu

mi ned a give ugh cu radi al

when v a r i a b i n g s c f the cate t ro , in d juste zero the c t meas moti on r r i c a n

by as- n mul us

legs averaged le 9e ale of pass . hat the

which d by i n the enter ured

for es ,

the basic 1 sec digital values are converted to a 6 sec block average in order to minimize noise in the data. For cumulus clouds, a weighted 4 sec (binomially smoothed) running mean is used.

PROFILE OF VERTICAL MOTION IN HURRICANE DEBBIE (1969)

The draft scale vertical motion computations were de- termined for all radial legs in Hurricane Debbie on 18 and 20 August 1969, by the 39 - C DC-6 aircraft which was the only aircraft capable of making such measurements on those occa- sions. Of the 10 radial penetrations made on the 20th, and of seven made on the 18th by this aircraft a total of eight and five passes, respectively, were made along a southwest- northeast azimuth. Most of the penetrations began and ended about 70 km from the center and all of them penetrated both of the eyewalls and the inner clear region of the eye.

showe pass a r r i v m o t i o meti c and t eye w ai rcr clear regi o compo eight (The and i

Exa d tha due t e at n pro ally he fi as av aft i

eye. n i n si te

or f inner s not

m i n a t i t ther o the a comp f i 1 es averag ve pas eraged nto (o Exce f i gure prof i 1 ive po p o r t i shown

on of th e was co rapidly osite pi for the ed toget ses on t

with re r from) pt for t

F-l whe es of ve i nts , re on of th

here . )

e i rid i

nsi der s h i f t i cture southw her fo he 18t s p e c t the ey he out re the r t i c a 1 s p e c t i e clea

v i d u a 1 v able var ng echo for the es t-nort r the e i h . Each to the p ewall cl er porti re were moti on vely, fo r eye wa

ertical mo i a b i 1 i ty f patterns . storm, the heast legs ght passes radial 1 e oi nt of en oud from ( ons of the fewer obse represent r the 20th s compos it

tion

rom p

In o

vert

were

on t

g fro

try o

or i n

eyew

r v a t i

an av

and ed se

prof i 1 es ass to rder to i cal

ari th- he 20th m the f the to) the all cl oud ons , the erage of 18th. parately

doma

whi c

near

i nsi

regi

the

deep

maxi

sect

ing

vert

pass

Bot in of hiss ly neu de the on . T same o ened a mum as or) , w annul u i cal m e s w h i

h pro r i s i n urrou tral ) eye) he st n the pprec cent hi 1 e s was o t i o n ch sp

files

g mo t

nded

vert

and

rengt

18th

i ably

was 2

the m

abou

meas

anned

show s ion is by a mo ical mo al so on h of th

as on

in the -3 m se e a n r i s t 1 m s urement

only a

ome si found re nar tion n

the o e updr the 20

i nter c"1 (s ing mo ec" 1 o s were

few h

milarity in that a broad in the eyewall cloud region row ring of descending (or ear the eyewall (and just uter edges of the wall cloud afts appeared to be about th, although the storm had val. In figure F-l, the trongest in the southwest tion averaged over the ris- n both days. Because the

made from a series of ours, it is difficult to

F-2

VERTICAL VELOCITY (DEBBIE, 1969)

b 2.0

LU

in

o

tr»-

>o

_j

>

0.0

2.0

Aug 18

WIDTH OF EYE Aug 18

sAug 20

WIDTH OF EYE Aug 20

_L

1

-L

_L

I

_L

J_

_L

2.0

0.0

•2.0

60 40 20 0 20 40 60 NE DISTANCE FROM EYE CENTER (KM.) SW

Figure F-l. Composited vertical velocity profile for Hurri- cane Debbie as determined from the RFF 39-C DC-6 aircraft . The profile represents an average of 8 radial legs on 20 August 19693 and 5 radial legs on 18 August^ which were on a

northeast-southwest azimuth . Compositing was done with respect to the inner face of the eyewall cloudy the mean positions of which are indicated by the width of the eye.

assess the effects of seeding on the updraft profile in Hur- ricane Debbie. The composite profiles, however, demonstrate the possible use of vertical motions in evaluating seeding experiments (see app. E in this report).

ACCURACY OF THE VERTICAL MOTIONS

Carlson and Sheets (1971) have discussed deficiencies in the measurement of draft scale vertical motion and the ac- curacy of the calculations, based on a comparison with simul- taneous measurements made with the RFF gust probe system in a series of test passes through individual cumulus clouds. Their results indicate that the measurement accuracy depends on the scale in question and on the intensity of the turbulent motions (the variance of W). Reliability of the measurements is considered to be greatest for updrafts on the scale of the cumulus cloud (1 to 10 km) and for strong vertical motions.

F-3

But f decre A pos exist 0.5 m ing i i n a the d the a per s 1 ar u weake litud air w less, even this (fig. fore , downd in an

or scales ases rapi s i b 1 e n o i

with a f

sec- * . ntens i ty p a r t i c u 1 a raft , and mpl i tude econd. C pdraft or r v e r t i c a e of the here the

A minim in clear order. I

F-l ) , th

the magn rafts may

i n d i v i d u

of mo d 1 y w i se f re requen Absol u of the r draf

the u val ue onvers

downd 1 moti moti on maxi mu urn unc air w h n comp e n o i s i tude

have al pas

tion th de quenc cy of te er vert t pro ncert when ely , raft ons a s the m dra ertai ere t o s i t e e may of th more s .

a kilome creasing y (that

5-10 se rors app ical mot file dec ainty is the peak the perc prof i 1 e nd may b msel ves ft speed nty of 0 he verti s such a

be cane e broad s i g n i f i c

ter o wave of ai c and ear t ions, rease prob val u entag decre ecome i n we s are .4-0. cal v s the el ed prof i ance

r 1 es 1 engt rcraf

an a o i nc

but s wit ably e exc e err ases

comp ak cu

a me 8ms e 1 o c i

one to so le of than

s , th h of t osc mpl i t rease the p h the a sma eeds or fo with arabl mul us ter p ec" l ty va s hown me ex updr i t wo

e uncert the updr illation ude of a

with in ercent e

a m p 1 i t u 11 fract a few me r a part i ncreasi e to the

or in c er secon may be p r i a n c e i

for Deb tent ; th afts and ul d have

ai nty aft. ) may bout creas- rro r de of ion of ters i cu- ngly

amp- 1 ear dor resent s of bi e ere-

had

V turns an brought For that i ty only s tan t 1 e kept to are nece cumul us detri men critical ting c h a silver i In the f ai rcraf t vertical known .

e r t i c

d dur

about

reas

i n s

vel w

a mi n

s s a r i

updra

tal t

i n d

nges

o d i d e

uture

wh i c

vel o

al motio ing sign

by the on the c trai ght here the i m u m . 0 ly made fts of t o the me e t e r m i n i are also

burner , an ang h will h city sin

ns are a i f i c a n t pilot at a 1 c u 1 a t i line (or

power s c c a s i o n a by the p he eyewa asuremen ng the b

made du is opera 1 e of at opef ul ly ce , at p

1 so adve changes tempti ng ons are

radial ) e 1 1 i n g c

I power i 1 o t in

I I cl oud ts but a asic dra ring c 1 o ted on b tack van

i mprove resent ,

rsely in ai

to c felt

pass hange s e 1 1 i penet

of a re no ft pr ud se oard e wi 1

the aj i s

affected rcraft al limb or d to have s es flown s by the ng change rati ng i n

h u r r i c a n t c o n s i d e ofile. P e d i n g run the DC-6 1 be moun measureme

not accu

by sharp t i t u d e escend . ome val i d- at a con- pilot are s , which tense e , are red to be ower set- s when the aircraft, ted on the nts of rately

REFERENCE

Carlson, T. N., and R. C. Sheets (1971): Comparison of draft scale vertical velocities computed from gust probe and conventional data collected by a DC-6 aircraft. Tech- nical Memorandum ERLTM-NHRL No. 91, NOAA, Dept. of Commerce, NHRL, Miami, Fla.

F-4

APPENDIX G

AN ESTIMATE OF THE FRACTION ICE IN TROPICAL STORMS

W. D. Scott and C. K. Dossett National Hurricane Research Laboratory

INTRODUCTION

With the present concept of the modification of tropi- cal storms, a considerable amount of supercooled water must exist above the freezing level in the storm cloud system. This thinking precludes modification of the storm if the supercooled water has already frozen and turned to ice. Hence, an estimate of the ice content of the clouds at levels between and -20°C would help us assess the probability of being able to modify the storm, and, perhaps, give an a posteriori judgment on the success of a seeding mission.

We currently have acquired three instruments that should give an estimate of ice concentration during a flight into a storm. These are the foil impactor, the continuous particle replicator, and the ice particle counter. The foil impactor has been described in previous STORMFURY Reports (see Sheets, 1969; Hindman, 1970) and some data from the cloud- line experiments are presented in this report by Hindman (app. E). The particles are impacted on a strip of aluminum foil and the size and character of the particles are derived from the impressions they make.

The ice particle counter was recently acq a contract with Mee Industries, Altadena, Califo an optical technique which measures the scintill "twinkles" ice crystals make when they reflect 1 secular faces. It is now undergoing calibration preliminary test results indicate that it can co tides in real time with a 75 percent or better even in the worst case when large water drops ar the sampl e .

The continuous particle (formvar) replica vice which captures cloud particles (i.e., dropl and ice crystals) and forms plastic replicas of mm motion picture film. The device currently in was also manufactured by Mee Industries. Its es tures are nearly identical to the instrument man

uired through rnia. It uses a t i o n s or ight off their

tests , but unt ice par- rel i abi 1 i ty e present in

tor is a d e - ets , rai ndrops them on a 16-

operation sential fea- ufactured by

Meteorology Research, Inc., and described by Sheets (1969); the instrument and its basic principles have been used for years, and several different versions of it are presently being used (see for example: MacCready and Todd, 1964; Spyers-Duran and Braham, 1967; Ruskin, 1967; Patrick and Gagin, 1971). It has several deficiencies, but it does seem reasonable that the instrument can be used to obtain a sub- jective estimate of the fraction ice in clouds, i.e., that fraction of the total hydrometeor population considered to be ice. With the continued operation of the instrument in hur- ricanes and tropical storms, a large quantity of in-cloud data has been amassed. In this report some of the more recent data are considered, and the fraction ice at different levels in these storms estimated.

THE FLIGHT TRACKS

The aircraft flight tracks on which the data were taken are presented in figures G-la, G-lb, and G-lc and are represented by arrows. On figures G-la and G-lb the orienta tion and the relative locations of the clouds are preserved;

STORM INGA FLIGHT 690930B

//

CLOUD CENTER

~ 60 N M NE of Storm Center

% IC E

l.lln

HYDROMETEOR /^f/ COVERAGE

jL ill llllllllllll llllllllLll,„,Lll llLyl !Hnl uljlLJ LlillllL

/mdtAgt/mdt/ /mdt/mdt/mdt/ /mdwvv /lgt

(See text for on explanation of Symbols)

CLOUD CENTER S

~ 20 N.M

N of Storm Center

25

SCALE ( N M )

50

STORM FELICE

ALT 18,000

TEMP -0 3°to-1.2°C

FLIGHT TRACK ~70 N M NE of Storm Center

Figure G-la. Sampling locations in Tropical Storms "Inga"

and "Fe lice . "

G-2

STORM : TD# 14 FLIGHT^ 701002A

X

CLOUD CENTER 150 N.M. E from Storm Center

(See text for meaning of Symbols)

CLOUD CENTER

~150 N.M. from Storm Center

oh

25 SCALE (N.M.)

50

Figure G-lb. Sampling locations in Tropical Depression

Number 14.

G-3

STORM: TD*14 FLIGHT: 701003A

(See text for explanation of symbols)

CLOUD CENTER ~10N.M

E. of Storm

Center

CLOUD CENTER ~90N.M.

NE of Storm

Center

22222

% ICE

ooooooou- COVERAGE

LGT MDT

25 SCALE (N M.)

50

Figure G-lo. Sampling locations for Tropical Depression

Number 14.

on figure G-lc the two clouds were slightly farther apart than is shown. The cloudy shapes represent the approximate extent of visible cloudiness, and the crosshatched area on figure G-la is the area where a significant radar echo was ob- served. The scale is constant on all the figures; altitudes, temperatures, and the relationship of each cloud to the storm center are indicated.

G-4

A summary of all the results is shown in figure G-2. At the time the data were taken Tropical Storm Inga was in- creasing in intensity and had just produced hurricane-force winds. "Felice" appeared to be developing into a hurricane but it never became one. Tropical Depression No. 14 never did reach the status of a tropical storm, but the same storm sys- tem had flooded the island of Barbados and subsequently caused massive flooding in Puerto Rico.

STORM

TIME

ALTITUDE

TEMP

% ICE

% COVERED

TROPICAL

DEPRESS.

#14

2003- 2003-

2011 Z 2019 Z

18K 18K

■3.5° to -4.5°C -3.0° to -4.0° C

TROPICAL

DEPRESS.

#14

1804-

1711

1702-

1632-

1543

1427

1405

i819 Z 1727 Z 1704 Z 1633 Z 1544 Z 1429 Z 1406 Z

18K 18 K 18K 17.6 K 11. 6K 11.6 K 11.6 K

-3.0° to -4.0°C -2.5° to -4.0° C - 3.0° to- 3.5° C -2.0° to- 3.0° C

6.0° C

7.0° C 8.0° to 7 5°C

700915 A "FELICE"

1743-1745 Z

18 K

-0.3° to -1.2° C

690930 B "INGA"

1414

1354 1247

1418 Z 1408 Z 1249 Z

19 K 19 K

9K

12° to- 2.0° C 2.0° to 1.0° C 11.5° C

0%

0%

Figure G-2. Storm data.

6-5

THE ESTIMATED FRACTION ICE

The data were interpreted by viewing the projected image of the replaced crystals with a 16-mm motion picture projector. The magnification was such that 1 mm of distance on the film was projected to make 8 inches on the screen. All particles that appeared to have a crystalline character were assumed to be ice. That is, any particle with a non- spherical shape was assumed to be ice. As overall judgment was made on a single frame; one frame in approximately eyery 200 frames was chosen. The estimates of fraction ice are shown in detail in figures G-la, G-lb, and G-lc. The bars represent the fraction ice which is the fraction of the total hydrometeor population that was considered ice. Below the abscissas are shown the relative quantity of hydrometeors that were sampled in terms of coverage of the 16-mm film. The blank areas indicate yery light coverage. The circles represent hydrometeor samples that contained no detectable ice; the vacant spaces between the bars indicate either that no sample was taken, that there was an insufficient number of hydrometeors to estimate the fraction ice, or that the sample was too poor to make a judgment.

Several small clouds in the same general position rela- tive to Tropical Depression No. 14 are not shown on figure G-lb. A sample taken from 1406Z to 1407Z in clear air showed the presence of cloud droplets with what appears as a small amount of ice. In this instance there were three small clouds showing radar returns within 10 n miles. An in-cloud sample taken between 1427Z and 1428Z indicated a moderate amount of liquid water and little ice. A third sample between 1632Z and 1633Z was taken outside the visible cloud and contained only ice in small quantities; again, a cloud with a radar echo was within 10 n miles. Of these samples, all were taken between the and 8°C levels except the last which was taken between -2° and -3°C and, accordingly, contains mostly ice.

DISCUSSION

The observations of appreciable quantities of both liquid and solid hydrometeors outside the cloud boundaries is interesting and may shed light on the possibility of natu- ral seeding by nearly glaciated clouds. It also points to the intangible character of a cloud boundary. At this time, however, in many of the samples, the possibility still exists

G-6

that there is an improper time correlation. An electronic counter with a digital readout is currently being added to the instrument which should help to alleviate this problem in future flights.

at diff much as data in warmer course , all the Depress d i s s i p a that th by simu ogy Res of rema tal s ( s f ormvar were re

Figure erent t

1 ° C in d i c a t e tempera

the da

data a ion No. t i o n st e data 1 taneou earch , rkably ee fig.

sampl e pi i c a t e

G-3 sh empera

error that a tures ta may t the

14, a age at for Tr s samp Inc. ) . detail

G-4) . s ; but d.

ows a tures

and

1 arg (belo

mere col de nd it

the

o p i c a

les t

The

ed im

The

nume

plot of The vo most like e portion w the -5° ly ref 1 ec r tempera

was pass time. It 1 Depress aken by t

foil sam pressions se crysta rous , sma

the e rtex ly ar

of i C el e t the tures ing t

i s i ion N he fo pi es

of s Is di 1 1 er ,

s tima tempe e a 1 ce i s v a t i o age are hroug ntere o. 14 i 1 i m showe tel la d not amor

ted f ratur it tie

pres n 1 ev of th from hat sting

are pacto d a 1 r and

appe phous

r a c t i es ma

1 ow. en t a el), e s to Tropi empor , how corro r ( Me arge

need ar in

i ce

on l ce y be as

The t the

Of rm since cal ary ever , borated teorol - number le crys-

the pi eces

The data of figure G-3 amount of ice at the warm temp suit of drop breakup and disto before drying that created som

rEMP °c

6-i

4- 2-

0

2- 4-

6 8-

10-

12

0

50

FRACTION ICE

Figure G-3. Fraction ice at different temperatures in tropical storms.

100

al so

erat

rtio

ewha

i ce

part

like

pure

meas

of o

tic!

m i s i

The

sure

+ 11 .

i ce-

four

of p

the

the

be p

most

deri

f ram

sed

flig Stor

show a ures . ns of t t cryst may hav i a 1 1 y m ly, how ly stat ure of ccurren e r e p 1 i n terpre worst d ment of 5°C, co like c h

frames oor qua error b 1 evel o laced i

s i g n i f ved fro es . )

All without ht 1 eve m I nga ,

n ano This he dr a 1 1 i n e bee el ted ever , i s t i c the r ce of c a t i o tati o i s c r e

50 p rresp aract

i n e 1 i ty . ars i f con n the i c a n t m j ud

mal ou may b ops d e sha n pre stat this al an e 1 a t i i nad n and n of pancy ercen onds e r i s t ight

The

n d i c a

f i d e n

val u

data

gment

sly hi e the uri ng pes . sent i e . Mo

res ul d give ve f re equate

subse the da , a me t ice to obs i c s in i n a s

size tes ro ce tha e. (T

poi nt s on 2

gh re- or

Al so , n a st

t i s s a quency

par- quent ta. a- at e r v i n g

only ampl e of

ughly t can he

i s 78

the data were proces- knowledge of the

Is, and in Tropi cal the analysis was

G-7

., ,<s.i

Figure G-4

Impressions of stellar and needle ice crystals on the foil impaotor .

repeated by both authors independently on alternate, but staggered, frames. The results are shown in figure G-5, and the data points with the error bars represent this comparison. Another comparison was made between samples in Tropical Depres- sion No. 14, in flights at the same temperature but at slightly different times. These data are represented by the triangles.

The airborne continuous particle replicator has been criticized on several points, including: (a) the nonstatis- tical size of the sample; (b) the possibility of particle breakup producing misleading numbers of ice particles; and (c) the unknown collection efficiency of the sampling boom due to pressure fluctuations and flow in and out of the boom. Niemann and Mee (1970) have completed the analysis of the 1968 cloud hydrometeor data for the Experimental Meteorology Laboratory. Occasionally they found gross discrepancies in the data, even as regards the presence or absence of ice. Figure G-5 presents an appraisal of the possible data hand- ling problems as the usefulness of the instrument is limited by one's ability to interpret the data it presents. It ap- pears that the criticisms above (a, b, and c) are not limiting

G-8

the v i n s t e m i s j u thems ure G that pect ( perh the t error to es

al ue o ad, t h dgment el ves -5, al o c c a s i to mis aps 10 i m e ) b , the tima te

f the data e p o s s i b i 1 s of the d are i nvol v 1 i n a 1 1 , onal ly one i nterpret

to 20 per ut , accept device can

the tract

, but

i ty of

a ta

e d . F i g -

says

can ex- the data cent of i n g this

be used ion ice.

CONCLUSIONS

that i ce s tor -5°C ment (196 us i n here s tor i ns t es ti come

Thes

c o n s i d can occ ms a t t , an ob

with t 7) but g data

are of ms . Bu ruments mates o

more r

e data erabl e ur i n empera servat he wor in con from H

a 1 im t , as

and d f the el i a b 1

i nd amo trop ture i on k of trad urri i ted data ata f rac e .

i ca te unts of i cal s above in agree

R u s k i n i c t i o n t cane Gl a nature from mo r e d u c t i o t i o n ice

100

80

t-

LJ LJ

en

CO

<

60

40

20 x

I l I I

SIZE 8 SHAPE INDICATES ACCURACY Staggered measurements by different observers Measurements at different times TD « 14, Temp~ -3 to "4°C

+

0

20 40 60 80

MEASUREMENT NO. 1

100

Figure G-5. The accuracy of the measurement of the frac- tion ice with the continuous particle replicator .

o the findings of Sheets (1969) dys . However, the data presented and may not apply to mature re storms are analyzed and our n techniques are improved, our in tropical storms should be-

MacCready, P. I sampl er

REFERENCES

, and C. J. Todd (1964): Continuous particle

Journal of Applied Meteorology 3 3} pp. 450-460

Niemann, B. L., and T. R. Mee (1970): Analysis of cloud par- ticle samples for ESSA-NRL cumulus experiments. Final Report to Experimental Meteorology Branch, ESSA, Miami , Fla., Contract E22-96-69 (N ) , p. 8.

Patrick, J., and A. Gag in (1971): Ice crystals in cumulus

cl ouds--prel imi nary results, Studies of the microphys- ical aspects of cloud processes leading to the forma- tion of precipitation. Report No. 4, The Hebrew Uni- versity of Jerusalem, Dept. of Meteorology, Cloud and Rain Physics Laboratory.

G-9

Ruskin, R. E. (1967): Measurements of water-ice budget charges at -5°C in Agl-seeded tropical cumulus. Journal of Applied Meteorology 3 63 pp. 72-81.

Sheets, R. C. (1969): Preliminary analysis of cloud physics data collected in Hurricane Gladys (1968). Project STORMFURY Annual Report 1969, U.S. Dept. of Navy and U.S. Dept. of Commerce, Appendix D.

Spyers-Duran , P. A., and R. R. Braham, Jr. (1967): An air- borne continuous cloud particle replicator. Journal of Applied Meteorology 3 63 pp. 1108-1113.

G-10

APPENDIX H

ICE-PHASE MODIFICATION POTENTIAL OF CUMULUS CLOUDS IN HURRICANES

David A. Matthews Navy Weather Research Facility

INTRODUCTION

cumul u modi f i natura cl oud verti c modi f i steady et al . test t may be that a s e e d i n

An e s cl o c a t i o 1 and virtu al ve c a t i o -stat , 197 he su

real re di g are

x a m i n a t i u d s in a n potent modi f i e al tempe locity m n potent e cumul u 1). Mod ggestion ized by spl aced a .

on of hurr i al i d (1) ratur a x i m u i a 1 i s mod i f i c a s (Ge s e e d i s 1 i g h

i ce- i c a n e s def

rai n e dep m , an s pre el (W tion ntry , ng 1 e tly o

phase envi i ned fall , artur d (5) di cte e i n s t poten 1971 ss f u utwar

modi ronme as th

(2) e fro

hei g d by ei n a ti al ) tha lly d d fro

f i c a t i o n t is p e diffe surface m the e ht of c a one-d n d D a v i resul ts t i n c r e evel ope m the p

n pote resent rence

press nvi ron 1 oud t imensi s, 196

are u ased e d cumu resent

n t i a 1 of ed. The between ure , (3) ment , (4) ops. The onal 8; Lowe sed to f fects 1 us eel 1 s eyewal 1

This paper will describe the decreases in surface pres sure, the increases in rainfall, and the increases in cloud top height as derived from model simulation of ice-phase modi fi cation using 87 soundings observed within 100 n miles of hurricane eyes as well as five average hurricane soundings from Sheets (1969) .

CLOUD MODEL

The Pennsylvania State University-Navy Weather Research Facility one-dimensional cumulus model (Lowe et al . , 1971) was used to determine the modification potential. This model per- forms an integration of the vertical equation of kinetic energy for a rising cloud tower (a rising parcel in the cloud core). The basic physical assumptions of the model are as follows:

(1) None of the physical parameters investigated varies with time.

(2)

(3) (4) (5)

(6)

(7)

The

trai

Entr

towe

Vert

of b

Clou

dens

1 eve

1 i qu

grow

of d

CI ou

tion

dew

Seed

at a

cloud t n i n g j e ai nment r radiu i cal ac uoyancy d buoya a t i o n u 1 , late id wate t h is s eposi ti d base

1 evel point v i n g is

specif

ower exa t.

is inve s . c e 1 e r a t i

forces ncy is g p to the nt heat r stimul ol ely a on .

is 1 o c a t (CCL) ba al ues . simul ate ied temp

mined has the form of an en-

rsely proportional to the cloud

on is expressed as a function and drag forces, enerated by latent heat of con- level of nucleation. At this of fusion from freezing all ates buoyancy. Subsequent result of the released heat

ed at the convective condensa- sed on surface temperature and

d by freezing all liquid water erature .

Seeding was simulated by using two nucleation tempera- tures, permitting an examination of the effects of different seeding materials. Temperatures of -5°C and -10°C simulated seeding by an Agl -NH.+ I-acetone system and an Agl «NaI-acetone system, respectively (see app. E).

Cloud core radii were selected to correspond with those selected by Sheets (1969). Cloud bases located at the CCL were found to be in agreement with those assumed by Sheets; however, they were generally about 200 m higher (see table H-l).

Table H-l. A Comparison of Cloud Bases Selected by Sheets (1969) and Those Corresponding to the Convective Condensa- tion Level (CCL) for the Same Five Average Soundings . Sam- ple Size from Which the Average Soundings Were Compiled Is Also Shown.

Surface Pressure (mb)

Cloud Base Sheets

CCL (m)

Sampl e Size

P

<

995

200

443

995

<

P

<

999

200,

300

415

1000

<

P

<

1004

300,

500

492

1005

<

P

<

1009

500,

750

720

1010

<

P

<

1014

500,

750

997

8 12 19 26 22

H-2

DISCUSSION OF MODIFICATION POTENTIAL RESULTS

Table H-2 presents average values of model results and the modification potential for five average hurricane soundings presented by Sheets (1969). The results of three cloud radii (1.5, 3.2, 5.0 km) and three nucleation temperatures (-5°, -10°, -25°C) are presented. The -5° and -10°C temperatures simulated artificial modification by Agl and Agl'Nal ice nuclei, respectively; the -25°C temperature simulated natural f reezi ng .

Average values of cloud model results for the modified clouds in table H-2(a) show increases over values for the natural cloud. In table H-2(b) a comparison of seeding with Agl ice nuclei (-5°C) and Agl-Nal ice nuclei (-10°C) shows significant increases in the average values over those of natural nucleation. The rainfall and surface pressure values in table H-2(c) for the -5°C nucleation temperature are 8 and 63 percent higher, respectively, than those values at -10°C. This difference indicates that the Agl ice nuclei may be ex- pected to be somewhat more effective than AgI*NaI ice nuclei in glaciating clouds. The use of a seeding material active

Table H-2. Modification 'Potential Results

1 2

a) Average Values From the Natural Cloud and the Modified Clouds

Nucleation Temp. (°C)

-5

10

•25

-5

10 -25

-10

■25

-5 -10

25

10 -25

Radi u: (km)

Rainfall

(in)

Base Press . Change ( mb )

Cloud Top (m)

Vi rt . Temp . Depart . (°C]

Max. Ve (tn sec"

')

1.5 3.32.92.2 0.5 0.4 3.2 5.2 5.1 4.8 1.3 1.3 5.0 5.9 5.7 5.6 2.3 2.1

0.2 11094 10174 8254 1 .0 13050 1 3174 12454 1 .7 14094 13814 1 3854

1.9 1.9 1.7

3.6 3.5 3.4 4.2 4.4 4.2

4.4 9 13.8 13 17.4 18

.4 9.3 .0 11.9 .2 14.9

Nucl e

Temp .

(b) Differences in Average Values Between the Modified Clouds and

Cloud a ti on r (°C) "J

the Natural

10

-5

10

-10

-5

10

Nucleation temperature -25°C. Nucleation temperature -5°, - 1 C .

•10

1 .5

1 .1

0.7

0.2

0.2

2840

2400

0.5

0.3

0.6

0.7

3.2

0.4

0.3

0.2

0.3

750

720

0.2

0.2

3.1

2.1

5.0

0.3

0.1

0.6

0.4

400

-50

0.3

0.2

3.7

3.2

(c

) Avera

ge Percent Chan

ges of

Modi fi cat i

on Potei

1 1 i a 1

Nucleation Temp. (°C)

-5

-10

-5

-10

-5

-10

-5

-10

-5

-10

1.5

50%

42%

187%

124%

40%

32%

46%

19%

7%

7%

3.2

9%

8%

58%

60%

10%

9%

7%

6%

25%

16%

5.0

9%

4%

34%

21%

3%

-.2%

10%

8%

25%

22%

H-3

at warmer temperatures al clouds (whose tops have r levels) earlier in their colder activation tempera

The greatest chang 1.5 km radius. This re la perty of one-dimensional qualitatively valid. The as fol 1 ows :

( 1 ) In the model t latent heat of the hydrometeo total increase upon the verti meteor content must produce s upper level hy set the effect t i o n level.

(2) The maximum gr i s often 1 i mi t which prevent

i f i cations in lesser entrain clouds permit ble layers and the increased smal 1 er radi i 1 ayers , thus r increase of to

(3) Large radii cl state al ready grow only slig many larger ra experiments sh meteor content this is a qual quantitative i model resul ts , These models d flow at the to permit a net i saturated air. val i di ty of th sul ts .

so enables modification of smaller eached -5°C levels but not -10°C development than does material having tures .

e in potential occurs in clouds of tionship is to some extent the pro- steady-state models and, at best, is explanation for the relationship is

he initial effect of the additional fusion from seeding will decrease r concentration by evaporation. The

in rainfall is directly dependent cally integrated increase of hydro- ; hence, the net effect of seeding ufficient cloud growth to increase drometeor content to more than off- of increased warming at the glacia-

owth o ed by growth the am ment r them t

grow buoyan cl ouds e s u 1 1 i tal hy ouds , have t htly t d i i c 1 ow a n

(see i tati v nterpr

i n th o not p of t ncreas Howe e qual

f uns the h

thro b i e n t ates o pen up to cy fr

to p ng in drome howev ops a hroug ouds et de Lowe ely v etati i s re accom hese e i n ver , i tati

eeded smal igher entr ugh smal 1 ,

atmospher of unseede etrate the

the tropo om seeding ush throug

a large n teor conte er, which t the trop h seeding, in o n e - d i m crease in et al . , 19 alid relat on of one- spec t , is modate the 1 arge cl ou the total experi ence ve aspects

1 radii c ainment r

stable s e. Where d 1 arger se smal 1 , pause . H

permi ts h any sta et growth nt .

in the u n opause , w As a re ensi onal total hyd 71). Whi i o n s h i p , dimensi on not valid

i ncreas e ds and do upward fl

supports

of model

1 ouds ates trat- as radi i

s ta- ence , the ble

and

seeded

ill

suit,

model

ro-

le

strict

al

d out-

not ux of

the

re-

Within the limitations of the one-dimensional model and the sounding data used, the modification potential of average cloud top heights shows increases in cloud top heights of 2800 m for 1.5 km and 750 m for 5.0 km cloud-core radii.

H-4

Ex sounding 1 i s h e d by those of average h Cloud mod surface p and H-2(a into five g o r i e s . model , an averaged . the avera soundings

a m i n a t i o 1 oca ti on

five s u Sheets ( u r r i c a n e el resul ressures ) , and H

groups

Each sou

d the mo

Fi gure

ge modif

n of mo rel ati

rface p 1969) (

s o u n d i ts of m

are pr -2(b). a c c o r d i n d i n g w di f i cat s H-l (c i c a t i o n

d i f i c ve to ressu see t ngs c o d i f i esent

The ng to i t h i n ion p ), H-

pote

a t i o n

the h re cat able H orresp cati on ed in 87 sou the s a gro o t e n t i Kd), n t i a 1

potent u r r i c a e g o r i e

-1). o n d i n g poten f i gure n d i n g s ame su up was a 1 wit H-2(c) of the

i al a ne ce s cor Sheet

to t tial s H-l

were rface

exam hi n e , and

f i ve

s a fun

nter wa

respond

s d e r i v

hese ca

for the

(a), H-

al so d

pressu

i n e d w i

ach gro

H-2(d)

groups

c t i o n of s accomp' ing to ed five t e g o r i e s s e five Kb), i v i d e d re cate- th the up was

present

of

radii modi f i H-l(b) of 100 from 1 than t s i s t e n ures b cation is a 1 s two mo of pat t i m u m h u r r i c

Figu there catio , thi 0 mb. 015 m he in t for oth f

pote o con d i f i c tern modi f ane c

res H

may n pot s pre The b to d i v i d

all or f i n t i a 1 s i s t e a t i o n adds i c a t i enter

-1 an be a e n t i a f erre

patt 1005 ual m plots ve av

for nt fo

nucl f urth on po

d H-2 prefer 1 in h d 1 oca ern of mb is, a x i m u m of mo erage f i ve g r the eati on er sup t e n t i a

i ndi ca

red pr

u r r i c a

t i o n a

i ncre

howev

at 10

d i f i c a

soundi

roups

three

tempe port t 1 ard

te th essur nes . ppear a s i n g er, p

00 mb ti on ngs a of so cloud ratur oar

1 ocat

at fo e 1 oc

In f s at

modi robab . Th poten nd fo u n d i n

radi es . el ati ion w

r cloud a t i o n f i g u r e s a surfa f i c a t i o ly more is patt tial in r avera gs . Th i exami This co onshi p ith res

s of 1 or opt H-l(a) ce pre n pote

i mpor ern is

these ge mod i s pat ned an nsi s te betwee pect t

. 5 km i mum and ssure n t i a 1 tant con- fig- ifi- tern d the ncy n op- o the

The pattern of high modification potential at 995-1005 mb suggests the existence of cumuli which have vertical growth arrested by small stable stratifications induced in the ambient air, but which are high enough to permit the unseeded cloud tops to reach nucleation temperature. Sounding data were not available with lower pressures to check the potential at smal- ler radii. The pattern of decrease of potential with further increasing pressure (to 1010 mb), however, suggests that stable stratifications and upper level dryness restrict the cloud tops to levels below the required nucleation tempera- ture in which case the clouds would not respond to silver iodide seeding. This restriction in cloud tops is consistent with the pattern of tropical hurricane structures discussed by Palmen and Newton (1970).

H-5

CLOUD RADIUS = 1.5 km NUCLEATION TEMPERATURE = -5C

MODIFICATION POTENTIAL OF 5 AVERAGE SOUNDINGS

995 IOOO 1009 1010 1015 (mb) SURFACE PRES.'.URE

995 IOOO 1005 1010 1015 (mb) SURFACE PRESSURE

MODIFICA TION POTENTIAL OF 5 GROUPS OF INDIVIDUAL SOUNDINGS

4H

z 3 <

I

UJ

3

S OH

m

d

J L

(c)

995 IOOO 1005 1010 1015 (mb) SURFACE PRESSURE

4O0H UJ

£2 300-

200-

u

or

LU

a

100-

0-

-loo-

(d)

J L

995 IOOO 1005 1010 101^ ( mb I SURFACE PRESSURE

AZ , CLOUD TOP CHANGE (km)

AR, RAINFALL CHANGE (in) x

AP, CLOUD BASE PRESSURE CHANGE (mb) o

Figure H-l. Modification potential vs. surface pressure (-5°C nucleation temperature) . Modification potential is divided into three categories : Cloud top change from natural cloud top 3 rainfall change, and surface pressure changes for clouds modified at -5°C. Both values of modification poten- tial (a} c) and percentage changes (b 3 d) in modification potential are shown for five average soundings (a3 b) and five groups of individual soundings (c3 d) .

CLOUD RADIUS = 1.5 km NUCLEATION TEMPERATURE = -IOC

MODIFICATION POTENTIAL OF 5 AVERAGE SOUNDINGS

995 IOOO 1003 1010 1015 (mb) SURFACE PRESSURE

100

995 IOOO 1003 1010 1015 (mb) SURFACE PRESSURE

MODIFICATION POTENTIAL OF 5 GROUPS OF INDIVIDUAL SOUNDINGS

3-

LU

z <

I

u 2

UJ

t: h

8 o.

CD <

(c.)

993 IOOO 1005 1010 1013 SURFACE PRESSURE

( mb)

400'

UJ

| 300-

<

5 200-1

z

LU O

or

UJ

a.

100-

0-

-100'

J L

(d.)

995 IOOO 1005 1010 IOIS (mb) SURFACE PRESSURE

AZ , CLOUD TOP CHANGE (km)

AR, RAINFALL CHANGE (in) x

AP, CLOUD BASE PRESSURE CHANGE (mb)

Figure H-2. Modification potential vs. surface pressure (-10°C nucleation temperature) . Modification potential is divided into three categories : Cloud top change from natural cloud top j rainfall change^ and surface pressure changes for clouds modified at -5°C. Both values of modification poten- tial (a3 c) and percentage changes (b3 d) in modification potential are shown for five average soundings (a} b) and five groups of individual sounding s (c3 d) .

H-7

CONCLUSIONS

Significant increases in cloud growth, precipitation, and surface pressure change indicated by a one-dimensional model appear to support the latest STORMFURY hypothesis which postulates these increases from seeding. However, the effect of these increases on the storm's maximum winds still needs to be demonstrated.

Preferred seeding distances from the eye appear to exist in the hurricane environment. These may be a function of seeding material, cloud top temperature, and cloud radii.

RECOMMENDATIONS

(1) A detailed study of modification pote ious regions of the hurricane should be made usi data and cloud models. Such a study would provi information on regions of optimum modification p Dropsonde data should be collected from the 100- level down to the surface. These soundings coul using a WC-135 flying at 40,000 ft in a large "f pattern centered on the hurricane eye. Dropsond 10 minutes during a 1-hour pattern would provide data at systematic intervals from the eye in dif of the hurricane.

(2) Improved convective models would help mum seeding regions and levels for hurricane aba rect transmission of dropsonde data from reconna craft to ground computer facilities would enable cloud model analysis of modification potential t seeding operations.

(3) A study of cloud top temperatures thr ricane would also provide information on which r optimum cloud populations for modification.

(4) The feasibility of warm cloud modific to cold cloud modification should be examined be cloud modification may permit growth of small wa temperatures at which cold cloud modification wi tive. The combined use of warm cloud and cold c cation techniques would permit selective seeding without cloud top temperature restrictions.

ntial of var- ng dropsonde de val uabl e o tenti al .

to 200-mb d be made i gure-ei gh t " es made every

soundi ng ferent regions

define opti- tement. Di- issance air- real -time hroughout

oughout a hur- egions have

a t i o n prior cause warm rm clouds to 1 1 be ef fec- loud modifi- i n all regions

H-8

REFERENCES

Gentry, R. C. (1971): Progress on hurricane modification

research-October 1969 to October 1970. Presented at

Twelfth Inter agency Conference on Weather Modification, October 28-30, Virginia Beach, Va .

Lowe, P. R., D. C. Schertz and D. A. Matthews (1971): A

climatology of cumulus seeding potential for the Wes- tern United States. WEARSCHFAC Technical Paper No. 4- 71, 78 pp.

Palmen, E., and C. Newton (1969): Atmospheric Circulation Systems. Academic Press, N.Y., pp. 471-522.

Sheets, R. C. (1969): Computations of the seedability of clouds in the environment of a hurricane. Project STORMFURY Annual Report 1968, U.S. Dept. of Navy and U.S. Dept. of Commerce, Appendix E.

Weinstein, A. I., and L. G. Davis (1968): A parameterized model of cumulus convection. Report No. 11 to NSF, NSFGA-777, 41 pp.

H-9

APPENDIX I

USE OF LIGHT AIRCRAFT IN STORMFURY ACTIVITIES

Dr. S. D. Elliott, Jr., and Dr. William G. Finnegan Naval Weapons Center

INTRODUCTION

During the past three STORMFURY operating seasons, the Naval Weapons Center (NWC) has made one or two Navy-leased or contractor operated light aircraft available to the program for use during dry -run and cloudline experiment periods. This type of aircraft has provided a mainstay to other NWC programs in weather investigation and modification, and the opportun- ity was welcomed, both to pass on NWC experience in the effec- tive employment of such aircraft to other STORMFURY partici- pants, and to assess their utility in the STORMFURY operational context. As a result of three seasons' experience, some con- clusions may be drawn on this topic and some recommendations offered for future STORMFURY activities.

BACKGROUND

In 1965 and 1966, NWC participation in STORMFURY in- cluded making available an A3B jet aircraft and crew to aug- ment the RA3B's of VAP 62 in their employment as seeders. This aircraft and its military crew participated in both dry- runs, in the 1965 cumulus cloud experiments (Simpson et al . , 1965) and in the aborted deployments for Betsy in 1965 (STORMFURY Annual Report 1965) and Faith in 1966 (STORMFURY Annual Report 1966). Unfortunately, the NWC A3B was lost in 1967 on a cross-country flight.

In 1967 the Naval Air Facility (NAF), China Lake, made arrangements for long-term leasing of a Cessna 210 single- engine, high-wing, four-place aircraft (fig. 1-1). Equipped with retractable landing gear, full IFR instrumentation, a built-in oxygen system, and a turbo-charged engine, this 210, registry number N6877R, was capable of airspeeds in excess of 200 mph, altitudes exceeding 30,000 feet, and flight dur- ations of 5 hours or more. Special meteorological instrumen- tation was installed, and external racks designed to accom- modate a variety of attached and air-dropped pyrotechnic

Figure 1-1. Navy-leased Cessna 210 ( 7 7R) . Streamlined rack for STOBMFURY type air-dropped flares on pent wing ^ boom for burn-in-place flares on starboard wing.

nucleant generators. This aircraft and similar contractor- operated aircraft provided economical and flexible tools for the development and assessment of weather modification tech- niques in numerous experimental projects.

The 1968 STORMFURY schedule (Project STORMFURY, Opera- tion Plan No. 1-68) called for a dry-run exercise based at Naval Station Roosevelt Roads, Puerto Rico, with a briefing session on Monday, 5 August, and eyewall and rainband dry- runs on the 6th and 7th, the latter also to incorporate a test of the proposed cloudline experiment procedures. Cessna 210(77R) was flown to Puerto Rico for the week of 5-9 August and provided orientation and indoctrination for STORMFURY participants in current Navy-developed seeding techniques.

For 1969, the cloudline exercises were expanded to a full-scale experimental program scheduled to take place dur- ing the period 9 through 19 September (Project STORMFURY, Op- eration Plan No. 1-69). For this program, NWC made available two contractor-operated Cessna 401 low-wing, twin-engine, six to-eight place aircraft (fig. 1-2), having performance com- parable to that of the 210 but with considerably greater

1-2

paylo Opera a pro devel only N3221 had f the 4 a i r c r voi da 80 n carry terna Debbi ro tec e n v i r a i r c r two N

ad c a p a c i t i o n s , In totype me oped by t three sea 0Q, opera ive seats 01 permit aft were nee radar miles d i s and d i s p 1 1 y s i m i 1 e , but 1 o h n i c m i x t onment (P aft sched OAA DC-6'

ty. One 40 c. , of Holl teorol ogi ca he NWC Avia t s a v a i 1 a b 1 ted by Weat

available, s the use o equipped w i

systems co tance. Bot ense 52 STO ar to the S aded with a ure better roject STOR uled to par s , two Navy

1 , N32 i ster , 1 data t i o n 0 e for her Se

The f a no th Ben veri ng h aire RMFURY TORMFU

short sui ted MFURY t i c i p a

WC-12

20Q, operat Cal i form" a sensing an rdnance Dep passengers . rvi ce , Inc . twi n-engi ne se-mounted dix RDR-100 a 90 degre raft were a III a i r - d r RY I units er burning

to the clo Annual Repo te in these 1 N ' s , and a

ed by Met , was equ d recordi artmen t ,

The sec , Norman,

conf i gur radar, an

K-band w e forward 1 so equip opped fla used on H grain of udl i ne op rt, 1969)

exerci se

USAF WC-

eorologi cal i p p e d with ng system 1 eavi ng ond 401 ,

Okl ahoma , a t i o n of d both eather a-

sector to ped to res, ex- urri cane EW-20 py- erational . Other s were the 130.

All forces gathered at Naval Station Roosevelt Roads on 8 September. Cloudline experiments were conducted on 7 days during the period 9 through 18 September. The normal proce- dure was for the USAF WC-130 to depart Ramey AFB about 0900 local to scout the assigned operating areas for suitable cloud

Figure 1-2. Cessna 401 (20Q) in flight over NAVSTA Roosevelt Roads3 Puerto Rico ( STORMFURY Cloudline Experiments } Sep^ tember 1969).

1-3

groups. When these were located, within a range of 100 t n miles to the northeast or southeast of Roosevelt Roads, WC-121N's and DC-6's departed to take up their stations a establish radar surveillance and traffic control patterns 1 21 N ' s at 4,000 and 7,000 ft, on racetrack paths parallel and to either side of the cloudline) and instrumented pen tration and photographic tracks (DC-6's at cloud base and 18,000 ft, in a squared "figure-eight" around and through target group). The first 401 departed the base shortly a ward, rendezvoused with the other aircraft once the latte pre-seeding flight patterns had been established, and spe 60 to 90 minutes alternately seeding updrafts and growing cells at 18-19,000 ft (-5°C to -7°C) and withdrawing to c the area for penetration by the upper-level DC-6. If con tions warranted, the second 401 was called out from Roose Roads about 90 minutes after the first, and either contin seeding the selected group or joined the other aircraft a newly selected target. The two 401 's participated in six (20Q) and five (21Q) missions, flying a total of 30.5 hou normally carrying three Project officials and observers e Approximately 125 STORMFURY III flares were fired into cl line targets. In addition to seeding and indoctrination seeding procedures, the 401's provided photographic and v ual coverage of the experiment and aided in target select Only limited use of the instrument package installed aboa 20Q was made, but the potentialities of the system and pr cedures for its maintenance and use under field condition were established. Otherwise, aircraft performance was ex lent, only one mission being aborted due to a pyrotechnic rack wiring problem aboard 20Q; 21Q was, however, able to take over and complete the mission. In addition, both 40 were used on a stand-down day for a 1.5-hour air-to-air p tography mission, yielding valuable motion picture footag which has since been incorporated in NWC documentary film The aircraft were also used for several logistic flights transport personnel and equipment between Roosevelt Roads San Juan .

0 250 the

nd

(WC-

to e-

the f ter- rs nt

1 ear di- vel t ued

t a

rs , ach . oud- i n i s- ion. rd o- s eel -

1 's

ho- e

s . to and

as en es tab trol Addi t beha v array key p to Na vidua h i g h - cl oud avai 1 Annua

Opera ti rely 1 i s h i n g procedu i o n a 1 1 y i o r of s s i m i 1 ersonne vy deve 1 cloud perform line ex abi 1 i ty 1 Repor

t i o n a succe

the res t , val natur ar to 1 in 1 oped s , wh ance p e r i m

and t, 19

iiy.

ssf ul fligh o be uabl e al an

hurr the S

proc i ch w A6 je ents capab 69) .

the c i n a t pat used

mete d art i c a n e T0RMF edure oul d t see was t il i ti

1 oudl i c h i e v i terns , in fut orol og i f i c i a rai nb URY pr s for not ha der ai hus du es of

ne expe ng thei and co ure ST0 i c a 1 da 1 ly mod ands . ogram w sel ecti ve been rcraf t . e in no 20Q and

ri men

r pri

mmuni

RMFUR

ta we

i f i e d

Final

ere d

ng an

poss

The

smal

21Q

ts were mary pu cations Y opera re secu

1 i near ly, mos i recti y d seedi i b 1 e w i

succes 1 measu (Projec

regarded rpose of

and con- tions . red on the

cl oud t of the

exposed n g i ndi - th the s of the re to the t STORMFURY

1-4

1970 DRY-RUN/ CLOUDLINE OPERATIONS

ul ed

run

(Pro

vi ou

had

the

deve

fore

by t

a da

spac

Wedn

ing

sonn

ti on

i ndo

stan

miss

flar

On t

expe

1 21 N

Cess

I n s

tal

appr

were

flig

prov

expe

Fo for exerc ject s yea been WMU-2 1 oped deci he NW ta-co e. T esday m i s s i el i n al ac c t r i n d-dow ion t es un he 27 ri men 1 s , a na de ummar fligh o x i m a f i re hts w i ded ri men

r 1970, t the perio ises 20-2 STORMFURY r , one of equipped type, wh acetone- ded that C staff, "Meeting he Cessna , 23 July o n s , d u r i v o 1 v e d in t i v i t i e s a t i o n in n day, me o test tw der consi th, 28th, ts togeth nd the WC parted fo y, 21Q ma ts , for a tely 80 r d . I n ad ere condu a s i g n i f i tal a c t i v

he STORMFURY d 24-31 July 3 July at Na

Operation 0

the NOAA DC to dispense ile the DC-6 burning nucl only one Ces equipped for system in or

arrived in . On the 24 ng which var

ordnance de connected wi seeding proc mbers of the o newly deve deration for

and 29th, 2 er with the -130. On th r China Lake de a total o

total durat ounds of var dition, seve cted. These cant contrib i t i e s .

CI oudl i , immedi val Stat rder No. -6's (39 ST0RMFUR

a d d i t i o eant gen sna 401

ai r-dro der to r Puerto R th and 2 i o u s mil vel opmen th STORM edures .

NWC sta loped ty

future 1 Q parti two DC-6 e e v e n i n , to mee f eight ion of 1 ious typ ral phot

1 i ght a ution to

ne exerc ately fo ion Roos

1-70). C) as we Y pyrote nal ly ca era tor . (21 Q) wo pped fla etain ma i c o on t 5th it f itary an t, seedi FURY rec

On the ff flew pes of a ST0RMFUR ci pated 's, the g of the t other trai ni ng 7 . 7 hour es of py ographi c i rcraf t

ST0RMFU

i ses w 1 1 owi n evel t

Duri n 11 as c h n i c r r i e d

It wa u 1 d be res bu x i m u m he eve 1 ew f o d civi ng , an e i v e d 26th, an exp i r - d r o Y appl in c 1 o B-57,

29th, commi t

and e s , dur rotech

and 1 thus o RY tra

ere s g the Roads g the the B fl are an RF s the

brou t wit seati ning ur tr 1 i an d ope i nten a pro erime pped i c a t i udl i n two W

the ments x p e r i i ng w ni c f o g i s t nee a i ni ng

ched- dry-

pre- -57 s of F- re- ght hout

ng

of

ai n-

per-

ra-

s i ve

ject

ntal

ons .

e

C-

men- hi ch 1 ares i c

gain and

CONCLUSIONS

Experience with the use of light aircraft in connection with STORMFURY activities, as cited above, leads to certain conclusions regarding their utility in the following fields:

(a) Training. NWC-sponsored light aircraft provided training in seeding techniques pertinent to the hurricane environment for key STORMFURY personnel during one flight in 1968 and four in 1970, in connection with the dry-run exer- cises. The cloudline experiments in 1969 and 1970 provided further opportunities for such indoctrination. This was ac- complished at much lower cost ($50 per flight hour for the single-engined 210, and $100 per hour for the 401 twin), and

1-5

with much greater flexibility than woul had the larger aircraft employed in STO ations been used for this task. This u be continued during future STORMFURY se

(b) Independent Experiments . As pyrotechnic tests conducted on 26 July the tests carried out during the 1969 a ercises, these light aircraft are ideal ing of novel seeding materials and tech either alone, or in conjunction with at craft. It is essential that such tests maximum flexibility in operations, sine have only limited predictability. Such be carried out in future seasons, as ne systems are developed.

(c) Organized Experiments . The aircraft in complex, preplanned operati other airplanes is more limited, althou Although the Cessna 210 and 401 aircraf capabilities not significantly inferior W C - 1 2 1 N ' s and superior in the case of a flight duration (4^ to 5 hours for over a full passenger load, and 2 to 3 hours altitude flight) requires their use in and with the B-57 in 1970) for protract larly, their maximum effective operatin approximately 250 miles, when coupled w that experimental activities be conduct at sea (to avoid complications inherent trolled airspace) limits their usefulne are scarce. It should be noted, howeve aircraft such as the A6 and B-57 are si flight duration, although not in range, and radio equipment (VHF only) are also range use at sea. Within these limitat ued use of light aircraft in cloudline des i rabl e .

(d) Hurriaane Operations . It is aircraft of this class would be of any hurricane seeding operation, except pos in which outlying rainbands pass relati able operating base.

(e) Miscellaneous . On many occa 3 years, the NWC-provided aircraft prov rapid, and flexible means for transport ment. They also proved highly effectiv graphy for both documentation and data

d have been the case RMFURY hurricane oper- se shoul d def i ni tely asons .

exemplified by the 1970 and by some of nd 1970 cloudline e x -

for preliminary test- niques, operati ng

most , two other ai r-

be pi anned to permi t e the results obtained

tests will undoubtedly w nucleant-generating

util ons gh s t ha

to 1 ti t -wat

of rela ed e

g ra i th ed a

i n

ss w

r, t

mi 1 a

Av

uns ions expe

i ty of th i nvol vi ng till subs ve perfor the DC-6' u d e , t h e i er operat oxygen fo y s (as in xperimen t d i u s at s the requi t 1 east 1 the use o hen s u i t a hat high- r 1 y limit a i 1 a b 1 e n u i t e d for , however riments a

e 1 ight

several tanti al . mance s and r 1 i mi ted i ons wi th r high

1969, s . S i m i - ea of rement 00 n miles f con- bl e cl ouds performance ed in a v i g a t i o n

long , conti n- ppears

doubtful whether light utility in an actual sibly in a situation vely close to a suit- si ons during the last ided an inexpensive, ing personnel and equip e in obtaining photo- assessment purposes.

1-6

It thus appears that continued use of at least one light aircraft (preferably twin-engined for safety and per- formance reasons) is desirable for future STORMFURY seasons, at least in connection with dry-run, cloudline and equivalent activities. The Naval Weapons Center, plans to continue pro- viding this c a p a b i 1 i ty .

REFERENCES

Simpson, J., et al . (1965): STORMFURY Cumulus Seeding Experi- ment, 1965, Preliminary Summary, Project STORMFURY Re- port No. 1-65. U.S. Navy/Weather Bureau, 1 November.

STORMFURY Staff (1966): Project STORMFURY Annual Report,

1965. U.S. Dept. of Navy and U.S. Dept. of Commerce.

STORMFURY Staff (1967): Project STORMFURY Annual Report,

1966. U.S. Dept. of Navy and U.S. Dept. of Commerce.

STORMFURY Staff (1968): Project STORMFURY Operation Plan

No. 1-6 8. U.S. Fleet Weather Facility, Jacksonville, Florida. p . D-l .

STORMFURY Staff (1969): Project STORMFURY Operation Plan

No. 1-69. U.S. Fleet Weather Facility, Jacksonville, Florida. p. G-l.

STORMFURY Staff (1970): Project STORMFURY Annual Report,

1969. U.S. Dept. of Navy and U.S. Dept. of Commerce.

STORMFURY Staff (1970): Project STORMFURY Operation Order

No. 1-70. U.S. Fleet Weather Facility, Jacksonville, Florida. pp. D-I-l , D-V-l .

1-7

APPENDIX J

USE OF ECHO VELOCITIES TO EVALUATE HURRICANE MODIFICATION EXPERIMENTS

Peter G. Black National Hurricane Research Laboratory

ABSTRACT

Echo velocities computed from airborne radar at six time intervals over the entire storm before and during the seeding of Hurri- cane Debbie on 20 August 1969, reveal that mean echo speeds equaled or exceeded cycl ostrophi c winds computed from 12,000-ft. D-value data as well as measured 12,000-ft winds after a correction for water motion was applied. In the time period from just before seeding began to just after seeding ended, azimuthal mean echo speed increases ranging from 30 knots at the 100 n mile radius to 10 knots in the outer eyewall were found. In this same period, the mean echo crossing angle changed from 5 degrees inward to 5 degrees outward at the 100 n mile radius. Deviations about the azimuthal mean echo speed and crossing angle indicated that wave number 2 accounted for nearly all of the variance around the storm's circumference at all radii. The deviations remained fixed in time between radii of 25 and 150 n mile, but rotated with the major axis in the inner and outer eyewalls. It is suggested that these echo motions approximate the air flow in the lower levels of the hurricane.

INTRODUCTION

For some time attention has been focused on the symmet- rical features of the hurricane circulation, with the only asymmetry on the scale larger than that of the rainbands being introduced by the motion of the storm. Aircraft and ship data collected in storms have been too sparse in space and time to

adequately describe other asymmetries of these larger scales. Considerable time variation in wind speed profiles on the rainband scale and smaller through several hurricanes has been measured. This has been attributed to the "natural var- iation" in storm intensity. However, it is a distinct possi- bility that the time change in these wind speed profiles can be partly due to the advection of horizontal asymmetries. Furthermore, in hurricane modification experiments, the pos- sibility exists that the seeding location relative to hori- zontal asymmetries may have an important bearing on the out- come of the experiment.

Therefore, in this report, an attempt has been made to define the low-level asymmetries in a hurricane and their change with time using the motion of small precipitation echoes. Ten-minute time periods were used to define a motion field over a portion of the hurricane circulation within 150 n miles of the storm center. Several of these time periods were composited to give an average 1-hour motion field over the entire hurricane circulation. Radial and azimuthal pro- files of the echo speed and crossing angle were constructed for 6 one-hour time periods. These profiles were compared with aircraft wind measurements where they were available.

canes p a r t i c Florid August motion rel ate and Se 1 a t i o n Conn i e Hel ene He f ou around s torm echo v the ec (1963) a grou ment b the me

Many and a ul ar a to

1949

of i d wel nn (1

of e , Dia

of 1 nd sy

the speed e 1 o c i hoes

comp nd ba etwee an wi

auth ttemp 1 evel compu . He sol at 1 wit 963, cho v ne , a 958; sterna storm , and ties moved uted sed r n the nd be

ors ha

ted to

Li g

te ech

c o i n e ed con h the 1965) e 1 o c i t nd Ion Debra tic v a , with

with with a

s 1 owe echo v adar o

echo tween

ve co rel a da (1 o vel d the v e c t i 700 m have i es w e of of 19 r i a t i day echo i rcra r tha e 1 o c i n Ok i vel oc cl oud

mpute te th 955) o c i t i

term ve ce b win done i t h i n 1955; 59 ; a ons i vs . n cross ft wi n the ties nawa . i t i e s

base

d ech

ese v

used

es in

"spa

lis s

ds.

ex ten

Hurr

Audr

nd pr

n ech

i g h t ,

ing a

nds a

wind

in Ty

He

near

and

o vel o e 1 o c i t land b

the h winds" ince h Senn e s i v e w i c a n e s ey of i n c i p a o vel o

with ngle. nd fou s at a phoon found

r a w i n cloud

cities ies to ased r u r r i c a

to re e said t al . ork on

Edna 1957; lly, d c i ty w

I and v Senn

nd tha

II lev Nancy wery g sonde top .

i n h

wind adar ne of f er t

they (1960

the of 19 Dai sy onna i th a s . se compa t i n els. of 19 ood a s t a t i

urn - s at a i n

23-28 o the

cor- a, 1960b) cal cu- 54;

and of 1960. zimu th a , with red general

Watanabe 61 from gree- ons and

Fujita (1959) used airborne radar to compute echo vel- ocities in Hurricane Carrie of 1957. His technique involved placing each radar photograph at the aircraft position given by the Doppler navigation system and then tracing the succes- sive position of various radar echoes. However, any error in

J-2

the Doppler fix will result in an error in the echo velocity. Jordan (1960) also used airborne radar to compute echo velo- cities in Hurricane Daisy of 1958. He used the hurricane cen ter as a reference point for his calculations. He noted rela tively good agreement between his echo velocities within the eyewall region and aircraft measured winds at 13,000 ft

The ab ship appears particular level

DATA ANALYSIS

the s

were

puted

board

compu

fly in

c a t i o

used

photo

wi th

techn

t i n u i

posit

point

north

the e

In t e e d i n g used . from a WB- ted f r g at 1 ns of to con graphs respec i q u e y ty on i o n i n g and o , resp cho po

his st

exper

Echo

pr imar

47 fly

om the

,000 f

these

struct

taken

t to t

i el ds

the ec

the p

r i e n t a

e c t i v e

s i t i o n

udy , a i ment v e 1 o c i 11 y th i rig at

Navy t. Se radars

p i c t u

at 30 he hur extrem ho mot hotogr t i o n ( ly) wi

when

i r b o r n in Hur ties o e Ai r

39,00 APS-20 e Bl ac Fuj re seq -sec i r i c a n e ely ac ion c a aphs w namely 11 be pro jec

e rad r i c a n vera Force 0 ft. , 10- k et i ta ' s uence nterv

cent curat n be i th r

the immed ted i

ar data e Debbi 1 0 - m i n APS-64 Echo cm rada al . (19 movi e- s using al s whi er and e resul o b t a i n e espect h u r r i c a i ately n movie

col 1 ect e, 20 Au ute peri , 3-cm r v e 1 o c i t i r on boa 71) for loop tec

ai rborn ch had b true nor ts since d , and a to the s ne cente obvi ous

form on

ed du gust od we adar es we rd a the s hni qu e rad een r th.

30 s ny er ame f r and by a

a sc

ri ng 1969, re corn- on

re also WC-121N p e c i f i - e was ar

egistered This ec con- rors in i xed

true jump in reen .

Short period oscillations in the storm speed during the 10-minute interval used for computing echo velocities are not thought to be large enough to bias the echo velocities by more than 1 or 2 knots. Senn (1965) has indicated average fluctuations in the speed of Hurricane Donna on the order of about 5 knots in 1 hour with maximum fluctuations on the or- der of 10 knots in 1 hour. Such fluctuations were not detected in the motion of Hurricane Debbie. However, errors in air- craft navigation and eye location were such that they could have existed.

J-3

Usually, four or five 10-minute average echo velocity fields were composited to obtain the echo velocity field characteristic of a 1-hour time interval. The short period storm motion fluctuations should be sufficiently random to cancel out when the 1-hour composites are compared with each other .

ECHO VELOCITY PROFILES

One-hour echo velocity composites were prepared for the time periods 1100-1200Z, 1600-1700Z, 1700-1800Z, 1800- 1900Z, 1900-2000Z, and 2000-2100Z. Usable data were not available for any other time periods. The above times cover a period from 1 hour before seeding began (about 1200A) to 1 hour after seeding ended (about 2000Z).

The storm was divided into four quadrants defined by perpendicular lines oriented 45 degrees to the left and right of the storm motion vector (310 degrees in this case). All the echo velocity vectors within each quadrant were then com- posited into radial profiles of speed and crossing angle (defined as positive inward). The resulting scatter diagrams for selected time periods are shown in figures J-l to J-3. The mean scatter was about 10 knots for the speed and about 10 degrees for the crossing angle, which is well within the scatter that would be introduced by short period fluctuations in the storm speed. A portion of this scatter (perhaps half) can be accounted for by azimuthal variations in echo velocity as will be seen in a later section.

Relative wind profiles measured by RFF aircraft at 12,000 ft as well as computed cycl ostrophi c wind profiles were superimposed, where available, in the left and right quadrants. The cycl ostrophi c winds were computed from

C =

V

AD

f9 A?

(J.l)

where r is the radius from the storm center, Ar was chosen as 2 n miles, and AD was the D-value gradient which was sub jectively smoothed. Relative winds based on reports from Navy aircraft at 1,000 ft, 6,000 ft, and 10,000 ft are also plotted where available.

J-4

HURRICANE DEBBIE

AUGUST 20, 1969 1100-1200 Z

+ 2<f- -

-20°-

120 100

80

60

40

20 -

J.

I

- +20°

-20°

RIGHT (3) J I I L

120 100 80 60 40 20

140 120 100 80 60 40 20

20 40 60 80 100 120 140

t20"

0'

-20'

120

100

80

60

40

20

_L

J_

FRONT (3) J J I Li

INNER EYE

*e*

OUTER EYE

_L

.—A'.'--'

M>

Qr

BACK (23) J I I I

JL

+20°

-20°

H120 100 80 60

40 20

140 120 100 80 60 40 20 0 20 40 60 80 100 120 140

RADIUS (N.MI.)

RELATIVE ECHO MOTION PROFILE

RELATIVE WIND PROFILE (12,000 FT.)

GRADIENT WIND PROFILE

A ESTIMATED SURFACE

A 1,000 FT. WIND

O 6,000 FT. WIND

10,000 FT. WIND

WIND

Figure J-l. Relative echo speed (bottom panel) and crossing angle (top panel) profiles compared with relative 1 2 , 000- ft wind and cyclostrophic wind profiles , as well as scattered surface, 1,000 ft, 6,000 ft, and 10,000 ft relative wind reports for 1100 to 1200Z, 20 August 1969. The vertical lines indicate the inner edges of the inner and outer eye- walls.

J-5

HURRICANE DEBBIE

AUGUST 20, 1969 1600- 1700 Z

+ 20° -

CO

140 120 100 80 60 40 20

20 40 60 80 100 120 140

CO

+ 20°

-20°

120

100

80

60

40

20

x" . / \-

FRONT (56)

1

i

INNER EYE

«y-

OUTER EYE

f\ i

/V

l'\

I

"13

i

A

l&

BACK (33) i i I

+20'

-?n°

20<

-1120 100 80 60 40 20

140 120 100 80 60 40 20 0 20 40 60 80 100 120 140

RADIUS (N. Ml.)

RELATIVE ECHO MOTION PROFILE

RELATIVE WIND PROFILE (12,000 FT.)

GRADIENT WIND PROFILE

A ESTIMATED SURFACE WIND

1,000 FT. WIND

O 6,000 FT. WIND

10,000 FT. WIND

Figure J-2. Same as figure 1 except for the time period from 1600 to 1700Z3 20 August 1969.

J-6

HURRICANE DEBBIE

AUGUST 20, 1969 1700-1800 Z

+ 20°-

to

140 120 100 80 60 40 20 0 20 40 60 80 100 120 140

CO

+ 20°

1 1 1 1 1 1

i

1 1 1 1 1 1

-* '• •• -"A

-20°

s'r\> •".".* ..' * '*- '-':-

r>

>

*1

INNER EYE

i

<

^"^'A!^-

120

-

01

ITER EYE

100

*

/

1

v0

''t

b

X

80 60

\

/

I

. / /

/

40

* y <* .- x

* ** ^- -* ~*

20

n

FRONT (75) i i i i i i

1

BACK (59)' i i i i i i

+20°

H-20° 120 100 80 60 40 20

140 120 100 80 60 40 20 0 20 40 60 80 100 120 140

RADIUS (N.MI.)

RELATIVE ECHO MOTION PROFILE

RELATIVE WIND PROFILE (12,000 FT.)

GRADIENT WIND PROFILE

A ESTIMATED SURFACE WIND

A 1,000 FT. WIND

O 6,000 FT. WIND

10,000 FT. WIND

Figure J-3. Same as figure 1 except for the time period from 1700 to 1800Z3 20 August 1969.

J-7

The mean location of the inner edge of the inner and outer eyewalls during the hour is indicated by the vertical lines. Seeding times, radii, and azimuths are given in table J-l .

are

12,0

exce

quad

30-5

at 1

rel a

radi

radi

prof

cl OS

of t

to m

cal c

(196

move

1963

wind

75 k

40 n

10 k

show

the

The

wind

cent

wind

the

The results indicate that the mea generally in balance with the cyclos 00 ft. However, in some cases, the ed the cycl os trophi c winds by about rant, 30-40 n miles radius, fig. J-l 0 n miles radius, fig. J -3). The me 2,000 ft appeared to be about 10 kno tive echo speeds and the cyclostroph us of 40 n miles. Where data are av us, there appears to be much closer i 1 es .

n relative echo speeds trophi c wi nds at rel ati ve echo speeds 5 knots (e.g., 1 eft ; and right quadrant, asured relative winds ts less than the mean ic winds out to a ailable beyond that agreement between the

Th troph he mo eas ur ul ate 3 ) wo ment , the s. F nots

mile nots n to radi u Doppl

by 5 er . s bee cycl o

e disc i c win v i n g s e the d. Fi rk by to wi n

data i gure to 100 s of H or mor be nea s of m e r win

to 10 When t ome eq s troph

repancy b d s might ea surfac ai re raft gure J-4 Black et d speed . of Grocot J-4 indie

knots (c u r r i c a n e e woul d b rly paral a x i m u m w i ds would

knots or his cor re ual to an i c winds.

etwee p o s s i e on groun repre al. (

Us i n t wer ates orres Debbi e pos lei t nd (2 thus

more c t i o n d i n

n the bly b the a d spe sents 1967) g dat e ext that pondi e) a s i b 1 e o the 2 n m be an wi th i s a come

rel at e expl i r b o r n ed fro

an ex

i n re a from ended for wi ng to water . The

wind i 1 e s i

under in 40 p p 1 i e d cases

l ve ai ne e Do m wh tens 1 ati

Hur to h nd s thos moti

wat out n th esti n mi , th si ig

wi nds d by t ppl er i ch th ion of ng sea ri cane u r r i c a peeds e meas on of er mot to at e case mate o 1 es of e rel a htly g

and

he e

rada

e wi

Gro

sur

Flo

ne f

rang

ured

from

i on

1 eas

of

f th

the

ti ve

reat

the cy- f f ects r used nds are cott ' s face ra of orce i ng from

wi th i n

5 to has been t twice Debbie) . e true

s to rm

measured er than

Table J-l. Seeding Times and Locations for Hurricane

Debbie, 20 August 1969.

Seeding Time (Z)

Range Interval ( n miles)

Azi muth (from true North)

115630-11 5830 140140-140330 161345-161545 175750-1 75950 195350-195620

15-22 12-25 11-25 12-27 18-34

022-001 044-034 357-351 018-010 356-359

J-8

WM

1

^

(kts)

O - FROM GROCOTT

•/

20

J*

/

*/

10

^i—

o __«—

.

1

**^m

1

-20

10

0

50

WS (kts)

100

Figure J-4. Sea surface water motion (WM) as a function of wind speed (WS) (after Black, 1967; Grocott, 1963).

There are several possible theoretical explanations for the suggested inbalance between cycl os trophi c and measured relative winds. Among these are (1) storm not in steady state (especially true if storm is responding to seeding), (2) frictional accelerations, and (3) vertical and horizontal advection of momentum by the asymmetries.

Relative winds measured at 1,000 ft and surface winds estimated from the appearance of the state of the sea were made generally between radii of 50 and 125 n miles and tended to agree remarkably well. They were in general about 10 knots greater than the mean relative echo speed profiles in the left and back quadrants, but about 15 knots less than the echo speed profiles in the right and front quadrants. Ross (1971), in a recent study, has been able to relate areal coverage of white caps on the sea surface to wind speed at the 20-m level, up to a wind speed of 50 knots. He has found that the 20-m wind is about 20 percent less than the wind at a flight alti- tude of about 1,000 ft. Therefore, it is felt that the esti- mated surface winds are too high and should be reduced by at least 10 to 15 knots. The 6,000 ft and 10,000 ft winds were in relatively good agreement with the echo speed profiles.

J-9

A time history of the mean relative echo speed and crossing angle profiles is given in figure J-5. The figure indicates that the echo speeds tend to increase with time at radii of from 40 to 150 n miles in all quadrants of the storm The increase was on the order of 10 to 20 knots. This result is consistent with the results of Hawkins (1971) which indi- cated an increase in the winds in the left quadrant at radii from 75 to 200 n miles of 10 to 15 knots from well before to well after the seeding experiment. This result is further substantiated by the time change of the azimuthal mean echo speed given in a later section.

It should be noted that the echo speeds fall off most rapidly in the left quadrant, reaching a mean value of about 10 knots at 150 n miles radius. A sharp shear line has been shown to exist in this quadrant at radii larger than 150 n miles by the low-level streamline analysis of Fujita and Black (1970), based on low cloud motions. The echo speeds fall off to about 30 knots at 150 n miles radius in the right and back quadrants. This result is also illustrated clearly in the azimuthal profiles.

Figure J-5 also shows that the crossing angle becomes more negative with time in all quadrants, indicating the echoes are tending to move outward more as time progresses. Of special note is the change evident in the back quadrant where crossing angle changes from 20 degrees inward at 75 n miles radius before seeding to 15 degrees outward after seed- ing are evident.

These results tend to be in the sense anticipated by the numerical modification experiments of Rosenthal (1971) which predicted an increase in the winds outside the seeded eyewall region, even as the maximum wind was reduced and moved outward. Therefore, these results appear to support the contention that a modification of Hurricane Debbie was indeed achieved.

A POSSIBLE MECHANISM GOVERNING ECHO MOTIONS IN A HURRICANE

Some clarification is needed concerning the mechanism responsible for the observed echo velocities. It was men- tioned earlier that in some cases, agreement was found be- tween echo speeds and the 700 mb winds. This is probably fortuitous. Watanabe (1963) has suggested, using rawinsonde data, that echo velocities agree best with the mean wind be- tween the echo base and the echo top, which Senn (see app. !<) has shown is generally not much higher than 30,000 ft. This

J-10

HURRICANE DEBBIE TIME HISTORY OF ECHO

AUGUST 20, 1969 MOTION PROFILES

+ 20° -20° 120 100 80 60 40 20 0

+ 20°

-20°

120

100

80

1 1 1 1 1 1 1

- INFLOW CROSSING

1 1 I I I I ANGLE

1 i

' L'- m f <ii , , _, _ 1 !■

.___"_.- .^•"

■"~*i'.,

-^

OUTFLOW

SPEED

PROFILE

-

•M

h

_

••#

.'.'V.

-

•-'''yy 1

:V V ^ ..

- ^^

I *-»-.

_

^~- ~^^^s'

s

,''■■- LEFT II

RIGHT 1 1 I I I I

1

140 120 100 80 60 40 20

20 40 60 80 100 120 140

</)

60

40

20 -

- /A/FLOW

1 I I

CROSSING

OUTFLOW

SPEED

;/ ,/ I' V

■' »

FRONT

j

J_

JL

I

PROFILE

+20° -20° 120 100 80 60 40 20 0

+20°

-20°

120

\ 100

80

60

40

20

BACK

I L

I

140 120 100 80 60 40 20 0

RADIUS

1100 - 1200 Z

1600- 17002

1700- 1800 Z

Figure J-5. Time change of echo files for four quadrants

20 40 60 80 100 120 140

(N. Ml.)

1800 - 1900 Z

1900 -2000Z

2000-2100Z

speed and crossing angle pro- of Hurricane Debbie.

J-ll

mean wind, in many cases, appears to be nearly that at 10,000 ft (about 700 mb). However, Senn (1965) has observed that in general, echoes move fast early in their lifetime and slower later in their lifetime. Watanabe, in order to account for the scatter in his data about the 700 mb wind, suggests he was observing echo velocities at different stages in their lifetime, and hence moving at different velocities.

I ported b a substa sec" * ) , air near echo may boundary move wit vel oci ty (1971 ) h the shea their t e the rada the echo the low- most of resul tan The echo t i v e of agree be

t is n e h a v i o nti al moves

cloud

be ti , as o h the

is su ave us r , ass rmi nal r i s o

bound level it was t echo

moti o the le tter w

0 w s u g r coul verti c with t base .

1 ted,

u 1 1 i n e 1 ow-1 e s tai ne ed the u m i n g

vel oc bservi ary of speed . taken vel oc n data vel f r ith th

gested d be t al vel he hor

Even due to d by G vel wi d. In

verti preci p i t i e s . ng act

an ac The

from i t i e s

of Jo om 20, e 1 owe

that t hat the ocity ( i z o n t a 1 though

verti c entry e nd spee

fact S c a 1 til i t a t i o n There i vely g ti vely present an aire agreed rdan (1 000 to r-1 evel

he re

grow proba

mome the v al wi t al . d as enn ( t of

part fore , rowi n growi

data raft best 960), 30,00

wind

ason fo i n g e c h bly gre ntum of erti cal nd shea

(1970) long as 1966) a radar e i c 1 e s w

at al 1 g conve ng echo

i nd i ca at 39,0 with th

which 0 ft, a s .

r the o , su ater

the

prof r, th , wi 1

the nd Bl choes ere f

1 eve cti ve

will te th

00 ft e 1 ow were

1 so t

above s t a i n e than 1 i nf 1 ow i 1 e of e echo 1 stil v e r t i c ack et

to i n ailing Is in

echoe

move is sin , and -1 evel repres ended

re- d by 0 m i ng

the

1 al

al . fer

at whi ch s ,

with ce the

winds enta- to

In the case of precipitation falling through weak di- luted updrafts (on the order of 1 or 2 m sec1) , the tilt of the echo would still be in the same sense as outlined in the above paragraph, but more tilted. In this case, the echo boundary could be expected to move with nearly the speed of the wind at the precipitation generating level. However, this type of echo tends to be more diffuse than the actively grow- ing one and hence harder to follow. Therefore, most of the echoes used in this study were most probably near their ma- ture stage.

If the above argument is valid, most of the echoes probably represent the flow in the inflow layer, modified slightly by entrainment. Trends in the mean echo velocities in particular quadrants or range intervals should therefore indicate trends in the low-level flow field. Deviations from the mean echo velocities around the circumference of the storm at different radii are then a measure of the asym- metries in the low-level flow.

J-12

THE LOW-LEVEL ASYMMETRIC STRUCTURE OF HURRICANE DEBBIE AS REVEALED BY ECHO VELOCITIES

Study of the variation in echo velocity with azimuth in Hurricane Debbie is presently underway. Preliminary re- sults indicate the following:

( 1 ) The mean echo s the storm at ra (outer eyewal 1 ) 75-150 n miles

f i gure J-6 . In began until % h 30 knots at the knots in the ou creased in this from 10-15 n mi knots .

(2) Superimposed on eyewal 1 was a s cated by the th each range inte to f ol 1 ow each smal 1 er decreas another increas pear to be thre the 1 ong peri od shorter period hour or two, an with a period o

( 3) The echo speed about 1 1 knots . the deviations inner range int with time .

(4) The mean cross i of the storm de d i c a t i n g less i Th i s is s hown i occurred in the of from about 5 outward was mea val s the decrea about zero. Th the mean genera time period stu tion during the the 1 arges t dev range interval.

peeds around the circumference of nge intervals of 18-28 n miles , 28-50 n miles, 50-75 n miles, and increased with time as shown in creases from h. hour before seeding our after seeding ended ranged from

outermost range interval to 10 ter eyewall. The echo speeds de- time period in the range interval les (inner eyewall) by about 20

the horte in so rval , s e e d i e unt e occ e ti m

tren fluct d (c) f les devi a

At i n c r e erval

ng an

creas

nf 1 ow

n fig

oute

degr

sured

se wa

e ave

lly t

died.

time

i a t i o

upward trend beyond the inner r period fluctuation, indi- lid lines on figure J-6. At

a 5-10 knot increase appeared ng followed by a slightly il the next seeding, when urred. Therefore, there ap- e scales of echo motion: (a) d over several hours, (b) the uations with a period of an

the deviations about the mean s than 1 hour.

tions from the mean averaged the two outer range intervals, ased with time. At the three s, the deviations decreased

gle a ed at

i n t ure J r ran ees i . At s abo rage ended The

peri ns oc

round the al 1 rang he time p -7. The g e i n t e r v nward to

the othe ut 5 degr maximum d to decre average od was ab c u r r i n g a

ci rcumf erence e intervals, i n - eriod studied, largest decrease al where a change about 5 degrees r range inter- ees i nward to eviations from ase during the maximum devi a - out 8 degrees, t the outermost

J-13

HURRICANE "DEBBIE"

AUGUST 20, 1969

*i #2 #3 #4 #5

11 12 13 14 15 16 17 18 19 20 21

11 12 13 14 15 16 17 18 19 20 21 #1 #2 #3 #4 #5 TIME (GMT) MEAN ECHO SPEED AND DEVIATION (KTS.)

Figure J-G. Azimuth ally averaged echo speeds at selected range intervals together with the mean maximum deviations about the azimuthal mean. Scale for the mean values (solid circles ) is on the left and the scale for the deviations (open circles) is on the right. The thin vertical lines indicate the seeding times.

J-14

HURRICANE "DEBBIE AUGUST 20. 1969

#1 #2 #3 #4 #5

11 12 13 14 15 16 17 18 19 20 21_

11 12 13 14 15 16 17 18 19 20 21

#1 #2 #3 #4 #5

TIME (GMT.)

MEAN ECHO CROSSING ANGLE AND DEVIATION

(DEGREES)

Figure J-7. Azimuthally averaged echo crossing angles at se- lected range intervals together with the mean maximum devia- tions about the azimuthal mean. Scale for the mean values (solid circles) is on the left and the scale for the devia- tions (open circles ) is on the right. The thin vertical lines indicate the seeding times.

J-15

(5) When the echo speed devi as a function of azimuth dominant wave number at iods studied. This was deviations were plotted

(6) The general tendency was viations in the outer th in the front and right r viations in the right fr in figure J-8.

(7) The phase of the cross in exactly one-half wavelen deviations in each of th This meant that negative ward moving echoes) were and rear quadrants, with tions (inward moving ech right front quadrants, and minima are located a angle. Likewise, the ma angles occur at the mean echo speed is decelerati is outward, and as the e stream, the crossing ang

(8) Figure J-9 illustrates h deviations around the in rotate cyclonically with tion rate of the major a (1971). Fol 1 owi ng each relative location of the crossing angle maximum c different amounts during after seeding to 1 hour ting, maintaining their eration. The significan sent. However, it seems for the period of about rate of rotation of the tions nearly matches tha

(9) The relation between the angle deviations was not intervals, but generally with crossing angle mini

(10) The faster moving, outwa outer eyewall regions te solid looking echoes whe posite at the same time inward moving echoes ten portion of the eyewall b which tended to protrude

ations from the mean were plo , wave number 2 appeared to b all radius intervals and time true also when the crossing a as a function of azimuth.

for the positive echo speed ree range intervals to be loc ear quadrants with negative d ont and left quadrants, as sh

g angle deviations was almost

gth out of phase with the spe

e outer three range intervals

crossing angle deviations (o

most common in the left fron

positive crossing angle devi

oes) located in the rear and

This means that the speed max

t the position of zero cross i

ximum inward and outward cros

echo speed. Furthermore, as

ng downstream the crossing an

cho speed is accelerating dow

le is inward.

ow the speed and crossing ang

ner and outer eyewalls tended

time nearly matching the rot

xis as described by Black et

of the last three seedings th

major axis, speed maximum, a

Ranged as each decelerated by

the time period from 15 minu

after seeding and then accele

new phases until the next dec

ce of this is not known at pr

quite significant that, exce

an hour after each seeding, t

speed and crossing angle devi

t of the major axis.

phases of the speed and cros

as clear-cut as the outer ra

the speed maxima corresponde

ma (outward motion ) .

rd moving echoes in the inner

nded to be correlated with mo

n compared with a PPI radar c

interval, while the slower mo

ded to be correlated with the

roken into individual cells,

into the eye occasionally.

tted e the per- ngl e

de- ated e- own

ed

ut-

t

a-

i ma ng

sing the gle n -

le

to a- al . e nd

tes

ra-

el-

e-

pt

he

a-

sing di us d

and re om- v i n g ,

This

J-16

HURRICANE "DEBBIE"

AUGUST 20, 1969

CO

10

w 0

>•

-10

1130- 2030 Z

-LEFT-REAR-

-LEFT-FRONT*

A"

150 >R >25

-BRIGHT FR0NT-^|<^RI6HT- REAR-

BACK H«« LEFT M* FRONT H* RIGHT H*— BACK

10°

0"

1

H-io«

ECHO SPEED AND CROSSING ANGLE DEVIATIONS

Figure J-8. Azimuthal variation of eoho speed [solid curve) and crossing angle (dashed curve) beyond the eyewall dur- ing the time period studied.

result is in agreement with echo velocity analyses of the eyewall region of Hurricane Carrie by Fujita (1959), of Hurricane Daisy by Jordon (1960), and of Hurricane Celia by Fujita (1971).

CONCLUSIONS

J-17

HURRICANE "DEBBIE"

1600 1700

1800

AUGUST 20, 1969

1900 2000 2100

' A V ' /' /'

150°

STORM MOTION

3 30'

300°

STORM MOTION

2000

2100

FAST

( , ) ANGULAR R

( . ) ANGULAR R

1900 SLOW TIME (GMT) ) ANGULAR ROTATION OF EYEWALL MAJOR AXIS

OTATION OF ECHO CROSSING ANGLE MAXIMUM OTATION OF ECHO SPEED MAXIMUM

Figure J-9. Angular rotation of the eyewall major axis ini- tially in the front quadrant together with the eoho speed and crossing angle maxima initially just upstream from this major axis position are all indicated by thick lines. The position of the major axis initially in the rear quadrant together with the echo speed and crossing angle maxima just upstream are indicated by thin lines.

The top panel is the rotation rates for the inner eyewall and the bottom panel is the rotation rates for the outer eyewall . Black retangles indicate the seeding time and location for the third, fourth, and fifth seedings . Thin vertical lines delineate the slow moving time periods fol- lowing each seeding from the fast moving time periods .

J-18

experiments since the appearance of the eyewall region on radar could then be used to direct seeding aircraft to the locations where the seeding agent will be most effective.

REFERENCES

Black, P. G., J. J. O'Brien and B. M. Lewis (1967): Ocean motion beneath a hurricane and its influence on the operation of airborne Doppler radar. Fifth Technical Conference on Hurricanes and Tropical Meteorology, Caracas, Venezuela, November.

Black, P. G., H. V. Senn and C. L. Courtright (1971): Some airborne radar observations of precipitation tilt, bright band distribution and eye configuration changes during the 1969 multiple seeding experiments in Hurri- cane Debbie. Submitted to Monthly Weather Review.

Fujita, T. T. (1959): A computation method of velocity of

individual echoes inside hurricanes. Final Report CWB 9530, May, 7 pp.

Fujita, T. T., and H. Grandoso (1968): Split of a thunder- storm into anticyclonic and cyclonic storms and their motion as determined from numerical model experiments. Journal of Atmospheric Sciences , 25, (3), May, pp. 416-438.

Fujita, T. T. (1971): private communication.

Gentry, R. C, T. T. Fujita and R. C. Sheets (1970): Air- craft, spacecraft, satellite and radar observations of Hurricane Gladys, 1968. Journal of Applied Meteor- ology s 9, (6), December, pp. 837-850.

Grocott, D. F. H. (1963): Doppler correction for surface movement. Journal of the Institute for Navigation, 16, pp. 57-63.

Hawkins, H. F. (1971): Comparison results of the Hurricane

Debbie, 1969, modification experiments with those from Rosenthal's numerical model simulation experiments. Monthly Weather Review, 99, (5), May, pp. 427-434.

Jordon, C. L. (1960): Spawinds for the eyewall of Hurricane Daisy of 1958. Proceedings of the Eighth Weather Radar Conference, April 11-14, pp. 219-226.

J-19

Ligda, M. G. H. (1955): Analysis of motion of small precipi- tation areas and bands in the hurricane of August 23- 28, 1949. Technical Note No. 3, Massachussets Insti- tude of Technology, 41 pp.

Rosenthal, S. L. (1971): A circularly symmetric, primitive equation model of tropical cyclones and its response to artificial enhancement of the convective heating function. Monthly Weather Review, 99, (5), May, pp. 414-426.

Ross, D. (1971): private communication.

Senn, H. V. (1960): The mean motion of radar echoes in the complete hurricane. Proceedings of the Eight Weather Radar Conference, April 11-14, pp. 427-434.

Senn, H. V., H. W. Hiser and R. D. Nelson (1960): Studies of the evolution and motion of radar echoes from hurri- canes. Final report, U.S. Weather Bureau, Report No. 8944-1, August.

Senn, H. V. (1963): Radar precipitation echo motion in Hurri- cane Donna. Proceedings of the Third Technical Confer- ence on Hurricanes and Tropical Meteorology , June 6-12.

Senn, H. V., and J. A. Stevens (1965): A summary of empirical studies of the horizontal motion of small radar precip- itation echoes in Hurricane Donna and other tropical storms. Technical Note 17-NHRL-74, November, 55 pp.

Senn, H. V. (1966): Precipitation shear and bright band ob- servations in Hurricane Betsy, 1965. Proceedings of the Twelfth Weather Radar Conference, American Meteor- ological Society, October, pp. 447-453.

Watanabe, K. (1963): Vertical wind distribution and weather echo (in the case of the typhoon). Proceedings of the Tenth Weather Radar Conference . April 22-25, pp. 222- 225.

J-20

APPENDIX K

A SUMMARY OF RADAR PRECIPITATION ECHO HEIGHTS IN HURRICANES

Harry V. Senn Rosenstiel School of Marine and Atmospheric Science

Uni versi ty of Miami

INTRODUCTION

In recent years the need for three-dimensional radar precipitation data in hurricanes has increased greatly. This is due partly to requirements of the National Weather Service for such information on existing storms, partly to satisfy the interests of those who must reconnoiter the storms with aircraft, but most importantly to fill gaps in the knowledge necessary for intelligent planning and execution of attempts to significantly modify hurricanes.

A large amount of height data and many case histories are available for various types of storms which occur over the United States because of the presence of radars capable of making observations. Some land-based RHI data on hurri- canes exist for storms approaching or over land, but these cases are not typical of over-water situations in the tropics Furthermore, such data are rarely obtained with radars having optimum vertical beamwidths (1 degree or less), transmitting frequencies, peak power, or data recording equipment. For instance, in several hurricanes which affected the southeast coast of Florida, each of the WSR-57 radars at Miami and Key West obtained only two or three Polaroid RHI photographs for later analysis. The sparsity of RHI data was due to lack of automatic data gathering equipment. During the same period, many days of routine, excellent PPI data were collected.

Unfortunately, RHI data for hurricanes farther from land are even more limited. Although nearly optimum airborne equipment has existed for almost two decades, Project STORM- FURY impetus was necessary before the APS-45 radars aboard the WC-121N reconnaissance aircraft were capable of obtaining documented RHI data useful to researchers.

The following is an attempt to summarize the RHI data from all sources on hurricanes in an attempt to arrive at a model which might be used to help determine where one might profitably direct modification efforts.

HURRICANES PRIOR TO 1958

Early observations by Wexler (1947), Ligda (1951), Jordan and Stowell (1955) either do not even mention radar echo top observations or they report on heights in a single narrow area of interest without indicating the general height population in hurricanes. Probably the most complete early report on echo heights was by Kessler and Atlas (1956) on Hurricane Edna, 1954, using the TPQ-6, FPS-4, and FPS-6 radars However, the observations were made at latitudes and times in the life history of the storm that they were most probably not representative of hurricanes in more tropical latitudes.

HURRICANE DAISY, 1958

Jordan et al . (1960) presented many features of Hurri- cane Daisy, 1958, including some RHI radar data taken in and near the eyewall region. They found the maximum echo tops to be about 65,000 ft with echoes "away from the eye..." less than 45,000 ft. "Daisy" was a \/ery well formed storm just northeast of the Bahama Islands at the time. The eye was open with classically clear blue skies above it, and the pre- cipitation pattern fairly typical (Senn and Hiser, 1959) ex- cept for the fact that the eyewall was open to the west and the heaviest precipitation, as well as spiral bands, had rotated to the southern regions.

HURRICANE JUDITH, 1959

In 1960, Senn et al . presented RHI data taken on the University of Miami MPS-4 radar on minimal Hurricane Judith,

1959, a small, late season typical of most hurricanes fi gurations .

storm. However, "Judith" was not in either PPI or RHI pattern con-

HURRICANE DONNA, 1960

Jordan and Schatzle (1961) published the first RHI picture of the eye taken on the U.S. Navy's APS-45 airborne radar when reporting on the "Double Eye of Hurricane Donna." Although the picture did not show it, they described the inner eyewall echo tops as 45,000 ft with the outer eyewall topped

K-2

near 30,000 ft. Using the land-based Univers MPS-4 radar, Senn and Hiser (1961) presented hensive data on echo tops in a major storm at latitudes. Table K-l summarizes the heights in the four quadrants of Hurricane Donna base tion of motion of the storm. (Since this was ing most of the period of observation, little be apparent if the reference line were north, ting to note that over 95 percent of the echo tops of less than 30,000 ft and over 78 perce low 20,000 ft. However, it is just as obviou one-third of all echoes had tops above the me suming this storm was typical with respect to echoes, probably only a small fraction of tho bright band were active towers; the rest had the mature stages. In the absence of suffici Senn et al . (1963) attempted to use far more PPI data using range variations to indicate a heights for comparisons with observed winds, was somewhat rewarding in the absence of othe but obviously did not produce echo heights to limits of an RHI radar, so no detailed compar storm data are presented.

i ty of Mia the f i rs t

sub- tropi of 3709 ec d on the d

northerly

di fferenc ) It is i es observe nt had top s that mor Iting leve

bright b a se above t reached or ent RHI da vol umi nous pproximate

The techn r better d

the accur i sons wi th

mi s compre- cal hoes i rec-

dur- e would nteres- d had s be- e than 1. As- nd he

passed ta ,

"Donna1

echo iq ue ata acy

other

HURRICANE DEBRA, 1961

Bigler and Hexter (1960) used CAPPI techniques to show the echo coverage at "standard," 10,000, 20,000, and 30,000 ft levels in Hurricane Debra (1961) as viewed by the 3-cm CPS-9

Table K-l. Number of Echoes by Height, Range, and Quadrant From MPS-4 Radar, Eurrioane Donna, 1960.

Quad.

0-89°

90-

179°

180-

269°

270-

■359°

TOTAL

% OF

Range*

<45

55

65

75

<45

55

65

75

<45

55

65

75

<45

55

65

75

TOTAL

02-10

19

7

4

2

2

5

5

6

5

7

2

1

25

1 1

9

4

114

03.1

12-20

293

154

97

41

250

214

151

97

325

1 72

119

53

34 8

330

1 70

97

2 801

75.5

22-30 ** 76

33

27

12

85

55

27

9

100

32

36

1 1

79

52

44

23

701

18.9

32-40

8

8

9

4

6

2

4

9

4

0

1

2

4

6

0

1

68

01 .8

42-50

2

5

4

2

2

6

0

0

1

0

1

0

0

2

0

0

25

00.7

TOTAL

398

207

141

61

345

282

187

121

435

211

159

67

456

291

223

125

3709

100.0

- Range

f ron

storm center nautic;

1 m i

les.

**HT.K'

FROM: Senn and Hiser (1961

K-3

radar. Although this radar is subject to very appreciable at- tenuation in such situations, the data are interesting from

several points of view. Some of those that did eye; others were 25 to is about 50 miles long This is the area which normal storms (Senn and

Very few echoes exceeded 30,000 ft. were in the northeast portion of the 50 miles north; but the largest area and 50 miles west of the storm center has fewer and less intense echoes in Hiser, 1959). However, "Debra" was

under increasing influence from land areas and no longer typ ical of an over-water, undisturbed low latitude formation.

HURRICANE CLE0, 1963

of Hu Miami 30-40 cores great eye t In th above "Cleo ti ve to 25 i n th excep ft, o

Echo

r r i c a n

1 s MPS

miles

in th

er ran

he f re

e eyew

32,00

" PP I

p o r t i o

,000 f

e rain

t for

nee to

heights e Cleo a -4 radar

from th at regio g e s , h e i quency o all, tow 0 ft. F and RHI ns of sp t near t shield, their co

33,000

were gain . He e s to n ext ghts f hig ers g i gure data i ral he ey and g res w ft.

stud using

foun rm ce e n d i n were her p enera s K-l super bands e. H enera hi ch

ied by

the 1

d the

nter t

g sign

mostly

reci pi

1 1 y ex

and K

impose

had t

eights

lly th

o c c a s i

Senn and-ba medi an o be 2 i f i c a n

1 ower tati on ceeded -2 are d. In ops on

were e same onal ly

(1965

sed U

hei g

0,000

tly h

; and

towe

28,0

typi that the 15,00 i n s were

) in all ni versi ty hts of ec

ft with i g h e r . A

nearer t rs was gr 00 ft wit cal views

study mo order of 0 ft fart pi ral ban

found at

regi ons

of hoes some t

he

eater . h some

of st ac- 20,000 her out d tails

25,000

HURRICANE BETSY, 1965

Hurricane Betsy (1965) echoes were studied both from the land-based University of Miami's radars and the APS-45 airborne set by Senn (1966). In fact, this was the first comprehensive study of most quadrants and ranges of a storm in a completely over-water environment. Unfortunately, when the APS-45 RHI data were gathered on 1 September 1965, "Betsy" was a minimal hurricane gradually increasing in intensity. However, the Betsy precipitation pattern was much more normal than Cleo's in 1963. The Betsy echo heights occasionally exceeded 40,000 ft in the eyewall, and the echoes tended to be higher in the front of the storm; whereas, in Cleo they were higher i n the right rear. Figures K-3 and K-4 show typ- ical Betsy composites of echo heights superimposed on PPI pre- sentations, and figures K-5 and K-6 show breakdowns of echo heights within 20 miles of the eyewall.

K-4

Figure K-l. Composite of typical PPI and RHI Cleo data 26-27 August 1964 from University of Miami MPS-4 radar.

K-5

N

Figure K-2. Hurricane Cleo3 26 August 1964, 2130 EST 3 UM/10- cm PPI with IEC; heights in k ft from MPS-^4; Circle includes eyewall precipitation; eye diameter 14 miles.

HURRICANE INEZ, 1966

Hurricane Inez (1966) echoes were also studied by Senn (1967) using an IEC device on the University of Miami's RHI radar. "Inez" was moving southwest toward the Florida Keys and was a most unusual, asymmetrical hurricane. Figures K-7 and K-8 show that some echoes exceeded 60,000 ft while almost all of the heaviest cores exceeded 20,000 ft. Almost the entire precipitation pattern consisted of a rather intense band of weather to the east and southeast of the storm cen- ter over the warm Straits of Florida waters with the entire western quadrants precipitation free. A further breakdown of

K-6

Figure K-3

Hurricane Betsy PPI with echo heights in k ftt APS-45, 1 September 1965.

K-7

Figure K-4

Hurricane Betsy PPI with echo heights in k ft3 MPS-43 7 and 8 September 1965.

K-8

STORM DIR W

0849-

-1433Z

2

40-

5 6

3

40-

3 4

40-

30-

7

5

1

2 30-

3

6 3

3 30-

5

4

3

3

2

4 5

1

20-

5

2

l 20-

5

5 4 3 2

3 20-

1

10-

10-

10-

r

r

~

X

M

x

•g

^

mi 5

10 1

15

20

mi 5

10 15

2

20

40

3 30

2

I 20-

ioH

20

10

4

QUAD

15

20

40-

2

30-

6

4

4

1

20-

3 2

2

3

10-

-

ac

■£

10

15

40-

4

1

30-

e

3

5

i

6

20-

1

2

10

-

X-

3

20

10

15

20

40-

6

2

30-

6

4

5

5

4

3

2

20-

5

6

1

10-

c

x

s

10

15

40-

3 4 5

4

5

30-

6

2

4

2

8

3

3

i 20-

2

6

5

io-

r

, E

20

10

8

15

20

Figure K- 5 . Number and height of echoes within 20 miles of eyewall by quadrant in Hurricane Betsy j 1 September 19653

APS-4 5.

heights by quadrant and range within 20 miles of the eyewall was made using data from an earlier period northeast of Miami and these are shown in figure K-9.

HURRICANE FAITH, 1966, AND HURRICANES BEULAH AND HEIDI , 1967

Also underway is a study of echo tops in Hurricanes Faith (1966), Beulah and Heidi (1967) using the APS-45 data However, these data are seriously lacking in important de- tails and are expected to yield only general results. Some of these are discussed and shown in the summary.

K-9

STORM

Uo

3 h

2 3

30

7

6

3

S

k

2

20

2

3

5

e

2

1

4

5

10

"^

4-

c

r mi

10

15 20

Uo

30

i*

it

3

6

20

it

5

5 3

3

3

5 2

10

u

X

r mi 5 1Q

2

Uo 30

20

10

15 20

r mi 5 10

15 20

Uo

30

1

2

1

i*

3

2

20

9

It

2

10

5

10

4

Dm v

15 20

UO

30 20

10

UO 1 30

3

k 20 10

10 15 20

10

6

15 20

Uo

1

30

5 3

1

20

2

2 1

10

«

10

7

15

20

UO

2

30

5

3

2

1

20

1

2

1 2

10

10

8

15

20

Figure K-6. Number and height of echoes within 20 miles of eyewall by quadrant in Hurricane Betsy 3 8 September 19653 MPS-4, 0012-1140Z.

HURRICANE DEBBIE, 1969

Hurricane Debbie (1969) was studied by Senn and Court right (1970), but results are only available for the eyewall region at present. These are shown on figures K-10 and K-ll A more complete study of the echo tops using the APS-45 air- borne data is underway.

SUMMARY

Figure K-12 summarizes the number of echoes by height categories for five storms, all over water and below 26°N latitude. Note that the data are not comparable in the sense

K-10

Figure K-7. Hurricane Inez, 4 October 19663 0750 EST, UM/10- cm PPI with IEC; heights in k ft from MPS-4; circle includes eyewall precipitation; eye diameter 20 miles.

that although all echoes were found within 20 n miles of the eyewall (not the storm center), the number of echoes is a function of the flight path, quality of data collected, etc., as well as the actual height population produced in the storm. Consequently, the data for each category are also given in percentages of the total for that storm.

Although echoes penetrate significantly above 30,000 to 35,000 ft at greater ranges, a summary of the composite fig- ures presented above shows that most of the taller echoes are within 20 n miles of the eyewall. Frequency distributions show the vast majority of all echoes to have 15,000 to 30,000 ft categories at all ranges should have no trouble finding echoes in the ft category in and near the eyewall.

tops in the

Generally, one 20,000 to 25,000

K-ll

60,000 ft +

50-59,999 ft

45-49,999 ft

40-44,999 ft

35-39,999 ft

30-34,999 ft

25-29,999 ft

Height of Echoes

20-24,999 ft

15-19,999 ft

10-14,999 ft

5-9,999 ft

0-4,999 ft

Figure K-8. Numb eaoh of

er and height of Hur three iso-echo oonto

rioane Inez eohoes ur intensities .

tn

K-12

60 50 Uo 30 20

10 ifcl

10

2

6

9

15

.c r in 60

5o Uo 30 20

10 10

7 10

8 lh 12

5

u r mi

2 1

6 3

10 6

it 7

60

50

Uo

30

* 20

8

2 10

50 Uo 30 20 10

10 15 20

3 3

e e

7

12

5

10 15 20 " r mi 5 1

60

5 5 6 7 19 12 5

1

3 2

5 3 9

6 7

10

2

10

6

15

5 1

5 ■»

8 7

7 6

15

60

50

Uo

30 l 2

7

1 10

20

20 u 60

50

Uo

3 30

7

4 20

10

5

7 8 1 1 7 7 7 2

3

5

i*

10

17

10

7

10

3

10

7

15

15

60 50

Uo

30 l i 20

3

10

STORM

DIR HSW

20 u

J5

60

50

Uo

3 30

5

5 20 10

20

9

10

7

10

3

10 9

Ik

10

4

10

8

15

15

20

3 3

5 3

7 5

1

20

Figure K-9 . Number and height of echoes within 20 miles of eyewall by quadrant in Hurricane Inez> 4 October 19663 MPS-4, 0030-2S40Z.

Not shown in these figures, but deduced from earlier work, is the fact that, except when a storm is approaching land, the echo height populations remain relatively station- ary with respect to the direction of storm motion rather than exhibiting a rotation around the storm center. It is not yet clear whether that also holds with respect to north, since most of the storms that could be considered representative were headed westerly or northerly when the observations were made. The tallest echoes, likewise, appear to be to the east and north of the storm center, and the south (or general rear) quadrants have the weakest, lowest echoes (sometimes not at all).

K-13

N "

/

/

/

NE-

(

(

I

(

E "

\

\

|

\

SE-

\

\

\

s -

|

\

J

)

SW

(

/

1

1

w

NW

/

'

)

)

/

(

/

I

i i i I

1 1 1 1

l 1 1 1

1 1 1 1

I 1 1 l

l f I i

fill

i I i i

i i 1 i

o o

<J- CN

o o

o o

o o <r cn

o o <r cn

o o <r cn

o o <r cn

o o <r cn

o o <r cn

Time: Z

Figure K-10.

1230 1245 1300 1315 1330 1430 1445 1500 1515 MAX. HT. K' OF ECHOES EACH QUADRANT APS-45 FURY G

Height of eyewall echoes 3 Hurricane Debbie 18 August 1969.

N NE E SE

S

SW

w

NW

i_l_l_l

JUL!

JJ

*%J

^

*Mr

m*

k**#

^

1415 1430 1445 1500 1515 1530 1545 1600 1615 1630 1645 1700 1715 1730 1745 1800 MAX. HT. K* OF ECHOES EACH QUADRANT APS-45 FURY H

Figure K-ll

Height of eyewall echoes^ Hurricane Debbie 20 August 1969.

K-14

Debbie F/H 8-20-69

Debbie F/G 8-20-69

<15 K'

>15 K' < 30 K'

>30 K'

8 8 (12%)

2 6 7 (38%)

3 5 1 (50%)

7 2 (13%)

2 ' 3 (39%)

2 5 9 (48%)

Debbie F/G 8-18-69

5 1 (10%)

1 8 2 (38%)

2 4 9 (52%)

Heidi '67

5 1 (24%)

8 3 (39%)

7 7 (37%)

Beulah '67

3 2 (19%)

6 0 (36%)

7 4 (45%)

Faith '66

1 9 (16%)

5 8 (50%)

3 9 (34%)

Cleo '64

3 8 (22%)

7 1 (41%)

6 4 (37%)

Figure K-12.

Number and percent of echoes by height within 20 miles of eyewall.

CONCLUSIONS

If one is looking for precipitation towers on the order of 20,000 to 25,000 ft outside the eyewall of a normal mature hurricane, he should find them in the north and east quadrants. A good RHI radar is a necessity, however, in a brief analysis of such clouds prior to any modification attempts since these quadrants are generally badly messed up by multi-layers of clouds, ample regions of "bright bands" (indicating melting hydrometers), etc., which make action purely on the basis of visual observations subject to uncertainty.

K-15

In fact, some of the above data lead to some rather perplexing questions regarding the seeding hypothesis used in Project STORMFURY. We have found the bright band in most quadrants and ranges of several hurricanes, as indicated in another paper in process. The results above show widespread echoes at heights where one expects glaciation, and certainly high level reconnaissance photos and satellite observations show an abundance of cirrus. However, one is also impressed with the general convective nature most echoes have on the RHI scope, many times in close proximity to the bright band. These observations suggest that echoes exist in all stages of generation and dissipation; but they do little to help an- swer the question of whether there is enough mixing of ice nu- clei in the wall cloud regions of interest to significantly alter the possible effects of seeding active towers there. The results above show widespread echoes at heights where one expects glaciation, and certainly high level reconnaissance photos and satellite observations show an abundance of cirrus. However, one is also impressed with the general convective nature most echoes have on the RHI scope, many times in close proximity to the bright band. These observations suggest that echoes exist in all stages of generation and dissipation; but they do little to help answer the question of whether there is enough mixing of ice nuclei in the wall cloud regions of interest to significantly alter the possible effects of seed- ing active towers there.

Unfortunately, it is not possible to draw a series of PPI-RHI composites for any storm found in a relatively undis- turbed tropical over-water environment simply because the data are too limited to date. Consequently, it seems essential that eyery effort be made to obtain such records with the only airborne radar presently capable of gathering high qual- ity RHI data, the Navy APS-45. Secondarily, more effort should be made to gather RHI data on WSR-57's, the new WMO supplied RC-32B weather radars in the Lesser Antillies, and others, in an attempt to better describe this most important hurricane precipitation pattern dimension, including the bright band and shear in e\/ery sector of the storm.

Bi gl er , S

REFERENCES Jr

S. G., and P. L. Hexter, Jr. (1960): Radar analysis f Hurricane Debra. Proceedings 8th Weather Radar onferenae3 American Meteorological Society, Cal . , pril , pp. 25-32.

K-16

Jordan, C. L., D. A. Hurt, and C. A. Lowrey (1960): On the

structure of Hurricane Daisy on 27 August 1958. Journal of Meteorology 3 American Meteorological Society, 17, pp. 337-348.

Jordan, C. L., and F. J. Schatzle (1961): The 'Double Eye' Hurricane Donna. Monthly Weather Review, 89, (9), September, pp. 354-356.

of

Jordan, H. M., and D. J. Stowell (1955): Some small-scale features of the track of Hurricane lone. Monthly Weather Review, 83, (9), September, pp. 210-215.

Kessler, E., and D. Atlas (1956): Radar-synoptic analysis of Hurricane Edna, 1954. Geophysical Research Papers No. 50, A.F.C.R.L., Bedford, Mass., July, p. 113.

Ligda, M. G. H. (1951): Radar storm detection. Compendium of Meteorology , American Meteorological Society, Boston, Mass. , pp. 1265-1289.

Senn, H. V. (1963): Radar precipitation echo motion in Hurri- cane Donna. Proceedings 3rd Technical Conference on Hurricanes and Tropical Meteorology. A. M.S., A.G.I. , and H.G.I, and M.G.U., Mexico City, Mexico, June 6-12, R.S.M.A.S. Contr. No. 463.

Senn, H. V. (1965): The three-dimensional distribution of precipitation in Hurricane Cleo. 4th Technical Con- ference on Hurricanes and Tropical Meteorology. A. M.S., Miami Beach, Fla., November.

Senn, H. V. (1966): Precipitation shear and bright band ob- servations in Hurricane Betsy, 1965. Proceedings 12th Weather Radar Conference, October 17-20, Oklahoma City, Okla., R.S.M.A.S. Contr. No. 710.

Senn, H. V. (1967): Radar Hurricane Research, Final Report,

ESSA, NHRL Contract No. E22-84-67(N ) , Report No. 8208-1, September, DDC AD 821-860.

Senn, H. V., and H. W. Hiser (1959): On the origin of hurri- cane spiral bands. A. M.S., Journal of Meteorology, 16, (4), August, pp. 419-426, R.S.M.A.S. Contr. No. 215.

Senn, H. V., H. W. Hiser, and R. D. Nelson (1960): Studies

of the evolution and motion of radar echoes from hurri- canes 1 July 1959 to 30 June 1960, Final Report. U.S. Weather Bureau, Contract CWB-9727, Report No. 8944-1, August.

K-17

Serin, H. V., and H. W. Hiser (1961): Effectiveness of various radars in tracking hurricanes. Proceedings 2nd Techni- aan Conference on Hurricanes^ A. M.S., Miami Beach, Fla. June, pp. 101-114, R.S.M.A.S. Contr. No. 318.

Senn, H. V., and C. L. Courtright (1970): Research, Final Report, ESSA, NHRL 41 -70 (N ) , October.

Radar Hurricane Contract No. E21-

Wexler, H. (1947): Structure of Hurricanes as determined by radar. Annals of N.Y. Academy Sciences 3 48t September 15, pp. 821-944.

K-18

APPENDIX L

PROJECT STORMFURY EXPERIMENTAL ELIGIBILITY IN THE WESTERN NORTH PACIFIC

William D. Mai 1 i nger National Hurricane Research Laboratory

INTRODUCTION

cane Si nc b i 1 i towa rul e in 1 sout Mexi that hurr wi th Ocea whi c 1963

Pro modi f e that ty rul rd fur s for 970 an hwest co is

there i c a n e in 18 n area h expe ; and

ject i c a t i

ti me es ha ther this d are North e 1 i g i

i s a co mi n hours

has ri men Debbi

STORM on ex

the ve be rel ax area

now

Atla ble f

smal g wit

af te been ts ha e, 19

FURY peri oper en c a tio el ig as f nti c or s 1 pr hi n r se util ve b 69) .

, the i ments , a t i n g a hanged ns of t i b i 1 i ty ol lows : , the C e e d i n g o b a b i 1 i 50 n mi e d i n g . " ized to een con

ntera was f reas sever he se

for "A a r i b b as 1 o ty (1 1 es o To

seed ducte

gency p ormal ly a u t h o r i al time e d i n g r seeding storm o ean Sea ng as t 0 perce f a pop date on the th d (Esth

ro ject organ zed an s prog e s t r i c were r hurr , or t he for nt or ul ated ly the ree hu er, 19

for ized d the ressi t i o n s 1 ast i c a n e he Gu ecast 1 ess) 1 and Atla r r i c a 61 ; B

hurri - in 1962.

el igi- vely . The changed

i n the If of

states

of the

area nti c

nes upon eul ah ,

St canes and and publ i 1969. Th Gulf of M and the w in the e a Mexico) a for STORM this repo 18-hour r poses of Western P because p if there p o r t u n i t i

u d i e s of

typhoons shed in t ese repor exico are estern No stern Nor re not co FURY seed rt. An u ule for t compari so a c i f i c . roper bas is to be es to jus

s t a t i s under he STO ts cov as ; th rth Pa th Pac n s i d e r i n g an pdate he Atl n with Thi s c es for a suf f tify t

t i c a 1

the o RMFURY ered t e east c i f i c i f i c a ed to d will to inc antic

the s

ompari

opera

i c i e n t

he Pro

proba 1 der

Annu he At ern P area . rea ( be su

not 1 ude areas e e d i n son i t i o n s

i ncr ject'

b i 1 i ti e

el i g i b i al Repo 1 anti c , a c i f i c

The h off the i tabl e be furt 1970 ca

will b g oppor s parti

in the ease in s move

s of 1 i ty rts

Car hurr urri

wes expe her ses e i n turn" cul a

Pac

exp to t

el ig rul e for 1 i b b e a i cane canes t coa rimen d i s c u under cl ude ties rly i i f i c erime he Pa

ible s we 968 n , a reg occ st o tal ssed the d fo i n t mpor are ntal ci f i

hurri - re made and nd

ions ; u r r i n g f targets

i n

new r pur- he

tant needed

op- c .

ATLANTIC OCEAN, CARIBBEAN SEA, AND GULF OF MEXICO STORMFURY AREAS

Figure L-l shows the eligible ar from 1968 through 1970. Table L-l show rences of hurricanes eligible for STORM ing the months of August, September, an through 1970 using the "18-hour after s rule. The addition of the storms which the change from the "24-hour" to "18-ho storms to the Atlantic, two to the Gulf the Caribbean. These additions increas tunities per year from an average of ap hurricanes per year eligible for seed in seeding eligibility rules regarding pos

eas for s the nu FURY exp d Octobe e e d i n g "

became ur" rule

of Mexi ed the e proxi ma t g under i t i o n of

s e e d i mber eri me r fro e 1 i g i e 1 i g i

adds co , a xpect ely 2 the c

the

ng used of occur- nts dur- m 1954 b i 1 i ty bl e under

three nd one to ed oppor-

to 2.35 urren t storm.

35°

30'

25°

20'

15'

10'

PROJECT STORMFURY OPERATIONAL AREAS (1968 1970)

ELIGIBLE EXPERIMENTAL STORM MUST BE PREDICTED TO REMAIN WITHIN OPERATIONAL AREA FOR/

Figure L-l. Project STORMFURY operational areas ( 1968-1970) . Eligible experimental storm must be predicted to remain within operational area for 18 hours after seeding.

L-2

1954

2

1955

4

1956

1

1957

1

1958

5

1959

2

1960

2

1961

2

1962

2

1963

3

1964

4

1965

2

1966

1

1967

0

1968

0

1969

2

1970

0

Table L-l. Annual Frequency of Hurricanes Eligible for Seed- ing Between 1 August and 31 October Under Forecasting Tech- niques Criteria Approved for STORMFURY Operations Subsequent

to 1970.

Year Atlantic Gulf of Mexico Caribbean Sea Total

0 1 3

0 1 5

0 0 1

0 0 1

0 0 5

0 0 2

0 1 3

1 0 3

0 0 2

0 1 4

1 0 5 0 0 2

0 0 1

0 0 0

0 0 0

1 0 3 0 0 0

TOTAL 33 3 4 40

This number is misleading on the high side because some of these storms either had structure considered unsuitable for experimentation or were changing rapidly in intensity at the time and might not have been used for experiments even though they fell within the criteria established for area seeding eligibility. In addition, some of the storms considered eli- gible in the Gulf of Mexico and Caribbean Sea might not have been seeded for political reasons.

WESTERN NORTH PACIFIC

Figure L-2 shows the proposed operational areas if ex- periments are to be conducted from Guam and Okinawa. The el- igibility rules considered in this study for the Western Pacific are: (1) The typhoon must be within 600 miles of the operations base for a minimum of 12 daylight hours, (2) maxi- mum winds must be at least 65 knots, and (3) the predicted movement of the typhoon must indicate that it will not be with' in 50 n miles of a populated land area within 24 hours after seeding.

L-3

120°E

130°E

140°E

150°E

160°E

170°E

180°E

40°N

TMOJECT STOHMFUMY A.XEJL

30°N

THREE MONTH AVERAGE OF 4.8 ELIGIBLE TYPHOON'S AUGUST , SEPTEMBER .OCTOBER (1961-1970)

20°N

10°N

Wake]

40°N

30° N

20°N

10°N

120°E 130°E 140°E 150°E 160°E 170°E 180°E

Figure L-2. Project STORMFURY area in the Western Pacific.

The list of Western Pacific typhoons eligible for seed ing was updated to include 1970 tropical cyclones and was divided into two categories: (1) those that could be used for STORMFURY experiments with forces limited to operations from Guam only, and (2) those which permitted free use of either Guam or Okinawa from which to launch experiments (see table L-2) .

Two of the 24 "Guam only" opportunities would have re- quired such rapid reaction in order to mount a seeding experi ment that they would probably have been missed. These storms formed within the 600 n mile radius of Guam and rapidly deep- ened while they continued to move out of the area. If a 48- hour notice to alert, deploy, and brief the participants in the experiment were required, both storms would definitely have been missed. A WP-3 or C-130 type aircraft might be used as a seeder in such cases when time does not permit the deployment of jet seeders to the operating base. If this is

jt feasible, STORMFURY monitoring missions without seeding might be conducted on shorter notice in these storms.

L-4

Table L-2. Western Pacific Typhoons Eligible for STORMFURY

Experiments - August^ September > and October (1961-1970).

~7, ~~r n , Combined use of

Year Guam 0n]y Guam and Okinawa

1961 2 6

1962 3 7

1963 2 6

1964 1 2

1965 3 7

1966 1 3

1967 3 4

1968 5 8

1969 2 2

1970 2 3

TOTAL 24 (2.4Q 48 (4.8i) 1 Number of storms per year

Seven of the 24 "Guam only" typhoons were also eligible later in their lives if forces operated from Okinawa. Several of these storms would have been eligible for seeding both from Guam and later from Okinawa, permitting two experiments on the same storm. It is also possible that a storm could be subjec- ted to two experiments from either Guam or Okinawa although this opportunity occurs infrequently.

The free use of both Guam and Okinawa as STORMFURY bases of operation is essential to obtaining a suitable num- ber of experiments during the 3-month period. Safety of per- sonnel and aircraft is paramount and will require a multitude of decisions concerning the best and safest use of the STORM- FURY forces. Examples of this are as follows: (1) A storm or typhoon approaching Guam from the east which, while eligi- ble for experimentation, would not be seeded because forces would have to execute a typhoon evacuation (aircraft flyaway) for safety reasons. If these aircraft could be deployed to Okinawa for their evacuation, when the storm had passed Guam a mission could be mounted from Okinawa and terminated in Guam. Some changes in operational plans and techniques will be required to execute this type of experiment. (2) A typhoon that develops while approaching the 600 n mile radius to the west of Guam would be eligible in many cases if Project air- craft could terminate their missions in Okinawa. This also will require modified STORMFURY flight plans and schedules in order to accomplish the experiment.

L-5

If the flexibility of using both Guam and Okinawa as STORMFURY operational bases is not possible, opportunities to seed some of the storms would be lost because Project aircraft might have to fly away from Guam until an approaching typhoon had safely passed. Upon return of the forces to Guam and after mission preparations, the typhoon would have approached or exceeded the maximum operating range of STORMFURY forces.

The study was further expanded to examine the number of calendar days during which a large number of tropical cy- clones exists in the Western Pacific to determine the effect that this factor would have on the availability and partici- pation of reconnaissance aircraft for STORMFURY operations. Cyclone activity (tropical depressions, tropical storms, and typhoons) during the 3- mo nth period of August, September, and October is listed by the number and percentage of days occur- rence in table L-3.

During the months of August, September, and October tropical cyclones occur somewhere in the western North Pacific Ocean 84 percent of the time or an average of 77 days out of the 92. Three or more tropical cyclones occur simultaneously during an average of about 9 of these 77 days. Fortunately, during some of these periods, because of their location and strength, the tropical cyclones did not all require full re- connaissance coverage. Reconnaissance forces may be hard

Table L-3,

Year

Tropical Cyclone Days in Western North Pacific August 3 September 3 October .

0

Number of Days with 0 to 5 Cyclones" 12 3 4

1960 1961 1962 1963

1964 1965 1966 1967

1968 1969 1970

8

7

15

23

10 24

11 9

15 32

8

41

22

14

4

38

39

8

0

23

39

15

0

40

25

4

0

42

29

1 1

0

35

24

9

0

40

25

16

0

39

30

8

6

31

37

9

0

48

11

1

0

60

23

1

0

437

304

96

10

39.7

27.6

8.7

0.9

43.1

30.0

9.5

1 .0

TOTAL DAYS 162 AVERAGE DAYS 14.8 % OF DAYS 16.1

3

0.3

0.3

% of tropical cyclone days with one or two cyclones - 87.2 % of tropical cyclone days with three or more cyclones-1 2 .8

L-6

pressed at times to participate in full scale Project STORM- FURY experiments during periods when there are three or more active cyclones, but should be able to provide reconnaissance on one cyclone while participating in Project STQRMFURY oper- ations on another. There are exceptions to these assumptions; but, in general, sufficient forces to conduct experiments should be available during 68 of the 77 cyclone days. When, because of other commitments, DOD reconnaissance and seeder aircraft are not available to mount a full seeding experiment, the remaining available Project aircraft can be utilized to gather data on the natural variability within typhoons.

CONCLUSIONS AND RECOMMENDATIONS

(1) Conducting operations in the Western Pacific is worthwhile and should increase the number of experimental op- portunities per average season by a factor of 2-3 over those experienced in the Atlantic regions provided that both Guam and Okinawa are available for use by STORMFURY forces. Addi- tion of a base in the Philippines and in other locations in the Pacific adds a few opportunities per 10 years, but most of the eligible storms can be worked from either Guam or Okinawa. If Guam is available, but Okinawa is not, the desirability of moving the project to the Pacific should be reconsidered because of the limited increase in the number

of expected opportunities over those in the Atlantic operating areas .

(2) During periods when there are three or more tropi- cal cyclones occurring simultaneously (13 percent of the cyclone active periods during August, September, and October), monitoring missions could be conducted on suitable storms using fewer forces and without actual seeding.

(3) Some additional experiments could be conducted on tropical storms and tropical depressions during periods when no eligible typhoon activity was occurring.

L-7

GPO 836 -595

41

U.S. DEPARTMENT OF COMMERCE

National Oceanic and Atmospheric Administration Environmental Research Laboratories

NOAA Technical Memorandum ERL NHRL-93

HORIZONTAL ASYMMETRIES IN A NUMERICAL MODEL OF A HURRICANE

James W. Trout Richard A. Anthes

National Hurricane Research Laboratory Coral Gables, Florida November 1971

TABLE OF CONTENTS

Page

ABSTRACT 1

1. INTRODUCTION 1

2. SUMMARY OF THE MODEL 2

3. COMPUTATIONAL PROCEDURE

3.1 The Polar Grid 5

3-2 Interpolation Schemes to the Polar Grid 5

k. THE ASYMMETRIC STAGE 7

*t.1 Time Variations of Azimuthal Standard Deviations. . 9

k.2 Harmonic Analysis of the Momentum and Temperature

Fields 13

5. EDDY FLOW RELATED TO THE MATURE VORTEX 17

5.1 Asymmetries in the Outflow Layer 20

5.2 Asymmetries in the Inflow Layer 2 5

6. HORIZONTAL TRANSPORT MECHANISM 27

6.1 Flux of Absolute Vorticity 28

6.2 Flux of Angular Momentum 30

6.3 Vertical Flux of Relative Angular Momentum 32

7- SUMMARY AND CONCLUSIONS 33

8. REFERENCES 36

i i i

HORIZONTAL ASYMMETRIES IN A NUMERICAL MODEL OF A HURRICANE

James W. Trout and Richard A. Anthes

Statistical techniques are employed to investigate the development and structure of horizontal asymmetries in the numerical model of a hurricane developed by Anthes et al. (1971a). Strong asymmetries in the momentum and temperature fields develop in the outflow layer at approximately 120 hours. Weaker asymmetries also develop in the inflow layer at this time. Harmonic analyses are used to determine the predominant scale of asymmetries. Detailed spatial analyses are carried out for the momentum and temperature fields in the mature asymmetric stage of the model. The analyses are compared to observational data compiled by Black and Anthes (1971). The results show that the model reproduces many observed features of a three-dimensional tropical cyclone.

1. INTRODUCTION

Recent experiments conducted with an asymmetric hurricane model (Anthes et al . , 1971a) dramatically illustrate certain asymmetric proper- ties of the horizontal and vertical motion fields. Examples of these are horizontal eddies in the upper tropospheric outflow layer, rainbands, and meandering of the hurricane eye. Two distinct stages are observed in a typical experiment. During the early stages, the storm circulation is quite symmetric about the vertical axis of rotation. In the second stage, the storm acquires marked asymmetric characteristics in the outflow layer, and the vertical motion patterns form spiral bands which resemble hurri- cane rainbands.

The purpose of this paper is to report the quantitative investigation of the nature and importance of the asymmetric character of the model storm. Various statistical measures are employed to show the

time-dependent development and locations of the asymmetries. Harmonic analysis of the radial and tangential wind components determines the pre- dominant scale of the asymmetries. Computations of fluxes of angular momentum and absolute vorticity show the importance of asymmetries as horizontal transport mechanisms. The asymmetries in the model outflow layer are compared with the asymmetric features of real storms (Black and Anthes, 197D .

2. SUMMARY OF THE MODEL

The equations are written in a-coordi nates (Phillips, 1957) on an f-plane. The equations of motion and the continuity, thermodynamic, and hydrostatic equations are identical to those utilized by Smagorinsky et al. (1965) for general circulation studies. The basic equations are given in Anthes et al . (1971a). The vertical structure of the model con- sists of an upper layer and a lower layer of equal pressure depth and a thinner Ekman boundary layer. The information levels for the dynamic and thermodynamic variables are staggered according to the method used by Kurihara and Holloway (19&7)

For computational economy, the horizontal mesh has been limited to a square grid with a uniform spacing of 30 km. The lateral boundary points approximate a circle, and all points are contained between radii of ^35 and 450 km. The thermodynamic grid points are staggered from the veloc- ity component grid points on the a-surfaces. A comprehensive summary of the mathematical details is given elsewhere (Anthes, 1972) and need not be repeated here.

The Matsuno ( 1 966 ) simulated forward-backward scheme is utilized in the model for the time integration scheme. The Matsuno scheme has the property of dampening the very high temporal frequencies associated with internal and external gravity waves. The lateral boundary conditions consist of a steady-state pressure and temperature on the boundary and a variable momentum based on extrapolation outward from the interior of the domain. The cumulus scale convective processes are parameterized simi- larly to the version of Rosenthal's (1970b) symmetric model. The current model also contains an explicit water vapor cycle. For further details refer to Anthes (1972). The initial conditions consist of an axisym- metric vortex in gradient balance. The minimum pressure is 1011 mb , and the environmental pressure on the lateral boundary is 1015 mb , yield- ing a maximum gradient wind of 18 m sec-1 at a radius of 2^0 km. With these initial conditions and utilizing a time step of k5 seconds, the experiment has been executed for 192 hours.

With symmetric initial and boundary conditions, the solutions to the differential equations must remain symmetric for all time. However, truncation and roundoff errors in the finite difference equations, as well as the lack of complete circular symmetry in boundary conditions, produce extremely weak asymmetries after the first time step. Although objections might be raised concerning the desirability of allowing the initial asymmetries to be generated by truncation, later experiments in which asymmetries were deliberately introduced in a random fashion yield essentially the same results during the asymmetric stage (Anthes, 1972).

Thus, it appears that the actual source of the initial asymmetries is un- important in the mature asymmetric stage.

3. COMPUTATIONAL PROCEDURE During the asymmetric stage an interesting anticyclonic looping of the eye is observed. This looping appears to be related to the asym- metric outflow and is discussed by Anthes (1972). The center of the grid is depicted as zero (fig. 1), with north-south, east-west deviations from the center plotted in kilometers.

NORTH 30

A

15-

0 (Km) -15

-30 -45

SOUTH

-60-

«*»""'

192

162 /

***\ 168

i

/

X

i

/ /

N \

wm

\

i

\

mm

\

i

\

\ \

\

m m,~ \

138 \

\

> 156 \

••

••.. 174*

-

\

132

\

-

\ \

\ \

* 144 i

/ !

-

\

. 150

i

±86^

^•^^_

' i

i i i

mm

X

/

«■

X.

/

^,

**

-'

- -

180

i

1 1 1

-_l

i i | £

-0

-60 -45 -30 -15 0 15 30 45 60 WEST - ( Km ) -EAST

Figure 1: Model vortex motion. Positions are labeled in hours.

3. 1 The Polar Grid The computation of circular averages and mean and eddy fluxes of vorticity and momentum requires interpolation from the cartesian grid system to a polar grid system whose origin is coincident with the looping vortex center. The rectangular (u) and (v) wind components are converted into tangential (V-v) and radial (V ) wind components by use of:

VA = (vX - uY)/R (1)

and

Vr = (uX - vY)/R (2)

where X and Y are the distances along the x and y axis between the vor- tex center and a given grid point; and R = (X2 + Y2)*. (3)

The cartesian arrays are interpolated to a polar coordinate grid consisting of 15 radial increments of 30 km (r = 15, ^5, 75-...) and 16 azimuthal increments of 22.5 degrees. The calculation extends to a radius of 435 km when the storm center is located on the center of the cartesian grid. When the storm center is located away from the grid center, the maximum radius of the polar grid is reduced.

3.2 Interpolation Schemes to the Polar Grid

The accuracy of two interpolation formulae is tested. The first of these is a bilinear interpolation formula:

s" =s,,j + hts,,J+rsi,j] + wVi.j-Si.j) (1-h)

+ <S|+1,J+r5|iJ+i>J3

eo

I-i

I+i

T(p)

J-i

J+l

Figure 2: Interpolation to polar grid point (P) . Here the interpolated value of S , at the location of the polar point

(fig. 2), is denoted by P. In (4), (l, J) is the grid point (row, column) index in the usual matrix sense; h and K are the coordinate distances from point P to grid point (I, J). Satisfactory results are obtainable with (*t) at large radii. However, at smaller radii the curvature in the variables associated with the hurricane vortex is too extreme for linear interpolation. The second method is a nine point interpolation function. The formula is a finite difference form of the truncated Taylor's expan- sion of a function of two independent variables.

s = s|J + .5h<s|>Jt1-s|>iM) + •5K(s|_,iJ-s|+1J) + •»,<si.j*i4Si.j-r2Si.j> + •5k2(si-i,j+si+i,j-2Si,j)

+ •25hK(S|_1)J+l-S|_1jJ_,-S|+,jJ+l+S|+1 (J_,). (5)

For all interpolations the base Doint (I, J) is selected so that h and K are not greater than one-half a grid increment.

6

Both interpolation formulae are applied to the function,

f(r) = (r+15)/30 (r in km). (6)

With the vortex center coincident with the grid center, (6) yields integer values increasing from 1 at r = 15 km to 15 at r = 435 km at al azimuth angles. Table 1 shows circular averages, for the first five radii, computed from data obtained by use of (4) and (5).

Table 1: Circular Averages Computed from Interpolation Scheme (4) and (5)

Radius Bilinear Interpolation 9-Point Interpolation

(km) Eqn. (4) Eqn. (5)

15 1.2071 1.0969

45 2.0529 2.0137

75 3-0447 2.9920

90 4.0211 4.0022

105 5.0230 5.0008

Table 1 clearly shows the superiority of the 9~Point Interpolation for- mula at small radii. Hence, interpolation formula (5) is utilized throughout this paper.

4. THE ASYMMETRIC STAGE Notable asymmetries of the cyclone circulation include large hori- zontal eddies in the upper tropospheric outflow region. Figure 3 shows the trajectories of 10 particles which are released in the lower levels of the cyclone and provides a qualitative view of the asymmetric circu- lation over the life cycle of a typical experiment. The trajectories are

T=90-282 HOURS

9 HOUR INTERVALS

Figure 3: Ten trajectories of parcels released in the boundary layer over an 8-day period.

computed over an 8-day period from the forecast velocity components. For additional illustrations and computational procedure refer to Anthes et al . (1971c). The figure greatly exaggerates the vertical dimension of the storm but clearly illustrates the asymmetric outflow characteristics. Particles, upon reaching the upper levels of the model, are carried out- ward from the vortex center, mainly in the northeast and southwest quad- rants. This should be contrasted to the nearly symmetric inflow depicted in the lower layers. The preferred quadrants of outflow reflect the asymmetric circulation around upper level horizontal eddies that are present during the 8-day period.

4.1 Time Variations of Azimuthal Standard Deviations

The principal measure of asymmetry employed here is the standard deviations (SD) from the azimuthal averages of momentum and temperature. Figure k and figure 5 are plots of SD versus time for the radial winds, tangential winds and temperature at selected radii in the inflow and out- flow layers.

Large SD are computed at very small radii (not plotted), where the interpolation error due to the relatively few cartesian grid point values is the greatest. However, the asymmetries are relatively small compared to the azimuthal means. The inflow asymmetries diminish rapidly with in- creasing radius. The outflow asymmetries, on the other hand, appear to be greatest near the 165 km radius (fig. k) . The ratio of the standard deviation to the mean at all radii is larger in the outflow layer.

Three distinct development phases of the model can be defined from the time variation of the SD. First, there is an "organizational phase,"

LEGEND

LEVEL 1 LEVEL 3

TEMPERATURE 0*1— i—i— r

285 Km.

345 Km.

0 24 46 72 96 120 144 166 192 TIME (HOURS)

285 Km.

0 24 46 72 96 120 144 168 192 TIME (HOURS)

285 Km.

0 24 48 72 96 120 144 168 192 TIME (HOURS)

RADIAL WIND

345 Km.

0 24 48 72 96 120 144 168 192 TIME (HOURS)

TANGENTIAL WIND

345 Km.

i I i I i I i I i

0 24 48 72 96 120 144 168 192 TIME (HOURS)

--f---r' I

24 46 72 96 120 144 168 192 TIME (HOURS)

Figure k\ Time variations of the standard deviations for temp eratures, radial winds, and tangential winds at inner radii.

10

TEMPERATURE

105 Km

0 24 46 72 96 120 144 168 192

TIME (HOURS)

105 Km

0 24 48 72 96 120 144 168 192 TIME (HOURS)

TANGENTIAL WIND

105 Km.

0 24 48 72 96 120 144 168 192

TIME (HOURS)

TEMPERATURE Mr— r

165 Km

TEMPERATURE

225 Km

0 24 48 72 96 120 144 168 192 TIME (HOURS)

RADIAL WIND

165 Km.

0 24 48 72 96 120 144 168 132 TIME (HOURS)

TANGENTIAL

WIND 165 Km.

' I ' I ' I ' I ' I ' I ' I i

o 6 -

24 48 72 96 120 144 168 192 TIME (HOURS) L£C€ND

0 24 48 72 96 120 144 168 192

TIME (HOURS)

RADIAL WIND

225 Km.

fc 5 -

' I ' I ' I ' I ' I ' I ' I i

pfcHT agga

0 24 48 72 96 120 144 168 192 TIME (HOURS)

TANGENTIAL

WIND 225 Km

i I i I ' I ' I ' I i I i I

> 5

24 48 72 96 120 144 168 192

TIME (HOURS)

LEVEL 1 LEVEL 3

Figure 5' Time variations of the standard deviations for temp' eratures, radial winds, and tangential winds at outer radii.

1 1

exhibited initially by the lack of asymmetries. Standard deviations of 0.5 m sec-1 or less are computed for both the radial and tangential winds during this phase. Increasing deviations first appear in the inflow layer and this is closely followed by the development of small asym- metries in the outflow layer. A period (symmetric phase) in which the SD's are small and relatively steady follows. Finally, an asymmetric phase begins at approximately 120 hours. This is characterized by the development of large scale asymmetries in the outflow layer and spiral bands of convection in the lower layer. At small radii, the SD of the tangential winds increases to 8 m sec x in the outflow layer. The asym- metries in the outflow layer radial wind field also experience rapid growth, but the magnitude of the SD is somewhat smaller than that of the tangential winds. The magnitude of the asymmetries of the two components is comparable in the inflow layer as are the circular means.

At the larger radii, both the inflow and outflow asymmetries de- crease with increasing radius (figs, k and 5). However, at a radius of 350 km from the vortex center, the asymmetries are still well defined and contain SD approximately equal to the magnitude of the mean radial and tangential flow. The lateral boundary conditions require the boundary velocity components to vanish at inflow points, and thus contribute to decreased SD's at large radii in the inflow layer.

The plots of temperature SD versus time also distinctly illustrate the three phases of the development of the model. However, the tempera- ture field is much more symmetric than the momentum field, as indicated by the small standard deviations of temperature. The decrease of SD with

12

increasing radius is due to the boundary conditions of a steady symmetric temperature .

h.2 Harmonic Analysis of the Momentum and Temperature Fields

The previous section established the rapid development of asym- metries at model time equal to 120 hours. In this section harmonic anal- ysis establishes the predominant scale of the asymmetries for both the inflow and outflow levels. Figures 6, 7, and 8 show the time variation of the scale of the percent variance accounted for by harmonic 1, 2, 3, k, and 8 at a typical inner {kS km) and outer (285 km) radius of the vortex.

An important feature revealed by the harmonic analysis is the pre- dominance of wave numbers k and 8 during the organizational and sym- metric stages of the vortex development. The grid boundary is an 8-sided figure comprised of k regular sides and k irregular sides. Wave number 8 is, therefore, probably a manifestation of the octagon shaped boundary of the grid. Wave number k is apparently a manifestation of the k irregular corners of the grid. Both wave patterns are also affected by errors associated with the numerical differencing scheme, especially in corner regions of the grid where the lateral boundary conditions may cause dif- ferent truncation errors. Recent investigations by Koss (1971) show that the numerical differencing utilized in an asymmetric vortex model can also induce error patterns that persist with time in the form of wave number k. Caution must be exercised in interpreting figures 6, 7, and 8. During the early stages of the experiment, the percent of variance con- tained by wave number k is very high (70% to 95%); however, the total

13

100%

RAOIAL WIND LEVEL i 45 Km.

100%

90%

24 48 72 96 120 144 168 192 TIME (HOURS)

RADIAL WIND

LEVEL 3 45 Km.

100%l I ' I ' I ' I ' I ' I ' I ' I '

90%

80%

70%

UJ 60%

u

z <

(E 50% ^40%

90%

20%

10%

0%

24 48

0%

100%

RADIAL WIND

LEVEL i 285 Km.

I ' I ' I ' I ' I ' I ' I ' I '

24 48

72 96 120 144 168 192 TIME (HOURS)

"T

RADIAL WIND

LEVEL 3 285 Km

I ' I ' I ' I

T

I'M

72 96 120 144 168 192

TIME (HOURS)

72 96 120 144 166 192

TIME (HOURS)

L EGEND

Ht -■ H4

Figure 6: Harmonic analysis of the model outflow layer and inflow layer radial wind component. Wave numbers 1, 2, 3, A, and 8 are illustrated at an inner and outer radius.

\k

100%

10% -

0%

TANGENTIAL WIND LEVEL i 45 Km.

i I i I i I i l i I i i ii

' ■"■' '

1D0%

0 24 48 72 96 120 144 168 192 TIME (HOURS)

TANGENTIAL WIND

LEVEL 3 45 Km

i I i I i I i I i I i I i I i I i

90% -

80% -

0%

TANGENTIAL WIND LEVEL 1 285 Km.

100%

90%

80%

70%

60% Id O

Z

| 50% ^40%

30%:

20%-

10%

0%«r

I I I I I I I I I I I I ' I I I I

100°/,

0 24 48 72 96 120 144 168 192 TIME (HOURS)

TANGENTIAL WIND LEVEL 3 285 Km.

i I i I i I i I i I i I i I i I i

80% -

0 24 48 72 96 120 144 168 192

TIME (HOURS)

0%

0 24 48 72 96 120 144 168 192 TIME (HOURS)

LEGEND

Figure 7: Harmonic analysis of the model outflow layer and inflow layer tangential wind component. Wave numbers 1, 2, 3, k, and 8 are illustrated at an inner and outer radius

15

TEMPERATURE LEVEL i 45 Km.

IOOXi I I I I I I I I I | I I I 1 I I I

0%,

-^ -, **■ I V I 1 I

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Hi H,

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Figure 8: Harmonic analysis of the model outlfow layer and inflow layer temperatures. Wave numbers 1, 2, 3, b , and 8 are illustrated at an inner and outer radius.

16

variance is very small. The SD of the tangential wind, for example, is only about 0.5 rn sec-1 contrasted with the mean flow of about 10 m sec in the outflow and 30 m sec-1 in the inflow layers.

The boundary induced wave numbers k and 8 are rapidly obscured by the presumably meteorological waves, 1, 2 and 3 with the onset of the asymmetric stages of the model. Figures 6, 7, and 8 all show the wave h trace and wave 1 trace intersecting at a time slightly less than 120 hours. Thereafter, the predominant wave is clearly wave 1 for both in- flow and outflow layers. Recent results (Anthes, 1972) show the growth of asymmetries in the outflow layer to be a result of barotropic insta- bility in which the energy source of the eddies is the kinetic energy of the mean flow. The temperature harmonic analysis shows essentially the same behavior as the momentum analysis, with wave number 1 becoming pre- dominant during the asymmetric stage. In summary it should be reempha- sized that the total variance in the inflow layer is small and that the temperature variance is small at both levels.

5. EDDY FLOW RELATED TO THE MATURE VORTEX This section presents a detailed analysis of the eddy flow in both the inflow and outflow levels during the mature stage of the vortex (17^ hours). Figures 9 and 10 are the streamline and isotjch analysis for the outflow and inflow levels, respectively. The asymmetric circulation in the outflow layer, the displacement of the vortex center from the grid center, and the relative symmetry of the inflow level, discussed earlier, are again illustrated by these figures. The isotach analysis shows that

17

STREAMLINES

LEVEL i

174 HOURS

Figure 9A: Streamlines - Level 1 ISOTACHS (M./SEC.) LEVEL 1

17** hours. 174 HOURS

Figure 9B: Isotachs (m./sec.) - Level 1 - 17^ hours

18

STREAMLINES

LEVEL 3

174 HOURS

Figure 10A: Streamlines - Level 3 - 1 74 hours. ISOTACHS (M./SEC.) LEVEL 3 174 HOURS

Figure 10B: Isotachs (m./sec.) - Level 3 - 1 74 hours

19

at least one or two maxima and minima can be located about the storm's center in the outflow layer.

5-1 Asymmetries in the Outflow Layer

Figure 11 shows the azimuthal means and SD for the upper level wind components at 1 7*t hours. The radial component is characterized by out- flow at all radii, with a maximum value of 7 m sec-1 at 75 km. The out- flow velocities decrease with increasing radii to a value of 2 m sec-1 at ^35 km, the edge of the domain. The tangential component is character- ized by a strong band of cyclonic winds near the center, with a maximum of Ik m sec"1 at hS km. The mean tangential winds become anticyclonic at a radius of 135 km and remain anticyclonic with increasing radii.

Black and Anthes (1971) used cirrus band motions, radiosonde winds, and limited aircraft data to construct similar figures for six individual Atlantic storms. They also presented data from Miller's (1958) mean Atlantic storm and Izawa's ( 1 964) mean Pacific storm. However, their calculations begin at approximately 105 km from the center and extend well beyond ^35 km. Two limitations exist in comparing the real storm data to the model storm data. First, the isolated nature of the vortex implies that the asymmetries and the mean flow diminish as the boundary is approached. In contrast, in the real atmosphere, the flow patterns at large radii interact with other atmospheric systems which produce addi- tional asymmetries. Second, near the center of the storms, Black and Anthes' data are compiled utilizing a coarse grid of 111 km as compared to the 30 km model grid. With these limitations in mind, a comparison be- tween the model figures and the actual storm data shows:

20

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1. There is favorable agreement between the magnitude of the model mean radial wind component (V ) compared with the six Atlantic storms. However, the magnitude of V is larger than either the Pacific or Atlantic mean profiles. Defining symmetry as a high ratio of the mean to the SD, the following comparisons of real and model outflow can be made:

(a) The SD approaches the magnitude of the mean radial wind in both the model and actual storm data.

(b) The magnitude of \l falls within the range of the magnitude of the real storm's radial winds.

(c) At large radii, the real storm tends to be more asymmetric than the model storm because the latter diminishes in in- tensity with increasing radius and the former merges with other large scale circulations.

(d) The magnitude of the asymmetries compares favorably with that of the mean Atlantic and Pacific storm's radial winds.

The harmonic analyses reveal the dominance of wave number 1 for both the model and the actual storm outflow. The percent of variance accounted for by the higher order wave numbers at increasing radii indi- cates the presence of more than one eddy in the outflow layer far from the model vortex center.

2. There is also favorable agreement between the magnitude of the

model mean tangential wind component (V ) compared with the actual storm

A

data, although again the model storm circulation is somewhat smaller in radial extent than the real storm circulation. Specifically, the model storm and the real storm show:

22

(a) a low ratio of the SD to the mean at inner radii, indica- ting symmetry;

(b) a higher ratio of the SD to the mean at the outer radii, indicating asymmetry;

(c) standard deviations for both tangential and radial wind components of about the same order of magnitude.

The harmonic analysis again shows a predominance of wave number 1 associated with the V,. Higher wave numbers appear at radii greater than 200 km and account for a larger percent of the variance than the higher

wave numbers associated with V .

r

Figure 12 shows the temperature departures from the mean tropical sounding (Herbert and Jordan, 1959) for both the inflow and outflow levels. The maximum departure of 7 degrees occurs to the east of the vortex center with smaller departures occurring to the west of the center The SD are small (less than 1°C) at all radii and approach zero with in- creasing radius, reflecting the steady state, uniform boundary conditions imposed on the temperature fields. The symmetry ratio of the mean to the SD is large, indicating that the temperature is nearly symmetric. The harmonic analysis shows a large percentage of the variance to be con- tained in harmonic one, with higher harmonics becoming more important at large radi i .

In summary, the model outflow momentum components are quite asym- metric, in agreement with the outflow asymmetries of the wind fields found in real storms. The temperature field is considerably more sym- metric than the corresponding wind fields.

23

TEMPERATURE DEPARTURES 174 HOURS

LEVEL 3

LEVEL 1

Figure 12: Temperature departures - 17*4 hours

2k

5.2 Asymmetries in the Inflow Layer Figure 13 exhibits the inflow level mean radial profiles and har- monic analysis for the model momentum and temperature fields at time equal to 17^ hours. Real storm data for a direct comparison are diffi- cult to obtain since most low-level studies have been performed at elevations considerably above the boundary layer.

The radial wind component is characterized by an inflow maximum of

28 m sec occurring at a radius of 75 km (same radius as the maxi

mum

outflow component). The inflow maximum rapidly diminishes to a value of

approximately 1 m sec" at R (k35 km). The small ratio of the SD to

max

the mean indicates some minor asymmetry at the outer radii. These fea- tures are within observable limits, but they are difficult to substanti- ate. This ratio is much smaller in the inflow layer than in the outflow layer, indicating a closer approximation to axial symmetry in the low levels .

The radial wind harmonic analysis shows that wave number 1 explains approximately 80-90 percent of the variance from 135 km outward. A possible verification of the dominance of wave 1 in the boundary level could be the track of low-level actual storm radar echoes as reported by Black (1971). By tracking and plotting the variations of echo velocities about an actual hurricane, Black found patterns which reproduced a nearly sinusoidal wave--hence, wave number 1.

Inward from 135 km, wave number h is large in the model storm. Additional data (not presented) show wave number h to be a persistent feature of the model during its life history before and after ]Jh hours.

25

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This condition is probably artificial and is a manifestation of the ini- tialization error due to the finite differencing scheme and boundary conditions. The standing wave number k does not occur in the upper out- flow layer which is upstream from the lateral boundary.

The mean tangential wind component is characterized by a maximum cyclonic circulation of k~J m sec-1 at a radius of 15 km (fig. 13) which

gradually diminishes to a value of k m sec-1 at R . For all radii, the

max

SD remains small with a maximum of 7 m sec-1 at hS km. The harmonic analysis shows that the greatest percent of the variance is contained in wave number 1. In summary, the small ratio of the SD to the mean indi- cates that the asymmetries in the boundary layer are much smaller than the asymmetries in the outflow layer.

The low-level temperature analysis (fig. 12) shows a maximum tem- perature deficit of 1.5°C. The deficit occurs at the vortex center with the remaining field characterized by flat gradients. Figure 13 displays the small SD found in the azimuthal mean temperatures and the strong boundary effects. Wave number 1 and 2 explain over 90% of the variance. Wave number k accounts for a smaller percent of the variance of tempera- ture than of momentum.

6. HORIZONTAL TRANSPORT MECHANISMS

The time variations and the scale of the boundary and outflow layer asymmetries have been discussed in previous sections. This section in- vestigates the importance of asymmetries as horizontal transport mecha- nisms. Computations of radially averaged horizontal and vertical fluxes

of absolute vorticity and angular momentum are presented, with the great- est emphasis placed on the horizontal transports.

27

6.1 Flux of Absolute Vorticity

The mean and eddy transports of absolute vorticity, v L and

r a

-A

v1 £' , for both the inflow and outflow levels of the model are presented in figure \k. The circularly averaged absolute vorticity, £ , is given

CI

by

C = JL^~ + f (7)

r9r '

where f is the coriolis parameter. The operator ( ) refers to the azimuthal mean at a given radius and ( )' refers to the departure from the mean. The outflow level flux of absolute vorticity shows that the eddy transports oppose the mean flux beyond 75 km. From 75 km to 165 km the eddy transport of vorticity is positive (outward) and dominant over the negative mean flux. Beyond 1 65 km, the mean flux becomes positive and is opposed by a negative eddy transport of vorticity of comparable magnitude. At the inner radii the mean and eddy transports are both positive with the mean flux much larger than the eddy flux.

The mean and eddy profiles of vorticity flux computed from the model experiment may be compared to similar profiles computed by Black and Anthes (1971) for real storms. Both model and real storms exhibit a radial annulus of substantial area in which the eddy transport of vor- ticity is negative and nearly balances the mean. This annular ring appears to be somewhat smaller in the model storm, a consequence perhaps of the overall small size of the model circulation. Comparisons near the center of the storm are difficult, because Black and Anthes1 data begin at 111 km from the storm center, and the errors associated with their

28

-1200

ABSOLUTE VORTICITY FLUX LEVEL i 174 HOURS

i r

T

i I r

j I i l_J I i I i I i l L

75 135 195 255 315

RADIUS (Km)

375 435

2000

1000

o

Id

?

ABSOLUTE VORTICITY FLUX LEVEL 3 174 HOURS

-1000-

-2000

1 1

1

1

1 | 1 | V

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v/C'aX

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-X^-X VrCa

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1 1

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. I.I.

0-

200

-0

- -100

15

75

135 195 255 315 375

RADIUS (Km)

-200

Figure \h: Profiles of mean and eddy transports of absolute vorticity for the model outflow and inflow levels.

29

measurements are maximum in this region. At the outer radii (r 195 km) the model transports agree in sign and magnitude with observations.

In summary, the eddies in the outflow layer (at moderate distances from the storm center) convey absolute vorticity inward toward the storm center and oppose the outward vorticity flux by the mean flow in both the real and model storm.

The boundary layer flux of absolute vorticity (fig. ]k) shows small positive eddy transports of vorticity at all radii in agreement with previous theoretical estimates (Anthes, 1970). The mean flux is strongly negative (inward) at all radii. Values range over two orders of magni- tude. Therefore, vorticity is conveyed inward by the mean flow and com- pletely dominates the eddy flow. This again emphasizes the basic sym- metry in the inflow layer.

6.2 Flux of Angular Momentum

The mean, the eddy and the total transports of relative angular mo- mentum, (weighted by radial distance), for both the outflow and inflow levels of the model are presented in figure 15- In the outflow layer, the mean flow transports negative momentum outward, while the eddies op- pose the mean flow by transporting pos i t i ve angular momentum outward. The mean and eddy terms are the same order of magnitude and tend to com- pensate for each other. In contrast, actual storm data of Black and Anthes (1971) show both components to have a net outward transport of negative relative angular momentum. However, the radial extent of the model is only half of that of the actual storm data and does not extend to the outer radii where the larger negative angular momentum fluxes are

30

o

id V)

15

ANGULAR MOMENTUM FLUX LEVEL i 174 HOURS

10

i i i i i r

l r r-

r2(v^vx+vTv()

1 1 1 1

0

i i i i i

s

-10

1 1 1

75

135 195 255 315 375 435

RADIUS (Km)

2o r- 1 r

-60

ANGULAR MOMENTUM FLUX LEVEL 3 174 HOURS 1 1 I I I l T

i r

J I I l I I L

J I I L

15 75 135 195 255

RADIUS (Km)

315

375 435

Figure 15: Profj_le_s of mea n (rvrvx^» eddy (r v'vp , and total (r2(v vx+v'vi) transports of angular momentum for the model outflow and inflow levels.

31

found (Palmen and Riehl, 1957)- In general, the magni tudes of the eddy momentum flux associated with the model and real storms are small inside ^tOO km. The model flux tends to be positive, and the flux associated with real storms tends to be negative.

The boundary layer flux of relative angular momentum (fig. 15) shows a very small outward eddy flux of positive angular momentum. The mean transport shows a strong inward flux of positive angular momentum. The mean completely dominates the eddy transport at all radii. This result is in agreement with Riehl and Malkus (1958), who found the eddy trans- ports of momentum to be either negligible or outward in the inflow layer of hurricane Daisy. These results also agree with Pfeffer (1958) who found that within a few hundred kilometers from the vortex center the horizontal -eddy processes are of the wrong sign to account for the inward transport of angular momentum in the inflow layer of hurricane Connie, 1955.

In summary, the eddy transport of angular momentum in the model out- flow layer is slightly positive; while in contrast, the eddy flux in real storms appears to be slightly negative. There is good agreement between the model and observations in the mean flux, however. In the inflow layer, the mean flux is dominant and is directed inward. The eddy flux is small, but directed outward, in good agreement with observations. 6.3 Vertical Flux of Relative Angular Momentum

It is of considerable importance to the overall dynamics of the model to determine the origin of the asymmetries in the outflow layer. As previously established, the outflow level is characterized by two

32

preferred quadrants of outflow (fig. 3). It is conceivable that azimuth- al variation in the vertical flux of relative angular momentum could be responsible for the two streams of outflow.

Figure 16 shows azimuthal mean radial profiles of the mean vertical

transport and eddy vertical transport of relative angular momentum,

\-\ X

( r v-v o ) , (r v|a ' ), where a is the "vertical velocity in the a-system.

The a information levels are staggered in the vertical from the dynamic

variables, necessitating the interpolation of the wind components to the

a levels. The radial profiles clearly show that the vertical flux of mo- mentum is predominantly from the mean current. Although the outflow occurs in two quadrants the vertical motion is bringing momentum to the outflow level in a symmetric fashion. Thus the asymmetries are develop- ing after the air reaches the outflow layer. This result is consistent with Anthes ' (1972) findings that the asymmetries are a result of dynamic instability in the horizontal flow, with the eddies growing at the ex- pense of the mean horizontal flow.

7. SUMMARY AND CONCLUSIONS Conventional statistical techniques have been utilized to show the formation and structure of horizontal asymmetries in the outflow and in- flow levels of a numerical hurricane model. The outflow layer is highly asymmetric, especially at the outer radii. The inflow layer contains relatively small asymmetries, and the approximation to axial symmetry is very good in the low levels. These results agree well with observations.

33

VERTICAL FLUX OF RELATIVE MOMENTUM LEVEL 2' 174 HOURS

50

0-w

o

CO

CM

-50

-100-

1

.... r p.- T T ,- ! r r T

"T"

<<*'"

rvxx*x

-

-

1

i . i . i . i .

_l_

15 75 135 195 255 315

RADIUS (Km)

375 435

VERTICAL FLUX OF RELATIVE MOMENTUM LEVEL 3' 174 HOURS

T r

-200

13.5 195 255 315 RADIUS (Km)

435

Figure 16: Profiles of mean and eddy vertical transports

of relative momentum for the model outflow and inflow levels

3*»

A comparison with real storms reveals that the model is capable of reproducing many observed features of the mature three-dimensional tropical cyclone. Slight differences between the observed and model vortices are attributed to the limited lateral extent of the model as the errors associated with the irregular boundary.

The mean transport of absolute vorticity beyond 200 km in the out- flow layer is outward from the storm center and is opposed by the eddy flux of absolute vorticity in both the real and model vortices. The mean flux of absolute vorticity in the model inflow layer is strongly in- ward and completely dominates the small eddy flow, in agreement with real storms. Beyond 135 km, the mean transport of relative angular momentum in the outflow layer is negative; the eddy flux of angular momentum is positive. Radial profiles of the vertical flux of momentum show that the vertical transport of momentum is dominated by the mean current, indica- ting that vertical eddies play no important role in the formation of the eddies in the outflow layer.

35

8. REFERENCES

Anthes, R. A. (1972), The development of asymmetries in a three-dimen- sional numerical model of a tropical cyclone, Monthly Weather Review, ( i n press) .

Anthes, R. A. (1970), The role of large-scale asymmetries and internal mixing in computing meridional circulations associated with the steady-state hurricane, Monthly Weather Review, 98, No. 7, July, 521-528.

Anthes, R. A., S. L. Rosenthal, and J. W. Trout (1971a), Preliminary re- sults from an asymmetric model of the tropical cyclone, Monthly Weather Review, (in press).

Anthes, R. A., J. W. Trout, and S. S. Ostlund (1971b), Three dimensional particle trajectories in a model hurricane, Weatherwise, (in press).

Anthes, R. A., J. W. Trout, and S. L. Rosenthal (1971c), Comparisons of tropical cyclone simulations with and without the assumption of circular symmetry, Monthly Weather Review, (in press).

Black, P. G. and R. A. Anthes (1971), On the asymmetric structure of the tropical cyclone outflow layer, Journal of the Atmospheric Sciences, (in press) .

Black, P. G. (1971), Use of echo velocities to evaluate hurricane modi- fication experiments, Project STORMFURY Annual Report 1970, U. S. Department of the Navy and U. S. Department of Commerce, Appendix J, J-1 - J-20.

Gray, W. M. ( 1 967) , The mutual variation of wind, shear and barocl i nici ty in the cumulus convective atmosphere of the hurricane, Monthly Weather Review, 95, No. 2, February, 55~73-

I zawa , T. (1964), On the mean wind structure of typhoons, Typhoon Research Laboratory, Technical Note N . 2, Meteorological Research Institute, Tokyo, Japan.

Koss , W. J. (1971), Numerical integration experiments with variable reso- lution two-dimensional cartesian grids using the box method, Monthly Weather Review, (in press).

Kurihara, Y. and J. L. Holloway (1967), Numerical integrations of a nine- level global primitive equation model formulated by the box method, Monthly Weather Review, 95, No. 8, August, 509-530.

36

Matsuno, T. (1966), Numerical integrations of the primitive equations by a simulated backward difference method, Journal of the Meteorologi- cal Society of Japan, kk , February, 76-83.

Miller, B. I. (1958), The three-dimensional wind structure around a

tropical cyclone, National Hurricane Research Project Report 15, U. S. Department of Commerce, National Hurricane Research Labora- tory, Miami, Florida, January, 41 pp.

Palmen, E. and H. Riehl (1957) , Budget of angular momentum and energy in tropical cyclones, Journal of Meteorology, 14, 1 50- 1 59 -

Pfeffer, R. L. (1958), Concerning the mechanics of hurricanes, Journal of Meteorology, 15, 113-119-

Phillips, N. A. (1957), A coordinate system having some special advan- tages for numerical forecasting, Journal of Meteorology, 1A, April, 184-185.

Riehl, H. and J. S. Malkus (1958), Some aspects of hurricane Daisy, Tellus, 13, 181-213.

Rosenthal, S. L. (1971), A circularly symmetric primitive equation model of tropical cyclones and its response to artificial enhancement of the convective heating functions, Monthly Weather Review, 99, No. 5, May, k]k-k26.

Rosenthal, S. L. (1970a), Experiments with a numerical model of tropical cyclone development some effects of radial resolution, Monthly Weather Review, 98, No. 2, February, 106-120.

Rosenthal, S. L. (19 70b) , A circularly symmetric primitive equation

model of tropical cyclone development containing an explicit water vapor cycle, Monthly Weather Review, 98, Vol. 9, September, 6^3~663.

Rosenthal, S. L. (1969), Numerical experiments with a multilevel primi- tive equation model designed to simulate the development of tropical cyclones: experiment I, ESSA Technical Memorandum ERLTM-NHRL 82, U. S. Department of Commerce, National Hurricane Research Labora- tory, Miami, Florida, 36 pp.

Smagorinsky, J., S. Manage, and J. L. Hoi loway (1965), Numerical results from a nine-level general circulation model of the atmosphere, Monthly Weather Review, 93, No. 12, December, 727-768.

37

USCOMM ERL

42

U.S. DEPARTMENT OF COMMERCE

National Oceanic and Atmospheric Administration

Environmental Research Laboratories

NOAA Technical Memorandum ERL AOML-14

FREE-AIR GRAVITY ANOMALIES

SOUTH OF PANAMA AND COSTA RICA

(NOAA SHIP OCEANOGRAPHER - AUGUST 1969)

Robert J. Barday Marine Geology and Geophysics Laboratory

Atlantic Oceanographic and Meteorological Laboratories Miami, Florida September 1971

TABLE OF CONTENTS

PAGE

1. INTRODUCTION 1

2. DATA ACQUISITION AND REDUCTION 2

2.1 Zeroed Meter Gravity 2

2.2 Gravity Meter Reading 3

2 . 3 Eotvos Correction 3

2.4 Drift Correction 8

3. DATA QUALITY 12

4. DATA PRESENTATION 12

5. DISCUSSION 14

6. ACKNOWLEDGEMENTS 18

7. REFERENCES 19 APPENDIX: Profiles 21

in

ILLUSTRATIONS

PAGE

Figure 1 6

Figure 2 9

Figure 3 11

Figure 4 13

Plate 1 (in pocket)

IV

FREE-AIR GRAVITY ANOMALIES SOUTH OF PANAMA AND COSTA RICA (NOAA SHIP OCEANOGRAPHER - August 1969)

Robert J. Barday

Free-air anomaly profiles from a geophysical investigation centered on the Panama Fracture Zone are presented with their corresponding bathymetric profiles. The quality of these profiles is indi- cated by a mean free-air anomaly discrepancy of 3.48 milligals with a standard deviation of 3.28 milligals for 99 crossings of the ship's track. These data support the existence of a deep, sedi- ment-filled depression at the northern end of the Panama Fracture Zone, the presence of a sediment- filled marginal trough east of the Coiba Ridge, and the accumulation of thick sedimentary deposits on the eastern flanks of both the Cocos and Coiba Ridges. The gravity data also suggest that there is no large-scale change in crustal structure across the Panama Fracture Zone, and the entire survey area may be slightly out of isostatic adjustment .

1. INTRODUCTION

In August 1969 a geophysical investigation of the Panama Fracture Zone was conducted by the National Oceanic and Atmospheric Administration Ship OCEANOGRAPHER. Depth, total magnetic intensity, and gravity meter readings were recorded continuously over approximately 11,200 km of track- line controlled by satellite navigation. This report presents free-air anomaly profiles and discusses certain

geological conclusions that are consistent with the observed gravity data.

2. DATA ACQUISITION AND REDUCTION

By definition, the free-air anomaly can be expressed as

FA=g0-Y0 CD

where Yo=978 0i+9 (1 + 0 0052884sin2c}>-0 . 0000059sin22<f>) is the theoretical sea level gravity given by the 19 30 internation- al gravity formula, and gQ is the observed gravity reduced to sea level. For sea level gravity observations

go=ZMG+R+Ec+Dc (2)

where ZMG (zeroed meter gravity) is a value equivalent to a gravity meter reading of zero, R is the meter reading (in milligals), Ec is the Eotvos correction, and Dc is the drift correction.

Both data acquisition and reduction can most easily be discussed from a term-by-term consideration of (2).

2.1 Zeroed Meter Gravity

The ZMG was obtained from a land tie at Rodman Naval Station, Canal Zone, immediately before the survey. [The details of the ZMG computation have been discussed by Orlin and Sibila (1966).] The base station is described by Woollard and Rose (1963) as follows:

WH 1015. Rodman Naval Base, at shore end of center of three piers next to large valve block painted black and yellow, Lamont No. BE 1-1.

2 . 2 Gravity Meter Reading

The gravity meter used for this survey was Askania "Sea Gravimeter Gss2 after Graf, Model C, No. 22 (Graf and Schulze, 1961; Schulze, 1962) mounted on an electrically erected Anschiitz Gyrotable. The gravity meter dial reading, Rj (R(j=R/Kcj where K, is a constant necessary to convert dial divisions into milligals), was recorded both digitally and on analog strip chart.

All digitized dial readings were plotted against time, and the values appearing to be inconsistent were checked against the analog strip chart. If discrepancies were found, the digitized values were adjusted. If the inconsistencies- persisted, the values in question were deleted unless they could be related to any changes in speed or changes in course less than 90°.

2 . 3 Eotvos Correction

Accurate navigation is critical to marine gravity ob- servations. At 5°N, the mean latitude of this survey, and at 2 7 km/hr, the average speed of this survey, the rates at

which the Eotvos correction changes with respect to course and speed are 2.1 milligals/0 (for a N-S trackline) and 3.7 milligals/km/hr (for an E-W trackline). If the free-air anomaly is to be determined to an accuracy of 1 milligal (the accuracy to which R was measured), the course and speed must be known within 0.5° and 0.2 km/hr, respectively.

Because the course and speed are computed from the smooth plotted track, their accuracy depends upon the accu- racy of the fixes, the elapsed time between fixes, and the interpolation method used to determine the ship's track between fixes .

This survey was controlled by the Navy's satellite navigation system with the AN/SRN-9 equipment (Guier, 1966). The accuracy of this system is largely influenced by uncer- tainty in the .ship's velocity. As a first approximation, a 1.8-km/hr error in the ship's velocity results in a 0.45-km error in the computed satellite fix (Stansell, 1970). If the velocity is estimated from sea trial data or the speed made good between previous fixes, as in the case of this survey, then the computed fixes may be in error by as much as 2 km.

The average time interval between fixes was 2 hr . At this interval an error of 45 km in the satellite fixes would result in a one-milligal error in the computed Eotvos

correction. However, the elapsed time between fixes ranged downward to 2 2 minutes implying a possible error in the Eotvos correction of 10 milligals or more.

The interpolation method used to determine the smooth plotted track was based on the assumption that the course and speed made good are constant between navigation points. (Navigation point is used here to mean a point where there is a satellite fix or a change in course and/or speed.) The computed Eotvos correction was, therefore, a discontin- uous step function rather than a continuous function between course and speed changes.

To remove these artificial discontinuities and minimize error in the Eotvos correction, the following technique was used (refer to fig. 1):

(1) For all but E-W lines both the speed made good, SMG

(B, fig. 1), and the difference between the course made good and the course steered, CMG-CST (A, fig. 1), were plotted against time. Both plots were then approxi- mated by piecewise continuous curves in which discontinuities occurred at any changes in speed and at changes in course greater than 10°.

(2) For E-W lines the Eotvos correction (C, fig. 1), rather than SMG and CMG-CST, was similarly treated.

(3) These piecewise continuous curves were, in turn, approximated by straight line segments.

10 11 12 1J 14 15 16 17 1800

Sgl

Figure 1. Based on the assumption that the course and speed made good are constant between navigation points , the difference between the course made good and the course steered (CMG-CST), the speed made good (SMG), and the Eotvos correction become piecewise continuous step

functions of time [dashed curves ( )]. The solid

curves ( ) illustrate a technique whereby these param- eters can be made to more closely approximate continuous functions of time (not shown for clarity). Curves A and B are from a N-S profile (No. 14) and curve C is from an E-W profile (No. 3). The numbers enclosed in boxes ( I3b91 ) signify the course steered for each seg- ment of the CMG-CST curve bounded by circles (o). The Eotvos correction used to compute the free-air anomaly is determined from a linear time interpolation of the circled values.

(4) The time, course, and speed or the time and Eotvos

correction at each break in slope were entered into a computer program that obtained the free-air anomaly at each data point using the Eotvos correction computed from a linear time interpolation of these parameters. For all but E-W lines the program also requires course and speed values immediately before and after each change in course steered. This technique is based on the assumption that the differ- ence between the course and speed made good and the ordered course and speed is the result of the current acting on the ship. Although current in this sense of the word includes many factors in addition to horizontal movement of the water, its effect on the ship should vary smoothly between large changes in course and speed. Therefore, the speed made good and the difference between the course made good and the course steered should be continuous functions of time be- tween speed changes and large changes in course steered. Because the Eotvos correction computed for E-W lines is insensitive to small changes in course, it must likewise be continuous .

2.4 Drift Correction

Because of instrumentation failure it was impossible to complete a land tie at the conclusion of this survey. The drift, D [D=-D /(t-t ) where t is the time of observation and tQ is the time of ZMG determination] , was determined as follows :

(1) The free-air anomaly was computed without a drift cor- rection.

(2) The differences AFA. . and At., where i<j were deter-

mined for each trackline intersection: AFA- =FA. . -FA. .

ID 31 13

and At . . =t . . -t + where FA., is the free-air anomaly and ID 31 ^ D1

t.. is the time of profile j at its intersection with profile i.

(3) The drift was computed by a least squares fit of the

function AFA=DxAt to the pairs AFA-., At...

Illustrated in figure 2 , this procedure follows from the

identities FAN-; EFA- -Dx( t . . -t ) and FAN . . EFA. . -Dx(t . . -t ) 1D ID !D o di D1 D1 °

where FAN., is the drift-corrected free-air anomaly of pro- Di

file j at its intersection with profile i. Therefore,

AFAN. .=FAN. .-FAN. . 3-D 31 ID

=FAji-Dx(tji-t0)-FAij+Dx(tij-t0)

=FA. .-FA- .-Dx(t. .-t. .) Di ID Di ID

=AFAi.-DxAti- .

+APA

'PAij

*VM±i-**Aifl>.^

-/\FA

Figure 2. A statistical method for determining drift. The free-air anomaly difference for each crossing of the ship's track is plotted against the corresponding time difference. The drift, D, is the slope of the straight line through the origin which (in a least squares sense) most closely fits all the points ( AFA— ,At.j_ ) .

Assuming that the correct drift would minimize the crossing errors ,

3D

N

^ '

l_j 13 13

i,3=l

N

= 0

-2x \ 'a. .x(AFA. .-DxAt. . )xAt. Z , ^ x3 ^ i:

= 0

N

N

/ (a- -xFAn- -xAt. )-Dx Y~ a..x(At..) =0 Z , !3 !3 13 L , 13 13

i»j=l i>3=l

2ZL a^xFA^xAt^

D=

EL^.-xCAt..)2

N

r

i,3=l where N=the number of tracklines and ^--=1 if i< j , or a...=0

if i>j .

The method outlined above is valid if a statistically significant number of crossings are available. For this survey (fig. 3), 99 crossings were used, and the computed drift of 0.17 milligals per day is consistent with the gravimeter's drift history.

In the final stages of data processing, time profiles of the free-air anomaly were plotted on an automatic X-Y plotter. Residual discontinuities at course and speed

10

FREE-AIR ANOMALY DIFFERENCE (JIILLIGALS)

<n * fooa)g>-frroOro-frg>coOM-frc*

rv>

w

yi

o>

oo

O (0

5

IB

c*i

Ui

-i 1 1 r

o o

o o

o o

o I o

o

' i , i I i 1,1

Figure 3. The free-air anomaly differences plotted against the corresponding time differences for 99 crossings of the ship's track. The slope of the solid line through the origin (0.17 milligals per day) is the drift of the gravimeter during this survey.

11

changes were smoothed out by eye or deleted, and appropriate corrections were applied to the raw data tape.

3. DATA QUALITY

Figure 4 is a histogram of free-air anomaly discrepan- cies [free-air anomaly discrepancy is defined here as the absolute value of the free-air anomaly difference, AFA. . (sect. 2.4)] at crossings of the ship's track. For 99 usable crossings the mean free-air anomaly discrepancy is 3.48 milligals with a standard deviation of 3.28 milligals. Free-air anomaly discrepancies larger than 10 milligals are without exception from regions of very steep gravitational gradient .

In regions of gentle gravitational gradient the free- air anomalies compare within 10 milligals to those furnished by Oregon State University and Lamont-Doherty Geological Observatory .

Satellite navigation contributed immeasurably to the data quality, and the calm seas (sea state 3 or less) en- countered throughout the survey kept the cross-coupling and off-leveling errors to a minimum.

4. DATA PRESENTATION

The data are presented in profile form with the free- air anomaly plotted above the corresponding bathymetry. All

12

24

23 22 21 20 19 18 17 16 15 14

g 13

12 11 10 9 8 7 6 5 4 3 2 1 0

-Mean

99 Crossings

Mean = 3.48 milligals

Standard Deviation = 3.28 milligals

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 FREE-AIR ANOMALY DISCREPANCY (MILLIGALS )

Figure 4. Histogram of free-air anomaly discrepancies at crossings of the ship's track.

13

profiles are numbered and keyed to an index map (see Appen- dix and Plate 1). The free-air anomaly profiles are plotted with a vertical scale labeled in milligals and selected to give them a "relief" comparable with the accompanying ba- thymetric profiles. Depths (after Grim, 1970a) are plotted in meters with a vertical exaggeration of 50:1. Those pro- files from trackline segments that are essentially N-S or E-W are plotted against latitude or longitude, respectively. All other profiles are plotted against distance.

The profiles are in three groups. The first includes all E-W profiles south of 7°N. Generally these profiles are arranged according to decreasing latitude. Included in the second group and arranged according to decreasing longitude are all the N-S profiles south of 7°N. The third group in- cludes the relatively short profiles north of 7°N and those profiles that are oblique to meridians and parallels of latitude .

The profiles presented were produced by an off line CalComp plotter with a computer program written by Grim (1970b) .

5. DISCUSSION

If the vertical exaggeration of the free-air anomaly profiles is selected to give them about the same "relief" as the bathymetric profiles , then they should look like

14

filtered versions of the bottom topography. Departures from this relationship are attributable to lateral varia- tions in the subsurface density.

The most striking departure of the free-air anomaly profiles from their corresponding bathymetric profiles is a negative anomaly, shown in profiles 33, 36, 38, 53, 54, and 55, associated with the northern extension of the Panama Fracture Zone. North of 7°N the western trough of the Panama Fracture Zone bends slightly to the west and develops an asymmetric V-shaped profile (profiles 38 and 55). Where- as the western flank of this trough is very steep, the nearshore, eastern flank has a gentle slope with a charac- teristically rugged appearance. The free-air anomaly associated with the western flank follows the bathymetry quite closely, decreasing sharply from +25 milligals or more to less than -25 milligals. The eastern flank free-air anomaly, however, departs radically from the bottom profile; whereas the bottom profile slopes toward the trough, the free-air anomaly in most cases slopes away from the trough. Furthermore, the free-air anomaly shoreward of the trough is considerably more negative than would be expected from the bathymetry.

In profile 5 5 the trough is marked only by an inflexion in the free-air anomaly. A -68-milligal low in the free-air anomaly profile lies about 40 km shoreward of the trough.

15

Similarly, the -6 2-milligal low of profile 36 is displaced about 20 km east of the trough. The f^ree-air anomaly of profile 38, on the other hand, apparently does not continue to decrease east of the trough. Profiles 33, 53, and the extreme eastern end of profile 54 show an inverse relation- ship between the slopes of the free-air anomaly and the characteristically rugged bathymetry.

These observations are consistent with the occurrence of a deep, sediment-filled depression that van Andel et al . (19 71) have proposed to exist between the Cocos and Coiba Ridges .

Another similar departure of the free-air anomaly from the bathymetry is the negative anomaly associated with a gentle bathymetric depression extending from the eastern edge of the survey area (80°W) to about 81°40'W on the east- ern flank of the Coiba Ridge. Although the axis of this depression is not crossed by any of the survey lines, it appears to be nearly coincident with profile 31 . The free- air anomaly, on the other hand, continues to decrease at least as far north as profile 1.

It is evident that this free-air anomaly pattern is a continuation of the negative anomaly belt (Hayes, 1966) that extends around the Gulf of Panama from the Peru-Chile Trench. Hayes suggested that the most significant contribution to this negative anomaly belt may be the "edge effect" (Worzel,

16

1965) of a steep continental slope. However, the observa- tion that west of 80°W the axis of this negative anomaly belt lies well shoreward of the bathymetric depression axis is better explained by the sequence of deep, sediment-filled marginal troughs proposed by van Andel et al . (19 71).

Especially evident in profile 3 is the departure of the free-air anomaly from the bathymetry on the eastern flanks of the Cocos and Coiba Ridges. West of the Panama Fracture Zone the eastern flank of the Cocos Ridge rises rather uniformly while the free-air anomaly levels off west of 8 3°40'W. The free-air anomaly centered over the crest of the Coiba Ridge falls off more rapidly to the east than might be expected from the bathymetry. These deviations of the free-air anomaly from the bottom topography are the re- flection of thick accumulations of sediment on the eastern flanks of both ridges (van Andel et al., 19 71, figs. 5B and 11G) . This profile also suggests that there is no large- scale change in crustal structure across the Panama Fracture Zone.

The entire survey area may be slightly out of isostatic adjustment, as indicated by an average free-air anomaly of between +10 and +20 milligals.

17

6 . ACKNOWLEDGEMENTS

I thank the officers and crew of the National Oceanic and Atmospheric Administration Ship OCEANOGRAPHER who made this study possible. Paul Grim furnished the data pre- sented in this report. He also supplied most of the computer programs used and assisted in many ways throughout this study. Additional gravity data were provided by Dr. Richard Couch, Oregon State University, and Manik Talwani, Lamont-Doherty Geological Observatory. R. K. Lattimore, Paul Grim, and Dr. George Peter assisted by reviewing the manuscript.

18

7. REFERENCES

Graf, A. and R. Schulze (1961), Improvements in the sea gravimeter Gss2, J. Geophys . Res. 6_6, 1811-1821.

Grim, P. J. (1970a), Bathymetric and magnetic anomaly pro- files from a survey south of Panama and Costa Rica, (unpublished report) ESSA Tech. Memo, ERLTM-AOML 9. (Environmental Research Laboratories, Boulder, Colorado 80302) .

Grim, P. J. (1970b), Computer program for automatic plotting of bathymetric and magnetic anomaly profiles , (unpub- lished report) ESSA Tech. Memo, ERLTM-AOML 8. (Environmental Research Laboratories, Boulder, Colorado 80302) .

Guier, W. H. (1966), Satellite navigation using integral

Doppler data -- the AN/SRN-9 equipment, J. Geophys. Res. 71, 5903-5910.

Hayes, D. E. (1966), A geophysical investigation of the Peru-Chile trench, Marine Geology ^ 309-351.

Orlin, H. and D. V. Sibila (1966), General instructions, gravity observations at sea, part II: askania stable platform mounted seagravimeter , U. S. Department of Commerce, ESSA, Coast and Geodetic Survey.

Schulze, R (1962), Automation of the sea gravimeter Gss2, J. Geophys. Res. 67, 3397-34-01.

19

Stansell, P. A., Jr. (1970), The Navy navigation satellite

system: description and status, The International Hydro- graphic Review, XLVII , 51-70.

van Andel, T. H., G. R. Heath, B. T. Malfait, D. F.

Heinrichs , and J. I. Ewing (1971), Tectonics of the Panama Basin, eastern equatorial Pacific, Geol . Soc. Amer. Bull. 8_2, 1489-1508.

Woollard, G. P. and J. C. Rose (196 3), International Gravity Measurements, Society of Exploration Geophysicists , Tulsa, Oklahoma, 518 p.

Worzel, J. L. (19 65), Deep structure of continental margins and mid-ocean ridges, In: W. F. Whittard and R. Brad- shaw (Editors), Submarine Geology and Geophysics -- Colston Papers, Butterworth, Washington, D.C., 335-359.

20

APPENDIX

Profiles

The following pages display the computer-produced pro- files from the survey area

Profile

Page

Profile

Page

Profile

Page

Profile

Page

1

22

14

35

27

23

42

27

3

24

15

49

28

44

43

37

4

40

16

36

29

51

44

29

5

26

17

25

30

44

45

43

6

37

18

39

31

23

46

31

7

28

19

49

32

48

47

38

8

42

20

40

33

48

48

29

9

30

21

27

34

46

49

38

10

34

22

41

36

46

50

31

11

32

23

49

38

47

51

34

12

51

24

42

39

37

52

50

13A

33

25

51

40

25

53

48

13B

33

26

43

41

43 |

54 55 62

47 45 45

Table 1. Index of Profiles

21

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PLATE 1

Reprinted from The American Association of Petroleum Geologists Bulletin 55, No. 10, 17 30-1740 .

43

Marine Geophysical Study Northeast of Trinidad-Tobago1

B. G. BASSINGER,2 R. N. HARBISON,2 and L. AUSTIN WEEKS3

Miami, Florida 33130, 33158

Abstract Marine geophysical measurements off Trinidad- Tobago delineate prominent structural trends revealed in the shallow sedimentary strata. Pilar block is one of the prominent structures along the boundary between the South American continent and Caribbean plate. The block is a narrow horst bounded on the north and south by major fault zones, which apparently continue from the Araya Peninsula of Venezuela eastward to about 58°50'W. Structural features north and south of the Pilar block either die out at the block or veer subparallel with it. North of the block, the Barbados Ridge is an anti- clinorium which shows evidence of folding and fracturing apparently as a single tectonic unit. Long-period, high- amplitude magnetic anomalies, forming a zone somewhat parallel with the Lesser Antilles arcuate trend, suggest that the prominent trends of the anticlinorium extend across the continental shelf to the Pilar block. Within the study area, the geophysical data show no evidence for extensive translation between the South American con- tinent and the Caribbean plate in comparatively recent time.

Introduction

During the summers of 1968 and 1969, the USC&GS ship Discoverer conducted recon- naissance marine geophysical investigations in the area off northern Venezuela and Trinidad and around the southern end of the Lesser An- tilles arc. Ship's traverses for this study covered the area south of 12°30'N between the To- bago Trough and Trinidad to 58°30'W (Fig. 1 ). The investigation was designed to study the eastward extension of the predominantly east- west-trending structures of northern Venezuela and Trinidad, and their structural relation to the island of Tobago and the Barbados Ridge on the north. Data collected west of the study

1 Manuscript received, August 24, 1970; accepted, December 3, 1970.

2 National Oceanic and Atmospheric Administration (NOAA), Atlantic Oceanographic and Meteorological Laboratories.

3 Consultant; formerly, Environmental Science Ser- vices Administration.

The writers are grateful to the officers and men of the USC&GS (NOAA) ship Discoverer and the AOML personnel who participated in the project. We are particularly indebted to G. A. Lapiene, Jr., and L. W. Mordock (USESSA) for their assistance in con- ducting the field work and to Sue O'Brien and George Merrill for drafting the figures. L. W. Butler and G. H. Keller critically reviewed the paper.

© 1971. The American Association of Petroleum Geologists. All rights reserved.

area are presented by Lattimore et al. (1971). Regional implications of both studies are dis- cussed by Weeks et al. (1971).

Seismic reflection profiles (SRP) were made only on traverses across postulated major struc- tural trends. Continuous gravity, magnetic, and bathymetric observations were recorded on all traverses. Within the study area of this paper, geophysical data were obtained along approxi- mately 3,430 km (1,850 n. mi) of ship's track with SRP records made over about 2,410 km (1,300 n. mi) of the area traversed. The sound source for the SRP system was a 164-cc (10 cu in.) pneumatic gun. Gravity and magnetic ob- servations were made with an Askania seagra- vimeter and a Varian nuclear resonance mag- netometer respectively. Position control was de- termined by the best source available dead reckoning, land ties by visual fixes and radar, Loran A and C, and Omega. These data were collected by methods described in Lattimore et al. (1971).

The track-line pattern and bathymetry in the study area are shown in Figure 1 of Weeks et al. (1971). Line drawings of representative SRP records correlated with gravity and mag- netic observations are presented in Figure 2. Parts of original SRP traverses are reproduced in Figures 3-7. In the interpretation of the SRP records, the reflector generally referred to as basement is the deepest observed reverberant reflector beyond which no penetration is ob- tained within the resolution of the equipment. This reflector, varying in acoustic character over the study area, corresponds in depth to the 3.97 km/sec (13,000 ft/sec) or higher veloc- ity material reported by Ewing et al. (1957).

Previous Investigations

Geologic structures of the islands of Trini- dad-Tobago and surrounding area have been described by numerous investigators. Some of the results have been presented by Schuchert (1935), Maxwell (1948), and Suter (1960). In the study area, near-surface, shallow-water sedimentation and geologic structure were stud- ied by Koldewijn (1958), van Andel and Sachs (1964), and van Andel (1967). Deep crustal studies based on seismic refraction results in

1730

Marine Geophysical Study Northeast of Trinidad-Tobago

1731

Fig. 1. Major structural trends and location of representative traverses. Barbados anticlinorium is complex of structures lying east of Tobago Trough through East ridge.

the Caribbean, across the Lesser Antilles island arc, and in the Atlantic were summarized by Officer et al. (1959). Some of these velocity data were analyzed by Ewing et al. (1957) and later utilized in presenting a summary of the crustal section of the Caribbean area (Edgar, 1968). Higgins (1959) compared the offshore velocity data with similar velocities from geo- logic structures on Trinidad. Recently, Sykes and Ewing (1965) discussed the seismicity of the Caribbean for the period 1950-1964 and related its occurrence to boundaries between prominent structures.

The Caribbean plate and adjacent South American continent have been described as contrasting crustal blocks with great horizontal movements along major boundary faults. Di-

verse interpretations were made concerning the interaction between these crustal blocks and the boundary fault systems. Hess (1938) suggested that the Caribbean block was translated east- ward 80-160 km (50-100 mi). However, Eardley (1954) summarized the earlier hy- potheses and presented an argument for subsi- dence of the Caribbean basin. On the contrary, Rod (1956) implied that the overall displace- ment within the Caribbean area of more than 100 km (62 mi) was not unreasonable, based on an analysis of the supposed strike-slip fault system along northern Venezuela. In further support of strike-slip movement, Alberding (1957), applying the principle of wrench-fault tectonics of Moody and Hill ( 1956) to northern South America, concluded that during the Cre-

1732

B. G. Bassinger, R. N. Harbison and L. Austin Weeks

MILUGAIS J -1-50

-1-100

I PB

- -50

- -50

-1-100

"BASEMENT" HORIZONTAL SCALE VARIABLE

Fig. 2. Residual magnetic field intensity (regional field removed by inspection), free-air gravity anomaly, and seismic reflection profiles. Vertical scale of seismic records is two-way time. Position numbers are hours. CS, Central syncline; ER, East ridge; ETS, East Tobago syncline; NTA, North Tobago anticline; PB, Pilar block; TT, Tobago Trough; and WR, West ridge.

taceous the Araya and Paria Peninsulas of Venezuela and the Northern Range of Trinidad formerly were 475 km (295 n. mi) west. A study of the pre-Tertiary rocks along one of the several prominent east-west-trending faults across northern Venezuela suggested no more than 10-15 km (6-9 n. mi) of strike-slip movement along the El Pilar fault (Metz, 1964). However, recent field mapping in the Northern Range of Trinidad (Potter, 1968) re- vealed only vertical displacement of up to 1.8 km (6,000 ft). In addition, seismic-reflection profiling and sediment coring indicated that the tectonics of the margins of the Caribbean ba-

sins show vertical rather than horizontal dis- placements (Ewing et ah, 1967).

Results and Discussion

The geophysical data suggest a division of the study area into three prominent structural features: (1) Pilar block, (2) Barbados anticli- norium, and (3) Tobago Trough. Pilar block is defined as the tectonically positive element bounded on the north and south by faults of major displacement. The block consists of the Araya and Paria Peninsulas of Venezuela and their continuation through the Northern Range of Trinidad. Barbados anticlinorium is the

Marine Geophysica! Study Northeast of Trinidad-Tobago

1733

r GAMMAS

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Fig. 2 (Continued)

complex of structures lying between the To- bago Trough and the Atlantic basin, and is di- vided into two separate tectonically positive structures separated by a medial syncline (Weeks et ah, 1969). These structures are: West ridge, Central syncline, and East ridge. North Tobago anticline and East Tobago syn- cline are two subsidiary structures west of the West ridge. Tobago Trough is the tectonically negative element separating the Lesser Antilles from the Barbados anticlinorium (Fig. 1).

Pilar Block

A correlation of earthquake epicenter loca- tions with structural units in the Paria Penin- sula region of Venezuela seems to indicate two sequences of tectonic events (Sykes and Ewing, 1965). According to that study, one series of events north and another south of 10°36'N may suggest movements along two major fault

zones. Although the epicenter locations are confined to a small area of the Paria Peninsula, our data farther east support their conclusion. Within the study area, the Pilar block is a dis- tinct structural unit, bounded on the north and south by prominent fault zones which appar- ently continue eastward to about 58°50'W (Fig. 1).

The traverse through the Dragon's Mouth (profile A- A', Figs. 2, 3) shows the Pilar block as a partly buried horst flanked by sedimentary strata. Presumably, this basement block is the lateral continuation of pre-Late Jurassic to Late Cretaceous metamorphic rocks of the Northern Range and Paria Peninsula mapped by Kugler (1961). Small down-to-the-north growth faults are present near the north end of the profile. The southern half of the profile shows a shal- low zone of relatively transparent sediments ap- parently transgressing the block from the south.

B. G. Bassinger, R. N. Harbison and L. Austin Weeks

SEC |8 19

PILAR BLOCK

Fig. 3.-

-North-south seismic reflection profile through Dragon's Mouth (profile A-A', Fig. 1) showing Pilar block adjacent to thick sedimentary sequences. Vertical scale is two-way time.

In the same area the free-air gravity gradient of 90 mgals is consistent with a thick accumula- tion of sediments in the Gulf of Paria on the south, but is also in part a reflection of the re- gional gradient. This regional gravity trend is the northern flank of an arcuate gravity low paralleling the Lesser Antilles (Bush and Bush, 1969), which is coincident with a negative Bouguer anomaly along the Barbados Ridge. This negative anomaly is apparently the result of intermediate velocity material that lies in downwarped high-velocity layers (Officer et al., 1959). In addition to the regional field, local anomalies of a few milligals are related to the block and to the near-surface arched structure observed in the SRP records near location 19.5. The suggestion of major tectonic activity is confirmed further by a change from a high-am- plitude, long-period to a low-amplitude, short period magnetic trace near the northern margin of the block. These short-period variations of up to 10 y may be caused by lithologic changes in the observed part of the Pilar block similar to those found in exposed rocks of the Paria Pen- insula and Northern Range.

The SRP record off the north coast of Trini- dad suggests a basement complex that is most probably an eastward continuation of the Pilar block (profile B-B', Fig. 2). North of the base- ment block, a zone of normal down-to-the-north

growth faulting correlates well with similar fea- tures on the west in profile A-A'. These occur- rences, which coincide with an increase in grav- ity also suggest a rise in the basement complex.

A seismic refraction traverse (line 24 of Ew- ing et al., 1957) crosses the northern ends of profile A-A' and B-B'. It shows relatively flat- lying sedimentary sequences with velocities of 1.66-1.93 km/sec (5,500-6,300 ft/sec) un- derlain by north-dipping velocity sequences of 2.75-4.80 km/sec (9,000-15,800 ft/sec). A comparison of these velocities with those re- corded in south and central Trinidad suggests that the uppermost sedimentary layers above the 2.75 km/ sec (9,000 ft/ sec) layer are post- Pliocene material (Higgins, 1959). The upper half of the 1.93 km/sec (6,300 ft/sec) sedi- ment sequence, showing evidence of down-to- the-north normal growth faults, can be traced close to the surface near the southern end of the profile adjacent to a basement complex (Profile B-B', Fig. 2).

Near the north end of profile A-A' (Fig. 2), Ewing et al. (1957) obtained a depth of 3.1 km (10,200 ft) to the top of the 4.8 km/ sec (15,800 ft/ sec) layer and related it to the north flank of the Northern Range. In support of that conclusion, Higgins (1959), correlating these velocities with those recorded in Trinidad, suggested that material with the same velocity

Marine Geophysical Study Northeast of Trinidad-Tobago

1735

may be related to the Northern Range meta- morphic rocks. If the top of the 4.8 km/ sec (15,800 ft/sec) interface is projected to the northern margin of the exposed Pilar block and if one assumes that the exposed block in the Dragon's Mouth is comparable material, a min- imum vertical displacement of 2.3 km (7,800 ft) is indicated along the north boundary fault system of Trinidad. This displacement is com- parable with, but somewhat greater than, the 1.8 km (6,000 ft) uplift reported by Potter (1968) for the Northern Range along the El Pilar fault system.

The impression conveyed by the structural cross sections through Trinidad (Kugler, 1961) is that the Pilar block becomes less pronounced toward the east. Our geophysical information is in agreement with that conclusion. From loca- t;on 20 (profile C-C, Fig. 2) off the northern coast of Trinidad to midway between the off- shore projection of the Pilar block, the SRP rec- ords show well-stratified, shallow sedimentary strata of up to 1.0-sec penetration in an area where, according to Koldewijn (1958), only a few centimeters of recent sediments have been found above older deposits. These relatively undeformed sediments are a strong indication of a lack of postdepositional tectonic activity in the vicinity of the northern boundary fault sys- tem of Trinidad.

The stratigraphic section south of the pro- jected El Pilar fault system contrasts markedly with that on the north (profile C-C, Fig. 2). Off the east coast of Trinidad, the shallow sedi- mentary strata are faulted, folded, and broadly arched, and thus resemble the structures of southern Trinidad shown by Kugler (1961).

The basement complex centered around loca- tion 3.7 can be traced across the shelf through shoals and banks to Radix Point. These occur- rences seem to indicate that the northeast-south- west-striking tectonic belts of Trinidad continue across the continental shelf a conclusion in general agreement with Koldewijn's (1958) structural trend map.

Gravity observations in the area of the off- shore projection of the Pilar block (profile C- C, Fig. 2) show no large density contrast at any depth within the crust as found in the Dragon's Mouth profile (profile A-A', Fig. 2). However, the only positive suggestion of the continuation of an uplifted feature across the shelf is revealed by a minor gravity anomaly of less than 8 mgal between locations 0.2 and 1.5. This anomaly coincides with low-amplitude magnetic signatures of approximately 10 y, which may be the result of faulting with subse- quent intrusion or local susceptibility contrasts.

Off the east coast of Trinidad, the Pilar block is easily identified in the vicinity of loca- tion 23.8 (profile D-D', Figs. 2, 4) as an ex- posed basement complex showing evidence of planation. On six successive crossings to 58°50' W, the El Pilar fault is characterized by a base- ment-sediment contact, but the northern boundary fault is less obvious (profile E-E', Figs. 2, 5, 6). These observations confirm the interpretation of Collette et al. (1969), that the block apparently acts as a barrier preventing the northward flow of sediments.

Barbados Anticlinorium

The East ridge could not be traced west of 60 °W, just off the Trinidad shelf. In that area,

4. ^tfSju-v

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PILAR BLOCK

Fig. 4. Part of north-south seismic reflection profile D-D' (Fig. 1) showing Pilar block near shelf edge.

Vertical scale is two-way time.

1736

B. G. Bassinger, R. N. Harbison and L. Austin Weeks SEC

2 3

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PILAR BLOCK

Fig. 5.-

-Part of north-south seismic reflection profile E-E' (Fig. 1) showing Pilar block adjacent to level sedimentary sequences of different depths. Vertical scale is two-way time.

the ridge apparently either dies out or plunges below the flat-lying sediments of the Central syncline (Fig. 1). Its northward projection east of 59° 10' is based primarily on bathymetry (Fig. 1 of Weeks et al, 1971). Near the Pilar block, much of the trend is characterized by three basement highs, with intervening strata whose sedimentary layers seem to exhibit a pro- gressive increase in dip with increasing depth (profile E-E', Figs. 2, 5). This deformation and the apparent termination of the East ridge be- low the Central syncline imply that the process which formed the ridge has been primarily ver- tical and persistently active during the period of sedimentation.

The Central syncline separates the West and East ridges and extends from near the Pilar block between Trinidad and Tobago to the northeast limit of the study area. Within the shelf area north of Trinidad, the syncline occu- pies a topographic depression with somewhat conformable sedimentary reflectors (profile C- C, Fig. 2), probably reflecting a continuation of a linear bathymetric low southeast of To- bago (Fig. 1 of Weeks et al., 1971). Along the line of track, the feature is bounded on the southeast by a fault that extends to the surface. There, the gravity anomaly is produced in part by an accumulation of lower density sediments

and in part by a density differential resulting from faulting at depth. Off the shelf edge the syncline is defined more clearly by relatively undeformed, gently downfolded reflectors which continue under a layered sequence (pro- file D-D', Figs. 2, 7).

Off the continental shelf the prominent flank- ing unconformities of the Central syncline gen- erally die out toward the northeast (Fig. 1). The older folded sediments of the West and East ridges plunge under the syncline beneath a younger unconformable wedge of well-strati- fied, almost horizontal sediments (profile E-E', Fig. 2).

The West ridge is a continuous element of the Barbados anticlinorium that extends from north of Barbados, across the study area through Tobago, and well into the shelf area off Trinidad. First indications of this feature are thinning sedimentary sequences below the ap- parently flat shelf at the beginning of profile C- C (Fig. 2). However, the rise is more apparent on seismic reflection profiles about 10°55'N (Lowrie and Escowitz, 1969) . In this area of the shelf, an arched sedimentary zone is marked by a change of sedimentary environment with dis- tinctive patterns of reflectors. The characteristic pattern of reflectors, presumably post-Pliocene material, occupies the near-surface area be-

Marine Geophysical Study Northeast of Trinidad-Tobago

1737

tween the Dragon's Mouth and the West ridge axis. The suggestion of an arched zone is con- firmed further by an increase in gravity and a small isolated magnetic anomaly that may re- flect a shallowing of the basement surface.

Near the shelf edge the West ridge is ex- pressed as an exposed basement complex (pro- file D-D', Figs. 2, 7). Northeastward the ridge is marked by an irregular surface that widens rapidly and plunges well below thick sedimen- tary sequences (profile E-E', Fig. 2). Although the reflected basement surface has different acoustic characteristics across the traverse, near location 13 it corresponds in depth to the 3.97 km/sec (13,000 ft/ sec) material reported by Ewing et al. (1957). On the margins of the ridge, the basement surface and its sediment overburden plunge well below the seismic pene- tration limit in both the Central syncline and Tobago Trough.

North Tobago anticline and East Tobago syncline are separate tectonic elements within the Barbados anticlinorium. In the Tobago area the North Tobago anticline shows well-defined reflectors cut by small, normal down-to-the-

south faults, principally south of the crest of the anticline (profile D-D', Fig. 2). These strata belong to the pre-unconformity suite of rocks, for they plunge under the younger beds of the Tobago Trough (profile E-E', Fig. 2). Over this general area, the magnitude of the gravity anomaly (in part reflecting sea-floor topography) compared to the surrounding area and the disruption of the regional magnetic field suggest deeper structural implications as a result of the development of the structures near Tobago. A definite correlation exists between the magnetic anomalies in this area and the magnetic anomaly zone traced across the shelf by Lattimore et al. (1971). Even though the amplitudes of the anomalies are considerably less than those identified farther southwest, the overall disruption of the magnetic field is com- parable in extent.

The close double-anomaly (two source) pat- tern observed on profile B-B' (Fig. 2) is help- ful in making a reasonable correlation within the study area (Fig. 1). These anomalies ap- pear to be part of a large arcuate magnetic anomaly zone, occupying an area approxi-

PILAR BLOCK

Fig. 6. North-south seismic reflection profile F-F (Fig. 1) showing Pilar block (on south) adjacent to thick sedimentary sequence near 59°W. Vertical scale is two-way time.

1738

B. G. Bassinger, R. N. Harbison and L. Austin Weeks

lO

•.-**

\ij •!

X

_J

I

.S..1

o

O <u

^>

c

S o

> I/)

o

J3 C

^ o

■S 3

mately 60 km (35 n. mi) wide that extends across the shelf somewhat parallel with the is- land arc system. They continue across the shelf in a northeast direction, disrupting the mag- netic field as multiple source anomalies off To- bago (profile D-D', Fig. 2) and terminating be- fore profile E-E' (Fig. 2). On the south the anomalies appear to terminate abruptly at the Pilar block (profile A-A', Fig. 2). These prom- inent features can be attributed only to deep- seated structures related to the island arc sys- tem.

Peters' method (Peters, 1949) of depth de- termination applied to the magnetic anomaly observed near 11°17'N and 61°19'W reveals a depth to source of approximately 3.7 km (12,000 ft). The depth reliability of such deter- minations, however, depends on the absence of disturbing effects from other magnetic bodies, and assumes that polarization of the body is uniform and essentially vertical. In this general area, seismic refraction data indicate a depth of 3.2 km (10,500 ft) to the top of the 4.85 km/ sec (15,900 ft/sec) layer, which Ewing et al. ( 1957) considered to be the north flank of the Northern Range metamorphic rocks. Conse- quently, the material causing the magnetic anomaly apparently would be emplaced near the top of the material having comparable ve- locity to that of the metamorphic rocks of the Northern Range.

Off the northeast coast of Tobago between 11°12'N and 11°23'N to 60°25'W, a distinc- tive magnetic pattern of short-period, high-am- plitude anomalies is in sharp contrast to the high-amplitude, long-period anomalies of the surrounding area (Fig. 1). These high-fre- quency observations are attributed to shallow variations in the magnetic susceptibility, proba- bly caused by near-surface intrusive activity. This zone is considered to be related to a tec- tonic unit of high magnetic susceptibility that is useful in delineating the near-surface eastern limit of the volcanic rocks similar to those mapped on Tobago by Maxwell (1948).

Summary and Conclusions

The Pilar block is a distinct structural unit expressed as a relatively narrow horst, bounded both north and south by prominent fault zones. From the Dragon's Mouth to about 61°12'W, the block appears to be flanked on the north by moderately deformed sediments of presumably post-Pliocene age. In this general area, refrac- tion data indicate an overall displacement of at least 2.3 km (7,800 ft), which is comparable to

Marine Geophysical Study Northeast of Trinidad-Tobago

1739

an earlier estimate of 1.8 km (6,000 ft) of uplift along the El Pilar fault. The block is a rigid unit traceable from the Araya Peninsula of Venezuela to 59°50'W however, it is not immune to extensional collapse features, such as the Dragon's Mouth. Outside the shelf edge the El Pilar fault system is characterized by its sediment-basement contact. In this area the block apparently acts as a barrier preventing the northward flow of sediments. As a result, sedimentary accumulations equivalent to more than 2.0 sec of penetration are found south of the fault near 59°W. Prominent structures on the north and south either die out or change trend to subparallel with the Pilar block. South of the block, structures apparently continue across the various shoals and banks of the shelf and terminate at the block. In this area, struc- tures revealed by the SRP records near the shelf edge are similar to those in structural cross sections of eastern Trinidad.

Barbados anticlinorium is folded and faulted apparently as a tectonic unit. The observed basement complex plunges to depths beneath the sediments of the shelf beyond the limit of penetration of the SRP equipment. Much of the trend of the anticlinorium within the study area is occupied by magnetic anomalies of var- ied characteristics. A zone approximately 60 km (35 n, mi) wide, approximately parallel with the principal arcuate trend of the island arc system, contains high-amplitude, long-pe- riod magnetic anomalies. This zone continues across the shelf and through Tobago but does not extend east of about 60°W. Depth compu- tations on one of these anomalies reveals a depth to source of about 3.7 km (12,000 ft), implying that the source is emplaced near the surface of the 4.85 km/sec (15,900 ft/ sec) velocity material, which is believed to be com- parable with the Northern Range metamorphic rocks. If these are in fact related, a sedimentary accumulation of 3.2 km (10,500 ft) as re- vealed by refraction data is expected in the area off northern Trinidad. In sharp contrast to these prominent magnetic anomalies, but per- haps originating from the same source, high- amplitude, short-period anomalies indicative of a near-surface source occupy an area 1 1 km (6 n, mi) northeast of Tobago. These anomalies are apparently related to the igneous rocks ex- posed in Tobago,

Off the shelf the Barbados anticlinorium is characterized by a basement complex of 3.97 km/ sec (13,000 ft/sec) velocity rraterial with a sedimentary overburden. These older

sediments plunge under the flat-lying deposits of the Tobago Trough and Central syncline. The younger, relatively undeformed, sediments to 1.0-sec penetration have not been affected by any significant tectonic activity since their de- position.

If the Caribbean plate and the adjacent South American continent are contrasting crus- tal blocks with great horizontal movements along major boundary faults, a condition re- quired by "new global tectonics," some evi- dence of transform faulting should be observed near the shelf edge, along the north boundary fault zone of Trinidad, or along the El Pilar fault zone. The following points lend little sup- port to extensive translation of such plates.

1. The observation that the deeper trends of the Barbados anticlinorium continue well into the shelf area implies that there is no major translation near the shelf edge. This conclusion is supported also by the continuation of the deeper structural trends of the volcanic island arc across the shelf and through Los Testigos Islands.

2. The north boundary fault zone of Trini- dad apparently terminates or plunges under at least 1.0 sec penetration of relatively unde- formed sedimentary strata in an area where the recent depositional rate is low. Consequently, the north-bounding fault system shows no evi- dence of relatively recent movement.

3. The lack of an obvious gouge zone along the El Pilar fault system, as might be expected in wrench faulting, and the absence of a mea- surable offset in the continental slope near the continuation of the fault system do not support extensive translation in comparatively recent time.

References Cited

Alberding, H., 1957, Application of principles of wrench-fault tectonics of Moody and Hill to north- ern South America: Geol. Soc. America Bull., v. 68, p. 785-790.

Bush, S. A., and P. A. Bush, 1969, Isostatic gravity map of the eastern Caribbean region: Gulf Coast Assoc. Geol. Socs. Trans., v. 19, p. 281-285.

Collette B. J., J. I. Ewing, R. A. Lagaay, and M. Tru- chan, 1969, Sediment distribution in the oceans the Atlantic between 10° and 19°N: Marine Geology, v. 7, p. 279-347.

Eardley, A. J., 1954, Tectonic relations of North and South America: Am. Assoc. Petroleum Geologists Bull., v. 38, no. 5, p. 707-773.

Edgar, N. T., 1968, Seismic refraction and reflection in the Caribbean Sea: Ph.D. dissert., Columbia Univ., 163 p.

Ewing, J. I , C. B. Officer, H. R. Johnson, and R. S. Edwards, 1957, Geophysical investigations in the eastern Caribbean Trinidad shelf, Tobago Trough,

1740

B. G. Bassinger, R. N. Harbison and L. Austin Weeks

Barbados ridge, Atlantic Ocean: Geol. Soc. America Bull., v. 68, p. 897-912.

M. Talwani, M. Ewing, and T. Edgar, 1967,

Sediments of the Caribbean: Internat. Conf. Tropi- cal Oceanography Proc, Miami Univ., 1965, p. 88- 102.

Hess, H. H., 1938, Gravity anomalies and island arc structure with particular reference to the West In- dies: Am. Philos. Soc. Proc, v. 79, p. 71-96.

Higgins, G. E., 1959, Seismic velocity data from Trini- dad, B. W. I., and comparison with the Caribbean area: Geophysics, v. 24, p. 580-597.

Koldewijn, B. W., 1958, Sediments of the Paria-Trini- dad shelf, v. 3 of Reports of the Orinoco Shelf expe- dition: The Hague, Mouton and Co., 109 p.

Kugler, H. K., 1961, Geological map of Trinidad and geological sections through Trinidad: pub. for Petro- leum Assoc. Trinidad; Zurich, Orell Fussli, and Lon- don, E. Strand.

Lattimore, R. K., L. A. Weeks, and L. W. Mordock, 1971, Marine geophysical reconnaissance of con- tinental margin north of Paria Peninsula, Venezuela: Am. Assoc. Petroleum Geologists Bull., v. 55, no. 10, p. 1719-1729.

Lowrie, A., and E. Escowitz, 1969, Global ocean floor analysis and research data series, v. 1: U. S. Naval Oceanog. Office, p. 971.

Maxwell, J. C, 1948, Geology of Tobago, B. W. I.: Geol. Soc. America Bull., v. 59, p. 801-854.

Metz, H. L., 1964, Geology of the El Pilar fault zone, state of Sucre, Venezuela: Ph.D. thesis, Princeton Univ., 102 p. .

Moody, J. D., and M. J. Hill, 1956, Wrench-fault tec- tonics: Geol. Soc. America Bull., v. 67, p. 1207- 1246.

Officer, C. B., J. I. Ewing, J. F. Hennion, D. G. Hark- rider, and D. E. Miller, 1959, Geophysical investi-

gations in the eastern Caribbean: summary of 1955 and 1956 cruises, in L. H. Ahrens et al., eds., Physics and chemistry of the earth, v. 3 : New York, Perga- mon Press, p. 17-109.

Peters, L. J., 1949, The direct approach to magnetic interpretation and its practical applications: Geo- physics, v. 14, p. 290-320.

Potter, H. C, 1968, Faulting in the Northern Range of Trinidad (abs) : 23d Internat. Geol. Cong. Rept, Prague, p. 95.

Rod, E, 1956, Strike-slip faults of northern Venezuela: Am. Assoc. Petroleum Geologists Bull., v. 40, no. 3, p. 457-476.

Schuchert, C, 1935 (1968 Reprint), Historical geology of the Antillean-Caribbean region: New York and London, Hafner Pub. Co., 811 p.

Suter, H. H., 1960, The general and economic geology of Trinidad, B.W.I. : London, Her Majesty's Statio- nery Office, 145 p.

Sykes, L. R., and M. Ewing, 1965, The seismicity of the Caribbean region: Jour. Geophys. Research, v. 70, p. 5065-5074.

van Andel, Tj. H., 1967, The Orinoco delta: Jour. Sed. Petrology, v. 37, no. 2, p. 297-310.

and P. L. Sachs, 1964, Sedimentation in the

Gulf of Paria during the Holocene transgressions a subsurface acoustic reflection study: Jour. Marine Research, v. 22, p. 30-50.

Weeks, L. A., R. K. Lattimore, R. N. Harbison, B. G. Bassinger, and G. F. Merrill, 1969, Structural rela- tionships between Lesser Antilles, Venezuela, and Trinidad-Tobago (abs.): Gulf Coast Assoc. Geol. Socs. Trans., v. 19, p. 321.

and 1971, Struc- tural relations among Lesser Antilles, Venezuela, and Trinidad-Tobago: Am. Assoc. Petroleum Geologists Bull., v. 55, no. 10, p. 1741-1752.

44

Reprinted from Marine Geology 11, 201-207

RAPID AND RELIABLE TECHNIQUE FOR DETERMINING UNIT WEIGHT AND POROSITY OF DEEP-SEA SEDIMENTS

RICHARD H. BENNETT and DOUGLAS N. LAMBERT

National Oceanic and Atmospheric Administration, Atlantic Oceanographic and Meteorological Laboratories, Marine Geology and Geophysics Laboratory, Miami, Fla. (U.S.A.)

(Received March 10, 1971)

ABSTRACT

Bennett, R. H. and Lambert, D. N., 1971. Rapid and reliable technique for determining unit weight and porosity of deep-sea sediments. Marine Geo/., 11: 201-207.

A rapid and reliable technique is explained for determining unit weight and porosity of deep-sea sediment from water content and average grain density measurements. Comparisons are made between this method and the standard tube method (volumetric), with 77 samples. The correlation coefficient is found to be 0.994 with a standard deviation between the methods of ± 0.01 g/cm3. The two techniques used to determine porosity are found to have a correlation coefficient of 0.998 with a standard deviation of 0.42%.

A nomographic chart is shown which permits rapid determination of unit weight using water content and average grain density.

INTRODUCTION

Unit weight of submarine sediments, also referred to as wet bulk density or saturated unit weight, is a function of the grain specific gravity and water content. By definition, unit weight is the weight per unit of volume regardless of the degree of saturation (A.S.T.M., 1967). However, submarine sediments, especially deep-sea sediments, are usually totally saturated.

A common technique for measuring unit weight is by inserting a tube of known volume into a sediment mass, such as a core, extracting the tube and sediment and determining the sediment weight. This gives a measure of the mass in grams per unit of volume. Difficulty in eliminating small voids between the cylinder wall and the sample as well as the influence of gases which may be present in the interstitial water due to the change from high hydrostatic pressure to at- mospheric pressure could affect the unit weight as measured in the laboratory. In an undisturbed sediment sample the relative proportions of water to solids are not destroyed and at 100% saturation, unit weight is at a maximum. Bennett et al. (1970) consider + 1 % of the observed value to be a reasonable estimate of the reproducibility of the tube method.

Porosity (/?), defined as the ratio of the volume of the voids to the total volume of the sediment mass, is usually computed from unit weight, average grain

Marine Geo/., 11(1971) 201-207

202 R. H. BENNETT AND D. N. LAMBERT

density, water content and an assumed interstitial water density. It is sometimes determined from the void ratio by the relationship n = e/(l + e ). Void ratio (e) is defined as the ratio of the volume of the voids to the volume of the solids.

The purpose of this study is to describe a rapid and reliable technique for determining unit weight and porosity of deep-sea sediment with an evaluation of the method using various sediment types. Carbonate content of the sediments ranged from less than 10% to greater than 98%, and textures ranged from less than 1 % to greater than 66 % sand-size particles.

TECHNIQUES AND BASIC PRINCIPLES

An advantage of the technique employed here for determining unit weight and porosity is that raw data from water content and grain density measurements are used. These data are frequently studied by the marine geologist and ocean engineer concerned with mass physical properties of submarine sediments and are usually numerous and readily available from laboratory reports.

Water content measurements are determined from approximately 10-20 g samples of sediment taken from the center of a core. The sample is immediately weighed and dried for about 24 h at 1 10°C and then reweighed to determine water loss. Average grain density is usually found by volumetric displacement of distilled water by the solids in a calibrated flask (Lambe, 1951). From these three measure- ments, weight of dry solids, weight of water driven off during drying, and the average grain density, the unit weight (y) can be easily determined by the following relationships:

W WD

y = ^ = ^ (1)

7 , w W, + WWD% K '

Dg + W"

where Wx = Wv + fVd; IVW = weight of the water = approximately the volume of water; WA = weight of dry solids including salts; Dg average grain density.

The total weight (Wt) of the sample taken for water content determination is equal to the weight of the water lost during oven drying (Ww) plus the weight of the dry solids (Wd). For practical purposes Wv is equivalent to the volume of water in the cgs system. The weight of the solids divided by the average grain density (WJDg) is the volume of the dry solids. The weight of the dry solids con- tains the weight of the salt. However, this increase in the volume of the solids, due to the presence of salts, closely approximates the slight deficit in the volume of the water (W^) owing to the dissolved salts in the interstitial water. Therefore, by definition, the unit weight of the sample is equal to the total weight divided by the total volume. Similar expressions may be equated with eq.l in text books on soil mechanics such as Terzaghi and Peck (1967), Scott (1963) and Wu (1966) and

Marine Geol., 11(1971) 201-207

UNIT WEIGHT AND POROSITY OF DEEP-SEA SEDIMENTS 203

are usually intended to show the relationships among density, porosity, and void ratio for a given sediment mass.

Porosity (n), expressed in percent, is the ratio of the volume of the voids to the total volume of the sediment mass and can be determined by the relationship:

V + V n = w + "ss x 100 (2)

-^ + W D, w

Vs% is the volume of the salts in solution. Again, Vv is equal to the volume of the water and approximately equal to the weight of the water in grams. If V%& is neglected or considered negligible the equation then becomes:

W Y- x 100 (3)

£ + *

Vss is very close to 1.2% of Vw for concentrations of dissolved salts of 35%0.

RELIABILITY

As a measure of the reliability of the above technique expressed by eq.l, 77 unit weight measurements were determined using this method and compared with unit weight determinations using the tube method. In addition, porosity was determined using eq.3 from the same raw data used to obtain unit weight. These values were compared with porosities calculated from unit weight measurements determined by the tube method, average grain density and water content values with no corrections for salt content. Correlation coefficients were determined for unit weight and porosity. A linear correlation coefficient of +0.994 was found between the two unit weight techniques with 67% of all measured values falling within +0.01 g/cm3 of each other. A linear correlation coefficient of +0.998 was found between the two porosity methods with 67% of all measured values falling within +0.42% of each other. The significance of these data shows that for all practical purposes, the correlation between the techniques is nearly perfect and that either method for determining unit weight and porosity is as good as the other.

RELATIONSHIPS

The effect of large differences in drying temperatures has been found to be not as critical as might be expected. Using eq.l and data from Lambe (1951), differences in drying temperatures from 90 °C to 190°C increase the unit weight measurement by only 0.002-0.004 g/cm3. Porosity values determined by eq.3 however, show differences ranging between 1 % and 3% when drying temperature varies from 90 °C to 190°C. Usually consistent techniques and control of tem-

Marine Geo!., 11(1971) 201-207

204 K. H. BENNETT AND D. N. LAMBERT

perature within reasonable limits are well within the means of most soils labo- ratories.

Examination of eq.l reveals that large changes in average grain density are necessary to appreciably affect the unit weight measurement. Clearly, the higher the water content the less average grain density variation influences those deter- minations. For example, with a water content of 50% an increase in average grain density from 2.75 to 2.80 increases the unit weight from 1.736 to 1.750. However, at a water content of 100 % a change in the grain density of 0.05 changes the unit weight by only 0.007 g/cm3. The other parameters Wt, Ww and Wd depend upon the accuracy of the balance which is usually well within the reproducibility of the technique described here.

Due to the above relationships, difficulty in determining unit weight and porosity of relatively clean sands by the proposed method might be encountered because such sediments are usually characterized by low water contents. Obtaining a true water content for this sediment type may be difficult. However, accurate unit weight and porosity values of a relatively clean sand are also difficult to obtain with the tube method because of possible loss of pore water in inserting the tube into the sediment and its subsequent handling.

DISCUSSION

Several advantages of the technique expressed in eq.l for determining unit weight are apparent. If gas is present it does not affect the measurement, and values of unit weight for 100% saturation at a given water content are obtained. This is considered by the authors to be a closer approximation of the actual unit weight, in situ, than values obtained by the tube method (volumetric), especially for sediment that includes gas. In addition, unit weight and porosity can be deter- mined for relatively thin stratified sediment with a minimum amount of material and for small irregularly shaped pieces of cohesive sediment not amenable to the tube method. Volumetric errors introduced in the tube method include error resulting in the incomplete filling of the tube with sediment and inaccurate meas- urement of the radius of the tube (any error in the radius is squared).

Unit weight and porosity, using the relationships of eq.l and 3, are deter- mined from measured parameters which consequently avoids the use of any as- sumed values such as the density of interstitial water and average grain density. However, relatively large variations in the average grain density are required to appreciably influence the unit weight determination by eq.l. Large changes in the drying temperatures such as 90°-190 C usually have small affects on the unit weight determination; however, porosity by eq.3 is more responsive to these temperature differences. Control of temperature is important when porosity values are critical and comparable to within 1 % of the observed values.

Fig. 1 was constructed using eq.l with a range of average grain density

Marine Geo/., 1 1 ( 1 97 1 ) 20 1 -207

UNIT WEIGHT AND POROSITY OF DEEP-SEA SEDIMENTS

205

f8

o

-a c

60

o E c

2

A1ISN3Q NlVilO 30V»3AV

Mviw Ceo/., 11(1971) 201-207

206 R- H. BENNETT AND D. N. LAMBERT

values from 1.70 to 3.19 and a number of selected weights of dry solids (Wd) and water (H/w). This nomographic chart shows average grain density plotted against unit weight with isolines for water content (used here as WJWA x 100) ranging between 25% and 600"^,. Clearly, the relationship is non-linear and the isolines (delineating water content) would ultimately converge at a value of 1.00. The relationships among porosity, unit weight, and grain density have been clearly depicted by Richards (1962). The advantage of this chart is that, given values of average grain density and water content, values for unit weight can be readily determined. The chart covers values for average grain density and water content most commonly found in submarine sediments (Keller and Bennett, 1970). Detailed tables for determining unit weight from water content and average grain density have been compiled and will form the bulk of a N.O.A.A. Technical Memorandum (Bennett and Lambert, in preparation).

In deep-sea sediments, unit weight as measured in the laboratory, may be lower than in situ unit weight owing to the increase in the density of interstitial water at high hydrostatic pressures. This effect has been shown by Hamilton (1969) to be significant, especially for deep-sea sediments with high porosities (75 %— 85 % ). At these porosities, such as in the deep Central Pacific (5,000 m), the increase in unit weight can be 0.02 g/cm3.

Sediments high in organic carbon content may significantly influence meas- urement of average grain density, therefore caution should be exercised when dealing with such materials.

acknowledgements

The authors express their sincere appreciation to Drs. George H. Keller, Edwin L. Hamilton, Peter A. Rona, Louis W. Butler and Adrian F. Richards for their critical review of the manuscript. Many thanks are due to Paul J. Grim and Alan Herman for their competent computer programming of the nomographic chart and statistical parameters. The helpful discussions with John W. van Lan- dingham are appreciated.

references

American Society for Testing Materials, 1967. 1967 Book of A.S.T.M. Standards, Part II.

A.S.T.M., Philadelphia, Pa., pp. 285-302. Bennett, R. H., Lambert, D. N. and Grim, P. J., in preparation. Tables for determining unit

weight of deep-sea sediments using water content and average grain density. Natl. Oceanic

Atmospheric Admin., Tech. Mem., ERL TM-AOML. Bennett, R. H., Keller, G. H. and Busby, R. F., 1970. Mass property variability in three closely

spaced deep-sea sediment cores. J. Sediment. Petrol., 40: 1038-1043. Hamilton, E. L., 1969. Sound velocity, elasticity, and related properties of marine sediments,

North Pacific III. Prediction of in situ properties. Naval Undersea Res., Develop. Center,

NUC TP: 145 pp.

Marine Geo/., 1 1(1971) 201-207

UNIT WEIGHT AND POROSITY OF DEEP-SEA SEDIMENTS 207

Keller, G. H. and Bennett, R. H., 1970. Variations in the mass physical properties of selected

submarine sediments. Marine Geol., 9: 215-223. Lambe, T. W., 1951. So/7 Testing for Engineers. Wiley, New York, N.Y., 165 pp. Richards, A. F., 1962. Investigations of deep-sea sediment cores, II. Mass physical properties.

U.S. Navy Hydrograph. Office, Tech. Rept., TR-106: 146 pp. Scott, R. F., 1963. Principles of Soil Mechanics. Addison-Wesley, Reading, Mass., 550 pp. Terzaghi, K. and Peck, R., 1967. Soil Mechanics in Engineering Practice. Wiley, New York,

N.Y., 2nd ed., 729 pp. Wu, T. H., 1966. Soil Mechanics. Allyn and Bacon, Boston, Mass., 431 pp.

Marine Geol., 11(1971) 201-207

45

U.S. DEPARTMENT OF COMMERCE

National Oceanic and Atmospheric Administration Environmental Research Laboratories

NOAA Technical Memorandum ERL AOML-13

TABLES FOR DETERMINING UNIT WEIGHT

OF DEEP-SEA SEDIMENTS FROM WATER CONTENT

AND AVERAGE GRAIN DENSITY MEASUREMENTS

Richard H. Bennett

Douglas N. Lambert

Paul J. Grim

Marine Geology and Geophysics Laboratory

Atlantic Oceanographic and Meteorological Laboratories Miami, Florida August 1971

TABLE OF CONTENTS

PAGE

1. INTRODUCTION 1

2. MEASUREMENTS AND PROCEDURES 2

3. TABULAR RESULTS 3

4. SUMMARY AND CONCLUSIONS 5

5. REFERENCES 5 FIGURE 7 TABLES 8-56

in

TABLES FOR DETERMINING UNIT WEIGHT OF DEEP-SEA SEDIMENTS FROM WATER CONTENT AND AVERAGE GRAIN DENSITY MEASUREMENTS

Richard H. Bennett, Douglas N. Lambert and Paul J. Grim

An expedient and reliable method is shown for determining unit weight of deep-sea sediment using water content and average grain density measure- ments. Tables form the bulk of this report with water contents ranging from 25 percent to 700 per- cent and average grain densities ranging from 1.70 to 3.10. A nomographic chart is included to supplement the tables .

1. INTRODUCTION Unit weight of submarine sediments, also referred to as mass unit weight, is a function of the grain specific grav- ity and water content. By definition, unit weight is the weight (solids plus water) per unit of total volume of a sediment mass, regardless of the degree of saturation (ASTM, 1967). Bennett and Lambert (in press) have presented a rapid and reliable technique, using the above relationships, to determine unit weight (y) for laboratory measured values of water content (Ww/W^ x 100, the weight of the water to the weight of the dried solids) and average grain density (DG) . This relationship is expressed as

W. W W DG

Y = t = t _ t

V W

d + v,

w d w

t d+W W + W DG

DG where total weight (W. ) of a sediment sample equals the

weight of water (W ) , approximately equal to the volume of

w

water, plus the weight of the dry solids (W^) including salts. The total volume is the dry solids (Wj/DG) plus the volume of the water.

2. MEASUREMENTS AND PROCEDURES As a measure of the reliability of the above technique, 77 unit weights were determined using this method and com- pared with analyses by the standard tube method (volumetric) (Richards, 1962). A linear correlation coefficient of + 0.99M- was found between the two unit weight techniques with 67 percent of all measured values falling within ± 0.01 g/cc of each other. These data show that for all practical pur- poses , correlation between the techniques is nearly perfect and that either method for determining unit weight is equally useable.

Several advantages of the technique expressed in the above equation are apparent. If gas is present it does not affect the measurement, and values of unit weight for 100 percent saturation at a given water content are obtained.

This is considered by the authors to be a closer approxima- tion of the actual in_ situ unit weight, of deep-sea sediment, than values obtained by the tube method (volumet- ric), especially for sediment that includes gas. In addition, unit weight can be determined for relatively thin stratified sediment with a minimum amount of material and for small irregularly shaped pieces of cohesive sediment not amenable to the tube method. Volumetric errors intro- duced in the tube method include error resulting in the incomplete filling of the tube with sediment and inaccurate measurement of the radius of the tube (any error in the radius is squared) .

3. TABULAR RESULTS The bulk of this report consists of tables for deter- mining unit weight using the given equation. These tables include the range of values for water content and average grain density commonly found in submarine sediments (Keller and Bennett, 19 70). The respective tables are established for water contents at one-percent intervals from 2 5 to 100 percent, five-percent intervals from 100 to 200 percent and at ten-percent intervals from 200 to 700 percent. Water content is given at the heading of each table, and the left- hand column (DG) shows the range of average grain densities (1.70 to 3.10). To find the unit weight of a particular

sediment sample, select the table which nearly approximates or equals the water content for that sample and then locate the grain density of the sample to the first decimal place in the lefthand column. Move across the row to the appro- priate column (numbered zero through nine at the top of each column) for the second decimal place of the average grain density. The number given in this column is the unit weight for that particular sample given to the third decimal place.

Also included in this report is a nomographic chart (fig. 1) constructed using the above equation with a range of average grain density values from 1.70 to 3.19 and a num- ber of selected weights of dry solids (W-,) and water (W ) . The chart shows average grain density plotted against unit weight with isolines for water content (used here as W /W, x 100) ranging between 25 and 600 percent. Clearly the relationship is non-linear and the isolines (delineating water content) would ultimately converge at a value of 1.00. The advantage of this chart is that, given values of average grain density and water content, reliable values for wet unit weight are readily determined. For more detailed values of unit weight the authors recommend the use of the included tables .

4. SUMMARY AND CONCLUSIONS Laboratory measurement of water content and average grain density is particularly useful for determining unit weight of deep-sea sediment especially for samples not amen- able to the tube (volumetric) method. Data show that for all practical purposes, correlation between techniques is nearly perfect. Use of the tables or nomographic chart is expedient and reliable.

5. REFERENCES

American Society for Testing Materials, 1967, 1967 Book of ASTM Standards, Part II. Philadelphia, Pa., p. 285-302

Bennett, Richard H. and Douglas N. Lambert, 19 71, Rapid and Reliable Technique for Determining Unit Weight and Porosity of Deep-Sea sediments, Vol. 11 (in press Marine Geology) .

Keller, G. H. and R. H. Bennett, 1970, Variations in the mass physical properties of selected submarine sedi- ments, Marine Geology, 9: p. 215-223.

Richards, A. F., 1962, Investigations of deep-sea sediment cores, II. Mass Physical Properties: Tech. Rept . , TR-10 6 U.S. Navy Hydrographic Office, Washington, D.C. 146 p.

3 O)

UISN3Q NIVaO 30V83AV

TABLE 1 Unit weight as a function of average grain density and water content

Unit Weights

WATER CONTENT 25 PERCENT

0G01 23456789

1.70

1.491

1.497

1.503

1.510

1.516

1.522

1.528

1.534

1.540

1.546

1.80

1.552

1.558

1.564

1.569

1.575

1.581

1.587

1.593

1.599

1.604

1.90

1.61C

1.616

1.62?

1.627

1.633

1.639

1.644

1.650

1.656

1.661

2.00

1.667

1.672

1.673

1.683

1.689

1.694

1.700

1.705

1.711

1.716

2.10

1.721

1.727

1.732

1.737

1.743

1.748

1.753

1.759

1.764

1.769

2.20

1.774

1.779

1.785

1.790

1.795

1.800

1.305

1.810

1.815

1.820

2.30

1.825

1.830

1.835

1.840

1. 845

1.850

1.855

1.860

1.865

1.870

2.40

1.875

1.880

1.885

1.390

1.894

1.899

1.904

1.909

1.914

1.918

2.50

1.923

1.928

1.933

1.937

1 .942

1.947

1.951

1.956

1.960

1.965

2.60

1.970

1.974

1.979

1.983

1.988

1.992

1.997

2.001

2.006

2.010

2.70

2.015

2.019

2.024

2.028

2.033

2.037

2.041

2.046

2.050

2.054

2.80

2.059

2.063

2.067

2.072

2.076

2.080

2.035

2.089

2.093

2.097

2.°0

2.101

2. 106

2.110

2.114

2.118

2.122

2.126

2.131

2.135

2.139

3.00

2. 143

2.147

2.151

2.155

2.159

2.163

2.167

2.171

2.175

2.179

3.10

2.183

2.187

2.191

2.195

2. 199

2.203

2.207

2.211

2.214

2.218

WATER CONTENT 26 PERCENT

DG 0 1 2 :

>-

(SI

1.70

1.485

1.491

1.498

1.504

1.510

1.515

1.521

1.527

1.533

1.539

1.80

1.545

1.551

1.557

1.562

1.563

1.574

1.580

1.585

1.591

1.597

Z

1.90

1.602

1.608

1.614

1.619

1.625

1.630

1.636

1.641

1.647

1.652

LU

Q

2.00

1.658

1.663

1.669

1.674

1.630

1.635

1.6 90

1.696

1.701

1.706

2.10

1.712

1.717

1.722

1.727

1.732

1.738

1.743

1.748

1.753

1.758

Z

2.20

1.763

1.768

1. 774

1.779

1.784

1.789

1.794

1.799

1.804

1.809

<

o

2.30

1.814

1.318

1.32 3

1.828

1.833

1.838

1.843

1.848

1.852

1.857

2.40

1.862

1.867

1.372

1.8 76

1.881

1.886

1.3 90

1.395

1.900

1.904

Ui

o

2.50

1.909

1.914

1.918

1.923

1.927

1.932

1.937

1.941

1 .946

1.950

2.60

1.955

1.959

1.964

1.963

1.972

1.977

1.981

1.986

1.990

1.994

<

2.70

1.999

2.003

2.007

2.012

2.016

2.020

2.025

2.029

2.033

2.037

ex m

2.80

2.042

2.046

2.050

2.054

2.058

2.063

2.067

2.071

2.075

2.079

>

2.90

2.08.3

2.087

2.0Q1

2.095

2. 100

2.104

2.108

2.112

2.116

2.120

<

3.00

2.124

2. 128

2. 132

2. 135

2. 139

2. 143

2.147

2.151

2.155

2.159

3.10

2.163

2.167

2.170

2.174

2. 178

2.182

2.186

2. 190

2.193

2.197

WATER CONTENT 27 PERCENT

DO 0 1 2

1.70

1.480

1.486

1.492

1.498

1.503

1.509

1.515

1.521

1.527

1.533

1.80

1.538

1.544

1.550

1.556

1.561

1.567

1.572

1.578

1.534

1.589

1.90

1.595

1.600

1.606

1.611

1.617

1.622

1.628

1.633

1.639

1.644

2.00

1.649

1.655

1.660

1.665

1.671

1.676

1.681

1.636

1.692

1.697

2.10

1.702

1.707

1.712

1.717

1.723

1.728

1.733

1.738

1.743

1.748

2.20

1.753

1.758

1.763

1.768

1.77*3

1.778

1.783

1.787

1.792

1.797

2.30

1.802

1.807

1.312

1.816

1.321

1.826

1.831

1.335

1.840

1.845

2.40

1.850

1.854

1.859

1.863

1.868

1.873

1.877

1.8«2

1.886

1.891

2.50

1.896

1.900

1.905

1.909

1.914

1.918

1.922

1.927

1.931

1.936

2.60

1.940

1.944

1.949

1.953

1.957

1.962

1.966

1.970

1.975

1.979

2.70

1.983

1.987

1.992

1.996

2.000

2.004

2.008

2.013

2.017

2.021

2.80

2.025

2.029

2.033

2.037

2.041

2.045

2.050

2.054

2.058

2.062

2.90

2.066

2.070

2.074

2.078

2.081

2.085

2.089

2.093

2.007

2.101

3.00

2.105

2.109

2.113

2.117

2.120

2.124

2.128

2.132

2.136

2.139

3. 10

2.143

2.147

2.151

2.154

2.158

2.162

2.166

2.169

2.173

2.177

WATER CONTENT

2* PERCENT

DG

1.70

1.474

1.480

1.486

1.492

1.498

1.503

1.509

1.515

1.521

1.526

1.80

1.532

1.538

1.543

1.549

1.554

1.560

1.565

1.571

1.577

1.582

1.90

1.587

1.593

1.598

1.604

1.609

1.614

1.620

1.625

1.630

1.636

2.00

1.641

1.646

1.652

1.657

1.662

1.667

1.672

1.677

1.683

1.688

2.10

1.693

1.698

1.703

1.708

1.713

1.718

1.723

1.728

1.733

1.738

2.20

1.743

1.747

1.752

1.757

1 .762

1.767

1.772

1.776

1.781

1.786

2.30

1.791

1.795

1.800

1.805

1.810

1.814

1.819

1.824

1.828

1.833

2.40

1.837

1.842

1.846

1.351

1.856

1.860

1.865

1.869

1.873

1.878

2.50

1.882

1.887

l.d91

1.396

1.900

1.904

1.909

1.913

1.917

1.922

2.60

1.926

1.930

1.934

1.939

1.943

1.947

1.951

1.956

1.960

1.964

2.70

1.963

1.972

1.976

1.981

1.985

1.989

1.993

1.997

2.001

2.005

2.80

2.009

2.013

2.017

2.021

2.025

2.029

2.033

2.037

2.041

2.045

2.Q0

2.049

2.052

2.056

2.060

2.064

2.068

2.072

2.076

2.079

2.083

3.00

2.087

2.091

2.094

2.098

2.102

2.106

2.109

2.113

2.117

2.121

3.10

2.124

2. 123

2.132

2.135

2.139

2.142

2.146

2. 150

2.153

2.157

WATER CONTENT

29 PERCENT

OG

1.70

1.469

1.475

1.480

1.486

1.492

1.498

1.503

1.509

1.514

1.520

1.80

1.526

1.531

1.537

1.542

1.548

1.553

1.559

1.564

1.570

1.575

1.90

1.580

1.586

1.591

1.596

1.602

1 .607

1.612

1.617

1.623

1.623

2.00

1.633

1.638

1.643

1.648

1.653

1.659

1.664

1.669

1.674

1.679

2.10

1.684

1.689

1.694

1.699

1.703

1.708

1.713

1.718

1.723

1.728

2.20

1.733

1.737

1.742

1.747

1.752

1.756

1.761

1.766

1.771

1 .775

2.30

1.780

1.734

1.789

1.794

1. 798

1.803

1.807

1.812

1.816

1.821

2.40

1.325

1.830

1.834

1.839

1.843

1.848

1.852

1.856

1.861

1.865

2.50

1.8 70

1.874

1.378

1.383

1.887

1.391

1.895

1.900

1.904

1 .908

2.60

l.°12

1.916

1.921

1.925

1.929

1.933

1.937

1.941

1.945

1.949

2.70

1.953

1.957

1.962

l.Q66

1.970

1.974

1.978

1.932

1.985

1.989

2.80

1.993

1.997

2.001

2.005

2.009

2.013

2.017

2.021

2.024

2.028

2.90

2.032

2.036

2.040

2.043

2.047

2.051

2.055

2.058

2.062

2.066

3.00

2.070

2.073

2.077

2.0R1

2.034

2.088

2.091

2.095

2.099

2.102

3.10

2.106

2.109

2.U3

2.1 17

2. 120

2.124

2.127

2. 131

2.134

2.138

WATER CONTENT

30 PERCENT

DG

1.70

1.464

1.469

1.475

1.481

1.436

1.492

1.497

1.503

1.508

1.514

1.30

1.519

1.525

1.530

1.536

1.541

1.547

1.552

1.557

1.563

1.568

1.90

1.573

1.579

1.584

1.5 39

1.594

1.599

1.605

1.610

1.615

1.620

2.00

1.625

1.630

1.635

1.640

1.645

1.650

1.655

1.660

1.665

1.670

2.10

1.675

1.680

1.685

1.689

1.694

1.699

1.704

1.709

1.713

1.718

2.20

1.723

1.72S

1.732

1.737

1.742

1.746

1.751

1.756

1.760

1.765

2.30

1.769

1.774

1.773

1.783

1.787

1.792

1.796

1.801

1.805

1.810

2.40

1.814

1.818

1.823

1.827

1.831

1.836

1.840

1.844

1.849

1.853

2.50

1.857

1.861

1.366

1.8 70

1.874

1.878

1.882

1.337

1.891

1.895

2.60

1.899

1.903

1.907

1.911

1.915

1.919

1.923

1.927

1.931

1.935

2.70

1.939

1.943

I.947

1.951

1.955

1.959

1.963

1.967

1.971

1.974

2.30

1.978

1.982

1.986

1.990

1.994

1.997

2.001

2.005

2.009

2.012

2.90

2.016

2.020

2.023

2.027

2.031

2.034

2.038

2.042

2.045

2.049

3.00

2.053

2.056

2.060

2.063

2.067

2.070

2.074

2.078

2.081

2.085

3.10

2.088

2.092

2.095

2.098

2.102

2.105

2.109

2.112

2.116

2.119

WATFR CONTENT 31 PERCENT DG 0 1 2 3

1.70

1.458

1.464

1.470

1.475

1.481

1.486

1.492

1.497

1.503

1 .508

1.80

1.513

1.519

1.524

1.530

1 .535

1.540

1.545

1.551

1.556

1.561

1.90

1.566

1.572

1.577

1.592

1.537

1.592

1.597

1.602

1.607

1.612

2.00

1.617

1.622

1.627

1.632

1.637

1.642

1.647

1.652

1.657

1.661

2.10

1.666

1.671

1.676

1.681

1.635

1.690

1.695

1.699

1.704

1 .709

2.20

1.713

1.719

1.723

1.727

1.732

1.736

1.741

1.745

1.750

1.754

2.30

1.759

1.763

1.760

1.772

1.777

1.781

1.785

1.790

1.794

1.798

2.40

1.803

1.807

1.811

1.816

1.820

1.824

1.828

1.833

1.837

1.841

2.50

1.845

1.849

1.853

1.857

1.862

1 .866

1.870

1.374

1.978

1.882

2.60

1.886

1.890

1.894

1.898

1.902

1.906

1.910

1.914

1.918

1.92k;

2.70

1.925

1.929

1.933

1.937

1.941

1.945

1.948

1.952

1.956

1 .960

2.80

1.964

1.967

1.971

1.975

1.979

1 .982

1.986

1.990

1.993

1.9Q7

2.90

2.001

2.004

2.0C8

2.011

2.015

2.019

2.022

2.026

2.029

2.033

3.00

2.036

2.040

2.043

2.047

2.050

2.054

2.057

2.061

2.064

2.067

3.10

2.071

2.074

2.078

2.081

2.084

2.03e

2.091

2.094

2.0°8

2.101

WATER CONTENT

OG

32 PERCENT

1.70

1.453

1.459

1.464

1.470

1.475

1.431

1.486

1.49 2

1.497

1.502

1.80

1.509

1.513

1.518

1.523

1.529

1.534

1.539

1.544

1.549

1.555

1.90

1.560

1.565

1.570

1.575

1.530

1 .535

1.5 90

1.595

1.600

1.605

2.00

1.610

1.615

1.620

1.624

1.629

1.634

1.639

1.644

1.648

1.653

2.10

1.658

1.663

1.667

1.672

1.677

1.681

1.686

1.691

1.695

1 .700

2.20

1.704

1.709

1.713

1.718

1.722

1.727

1.731

1.736

1.740

1.744

2.30

1.749

1.753

1.753

1.762

1. 766

1.771

1.775

1.7 79

1.783

1.783

2.40

1.792

1.796

1.800

1.8 04

1.809

1.313

1.817

1.821

1.825

1 .329

2.50

1.833

1.837

1.841

1.845

1.850

1.854

1.858

1.862

1.865

1 .869

2.60

1.873

1.877

1.381

1.885

1.889

1 .893

1.897

1.901

1.904

1.908

2.70

1.912

1.916

1.920

1.923

1.927

1.931

1.935

1.938

1.942

1.946

2.80

I.049

1.953

1.957

1.960

1.964

1.96 3

1.971

1.975

1.978

1.982

2.90

1.985

1.989

1.993

1.996

2.000

2.003

2.007

2.010

2.014

2.017

3.00

2.020

2.024

2.027

2.031

2. C34

2.03 7

2.041

2.044

2.048

2.051

3.10

2.054

2.058

2.061

2.064

2.067

2.071

2.074

2.077

2.080

2.084

WATER CONTENT

DG

33 PERCENT

1.70

1.448

1.454

1.459

1.465

1.470

1.475

1.481

1.486

1.491

1.497

1.80

1.502

1.507

1.51?

1.517

1.523

1.528

1.533

1.538

1.543

1.548

1.90

1.553

1.558

1.563

1.563

1.573

1.578

1.583

1.588

1.593

1.593

2.00

1.602

1.607

1.612

1.617

1.622

1.626

1.631

1.636

1.640

1.645

2.10

1.650

1.654

1.659

1.664

1.669

1.673

1.677

1.682

1.636

1.691

2.20

1.6^5

1.700

1.704

1.709

1.713

1.717

1.722

1.726

1.730

1.735

2.30

1.739

1.743

1.749

1.752

1.756

1.760

1.765

1.769

1 .773

1.777

2.40

1.781

1.785

1.790

1.794

1.798

1.802

1.8 06

1.810

1.814

1 .818

2.50

1.822

1.826

1.830

1.834

1.838

1 .842

1.846

1.850

1.853

1.857

2.60

1.361

1.865

1.36°

1.873

1.876

1.880

1.884

1.888

1.892

1.895

2.70

1.899

1.903

1.906

1.910

1.914

1.917

1.921

1.^25

1.928

1.932

2.80

1.936

1.939

1.943

1.946

1.950

1.953

1. 957

1.960

1.964

1.967

2.90

1.971

1.974

1.978

1.981

1.985

1.938

1.991

1.995

1.998

2.002

3.00

2.005

2.008

2.012

2.015

2.018

2.022

2.025

2.028

2.032

2.035

3.10

2.038

2.041

2.045

2.048

2.051

2.054

2.057

2.061

2.064

2.067

10

WATER CONTENT

34 PERCENT

DG

1.70

1.444

1.449

1.454

1.460

1.465

1.470

1.475

1.481

1.486

1.491

1.80

1.496

1.501

1.507

1.512

1 .517

1.522

1.527

1.532

1.537

1.542

1.90

1.547

1.552

1.557

1.562

1.566

1.571

1.576

1.581

1.586

1.590

2.00

1.595

1.600

1.605

1.609

1.614

1.619

1.623

1.628

1.633

1.637

2. 10

1.642

1.646

1.651

1.655

1.660

1.664

1.669

1.673

1.678

1.682

2.20

1.686

1.601

1.695

1.700

1.704

1.708

1.713

1.717

1.721

1.725

2.30

V730

1.734

1 .738

1.742

1.746

1.750

1.755

1.759

1.763

1.767

2.40

1.771

1.775

1.779

1.783

1.787

1.791

1.795

1.799

1.803

1.807

2.50

1.811

1.815

1.819

1.822

1. 826

1.830

1.834

1.838

1.842

1 .845

2.60

1.849

1.853

1.857

1.861

1. 864

1.868

1.872

1.875

1.879

1.883

2.70

1.886

L890

1.894

1.897

1.901

1.904

1.903

1.012

1.915

1.919

2.80

1.922

1.926

1.920

1.933

1.936

1.940

1.943

1.946

1.950

1.953

2.90

1.957

1.960

1.963

1.967

1.970

1.974

1.977

1.980

1.984

1.987

3.00

1.990

1.993

1.997

2.000

2.003

2.006

2.010

2.013

2.016

2.019

3.10

2.022

2.026

2.029

2.032

2.035

2.038

2.041

2.044

2.047

2.051

WATER CONTENT

35 PERCENT

DG

1.70

1.439

1.444

1.440

1.455

1.460

1.465

1.470

1.475

1.481

1 .486

1.80

1.491

1.496

1.501

1.506

1.511

1.3-1 6

1.521

1.526

1.531

1.536

1.90

1.541

1.545

1.550

1.555

1.560

1.565

1.560

1.574

1.579

1.584

2.00

1.588

1.593

1.598

1.602

1.607

1.611

1.616

1.620

1.625

1.630

2.10

1.6 34

1.638

1.64 3

1.647

1.652

1.656

1.661

1.665

1.669

1.674

2.20

1.678

1.682

1.687

1.6°1

1.695

1.609

1.7 04

1.708

1.712

1.716

2.30

1.720

1.724

1.728

1.733

1.737

1.741

1.745

1.749

1.753

1.757

2.40

1.761

1.765

1.769

1.773

1.777

1.781

1.785

1.788

1.792

1.796

2.50

1.0CC

1. «04

l.ROR

1.811

1.815

1.819

1.823

1.827

1.830

1.834

2.60

1.838

1.841

1.845

1.849

1.852

1.856

1.860

1.P63

1.867

1.870

2.70

1.874

1.878

1.381

1.885

1.888

1.892

1.895

1.899

1.902

1.906

2.80

1.909

1.913

1.916

1.91Q

1.923

1.926

1.930

1.933

1.936

1.940

2.90

1.943

1.946

1.95C

1.953

1.956

1.959

1.963

1.966

1.969

1.972

3.00

1.976

1.979

1.98 2

1.985

1.988

1.992

1.995

1.998

2.001

2.004

3.10

2.0C7

2.010

2.013

2.016

2.020

2.02 3

2.026

2.029

2.032

2.035

WATER CONTENT

36 PERCENT

DG

1.70

1.434

1.439

1.445

1.450

1.455

1.460

1.465

1.470

1.475

1.480

1.80

1.485

1.490

1.495

1.500

1.505

1.510

1.515

1.520

1.525

1.530

1.90

1.534

1.5 39

1.54 4

1.549

1.553

1.558

1.563

1.568

1.572

1.577

2.00

1.531

1.586

1.591

I.505

1.600

1.604

1.6 09

1.613

1.618

1.622

2.10

1.626

1.631

1.635

1.640

1.644

1.648

1.653

1.657

1.661

1 .665

2.20

1.670

1.6 74

1.678

1.6 82

1.686

1.691

1.695

1.699

1.703

1.707

2.30

1.711

1.715

1.719

1.723

1.727

1.731

1.735

1.739

1.743

1.747

2.40

1.751

1.755

1.759

1.763

1.767

1.770

1.774

1.778

1.782

1.786

2.50

1.789

1.793

1.797

1.801

1.804

1.808

1.812

1.815

1.819

1.823

2.60

1.826

1.830

1.334

1.837

1.841

1.844

1.848

1.852

1.355

1.359

2.70

1.862

1.866

1.369

1.873

1.876

1.879

1.883

1.886

1.890

1.893

2.80

1.896

1.900

1 .903

1.906

l.oio

1 .913

1.916

1.920

1.923

1.926

2.90

1.930

1.933

1.936

1.939

1.942

1.946

1.949

1.952

1.955

1.953

3.00

1.962

1.965

1.968

1.971

1.974

1.977

1.980

1.983

1.986

1.989

3.10

1.992

1.905

1.998

2.001

2.004

2.007

2.010

2.013

2.016

2.019

11

WATER CONTENT

37 PERCENT

DG

1.70

1.430

1.435

1.440

1.445

1.450

1.455

1.460

1.465

1.470

1.475

1.80

1.480

1.485

1.490

1.495

1.500

1.505

1.509

1.514

1.519

1.524

1.90

1.528

1.533

1.538

1.543

1.547

1.552

1.556

1.561

1.566

1.570

2.00

1.575

1.5 7Q

1.584

1.588

1.593

1.597

1.602

1.606

1.610

1.615

2.10

1.619

1.623

1.628

1.632

1.636

1.640

1.645

1.649

1.653

1.657

2.20

1.662

1.666

1.670

1.674

1.678

1.682

1.686

1.690

1.694

1.698

2.30

1.702

1.706

1.710

1.714

1.718

1.722

1.726

1.730

1.734

1.738

2.40

1.742

1.745

1.74Q

1.753

1.757

1.761

1.764

1. 768

1.772

1.776

2.50

1.779

1.783

1.787

1.790

1.794

1.798

1.801

1.805

1.808

1.812

2.60

1.815

1.819

1.823

1.826

1.830

1.813

1.837

1.840

1.844

1.847

2.70

1.850

1.854

1.857

1.861

1.864

1.867

1.871

1.874

1.877

1.881

2.80

1.884

1.887

1.891

1.894

1.897

1.900

1.904

1.907

1.910

1.913

2.90

1.917

1.920

1.923

1.926

1.929

l.°32

1.935

1.939

1.942

1.945

3.00

1.948

1.951

1.954

1.957

1.960

1.963

1.966

1.969

1.972

1.975

3.10

1.978

1.981

1.984

1.987

1.990

I.Q93

1.996

1.999

2.002

2.004

WATER CONTENT

38 PERCENT

DG

1.70

1.425

1.430

1.435

1.440

1.445

1.450

1.455

1.460

1.465

1.470

1.80

1.475

1.480

1.485

1.490

1.494

1.499

1.504

1.509

1.513

1.518

1.90

1.523

1.527

1.532

1.537

1.541

1.546

1.550

1.555

1.559

1.564

2.00

1.568

1.573

1.577

1.581

1.586

1.590

1.595

1.599

1.603

1.608

2.10

1.612

1.616

1.620

1.625

1.629

1.633

1.637

1.641

1.645

1.649

2.20

1.654

1.658

1.662

1.666

1.670

1.674

1.678

1.682

1.686

1.690

2.30

1.694

1.698

1.702

1.705

1.709

1.713

1.717

1.721

1.725

1.728

2.40

1.732

1.736

1.740

1.743

1.747

1.751

1.755

1.758

1.762

1.766

2.50

1.769

1.773

1.776

1.780

1.784

1.787

1.791

1.794

1.798

1.801

2.60

1.805

1.808

1.812

1.815

1.819

1.822

1.826

1.829

1.832

1.836

2.70

1.839

1.842

1.846

1.849

1.852

1.856

1.859

1.862

1.866

1.869

2.80

1.872

1.875

1.879

1.882

1. 885

1.888

1.891

1.894

1.898

1.901

2.90

l.°04

1.907

1.910

1.913

1.916

1.919

1.922

1.925

1.929

1.932

3.00

1.935

1.93 8

1.941

1.944

1.947

1.950

1.952

1.955

1.958

1.961

3.10

1.964

1.967

1.970

1.973

1.976

1.979

1.981

1.984

1.987

1.990

WATER CONTENT

39 PERCENT

DG

1.70

1.421

1.426

1.431

1.436

1.441

1.446

1.451

1.456

1.460

1.465

1.80

1.470

1.475

1.480

1.484

1.489

1.494

1.498

1.503

1 .508

1.512

1.90

1.517

1.522

1.526

1.531

1.535

1.540

1.544

1.549

1.553

1.557

2.00

1.562

1.566

1.571

1.575

1.579

1.583

1.588

1.592

1.596

1.601

2.10

1.605

1.609

1.613

1.617

1.621

1.626

1.6 30

1.634

1.638

1.642

2.20

1.646

1.650

1.654

1.658

1.662

1.666

1.670

1.674

1.678

1.681

2.30

1.685

1.689

1.693

1.697

1.701

1.704

1.708

1.712

1.716

1.719

2.40

1.723

1.727

1.731

1.734

1.738

1.741

1.745

1.749

1.752

1.756

2.50

1.759

1.763

1.767

1.770

1.774

1.777

1.781

1.784

1.788

1.791

2.60

1.794

1.798

1.801

1.805

1.808

1.811

1.815

1.818

1.821

1.825

2.70

1.828

1.831

1.835

1.838

1.841

1.844

1.848

1.851

1.854

1.857

2.80

1.860

1.864

1.867

1.870

1.873

1.876

1.8 79

1.882

1.885

1.889

2.90

1.892

1.895

1.898

1.901

1.904

1.907

1.910

1.913

1.916

1.919

3.00

1.922

1.925

1.928

1.930

1.933

1.936

1.939

1.942

1.945

1.948

3.10

1.951

1.953

1.956

1.959

1.962

1.965

1.968

1.970

1.973

1.976

12

WATER CONTENT 40 PERCENT

OG 0123456789

1.70 1.417 1.422 1.427 1.431 1.436 1.441 1.446 1.451 1.456 1.460

1.80 1.465 1.470 1.475 1.479 1.484 1.489 1.493 1.498 1.502 1.507

1.^0 1.511 1.516 1.520 1.525 1.529 1.534 1.538 1.543 1.547 1.551

2.00 1.556 1.560 1.564 1.568 1.573 1.577 1.581 1.585 1.590 1.594

2.10 1.598 1.602 1.606 1.610 1.614 1.618 1.622 1.626 1.630 1.634

2.20 1.638 1.642 1.646 1.650 1.654 1.658 1.662 1.666 1.669 1.673

2.30 1.677 1.681 1.685 1.688 1.692 1.696 1.700 1.703 1.707 1.711

2.40 1.714 1.718 1.722 1.725 1.729 1.732 1.736 1.739 1.743 1.746

2.50 1.750 1.753 1.757 1.760 1.764 1.767 1.771 1.774 1.778 1.781

2.60 1.784 1.788 1.791 1.794 1.798 1.801 1.804 1.808 1.811 1.814

2.70 1.817 1.821 1.824 1.827 1.830 1.833 1.837 1.840 1.843 1.846

2.80 1.849 1.852 1.855 1.858 1.861 1.864 1.868 1.871 1.874 1.877

2.90 1.880 1.883 1.886 1.889 1.892 1.894 1.897 1.900 1.903 1.906

3.00 1.909 1.912 1.915 1.918 1.Q21 1.923 1.926 1.929 1.932 1.935

3.10 1.937 1.940 1.943 1.946 1.949 1.951 1.954 1.957 1.959 1.962

WATER CONTENT 41 PERCENT

OG 0123456789

1.70 1.412 1.417 1.422 1,427 1.432 1.437 1.441 1.446 1.451 1.456

1.80 1.460 1.465 1.470 1.474 1.479 1.483 1.488 1.492 1.497 1.501

1.90 1.506 1.510 1.515 1.519 1.524 1.528 1.532 1.537 1.541 1.545

2.00 1.549 1.554 1.558 1.562 1.566 1.570 1.575 1.579 1.583 1.587

2.10 1.591 1.595 1.599 1.603 1.607 1.611 1.615 1.619 1.623 1.627

2.20 1.631 1.635 1.639 1.643 1.646 1.650 1.654 1.658 1.662 1.665

2.30 1.669 1.673 1.677 1.680 1.684 1.688 1.691 1.695 1.69-8 1.702

2.40 1.706 1.709 1.713 1.716 1.720 1.723 1.727 1.730 1.734 1.737

2.50 1.741 1.744 1.748 1.751 1.754 1.758 1.761 1.764 1.768 1.771

2.60 1.774 1.778 1.781 1.784 1.788 1.791 1.794 1.797 1.800 1.804

2.70 1.807 1.810 1.813 1.816 1.819 1.823 1.826 1.829 1.832 1.835

2.80 1.838 1.841 1.844 1.847 1.850 1.853 1.856 1.859 1.862 1.865

2.90 1.868 1.971 1.874 1.877 1.880 1.883 1.885 1.888 1.891 1.894

3.00 1.897 1.900 1.903 1.905 1.908 1.911 1.914 1.916 1.919 1.922

3.10 1.925 1.927 1.930 1.933 1.936 1.938 1.941 1.944 1.946 1.949

WATER CONTENT 42 PERCENT

DG 0123456789

1.70 1.408 1.413 1.418 1.423 1.428 1.432 1.437 1.442 1.446 1.451

1.80 1.456 1.460 1.465 1.469 1.474 1.478 1.483 1.487 1.492 1.496

1.90 1.501 1.505 1.509 1.514 1.518 1.522 1.527 1.531 1.535 1.539

2.00 1.543 1.548 1.552 1.556 1.560 1.564 1.568 1.572 1.576 1.580

2.10 1.584 1.588 1.592 1.596 1.600 1.604 1.608 1.612 1.616 1.620

2.20 1.624 1.623 1.631 1.635 1.639 1.643 1.646 1.650 1.654 1.658

2.30 1.661 1.665 1.669 1.672 1.676 1.679 1.683 1.687 1.690 1.694

2.40 1.697 1.701 1.704 1.708 1.711 1.715 1.718 1.722 1.725 1.728

2.50 1.732 1.735 1.738 1.742 1.745 1.748 1.752 1.755 1.758 1.762

2.60 1.765 1.768 1.771 1.774 1.778 1.781 1.784 1.787 1.790 1.794

2.70 1.797 l.ROO 1.803 1.806 1.809 1.812 1.815 1.813 1.821 1.824

2.80 1.827 1.830 1.833 1.836 1.839 1.342 1.845 1.848 1.851 1.854

2.90 1.857 1.860 1.862 1.865 1.868 1.871 1.874 1.877 1.879 1.882

3.00 1.885 1.888 1.890 1.893 1.896 1.899 1.901 1.904 1.907 1.910

3.10 1.912 1.915 1.918 1.920 1.923 1.926 1.928 1.931 1.933 1.934

13

WATER CONTENT

43 PERCENT

DG

1.70

1.404

1.409

1.414

1.419

1.423

1.42 8

1.433

1.437

1.442

1.446

1.80

1.451

1.455

1.460

1.464

1.469

1.473

1.478

1.482

1.487

1.491

1.90

1.495

1.500

1.504

1.508

1.512

1.517

1.521

1.525

1.529

1.533

2.00

1.538

1.542

1.546

1.550

1.554

1.558

1.562

1.566

1.570

1.574

2.10

1.578

1.582

1.5 86

1.5Q0

1.594

1.598

1.601

1.605

1.609

1.613

2.20

1.617

1.620

1.624

1.628

1.632

1.635

1.639

1.643

1.646

1.650

2.30

1.654

1.657

1.661

1.664

1.668

1.671

1.675

1.679

1.682

1.686

2.40

1.689

1.692

1.696

1.699

1.703

1.706

1.709

1.713

1.716

1.720

2.50

1.723

1.726

1.730

1.733

1.736

1.739

1.743

1.746

1.749

1.752

2.60

1.755

1.759

1.762

1.765

1.768

1.771

1.774

1.777

1.781

1.784

2.70

1.787

1.790

1.793

1.796

1.799

1.802

1.805

1.808

1.811

1.814

2.80

1.817

1.820

1.823

1.825

1.828

1.831

1.834

1.837

1.840

1.843

2.90

1.846

1.848

1.851

1.854

1.857

1.860

1.862

1.865

1.868

1.871

3.00

1.873

1.876

1.879

1.881

1.884

1.887

1.890

1.892

1.895

1.897

3.10

1.900

1.903

1.905

1.908

1.911

1.913

1.916

1.918

1.921

1.923

WATER CONTENT

44 PERCENT

DC

1.70

1.400

1.405

1.410

1.414

1.419

1.424

1.428

1.433

1.437

1.442

1.80

1.446

1.451

1.455

1.460

1.464

1.469

1.473

1.477

1.482

1.486

1.90

1.490

1.494

1.499

1.503

1.507

1.511

1.515

1.520

1.524

1.528

2.00

1.532

1.536

1.540

1.544

1.548

1.552

1.556

1.560

1.564

1.568

2.10

1.572

1.576

1.579

1.583

1.587

1.591

1.595

1.599

1.602

1.606

2.20

1.610

1.613

1.617

1.621

1.624

1.628

1.632

1.635

1.639

1.643

2.30

1.646

1.650

1.653

1.657

1.660

1.664

1.667

1.671

1.674

1.678

2.40

1.681

1.684

1.688

1.691

1.694

1.698

1.701

1.704

1.708

1.711

2.50

1.714

1.718

1.721

1.724

1.727

1.730

1.734

1.737

1.740

1.743

2.60

1.746

1.749

1.753

1.756

1.759

1.762

1.765

1.768

1.771

1.774

2.70

1.777

1.780

1.783

1.786

1.78Q

1.792

1.795

1.798

1.801

1.804

2.80

1.806

1.809

1.812

1.815

1.818

1.821

1.824

1.826

1.829

1.832

2.90

1.835

1.83-8

1.840

1.843

1.846

1.849

1.851

1.854

1.857

1.859

3.00

1.862

1.865

1.867

1.870

1.873

1.875

1.878

1.881

1.883

1.886

3.10

1.888

1.891

1.893

1.896

1.899

1.901

1.904

1.906

1.909

1.911

WATER CONTENT

45 PERCENT

DG

1.70

1.397

1.401

1.406

1.410

1.415

1.420

1.424

1.429

1.433

1.438

1.80

1.442

1.446

1.451

1.455

1.460

1.464

1.468

1.472

1.477

1.481

1.90

1.485

1.489

1.494

1.498

1.502

1.506

1.510

1.514

1.518

1.522

2.00

1.526

1.530

1.534

1.538

1.542

1.546

1.550

1.554

1.558

1.562

2.10

1.566

1.569

1.573

1.577

1.581

1.584

1.588

1.592

1.596

1.599

2.20

1.603

1.607

1.610

1.614

1.618

1.621

1.625

1.628

1.632

1.635

2.30

1.639

1.642

1.646

1.649

1.653

1.656

1.660

1.66 3

1.666

1.670

2.40

1.673

1.676

1.680

1.683

1.686

1.690

1.693

1.696

1.699

1.703

2.50

1.706

1.709

1.712

1.715

1.719

1.722

1.725

1.728

1.731

1.734

2.60

1.737

1.740

1.743

1.747

1.750

1.753

1.756

1.759

1.762

1.765

2.70

1.767

1.770

1.773

1.776

1.779

1.782

1.785

1.788

1.791

1.794

2.80

1.796

1.799

1.802

1.805

1.808

1.811

1.813

1.816

1.819

1.822

2*90

1.824

1.827

1.830

1.832

1.835

1.838

1.840

1.843

1.846

1.848

3.00

1.851

1.854

1.856

1.859

1.861

1.864

1.867

1.869

1.872

1.874

3.10

1.877

1.879

1.882

1.884

1.887

1.889

1.892

1.894

1.897

1.899

14

WATFR CONTENT

46 PERCENT

DG

1.70

1.393

1.397

1.402

1.407

1.411

1.416

1.420

1.424

1.429

1.433

1.80

1.438

1.442

1.446

1.451

1.455

1.459

1.463

1.468

1.472

1.476

1.90

1.480

1.484

1.489

1.493

1.497

1.501

1.505

1.509

1.513

1.517

2.00

1.521

1.525

1.529

1.533

1.537

1.540

1.544

1.548

1.552

1.556

2.10

1.560

1.563

1.567

1.571

1.574

1.578

1.582

1.586

1.589

1.593

2.20

1.596

1.600

1.604

1.607

1.611

1.614

1.618

1.621

1.625

1.628

2.30

1.632

1.635

1.639

1.642

1.645

1.649

1.652

1.655

1.659

1.662

2.40

1.665

1.669

1.672

1.675

1.678

1.682

1.685

1.688

1.691

1.695

2.50

1.698

1.701

1.704

1.707

1.710

1.713

1.716

1.719

1.723

1.726

2.60

1.729

1.732

1.735

1.738

1.741

1.744

1.747

1.749

1.752

1.755

2.70

1.758

1.761

1.764

1.767

1.770

1.773

1.775

1.778

1.781

1.784

2.80

1.787

1.789

1.792

1.795

1.798

1.801

1.803

1.806

1.809

1.811

2.90

1.814

1.817

1.819

1.822

1.82 5

1.827

1.830

1.833

1.835

1.838

3.00

1.840

1.843

1.845

1.848

1.851

1.853

1.856

1.858

1.861

1.863

3.10

1.866

1.868

1.871

1.873

1.875

1.878

1.880

1.883

1.885

1.888

WATER CONTENT 47 PERCENT DG 0 1 2 3

1.70

1.389

1.394

1.398

1.403

1.407

1,412

1.416

1.420

1.425

1.429

1.80

1.433

1.439

1.442

1.446

1.450

1.455

1.459

1.463

1.467

1.471

1.90

1.475

1.480

1.484

1.488

1.492

1.496

1.500

1.504

1.508

1.512

2.00

1.515

1.519

1.523

1.527

1.531

1.535

1.539

1.542

1.546

1.550

2.10

1.554

1.557

1.561

1.565

1.568

1.572

1.576

1.579

1.583

1.586

2.20

1.590

1.594

1.597

1.601

1.604

1.608

1.611

1.614

1.618

1.621

2.30

1.625

1.628

1.631

1.635

1.638

1.641

1.645

1.648

1.651

1.655

2.40

1.658

1.661

1.664

1.668

1.671

1.674

1.677

1.680

1.683

1.687

2.50

1.690

1.693

1.696

1.699

1.702

1.705

1.708

1.711

1.714

1.717

2.60

1.720

1.723

1.726

1.729

1.732

1.735

1.738

1.741

1.743

1.746

2.70

1.749

1.752

1.755

1.758

1.761

1.763

1.766

1.769

1.772

1.774

2.80

1.777

1.780

1.783

1.785

1.788

1.791

1.793

1.796

1.799

1.801

2.^0

1.804

1.807

1.809

1.812

1.815

1.817

1.820

1.822

1.825

1.827

3.00

1.830

1.832

1.835

1.837

1.840

1.842

1.845

1.847

1.850

1.852

3.10

1.855

1.857

1.860

1.862

1.864

1.867

1.869

1.872

1.874

1.876

WATER CONTENT

48 PERCENT

DG

1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 2.50 2.60 2.70 2.80 2.90 3.00 3.10

0

1.385 1.429 1.471 1.510 1.548 1.584 1.618 1.651 1.682 1.712 1.740 1.768 1.794 1.820 1.844

1

1.390 1.433 1.475 1.514 1.551 1.587 1.621 1.654 1.685 1.715 1.743 1.771 1.797 1.822 1.846

1.394 1.438 1.479 1.518 1.555 1.591 1.625 1.657 1.688 1.718 1.746 1.773 1.799 1.825 1.849

1.399 1.442 1.483 1.522 1.559 1.594 1.628 1.660 1.691 1.720 1.749 1.776 1.802 1.827 1.851

1.403 1.446 1.487 1.525 1.562 1.598 1.631 1.663 1.694 1.723 1.752 1.779 1.805 1.830 1.854

1.408 1.450 1.491 1.529 1.566 1.601 1.634 1.666 1.697 1.726 1.754 1.781 1.807 1.832 1.856

1.412 1.454 1.495 1.533 1.570 1.604 1.638 1.669 1.700 1.729 1.757 1.784 1.810 1.834 1.858

1.416 1.458 1.499 1.537 1.573 1.608 1.641 1.673 1.703 1.732 1.760 1.787 1.812 1.837 1.861

8

1.421 1.463 1.502 1.540 1.577 1.611 1.644 1.676 1.706 1.735 1.763 1.789 1.815 1.839 1.863

1.425 1.467 1.506 1.544 1.580 1.615 1.647 1.679 1.709 1.738 1.765 1.792 1.817 1.842 1.865

15

WATER CONTENT

49 PERCENT

DG

1.70

1.382

1.386

1.391

1.395

1.399

1.404

1.408

1.412

1.417

1.421

1.80

1.425

1.429

1.433

1.438

1.442

1.446

1.450

1.454

1.458

1.462

1.90

1.466

1.470

1.474

1.478

1.482

1.486

1.490

1.494

1.497

1.501

2.00

1.505

1 .509

1.513

1.516

1.520

1.524

1.528

1.531

1.535

1.539

2.10

1.542

1.546

1.549

1.553

1.556

1.560

1.564

1.567

1.571

1.574

2.20

1.577

1.581

1.584

1.588

1.591

1.595

1.598

1.601

1.605

1.608

2.30

1.611

1.614

1.618

1.621

1.624

1.627

1.631

1.634

1.637

1 .640

2.40

1.643

1.647

1.650

1.653

1.656

1.659

1.662

1.665

1.668

1.671

2.50

1.674

1.677

1.680

1.683

1.686

1.689

1.692

1.695

1.699

1.701

2.60

1.704

1.706

1.709

1.712

1.715

1.718

1.721

1.723

1.726

1.729

2.70

1.732

1.735

1.737

1.740

1.743

1.745

1.748

1.751

1.754

1.756

2.80

1.759

1.761

1.764

1.767

1.769

1.772

1.775

1.777

1.780

1.782

2.90

1.785

1.787

1.790

1.792

1.795

1.797

1.800

1.802

1.805

1.807

3.00

1.810

1.812

1.815

1.817

1.810

1.822

1.824

1.827

1.829

1.831

3.10

1.834

1.836

1.838

1.841

1.843

1.845

1.848

1.850

1.852

1.854

WATER CONTENT

50 PERCENT

OG

1.70

1.378

1.383

1.387

1.391

1.396

1.400

1.4 04

1.408

1.413

1.417

1.80

1.421

1.425

1.429

1.433

1.437

1.442

1.446

1.450

1.454

1.458

1.90

1.462

1.465

1.469

1.473

1.477

1.481

1.485

1.489

1.492

1.496

2.00

1.500

1.504

1.507

1.511

1.515

1.519

1.522

1.526

1.529

1.533

2.10

1.537

1.540

1.544

1.547

1.551

1.554

1.558

1.561

1.565

1.568

2.20

1.571

1.575

1.578

1.582

1.585

1.598

1.592

1.595

1.598

1.601

2.30

1.605

1.608

1.611

1.614

1.619

1.621

1.624

1.627

1.630

1.633

2.40

1.636

1.639

1.643

1.646

1.649

1.652

1.655

1.658

1.661

1.664

2.50

1.667

1.670

1.673

1.6 75

1.678

1.681

1.684

1.687

1.690

1.69 3

2.60

1.696

1.698

1.701

1.704

1.707

1.710

1.712

1.715

1.718

1.721

2.70

1.723

1.726

1.729

1.732

1.734

1.737

1.739

1.742

1.745

1.747

2.80

1.750

1.753

1.755

1.758

1.760

1.763

1.765

1.768

1.770

1.773

2.90

1.776

1.778

1.780

1.783

1.785

1.788

1.7 90

1. 793

1.795

1.798

3.00

1.800

1.802

1.805

1.807

1.810

1.812

1.814

1.817

1.819

1.821

3.10

1.824

1.826

1.828

1.830

1.833

1.835

1.837

1.839

1.842

1.944

WATER CONTENT

51 PERCENT

DG

1.70

1.375

1.379

1.384

1.388

1.392

1.396

1.401

1.405

1.409

1.413

1.80

1.417

1.421

1.425

1.429

1.433

1.437

1.441

1.445

1.449

1.453

1.90

1.457

1.461

1.465

1.469

1.473

1.476

1.480

1.484

1.488

1.491

2.00

1.495

1.499

1.502

1.506

1.510

1.513

1.517

1.521

1.524

1.528

2.10

1.531

1.535

1.538

1.542

1.545

1.549

1.552

1.555

1.559

1.562

2.20

1.566

1.569

1.572

1.575

1.579

1.582

1.585

1.589

1.592

1.595

2.30

1.598

1.601

1.605

1.608

1.611

1.614

1.617

1.620

1.623

1.626

2.40

1.629

1.633

1.636

1.639

1.642

1.645

1.648

1.651

1.653

1.656

2.50

1.65^

1.662

1.665

1.668

1.671

1.674

1.677

1.679

1.682

1.685

2.60

1.688

1.691

1.693

1.696

1.699

1.702

1.704

1.707

1.710

1.713

2.70

1.715

1.718

1.721

1.723

1.726

1.728

1.731

1.734

1.736

1.739

2.80

1.741

1.744

1.746

1.749

1.752

1.754

1.757

1.759

1.762

1.764

2.90

1.766

1.769

1.771

1.774

1.776

1.779

1.781

1.78 3

1.786

1.788

3.00

1.791

1.793

1.795

1.798

1.800

1.802

1.804

1.807

1.809

1.811

3.iu

1.814

1.816

1.818

1.820

1.823

1.825

1.827

1.829

1.831

1.834

16

WATER CONTENT

52 PERCENT

DG

1.70

1.372

1.376

1.380

1.384

1.388

1.393

1.397

1.401

1.405

1.409

1.80

1.413

1.417

1.421

1.425

1.429

1.433

1.437

1.441

1.445

1.449

1.90

1.453

1.457

1.460

1.464

1.468

1.472

1.475

1.479

1.483

1.48 7

2.00

1.4P0

1.494

1.497

1.501

1.505

1.508

1.512

1.515

1.519

1.522

2. 10

1.526

1.529

1.533

1.536

1.540

1.543

1.546

1.550

1.553

1.556

2.20

1.560

1.563

1.566

1.570

1.573

1.576

1.5 79

1.582

1.586

1.589

2.30

1.592

1.595

1.598

1.601

1.604

1.608

1.611

1.614

1.617

1.620

2.40

1.623

1.626

1.629

1.632

1.635

1.638

1.641

1.643

1.646

1.649

2.50

1.652

1.655

1.658

1.661

1.664

1.666

1.669

1.672

1.675

1.678

2.60

1.680

1.683

1.686

1.638

1.691

1.694

1.697

1.699

1.702

1.705

2.70

1.707

1.710

1.712

1.715

1.718

1.720

1.723

1.725

1.728

1.730

2.80

1.733

1.735

1.738

1.740

1.743

1.745

1.748

1.750

1.753

1.755

2.90

1.758

1.760

1.762

1.765

1.767

1.770

1.7 72

1.774

1.777

1.779

3.00

1.781

1.784

1.786

1.788

1.790

1.793

1.795

1.797

1.800

1.802

3.10

1.804

1.806

1.808

1.811

1.813

1.815

1.817

1.819

1.822

1.824

WATER CONTENT

53 PERCENT

DG

1.70

1.368

1.372

1.377

1.381

1.385

1.389

1.393

1.397

1.401

1.405

1.80

1.409

1.413

1.417

1.421

1.425

1.429

1.433

1.437

1.441

1.445

1.90

1.448

1.45?

1.456

1.460

1.463

1.467

1.471

1.475

1.478

1.482

2.00

1.485

1.489

1.493

1.496

1.500

1.503

1.507

1.510

1.514

1.517

2.10

1.521

1.524

1.527

1.531

1. 534

1.538

1.541

1.544

1.547

1.551

2.20

1.554

1.557

1.561

1.564

1.567

1.570

1.573

1.576

1.580

1.583

2.30

1.586

1.589

1.592

1.595

1.598

1.601

1.604

1.607

1.610

1.613

2.40

1.616

1.619

1.622

1.625

1.623

1.631

1.634

1.637

1.639

1.642

2.50

1.645

1.648

1.651

1.654

1.656

1.659

1.662

1.665

1.667

1.670

2.60

1.673

1.676

1.678

1.681

1.684

1.686

1.689

1.691

1.694

1.697

2.70

1.699

1.702

1.704

1.707

1.710

1.712

1.715

1.717

1.720

1.722

2.80

1.725

1.727

L730

1.732

1.734

1.737

1.739

1.742

1.744

1.747

2.90

1.749

1.751

1.754

1.756

1.758

1.761

1.763

1.765

1.768

1.770

3.00

1.772

1.774

1.777

1.779

1.781

1.793

1.786

1.788

1.790

1.792

3.10

1.795

1.797

1.799

1.801

1.803

1. 805

1.808

1.810

1.812

1.814

WATER CONTENT

54 PERCENT

OG

1.70

1.365

1.369

1.373

1.377

1.382

1.396

1.390

1.394

1.398

1.402

1.80

1.406

1.410

1.414

1.417

1.421

1.425

1.429

1.433

1.437

1.440

1.90

1.444

1.449

1.452

1.455

1.459

1.463

1.466

1.470

1.474

1.477

2.00

1.481

1.484

1.488

1.491

1 .495

1.498

1.502

1.505

1.509

1.512

2.10

1.515

1.519

1.522

1.526

1.529

1.532

1.535

1.539

1.542

1.545

2.20

1.548

1.552

1.555

1.558

1.561

1.564

1.567

1.571

1.574

1.577

2.30

1.580

1.583

1.586

1.589

1.592

1.595

1.598

1.601

1.604

1.607

2.40

1.610

1.613

1.616

1.618

1.621

1.624

1.627

1.630

1.633

1.636

2.50

1.638

1.641

1.644

1.647

1.649

1.652

1.655

1.658

1.660

1.663

2.60

1.666

1.668

1.671

1.673

1.676

1.679

1.681

1.684

1.686

1.689

2.70

1.692

1.694

1.6^7

1.699

1.702

1.704

1.707

1.709

1.712

1.714

2.80

1.717

1.719

1.721

1.724

1.726

1.729

1.731

1.733

1.736

1.738

2.90

1.740

1.743

1.745

1.747

1.750

1.752

1.754

1.757

1.759

1.761

3.00

1.763

1.766

1.768

1.770

1.772

1.774

1.777

1.779

1.781

1.783

3.10

1.785

1.787

1.790

1.792

1.794

1.796

1.798

1.800

1.802

1.804

17

MATER CONTENT 55 PERCENT DG 0 1 2 3

1.70

1.362

1.366

1.370

1.3 74

1.378

1.382

1.386

1.390

1.394

1.398

1.80

1.402

1.406

1.410

1.414

1.417

1.421

1.425

1.429

1.433

1.436

1.90

1.440

1.444

1.447

1.451

1.455

1.458

1.462

1.466

1.469

1.473

2.00

1.476

1.480

1.483

1.487

1.490

1.494

1.497

1.500

1.504

1.507

2.10

1.510

1.514

1.517

1.520

1.524

1.527

1.530

1.533

1.537

1.540

2.20

1.543

1.546

1.549

1.552

1.556

1.559

1.562

1.565

1.568

1.571

2.30

1.574

1.577

1.580

1.583

1.586

1.589

1.592

1.595

1.598

1.601

2.40

1.603

1.606

1.609

1.612

1.615

1.618

1.620

1.623

1.626

1.629

2.50

1.632

1.634

1.637

1.640

1.642

1.645

1.648

1.651

1.653

1.656

2.60

1.658

1.661

1.664

1.666

1.669

1.671

1.674

1.677

1.679

1.682

2.70

1.684

1.687

1.689

1.692

1.694

1.697

1.699

1.701

1.704

1.706

2.80

1.709

1.711

1.713

1.716

1.718

1.721

1.723

1.725

1.728

1.730

2.90

1.732

1.734

1.737

1.739

1.741

1.744

1.746

1.748

1.750

1.753

3.00

1.755

1.75 7

1.759

1.761

1.763

1.766

1.768

1.770

1.772

1.774

3.10

1.776

1.778

1.781

1.783

1.785

1.787

1.789

1.791

1.793

1.795

WATER CONTENT

DG

56 PERCENT

1.70

1.359

1.3 63

1.367

1.371

1.375

1.379

1.383

1.387

1.391

1.395

1.80

1.398

1.402

1.406

1.410

1.414

1.417

1.421

1.42 5

1.429

1.432

1.90

1.436

1.440

1.443

1.447

1.451

1.454

1.458

1.461

1.465

1.468

2.00

1.472

1.475

1.479

1.482

1.485

1.489

1.492

1.496

1.499

1.502

2.10

1.506

1.509

1.512

1.515

1.519

1.522

1.525

1.528

1.531

1.534

2.20

1.538

1.541

1.544

1.547

1.550

1.553

1.556

1.559

1.562

1.565

2.30

1.568

1.571

1.574

1.577

1.580

1.583

1.5 86

1.589

1.592

1.594

2.40

1.597

1.600

1.603

1.606

1.609

1.611

1.614

1.617

1.620

1.622

2.50

1.625

1.628

1.630

1.633

1.636

1.638

1.641

1.644

1.646

1.649

2.60

1.651

1.654

1.657

1.659

1.662

1.664

1.667

1.669

1.672

1.674

2.70

1.677

1.679

1.682

1.684

1.687

1.689

1.691

1.694

1.696

1.699

2.80

1.701

1.703

1.706

1.708

1.710

1.713

1.715

1.717

1.720

1.722

2.90

1.724

1.726

1.729

1.731

1.733

1.735

1.738

1.740

1.742

1.744

3.00

1.746

1.748

1.751

1.753

1.755

1.757

1.759

1.761

1.763

1.765

3.10

1.768

1.770

1.772

1.774

1.776

1.778

1.780

1.782

1.784

1.786

WATER CONTENT

OG

57 PERCENT

1.70

1.356

1.360

1.364

1.368

1.372

1.3 75

1.379

1.383

1.387

1.391

1.80

1.395

1.399

1.402

1.406

1.410

1.414

1.417

1 . 42 1

1.425

1.428

1.90

1.432

1.436

1.439

1.443

1.446

1.450

1.453

1.457

1.460

1.464

2.00

1.467

1.471

1.474

1.477

1.481

1.484

1.488

1.491

1.494

1.497

2.10

1.501

1.504

1.507

1.510

1.514

1.517

1.520

1.523

1.526

1.529

2.20

1.532

1.535

1.539

1.542

1. 545

1.548

1.551

1.554

1.557

1.560

2.30

1.563

1.565

1.568

1.571

1.574

1.577

1.580

1.583

1.586

1.588

2.40

1.591

1.594

1.597

1.600

1.602

1.605

1.608

1.610

1.613

1.616

2.50

1.619

1.621

1.624

1.627

1.629

1.632

1.634

1.637

1.640

1.642

2.60

1.645

1.647

1.650

1.652

1.655

1.657

1.660

1.662

1.665

1.667

2.70

1.670

1.672

1.674

1.677

1.679

1.682

1.684

1.686

1.689

1.691

2.80

1.693

1.696

1.698

1.700

1.703

1.705

1.707

1.709

1.712

1.714

2.90

1.716

1.718

1.721

1.723

1.725

1.727

1.729

1.732

1.734

1.736

3.00

i.738

1.740

1.742

1.744

1.746

1.749

1.751

1.753

1.755

1.757

3.10

1.759

1.761

1.763

1.765

1.767

1.769

1.771

1.773

1.775

1.777

18

WATER CONTENT

58 PERCENT

OG

1.70

1.352

1.356

1.360

1.364

1.368

1.372

1.376

1.380

1.384

1.388

1.80

1.391

I. 395

1.399

1.403

1.406

1.410

1.414

1.417

1.421

1.425

1.90

1.428

1.432

1.435

1.439

1.442

1.446

1.449

1.453

1.456

1.460

2.00

1.463

1.466

1.470

1.473

1.476

1.480

1.483

1.486

1.489

1.493

2.10

1.496

1.49Q

1.502

1.506

1.509

1.512

1.515

1.518

1.521

1.524

2.20

1.527

1.530

1.533

1.536

1.539

1.542

1.545

1.548

1.551

1.554

2.30

1.557

1.560

1.563

1.566

1.568

1.571

1.574

1.577

1.580

1.583

2.40

1.585

1.588

1.591

1.594

1.596

1.599

1.602

1.604

1.607

1.610

2.50

1.612

1.615

1.617

1.620

1.623

1.625

1.628

1.630

1.633

1.635

2.60

1.638

1.640

1.643

1.645

1.648

1.650

1.653

1.655

1.658

1.660

2.70

1.663

1.665

1.667

1.670

1.672

1.674

1.677

1.679

1.681

1.684

2.80

1.686

1.688

1.691

1.693

1.695

1.697

1.700

1.702

1.704

1.706

2.90

1.708

1.711

1.713

1.715

1.717

1.719

1.721

1.724

1.726

1.728

3.00

1.730

1.732

1.734

1.736

1.738

1.740

1.742

1.744

1.746

1.749

3.10

1.751

1.753

1.755

1.757

1.759

1.761

1.762

1.764

1.766

1.768

WATER CONTENT

59 PERCENT

OG

1.70

1.349

1.353

1.357

1.361

1.365

T.369

1.373

1.377

1.380

1.384

1.80

1.388

1.392

1.395

1.399

1.403

1.406

1.410

1.414

1.417

1.421

1.90

1.424

1.428

1.431

1.435

1.438

1.442

1.445

1.449

1.452

1.455

2.00

1.459

1.462

1.465

1.469

1.472

1.475

1.478

1.482

1.485

1.488

2.10

1.491

1.494

1.498

1.501

1.504

1.507

1.510

1.513

1.516

1.519

2.20

1.522

1.525

1.528

1.531

1.534

1.537

1.540

1.543

1.546

1.549

2.30

1.552

1.554

1.557

1.560

1.563

1.566

1.568

1.571

1.574

1.577

2.40

1.579

1.5*2

1.585

1.588

1.590

1.503

1.596

1.598

1.601

1.603

2.50

1.606

1.609

1.611

1.614

1.616

1.619

1.621

1.624

1.626

1.629

2.60

1.631

1.634

1.636

1.639

1.641

1.644

1.646

1.648

1.651

1.653

2.70

1.656

1.658

1.660

1.663

1.665

1.667

1.670

1.672

1.674

1.676

2.80

1.679

1.681

1.683

1.685

1.688

1.690

1.692

1.694

1.697

1.699

2.90

1.701

1.703

1.705

1.707

1.709

1.712

1.714

1.716

1.718

1.720

3.00

1.722

1.724

1.726

1.728

1.730

1.732

1.734

1.736

1.738

1.740

3.10

1.742

1.744

1.746

1.748

1.750

1.752

1.754

1.756

1.758

1.760

WATER CONTENT

60 PERCENT

DG

1.70

1.347

1.350

1.354

1.358

1.362

1.366

1.370

1.373

1.377

1.381

1.80

1.385

1.388

1.392

1.396

1.399

1.403

1.406

1.410

1.414

1.417

l.°0

1.421

1.424

1.428

1.431

1.434

1.438

1.441

1.445

1.448

1.451

2.00

1.455

1.458

1.461

1.464

1.468

1.471

1.474

1.477

1.480

1.484

2.10

1.487

1.490

1.493

1.496

1.499

1.502

1.505

1.508

1.511

1.514

2.20

1.517

1.520

1.523

1.526

1.529

1.532

1.535

1.538

1.541

1.543

2.30

1.546

1.549

1.552

1.555

1.557

1.560

1.563

1.566

1.568

1.571

2.40

1.574

1.576

1.579

1.582

1. 584

1.587

1.590

1.592

1.595

1.597

2.50

1.600

1.603

1.605

1.608

1.610

1.613

1.615

1.618

1.620

1.623

2.60

1.625

1.627

1.630

1.632

1.635

1.637

1.639

1.642

1.644

1.647

2.70

1.649

1.651

1.653

1.656

1.658

1.660

1.663

1.665

1.667

1.669

2.80

1.672

1.674

1.676

1.678

1.680

1.683

1.685

1.687

1.689

1.691

2.90

1.693

1.696

1.698

1.700

1.702

1.704

1.706

1.708

1.710

1.712

3.00

1.714

1.716

1.718

1.720

1.722

1.724

1.726

1.728

1.7J0

1.732

3.10

1.734

1.736

1.738

1.740

1.742

1.744

1.746

1.748

1.750

1.752

19

WATER CONTENT

61 PERCENT

DG

1.70

1.344

1.348

1.351

1.355

1.359

1.363

1.367

1.370

1.374

1.378

1.80

1.381

1.385

1.389

1.392

1.396

1.399

1.403

1.406

1.410

1.413

1.90

1.417

1.420

1.424

1.427

1.431

1.434

1.437

1.441

1.444

1.447

2.00

1.450

1.454

1.457

1.460

1.463

1.467

1.4 70

1.473

1.476

1.479

2.10

1.482

1.485

1.488

1.491

1.494

1.498

1.501

1.504

1.506

1.509

2.20

1.512

1.515

1.518

1.521

1.524

1.527

1.530

1.533

1.535

1.538

2.30

1.541

1.544

1.547

1.549

1.552

1.555

1.557

1.560

1.563

1.566

2.40

1.568

1.571

1.573

1.576

1.579

1.581

1.534

1.586

1.589

1.592

2.50

1.594

1.597

1.599

1.602

1.604

1.607

1.609

1.611

1.614

1 .616

2.60

1.619

1.621

1.624

1.626

1.628

1.631

1.633

1.635

1.638

1.640

2.70

1.642

1.645

1.647

1.649

1.651

1.654

1.656

1.658

1.660

1.662

2.80

1.665

1.667

1.669

1.671

1.673

1.676

1.678

1.680

1.682

1.684

2.90

1.686

1.638

1.690

1.692

1.694

1.697

1.699

1.701

1.703

1.705

3.00

1.707

1.709

1.711

1.713

1.715

1.717

1.719

1.721

1.723

1.724

3.10

1.726

1.728

1.730

1.732

1.734

1.736

1.738

1.740

1.742

1.743

WATER CONTENT

62 PERCENT

DG

1.70

1.341

1.345

1.348

1.352

1.356

1.360

1.363

1.367

1.371

1.374

1.80

1.378

1.382

1.385

1.389

1.392

1.396

1.399

1.403

1.406

1.410

1.90

1.413

1.417

1.420

1.423

1.427

1.430

1.433

1.437

1.440

1.443

2.00

1.446

1.450

1.453

1.456

1.459

1.462

1.465

1.469

1.472

1.475

2.10

1.478

1.481

1.484

1.487

1.490

1.493

1.496

1.499

1.502

1.505

2.20

1.508

1.511

1.513

1.516

1.519

1.522

1.525

1.528

1.530

1.533

2.30

1.536

1. 539

1.541

1.544

1.547

1.549

1.552

1.555

1.557

1.560

2.40

1.563

1.565

1.568

1.570

1.573

1.576

1.578

1.581

1.533

1.536

2.50

1.588

1.591

1.593

1.596

1.598

1.601

1.603

1.605

1.608

1.610

2.60

1.613

1.615

1.617

1.620

1.622

1.624

1.627

1.629

1.631

1.633

2.70

1.636

1.638

1.640

1.643

1. 645

1.647

1.649

1.651

1.654

1.656

2.80

1.658

1.660

1.662

1.664

1.666

1.669

1.671

1.673

1.675

1.677

2.90

1.679

1.681

1.683

1.635

1.687

1.639

1.691

1.693

1.695

1.697

3.00

1.699

1.701

1.703

1.705

1.707

1.709

1.711

1.713

1.715

1.717

3.10

1,719

1.721

1.722

1.724

1.726

1.728

1.730

1.732

1.734

1.735

WATER CONTENT

63 PERCENT

DG

1.70

1.338

1.342

1.346

1.349

1.353

1.357

1.360

1.364

1.368

1.371

1.80

1.375

1.3 78

1.382

1.386

1.38^

1.393

1.396

1.399

1.403

1.406

1.90

1.410

1.413

1.416

1.420

1.423

1.426

1.430

1.433

1.436

1.439

2.00

1.442

1.446

1.449

1.452

1.455

1.458

1.461

1.464

1.467

1.470

2.10

1.474

1.477

1.430

1.483

1.485

1.488

1.491

1.494

1.497

1.500

2.20

1.503

1.506

1.509

1.511

1.514

1.517

1.520

1.523

1.525

1.528

2.30

1.531

1.534

1.536

1.539

1.542

1.544

1.547

1.550

1.552

1.555

2.40

1.557

1.560

1.562

1.565

1.568

1.570

1.573

1.575

1.578

1.580

2.50

1.583

1.585

1.587

1.590

1.592

1.595

1.597

1.599

1.602

1.604

2.60

1.607

1.609

1.611

1.613

1.616

1.618

1.620

1.623

1.625

1.627

2.70

1.629

1.632

1.634

1.636

1.638

1.640

1.643

1.645

1.647

1.649

2.80

1.651

1.653

1.655

1.658

1.660

1.662

1.664

1.666

1.668

1.670

2.90

1.672

1.674

1.676

1.678

1.680

1.682

1.684

1.636

1.688

1.690

3.00

1.692

1.694

1.696

1.698

1.700

1.702

1.704

1.705

1.707

1.709

3.10

1.711

1.713

t.715

1.717

1.719

1.720

1.722

1.724

1.726

1.728

20

WATER CONTENT

64 PERCENT

DG

1.70

1.335

1.339

1.343

1.346

1.350

1.354

1.357

1.361

1.365

1.368

1.80

1.372

1.375

1.379

1.382

1.386

1.389

1.393

1.396

1.399

1.403

1.90

1.406

1.409

1.413

1.416

1.419

1.423

1.426

1.429

1.432

1.435

2.00

1.439

1.442

1.445

1.448

1.451

1.454

1.457

1.460

1.463

1.466

2.10

1.469

1.472

1.475

1.478

1.481

1.484

1.487

1.490

1.493

1.496

2.20

1.498

1.501

1.504

1.507

1.510

1.512

1.515

1.518

1.520

1.523

2.30

1.526

1.529

1.531

1.534

1.537

1.539

1.542

1.544

1.547

1.549

2.40

1.552

1.555

1.557

1.560

1.562

1.565

1.567

1.570

1.572

1.574

2.50

1.577

1.579

1.582

1.584

1.587

1.589

1.591

1.594

1.596

1.598

2.60

1.601

1.603

1.605

1.607

1.610

1.612

1.614

1.617

1.619

1.621

2.70

1.623

1.625

1.628

1.630

1.632

1.634

1.636

1.638

1.640

1.643

2.80

1.645

1.647

1.649

1.651

1.653

1.655

1.657

1.659

1.661

1.663

2.90

1.665

1.667

1.669

1.671

1.673

1.675

1.677

1.679

1.681

1.683

3.00

1.685

1.687

1.689

1.691

1.693

1.694

1.696

1.698

1.700

1.702

3.10

1.704

1.706

1.707

1.709

1.711

1.713

1.715

1.716

1.718

1.720

WATER CONTENT

65 PERCENT

DG

1.70

1.333

1.336

1.340

1.344

1.347

1.351

1.354

1.358

1.362

1.365

1.80

1.369

1.37?

1.376

1.379

1.383

1.3 86

1.389

1.393

1.396

1.399

1.90

1.403

1.406

1.409

1.413

1.416

1.419

1.422

1.425

1.429

1.432

2.00

1.435

1.438

1.441

1.444

1.447

1.450

1.453

1.456

1.459

1.462

2.10

1.465

1.468

1.471

1.474

1.477

1.480

1.483

1.485

1.488

1.491

2.20

1.494

1.497

1.499

1.502

1.505

1.508

1.510

1.513

1.516

1.518

2.30

1.521

1.524

1.526

1.529

1.532

1.534

1.537

1.539

1.542

1.544

2.40

1.547

1.549

1.552

1.554

1.557

1.559

1.562

1.564

1.567

1.569

2.50

1.571

1.574

1.576

1.579

1.581

1.583

1.586

1.588

1.590

1.593

2.60

1.595

1.597

1.599

1.602

1.604

1.606

1.608

1.610

1.613

1.615

2.70

1.617

1.619

1.621

1.624

1.626

1.628

1.630

1.632

1.634

1.636

2.80

1.638

1.640

1.642

1.644

1.647

1.649

1.651

1.653

1.655

1.657

2.90

1.659

1.661

1.663

1.664

1.666

1.668

1.670

1.672

1.674

1.676

3.00

1.678

1.680

1.682

1.684

1.685

1.687

1.689

1.691

1.693

1.695

3.10

1.697

1.698

1.700

1.702

1.704

1.705

1.707

1.709

1.711

1.713

WATER CONTENT

66 PERCENT

DG

1

8

1.70 1.80 l.°0 2.00 2.10 2.20 2.30 2.40 2.50 2.60 2.70 2.80 2.90 3.00

3.10

1.330 1.366 1.399 1.431 1.461 1.489 1.516 1.542 1.566 1.589 1.611 1.632 1.652 1.671 1.689

1.3 34 1.369 1.403 1.434 1.464 1.492 1.519 1.544 1.568 1.591 1.613 1.634 1.654 1.673

1.691

1.337 1.373 1.406 1.437 1.467 1.495 1.521 1.547 1.571 1.594 1.615 1.636 1.656 1.675 1.693

1.341 1.3 76 1.409 1.440 1.470 1.498 1.524 1.549 1.573 1.596 1.617 1.638 1.658 1.677 1.695

1.344 1.379 1.412 1.443 1.473 1.500 1.527 1.552 1.575 1.598 1.620 1.640 1.660 1.679 1.697

1.348 1.383 1.415 1.446 1.475 1.503 1.529 1.554 1.578 1.600 1.622 1.642 1.662 1.680 1.698

1.352 1.386 1.419 1.449 1.478 1.506 1.532 1.556 1.580 1.602 1.624 1.644 1.664 1.682 1.700

1.355 1.389 1.422 1.452 1.481 1.508 1.534 1.559 1.582 1.605 1.626 1.646 1.665 1.684 1.702

1.359 1.393 1.425 1.455 1.484 1.511 1.537 1.561 1.585 1.607 1.628 1.648 1.667 1.686 1.703

1.362 1.396 1.428 1.458 1.487 1.514 1.539 1.564 1.587 1.609 1.630 1.650 1.669 1.688 1.705

21

WATER CONTENT

67 PERCENT

DG

1.70

1.327

1.331

1.335

1.338

1.342

1.345

1.349

1.352

1.356

1.359

1.80

1.363

1.366

1.369

1.373

1.376

1.380

1.383

1.386

1.389

1.393

1.90

1.396

1.399

1.402

1.406

1.409

1.412

1.415

1.418

1.421

1.424

2.00

1.427

1.430

1.433

1.436

1.439

1.442

1.445

1.448

1.451

1.454

2.10

1.457

1.460

1.463

1.466

1.468

1.471

1.474

1.477

1.480

1.482

2.20

1.485

1.488

1.490

1.493

1.496

1.499

1.501

1.504

1.506

1.509

2.30

1.512

1.514

1.517

1.519

1.522

1.524

1.527

1.529

1.532

1.534

2.40

1.537

1.539

1.542

1.544

1.547

1.549

1.551

1.554

1.556

1.558

2.50

1.561

1.563

1.565

1.568

1.570

1.572

1.575

1.577

1.579

1.581

2.60

1.584

1.586

1.588

1.590

1.592

1.594

1.5 97

1.599

1.601

1.603

2.70

1.605

1.607

1.609

1.612

1.614

1.616

1.618

1.620

1.622

1.624

2.80

1.626

1.628

1.630

1.632

1.634

1.636

1.638

1.640

1.642

1.644

2.90

1.646

1.648

1.649

1.651

1.653

1.655

1.657

1.659

1.661

1.663

3.00

1.664

1.666

1.668

1.670

1.672

1.674

1.675

1.677

1.679

1.681

3.10

1.682

1.684

1.686

1.688

1.689

1.691

1.693

1.695

1.696

1.698

WATER CONTENT

68 PERCENT

OG

1.70

1.325

1.328

1.332

1.335

1.339

1.342

1.346

1.349

1.353

1.356

1.80

1.360

1.363

1.366

1.370

1.373

1.376

1.380

1.383

1.386

1.389

1.90

1.393

1.396

1.399

1.402

1.405

1.408

1.412

1.415

1.418

1.421

2.00

1.424

1.427

1.430

1.433

1.436

1.439

1.442

1.444

1.447

1.450

2.10

1.453

1.456

1.459

1.462

1.464

1.467

1.470

1.473

1.475

1.478

2.20

1.481

1.483

1.486

1.489

1.491

1.494

1.497

1.499

1.502

1.504

2.30

1.507

1.510

1.512

1.515

1.517

1.520

1.522

1.525

1.527

1.529

2.40

1.532

1.534

1.537

1.539

1.542

1.544

1.546

1.549

1.551

1.553

2.50

1.556

1.558

1.560

1.562

1.565

1.567

1.569

1.571

1.574

1.576

2.60

1.578

1.580

1.582

1.585

1.587

1.589

1.591

1.593

1.595

1.597

2.70

1.599

1.602

1.604

1.606

1.608

1.610

1.612

1.614

1.616

1.618

2.80

1.620

1.622

1.624

1.626

1 .628

1.630

1.632

1.634

1.635

1.637

2.90

1.639

1.641

1.643

1.645

1.647

1.649

1.651

1.652

1.654

1.656

3.00

1.658

1.660

1.662

1.663

1.665

1.667

1.669

1.670

1.672

1.674

3.10

1.676

1.677

1.679

1.681

1.683

1.684

1.686

1.688

1.689

1.691

WATER CONTENT

69 PERCENT

DG

1.70

1.322

1.326

1.329

1.333

1.336

1.340

1.343

1.347

1.350

1.353

1.80

1.357

1.360

1.364

1.367

1.370

1.373

1.377

1.380

1.383

1.386

1.90

1.389

1.393

1.396

1.399

1.402

1.405

1.408

1.411

1.414

1.417

2.00

1.420

1.423

1.426

1.429

1.432

1.435

1.438

1.441

1.443

1.446

2.10

1.449

1.452

1.455

1.458

1 . 460

1.463

1.466

1.469

1.471

1.474

2.20

1.477

1.479

1.482

1.484

1.487

1.490

1.492

1.495

1.497

1.500

2.30

1.503

1.505

1.508

1.510

1.513

1.515

1.517

1.520

1.522

1.525

2.40

1.527

1.529

1.532

1.534

1.537

1.539

1.541

1.544

1.546

1.548

2.50

1.550

1.553

1.555

1.557

1.559

1.562

1.564

1.566

1.568

1.570

2.60

1.573

1.575

1.577

1.579

1.581

1.583

1.585

1.588

1.590

1.592

2.70

1.594

1.596

1.598

1.600

1.602

1.604

1.606

1.608

1.610

1.612

2.80

1.614

1.616

1.618

1.620

1.622

1.624

1.626

1.627

1.629

1.631

2.90

1.633

1.635

1.637

1.639

1.641

1.642

1.644

1.646

1.648

1.650

3.00

1.651

1.653

1.655

1.657

1.659

1.660

1.662

1.664

1.666

1.667

3.10

1.669

1.671

1.672

1.674

1.676

1.677

1.679

1.681

1.682

1.684

22

WATER CONTENT 70 PERCENT

DG 0123456789

1.70 1.320 1.323 1.327 1.330 1.334 1.337 1.341 1.344 1.347 1.351

1.80 1.354 1.357 1.361 1.364 1.367 1.370 1.374 1.377 1.380 1.383

1.90 1.386 1.389 1.392 1.396 1.3°Q 1.402 1.405 1.408 1.411 1.414

2.00 1.417 1.420 1.423 1.425 1.428 1.431 1.434 1.437 1.440 1.443

2.10 1.445 1.448 1.451 1.454 1.456 1.459 1.462 1.464 1.467 1.470

2.20 1.472 1.475 1.478 1.480 1.483 1.485 1.488 1.491 1.493 1.496

2.30 1.498 1.501 1.503 1.506 1.508 1.510 1.513 1.515 1.518 1.520

2.40 1.522 1.525 1.527 1.529 1.532 1.534 1.536 1.539 1.541 1.543

2.50 1.545 1.548 1.550 1.552 1.554 1.557 1.559 1.561 1.563 1.565

2.60 1.567 1.570 1.572 1.574 1.576 1.578 1.580 1.582 1.584 1.586

2.70 1.588 1.590 1.592 1.594 1.596 1.598 1.600 1.602 1.604 1.606

2.80 1.608 1.610 1.612 1.614 1.616 1.618 1.620 1.621 1.623 1.625

2.90 1.627 1.629 1.631 1.633 1.634 1.636 1.638 1.640 1.642 1.643

3.00 1.645 1.647 1.649 1.650 1.652 1.654 1.656 1.657 1.659 1.661

3.10 1.662 1.664 1.666 1.667 1.669 1.671 1.672 1.674 1.676 1.677

WATER CONTENT 71 PERCENT

DG 0123456789

1.70 1.317 1.321 1.324 1.328 1.331 1.334 1.338 1.341 1.345 1.348

1.80 1.351 1.354 1.358 1.361 1.364 1.367 1,371 1.374 1.377 1.380

1.90 1.383 1.386 1.389 1.392 1.395 1.398 1.401 1.404 1.407 1.410

2.00 1.413 1.416 1.419 1.422 1.425 1.428 1.430 1.433 1.436 1.439

2.10 1.442 1.444 1.447 1.450 1.452 1.455 1.458 1.461 1.463 1.466

2.20 1.468 1.471 1.474 1.476 1.479 1.481 1.484 1.486 1.489 1.491

2.30 1.494 1.496 1.499 1.501 1.503 1.506 1.508 1.511 1.513 1.515

2.40 1.518 1.520 1.522 1.525 1.527 1.529 1.532 1.534 1.536 1.538

2.50 1.541 1.543 1.545 1.547 1.549 1.552 1.554 1.556 1.558 1.560

2.60 1.562 1.564 1.566 1.568 1.571 1.573 1.575 1.577 1.579 1.581

2.70 1.583 1.585 1.587 1.589 1.591 1.593 1.595 1.597 1.599 1.600

2.80 1.602 1.604 1.606 1.608 1.610 1.612 1.614 1.616 1.617 1.619

2.°0 1.621 1.623 1.625 1.627 1.628 1.630 1.632 1.634 1.635 1.637

3.00 1.639 1.641 1.642 1.644 1.646 1.648 1.649 1.651 1.653 1.654

3.10 1.656 1.658 1.659 1.661 1.663 1.664 1.666 1.668 1.669 1.671

WATER CONTENT 72 PERCENT

DG 0123456789

1.70 1.315 1.318 1.322 1.325 1.328 1.332 1.335 1.339 1.342 1.345

1.80 1.348 1.352 1.355 1.358 1.361 1.364 1.368 1.371 1.374 1.377

1.90 1.380 1.383 1.386 1.389 1.392 1.395 1.398 1.401 1.404 1.407

2.00 1.410 1.413 1.416 1.418 1.421 1.424 1.427 1.430 1.432 1.435

2.10 1.438 1.441 1.443 1.446 1.449 1.451 1.454 1.457 1.459 1.462

2.20 1.464 1.467 1.470 1.472 1.475 1.477 1.480 1.482 1.485 1.487

2.30 1.489 1.492 1.494 1.497 1.499 1.501 1.504 1.506 1.509 1.511

2.40 1.513 1.516 1.518 1.520 1.522 1.525 1.527 1.529 1.531 1.534

2.50 1.536 1.538 1.540 1.542 1.544 1.547 1.549 1.551 1.553 1.555

2.60 1.557 1.559 1.561 1.563 1.565 1.567 1.569 1.571 1.573 1.575

2.70 1.577 1.579 1.581 1.583 1.585 1.587 1.589 1.591 1.593 1.595

2.80 1.597 1.599 1.601 1.602 1.604 1.606 1.608 1.610 1.612 1.613

2.90 1.615 1.617 1.619 1.621 1.622 1.624 1.626 1.628 1.629 1.631

3.00 1.633 1.635 1.636 1.638 1.640 1.641 1.643 1.645 1.646 1.648

3.10 1.650 1.651 1.653 1.655 1.656 1.658 1.659 1.661 1.663 1.664

23

WATER CONTENT

73 PERCENT

DG

1.70

1.312

1.316

1.319

1.323

1.326

1.329

1.333

1.336

1.339

1.342

1.80

1.346

1.349

1.352

1.355

1.358

1.362

1.365

1.368

1.371

1.374

1.90

1.377

1.380

1.383

1.386

1.389

1.392

1.395

1.398

1.401

1.404

2.00

1.407

1.409

1.412

1.415

1.418

1.421

1.423

1.426

1.429

1.432

2.10

1.434

1.437

1.440

1.442

1.445

1.448

1.450

1.453

1.455

1.458

2.20

1.460

1.463

1.466

1.468

1.471

1.473

1.4 76

1.478

1.480

1.483

2.30

1.485

1.488

1.490

1.492

1.495

1.497

1.499

1.502

1.504

1.506

2.40

1.509

1.511

1.513

1.516

1.518

1.520

1.522

1.524

1.527

1.529

2.50

1.531

1.533

1.535

1.537

1.540

1.542

1.544

1.546

1.548

1.550

2.60

1.552

1.554

1.556

1.558

1.560

1.562

1.564

1.566

1.568

1.570

2.70

1.572

1.5 74

1.576

1.578

1.580

1.582

1.584

1.586

1.588

1.589

2.80

1.591

1.593

1.595

1.597

1.599

1.601

1.602

1.604

1.606

1.608

2.90

1.610

1.611

1.613

1.615

1.617

1.618

1.620

1.622

1.624

1.625

3.00

1.627

1.629

1.630

1.632

1.634

1.635

1.637

1.639

1.640

1.642

3.10

1.644

1.645

1.647

1.648

1.650

1.652

1.653

1.655

1.656

1.658

WATER CONTENT

7* PERCENT

DG

1.70

1.310

1.313

1.317

1.320

1.323

1.327

1.330

1.333

1.337

1.340

1.80

1.343

1.346

1.349

1.353

1.356

1.359

1.362

1.365

1.368

1.371

1.90

1.374

1.377

1.380

1.383

1.386

1.389

1.392

1.395

1.398

1.400

2.00

1.40 3

1.406

1.409

1.412

1.414

1.417

1.420

1.423

1.425

1.428

2.10

1.431

1.433

1.436

1.439

1.441

1.444

1.446

1.449

1.452

1.454

2.20

1.457

1.45Q

1.462

1.464

1.467

1.469

1.471

1.474

1.476

1.479

2.30

1.481

1.484

1.486

1.488

1.491

1.493

1.495

1.497

1.500

1.502

2.40

1.504

1.507

1.509

1.511

1.513

1.515

1.518

1.520

1.522

1.524

2.50

1.526

1.528

1.531

1.533

1.535

1.537

1.539

1.541

1.543

1.545

2.60

1.547

1.549

1.551

1.553

1.555

1.557

1.559

1.561

1.563

1.565

2.70

1.567

1.569

1.571

1.573

1.575

1.577

1.578

1.580

1.582

1.584

2.80

1.5 86

1.588

1.590

1.591

1.593

1.595

1.597

1.599

1.600

1.602

2.90

1.604

1.606

1.607

1.609

1.611

1.613

1.614

1.616

1.618

1.619

3.00

1.621

1.623

1.624

1.626

1 .628

1.629

1.631

1.633

1.634

1.636

3.10

1.638

1.639

1.641

1.642

1.644

1.645

1.647

1.649

1.650

1.652

WATER CONTENT

75 PERCENT

DG

1.70

1.308

1.311

1.314

1.318

1.321

1.324

1.328

1.331

1.334

1.337

1.80

1.340

1.344

1.347

1.350

1.353

1.356

1.3 59

1.362

1.365

1.368

1.90

1.371

1.374

1.377

1.380

1.383

1.386

1.389

1.392

1.3 94

1.397

2.00

1.400

1.403

1.406

1.408

1.411

1.414

1.417

1.419

1.422

1.425

2.10

1.427

1.430

1.432

1.435

1.438

1.440

1.443

1.445

1.448

1.450

2.20

1.453

1.455

1.458

1.460

1.463

1.465

1.468

1.470

1.472

1.475

2.30

1.477

1.479

1.482

1.484

1.486

1.489

1.491

1.493

1.496

1.498

2.40

1.500

1.502

1.504

1.507

1.509

1.511

1.513

1.515

1.517

1.520

2.50

1.522

1.524

1.526

1.528

1.530

1.532

1.534

1.536

1.538

1.540

2.60

1.542

1.544

1.546

1.548

1.550

1.552

1.554

1.556

1.558

1.560

2.70

1.562

1.564

1. 566

1.568

1.570

1.571

1.573

1.575

1.577

1.579

2.80

1.581

1.582

1.584

1.586

1.588

1.590

1.591

1.593

1.595

1.597

2.00

1.598

1.600

1.602

1.604

1.605

1.607

1.609

1.610

1.612

1.614

3.00

1.615

1.617

1.619

1.620

1.622

1.624

1.625

1.627

1.628

1.630

3.10

1.632

1.633

1.635

1.636

1.638

1.639

1.641

1.642

1.644

1.646

24

WATER CONTENT 76 PERCENT

DG 0123456789

1.70 1.305 1.309 1.312 1.315 1.319 1.322 1.325 1.328 1.332 1.335

1.80 1.338 1.341 1.344 1.347 1.350 1.353 1.356 1.359 1.362 1.365

1.90 1.368 1.371 1.374 1.377 1.380 1.383 1.386 1.388 1.391 1.394

2.00 1.397 1.400 1.402 1.405 1.408 1.410 1.413 1.416 1.418 1.421

2.10 1.424 1.426 1.429 1.431 1.434 1.437 1.439 1.442 1.444 1.447

2.20 1.449 1.452 1.454 1.456 1.459 1.461 1.464 1.466 1.468 1.471

2.30 1.473 1.475 1.478 1.480 1.482 1.485 1.487 1.489 1.491 1.494

2.40 1.496 1.498 1.500 1.502 1.504 1.507 1.509 1.511 1.513 1.515

2.50 1.517 1.519 1.521 1.523 1.526 1.528 1.530 1.532 1.534 1.536

2.60 1.538 1.540 1.542 1.544 1.546 1.547 1.549 1.551 1.553 1.555

2.70 1.557 1.559 1.561 1.563 1.564 1.566 1.568 1.570 1.572 1.574

2.80 1.575 1.577 1.579 1.581 1.583 1.584 1.586 1.588 1.590 1.591

2.90 1.593 1.595 1.596 1.598 1.600 1.601 1.603 1.605 1.606 1.608

3.00 1.610 1.611 1.613 1.615 1.616 1.618 1.619 1.621 1.623 1.624

3.10 1.626 1.627 1.629 1.630 1.632 1.633 1.635 1.637 1.638 1.640

WATER CONTENT 77 PERCENT

DG 0123456789

1.70 1.303 1.306 1.310 1.313 1.316 1.319 1.323 1.326 1.329 1.332

1.80 1.335 1.338 1.341 1.345 1.348 1.351 1.354 1.357 1.360 1.362

1.90 1.365 1.368 1.371 1.374 1.377 1.380 1.383 1.385 1.388 1.391

2.00 1.394 1.396 1.399 1.402 1.405 1.407 1.410 1.413 1.415 1.418

2.10 1.420 1.423 1.425 1.428 1.431 1.433 1.436 1.438 1.441 1.443

2.20 1.445 1.448 1.450 1.453 1.455 1.457 1.460 1.462 1.465 1.467

2.30 1.469 1.471 1.474 1.476 1.478 1.481 1.4*3 1.435 1.487 1.489

2.40 1.492 1.494 1.496 1.4^8 1.500 1.502 1.504 1.507 1.509 1.511

2.50 1.513 1.515 1.517 1.519 1.521 1.523 1.525 1.527 1.529 1.531

2.60 1.533 1.535 1.537 1.539 1.541 1.543 1.545 1.546 1.548 1.550

2.70 1.552 1.554 1.556 1.558 1.560 1.561 1.563 1.565 1.567 1.569

2.80 1.570 1.572 1.574 1.576 1.577 1.579 1.581 1.583 1.584 1.586

2.90 1.588 1.589 1.591 1.593 1.594 1.596 1.598 1.599 1.601 1.603

3.00 1.604 1.606 1.607 1.609 1.611 1.612 1.614 1.615 1.617 1.618

3.10 1.620 1.622 1.623 1.625 1.626 1.628 1.629 1.631 1.632 1.634

WATER CONTENT 78 PERCENT

DG 0123456789

1.70 1.301 1.304 1.307 1.311 1.314 1.317 1.320 1.323 1.327 1.330

1.80 1.333 1.336 1.33° 1.342 1.345 1.348 1.351 1.354 1.357 1.360

1.90 1.363 1.365 1.368 1.371 1.374 1.377 1.380 1.382 1.385 1.388

2.00 1.391 1.3Q3 1.3<?6 1.399 1.401 1.404 1.407 1.409 1.412 1.414

2.10 1.417 1.420 1.422 1.425 1.427 1.430 1.432 1.435 1.437 1.439

2.20 1.442 1.444 1.447 1.449 1.451 1.454 1.456 1.458 1.461 1.463

2.30 1.465 1.468 1.470 1.472 1.474 1.477 1.479 1.481 1.483 1.485

2.40 1.487 1.490 1.492 1.494 1.496 1.498 1.500 1.502 1.504 1.506

2.50 1.508 1.511 1.513 1.515 1.517 1.519 1.521 1.523 1.524 1.526

2.60 1.528 1.530 1.532 1.534 1.536 1.538 1.540 1.542 1.544 1.545

2.70 1.547 1.549 1.551 1.553 1.555 1.556 1.558 1.560 1.562 1.564

2.80 1.565 1.567 1.569 1.571 1.572 1.574 1.576 1.577 1.579 1.581

2.90 1.582 1.584 1.586 1.587 1.589 1.591 1.592 1.59% 1.596 1.597

3.00 1.599 1.600 1.602 1.604 1.605 1.607 1.608 1.610 1.611 1.619

3.10 1.614 1.616 1.617 1.619 1.620 1.622 1.623 1.625 1.626 1.628

25

WATER CONTENT 79 PERCENT DG 0 1 2

1.70

1.299

1.302

1.305

1.308

1. 312

1.315

1.318

1.321

1.324

1.327

1.80

1.330

1.333

1.336

1.339

1.342

1.345

1.348

1.351

1.354

1.357

1.90

1.360

1.363

1.366

1.368

1.371

1.374

1.377

1.379

1.382

1.385

2.00

1.388

1.390

1.393

1.396

1.398

1.401

1.403

1.406

1.409

1.411

2.10

1.414

1.416

1.419

1.421

1.424

1.426

1.429

1.431

1.433

1.436

2.20

1.438

1.441

1.443

1.445

1.448

1.450

1.452

1.455

1.457

1.459

2.30

1.461

1.464

1.466

1.468

1.470

1.473

1.475

1.477

1.479

1.481

2.40

1.483

1.486

1.488

1.490

1.492

1.494

1.496

1.498

1.500

1.502

2.50

1.504

1.506

1.508

1.510

1.512

1.514

1.516

1.518

1.520

1.522

2.60

1.524

1.526

1.528

1.530

1.532

1.533

1.535

1.537

1.539

1.541

2.70

1.543

1.544

1.546

1.548

1.550

1.552

1.553

1.555

1.557

1.559

2.80

1.560

1.562

1.564

1.5 66

1.567

1.569

1.571

1.572

1.574

1.576

2.90

1.577

1.579

1.581

1.582

1.584

1.585

1.587

1.589

1.590

1.592

3.00

1.593

1.595

1.597

1.598

1.600

1.601

1.603

1.604

1.606

1.607

3.10

1.609

1.610

1.612

1.613

1.615

1.616

1.618

1.619

1.621

1.622

WATER CONTENT 80 PERCENT

OG 0123456789

1.70 1.297 1.300 1.303 1.306 1.309 1.312 1.316 1.319 1.322 1.325

1.80 1.328 1.331 1.334 1.337 1.340 1.343 1.346 1.349 1.351 1.354

1.90 1.357 1.360 1.363 1.366 1.368 1.371 1.374 1.377 1.379 1.382

2.00 1.385 1.387 1.390 1.393 1.395 1.398 1.400 1.403 1.405 1.408

2.10 1.410 1.413 1.415 1.418 1.420 1.423 1.425 1.428 1.430 1.432

2.20 1.435 1.437 1.439 1.442 1.444 1.446 1.449 1.451 1.453 1.456

2.30 1.458 1.460 1.462 1.464 1.467 1.469 1.471 1.473 1.475 1.477

2.40 1.479 1.482 1.484 1.486 1.488 1.490 1.492 1.494 1.496 1.498

2.50 1.500 1.502 1.504 1.506 1.508 1.510 1.512 1.514 1.516 1.518

2.60 1.519 1.521 1.523 1.525 1.527 1.529 1.531 1.533 1.534 1.536

2.70 1.538 1.540 1.542 1.543 1.545 1.547 1.549 1.550 1.552 1.554

2.80 1.556 1.557 1.559 1.561 1.562 1.564 1.566 1.567 1.569 1.571

2.90 1.572 1.574 1.576 1.577 1.579 1.580 1.582 1.584 1.585 1.587

3.00 1.588 1.590 1.591 l.5°3 1.594 1.596 1.597 1.599 1.600 1.602

3.10 1.603 1.605 1.606 1.608 1.609 1.611 1.612 1.614 1.615 1.617

WATER CONTENT 81 PERCENT

OG 0123456789

1.70 1.294 1.298 1.301 1.304 1.307 1.310 1.313 1.316 1.319 1.322

1.80 1.325 1.328 1.331 1.334 1.337 1.340 1.343 1.346 1.349 1.352

1.90 1.354 1.357 1.360 1.363 1.366 1.368 1.371 1.374 1.376 1.379

2.00 1.382 1.384 1.387 1.390 1.392 1.395 1.397 1.400 1.402 1.405

2.10 1.407 1.410 1.412 1.415 1.417 1.419 1.422 1.424 1.427 1.429

2.20 1.431 1.434 1.436 1.438 1.441 1.443 1.445 1.447 1.450 1.452

2.30 1.454 1.456 1.458 1.461 1.463 1.465 1.467 1.469 1.471 1.473

2.40 1.476 1.478 1.480 1.482 1.484 1.486 1.488 1.490 1.492 1.494

2.50 1.496 1.498 1.500 1.502 1.504 1.506 1.508 1.509 1.511 1.513

2.60 1.515 1.517 1.519 1.521 1.523 1.524 1.526 1.528 1.530 1.532

2.70 1.533 1.535 1.537 1.539 1.540 1.542 1.544 1.546 1.547 1.549

2.80 1.551 1.552 1.554 1.556 1.558 1.559 1.561 1.562 1.564 1.566

2.90 1.567 1.569 1.571 1.572 1.574 1.575 1.577 i.578 1.580 1.582

3.00 1.583 1.585 1.586 1.588 1.589 1.591 1.592 1.594 1.595 1.597

3.10 1.598 1.600 1.601 i.602 1.604 1.605 1.607 1.608 1.610 1.611

26

WATER CONTENT

82 PERCENT

DG

1.70

1.292

1.296

1.299

1.302

1.305

1.308

1.311

1.314

1.317

1.320

1.80

1.323

1.326

1.329

1.332

1.335

1.338

1.341

1.343

1.346

1.349

l.°0

1.352

1.355

1.357

1.360

1.363

1.366

1.368

1.371

1.374

1.376

2.00

1.379

1.381

1.384

1.387

1.389

1.392

1.394

1.397

1.399

1.402

2.10

1.404

1.407

1.409

1.411

1.414

1.416

1.419

1.421

1.423

1.426

2.20

1.428

1.430

1.433

1.435

1.437

1.439

1.442

1.444

1.446

1.448

2.30

1.450

1.453

1.455

1.457

1.459

1.461

1.463

1.465

1.468

1.470

2.40

1.472

1.474

1.476

1.478

1.480

1.482

1.484

1.486

1.488

1.490

2.50

1.492

1.4<?4

1.496

1.498

1.500

1.501

1.503

1.505

1.507

1.509

2.60

1.511

1.513

1.515

1.516

1.518

1.520

1.522

1.524

1.525

1.527

2.70

1.529

1.531

1.532

1.534

1. 536

1.538

1.539

1.541

1.543

1.544

2.80

1.546

1.548

1.549

1.551

1.553

1.554

1.556

1.558

1.559

1.561

2.90

1.562

1.564

1.566

1.567

1.569

1.570

1.572

1.573

1.575

1.577

3.00

1.578

1.580

1.581

1.583

1.584

1.5 86

1.587

1.589

1.590

1.591

3.10

1.503

1.504

1.596

1.597

1.599

1.600

1.601

1.603

1.604

1.606

WATER CONTENT

83 PERCENT

DG

1.70

1.290

1.293

1.297

1.300

1.303

1.306

1.309

1.312

1.315

1.318

1.80

1.321

1.324

1.327

1.330

1.332

1.335

1.338

1.341

1.344

1.346

I. <»0

1.349

1.352

1.355

1.357

1.360

1.363

1.365

1.368

1.371

1.373

2.00

1.376

1.379

1.381

1.384

1.386

1.389

1.391

1.394

1.396

1.399

2.10

1.401

1.403

1.406

1.408

1.411

1.413

1.415

1.418

1.420

1.422

2.20

1.425

1.427

1.429

1.431

1.434

1.436

1.438

1.440

1.443

1.445

2.30

1.447

1.449

1.451

1.453

1.455

1.458

1.460

1.462

1.464

1.466

2.40

1.468

1.470

1.472

1.474

1.476

1.478

1.4 30

1.482

1.484

1.486

2.50

1.488

1.490

1.492

1.494

1.495

1.497

1.499

1.501

1.503

1.505

2.60

1.507

1.508

1.510

1.512

1.514

1.516

1.517

1.519

1.521

1.523

2.70

1.525

1.526

1.528

1.530

1.531

1.533

1.535

1.537

1.538

1.540

2.80

1.542

1.543

1.545

1.546

1.548

1.550

1.551

1.553

1.555

1.556

2.90

1.558

1.559

1.561

1.562

1.564

1.565

1.567

1.569

1.570

1.572

3.00

1.573

1.575

1.576

1.578

1.579

1.580

1.582

1.583

1.585

1.586

3.10

1.588

1.589

1.591

1.592

1.593

1.595

1.596

1.598

1.599

1.600

WATER CONTENT

84 PERCENT

DG

1.70

1.288

1.291

1.295

1.298

1.301

1.304

1.307

1.310

1.313

1.316

1.80

1.318

1.321

1.324

1.327

1.330

1.333

1.3 36

1.338

1.341

1.344

1.90

1.347

1.349

1.352

1.355

1.357

1.360

1.363

1.365

1.368

1.371

2.00

1.373

1.376

1.378

1.381

1. 383

1.386

1.388

1.391

1.393

1.396

2.10

1.398

1.400

1.403

1.405

1.407

1.410

1.412

1.414

1.417

1.419

2.20

1.421

1.424

1.426

1.428

1.430

1.433

1.435

1.437

1.439

1.441

2.30

1.443

1.446

1.448

1.450

1.452

1.454

1.456

1.458

1.460

1.462

2.40

1.464

1.466

1.468

1.470

1.472

1.474

1.476

1.478

1.480

1.482

2.50

1.484

1.486

1.488

1.490

1.491

1.493

1.495

1.497

1.499

1.501

2.60

1.503

1.504

1.506

1.508

1.510

1.511

1.513

1.515

1.517

1.518

2.70

1.520

1.522

1.524

1.525

1.527

1.529

1.530

1.532

1.534

1.535

2.80

1.537

1.539

1.540

1.542

1.543

1.545

1.547

1.548

1.550

1.551

2.90

1.553

1.555

1.556

1.558

1.559

1.561

1.562

1.564

1.565

1.567

3.00

1.568

1.570

i.571

1.573

1.574

1.576

1.577

1.578

1.580

1.581

3.10

1.583

1.584

1.586

1.587

1.588

1.590

1.591

1.592

1.594

1.595

27

WATER CONTENT

85 PERCENT

DG

1.70

1.286

1.289

1.292

1.295

1.299

1.302

1.304

1.307

1.310

1.313

1.80

1.316

1.31-9

1.322

1.325

1.328

1.330

1.333

1.336

1.339

1.341

1.90

1.344

1.347

1.350

1.352

1.355

1.357

1.360

1.36 3

1.365

1.368

2.00

1.370

1.373

1.375

1.378

1.380

1.333

1.385

1.388

1.390

1.393

2.10

1.395

1.397

1.400

1.402

1.404

1.407

1.409

1.411

1.414

1.416

2.20

1.418

1.420

1.423

1.425

1.427

1.429

1.431

1.434

1.436

1.438

2.30

1.440

1.442

1.444

1.446

1.448

1.450

1.452

1.454

1.457

1.459

2.40

1.461

1.463

1.465

1.466

1.468

1.470

1.472

1.474

1.476

1.478

2.50

1.480

1.482

1.484

1.486

1.487

1.489

1.491

1.49 3

1.495

1.497

2.60

1.498

1.500

1.502

1.504

1.506

1.507

1.5 09

1.511

1.513

1.514

2.70

1.516

1.518

1.519

1.521

1.523

1.524

1.526

1.528

1.529

1.531

2.80

1.533

1.534

1.536

1.537

1.539

1.541

1.542

1.544

1.545

1.547

2.90

1.548

1.550

1.551

1.553

1.554

1.556

1.557

1.559

1.560

1.562

3.00

1.563

1.565

1.566

1.568

1.569

1.571

1.572

1.573

1.575

1.576

3.10

1.578

1.579

1.581

1.582

1.583

1.585

1.586

1.587

1.589

1.590

WATER CONTENT

86 PERCENT

PG

1.70

1.284

1.287

1.290

1.293

1.206

1.299

1.302

1.305

1.308

1.311

1.80

1.314

1.317

1.320

1.322

1.325

1.328

1.331

1.334

1.336

1.339

1.90

1.342

1.344

1.347

1.350

1.352

1.355

1.357

1.360

1.363

1.365

2.00

1.368

1.370

1.373

1.375

1.378

1.380

1.382

1.385

1.387

1.390

2.10

1.392

1.394

1.397

1.399

1.401

1.404

1.406

1.408

1.410

1.413

2.20

1.415

1.417

1.419

1.422

1.424

1.426

1.428

1.430

1.432

1.434

2.30

1.437

1.439

1.441

1.443

1.445

1.447

1.449

1.451

1.453

1.455

2.40

1.457

1.459

1.461

1.463

1.465

1.467

1.469

1.471

1.472

1.474

2.50

1.476

1.478

1.480

1.482

1.484

1.485

1.487

1.489

1.491

1.493

2.60

1.494

1.496

1.498

1.500

1.501

1.503

1.505

1.507

1.508

1.510

2.70

1.512

1.513

1.515

1.517

1.518

1.520

1.522

1.523

1.525

1.527

2.80

1.528

1.530

1.531

1.533

1.535

1.536

1.538

1.539

1.541

1.542

2.90

1.544

1.545

1.547

1.548

1.550

1.551

1.553

1.554

1.556

1.557

3.00

1.559

1.560

1.562

1.563

1.564

1.566

1.567

1.569

1.570

1.571

3.10

1.573

1.574

1.576

1.577

1.578

1.580

1.581

1.582

1.584

1.585

WATER CONTENT

87 PERCENT

DG

1.70

1.282

1.285

1.288

1.291

1.294

1.297

1.300

1.303

1.306

1.309

1.80

1.312

1.315

1.317

1.320

1.323

1.326

1.328

1.331

1.334

1.337

1.90

1.339

1.342

1.345

1.347

1.350

1.352

1.355

1.357

1.360

1.362

2.00

1.365

1.367

1.370

1.372

1.375

1.377

1.380

1.382

1.384

1.387

2.10

1.389

1.391

1.394

1.396

1.398

1.401

1.403

1.405

1.407

1.410

2.20

1.412

1.414

1.416

1.418

1.421

1.423

1.425

1.427

1.429

1.431

2.30

1.433

1.435

1.437

1.439

1.441

1.443

1.445

1.447

1.449

1.451

2.40

1.453

1.455

1.457

1.459

1.461

1.463

1.465

1.467

1.469

1.471

2.50

1.472

1.474

1.476

1.478

1.480

1.482

1.483

1.485

1.487

1.489

2.60

1.490

1.492

1.494

1.496

1.497

1.499

1.501

1.503

1.504

1.506

2.70

1.508

1.509

1.511

1.513

1.514

1.516

1.517

1.519

1.521

1.522

2.80

1.524

1.525

1.527

1.529

1.530

1.532

1.533

1.535

1.536

1.538

2.90

1.539

1.541

1.542

1.544

1.545

1.547

1.548

1.550

1.551

1.553

3.00

1.554

1.555

1.557

1.558

1.560

1.561

1.563

1.564

1.565

1.567

3.10

1.568

1.569

1.571

1.572

1.573

1.575

1.576

1.577

1.579

1.580

28

WATER CONTFNT

88 PERCENT

DG

1.70

1.280

1.283

1.286

1.289

1.292

1.295

1.298

1.301

1.304

1.307

1.80

1.310

1.312

1.315

1.318

1.321

1.323

1.326

1.329

1.332

1.334

1.90

1.337

1.339

1.342

1.345

1.347

1.350

1.352

1.355

1.357

1.360

2.00

1.362

1.365

1.367

1.370

1.372

1.374

1.377

1.379

1.382

1.384

2.10

1.3P6

1.389

1.391

1.393

1.395

1.308

1.400

1.402

1.404

1.407

2.20

1.409

1.411

1.413

1.415

1.417

1.419

1.422

1.424

1.426

1.428

2.30

1.430

1.432

1.434

1.436

1.438

1.440

1.442

1.444

1.446

1.448

2.40

1.450

1.452

1.454

1.456

1.458

1.459

1.461

1.463

1.465

1.467

2.50

1.469

1.471

1.472

1.474

1.476

1.478

1.480

1.481

1.483

1.485

2.60

1.487

1.488

1.490

1.492

1.494

1.495

1.497

1.499

1.500

1.502

2.70

1.504

1.505

1.507

1.508

1.510

1.512

1.513

1.515

1.516

1.518

2.80

1.520

1.521

1.523

1.524

1.526

1.527

1.529

1.530

1.532

1.533

2.90

1.535

1.536

1.538

1.539

1.541

1.542

1.544

1.545

1.547

1.548

3.00

1.549

1.551

1.552

1.554

1.555

1.556

1.558

1.559

1.561

1.562

3.10

1.563

1.565

1.566

1.567

1.569

1.570

1.571

1.573

1.574

1.575

HATER CONTENT

89 PERCENT

DG

1.70

1.279

1.282

1.284

1.287

1.290

1.2Q3

1.296

1.299

1.302

1.305

1.80

1.307

1.310

1.313

1.316

1.318

1.321

1*324

1.327

1.329

1.332

1.90

1.334

1.3 37

1.340

1.342

1.345

1.347

1.350

1.352

1.355

1.357

2.00

1.360

1.362

1.365

1.367

1.369

1.372

1.374

1.376

1.379

1.381

2.10

1.38 3

1.386

1.388

1.390

1.392

1.395

1.397

1.399

1.401

1.404

2.20

1.406

1.408

1.410

1.412

1.414

1.416

1.418

1.420

1.423

1.425

2.30

1.427

1.429

1.431

1.433

1.435

1.437

1.439

1.441

1.443

1.445

2.40

1.446

1.448

1.450

1.452

1.454

1.456

1.458

1.460

1.461

1.463

2.50

1.465

1.467

1.469

1.471

1.472

1.474

1.476

1.478

1.479

1.481

2.60

1.483

1.485

1.486

1.488

1.490

1.491

1.493

1.495

1.496

1.498

2.70

1.500

1.501

1.503

1.504

1. 506

1.508

1.509

1.511

1.512

1.514

2.80

1.515

1.517

1.519

1.520

1.522

1.523

1.525

1.526

1.528

1.529

2.90

1.531

1.532

1.534

1.535

1. 536

1.538

1.539

1.541

1.542

1.544

3.00

1.545

1.546

1.548

1.549

1.551

1.552

1.553

1.555

1.556

1.557

3.10

1.559

1.560

1.561

1.563

1.564

1.565

1.567

1.568

1.569

1.570

WATER CONTENT

90 PERCENT

DG

8

1.70 1.30 1.90 2.00 2.10 2.20 2.30 2.40 2.50 2.60 2.70 2.80 2.90 3.00 3.10

1.277 1.305 1.332 1.357 1.381 1.403 1.423 1.443 1.462 1.479 1.496 1.511 1.526 1.541 1.554

1.280 1.308 1.335 1.360 1.383 1.405 1.425 1.445 1.463 1.481 1.497 1.513 1.528 1.542 1.555

1.283 1.311 1.337 1.362 1.385 1.407 1.427 1.447 1.465 1.482 1.499 1.514 1.529 1.543 1.557

1.285 1.314 1.340 1.364 1.387 1.409 1.429 1.449 1.467 1.484 1.500 1.516 1.531 1.545 1.558

1.288 1.316 1.342 1.367 1.390 1.411 1.431 1.451 1.469 1.486 1.502 1.517 1.532 1.546 1.559

1.291 1.319 1.345 1.369 1.392 1.413 1.433 1.452 1.470 1.487 1.504 1.519 1.534 1.547 1.561

1.2 94 1.322 1.347 1.371 1.394 1.415 1.435 1.454 1.472 1.489 1.505 1.520 1.535 1.549 1.562

1.297 1.324 1.350 1.374 1.396 1.417 1.437 1.456 1.474 1.491 1.507 1.522 1.536 1.550 1.563

1.300 1.327 1.352 1.376 1.398 1.419 1.439 1.458 1.476 1.492 1.508 1.523 1.538 1.551 1.564

1.303 1.330 1.355 1.378 1.401 1.421 1.441 1.460 1.477 1.494 1.510 1.525 1.539 1.553 1.564

29

WATER CONTENT 91 PERCENT

DG 0123456789

1.70 1.275 1.278 1.281 1.284 1.286 1.289 1.292 1.295 1.298 1.301

1.80 1.303 1.306 1.309 1.311 1.314 1.317 1.319 1.322 1.325 1.327

1.90 1.330 1.332 1.335 1.337 1.340 1.342 1.345 1.347 1.350 1.352

2.00 1.355 1.357 1.359 1.362 1.364 1.366 1.369 1.371 1.373 1.376

2.10 1.378 1.380 1.382 1.385 1.387 1.389 1.391 1.393 1.395 1.398

2.20 1.400 1.402 1.404 1.406 1.408 1.410 1.412 1.414 1.416 1.418

2.30 1.420 1.422 1.424 1.426 1.428 1.430 1.432 1.434 1.436 1.438

2.40 1.440 1.442 1.443 1.445 1.447 1.449 1.451 1.453 1.454 1.456

2.50 1.458 1.460 1.462 1.463 1.465 1.467 1.469 1.470 1.472 1.474

2.60 1.475 1.477 1.479 1.480 1.482 1.484 1.485 1.487 1.489 1.490

2.70 1.492 1.493 1.495 1.497 1.498 1.500 1.501 1.503 1.504 1.506

2.80 1.507 1.509 1.510 1.512 1.513 1.515 1.516 1.518 1.519 1.521

2.90 1.522 1.524 1.525 1.526 1.528 1.529 1.531 1.532 1.533 1.535

3.00 1.536 1.538 1.539 1.540 1.542 1.543 1.544 1.546 1.547 1.548

3.10 1.550 1.551 1.552 1.553 1.555 1.556 1.557 1.559 1.560 1.561

WATER CONTENT 92 PERCENT

DG 0123456789

1.70 1.273 1.276 1.279 1.282 1.285 1.287 1.290 1.293 1.296 1.298

1.80 1.301 1.304 1.307 1.309 1.312 1.315 1.317 1.320 1.322 1.325

1.90 1.328 1.330 1.333 1.335 1.338 1.340 1.342 1.345 1.347 1.350

2.00 1.352 1.354 1.357 1.359 1.362 1.364 1.366 1.368 1.371 1.373

2.10 1.375 1.377 1.380 1.382 1.384 1.386 1.388 1.390 1.393 1.395

2.20 1.397 1.399 1.401 1.403 1.405 1.407 1.409 1.411 1.413 1.415

2.30 1.417 1.419 1.421 1.423 1.425 1.427 1.429 1.431 1.433 1.435

2.40 1.436 1.438 1.440 1.442 1.444 1.446 1.447 1.449 1.451 1.453

2.50 1.455 1.456 1.458 1.460 1.462 1.463 1.465 1.467 1.468 1.470

2.60 1.472 1.473 1.475 1.477 1.478 1.480 1.482 1.483 1.485 1.486

2.70 1.488 1.490 1.491 1.493 1.494 1.496 1.497 1.499 1.500 1.502

2.80 1.503 1.505 1.506 1.508 1.509 1.511 1.512 1.514 1.515 1.517

2.90 1.518 1.519 1.521 1.522 1.524 1.525 1.526 1.528 1.529 1.531

3.00 1.532 1.533 1.535 1.536 1.537 1.539 1.540 1.541 1.543 1.544

3.10 1.545 1.546 1.548 1.549 1.550 1.552 1.553 1.554 1.555 1.557

WATER CONTENT 93 PERCENT

DG 0123456789

1.70 1.271 1.274 1.277 1.280 1.283 1.285 1.288 1.291 1.294 1.296

1.80 1.299 1.302 1.305 1.307 1.310 1.312 1.315 1.318 1.320 1.323

1.90 1.325 1.328 1.330 1.333 1.335 1.333 1.340 1.343 1.345 1.347

2.00 1.350 1.352 1.354 1.357 1.359 1.361 1.364 1.366 1.368 1.370

2.10 1.373 1.375 1.377 1.379 1.381 1.383 1.386 1.388 1.390 1.392

2.20 1.394 1.396 1.398 1.400 1.402 1.404 1.406 1.408 1.410 1.412

2.30 1.414 1.416 1.418 1.420 1.422 1.424 1.426 1.428 1.429 1.431

2.40 1.433 1.435 1.437 1.439 1.440 1.442 1.444 1.446 1.448 1.449

2.50 1.451 1.453 1.455 1.456 1.458 1.460 1.461 1.463 1.465 1.466

2.60 1.468 1.470 1.471 1.473 1.475 1.476 1.478 1.479 1.481 1.483

2.70 1.484 1.486 1.487 1.489 1.490 1.492 1.493 1.495 1.496 1.498

2.30 1.499 1.501 1.502 1.504 1.505 1.507 1.508 1.510 1.511 1.513

2.90 1.514 1.515 1.517 1.518 1.520 1.521 1.522 1.524 1.525 1.526

J. 00 1.528 1.529 1.530 1.532 1.533 1.534 1.536 1.537 1.538 1.540

3.10 1,541 1.542 1.543 1.545 1.546 1.547 1.548 1.550 1.551 1.552

30

WATER CONTENT

94 PERCENT

DG

1.70

1.269

1.272

1.275

1.278

1.281

1.284

1.286

1.289

1.292

1.294

1.80

1.297

1.300

1.302

1.305

1.308

1.310

1.313

1.315

1.318

1.321

l.Q0

1.323

1.326

1.328

1.330

1.333

1.335

1.338

1.340

1.343

1.345

2.00

1.347

1.350

1.352

1.354

1.356

1.359

1.361

1.363

1.365

1.368

2.10

1.370

1.372

1.374

1.376

1. 3 79

1.381

1.383

1.385

1.387

1.389

2.20

1.391

1.393

1.395

1.397

1.399

1.401

1.403

1.405

1.407

1.409

2.30

1.411

1.413

1.415

1.417

1.419

1.421

1.423

1.424

1.426

1.428

2.40

1.430

1.432

1.434

1.435

1.437

1.439

1.441

1.443

1.444

1.446

2.50

1.448

1.449

1.451

1.453

1.455

1.456

1.458

1.460

1.461

1.463

2.60

1.465

1.466

1.468

1.469

1.471

1.473

1.474

1.476

1.477

1.479

2.70

1.480

1.482

1.484

1.4«5

1.487

1.483

1.490

1.491

1.493

1.494

2.80

1.496

1.497

1.499

1.500

1.501

1.503

1.5 04

1.506

1.507

1.509

2.90

1.510

1.511

1.513

1.514

1.515

1.517

1.518

1.520

1.521

1.522

3.00

1.5 24

1.525

1.526

1.528

1.529

1.530

1.531

1.533

1.534

1.535

3.10

1.537

1.538

1.539

1.540

1.542

1.543

1.544

1.545

1.546

1.543

WATER CONTENT

95 PERCENT

DG

1.70

1.268

1.271

1.273

1.276

1.2 79

1.282

1.284

1.287

1.290

1.293

1.90

1.295

1.298

1.300

1.303

1.306

1.308

1.311

1.313

1.316

1.318

1.90

1.321

1.323

1.326

1.328

1.331

1.333

1.335

1.338

1.340

1.343

2.00

1.345

1.347

1.349

1.352

1.354

1.356

1.358

1.361

1.363

1.365

2.10

1.367

1.369

1.372

1.374

1.376

1.378

1.380

1.382

1.384

1.386

2.20

1.388

1.390

1.392

1.394

1.396

1.398

1.400

1.402

1.404

1.406

2.30

1.409

1.410

1.412

1.414

1.416

1.418

1.419

1.421

1.423

1.425

2.40

1.427

1.429

1.430

1.432

1.434

1.436

1.438

1.439

1.441

1.443

2.50

1.444

1.446

1.448

1.450

1.451

1.453

1.455

1.456

1.459

1.459

2.60

1.461

1.463

1.464

1.466

1.468

1.469

1.471

1.472

1.474

1.475

2.70

1.477

1.478

1.480

1.431

1.483

1.484

1.486

1.487

1.489

1.490

2.80

1.492

1.493

1.4^5

1.496

1.498

1.499

1.500

1.502

1.503

1.505

2.90

1.506

1.507

1.509

1.510

1.511

1.513

1.514

1.516

1.517

1.519

3.00

1.519

1.521

1.522

1.523

1.525

1.526

1.527

1.529

1.530

1.531

3.10

1.532

1.534

1.535

1.536

1.537

1.539

1.540

1.541

1.542

1.543

WATER CONTENT

96 PERCENT

DG

1.70

1.266

1.269

1.272

1.2 74

1.277

1.280

1.283

1.285

1.288

1.291

1.80

1.293

1.296

1.298

1.301

1.304

1.306

1.309

1.311

1.314

1.316

1.90

1.319

1.321

1.324

1.326

1.328

1.331

1.333

1.335

1.338

1.340

2.00

1.342

1.345

1.347

1.349

1.352

1.354

1.356

1.358

1.360

1.363

2.10

1.365

1.367

1.369

1.371

1.373

1.375

1.377

1.379

1.382

1.384

2.20

1.386

1.388

1.390

1.392

1.394

1.396

1.398

1.399

1.401

1.403

2.30

1.405

1.407

1.409

1.411

1.413

1.415

1.416

1.418

1.420

1.422

2.40

1.424

1.426

1.427

1.429

1.431

1.433

1.434

1.436

1.439

1.439

2.50

1.441

1.443

1.445

1.446

1.448

1.450

1.451

1.453

1.454

1.456

2.60

1.458

1.459

1.461

1.462

1.464

1.466

1.467

1.469

1.470

1.472

2.70

1.473

1.475

1.476

1.478

1.47°

1.481

1.482

1.484

1.485

1.487

2.30

1.488

1.490

1.40 1

1.4P2

1.494

1.495

1.497

1.498

1.499

1.501

2.90

1.502

1.503

1.505

1.506

1.508

1.509

1.510

1.512

1.513

1.514

3.00

1.515

1.517

1.518

1.519

1.521

1.522

1.523

1.524

1.526

1.527

3.10

1.528

1.529

1.531

1.532

1.533

1.534

1.535

1.537

1.538

1.539

31

WATER CONTENT

97 PERCENT

DG

1.70

1.264

1.267

1.270

1.273

1.275

1.278

1.281

1.283

1.286

1.289

1.80

1.2<U

1.294

1.297

1.299

1. 302

1.304

1.307

1.309

1.312

1.314

1.90

1.317

1.319

1.321

1.324

1.326

1.329

1.331

1.333

1.336

1.338

2.00

1.340

1.342

1.345

1.347

1.349

1.351

1.354

1.356

1.358

1.360

2.10

1.362

1.364

1.366

1.369

1.371

1.373

1.375

1.377

1.379

1.381

2.20

1.383

1.3 85

1.387

1.389

1.391

1.393

1.395

1.397

1.399

1.400

2.30

1.402

1.404

1.406

1.408

1.410

1.412

1.413

1.415

1.417

1.419

2.40

1.421

1.422

1.424

1.426

1.428

1.429

1.431

1.433

1.435

1.436

2.50

1.438

1.440

1.441

1.443

1.445

1.446

1.448

1.449

1.451

1.453

2.60

1.454

1.456

1.457

1.459

1.461

1.462

1.464

1.465

1.467

1.468

2.70

1.470

1.471

1.473

1.474

1.476

1.477

1.4 79

1.480

1.482

1.48 3

2.80

1.484

1.486

1.487

1.489

1.490

1.491

1.493

1.494

1.496

1.497

2.90

1.498

1.500

1.501

1.502

1.504

1.505

1.506

1.508

1.509

1.510

3.00

1.512

1.513

1.514

1.515

1.517

1.518

1.519

1.520

1.522

1.523

3.10

1.524

1.525

1.527

1.528

1.529

1.530

1.531

1.533

1.534

1.535

WATER CONTENT

98 PERCENT

DG

1.70

1.263

1.265

1.268

1.271

1.274

1.276

1.2 79

1.282

1.234

1.287

1.80

1.289

1.292

1.295

1.297

1.300

1.302

1.305

1.307

1.310

1.312

1.90

1.314

1.317

1.319

1.322

1.324

1.326

1.329

1.331

1.333

1.336

2.00

1.338

1.340

1.342

1.345

1.347

1.349

1.351

1.353

1.355

1.358

2.10

1.360

1.362

1.364

1.3 66

1.368

1.370

1.372

1.374

1.376

1.378

2.20

1.380

1.382

1.384

1.386

1.388

1.390

1.392

1.394

1.396

1.398

2.30

1.400

1.401

1.403

1.405

1.407

1.409

1.411

1.412

1.414

1.416

2.40

1.418

1.419

1.421

1.423

1.425

1.426

1.428

1.430

1.431

1.433

2.50

1.435

1.436

1.438

1.440

1.441

1.443

1.445

1.446

1.448

1.449

2.60

1.451

1.453

1.454

1.456

1.457

1.459

1.460

1.462

1.463

1.465

2.70

1.466

1.468

1.469

1.471

1.472

1.474

1.475

1.476

1.478

1.479

2.30

1.481

1.482

1.484

1.485

1.486

1.488

1.489

1.490

1.492

1.493

2.90

1.495

1.496

1.497

1.499

1.500

1.501

1.502

1.504

1.505

1.506

3.00

1.508

1.509

1.510

1.511

1.513

1.514

1.515

1.516

1.518

1.519

3.10

1.520

1.521

1.522

1.524

1.525

1.526

1.527

1.528

1.530

1.531

WATER CONTENT

99 PERCENT

DG

1.70

1.261

1.264

1.266

1.269

1.272

1.274

1.277

1.280

1.282

1.285

1.80

1.288

1.290

1.293

1.295

1.298

1.300

1.303

1.305

1.308

1.310

1.90

1.312

1.315

1.317

1.320

1.322

1.324

1.326

1.329

1.331

1.333

2.00

1.336

1.338

1.340

1. 342

1.344

1.347

1.349

1.351

1.353

1.355

2.10

1.357

1.359

1.361

1.363

1.366

1.368

1.370

1.372

1.374

1.376

2.20

1.378

1.380

1.382

1.383

1.385

1.387

1.389

1.391

1.393

1.395

2.30

1.397

1.399

1.400

1.402

1.404

1.406

1.408

1.409

1.411

1.413

2.40

1.415

1.416

1.418

1.420

1.422

1.423

1.425

1.427

1.423

1.430

2.50

1.432

1.433

1.435

1.437

1.438

1.440

1.441

1.443

1.445

1.446

2.60

1.448

1.449

1.451

1.452

1.454

1.455

1.457

1.458

1.460

1.461

2.70

1.463

1.464

1.466

1.467

1.469

1.470

1.472

1.473

1.474

1.476

2.80

1.477

1.479

1.480

1.481

1.483

1.484

1.485

1.487

1.488

1.489

2.90

1.491

1.492

1.493

1.495

1.496

1.497

1.499

1.500

1.501

1.503

3.00

1.504

1.505

1.506

1.508

1.509

1.510

1.511

1.512

1.514

1.515

3.10

1.516

1.517

1.518

1.520

1.521

1.522

1.523

1.524

1.526

1.527

32

WATER CONTENT 100 PERCENT

OG

1.70

1.259

1.262

1.265

1.267

1.270

1.273

1.275

1.278

1.281

1.283

1.80

1.286

1.288

1.291

1.293

1.296

1.298

1.301

1.303

1.306

1.308

1.90

1.310

1.313

1.315

1.317

1.320

1.322

1.324

1.327

1.329

1.331

2.00

1.333

1.336

1.338

1.340

1.342

1.344

1.346

1.349

1.351

1.353

2.10

1.355

1.357

1.359

1.361

1.363

1.365

1.367

1.369

1.371

1.373

2.20

1.375

1.377

1.379

1.381

1.383

1.385

1.387

1.388

1.390

1.392

2.30

1.394

1.396

1.398

1.399

1.401

1.403

1.405

1.407

1.408

1.410

2.40

1.412

1.413

1.415

1.417

1.419

1.420

1.422

1.424

1.425

1.427

2.50

1.429

1.430

1.432

1.433

1.435

1.437

1.438

1.440

1.441

1.443

2.60

1.444

1.446

1.448

1.449

1.451

1.452

1.454

1.455

1.457

1.458

2.70

1.459

1.461

1.462

1.464

1.465

1.467

1.468

1.469

1.471

1.472

2.80

1.474

1.475

1.476

1.478

1.479

1.481

1.482

1.483

1.485

1.486

2.90

1.487

1.488

1.490

1.491

1.492

1.494

1.495

1.496

1.497

1.499

3.00

1.500

1.501

1.502

1.504

1.505

1.506

1.507

1.509

1.510

1.511

3.10

1.512

1.513

1.515

1.516

1.517

1.518

1.519

1.520

1.522

1.523

WATER CONTENT 105 PERCENT

DG

1.70

1.251

1.254

1.257

1.259

1.262

1.264

1 .267

1.269

1.272

1.274

1.80

1.277

1.279

1.282

1.284

1.286

1.289

1.291

1.294

1.296

1.298

1.90

1.301

1.303

1.305

1.307

1.310

1.312

1. 314

1.316

1.318

1.320

2.00

1.323

1.325

1.327

1.329

1.331

1.333

1.335

1.337

1.339

1.341

2.10

1.343

1.345

1.347

1.349

1.351

1.353

1.355

1.357

1.359

1.361

2.20

1.363

1.364

1.366

1.368

1.370

1.372

1.3 74

1.3 75

1.377

1.379

2.30

1.381

1.382

1.384

1.386

1.388

1.389

1.391

1.393

1.394

1.396

2.40

1.398

1.399

1.401

1.403

1.404

1.406

1.407

1.409

1.411

1.412

2.50

1.414

1.415

1.417

1.418

1.420

1.421

1.423

1.424

1.426

1.427

2.60

1.429

1.430

1.432

1.433

1.435

1.436

1.438

1.439

1.440

1.442

2.70

1.443

1.445

1.446

1.447

1.449

1.450

1.452

1.453

1.454

1.456

2.80

1.457

1.458

1.459

1.461

1.462

1.463

1.465

1.466

1.467

1.468

2.90

1.470

1.471

1.472

1.473

1.475

1.476

1.477

1.478

1.480

1.481

3.00

1.482

1.483

1.484

1.485

1.4*7

1.488

1.489

1.490

1.491

1.492

3.10

1.494

1.495

1.4°6

1.497

1.498

1.499

1.500

1.501

1.502

1.504

WATER CONTENT 110 PERCENT

DG

1.70

1.244

1.246

1.249

1.251

1.254

1.256

1.259

1.261

1.264

1.266

1.80

1.268

1.271

1.273

1.275

1.278

1.280

1.282

1.285

1.287

1.289

1.90

1.291

1.293

1.296

1.298

1.300

1.302

1.304

1.306

1.308

1.310

2.00

1.312

1.315

1.317

1.319

1.321

1.323

1.325

1.327

1.328

1.330

2.10

1.332

1.334

1.336

1.338

1.340

1.342

1.344

1.345

1.347

1.349

2.20

1.351

1.353

1.354

1.356

1.358

1.360

1.361

1.363

1.365

1.367

2.30

1.368

1.370

1.372

1.373

1.375

1.377

1.378

1.380

1.381

1.383

2.40

1.385

1.386

1.388

1.389

1.391

1.392

1.394

1.395

1.397

1.399

2.50

1.400

1.40L

1.403

1.404

1.406

1.407

1.409

1.410

1.412

1.413

2.60

1.415

1.416

1.417

1.419

1.420

1.421

1.423

1.424

1.426

1.427

2.70

1.428

1.430

1.431

1.432

1.433

1.435

1.436

1.437

1.439

1.440

2.80

1.441

1.442

1.444

1.445

1.446

1.447

1.449

1.450

1.451

1.452

2.90

1.453

1.455

1.456

1.457

1.458

1.459

1.461

1.462

1.463

1.464

3.00

1.465

1.466

1.467

1.468

1.470

1.471

1.472

1.473

1.474

1.475

3.10

1.476

1.477

1.478

1.4 79

1.480

1.482

1.483

1.484

1.485

1.486

33

WATER CONTENT 115 PERCENT

DG 0123456789

1.70 1.237 1.239 1.242 1.244 1.247 1.249 1.251 1.254 1.256 1.258

1.80 1.261 1.263 1.265 1.267 1.270 1.272 1.274 1.276 1.278 1.280

1.90 1.283 1.285 1.287 1.289 1.291 1.293 1.295 1.297 1.299 1.301

2.00 1.303 1.305 1.307 1.309 1.311 1.313 1.315 1.317 1.318 1.320

2.10 1.322 1.324 1.326 1.328 1.329 1.331 1.333 1.335 1.336 1.338

2.20 1.340 1.342 1.343 1.345 1.347 1.348 1.350 1.352 1.353 1.355

2.30 1.357 1.358 1.360 1.361 1.363 1.365 1.366 1.368 1.369 1.371

2.40 1.372 1.374 1.375 1.377 1.378 1.380 1.381 1.383 1.384 1.386

2.50 1.387 1.389 1.390 1.391 1.393 1.394 1.396 1.397 1.398 1.400

2.60 1.401 1.402 1.404 1.405 1.406 1.408 1.409 1.410 1.412 1.413

2.70 1.414 1.415 1.417 1.418 1.419 1.420 1.422 1.423 1.424 1.425

2.80 1.427 1.428 1.429 1.430 1.431 1.432 1.434 1.435 1.436 1.437

2.90 1.438 1.439 1.441 1.442 1.443 1.444 1.445 1.446 1.447 1.448

3.00 1.449 1.451 1.452 1.453 1.454 1.455 1.456 1.457 1.458 1.459

3.10 1.460 1.461 1.462 1.463 1.464 1.465 1.466 1.467 1.468 1.469

HATER CONTENT 120 PERCENT

DG 0123456789

1.70 1.230 1.233 1.235 1.237 1.240 1.242 1.244 1.246 1.249 1.251

1.80 1.253 1.255 1.258 1.260 1.262 1.264 1.266 1.268 1.270 1.272

1.90 1.274 1.276 1.278 1.280 1.282 1.284 1.286 1.288 1.290 1.292

2.00 1.294 1.296 1.298 1.300 1.302 1.303 1.305 1.307 1.309 1.311

2.10 1.313 1.314 1.316 1.318 1.320 1.321 1.323 1.325 1.326 1.328

2.20 1.330 1.331 1.333 1.335 1.336 1.338 1.339 1.341 1.343 1.344

2.30 1.346 1.347 1.349 1.350 1.352 1.353 1.355 1.356 1.358 1.359

2.40 1.361 1.362 1.364 1.365 1.367 1.368 1.369 1.371 1.372 1.374

2.50 1.375 1.376 1.378 1.379 1.380 1.382 1.383 1.384 1.386 1.387

2.60 1.388 1.390 1.391 1.392 1.393 1.395 1.396 1.397 1.398 1.400

2.70 1.401 1.402 1.403 1.405 1.406 1.407 1.408 1.409 1.411 1.412

2.80 1.413 1.414 1.415 1.416 1.417 1.419 1.420 1.421 1.422 1.423

2.Q0 1.424 1.425 1.426 1.427 1.428 1.430 1.431 1.432 1.433 1.434

3.00 1.435 1.436 1.437 1.438 1.439 1.440 1.441 1.442 1.443 1.444

3.10 1.445 1.446 1.447 1.448 1.449 1.450 1.451 1.452 1.453 1.454

WATER CONTENT 125 PERCENT

DG 0123456789

1.70 1.224 1.226 1.229 1.231 1.233 1.235 1.237 1.240 1.242 1.244

1.80 1.246 1.248 1.250 1.252 1.255 1.257 1.259 1.261 1.263 1.265

1.90 1.267 1.269 1.271 1.273 1.274 1.276 1.278 1.280 1.282 1.284

2.00 1.286 1.288 1.289 1.291 1.293 1.295 1.297 1.298 1.300 1.302

2.10 1.303 1.305 1.307 1.309 1.310 1.312 1.314 1.315 1.317 1.318

2.20 1.320 1.322 1.323 1.325 1.326 1.328 1.329 1.331 1.332 1.334

2.30 1.335 1.337 1.338 1.340 1.341 1.343 1.344 1.346 1.347 1.349

2.40 1.350 1.351 1.353 1.354 1.356 1.357 1.358 1.360 1.361 1.362

2.50 1.364 1.365 1.366 1.368 1.369 1.370 1.371 1.373 1.374 1.375

2.60 1.376 1.378 1.379 1.380 1.381 1.383 1.384 1.385 1.386 1.387

2.70 1.389 1.390 1.391 1.392 1.393 1.394 1.396 1.397 1.398 1.399

2.80 1.400 1.401 1.402 1.403 1.404 1.405 1.407 1.408 1.409 1.410

2.90 1.411 1.412 1.413 1.414 1.415 1.416 1.417 1.418 1.419 1.420

9.00 1.421 1.422 1.423 1.424 1.425 1.426 1.427 1.428 1.429 1.430

3.10 1.431 1.432 1.433 1.434 1.435 1.435 1.436 1.437 1.438 1.439

31+

WATER CONTENT 130 PERCENT

OG

1.70

1.218

1.220

1.222

1.225

1.227

1.229

1.231

1.233

1.235

1.237

1.80

1.240

1.242

1.244

1.246

1.248

1.250

1.252

1.254

1.256

1.257

1.90

1.259

1.261

1.263

1.265

1.267

1.269

1.271

1.272

1.274

1.276

2.00

1.278

1.280

1.281

1.283

1.285

1.286

1.288

1.290

1.292

1.293

2.10

1.295

1.297

1.298

1.300

1.301

1.303

1.305

1.306

1.308

1.309

2.20

1.311

1.312

1.314

1.315

1.317

1.313

1.320

1.321

1.323

1.324

2.30

1.326

1.327

1.329

1.330

1.332

1.333

1.334

1.336

1.337

1.338

2.40

1.340

1.341

1.342

1.344

1.345

1.346

1.348

1.349

1.350

1.352

2.50

1.353

1.3 54

1.355

1.357

1.358

1.359

1.360

1.362

1.363

1.364

2.60

1.365

1.366

1.368

1.369

1.370

1.371

1.372

1.374

1.375

1.376

2.70

1.377

1.378

1.379

1.380

1.381

1.383

1.384

1.385

1.386

1.387

2.80

1.388

1.389

1.390

1.391

1.392

1.3Q3

1.394

1.395

1.396

1.397

2.90

1.398

1.399

1.400

1.401

1.402

1.40 3

1.404

1.405

1.406

1.407

3.00

1.408

1.409

1.41C

1.411

1.412

1.413

1.414

1.415

1.416

1.417

3.10

1.417

1.418

1.419

1.420

1.421

1.422

1.423

1.424

1.425

1.425

WATER CONTENT 135 PERCFNT

DG

1.70

1.212

1.215

1.217

1.210

1.221

1.223

1.225

1.227

1.229

1.231

1.80

1.233

1.235

1.237

1.239

1.241

1.243

1.245

1.247

1.249

1.251

1.90

1.252

1.254

1.256

1.253

1.260

1.262

1.263

1.265

1.267

1.269

2.00

1.270

1.272

1.274

1.275

1.277

1.279

1.230

1.282

1.284

1.285

2.10

1.287

1.233

1.290

1.292

1.2^3

1.295

1.296

1.298

1.299

1.301

2.20

1.302

1.304

1.305

1.307

1.308

1.310

1.311

1.312

1.314

1.315

2.30

1.317

1.318

1.319

1.321

1.322

1.324

1.325

1.326

1.328

1.329

2.40

1.330

1. 331

1.333

1.334

1.335

1.337

1.338

1.339

1.340

1.342

2.50

1.343

1.344

1.345

1.347

1.348

1.349

1.350

1.351

1.352

1.354

2.60

1.355

1.356

1.357

1.358

1.359

1.360

1.362

1.363

1.364

1.365

2.70

1.366

1.367

1.368

1.369

1.370

1.371

1.372

1.373

1.374

1.376

2.80

1.377

1.378

1.379

1.380

1.381

1.382

1.383

1.384

1.385

1.386

2.90

1.387

1.388

1.389

1.389

1.3°0

1.391

1.392

1.393

1.394

1.395

3.00

1.396

1.397

1.398

1.399

1.400

1.401

1.401

1.402

1.40 3

1.404

3.10

1.405

1.406

1.407

1.408

1.408

1.409

1.410

1.411

1.412

1.413

WATER CONTENT 140 PERCENT

OG

1 .70

1.207

1.209

1.211

1.213

1.215

1.217

1.219

1.221

1.223

1.225

1.80

1.227

1.229

1.231

1.233

1.235

1.237

1.239

1.240

1.242

1.244

1.90

1.246

1.248

1.240

1.251

1.253

1.255

1.256

1.258

1.260

1.261

2.00

1.263

1.265

1.266

1.268

1.270

1.271

1.273

1.274

1.276

1.278

2.10

1.279

1.281

1.282

1.2«4

1.285

1.287

1.288

1.290

1.291

1.293

2.20

1.294

1.296

1.297

1.298

1.300

1.301

1.303

1.304

1.305

1.307

2.30

1.308

1.30O

1.311

1.312

1.313

1.315

1.316

1.317

1.319

1.320

2.40

1.321

1.322

1.324

1.325

1.326

1.327

1.329

1.330

1.331

1.332

2.50

1.333

1.335

1.336

1.337

1.338

1.339

1.340

1.341

1.343

1.344

2.60

1.345

1.346

1.347

1.348

1.349

1.350

1.351

1.352

1.354

1.355

2.70

1.356

1.357

1.358

1.350

1. 360

1.361

1.362

1.363

1.364

1.365

2.80

1.366

1.367

1.368

1.369

1.370

1.371

1.372

1.373

1.374

1.375

2.90

1.375

1.376

1.377

1.378

1.379

1.380

1.331

1.332

1.383

1.384

3.00

1.385

1.385

1.386

1.387

1.388

1.389

1.390

1.391

1.392

1.392

3.10

1.393

1.394

1.395

1.396

1.397

1.397

1.398

1.399

1.400

1.401

3 5

WATER CONTENT 145 PERCENT

OG

1.70

1.202

1.204

1.206

1.208

1.210

1.212

1.214

1.216

1.218

1.220

1.80

1.222

1.223

1.225

1.227

1.229

1.231

1.233

1.234

1.236

1.238

1.90

1.240

1.241

1.243

1.245

1.247

1.248

1.250

1.252

1.253

1.255

2.00

1.256

1.258

1.260

1.261

1.263

1.264

1.266

1.267

1.269

1.270

2.10

1.272

1.273

1.275

1.276

1.278

1.279

1.281

1.282

1.284

1.235

2.20

1.296

1.288

1.289

1.291

1.292

1.293

1.295

1.296

1.297

1.299

2.30

1.300

1.301

1.302

1.304

1.305

1.306

1.308

1.309

1.310

1.311

2.40

1.312

1.314

1. 315

1.316

1.317

1.319

1.320

1.321

1.322

1.323

2.50

1.324

1.325

1.327

1.328

1.329

1.330

1.331

1.332

1.333

1.334

2.60

1.335

1.337

1.338

1.339

1.340

1.341

1.342

1.343

1.344

1.345

2.70

1.346

1.347

1.348

1.349

1.350

1.351

1.352

1.353

1.354

1.355

2.80

1.356

1.357

1.358

1.359

1.360

1.360

1.361

1.362

1.363

1.364

2.°0

1.365

1.366

1.367

1.368

1.369

1.369

1.370

1.371

1.372

1.373

3.00

1.374

1.375

1.376

1.376

1.377

1.378

1.3 79

1.380

1.381

1.381

3.10

1.382

1.383

1.384

1.3 85

1.385

1.386

1.387

1.398

1.389

1.389

WATER CONTENT 150 PERCENT

DG

1.70

1. 197

1.199

1.201

1.203

1.205

1.207

1.209

1.211

1.213

1.214

1.80

1.216

1.218

1.220

1.222

1.223

1.225

1.227

1.229

1.230

1.232

1.90

1.234

1.235

1.237

1.239

1.240

1.242

1.244

1.245

1.247

1.248

2.00

1.250

1.252

1.253

1.255

1.256

1.258

1.2 59

1.261

1.262

1.264

2.10

1.265

1.267

1.268

1.269

1.271

1.272

1.274

1.2 75

1.276

1.278

2.20

1.279

1.280

1.282

1.283

1.284

1.286

1.287

1.288

1.290

1.291

2.30

1.292

1.293

1.295

1.296

1.297

1.298

1.300

1.301

1.30 2

1.303

2.40

1.304

1.306

1.307

1.308

1.309

1.310

1.311

1.312

1.314

1.315

2.50

1.316

1.317

1.318

1.319

1.320

1.321

1.322

1.323

1.324

1.325

2.60

1.327

1.328

1.329

1.330

1.331

1.332

1.333

1.334

1.335

1.336

2.70

1.337

1.338

1.339

1.340

1.341

1.341

1.342

1.343

1.344

1.345

2.80

1.346

1.347

1.348

1.349

1.350

1.351

1.352

1.352

1.353

1.354

2.Q0

1.355

1.356

1.357

1.358

1.359

1.359

1.3 60

1.361

1.362

1.363

3.00

1.364

1.364

1.365

1.366

1.367

1.368

1.3 69

1.369

1.370

1.371

3.10

1.372

1.372

1.373

1.374

1.375

1.376

1.3 76

1.377

1.373

1.379

WATER CONTENT 155 PERCENT

DG

1.70

1.193

1.194

1.196

1. 198

1.200

1.202

1.204

1.206

1.208

1.209

1.80

1.211

1.213

1.215

1.216

1.218

1.220

1.221

1.223

1.225

1.226

1.90

1.228

1.230

1.231

1.233

1.235

1.236

1.238

1.239

1.241

1.242

2.00

1.244

1.245

1.247

1.248

1.250

1.251

1.253

1.254

1.256

1.257

2.10

1.259

1.260

1.261

1.263

1.264

1.265

1.267

1.268

1.269

1.271

2.20

1.272

1.273

1.275

1.276

1.277

1.279

1.280

1.281

1.232

1.284

2.30

1.285

1.236

1.287

1.288

1.290

1.291

1.292

1.293

1.294

1.295

2.40

1.297

1.298

1.299

1.300

1.301

1.302

1.303

1.304

1.306

1.307

2.50

1.308

1.3 09

1.310

1.311

1.312

1.313

1.314

1.315

1.316

1.317

2.60

1.318

1.319

1.320

1.321

1.322

1.323

1.324

1.325

1.326

1.327

2.70

1.328

1.329

1.330

1.331

1.332

1.333

1.333

1.334

1.335

1.336

2.80

1.337

1.338

1.339

1.340

1.341

1.341

1.342

1.343

1.344

1.345

2.90

1.346

1.347

1.347

1.348

1.349

1.350

1.351

1.352

1.352

1.353

3.00

1.354

1.355

1.356

1.356

1.357

1.358

1.359

1.359

1.360

1.361

3.10

1.362

1.363

1.363

i.364

1.365

1.365

1.366

1.367

1.368

1.368

36

WATER CONTENT 160 PERCENT

DG

1.70

1. 188

1.190

1.192

1. 194

1.196

1.197

1.199

1.201

1.203

1.204

1.80

1.206

1.208

1.210

1.211

1.213

1.215

1.216

1.218

1.220

1.221

1.90

1.223

1.224

1.226

1.227

1.229

1.231

1.232

1.234

1.235

1.237

2.00

1.238

1.240

1.241

1.242

1.244

1.245

1.247

1.248

1.250

1.251

2.10

1.252

1.254

1.255

1.256

1.258

1.259

1.260

1.262

1.263

1.264

2.20

1.265

1.267

1.268

1.269

1.271

1.272

1.273

1.274

1.275

1.277

2.30

1.278

1.2 79

1.280

1.281

1.282

1.234

1.285

1.286

1.287

1.288

2.40

1.289

1.290

1.291

1.293

1.294

1.295

1.2 96

1.297

1.298

1.299

2.50

1.300

1.301

1.302

1.303

1.304

1.305

1.306

1.307

1.308

1.309

2.60

1.310

1.311

1.312

1.313

1.314

1.315

1.316

1.317

1.318

1.319

2.70

1.320

1.320

1.321

1.322

1.323

1.324

1.325

1.326

1.327

1.328

2.80

1.328

1.329

1.330

1.331

1.332

1.333

1. 334

1.334

1.335

1.336

2.90

1.337

1.338

1.339

1.339

1.340

1.341

1.342

1.342

1.343

1.344

3.00

1.345

1.346

1.346

1.347

1.348

1.349

1.349

1.350

1.351

1.352

3.10

1.352

1.353

1.354

1.355

1.355

1.356

1.357

1.357

1.358

1.359

WATER CONTENT 165 PERCENT

DG

1.70

1. 184

1. 186

1.188

1.189

1.191

1.193

1. 195

1. 196

1.198

1.200

1.80

1.202

1.203

1.205

1.206

1.208

1.210

1.211

1.213

1.215

1.216

1.90

1.218

1.219

1.221

1.222

1.224

1.225

1.227

1.228

1.230

1.231

2.00

1.233

1.234

1.235

1.237

1.238

1.240

1.241

1.242

1.244

1.245

2.10

1.246

1.248

1.249

1.250

1.252

1.253

1.254

1.255

1.257

1.258

2.20

1.259

1.260

1.262

1.263

1.264

1.265

1.266

1.268

1.269

1.270

2.30

1.271

1.272

1.273

1.275

1.276

1.277

1.278

1.279

1.280

1.281

2.40

1.282

1.283

1.284

1.285

1.287

1.288

1.289

1.290

1.291

1.292

2.50

1.293

1.294

1.295

1.296

1.297

1.299

1.299

1.300

1.301

1.302

2.60

1.302

1.303

1.304

1.305

1.306

1.307

1.308

1.309

1.310

1.311

2.70

1.312

1.313

1.313

1.314

1.315

1.316

1.317

1.318

1.319

1.319

2.80

1.320

1.321

1.322

1.323

1.324

1.324

1.325

1.326

1.327

1.328

2.90

1.328

1.329

1.330

1.331

1.332

1.332

1.333

1.334

1.335

1.335

3.00

1.336

1.337

1.338

1.338

1.33^

1.340

1.341

1.341

1.342

1.343

3. 10

1.343

1.344

1.345

1.346

1.346

1.34 7

1.348

1.348

1.349

1.350

WATER CONTENT 170 PERCENT

DG

1.70

1.180

1.182

1.183

1.185

1.137

1.199

1.190

1.192

1.194

1.195

1.80

1.197

1.199

1.200

1.202

1.203

1.205

1.207

1.208

1.210

1.211

1.90

1.213

1.214

1.216

1.217

1.219

1.220

1.222

1.223

1.224

1.226

2.00

1.227

1.229

1.230

1.231

1.233

1.234

1.235

1.237

1.238

1.2 39

2.10

1.241

1.242

1.243

1.245

1.246

1.247

1.248

1.250

1.251

1.252

2.20

1.253

1.254

1.256

1.257

1.258

1.259

1.260

1.261

1.263

1.264

2.30

1.265

1.266

1.267

1.268

1.269

1.270

1.271

1.272

1.273

1.275

2.40

1.276

1.277

1.278

1.279

1.280

1.281

1.282

1.283

1.284

1.285

2.50

1.286

1.287

1.288

1.289

1.290

1.291

1.291

1.292

1.293

1.294

2.60

1.295

1.296

1.297

1.298

1.299

1.300

1.301

1.301

1.302

1.303

2.70

1.304

1.305

1.306

1.307

1.308

1.308

1.3 09

1.310

1.311

1.312

2.80

1.312

1.313

1.314

1.315

1.316

1.317

1.317

1.318

1.319

1.320

2.90

1.320

1.321

1.322

1.323

1.323

1.324

1.325

1.326

1.326

1.327

3.00

1.328

1.329

1.329

1.330

1.331

1.331

1.332

1.333

1.334

1.334

3.10

1.335

1.336

1.336

1.337

1.338

1.338

1.339

1.340

1.340

1.341

37

WATER CONTENT 175 PERCENT DG 0 1 2

1.70

1.176

1.178

I. 180

1.181

1.183

1.185

1.186

1.188

1.190

1.191

1.80

1.193

1.194

1. 196

1.198

1. 199

1.201

1.202

1.204

1.205

1.207

1.90

1.208

1.210

1.211

1.212

1.214

1.215

1.217

1.218

1.219

1.221

2.00

1.222

1.224

1.225

1.226

1.228

1.229

1.230

1.231

1.233

1.234

2.10

1.235

1.237

1.238

1.239

1.240

1.241

1.243

1.244

1.245

1.246

2.20

1.247

1.249

1.250

1.251

1.252

1.253

1.254

1.255

1.257

1.258

2.30

1.2 59

1.260

1.261

1.262

1.263

1.264

1.265

1.266

1.267

1.268

2.40

1.269

1.270

1.271

1.272

1.273

1.274

1.275

1.276

1.277

1.278

2.50

1.279

1.280

1.281

1.282

1.283

1.284

1.285

1.286

1.286

1.287

2.60

1.288

1.289

1.290

1.291

1.292

1.293

1.294

1.294

1.295

1.296

2.70

1.297

1.298

1.299

1.299

1.300

1.301

1.302

1.303

1.303

1.304

2.80

1.305

1.306

1.307

1.307

1.308

1.30Q

1.310

1.311

1.311

1.312

2.90

1.313

1.313

1.314

1.315

1.316

1.316

1.317

1.318

1.319

1.319

3.00

1.320

1.321

1.321

1.322

1.323

1.323

1.324

1.325

1.326

1.326

3.10

1.327

1.328

1.328

1.329

1.329

1.330

1.331

1.331

1.332

1.333

WATER CONTENT 180 PERCENT DG 0 1 2 :

1.70

1.172

1.174

1.176

1.1^7

1.179

1.181

1. 182

1.184

1.186

1.187

1.80

1.189

1.190

I. 192

1.193

1.195

1.196

1.198

1.199

1.201

1.202

1.90

1.204

1.205

1.206

1.208

1.209

1.211

1.212

1.213

1.215

1.216

2.00

1.217

1.219

1.220

1.221

1.223

1.224

1.225

1.226

1.228

1.229

2.10

1.230

1.231

1.233

1.234

1.235

1.236

1.237

1.238

1.240

1.241

2.20

1.242

1.243

1.244

1.245

1.246

1.248

1.249

1.250

1.251

1.252

2.30

1.253

1.254

1.255

1.256

1.257

1.258

1.2 59

1.260

1.261

1.262

2.40

1.263

1.2 64

1.265

1.266

1.267

1.268

1.269

1.270

1.271

1.272

2.50

1.273

1.274

1.275

1.275

1.276

1.277

1.278

1.279

1.280

1.281

2.60

1.282

1.283

1.283

1.284

1.285

1.286

1.287

1.288

1.288

1.289

2.70

1.290

1.291

1.292

1.293

1.293

1.294

1.295

1.296

1.296

1.297

2.80

1.298

1.299

1.300

1.300

1.301

1.302

1.303

1.303

1.304

1.305

2.90

1.305

1.306

1.307

1.308

1.308

1.309

1.310

1.310

1.311

1.312

3.00

1.312

1.313

1.314

1.315

1.315

1,316

1.317

1.317

1.318

1.318

3.10

1.319

1.320

1.320

1.321

1.322

1.322

1.323

1.324

1.324

1.325

WATER CONTENT 185 PERCENT DG 0 1 2

1.70

1.16Q

1.171

I. 172

1.174

1. 175

1.177

1.179

1.180

1.182

1.183

1.80

1.185

1.186

1.188

1.189

1.191

1.192

1.194

1. 195

1.197

1.198

1.90

1.199

1.201

1.202

1.203

1.205

1.206

1.208

1.209

1.210

1.211

2.00

1.213

1.214

1.215

1.217

1.218

1.219

1.220

1.222

1.223

1.224

2.10

1.225

1.226

1.228

1.229

1.230

1.231

1.232

1.233

1.234

1.236

2.20

1.237

1.238

1.239

1.240

1.241

1.242

1.243

1.244

1.245

1.246

2.30

1.247

1.248

1.249

1.250

1.251

1.252

1.253

1.254

1.255

1.256

2.40

1.257

1.258

1.259

1.260

1.261

1.262

1.263

1.264

1.265

1.266

2.50

1.267

1.268

1.268

1.269

1.270

1.271

1.272

1.273

1.274

1.275

2.60

1.275

1.276

1.277

1.278

1.2 79

1.280

1.280

1.281

1.282

1.283

2.70

1.284

1.284

1.285

1.286

1.287

1.287

1.288

1.289

1.290

1.291

2.80

1.291

1.292

1.293

1.293

1.294

1.295

1.296

1.296

1.297

1.298

2.90

1.299

1.299

1.300

1.301

1.301

1.302

1.303

1.303

1.304

1.305

3.00

1.305

1.306

1.307

1.307

1.308

1.309

1.309

1.310

1.311

1.311

3.10

1.312

1.312

1.313

1.314

1.314

1.315

1.316

1.316

1.317

1.317

38

WATER CONTENT 190 PERCENT

DG

1.70

1. 165

1.167

1.169

1.170

1.172

1.173

1.175

1.176

1.178

1.180

1.80

1.181

1.182

1.184

1.185

1.187

1.188

1.190

1.191

1.192

1.194

1.90

1. 195

1.197

1.198

1. 199

1.201

1.202

1.203

1.205

1.206

1.207

2.00

1.208

1.210

1.211

1.212

1.213

1.215

1.216

1.217

1.218

1.219

2.10

1.220

1.222

1.223

1.224

1.225

1.226

1.227

1.228

1.229

1.231

2.20

1.232

1.233

1.234

1.235

1.236

1.237

1.238

1.239

1.240

1.241

2.30

1.242

1.243

1.244

1.245

1.246

1.247

1.248

1.249

1.250

1.251

2.40

1.252

1.253

1.254

1.255

1.255

1.256

1.257

1.258

1.259

1.260

2.50

1.261

1.262

1.263

1.263

1.264

1.265

1.266

1.267

1.268

1.269

2.60

1.269

1.270

1.271

1.272

1.273

1.273

1.274

1.275

1.276

1.277

2.70

1.277

1.278

1.279

1.280

1.280

1.281

1.282

1.283

1.283

1.284

2.80

1.285

1.286

1.286

1.287

1.288

1.288

1.289

1.290

1.290

1.291

2.90

1.292

1.2Q3

1.293

1.294

1.295

1.295

1.296

1.297

1.297

1.298

3.00

1.299

1.299

1.300

1.300

1.301

1.302

1.302

1.303

1.304

1.304

3.10

1.305

1.305

1.306

1.307

1.307

1.308

1.308

1.309

1.310

1.310

WATER CONTENT 195 PERCENT

DG

1.70

1.162

1.164

1.165

1.167

1. 168

1.170

1.171

1. 173

1.174

1.176

1.80

1.177

1.179

1.180

1.182

1.183

1.184

1. 186

1.187

1.189

1.190

1.90

1.191

1.193

1.194

1.195

1. 197

1.198

1.199

1.200

1.202

1.203

2.00

1.204

1.205

1.207

1.208

1.209

1.210

1.211

1.212

1.214

1.215

2.10

1.216

1.217

1.218

1.219

1.220

1.221

1.223

1.224

1.225

1.226

2.20

1.227

1.228

1.229

1.230

1.231

1.232

1.233

1.234

1.235

1.236

2.30

1.237

1.238

1.239

1.240

1.241

1.242

1.243

1.244

1.245

1.246

2.40

1.246

1.247

1.248

1.249

1.250

1.251

1.252

1.253

1.254

1.254

2.50

1.255

1.256

1.257

1.258

1.259

1.260

1.260

1.261

1.262

1.263

2.60

1.264

1.264

1.265

1.266

1.267

1.268

1.268

1.269

1.270

1.271

2.70

1.271

1.272

1.273

1.274

1.274

1.275

1.2 76

1.276

1.277

1.278

2.80

1.279

1.279

1.280

1.281

1.281

1.282

1.283

1.283

1.284

1.285

2.°0

1.285

1.286

1.287

1.287

1.288

1.289

1.289

1.290

1.291

1.291

3.00

1.292

1.2Q3

1.293

1.294

1.294

1.295

1.296

1.296

1.297

1.297

3.10

1.298

1.299

1.299

1.300

1.300

1.301

1.302

1.302

1.303

1.303

WATER CONTENT 200 PERCENT

DG

1.70

1.159

1.161

1.162

1.164

1.165

1.167

1.168

1. 170

1.171

1.172

1.80

1.174

1.175

1.177

1.178

1.179

1.181

1.182

1.184

1.185

1.186

1.90

1. 188

1.189

1.190

1.191

1.193

1.1 Q4

1.195

1.196

1.198

1.199

2.00

1.200

1.201

1.202

1.204

1.205

1.206

1.2 07

1.208

1.209

1.210

2.10

1.212

1.213

1.214

1.215

1.216

1.217

1.218

1.219

1.220

1.221

2.20

1.222

1.223

1.224

1.225

1.226

1.227

1.228

1.229

1.230

1.231

2.30

1.232

1.233

1.234

1.235

1.236

1.237

1.238

1.239

1.240

1.240

2.40

1.241

1.242

1.243

1.244

1.245

1.246

1.247

1.247

1.248

1.249

2.50

1.2 50

1.251

1.252

1.252

1.253

1.254

1.255

1.256

1.256

1.257

2.60

1.258

1.2 59

1.260

1.260

1.261

1.262

1.263

1.263

1.264

1.265

2.70

1.266

1.266

1.267

1.268

1.269

1.269

1.2 70

1.271

1.271

1.272

2.80

1.273

1.273

1.274

1.275

1.275

1.276

1.277

1.277

1.278

1.279

2.90

1.279

1.280

1.281

1.281

1.282

1.283

1.283

1.284

1.284

1.285

3.00

1.286

1.286

1.287

1.288

1.288

1.289

1.289

1.290

1.291

1.291

3.10

1.292

1.292

1.293

1.293

1.294

1.295

1.295

1.296

1.296

1.297

39

WATER CONTENT 210 PERCENT

OG

1.70

1.153

1.155

1.156

1.158

1.159

1.160

1.162

1.163

1.165

1.166

1.80

1.167

1.169

1.170

1.171

1.173

1.174

1.175

1.177

1.178

1.179

1.90

1. 180

1.182

1. 183

1.184

1. 185

1.186

1. 188

1.189

1.190

1.191

2.00

1.192

1.193

1.195

1.196

1.197

1.198

1.199

1.200

1.201

1.202

2.10

1.203

1.204

1.205

1.206

1.207

1.209

1.210

1.211

1.212

1.213

2.20

1.214

1.215

1.215

1.216

1.217

1.218

1.219

1.220

1.221

1.222

2.30

1.223

1.224

1.225

1.226

1.227

1.227

1.228

1.229

1.230

1.231

2.40

1.232

1.233

1.233

1.234

1.235

1.236

1.237

1.238

1.238

1.239

2.50

1.240

1.241

1.242

1.242

1.243

1.244

1.245

1.245

1.246

1.247

2.60

1.248

1.248

1.249

1.250

1.251

1.251

1.252

1.253

1.253

1.254

2.70

1.255

1.256

1.256

1.257

1.258

1.258

1.259

1.260

1.260

1.261

2.80

1.262

1.262

1.263

1.2 64

1.264

1.265

1.265

1.266

1.267

1.267

2.90

1.268

1.269

1.269

1.270

1.270

1.271

1.272

1.272

1.273

1.273

3.00

1.274

1.275

1.275

1.276

1.276

1.277

1.2 77

1.278

1.279

1.279

3.10

1.280

1.280

1.281

1.281

1.282

1.282

1.283

1.283

1.284

1.284

WATER CONTENT 220 PERCENT

OG

1.70

1. 148

1.149

1.151

1.152

1.153

1.155

1.156

1.157

1.159

1.160

1.80

1.161

1.163

1.164

1.165

1.166

1.168

1.169

1. 170

1.171

1.173

1.90

1.174

1.175

1.176

1.177

1.178

1. 180

1.181

1. 182

1.183

1.184

2.00

1.185

1.186

1.187

1.188

1.190

1.191

1.192

1.193

1.194

1.195

2.10

1.196

1.197

1.198

1.199

1.200

1.201

1.202

1.203

1.204

1.205

2.20

1.205

1.206

1.207

1.208

1.209

1.210

1.211

1.212

1.213

1.214

2.30

1.215

1.215

1.216

1.217

1.218

1.219

1.220

1.220

1.221

1.222

2.40

1.223

1.224

1.225

1.225

1.226

1.227

1.228

1.228

1.229

1.230

2.50

1.231

1.232

1.232

1.233

1.234

1.234

1.235

1.236

1.237

1.237

2.60

1.238

1.239

1.240

1.240

1.241

1.242

1.242

1.243

1.244

1.244

2.70

1.245

1.246

1.246

1.247

1.248

1.248

1.249

1.250

1.250

1.251

2.80

1.251

1.252

1.253

1.253

1.254

1.254

1.255

1.256

1.256

1.257

2.90

1.257

1.258

1.259

1.259

1.260

1.260

1.261

1.261

1.262

1.263

3.00

1.263

1.264

1.264

1.265

1.265

1.266

1.266

1.267

1.267

1.2 68

3.10

1.26Q

1.269

1.270

1.270

1.271

1.271

1.272

1.272

1.273

1.273

WATER CONTENT 230 PERCENT

OG

1.70

1.143

1.144

1. 145

1.147

1. 148

1.149

1.151

1.152

1.153

1.154

1.80

1.156

1.157

1.158

1.159

1.161

1.162

1.163

1.164

1.165

1.166

1.90

1.168

1. 169

1.170

1.171

1.172

1.173

1.174

1.175

1.176

1.178

2.00

1.179

1. 180

1. 181

1. 182

1.183

1.184

1. 185

1. 186

1.187

1.188

2.10

1.189

1.190

1.191

1.192

1.193

1.193

1.194

1. 195

1.196

1.197

2.20

1.198

1.199

1.200

1.201

1.202

1.202

1.203

1.204

1.205

1.206

2.30

1.207

1.208

1.208

1.209

1.210

1.211

1.212

1.212

1.213

1.214

2.40

1.215

1.215

1.216

1.217

1.218

1.219

1.219

1.220

1.221

1.221

2.50

1.222

1.223

1.224

1.224

1.225

1.226

1.226

1.227

1.228

1.229

2.60

1.229

1.230

1.231

1.231

1.232

1.233

1.233

1.234

1.235

1.235

2.70

1.236

1.236

1.237

1.238

1.238

1.2 39

1.240

1.240

1.241

1.241

2.80

1.242

1.243

1.243

1.244

1.244

1.245

1.245

1.246

1.247

1.247

2.90

1.248

1.248

1.249

1.249

1.250

1.250

1.251

1.252

1.252

1.253

3.00

1.2 53

1.254

1.254

1.255

1.255

1.256

1.256

1.257

1.257

1.258

*• 10

1.^58

LEDI

1.259

1.260

1.260

1.261

1.261

1.262

1.262

1.263

40

WATER CONTENT 240 PERCENT

DG

1.70

1. 138

1.139

1.140

1.142

1. 143

1.144

1.145

1.147

1.143

1.149

1.80

1.150

1.152

1.153

1.154

1.155

1.156

1.157

1.159

1.160

1.161

1.90

1.162

1. 163

1.164

1.165

1. 166

1.167

1. 168

1. 169

1.170

1.171

2.00

1.172

1.173

1.174

1.175

1. 176

1.177

1.178

1. 179

1.180

1.181

2.10

1.182

1.183

1.184

1.185

1.186

1.187

1.188

1.138

1.189

1.190

2.20

1. 191

1.192

1.193

1.194

1.194

1.195

1.196

1.197

1.198

1.199

2.30

1.199

1.200

1.201

1.202

1.203

1.203

1.204

1.205

1.206

1.206

2.40

1.207

1.203

1.209

1.209

1.210

1.211

1.211

1.212

1.213

1.214

2.50

1.214

1.215

1.216

1.216

1.217

1.218

1.218

1.219

1.220

1.220

2.60

1.221

1.222

1.222

1.223

1.224

1.224

1.225

1.225

1.226

1.227

2.70

1.227

1.228

1.228

1.229

1.230

1.230

1.231

1.231

1.232

1.233

2.80

1.233

1.234

1.234

1.235

1.235

1.236

1.237

1.237

1.238

1.238

2.90

1.239

1.239

1.240

1.240

1.241

1.241

1.242

1.242

1.243

1.243

3.00

1.244

1.244

1.245

1.245

1.246

1.246

1.247

1.247

1.248

1.248

3.10

1.249

1.249

1.250

1.250

1.251

1.251

1.252

1.252

1.253

1.253

WATER CONTENT 250 PERCENT

DG

1.70

1.133

1. 135

1.136

1.137

1.138

1.140

1.141

1.142

1.143

1.144

1.80

1. 145

1.147

1.148

1. 149

1. 150

1.151

1.152

1.153

1.154

1.155

1.90

1.157

1.158

1.159

1. 160

1.161

1.162

1.163

1.164

1.165

1.166

2.00

1.167

1. 168

I. 169

1.170

1.170

1.171

1. 172

1. 173

1.174

1.175

2.10

1.176

1.177

1.178

1.179

1.180

1.180

1.181

1. 182

1.183

1.184

2.20

1.185

1.185

1.186

1.187

1. 188

1.189

1.189

1.190

1.191

1.192

2.30

1.193

1.193

1. 194

1.195

1. 196

1.196

1.197

1. 198

1.199

1.199

2.40

1.200

1.201

1.201

1.202

1.203

1.204

1.204

1.205

1.206

1.206

2.50

1.207

1.208

1.208

1.200

1.210

1.210

1.211

1.211

1.212

1.213

2.60

1.213

1.214

1.215

1.215

1.216

1.216

1.217

1.218

1.218

1.219

2.70

1.219

1.220

1.221

1.221

1.222

1.222

1.223

1.223

1.224

1.224

2.80

1.225

1.226

1.226

1.227

1.227

1.228

1.228

1.229

1.229

1.230

2.Q0

1.230

1.231

1.231

1.232

1. 232

1.233

1.233

1.234

1.234

1.235

3.00

1.235

1.236

1.236

1.237

1.237

1.238

1.238

1.239

1.239

1.240

3. 10

1.240

1.240

1.241

1.241

1.242

1.242

1.243

1.243

1.244

1.244

WATER CONTENT 260 PERCENT

DG

1.7Q

1. 129

1.130

1.132

1. 133

1.134

1.135

1.136

1. 137

1.139

1.140

1.80

1. 141

1.142

1.143

1. 144

1. 145

1.146

1.147

1.148

1.149

1.150

1.90

1.152

1. 153

1.154

1.155

1.156

1.157

1.157

1. 158

1.159

1.160

2.00

1.161

1.162

1.163

1.164

1. 165

1.166

1.167

1. 168

1.169

1.169

2.10

1.170

1.171

1.172

I. 173

1.174

1.175

1.175

1. 176

1.177

1.178

2.20

1.179

1. 179

1.180

1.181

1.182

1.132

1.183

1. 184

1.185

1.186

2.30

1. 186

1. 187

1. 188

1.18 8

1.189

1.190

1.191

1.191

1.192

1.193

2.40

1.193

1. 194

1.195

1.195

1. 196

1.197

1.197

1.198

1.199

1.199

2.50

1.200

1.201

1.201

1.202

1.203

1.203

1.204

1.204

1.205

1.206

2.60

1.206

1.207

1.207

1.208

1.209

1.209

1.210

1.210

1.211

1.211

2.70

1.212

1.21 3

1.213

1.214

1.214

1.215

1.215

1.216

1.216

1.217

2.80

1.217

1.218

1.218

1.219

1.219

1.220

1.220

1.221

1.221

1.222

2.90

1.222

1.223

1.223

1.224

1.224

1.225

1.225

1.226

1.226

1.227

3.00

1.227

1.228

1.228

1.229

1.229

1.230

1.230

1.230

1.231

1.231

3.10

1.232

1.232

1.233

1.233

1.234

1.234

1.2 34

1.235

1.235

1.236

41

WATER CONTENT 270 PERCENT

DG

1.70

1.125

1.126

1.128

1.129

1.130

1.131

1.132

1. 133

1.134

1.135

1.80

1.137

1.138

1.139

1.140

1.141

1.142

1.143

1.144

1.145

1.146

1.90

1.147

1.148

1. 149

1.150

I. 151

1.152

1.153

1.154

1.154

1.155

2.00

1.156

1.157

1.158

1.159

1.160

1.161

1.162

1.162

1.163

1.164

2.10

1.165

1.166

1.167

1.167

1.168

1.169

1.170

1. 171

1.171

1.172

2.20

1.173

1.174

1.174

1.175

I. 176

1.177

1.177

1. 178

1.179

1.180

2.30

1.180

1.181

1.182

1.182

1. 183

1.184

1.184

1.185

1.186

1.187

2.40

1.187

1.188

1.188

1.189

1.190

1.190

1.191

1.192

1.192

1.193

2.50

1.194

1.194

1. 195

1.195

1.196

1.197

1.197

1.198

1.198

1.199

2.60

1.200

1.200

1.201

1.201

1.202

1.202

1.203

1.203

1.204

1.205

2.70

1.205

1.206

1.206

1.207

1.207

1.208

1.208

1.209

1.209

1.210

2.80

1.210

1.211

1.211

1.212

1.212

1.213

1.213

1.214

1.214

1.215

2.°0

1.215

1.216

1.216

1.217

1.217

1.218

1.218

1.218

1.219

1.219

3.00

1.220

1.220

1.221

1.221

1.222

1.222

1.222

1.223

1.223

1.224

3.10

1.224

1.225

1.225

1.225

1.226

1.226

1.227

1.227

1.227

1.228

WATER CONTENT 280 PERCENT

DG

1.70 1

L.122

1.123

1.124

1.125

1.126

1.127

1.128

1. 129

1.130

1.131

1.80 1

L. 132

1.133

1.135

1.136

1. 137

1.138

1.139

1.140

1.140

1.141

1.90 1

1.142

1.143

1. 144

1.145

1. 146

1.147

1.148

1.149

1.150

1.151

2.00 1

1.152

1.152

1.153

1.154

1.155

1.156

1.157

1.157

1.158

1.159

2.10 ]

L.160

1.161

1.161

1.162

1.163

1.164

1.165

1.165

1.166

1.167

2.20 1

L. 168

I. 168

1.169

1. 170

1. 171

1.171

1.172

1. 173

1.173

1.174

2.30 1

1.175

1.175

1.176

I. 177

1. 177

1.178

1.179

1.179

1.180

1.181

2.40 ]

L.181

1.132

1.183

1.183

1. 184

1.184

1.185

1. 186

1.186

1.187

2.50 1

[.187

1.188

1.189

1.189

I. 190

1.190

1.191

1. 192

1.192

1.193

2.60 1

1.193

1.194

1.194

1.195

1.195

1.196

1.196

1.197

1.198

1.198

2.70 1

1.199

1.199

1.200

1.200

1.201

1.201

1.202

1.202

1.203

1.203

2.80 ]

L.204

1.204

1.205

1.205

1.206

1.206

1.206

1.207

1.207

1.208

2.90 1

..208

1.209

1..209

1.210

1.210

1.211

1.211

1.211

1.212

1.212

3.00 1

1.213

1.213

1.214

1.214

1.214

1.215

1.215

1.216

1.216

1.217

3.10 ]

L.217

1.217

1.218

1.218

1.219

1.219

1.219

1.220

1.220

1.220

WATER CONTENT 290 PERCENT

DG

1.70 ]

I. 118

1.119

1.120

1.121

1. 122

1.123

1.125

1. 126

1.127

1.128

1.80 1

.. 129

1.130

1.131

1. 132

1.133

1.134

1. 135

1.135

1.136

1.137

1.90 1

L. 138

1. 139

1.140

1.141

1.142

1.143

1.144

1.144

1.145

1.146

2.00 1

L.147

1.148

1.149

1.150

1. 150

1.151

1.152

1.153

1.154

1.154

2.10 ]

L.155

1.156

1.157

1.157

1. 158

1.159

1.160

1. 160

1.161

1.162

2.20 ]

L.163

1.163

1.164

1. 165

1.165

1.166

1.167

1.167

1.168

1.169

2.30 1

L. 169

1.170

1.171

1. 171

1.172

1.173

1.173

1. 174

1.175

1.175

2.40 1

L.176

1.176

1.177

1. 178

1. 178

1.179

1.179

1.180

1.181

1.181

2.50 1

L.182

1.182

1.183

1.184

1.184

1.185

1.185

1. 186

1.186

1.187

2.60 ]

L.187

1.188

1.188

1.189

1. 189

1.190

1.190

1.191

1.192

1.192

2.70 ]

1.193

1.193

1.194

1.194

1.194

1.195

1.195

I. 196

1.106

1.197

2.80 ]

L.197

1.198

1.198

1.199

1.199

1.200

1.200

1.201

1.201

1.201

2.90 1

1.202

1.202

1.203

1.203

1.204

1.204

1.205

1.205

1.205

1.206

3.00 1

1.206

1.207

1.207

1.207

1.208

1.208

1.209

1.209

1.209

1.210

3.10 ]

1.210

1.211

1.211

1.211

1.212

1.212

1.213

1.213

1.213

1.214

42

WATER CONTENT 300 PERCENT

DG

1.70 1

L.115

1.116

1.117

1.118

1. 119

1.120

1.121

1.122

1.123

1.124

1.80 I

L, 125

1.126

1.127

1.128

1. 129

1.130

1.131

1. 132

1.133

1.133

1.90 1

L.134

1. 135

1. 136

1.137

1. 138

1.139

1. 140

1.140

1.141

1.142

2.00 ]

L.143

1.144

1.144

1.145

1. 146

1.147

1.148

1. 148

1.149

1.150

2.io ;

L.151

1.151

1.152

1.153

1. 154

1.154

1. 155

1. 156

1.156

1.157

2.20 ]

L.158

1.159

1.159

1.160

1.161

1.161

1.162

1.163

1.163

1.164

2.30 ]

L. 165

1.165

1.166

1.166

1. 167

1.168

1.168

1.169

1.170

1.170

2.40 ]

L.171

1.171

1.172

1.172

1.173

1.174

1.174

1. 175

1.175

1.176

2.50 ]

L. 176

1. 177

1. 178

1. 178

1.179

1.179

1.180

1.180

1.181

1.181

2.60 ]

1.182

1.182

1. 183

1. 183

1. 184

1.184

1.185

1. 185

1.186

1.186

2.70 ]

L.187

1.187

1.188

1.188

1. 189

1.189

1.190

1.190

1.191

1.191

2.80 3

L.191

1.19?

1.192

1.193

1.193

1.194

1.194

1.195

1.195

1.195

2.90 ]

L.196

1.196

1. 197

1. 197

1. 198

1.198

1.198

1.199

1.199

1.200

3.00 ]

1.200

1.200

1.201

1.201

1.202

1.202

1.202

1.203

1.203

1.204

3.10 ]

1.2C4

1.204

1.205

1.205

1.205

1.206

1.2 06

1.206

1.207

1.207

WATER CONTENT 310 PERCENT

DG

1.70 ]

t.112

1.113

1.114

1.115

1. 116

1.117

1.118

1.119

1.120

1.121

1.80 1

..122

1.123

1.123

1.124

1.125

1.126

1.127

1.128

1.129

1.130

1.90 ]

L. 131

1. 131

1.132

1. 133

1.134

1. 135

1. 136

1.136

1.137

1.138

2-. 00 1

L.139

1.140

1.140

1.141

1. 142

1.143

1.144

1.144

1.145

1.146

2.10 1

L. 146

1.147

1.148

1. 149

1. 149

1.150

1.151

1. 151

1.152

1.153

2.20 1

L.153

1. 154

1.155

1. 155

1.156

1.157

1.157

1. 158

1.159

1.159

2.30 ]

.. 160

1. 161

1.161

1.162

1. 162

1.163

1.164

1.164

1.165

1.165

2.40 ]

L. 166

1.166

1.167

1. 168

1.168

1.169

1.169

1. 170

1.170

1.171

2.50

I. 171

1.17?

1.172

1.173

1. 174

1.174

1.175

1. 175

1.176

1.176

2.60 1

.. 177

1. 177

I. 178

r. 178

1.179

1.179

1.180

1.180

1.180

1.181

2.70 1

L.181

1.182

1.182

1.183

1.183

1.184

1.184

1. 185

1.185

1.186

2.80 1

L. 186

1. 186

1.187

1.187

1.188

1.188

1.189

1.189

1.189

1.190

2.90 1

..190

1.191

1.191

1.191

1.192

1.192

1.193

1. 193

1.193

1.194

3.00 1

L.194

1.195

1.195

1. 1°5

1.1*56

1.196

1. 196

1.197

1.197

1.198

3.10 1

L.198

1.198

1.199

1.199

1.199

1.200

1.200

1.200

1.201

1.201

WATER CONTENT 320 PERCENT

DG

1.70 ]

.. 109

1.110

1.111

1.112

1. 113

1.114

1.115

1. 116

1.116

1.117

1.80 1

. 118

1.119

1.120

1.121

1.122

1.123

1.124

1.125

1.125

1.126

l.°0 ]

L. 127

1.128

1.129

1. 130

1. 130

1. 131

1.132

1. 133

1.134

1.134

2.00 1

..135

1.136

1. 137

1.137

1.138

1.139

1.140

1,140

1.141

1.142

2.10 J

.. 142

1.143

1.144

1.145

1.145

1.146

1.147

1.147

1.148

1.149

2.20 1

..149

1.150

1.151

1. 151

1.152

1.152

1. 153

1.154

1.154

1.155

2.30 ]

1.156

1.156

1.157

1. 157

1.158

1.158

1.159

1.160

1.160

1.161

2.40 1

..161

1.162

1.162

1. 163

1.163

1.164

1.165

1.165

1.166

1.166

2.50 1

. 167

1. 167

1.168

1.168

1. 169

1.169

1.170

1. 170

1.171

1.171

2.60 ]

.. 172

1.172

1.173

1.173

1. 174

1.174

1. 175

1.175

1.175

1.176

2.70 ]

.176

1.177

1.177

1.178

1. 178

1.179

1. 179

1.179

1.180

1.180

2. 80 1

..1«1

1.181

1.182

1.182

I. 182

1.183

1.183

1. 184

1.184

1.184

2.90 1

.185

1.185

I. 186

1.186

1.186

1.187

1.187

1.188

1.188

1.188

3.00 ]

,.189

1.189

1.189

1.190

1.190

1.191

1.191

1.191

1.192

1.192

3.10

t.192

1.193

1.193

1.193

1.194

1.194

1.194

1.195

1.195

1.195

43

WATER CONTENT 330 PERCENT

DG

1.70 I

I. 106

1.107

1.108

1. 109

1.110

1.111

1.112

1.113

1.113

1.114

1.80 ]

L.115

1.1L6

1.117

1.118

1.119

1.120

1.120

1.121

1.122

1.123

1.90

L.124

1.125

1.125

1.126

1. 127

1.128

1.129

1.129

1.130

1.131

2.00 ]

L. 132

1.132

1. 133

1. 134

1. 135

1.135

1. 136

1. 137

1.137

1 .138

2.10 1

L.139

1.139

1.140

1.141

1.141

1.142

1. 143

1. 143

1.144

1.145

2.20 ]

..145

1.146

1. 147

1.147

1. 148

1.148

1.149

1.150

1.150

1.151

2.30 ]

L.151

1.152

1.152

1.153

1. 154

1.154

1.155

1.155

1.156

1.156

2.40 ]

L.157

1.157

1.158

1.159

1.159

1.160

1.160

1. 161

1.161

1.162

2.50 1

..162

1.163

1. 163

1.164

1.164

1.165

1.165

1.166

1.166

1.167

2.60 1

..167

1.167

1.168

1.168

1.169

1.169

1. 170

1. 170

1.171

1.171

2.70 ]

L. 172

1. 172

1.172

1. 173

1. 173

1.174

1.174

1.175

1.175

1.175

2.80 1

I. 176

1.176

1.177

1.177

1.177

1.178

1.178

1.179

1.179

1.179

2.90 1

L.180

1.180

1.181

1.181

1.181

1.182

1.182

1.182

1.183

1.183

3.00 ]

I. 183

1. 184

1.184

1.185

1.185

1.185

1. 186

1. 186

1.186

1.187

3.10 1

..187

1.187

1.188

1.188

1. 188

1.189

1.189

1. 189

1.190

1.190

WATER CONTENT 340 PERCENT

DG

1.70 ]

L. 103

1.104

1.105

1.106

1. 107

1.108

1. 109

I,

no

1.111

1.111

1.80 ]

L.112

1.113

1.114

1.115

1.116

1.117

1. 117

1,

118

1.119

1.120

1.90

L.121

1.121

1.122

1.123

1.124

1.125

1.125

1.

.126

1.127

1.127

2.00 ]

L.128

1.129

1. 130

1.130

1.131

1.132

1.132

1.

133

1.134

1.134

2.10 1

L.135

1*136

1.136

1.137

1. 138

1.138

1.139

1.

, 140

1.140

1.141

2.20 ]

L.142

1.142

1.143

1.143

I. 144

1.145

1.145

1.

146

1.146

1.147

2.30 ]

L.147

1.148

1.149

1.149

1. 150

1.150

1.151

1,

151

1.152

1.152

2.40 ]

L. 153

1.153

I. 154

1.154

1. 155

1.155

1.156

1.

156

1.157

1.157

2.50 i

1.158

1. 158

1.159

1.159

1.160

1.160

1. 161

1-

161

1.162

1.162

2.60 1

L. 163

1. 163

1.164

1.164

1.164

1.165

1.165

1.

,166

1.166

1.167

2.70 1

L. 167

1.167

1.168

1.168

1.169

1.169

1.169

1,

170

1.170

1.171

2.80 1

L. 171

1.171

1.172

1. 172

1. 173

1.173

I. 173

1,

174

1.174

1.175

2.90 ]

L.175

1.175

1.176

1. 176

1.176

1.177

1.177

1.

178

1.178

1.178

3.00

L.179

1.179

1.179

1. 180

I. 180

1.180

1.181

1,

181

1.181

1.182

3.10 1

L. 182

1. 182

1.183

1. 183

1. 183

1.184

1.184

1,

184

1.185

1.185

WATER CONTENT 350 PERCENT

OG

1.70 1

.. 101

1.102

1.103

1.103

1.104

1.105

1. 106

I.

107

1.108

1.109

1.80 !

.110

1.110

1.111

1.112

1. 113

1.114

1.115

L.

115

1.116

1.117

1.90 1

L.118

1.118

1.119

1.120

1.121

1.121

1.122

1.

123

1.124

1.124

2.00 1

.125

1. 126

1.126

1.127

1.128

1.128

1.129

1.

130

1.130

1.131

2.10 1

.. 132

1.132

1.133

1.134

1. 134

1.135

1. 136

1.

136

1.137

1.137

2.20 1

L. 138

1.139

1. 13Q

I. 140

1 . 140*

1.141

1.141

1.

142

1.143

1.143

2.30 ]

L. 144

1.144

1.145

1.145

1. 146

1.146

1. 147

1 .

147

1.148

1.148

2.40 1

..149

1.149

1.150

1.150

1.151

1.151

1.152

1.

152

1.153

1.153

2.50 ]

L.154

1.154

1.155

1.155

1. 156

1.156

1.157

1.

157

1.158

1.158

2.60 1

L. 158

1.159

1.159

1.160

1. 160

1.161

1.161

1.

161

1.162

1.162

2.70 I

L. 163

1.163

1.163

1.164

1.164

1.165

1.165

1.

165

1.166

1.166

2.80 1

..167

1.167

1.167

1. 168

1. 168

1.169

1.169

1.

169

1.170

1.170

2.90 ]

1.170

1.171

1.171

1.171

1.172

1.172

1.173

1.

173

1.173

1.174

3.00 ]

1.174

1.174

1.175

1.175

1.175

1.176

1.176

1.

176

1.177

1.177

3.10 1

L. 177

1.178

1.178

1.178

1.178

1.179

1.179

1.

179

1.180

1.180

44

WATER CONTENT 360 PERCENT

DG

1.70 ]

1.098

1.099

I. 100

1.101

1.102

1.103

1.104

1.104

1.105

1.106

1.80 J

1.107

1.108

1.109

1.109

I. 110

1.111

1.112

1.113

1.113

1.114

l.QO ]

L.115

1.116

1.116

1. 117

1.118

1.118

1.119

1.120

1.121

1.121

2.00 1

L.122

1.123

1.123

1.124

1.125

1.125

1.126

1.127

1.127

1.128

2.10 1

L, 129

1. 129

1.130

1.130

1. 131

1.132

1.132

1. 133

1.133

1.134

2.20 ]

1.135

1.135

1.136

1.136

1.137

1.137

1.138

1. 138

1.139

1.140

2.30 ]

1.140

1.141

1.141

1.142

1. 142

1.143

1.143

1.144

1.144

1.145

2.40 1

L.145

1.146

1.146

1.147

1.147

1.148

1.148

1. 149

1.149

1.150

2.50 ]

L. 150

1.150

1.151

1.151

1. 152

1.152

1.153

1.153

1.154

1.154

2.60 1

L.154

1.155

1.155

1.156

1.156

1.157

1.157

1. 157

1.158

1.158

2.70 ]

L.159

1.159

1. 159

1.160

1. 160

1.161

1.161

1.161

1.162

1.162

2.80 ]

L.162

1.163

1.163

1. 164

1.164

1.164

1.165

1.165

1.165

1.166

2.90 ]

L. 166

1.166

1.167

1.167

1.167

1.168

1.168

1.168

1.169

1.169

3.00 ]

L. 169

1.170

1.170

1.170

1.171

1.171

1.171

1.172

1.172

1.172

3.10 ]

L.173

1.173

1.173

I. 174

1. 174

1.174

1.175

1.175

1.175

1.175

WATER CONTENT 370 PERCENT

DG

1.70 1

.096

1.097

1.098

1.099

1.099

1.100

1.101

1.102

1.103

1.104

1.80 ]

L.104

1.105

1.106

1.107

1. 108

1.109

1.109

1. 110

1.111

1.111

1.90 1

..112

1.113

1. 114

1.114

1.115

1.116

1.116

1. 117

1.118

1.118

2.00 1

..119

1.120

1.120

1.121

1.122

1.122

1.123

1.124

1.124

1.125

2.10 ]

L- 125

1.126

1.127

1.127

1.128

1.128

1.129

1. 130

1.130

1.131

2.20 1

L.131

1.132

1.132

1.133

1. 134

1.134

1.135

1.135

1.136

1.136

2.30 1

..137

1.137

1.138

1.138

1. 139

1.139

1.140

1. 140

1.141

1.141

2.40 ]

L.142

1. 142

1.143

1. 143

1. 144

1.144

1.145

1.145

1.145

1.146

2.50 1

L. 146

1. 147

1.147

1. 148

1. 148

1.149

1.149

1.149

1.150

1.150

2.60 1

L- 151

1.151

1.151

1.152

1.152

1.153

1.153

1.154

1.154

1.154

2.70 ]

L. 155

1.155

1. 155

1.156

I. 156

1.157

1.157

1. 157

1.158

1.158

2.80 ]

L- 158

1.159

1.159

1.160

1.160

1.160

1.161

1. 161

1.161

1.162

2.90 ]

L.162

1.162

1.163

1.163

1. 163

1.164

1.164

1.164

1.165

1.165

3.00 1

..165

1.166

1.166

1.166

1.167

1.167

1.167

1.167

1.168

1.168

3.10 1

1.168

1.169

1.169

1.16°

1. 170

1.170

1.170

1. 170

1.171

1.171

WATER CONTENT 380 PERCENT

DG

1.70 ]

.094

1.095

1.096

1.096

1.097

1.098

1.099

1.100

1.100

1.101

1.80 1

.102

1.103

1.104

1.104

1.105

1.106

1.107

1.107

1.108

1.109

1.90 1

.109

1.110

1.111

1.112

1.112

1.113

1.114

1.114

1.115

1.116

2.00 1

. 116

1.117

1.118

1.118

1. 119

1.119

1.120

1.121

1.121

1.122

2.10 1

.122

1.123

1.124

1.124

1.125

1.125

1.126

1.127

1.127

1.128

2.20 1

..128

1.129

1.129

1. 130

1.130

1.131

1.131

1.132

1.132

1.133

2.30 1

.133

1. 134

1.134

1.135

1.135

1.136

1.136

1.137

1.137

1.138

2.40 1

..138

1.139

1.139

1. 140

1.140

1.141

1.141

1.142

1.142

1.142

2.50 1

.143

1.143

1.144

1.144

1.145

1.145

1.145

1.146

1.146

1.147

2.60 1

.147

1.147

1.148

1. 148

1.149

1.149

1.149

1.150

1.150

1.151

2.70 1

1.151

1.151

1.152

1.152

1.152

1.153

1.153

1.154

1.154

1.154

2.80 1

..155

1.155

1.155

1.156

1.156

1.156

1.157

1.157

1.157

1.158

2.90 1

1.158

1.158

1.159

1.159

1.159

1.160

1.160

1.160

1.161

1.161

3.00 1

1.161

1.162

1.162

1.162

1.163

1.163

1.163

1. 163

1.164

1.164

3.10

L. 164

1.165

1.165

1.165

1.165

1.166

1.166

1.166

1.167

1.167

45

WATER CONTENT 390 PERCENT

DG

1.70 1

L.092

1.093

1.093

1.094

1.095

1.096

1.097

1.097

1.098

1.099

1.80 1

L.100

1.101

1.101

1.102

1. 103

1.103

1.104

1.105

1.106

1.106

1.90 ]

1.107

1.108

1.108

1.109

1. 110

1.110

1.111

1.112

1.112

1.113

2.00 1

L.114

1.114

1.115

1.116

1. 116

1.117

1. 117

1. 118

1.119

1.119

2.10 1

L.120

1.120

1.121

1.121

1. 122

1. 123

1.123

1.124

1.124

1.125

2.20 1

.125

1.126

1.126

1.127

1.127

1.128

1.128

1.129

1.129

1.130

2.30 ]

L.130

1.131

1.131

1. 132

1.132

1.133

1.133

1.134

1.134

1.135

2.40 1

L.135

1.136

1.136

1.136

1. 137

1.137

1.138

1. 138

1.139

1.139

2.50 1

I. 140

1.140

1. 140

1.141

1. 141

1.142

1. 142

1. 142

1. 143

1.143

2.60 ]

L. 144

1. 144

1.144

1. 145

1. 145

1.146

1. 146

1. 146

1.147

1.147

2.70 1

i.147

1.148

1.148

1. 149

1.149

1.149

1.150

1. 150

1.150

1.151

2.80 ]

1.151

1.151

1.152

1.152

1.152

1.153

1.153

1. 153

1.154

1.154

2.90 ]

L.154

1.155

1.155

1.155

1.156

1.156

1.156

1.157

1.157

1.157

3.00 1

..157

1.153

1.158

1.158

1.159

1.159

1. 159

1. 160

1.160

1.160

3.10 ]

.160

1.161

1.161

1.161

1. 162

1.162

1.162

1.162

1.163

1.163

WATER CONTENT 400 PERCENT

DG

1.70 1

..090

1.091

1.091

1.092

1.093

1.094

1.095

1.095

1.096

1.097

1.80 ]

L.098

1.098

1.09°

1.100

1.100

1.101

1.102

1. 103

1.103

1.104

1.90 1

L.105

1.105

1.106

1.107

1. 107

1.108

1. 109

1. 109

1.110

1.110

2.00 1

L.lll

1.112

1.112

1. 11 3

1. 114

1.114

1.115

1. 115

1.116

1.116

2.10 !

L.117

1.118

1.118

1.119

1. 119

1.120

1. 120

1. 121

1.121

1.122

2.20 ]

L.122

1.123

1.123

1.124

1. 124

1.125

1.125

1. 126

1.126

1.127

2.30 1

.127

1.128

1.128

1 .129

1.129

1.130

1.130

1. 131

1.131

1.132

2.40 1

L.132

1. 133

1.133

1. 133

1. 134

1.134

1.135

1. 135

I. 136

1.136

2.50 1

L.136

1. 137

1. 137

1. 138

1. 138

1.138

1. 139

1. 139

1.140

1.140

2.60 1

. . 140

1.141

1.141

1.141

1.142

1.142

1. 143

1.143

1.143

1.144

2.70 ]

L. 144

1. 144

1.145

1.145

1. 145

1.146

1. 146

1.147

1.147

1.147

2.80 ]

.. 148

1.148

1.148

1.149

I. 149

1.149

1.150

1.150

1.150

1.150

2.90 ]

L.151

1. 151

1.151

1.152

1. 152

1.152

1.153

1.153

1.153

1.154

3.00 I

L. 154

1. 154

1.154

1. 155

1.155

1.155

1.156

1.156

1.156

1 .156

3.10 1

..157

1.157

1. 157

1. 158

1.158

1.158

1. 158

1.159

1.159

1.159

WATER CONTENT 410 PERCENT

DG

1.70 1

..0«3

1.089

1.089

1.090

1.091

1.092

1.093

1.093

1.094

1.095

1.80 1

..095

1.096

1.097

1.098

1.098

1.099

1. 100

1.100

1.101

1.102

1.90 1

..102

1.103

1.104

1.104

1. 105

1.106

1. 106

1.107

1.107

1.108

2.00 1

. 109

1.109

1.110

1. 110

1. Ill

1.112

1. 112

1. 113

1.113

1.114

2.10 ]

..114

1.115

1.116

1.116

1. 117

1.117

1.118

1. 118

l.l 19

1.119

2.20 ]

.. 120

1.120

1.121

1.121

1. 122

1.122

1.123

1. 123

1.124

1.124

2.30 1

.125

1.125

1.126

1.126

1. 126

1.127

1. 127

1.128

1.128

1.129

2.40 3

L.129

1. 130

1. 130

1 .130

1. 131

1.131

1. 132

1.132

1.133

1.133

2.50 1

.. 133

1. 134

1. 134

1.135

1. 135

1. 135

1.136

1.136

1.136

1.137

2.60 1

.137

1. 138

1.138

1.138

1. 139

1.139

1. 139

1. 140

1.140

1.140

2.70 1

L.141

1.141

1.142

1. 142

1. 142

1.143

1. 143

1. 143

1.144

1. 144

2.80 1

I. 144

1.145

1. 145

1. 145

1. 146

1.146

1.146

1. 146

1.147

1.147

2.90 1

,.147

1.148

1.148

1.148

1.149

1.149

1.149

1.150

1.150

1.150

3.00 1

L. 150

1.151

1.151

1.151

1.152

1.152

1.152

1.152

1.153

1.153

3.10

L.153

1.153

1.154

1.154

1.154

1.155

1.155

1.155

1.155

1.156

i+6

WATER CONTENT 420 PERCENT

DG

1.70 ]

L.086

1.087

1.088

1.088

1.089

1.090

1.091

1.091

1.092

1.093

1.80 1

L.093

1.094

1.095

1.096

1.096

1.097

1.098

1.098

1.099

1.100

1.90 1

I. 100

1.101

1.101

1.102

1.103

1.103

1.104

1.105

1.105

1.106

2.00 1

L. 106

I. 107

1.108

1.108

1.109

1.109

1.110

1.110

1.111

1.111

2.10 ]

L. 112

1. 113

1.113

1. 114

1. 114

1.115

1.115

1. 116

1.116

1.117

2.20 1

L. 117

1.118

1.118

1.119

1.119

1.120

1.120

1.121

1.121

1.121

2.30 ]

L. 122

1.122

1.123

1.123

1.124

1.124

1.125

1.125

1.125

1.126

2.40 1

L.126

1.127

1.127

1.128

1.128

1.128

1.129

1.129

1.130

1.130

2.50 ]

L.130

1.131

1.131

1.132

1.132

1.132

1.133

1.133

1.133

1.134

2.60 ]

L.134

1.135

1.135

1. 135

1. 136

1.136

1.136

1. 137

1.137

1.137

2.70 J

I. 138

1. 138

1.138

1. 139

1.139

1.139

1. 140

1.140

1.140

1.141

2.80 ]

L.141

1.141

1.142

1.142

1. 142

1.143

1.143

1.143

1.144

1.144

2.90 1

L.144

1.144

1.145

1.145

1.145

1.146

1.146

1.146

1.146

1.147

3.00 1

-.147

1.147

1.148

1.148

1.148

1.148

1.149

1.149

1.149

1.150

3.10 1

.. 150

1.150

1. 150

1.151

1.151

1.151

1.151

1. 152

1.152

1.152

WATEP CONTENT 430 PERCENT

DG

1.70 1

L.084

1.085

1.086

1.087

1.087

1.088

1.089

1.089

1.090

1.091

1.80 ]

L.092

1.092

1.093

1.094

1.094

1.095

1.096

1.096

1.097

1.098

1.90 1

L.098

1.099

1.099

1.100

1.101

1.101

1.102

1. 102

1.103

1.104

2.00 ]

L. 104

1.105

1.105

1.106

1.106

1.107

1.108

1.108

1.109

1.109

2.10 1

L. 110

1. 110

1.111

1.111

1.112

1.112

1.113

1.113

1.114

1.114

2.20 1

L.U5

1.115

1.116

1.116

1.117

1.117

1. 118

1.118

1.118

1.119

2.30 ]

L.119

1.120

1.120

1.121

1.121

1.122

1.122

1.122

1.123

1.123

2.40 1

L.124

1. 124

1.124

1.125

1.125

1.126

1.126

1. 126

1.127

1.127

2.50 1

L.128

1.128

1.128

1.129

1.129

1.130

1.130

1. 130

1.131

1.131

2.60 ]

L. 131

1.132

1. 132

1.132

1.133

1.133

1. 133

1.134

1.134

1.134

2.70 1

L.135

1.135

1.135

1.136

1.136

1.136

1. 137

1. 137

1.137

1.138

2.80 ]

L. 138

1.138

1.139

1.139

1. 139

1.140

1.140

1. 140

1.140

1.141

2.90 1

L.141

1.141

1.142

1.142

1. 142

1.142

1.143

1.143

1.143

1.144

3.00 1

L. 144

1. 144

1.144

1.145

1.145

1.145

1.145

1.146

1.146

1.146

3. 10 1

1.147

1. 147

1.147

1.147

1. 148

1.148

1.148

1. 148

1.149

1.149

WATER CONTENT 440 PERCENT

DG

1.70 1

..083

1.083

1.084

1.085

1.085

1.086

1.087

1.088

1.088

1.089

1 .80 1

..090

1.090

1.091

1.092

1.092

1.093

1.094

1.094

1.095

1.096

1.90 1

.096

1.097

1.097

1.098

1.099

1.099

1.100

1.100

1.101

1.101

2.00 1

.102

1.103

1.103

1.104

1.104

1.105

1.105

1.106

1.106

1.107

2.10 1

.107

1.108

1.108

1.109

1.109

1.110

1.110

1-111

1.11 1

1.112

2.20 1

I. 112

1.113

1.113

1.114

1.114

1.115

1.115

1.116

1.116

1.116

2.30 1

.117

1.117

1.118

1.118

1.119

1.119

1.119

1.120

1.120

1.121

2.40 1

.121

1.122

1.122

1.122

1.123

1.123

1.123

1.124

1.124

1.125

2.50 1

.125

1.125

1.126

1.126

1.126

1.127

1.127

1.128

1.128

1.128

2.60 1

..129

1.129

1.129

1.130

1.130

1.130

1.131

1.131

1.131

1.132

2.70 1

.132

1. 132

I. 133

1. 133

1. 133

1.134

1.134

1.134

1.135

1.135

2.80 1

..135

1. 135

1. 136

1. 136

1. 136

1.137

1. 137

1.137

1.138

1.138

2.90 1

>.138

1.138

1.139

1.139

1.139

1.139

1.140

1.140

1.140

1.141

3.00 1

.141

1.141

1.141

1.142

1.142

1.142

1.142

1.143

1.143

1.143

3.10 ]

L.143

1.144

1.144

1.144

1.144

1.145

1.145

1.145

1.145

1.146

47

WATER CONTENT 450 PERCENT

OG

1.70

L .08 1

1.082

1.082

1.083

1.084

1.085

1.085

1.086

1.087

1.087

1.80 1

L.088

1.089

1.089

1.090

1.091

1.091

1.092

1.092

1.093

1.094

1.90 ]

L.094

1.095

1.095

1.096

1.097

1.007

1.098

1.098

1.099

1.099

2.00 1

..100

1.101

1.101

1.102

1.102

1.103

1.103

1.104

1.104

1.105

2.10 1

L.105

1.106

1.106

1.107

1.107

1.108

1.108

1.109

1.109

I. 110

2.20 1

L.110

1.111

1.111

1.111

1.112

1.112

1.113

1.113

1.114

1.114

2.30 1

L.115

1.115

1.115

1.116

1.116

1.117

1.117

1.117

1.118

1.118

2.40 1

L.119

1.119

1.119

1.120

1.120

1.121

1.121

1.121

1.122

1.122

2.50 1

L. 122

1. 123

1.123

1.124

1.124

1.124

1.125

1.125

1.125

1.126

2.60 1

.126

1.126

1.127

1.127

I. 127

1.128

1.128

1.128

1.129

1.129

2.70 ]

..129

1.130

1.130

1.130

1. 131

1.131

1.131

1.131

1.132

1.132

2.80 1

L. 132

1.133

1.133

1.133

1. 134

1.134

1.134

1.134

1.135

1.135

2.90 1

1.135

1.136

1.136

1.136

1.136

1.137

1.137

1. 137

1.137

1.138

3.00 1

..138

1. 138

1.138

1.139

1.139

1.139

1.139

1.140

1.140

1.140

3. 10 1

..140

1.141

1.141

1.141

1.141

1.142

1.142

) . 142

1.142

1.143

WATER CONTENT 460 PERCENT

OG

1.70 1

L.079

1.080

1.081

1.081

1.082

1.083

1.084

1.084

1.085

1.086

1.80 1

L.086

1.087

1.08 7

1.088

1.089

1.089

1.090

1.091

1.091

1.092

1.90 ]

L.092

1.093

1.094

1.094

1.095

1.095

1.096

1.096

1.097

1.097

2.00 i

L.098

1.099

1.099

1.100

1.100

1.101

1.101

1. 102

1.102

1.103

2.10 1

L.103

1.104

1.104

1.105

1.105

1.106

1.106

1.107

1.107

1.107

2.20 1

L.108

1.108

1.109

1.109

1. 110

1.110

I. Ill

1. ill

1.111

1.112

2.30 1

[.112

1.113

1.113

1.113

1. 114

1.114

1.115

1.115

1.116

1.116

2.40 ]

L.116

1.117

1. 117

1. 117

1.118

1. 118

1.119

1.119

1.119

1.120

2.50 ]

L.120

1.120

1.121

1.121

1.121

1.122

1.122

1.122

1.123

1.123

2.60 1

L. 123

1.124

1.124

1.124

1.125

1.125

1.125

1.126

1.126

1.126

2.70 ]

L. 127

1.127

1.127

1.128

1. 128

1.128

1.129

1.129

1.129

1.129

2.80 1

L. 130

1.130

1.130

1.131

1.131

1.131

1.131

1. 132

1.132

1.132

2.90 ]

L. 132

1. 133

1.133

1.133

1.134

1.134

1.134

1.134

1.135

1.135

3.00 I

L.135

1. 135

1.136

1.136

1. 136

1.136

1. 137

1. 137

1.137

1.137

3.10 ]

L.138

1.138

1.138

1.138

1. 139

1.139

1. 139

1. 139

1.139

1.140

WATER CONTENT 470 PERCENT

OG

1.70

1.073

1.079

1.079

1.080

1.081

1.081

1.082

1.083

1.083

1.084

1.80

1.085

1.085

1.086

1.086

1.087

1.088

1.088

1.089

1.089

1.090

1.90

1.091

1.091

1.092

1.092

1.093

1.093

1.094

1.095

1.095

1.096

2.00

1.096

1.097

1.097

1.098

1.098

1.099

1.099

1.100

1.100

1. 101

2.10

I. 101

1.102

1.102

1.103

1. 103

1.104

1.104

1.104

1.105

1.105

2.20

1.106

1.106

1.107

1.107

1.108

1.108

1.108

1. 109

1.109

1.110

2.30

1.110

1.110

1- 111

1.111

1.112

1.112

1.112

1.113

1.113

1.114

2.40

1.114

1.114

1.115

1.115

1.115

1.116

1.116

1. 117

1.117

1.117

2.50

1.118

1.118

1.118

1.119

1.119

1.119

1.120

1.120

1.120

1.121

2.60

1.121

1.121

1.122

1.122

1.122

1.123

1.123

1.123

1.124

1.124

2.70

1.124

1.124

1.125

1.125

1.125

1.126

1.126

1.126

1.127

1.127

2.80

1.127

1.127

1.128

1.128

1.128

1.129

1.129

1.129

1.129

1.130

2.90

1.130

1.130

1.130

1.131

1.131

1.131

1.131

1.132

1.132

1.132

9.00

1.132

1.133

1.133

1.133

1.133

1.134

1.136

1.136

1.134

1.135

3.10

1.135

1.135

1.135

1.136

1.136

1.136

1.136

1.136

1.137

1.137

48

WATER CONTENT 480 PERCENT

DG

1.70 1

L.076

1.077

1.078

1.078

1.079

1.080

1.080

1.081

1.082

1.082

1.80 1

1.083

1.084

1.084

1.085

1.085

1.086

1.087

1.087

1.088

1.088

1.90 1

1.089

1.089

1.090

1.091

1.091

1.092

1.092

1.0^3

1.093

1.094

2.00 ]

L.094

1.095

1.095

1.096

1.096

1.097

1.097

1.098

1.098

1.099

2.10 1

L.099

1.100

1.100

1.101

1. 101

1.102

1.102

1. 102

1.103

1.103

2.20 ]

1.104

1.104

1.105

1.105

1.106

1.106

1. 106

1.107

1.107

1.108

2.30 ]

L.108

1.108

1. 109

1.109

1. 110

1.110

I. 110

1.111

I. Ill

1.111

2.40 ]

L. 112

1.112

1.113

1.113

1.113

1.114

1.114

1.114

1.115

1.115

2.50 1

L. 115

1.116

1.116

1.116

1. 117

1.117

1. 117

1. 118

1.118

1.118

2.60 ]

L.11Q

1.119

1.119

1.120

1. 120

1.120

1.121

1.121

1.121

1.121

2.70 1

L.122

1.122

1.122

1.123

1. 123

1.123

1.124

1. 124

1.124

1.124

2.80 1

L.125

1.125

1.125

1.125

1.126

1.126

1.126

1.127

1.127

1.127

2.90 ]

1.127

1.128

1.128

1.128

1.128

1.129

1.129

1.129

1.129

1.130

3.00 1

L. 130

1.130

1.130

1.131

1. 131

1.131

1.131

1.132

1.132

1.132

3.10 ]

..132

1.132

1. 133

1. 133

I. 133

1. 133

1.134

1.134

1.134

1.134

WATER CONTENT 490 PERCENT

DG

1.70 ]

L.075

1.076

1.076

1.077

1.078

1.078

1.079

1.080

1.080

1.081

1.80 1

L.081

1.082

1.083

1.083

1.084

1.084

1.085

1.086

1.086

1.087

1.90 ]

1.087

1.038

1.088

1.089

1.089

1.090

1.091

1.091

1.092

1.092

2.00 1

L.093

1.093

1.094

1.094

1.095

1.095

1.096

1.096

1.096

1.097

2.10 ]

L.097

1.098

1.098

1.099

1.099

1.100

1.100

1. 101

1.101

1.101

2.20 1

L.102

1.102

1.103

1. 103

1. 104

1.104

1.104

I. 105

1.105

1.106

2.30 ]

L.106

1.106

1.107

1.107

1.107

1.108

1.108

1.109

1.109

1.109

2.40 ]

L. 110

1.110

1.110

1.111

1. Ill

1.111

1.1 12

1. 112

1.113

1.113

2.50 1

L.113

1.114

1. 114

1.114

1.115

1.115

1.115

1.116

1.116

1.116

2.60 ]

1.116

1.117

1.117

1.117

1. 118

1.118

1.118

1. 119

1.119

1.119

2.70 ]

1.119

1.120

1. 120

1.120

1.121

1.121

1.121

1.121

1.122

1.122

2.80 1

1.122

1.123

1.123

1.123

1.123

1.124

1.124

1.124

1.124

1.125

2.90 1

L.125

1.125

1.125

1.126

1.126

1.126

1.126

1.127

1.127

1.127

3.00 ]

L.127

1.128

1.128

1.128

1.128

1.129

1.129

1.129

1.129

1.129

3.10 ]

L. 130

1.130

1.130

1.130

1.131

1.131

1.131

1. 131

1.131

1.132

WATER CONTENT 500 PERCENT

no

1.70

1.074

1.074

1.075

1.076

1.076

1.077

1.078

1.078

1.079

1.0 79

1.80

1.080

1.081

1.081

1.082

1.082

1.083

1.083

1.084

1.085

1.085

1.90

1.086

1.086

1.037

1.087

1.088

1.088

1.089

1.089

1.090

1.090

2.00

1.091

1*091

1.092

1.092

1.093

1.093

1.094

1.094

1.095

1.095

2.10

1.096

1.096

1.097

1.097

1.097

1.098

1.098

1.099

1.099

1.100

2.20

1.100

1.100

1.101

I. 101

1. 102

1.102

1.102

1. 103

1.103

1.104

2.30

1.104

1.104

1.105

1.105

1. 106

1.106

1.106

1.107

1.107

1.107

2.40

1.108

1.108

1.108

1.109

1.109

1.109

1.110

1.110

1.110

1.111

2.50

1.111

1.111

1.112

1.112

1.112

1.113

1.113

1.113

1.114

1.114

2.60

1.114

1.115

1.115

1.115

1.115

1.116

1.116

1.116

1.117

1.117

2.70

1. 117

1.118

1.118

1.118

1.113

1.119

1.119

1. 119

1.119

1.120

2.80

1.120

1.120

1.121

1.121

1.121

1.121

1.122

1.122

1.122

1.122

2.90

1.123

1.123

1.123

1.123

1.124

1.124

1.124

1.124

1.125

1.125

3.00

1.125

1.125

1.125

1.126

1.126

1.126

1.126

1.127

1.127

1.127

3.10

1.127

1.127

1.128

1.128

1.128

1.128

1.129

1.129

1.129

1.129

49

WATER CONTENT 510 PERCENT

OG

1.70

1.072

1.073

1.074

1.074

1.075

1.076

1.076

1.077

1.077

1.078

1.80

1.079

1.079

1.080

1.0 80

1.081

1.081

1.082

1.083

1.083

1.084

1.90

1.084

1.085

1.085

1.086

1.086

1.087

1.087

1.088

1.088

1.089

2.00

1.089

1.090

1.090

1.091

1.091

1.092

1.092

1.093

1.093

1.093

2.10

1.094

1.094

1.095

1.095

1.096

1.096

1.097

1.097

1.097

1.098

2.20

1.098

1.099

1.099

1.099

1.100

1.100

1.101

1.101

1.101

1.102

2.30

1.102

1.102

1.103

1.103

1.104

1.104

1.104

1.105

1.105

1.105

2.40

1.106

1.106

1.106

1.107

1.107

1.107

1.108

1.108

1.108

1.109

2.50

1. 109

1.109

1.110

1.110

1.110

1.111

1.111

1.111

1.112

1.112

2.60

1.112

1.113

1.113

1.113

1.113

1.114

1.114

1.114

1.115

1.115

2.70

1.115

1.115

1.116

1.116

1.116

1.116

1.117

1.117

1.117

1.118

2.80

1.118

1.118

1.118

1.119

1.119

1.119

1.119

1. 120

1.120

1.120

2.90

1.120

1.121

1.121

1.121

1.121

1.122

1.122

1.122

1.122

1.122

3.00

1.123

1.123

1.123

1.123

1.124

1.124

1.124

1.124

1.124

1.125

3.10

1.125

1.125

1.125

1.126

1.126

1.126

1.126

1.126

1.127

1.127

WATER CONTENT 520 PERCENT

OG

1.70

1.071

1.072

1.072

1.073

1.074

1.074

1.075

1.075

1.076

1.077

1.80

1.077

1.078

1.078

1.079

1.079

1.080

1.081

1.081

1.082

1.082

1.90

1.083

1.083

1.084

1.084

1.085

1.085

1.086

1.086

1.087

1.087

2.00

1.088

1.088

1.089

1.089

1.090

1.090

1.091

1.091

1.091

1.092

2.10

1.092

1.093

1.093

1.094

1.094

1.094

1.095

1.095

1.096

1.096

2.20

1.096

1.097

1.097

1.098

1.098

1.0Q8

1.099

1.099

1.100

1.100

2.30

1.100

1.101

1.101

1.101

1.102

1.102

1.102

1.103

1.103

1.104

2.40

1.104

1.104

1.105

1.105

1.105

1.106

1.106

1.106

1.107

1.107

2.50

1.107

1.107

1.10R

1.108

1.108

1.109

1.109

1. 109

1.110

1.110

2.60

1.110

1.110

1.111

1.111

1. Ill

1.112

1.112

1.112

1.112

1.113

2.70

1.113

1.113

1.114

1. 114

1.114

1.114

1.115

1.115

1.115

1.115

2.80

1.116

1.116

1.116

1.116

1.117

1.117

1.117

1.117

1.118

1.118

2.90

1.118

1.118

1.119

1.119

1.119

1.119

1.120

1.120

1.120

1.120

3.00

1.120

1.121

1.121

1.121

1.121

1.122

1.122

1.122

1.122

1.122

3.10

1.123

1.123

1.123

1.123

1.123

1.124

1.124

1.124

1.124

1.125

WATER CONTENT 530 PERCENT

OG

1.70

1.070

1.071

1.071

1.072

1.072

1.

,073

1.074

1.074

1.075

1 .075

1.80

1.076

1.076

1.077

1.078

1.078

1.

,079

1.0 79

1.080

1.080

1.081

1.90

1.081

1.082

1.082

1.083

1.083

1.

,084

1.084

1.085

1.085

1.086

2.00

1.086

1.087

1.08 7

1.088

1.088

1.

,088

1.089

1.089

1.090

1.090

2.10

1.091

1.091

1.092

1.092

1.092

1,

,093

1.093

1.094

1.094

1.094

2.20

1.095

1.095

1.096

1.096

1.096

1.

,097

1.097

1.097

1.098

1.098

2.30

1.099

1.099

1.09°

1.100

1. 100

1

.100

1.101

1. 101

1.101

1.102

2.40

1.102

1.102

1.103

1.103

1.103

1

,104

1.104

1.104

1.105

1.105

2.50

1.105

1.106

1.106

1.106

1.106

1.

,107

1.107

1.107

1.108

1.108

2.60

1.108

1.109

1.109

1.109

1.109

1.

,110

1.110

1.110

1.110

1.111

2.70

1.111

1.111

1.112

1.112

1.112

1.

,112

1.113

1.113

1.113

1.113

2.80

1.114

1.114

1.114

1.114

1.115

1

.115

1. 115

1. 115

1.116

1.116

2.90

1.116

1.116

1.117

1.117

1.117

1.

,117

1.117

1.118

1.118

1.118

3.00

1.118

1.119

1.119

1.119

1.119

1.

.119

1.120

1.120

1.120

1.120

3.10

1.120

1.121

1.121

1.121

1.121

1,

.122

1.122

1.122

1.122

1.122

50

WATER CONTENT 540 PERCENT DG 0 1 2 3

1.70

1.069

1.069

1

,070

1

.071

1.071

1.

072

1.072

1.073

1.074

1.074

1.80

1.075

1.075

1

.076

1

.076

1.077

1,

077

1.078

1.078

1.079

1.079

1.90

1.080

1.08C

1,

,081

I

.081

1.082

1,

082

1.083

1.093

1.084

1.084

2.00

1.085

1.085

1

,086

1

,086

1.087

1.

.087

1.087

1.088

1.088

1.089

2.10

1.089

1.090

1

.090

1

.090

1.091

1 ,

.091

1.092

1.092

1.092

1.093

2.20

1.093

1.094

1,

,094

1,

.094

1.095

I.

095

1.095

1.096

1.096

1.097

2.30

1.097

1.097

1

.098

1

.098

1.098

I

.099

1.099

1.099

1.100

1.100

2.40

1.100

1.101

i

.101

1

.101

1.102

1

.102

1.102

1. 103

1.103

1.103

2.50

1. 103

1.104

I,

, 104

1,

.104

1.105

1<

,105

1.105

1. 106

1.106

1.106

2.60

1. 106

1.107

1

.107

1

.107

1.107

1

.108

1.108

1.108

1.109

1.109

2.70

1.109

1.109

1

.110

1

.110

1.110

1.

.110

1.111

1.111

1.111

1.111

2.80

I. 112

1.112

I,

.112

1<

. 112

1. 113

1,

,113

1.113

1.113

1.114

1.114

2.90

1. 114

1.114

1

.115

1

.115

L.115

1

.115

1.115

1.116

1.116

1.116

3.00

1.116

1.116

1

,117

,117

1. 117

I,

,117

1.118

1.118

1.118

1.118

3.10

1.1 18

1.119

1

.119

1

.119

1.119

I

.119

1.120

1.120

1.120

1.120

WATER CONTENT 550 PERCENT

DG

1.70

1.068

1.068

1.069

1.069

1.070

1.-071

1.071

1.072

1.072

1.073

1.80

1.073

1.074

1.074

1.075

1.076

1.076

1.077

1.077

1.078

1.078

1.90

1.079

1.079

1.080

1.080

1.081

1.081

1.081

1.082

1.082

1.083

2.00

1.083

1.084

1.084

1.085

1.085

1.086

1.086

1.086

1.087

1.087

2.10

1.088

1.088

1.088

1.089

1.099

1.090

1.090

1.090

1.091

1.091

2.20

1.092

1.092

1.092

1.093

1.093

1.093

1.094

1.094

1.095

1.095

2.30

1.095

1.096

1.096

1.096

1.097

1.097

1.097

1.098

1.098

1.098

2.40

1.099

1.099

1.099

1.100

1.100

1.100

1.100

1.101

1.101

1.101

2.50

1.102

1.102

1.102

1.103

1.103

1.103

1.103

1. 104

1.104

1.104

2.60

1.105

1.105

1.105

1.105

1.106

1.106

1.106

1. 106

1.107

1.107

2.70

1.107

1.108

1.108

1.108

1.108

1.109

1.109

I. 109

1.109

1.110

2.80

1. 110

1. no

1. 110

I. 110

1. Ill

1.111

1.111

1.111

1.112

1.112

2.Q0

1. 112

1. 112

1. 113

1.113

1. 113

1.113

1. 113

1. 114

1.114

1.114

3.00

1.114

1.114

1. 115

1.115

1. 115

1.115

1.116

1.116

1.116

1.116

3.10

1.116

1.117

1.117

1. 117

1. 117

1.117

1.118

1. 118

1.118

1.118

WATER CONTENT 560 PERCENT

or,

1.70

1.067

1.067

1.068

1.068

1.069

1.069

1.070

1.071

1.071

1.072

1.80

1.072

1.073

1.07 3

1.074

1.074

1.075

1.075

1.076

1.076

1.077

1.90

1.077

1.078

1.C78

1.079

1.079

1.080

1.080

1.081

1.081

1.082

2.00

1.082

1.082

1.083

1.083

1.084

1.084

1.085

1.095

1.085

1.086

2.10

1.086

1.087

1.087

1.087

1.088

1.08 8

1.089

1.089

1.089

1.090

2.20

1.090

1.090

1.091

1.091

1.0Q2

1.092

1.092

1.093

1.093

1.093

2.30

1.094

1.094

1.094

1.095

1.095

1.095

1.096

1.096

1.096

1.097

2.40

1.097

1.097

1.098

1.098

1.098

1.099

1.099

1.099

1.099

1.100

2.50

1. 100

1. 100

1.101

1.101

1.101

I. 101

1.102

1. 102

1.102

1.103

2.60

1. 103

1.103

I. 103

1. 104

1. 104

1.104

1.104

1.105

1.105

1.105

2.70

1. 105

1.106

I. 106

1.106

1. 106

1.107

1. 107

1. 107

1.107

1.108

2.80

1. 108

1.108

1.108

1.109

1.109

1.109

1.109

1.110

1.110

1.110

2.90

1. 110

1.110

I. Ill

I. Ill

1. Ill

1.111

1.112

1.112

1.112

1.112

3.00

1.112

1.113

1.113

1.113

1.113

1.113

1.114

1.114

1.114

1.114

3.10

1.114

1.115

1.115

1.115

1.115

1.115

1.116

1.116

1.116

1.116

51

WATER CONTENT 570 PERCENT DG 0 I 2 3

1.70

1.065

1.066

1.067

1.067

1.068

1.068

1.069

1.069

1.070

1.071

1.80

1.071

1.072

1.072

1.073

1.073

1.074

1.074

1.075

1.075

1.076

1.90

1.076

1.077

1.077

1.077

1.078

1.078

1.0 79

1.079

1.080

1.080

2.00

1.081

1.081

1.082

1.082

1.082

1.083

1.083

1.084

1.084

1.084

2.10

1.085

1.085

1.086

1.086

1.086

1.087

1.087

1.08 8

1.088

1 .088

2.20

1.089

1.089

1.089

1.090

1.090

1.090

1.091

1.091

1.091

1.092

2.30

1.092

1.092

1.093

1.093

1.093

1.094

1.094

1.094

1.095

1.095

2.40

1.095

1.096

1.096

1.096

1.097

1.097

1.097

1.097

1.098

1.098

2.50

1.098

1.099

1.099

1.099

1.099

1.100

1. 100

1.100

1.101

1.101

2.60

1.101

1.101

1.102

1.102

I. 102

1.102

1.103

1.103

1.103

1.103

2.70

1.104

1.104

1.104

1.104

1.105

1.105

1.105

1.105

1.106

1.106

2.80

1.106

1.106

1.107

1.107

1.107

1.107

1.108

I. 108

1.108

1.108

2.90

1.108

1.109

1. 109

1. 109

1.109

1.109

1.110

1.110

1.110

1.110

3.00

1.110

1. Ill

1.111

1. Ill

1.111

1.112

1. 112

1.112

1.112

1.112

3.10

1. 112

1.113

1.113

1.113

1.113

1.113

1.114

1. 114

1.114

1.114

WATER CONTENT 580 PERCENT DG C 1 2 3

1.70

1.064

1.065

1.066

1.066

1.067

1.067

1.068

1.068

1.069

1.069

1.80

1.070

1.070

1.071

1.071

1.072

1.072

1.073

1.073

1.074

1.074

1.90

1.075

1.075

1.076

1.076

1.077

1.077

1.078

1.078

1.078

1.079

2.00

1.079

1.080

1.080

1.081

1.081

1.081

1.082

1.082

1.083

1.083

2.10

1.083

1.084

1.084

1.085

1.085

1.085

1.086

1.086

1.086

1.087

2.20

1.087

1.088

1.088

1.088

1.089

1.089

1.089

1.090

1.090

1.090

2.30

1.091

1.091

1.091

1.092

1.092

1.0^2

1.093

1.093

1.0°3

1.094

2.40

1.094

1.094

1.094

1.095

1.095

1.0°5

1.096

1.096

1.096

1.096

2.50

1.097

1.097

1.097

1.098

1.098

1.098

1.098

1.099

1.099

1.099

2.60

1.100

1.100

1.100

1.100

I. 101

1.101

1.101

1. 101

1.102

1.102

2.70

1.102

1.102

1.103

1.103

1.103

1.103

1.103

1.104

1.104

1.104

2.80

1.104

1.105

1.105

1.105

1.105

1.106

1.106

1.106

1.106

1.106

2.90

1.107

1.107

1.107

1. 107

1.107

1.108

1. 108

1. 108

1.108

1.108

3.00

1.109

1.109

1.10Q

1.109

1. 109

1.110

1. 110

1. no

1.110

1.110

3.10

1.111

1.111

1.111

1.111

1.111

1.112

1.112

1.112

1.112

1.112

WATER CONTENT 590 PERCENT

DG

1.70

1.063

1.064

1.065

1.065

1.066

1.066

1.067

1.067

1.068

1.068

1.80

1.069

1.069

1.070

1.070

1.071

1.071

1.072

1.072

1.073

1.073

1.90

1.074

1.074

1.075

1.075

1.076

1.076

1.076

1.077

1.077

1.078

2.00

1.078

1.079

1.079

1.079

1.080

1.080

1.081

1.081

1.081

1.082

2.10

1.082

1.083

1.083

1.083

1.084

1.084

1.084

1.085

1.085

1.085

2.20

1.086

1.086

1.087

1.087

1.087*

1.088

1.088

1.088

1.089

1.089

2.30

1.089

1.090

1.090

1.090

1.091

1.091

1.091

1.091

1.0Q2

1.092

2.40

1.092

1.093

1.093

1.093

1.094

1.094

1.094

1.094

1.095

1.095

2.50

1.095

1.096

1.096

1.096

1.096

1.097

1.097

1.097

1.097

1.098

2.60

1.098

1.098

1.098

1.099

1.099

1.099

1.099

1.100

1.100

1.100

2.70

1.100

1. 101

1. 101

1.101

1. 101

1.102

1. 102

1. 102

1. 102

1.103

2.80

1.103

1. 103

1.103

1. 103

1. 104

1.104

1.104

1.104

1.104

1.105

2.90

1.105

1.105

1.105

1.106

1.106

1.106

1.106

1.106

1.107

1.107

3.00

1.107

1.107

1.107

1.108

1.108

1.108

1.108

1.108

1.108

1.109

3.10

1.109

1.109

1.109

1.109

I. 110

1.110

1.110

1.110

1.110

1.110

52

WATER CONTENT 600 PERCENT

DG

1.70

1.063

1.063

1.064

1.064

1.065

1.065

1.066

1.066

1.067

1.067

1.80

1.068

1.068

1.069

1.069

1.070

1.070

1.071

1.071

1.072

1.072

1.90

1.073

1.073

1.073

1.074

1.074

1.075

1.075

1.076

1.076

1.077

2.00

1.077

1.077

1.C78

1.078

1.079

1.079

1.079

1.080

1.080

1.081

2.10

1.081

1.081

1.082

1.082

1.082

1.083

1.083

1.083

1.084

1.084

2.20

1.085

1.085

1.085

1.086

1.086

1.086

1.087

1.087

1.087

1.088

2.30

1.088

1.088

1.088

1.089

1.089

1.089

1.090

1.090

1.090

1.091

2.40

1.091

1.091

1.091

1.092

1.092

1.092

1.093

1.093

1.093

1.093

2.50

1.094

1.094

1.094

1.095

1.095

1.095

1.095

1.096

1.096

1.096

2.60

1.096

1.097

1.097

1.097

1.097

1.098

1.098

1.098

1.098

1.099

2.70

1 .099

1.099

1.099

1.100

1.100

1.100

1.100

I. 100

1.101

1.101

2.80

1.101

1.101

1.102

1.102

1.102

1.102

1.102

1.103

1.103

1.103

2.90

1.103

1.103

1. 104

1.104

1. 104

1.104

1.104

1.105

1.105

1.105

3.00

1.105

1.105

1.106

1.106

1. 106

1.106

1. 106

1. 107

1.107

1.107

3.10

1.107

1.107

1.108

1.108

1.108

1.108

1.108

1.108

1.109

1.109

WATER CONTENT 610 PERCENT

OG

1.70

1.062

1.062

1.063

1.063

1.064

1.064

1.065

1.065

1.066

1.066

1.80

1.067

1.067

1.068

1.068

1.069

1.069

1.070

1.070

1.071

1.071

1.90

1.071

1.072

1.072

1.073

1.073

1.074

1.074

1.075

1.075

1.075

2.00

1.076

1.076

1.07 7

1.077

1.077

1.078

1.078

1.079

1.079

1.079

2.10

1.080

1.080

1.08C

1.081

1.081

1.081

1.082

1.082

1.083

1.083

2.20

1.083

1.084

1.084

1.084

1.085

1.085

1.085

1.086

1.086

1.086

2.30

1.086

1.087

1.08 7

1.087

1.088

1.088

1.088

1.089

1.089

1.089

2.40

1.090

1.090

1.090

1.090

1.091

1.091

1.091

1.091

1.092

1.092

2.50

1.092

1.093

1.093

1.093

1.093

1.094

1.094

1.094

1.094

1.095

2.60

1.095

1.0Q5

1.095

1.096

1.096

1.096

1.096

1.097

1.097

1.097

2.70

1.097

1.098

1.098

1.098

1.098

1.098

1.099

1.099

1.099

1.099

2.80

1.100

1.100

1.100

1.100

1. 100

1.101

1.101

1.101

1.101

1.101

2.90

1.102

1.102

1.102

1.102

1.102

1.103

1. 103

1.103

1.103

1.103

3.00

1.104

1.104

1.104

1.104

1.104

1.105

1.105

1.105

1.105

1.105

3.10

1.105

1.106

1. 106

1.106

1.106

1.106

1.107

1. 107

1.107

1.107

WATER CONTENT 620 PERCENT

DG

1.70

1.061

1.061

1.062

1.062

1.063

1.063

1.064

1.064

1.065

1.065

1.80

1.066

1.066

1.067

1.067

1.068

1.068

1.069

1.069

1.070

1.070

1.90

1.070

1.071

1.071

1.072

1.072

1.073

1.073

1.073

1.074

1.074

2.00

1.075

1.075

1.075

1.076

1.076

1.077

1.077

1.077

1.078

1.078

2.10

1.078

1.079

1.079

1.080

1.080

1.080

1.081

1.081

1.081

1.082

2.20

1.082

1.082

1.083

1.083

1.083

1.084

1.084

1.034

1.085

1.085

2.30

1.085

1.085

1.086

1.0 86

1.086

1.087

1.087

1.087

1.088

1.088

2.40

1.088

1.088

1.089

1.089

1.089

1.090

1.090

1.090

1.090

1.091

2.50

1.091

1.091

1.091

1.092

1.092

1.092

1.092

1.093

1.093

1.093

2.60

1.093

1.094

1.094

1.094

1.094

1.095

1.095

1.095

1.095

1.096

2.70

1.0°6

1.0Q6

1.096

1.097

1.097

1.097

1.097

1.097

1.098

1.098

2.80

1.098

1.098

1.098

1.099

1.099

1.099

1.099

1.099

1.100

1.100

2.90

1.100

1.100

1.101

I. 101

1.101

1.101

1.101

1.101

1.102

1.102

3.00

1.102

1.102

1.102

1.103

1.103

1.103

1.103

1.103

1.104

1.104

3.10

1.104

1.104

1.104

1.104

1.105

1.105

1.105

1.105

1.105

1.105

53

WATER CONTENT 630 PERCENT DG 0 1 2 :

1.70

1.060

1.060

1.061

1.061

1.062

1.062

1.063

1.063

1.064

1.064

1.80

1.065

1.065

1.066

1.066

1.067

1.067

1.068

1.068

1.069

1.069

1.90

1.069

1.070

1.070

1.071

1.071

1.072

1.072

1.072

1.073

1.073

2.00

1.074

1.074

1.074

1.075

1.075

1.075

1.076

1.076

1.077

1.077

2.10

1.077

1.078

1.078

1.078

1.079

1.079

1.079

1.080

1.080

1.080

2.20

1.081

1.081

1.081

1.082

1.082

1.082

1.083

1.083

1.083

1.084

2.30

1.0F4

1.084

1.085

1.085

1.085

1.085

1.086

1.086

1.086

1.087

2.40

1.087

1.087

1.087

1.088

1.088

1.088

1.088

1.089

1.089

1.089

2.50

1.090

1.090

1.090

1.090

1.091

1.0^1

1.091

1.091

1.092

1.092

2.60

1.092

1.092

1.093

1.093

1.093

1.093

1.093

1.094

1.094

1.094

2.70

1.094

1.095

1.095

1.095

1.095

1.095

1.096

1.096

1.096

1.096

2.80

1.097

1.097

1.097

1.097

1.097

1.098

1.098

1.098

1.098

1.098

2.90

1.0<*9

1.099

1.099

1.099

1.099

1.100

1.100

1. 100

1.100

1.100

3.00

1.101

1.101

1.101

I. 101

1.101

1.101

1.102

1.102

1.102

1.102

3.10

1.102

1.102

1.103

1. 103

1.103

1.103

1.103

1. 103

1.104

1.104

WATER CONTENT 640 PERCENT

DG 0123456789

1.70 1.059 1.059 1.060 1.060 1.061 1.061 1.062 1.062 1.063 1.063

1.80 1.064 1.064 1.065 1.065 1.066 1.066 1.067 1.067 1.068 1.068

1.90 1.068 1.069 1.069 1.070 1.070 1.070 1.071 1.071 1.072 1.072

2.00 1.072 1.073 1.073 1.074 1.074 1.074 1.075 1.075 1.075 1.076

2.10 1.076 1.077 1.077 1.077 1.078 1.078 1.078 1.079 1.079 1.079

2.20 1.080 1.080 1.080 1.081 1.081 1.081 1.081 1.082 1.092 1.082

2.30 1.083 1.083 1.083 1.084 1.084 1.084 1.084 1.085 1.085 1.085

2.40 1.086 1.086 1.086 1.086 1.087 1.087 1.087 1.087 1.088 1.088

2.50 1.088 1.088 1.089 1.089 1 . 08« 1.089 1.090 1.090 1.090 1.090

2.60 1.091 1.091 1.091 1.091 1.092 1.092 1.092 1.092 1.093 1.093

2.70 1.093 1.093 1.093 1.094 1.094 1.094 1.094 1.095 1.095 1.095

2.80 1.095 1.095 1.096 1.096 1.096 1.096 1.096 1.097 1.097 1.097

2.90 1.097 1.097 K098 1.098 1.098 1.098 1.098 1.098 1.099 1.099

3.00 1.099 1.099 1.099 1.100 1.100 1.100 1.100 1.100 1.100 1.101

3.10 1.101 1.101 1.101 1.101 1.101 1.102 1.102 1.102 1.102 1.102

WATER CONTENT 650 PERCENT

DG 0123456789

1.70 1.058 1.059 1.059 1.060 1.060 1.061 1.061 1.062 1.062 1.063

1.80 1.063 1.063 1.064 1.064 1.065 1.065 1.066 1.066 1.067 1.067

1.90 1.067 1.068 1.068 1.069 1.069 1.069 1.070 1.070 1.071 1.071

2.00 1.071 1.072 1.072 1.073 1.073 1.073 1.074 1.074 1.074 1.075

2.10 1.075 1.075 1.076 1.076 1.076 1.077 1.077 1.077 1.078 1.078

2.20 1.078 1.079 1.079 1.079 1.080 1.080 1.080 1.081 1.081 1.081

2.30 1.082 1.082 1.082 1.082 1.083 1.083 1.083 1.084 1.084 1.084

2.40 1.084 1.085 1.085 1.065 i.085 1.086 1.086 1.086 1.086 1.087

2.50 1.087 1.087 1.087 I.Q08 1.088 1.088 1.088 1.089 1.089 1.089

2.60 1.089 1.090 1.09C I. "90 1.090 1.091 1.091 1.091 1.091 1.091

2.70 1.092 1.092 1.09T ».~S92 \.0°^ 1.0^3 1.093 ?.0Q3 !..0°3 1.094

2.80 1.094 1.094 1.09' -.194 1 . 0°5 1 . ooc \.095 1.095 1.095 1.096

2.90 1.096 1.096 1.0*6 '.0°6 1.^96 1.097 1.097 1.097 1.097 1.097

3.00 1.098 1.098 1.098 !.*•*•• 1.098 1.098 1.099 1.099 1.099 1.099

3.10 1.099 1.099 1.100 1.100 l.lOO 1.100 1.100 1.100 1.101 1 .101

54

WATER CONTENT 660 PERCENT

OG

1.70

1.057

1.058

1.058

1.059

1.059

1.060

1.060

1.061

1.061

1.062

1.80

1.062

1.063

1.063

1.063

1.064

1.064

1.065

1.065

1.066

1.066

1 .90

1.066

1.067

1.067

1.068

1.068

1.068

1.069

1.069

1.070

1.070

2.00

1.070

1.071

1.071

1.072

1.072

1.072

1.073

1.073

1.073

1.074

2.10

1.074

1.074

1.075

1.075

1.075

1.076

1.076

1.076

1.077

1.077

2.20

1.077

1.078

1.078

1.078

1.079

1.079

1.079

1.079

1.080

1.080

2.30

1.080

1.081

1.081

1.081

1.081

1.082

1.082

1.082

1.083

1.083

2.40

1.083

1.083

1.0*4

1.0 84

1.084

1.084

1.085

1.085

1.085

1.085

2.50

1.086

1.086

1.086

1.086

1.087

1.087

1.087

1.087

1.088

1.088

2.60

1.088

1.088

1.089

1.089

1.089

1.089

1.089

1.090

1.090

1.090

2.70

1.09C

1.091

1.091

1.091

1.091

1.091

1.092

1.092

1.0^2

1.092

2.80

1.092

1.093

1.093

1.093

1.093

1.093

1.094

1.094

1.094

1.094

2.90

1.0Q4

1.095

1.095

1.095

1.095

1.095

1.095

1.096

1.096

1.096

3.00

1.096

1.096

1.097

1.097

1.097

1.097

1.097

1.097

1.098

1.098

3.10

1.098

1.098

1.09 8

1.098

1.099

1.099

1.099

1.099

1.099

1.099

WATER CONTENT 670 PERCENT

n>G

1.70

1.056

1.057

1.057

1.058

1.058

1.059

1.059

1.060

1.060

1.061

1.80

1.061

1.062

1.062

1.063

1.063

1.063

1.064

1.064

1.065

1.065

1.90

1.066

1.066

1.066

1.067

1.067

1.068

1.068

1.068

1.069

1.069

2.00

1.069

1.070

1.070

1.071

1.071

1.071

1.072

1.072

1.072

1.073

2.10

1.073

1.073

1.074

1.074

1.074

1.075

1.075

1.075

1.076

1.076

2.20

1.076

1.077

1.077

1.077

1.077

1.078

1.078

1.078

1.079

1.079

2.30

1.079

1.080

1.080

1.080

1.080

1.081

1.081

1.081

1.081

1.082

2.40

1.082

1.082

1.082

1.083

1.083

1.083

1.084

1.084

1.084

1.084

2.50

1.085

1.035

1.085

1.085

1.085

1.086

1.086

1.036

1.036

1.087

2.60

1.087

1.087

1.087

1.088

1.088

1.088

1.088

1.088

1.089

1.089

2.70

1.089

1.089

1.089

1.090

1.090

1.090

1.090

1.090

1.091

1.091

2.80

1.091

1.091

1.091

1.092

1.092

1.092

1.092

1.092

I.O03

1.093

2.90

1.093

1.093

1.093

1.094

1.094

1.094

1.094

1.094

1.094

1.095

3.00

1.095

1.095

1.095

1.095

1.095

1.096

1.096

1.096

1.096

1.096

3.10

1.096

1.097

1.097

1.097

1.097

1.097

1.0O7

1.098

1.098

1.098

WATER CONTENT 680 PERCENT

OG

1.70

1.056

1.056

1.057

1.057

1.053

1.058

1.059

1.059

1.060

1.060

1.80

1.060

1.061

1.061

1.062

1.062

1.063

1.063

1.063

1.064

1.064

1.90

1.065

1.065

1.065

1.066

1.066

1.067

1.067

1.067

1.068

1.068

2.00

1.068

1.069

1.069

1.070

1.070

1.070

1.071

1.071

1.071

1.072

2.10

1.072

1.072

1.073

1.073

1.073

1.074

1.074

1.074

1.075

1.075

2.20

1.075

1.075

1.076

1.076

1.076

1.077

1.077

1.077

1.078

1.078

2.30

1.078

1.073

1.079

1 .079

1.079

1.080

1.080

1.080

1.080

1.081

2.40

1.081

1.081

1.081

1.082

1.082

1.082

1.082

1.083

1.083

1.083

2.50

1.083

1.034

1.084

1.084

1.084

1.085

1.085

1.085

1.085

1.085

2.60

1.086

1.036

1.086

1.086

1.087

1.087

1.087

1.087

1.08 7

1.088

2.70

1.088

1.038

1.088

1.088

1.089

1.089

1.089

1.089

1.089

1.090

2.R0

1.090

1.090

l.OOO

1.090

1.091

1.091

1.091

1.001

1.091

1.092

2.90

1.092

1.092

1.092

1.092

1.092

1.093

1.093

1.093

1.093

1.093

3.00

1.093

1.094

1.094

1.094

1.094

1.094

1.094

1.095

1.095

1.095

3.10

1.0O5

1.095

1.095

1.096

1.096

1.0O6

1.0O6

1.096

1.096

1.097

55

WATER CONTENT 690 PERCENT

DG 0123456789

1.70 1.055 1.055 1.056 1.056 1.057 1.057 1.058 1.058 1.059 1.059

t.80 1.060 1.0*0 1.060 1.061 1.061 1.062 1.062 1.063 1.063 1.063

1.90 1.064 1.064 1.065 1.065 1.065 1.066 1.066 1.066 1.067 1.067

2.00 1.068 1.068 1.068 1.069 1.069 1.069 1.070 1.070 1.070 1.071

2.10 1.071 1.071 1.072 1.072 1.072 1.073 1.073 1.073 1.074 1.074

2.20 1.074 1.074 1.075 1.075 1.075 1.076 1.076 1.076 1.076 1.077

2.30 1.077 1.077 1.078 1.078 1.078 1.078 1.079 1.079 1.079 1.079

2.40 1.080 1.030 1.080 1.080 1.081 1.081 1.081 1.081 1.082 1.082

2.50 1-082 1.032 1.083 1.083 1.083 1.083 1.084 1.084 1.084 1.084

2.60 1.084 1.085 1.085 1.085 1.035 1.086 1.086 1.086 1.086 1.086

2.70 1.087 1.037 1.087 1.087 1.087 1.088 1.088 1.088 1.088 1.088

2.80 1.089 1.039 1.089 1.089 1.089 1.090 1.090 1.090 1.090 1.090

2.90 1.090 1.0°1 1.091 1.091 1.091 1.091 1.091 1.092 1.092 1.092

3.00 1.092 1.092 1.092 1.0°3 1.093 1.093 1.093 1.093 1.093 1.094

3.10 1.094 1.094 1.004 1.094 1.094 1.095 1.095 1.095 1.095 1.095

WATER CONTENT 700 PERCENT

OG 0123456789

1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 2.50 2.60 2.70 2.30 2.°0 3.00 3.10 1.093 1.093 1.093 1.093 1.093 1.093 1.093 1.094 1.094 1.094

1.054

1.055

1.055

1.056

1.056

1.057

1.057

1.058

1.058

1.058

1.059

1.059

1.060

1.060

1.061

1.061

1.061

1.062

1.062

1.063

1.063

1.063

1.064

1.064

1.064

1.065

1.065

1.066

1.066

1.066

1.067

1.067

1.067

1.068

1.068

1.068

1.069

1.069

1.069

1.070

1.07C

1.070

1.071

1.071

1.071

1.072

1.0 72

1.072

1.073

1.073

1.073

1.073

1.074

1.074

1.074

1.075

1.075

1.075

1.075

1.076

1.076

1.076

1.077

1.077

1 .077

1.077

1.078

1.078

1.078

1.078

1.079

1.079

1.079

1.079

1.080

1.080

1.080

1.080

1.081

1.081

1.081

1.081

1.082

1.082

1.082

1.082

1.082

1.083

1.083

1.083

1.083

1.084

1.084

1.084

1.084

1.034

1.085

1.085

1.085

1.085

1.085

1.086

1.086

1.086

1.086

1.086

1.087

1.087

1.087

1.037

1.087

1.088

1.08 8

1.088

1.038

1.088

1.088

1.089

1.089

1.039

1.089

1.089

1.090

1.090

1.090

1.090

1.090

1.090

1.091

1.091

1.091

1.091

l.OOl

1.091

1.092

1.092

1.092

1.092

1.092

1.092

56

46

Reprinted from Marine Technology Society Journal 5_,

No. 5, 33.

NORTH ATLANTIC - GEOLOGY AND CONTINENTAL DRIFT (A Symposium)

Edited by Marshall Kay

Published by AAPG Press, Tulsa, Okla. 1081 pp; $32.00. Reviewed by: Robert S. Dietz, National Oceanic & Atmospheric Adm., Atlantic Oceanographic and Meteo- rological Lab. 901 S. Miami Ave., Miami, Fla. 33130

This weighty tome is a collection of 66 papers which examines in depth the stratigraphic and structural evidence that the far north Atlantic Ocean has been opened by continental drift. The papers were originally presented in August 1967 at the Gander Conference on "Stratigraphy and Structure Bearing on the Origin of the North Atlantic Ocean." Emphasis is placed upon paleontologic and orogenic-style comparisons between Appalachian foldbelt and presumably formerly contiguous foldbelts in Ireland and Great Britain but which now strike into the Atlantic discordantly. The book contains little information bearing upon marine geology except for a review paper by J.E. Nafe and C.L. Drake on the "Floor of the North Atlantic A Summary of Geophysical Data."

The volume contains the most comprehensive strati- graphic and structural comparison between Newfoundland and the British Isles ever published. It is divided into the following principle topics: (1) introductory papers, (2) the southeastern border of the orogenic belt, (3) the central orogenic belt, (4) the northwestern border of the orogenic belt, (5) late orogenic stratigraphy and structure, (6) arctic regions, and (7) interpretations of drift.

W.H. Harland's proposal for the opening of the far north Atlantic based mainly on studies in Spitzbergen is especially interesting. He advocates an ancestral Atlantic Ocean which closed in the Precambrian or early Paleozoic. The present blocking out of Greenland and the separation of Europe from North America then began in late Cretaceous. His arguments are supported by a series of palinspastic maps.

The scholarly treatise replete with its massive array of references is not easy reading, but it will interest the serious students of land geology and is an excellent source book which any good technical library should hold. With but few exceptions the authors appear to accept the probable validity of continental drift controlled by the process of sea floor spreading.

47

Reprinted from Meteoritics 6, No. 4, 258-259 .

SHATTER CONES (SHOCK FRACTURES) IN ASTROBLEMES

Robert S. Dietz

NOAA, Atlantic Oceanographic and Meteorological Laboratories, Miami, Florida 33130

Shatter cones, conical shock fractures, are known from more than a score of crypotoexplosion structures, presumed to be astroblemes (ancient meteorite or comet-head impact scars) around the world. These structures include: Steinheim Basin and Ries Basin in Germany; Vredefort Ring in

South Africa; Gosses Bluff in Australia; Rochechouart in France; Kentland, Wells Creek Basin, Crooked Creek, Serpent Mound, Flynn Creek, Sierra Madera, Decaturville, and Middlesboro in the U.S.A., and at Sudbury, Manicouagan, Nicholson Lake, Carswell Lake, Clearwater Lake West, Lake Mistastin, and Charlevoix in Canada. In addition, they occur at Kaalijarv and Lake Bosumtwi, modern meteorite craters. In addition to indicating shock overloading in excess of that which can be created by any endogenic explosion (e.g., cryptovolcanism), they permit vectoring of the force field since their formation precedes disruption and the cones point toward the oncoming shock wave. At several locations (Vredefort, Sudbury, Decaturville, Wells Creek, Sierra Madera, Kentland, Gosses Bluff and Charlevoix) they indicate that the explosion focus (ground zero) was either from above and/or inward toward the center of the structure. At Charlevoix, the finding of shatter cones by Rondot led to the discovery of the cryptoexplosion structure. Shatter cones are an especially useful criterion of shock in carbonate terranes, where shock metamorphic effects commonly are absent. Recently, Alexander and Hawk have used shatter cone distribution at Wells Creek Basin and Vredefort to compute the total energy of impact. Other aspects of the shatter cone criterion for astroblemes are reviewed. There remains little doubt but that, when shatter cones can be identified with certainty, they are a valid and definitive criterion for an astrobleme.

258

Reprinted from Meteoritics 6, No. 4, 259-260.

SUDBURY ASTROBLEME: A REVIEW

Robert S. Dietz

NOAA, Atlantic Oceanographic and Meteorological Laboratories Miami, Florida 33130

The Sudbury Basin in Ontario, Canada, is a now widely accepted astrobleme, or meteorite impact scar, created about 1700 m.y. ago. Evidence is provided by shatter coning, shock metamorphic effects, the Sudbury breccia, "geologic overkill," etc. A thick deposit of impact microbreecia (Onaping suevite) also was laid down in the crater. This astrobleme is of unusual interest not only because of its economic importance (dominating the world's nickel production), but also because extensive magmatism was associated with the impact, creating an extrusive lopolith. The origin of the so-called sublayer is now of critical importance in understanding the Sudbury event. The sublayer, composed of "quartz diorite," breccia and sulfides, forms a liner to the crater and invades the surrounding country rock as a spokelike injection extending 10 km or more. The sublayer appears to be the product of splash emplacement, a mixture of bolide and target rock injected just prior to the extrusion of the lopolith. It seems possible that the sulfide ores may be, at least in part, cosmogenic, derived from the substance of the bolide. The history of the Sudbury Basin as an astrobleme is also reviewed. The significance of shatter coning as evidence of shock, for reconstructing the force vector field, and for unraveling the timing of the event is also emphasized.

259

Reprinted from American Scientist 59_, No. 5, 627

49

MAXWELL, Arthur E., ed. The Sea: Ideas and Observations on Progress in the Study of the Seas. Vol. 4: New Concepts of Sea Floor Evolution. Part 1 : 791 pp. Part 2: 664 pp. Wiley-Interscience, 1970. $32.50 each.

This weighty and comprehensive volume of invited papers by 77 authors covering recent advances in our understanding of the ocean floor marks a major milestone. Its contents emphasize that a modern scientific revolution has been wrought by the new model of the earth based on plate tectonics and sea floor spreading. The ocean basins are young; they are born, expand, contract, and die while the con- tinents live on. The authors have been carefully chosen for their eminence, and the contents reveal that marine geology and geophysics is dominated by American scientists. Some papers jointly offered by American and Russian authors indicate a new level of workable collaboration be- tween the East and the West.

Volume 4 is subdivided into two tomes: the first, which concerns general observa- tions, contains 20 articles that treat the ocean floor worldwide on a discipline basis. Included are papers on marine geodesy; acidic, basic, and ultramafic rocks of the ocean floor; gravity; magnetic reversal anomalies; seismic reflection and refraction; paleomagnetism; seamount magnetism; gravity; heat flow; earth- quakes and tectonics; pre-Quaternary microfossil distribution ; etc.

The second tome describes the ocean floor regionally. Among its 14 articles are 5 on the Pacific floor, while the others cover most of the other oceans of the world. Two thorough papers on the structure of the little-known Indian Ocean and the Mediterranean basin are especially wel- come. A final part, which offers new con- cepts, contains a paper on sea floor spread- ing, by Fred Vine and the late Harry Hess, and one by J. Tuzo Wilson on transform faults.

Shortcomings are few in this excellent volume, but some may be noted. (1) In these times of voluminous literature, ab- stracts seem essential, but there are none. (2) The lack of any treatment of the Atlan- tic basin leaves a gap in an otherwise balanced regional coverage of the ocean floors of the world. (3) The high price places the volume beyond the grasp of most individual researchers, let alone the impecunious student. Thus, this series will serve only as a library source book and not as a replacement for the classic textbook The Oceans, arr avowed original intention. (4) The long delay between receipt of manuscripts (2-3 years) and the availabil- ity of the book means that the papers are somewhat out of date. (The volume is dated 1970, but actually was not available until spring 1971.) Fortunately, the papers were prepared after the 1967 sweeping conversion of marine geologists to sea floor spreading and plate tectonics. There is, however, no impact of the JOIDES (deep-sea drilling program) results. (5) Typographical errors are rather numer- ous.— Robert S. Dietz, Environmental Science Services, U. S. Department of Commerce

1971 September-October 627

50

Reprinted from Sea Frontiers 17, No. 4, 204-212

Those Shifty Continents

By Robert S. Dietz NOAA, Atlantic Oceanographic and Meteorological Laboratories

Miami, Florida

During the past decade, the con- cept of continental drift has undergone a remarkable transforma- tion from an outrageous hypothesis, through a period of nagging reapprais- al and finally to verification. The reality of drift is no longer questioned by the large majority of earth scientists but many problems remain unresolved. Most importantly, when did this drift begin and where were the continents in the beginning? In short, we need to understand the pattern of the conti- nental breakup and dispersion in space and time.

In modern context, continental drift is simply a necessary consequence of the even grander theory of plate tectonics. The term tectonics refers to the slow geological motions of the earth crust (up, down or sideways) and also to compressional folding and ex- tensional rifting. This concept holds that the earth's outer crust is divided into about nine major rigid plates, or spherical caps, separated by seams

something like the segments on a tur- tle's carapace. These 60-mile-thick plates are in slow but inexorable motion and they interact along their bound- aries, causing earthquakes among other things, in the process. The 22- mile-thick continents are granitic "plateaus" embedded within the plate. With the exception of the Pacific plate, each plate contains a continent, if India is included as a subcontinent. As the plates move so must the continents that ride piggyback upon them.

A Humpty-Dumpty Problem

We now believe that about 200 mil- lion years ago the continents were all joined together, forming the super- continent of Pangaea, meaning "all earth." Although the solution is not straightforward, we can in principle solve this jigsaw reconstruction or "Humpty-Dumpty" problem, and fit all of the continents back together again. We cannot do this for the plates since they change their size and shape.

204

The continental drift concept is not new. Reproduced here in lithograph is the first depiction of the drift opening of the Atlantic Ocean in The Creation and its Mysteries Explained: A Treatise. ..which Explains the Origin of America and its Primitive In- habitants, by A. Snider, published in Paris in 1859. Snider supposed that the Atlantic Ocean did not exist prior to the biblical flood. During the Deluge great volcanoes erupted which split off the Americas along with the island of Atlantis both of which drifted westward. Snider argued, by a series of farfetched assumptions, that the Americas somehow escaped the Deluge and were not covered with water. The ante- diluvian population therefore escaped the catastrophe and eventually evolved into the indigenes found by the European explorers. Snider concluded that "L'Amerique est reellement I'ancienne Atlantide de I'epoque antediluvienne," or "America is really the ancient Atlantis of antediluvian times."

They can grow either larger or smaller by adding new crust or resorbing old crust. The growth occurs at the so- called mid-ocean ridges, where the plates are pulled apart and new lava from the earth's mantle rises into the crack. The process may be likened to the freezing of newly exposed water as ice floes drift apart.

Where the Crust is Sucked In

Resorption of crust occurs in trenches or subduction (lead down) zones, those areas where the crustal plate dives steeply into the earth's mantle. Those rock components that are fusible in the earth's hot mantle rise again, causing volcanic activity, granitic intrusions and mountain build- ing. These subduction zones are found in the Pacific trenches and a line of filled trenches extending from Gibral- tar through the Himalayas to New Guinea known as the great Tethys subduction zone.

We may visualize the ideal crustal plate as being rectangular with a rift (a mid-ocean ridge) and a trench forming one pair of opposing margins. The other two opposing sides would be great shear zones, called transform faults, which are regions of slippage, along which crust is neither made nor destroyed, but rather conserved. An example well known to Americans is the San Andreas fault, which strikes through California and is a portion of the margin of the Pacific plate. Slip- page along this plate boundary was re- sponsible for the disastrous San Fran- cisco earthquake of 1906.

This remarkable new understanding of the earth, as important to geology (Continued on page 210)

Continental drift as envisioned by Al- fred Wegener, in his book Origin of Con- tinents and Ocean Basins. This volume was published in 1929, just prior to his death on the Greenland ice cap, where he had gone to prove by precise geodetic measurements that this subcontinent was drifting westward. Wegener first formal- ized the concept of drifting continents and is regarded the founder of the drift hypothesis. Considering its vintage, Wege- ner's idea that the world's land masses emerged from the single continent of Pangaea (a name he coined) was remark- ably precocious.

Wegener's interest in drift was trig- gered by "the direct impression produced by the congruency of the coastlines on either side of the Atlantic." Accordingly he fitted the continents together as in a jigsaw puzzle, but he distorted their out- lines. The enlargement of India is a good example. He also considered India as always being an integral part of Asia. The stippled areas in the lowest diagram are modern continental shelves.

Wegener's timing of the initial break- up of Pangaea (Upper Carboniferous, or 300 million years ago) is somewhat earli- er than the late Triassic breakup (200 million years ago) proposed by modern theorists. Wegener also erroneously sup- posed that much of the drifting occurred late in geologic time with Europe remain- ing attached to Greenland until about 1 million years ago. He also considered Africa and Eurasia to be fixed in position and used an arbitrary map grid. He ac- commodated the northward motion of India simply by the distortion of Eurasia.

206

UPPER CARBONIFEROUS

EOCENE

LOWER QUATERNARY

I: End of Permian, 225 million years ago

Map$ adapted from Journal of Geophysical Research

2: End of Triassic, 190 million years ago 3: End of Jurassic, 135 million years ago

4: End of Cretaceous, 65 million years ago

5: Today

A much simplified series of drawings which depict the breakup of Pangaea accord- ing to R. S. Dietz and John C. Holden, adapted from the original presentation in J. Geophysical Research (1970:75: p. 4939). The universal landmass is believed to have undergone initial separation into the supercontinents of Laurasia (northern group) and Gondwana (southern group) in the late Triassic, 200 million years ago. An east- west rift near the equator opened the proto-North Atlantic Ocean. Simultaneously the Indian Ocean commenced forming as well. In general, the new world has drifted westward while the continents surrounding the Indian Ocean (Africa, India and Australia) moved northward. Although his mechanisms for drift are no longer ac- cepted, Wegener interestingly proposed a "westward wandering" and a "flight from the poles." These maps confirm this westward drift but Wegener's flight from the poles is replaced as a drift from the south pole only.

This time-sequence map series is the first attempt ever to show the past positions of continents in absolute geographic coordinates. To achieve this absolute tracking of the continents, Dietz and Holden used as fix markers lavas thought to be derived in ascending plumes from the earth's deep mantle. Unlike earlier reconstructions none of the continents remain anchored in position, although Antarctica has moved rela- tively little. India and Australia have undergone exceedingly fast drift rates of more than 4 inches per year. Although moving at a slower rate of about 1 inch per year, North America has nevertheless drifted northwestward for 5,000 miles. (This drift rate is about equivalent to the length of a human body in a lifetime.) New York, now at 40°N latitude, originally was near the equator. The last major event was the detach- ment of Australia from Antarctica only 45 million years ago. The Himalaya Mountains were pushed up when India struck the underbelly of Asia about 25 million years ago.

The Atlantic Ocean is wholly new with the central North Atlantic opening first, the South Atlantic opening second, and finally, with the detachment of Greenland from Europe, the far North Atlantic opened and created a passage into the Arctic Ocean. The Indian Ocean is a complex basin created by the repositioning of landmasses asso- ciated with the closing of the Tethys Sea a huge embayment which once extended westward from the ancestral Pacific Ocean. Although still covering nearly a full hemi- sphere, the Pacific is growing ever smaller. Drift theorists call the ancestral Pacific Panthalassa, meaning universal sea.

To help clarify the breakup of Pangaea, two well-known oceanic landmarks, the Antilles and the Scotia arcs, are placed in their modern position on all of the charts. Also, for best centering of the landmasses, the vertical center line of the projection is the 20° E longitude meridian rather than Greenwich.

as the theory of evolution was to biol- ogy, was preceded by two develop- ments in the study of terrestrial magne- tism. The first involves detecting the changes in the position of the earth's magnetic pole (the polar method), and the other, reversals of the earth's magnetic field (the reversal method). These were critical to the ultimate proof of continental drift.

Where Did the North Pole Go?

In the late 1940's, scientists recog- nized that certain rocks, especially ancient lavas, are in effect "fossil com- passes." As freshly extruded lava cools through the Curie point at about 575° C, an imprint of the earth's magnetic field, as it existed at that point in time, is "frozen in.*' By collecting oriented samples of ancient lavas, specialists in paleomagnetism have clearly shown that these "fossil compasses" generally give a different solution for both the direction and the dip of the North Magnetic Pole than does a modern compass needle placed on the point from which the lava sample was taken. Some of these differences (but not-all) , established through thousands of mea- surements, could only be explained if continents had drifted.

As with many scientific techniques, there are significant limitations. The earth's surface is curved, so that three coordinates are needed to establish a fix on the globe. The "fossil compasses" of paleomagnetism can only provide orientation and magnetic latitude; longitude remains forever indetermi- nate. In the same way the navigator at sea with only a dip compass can, in principle, roughly determine his orien- tation with respect to the geographic

grid as well as his magnetic latitude but not his longitude. Unfortunately, using paleomagnetism no one has dis- covered as yet the equivalent of the chronometer, which makes the deter- mination of a ship's longitude possible. Because of this restriction, many scien- tists remained skeptical of the paleo- pole position evidence for continental drift.

Fortunately, an even more powerful method magnetic reversal was dis- covered within the past decade. In the late fifties, extensive regions of the ocean floor were first found to be char- acterized by strongmagnetic anomalies, or departures from the earth's normal ambient magnetic field. These were dis- posed in horizontal patterns like zebra stripes. British workers soon realized that these could be explained as growth increments of new ocean crust being added as the crustal plates spread apart at the mid-ocean ridges. There also was good evidence to show that the earth's magnetic poles flipped, with the North Magnetic Pole becoming the South Magnetic Pole and vice versa, every million years or so. This flipping is related to circulation patterns within the earth's nickel-iron core and not to any geographic tipping of the earth. With each flip a new anomaly is added to the pattern of a spreading ocean floor so that large regions of the ocean floor acted like a magnetic tape re- corder. It soon became possible to measure quite precisely the horizontal shifts of the plates a new dimension to which terrestrial geology was blind. We now have a magnetic chronology, rather analogous to the method of aging trees by ring counting, which extends 80 million years back in time.

210

The African crustal plate, upon which the continent of Africa is superimposed, is depicted in this diagram. Throughout its history the African plate has drifted north- ward and rotated counterclockwise. The plate is bordered on three sides by the Pan- African rift system, which has acted at various times as both a shear zone (especially on the Indian Ocean side) for accommodating the shifting of the plate, and a zone of sea floor spreading (especially on the Atlantic side) where new ocean floor has been extruded. The northward drift of the African plate is accommodated by a descent and resorption of the outer crust of the earth into the Tethyan trench system, a remnant of which now lies beneath the Mediterranean Sea. (Drawing by John C. Holden)

Thus it is now known that the earth's crust not only goes up and down but also moves sideways. The horizontal velocities of a few centimeters per year are slow by human standards, but they are ten, one hundred or a thousand times faster than other grand geologic processes like the rising of mountains, subsidence of land masses or the ero- sion of continents. It has long been known that Florida and the adjacent Bahama platform reveal a long history of continued subsidence of a few miles over the past 150 million years. But geologists have only recently realized that during this same interval these crustal blocks have drifted northwest- ward for more than 3,000 miles. When added to the vertical displacements and time the substance of classical geol- ogy— this new horizontal drift gives earth history a fourth dimension and increases its complexity.

Rewrite the Texts

The textbooks are now being re- written to incorporate this new mobil- istic philosophy, and an exciting era has come to the earth sciences. Practi-

cal benefits may ensue, once we under- stand the plate motions in detail. For example, it should then be possible to predict earthquakes with some preci- sion. A step in this direction was made recently by Robert Wallace of the United States Geological Survey. By analyzing the motions along Califor- nia's San Andreas fault, he predicts that there will be an important earth- quake every five years and a large earthquake every 15 years. A really disastrous quake, like that which shook San Francisco in 1906, will occur once each century.

ADDITIONAL READING

Other articles on continental drift that have appeared in Sea Frontiers:

Pothier, R. J. "Deep Sea Drilling Rec- ord," Vol. 14, No. 6, page 322.

Dietz, R. S. "More About Continental Drift," Vol. 13, No. 2, page 66.

Runcorn, S. K. "Corals and the History of the Earth's Rotation," Vol. 13, No. 1, page 4.

Creer, K. M. "Continents on the Move," Vol. 12, No. 3, page 148.

212

Reprinted from Earth-Science Reviews 7_

No

A9-A15

51

PORTRAIT

OF A SCIENTIST

FRANCIS SHEPARD

ROBERT S. DIETZ1 and K.O. EMERY2

Where Alph, the sacred river ran/ Through caverns measureless to man/ Down to the sunless sea. . . .

Coleridge

Geology has undergone a revolution during the past decade paced by discoveries about the ocean floor and this is where the geologic action is. To a significant degree, this revolution can be traced to one man, Francis Parker Shepard. His researches and those of his many students, numbering more than threescore, have left an indelible imprint on marine geology.

Francis P. Shepard (now Professor Emeritus of Submarine Geology at Scripps Institu- tion of Oceanography of the University of California at San Diego), a native of Brookline, Massachusetts, received his AB from Harvard University in 1920 and his PhD in 1922 from the University of Chicago. From 1923 to 1937 he was a faculty member of the University of Illinois, but his growing commitment to submarine geology drew him to the Scripps Institution of Oceanography at La Jolla, California firstly part time, and then full time after World War II. During the war years he served with the University of California Divi- sion of War Research, making sediment studies to help understand the behavior of under-

National Oceanic and Atmospheric Administration, Atlantic Oceanographic and Meteorological La- boratories, Miami, Florida. 2Woods Hole Oceanographic Institution, Woods Hole, Massachusetts

A9

water sound in relation to submarine detection, and compiling shelf sediment charts of foreign areas to support military operations. With the termination of hostilities, he re- turned to Scripps Institution where he has remained even after his retirement in 1966, and where he now continues to actively pursue his interests in marine geology.

A PROFILIC WRITER

Shepard's eminence derives from his cascade of scientific papers numbering nearly 200, plus several books. This output reflects his boundless energy and enthusiasm. Sub- marine Geology (Harper and Row) now is the standard text in the field. It was first pub- lished in 1948, went into a completely rewritten second edition in 1963, and a third edition is now under preparation. He also authored the popular book, The Earth Beneath the Sea (Johns Hopkins Press) in 1959, which has recently been reissued. In 1966 he pub- lished Submarine Canyons and Other Sea Valleys with Robert F. Dill as co-author. Ear- lier he also edited the monograph, Sediments of the Northwest Gulf of Mexico, published by the American Association of Petroleum Geologists. This was a byproduct of the Ameri- can Petroleum Institute's Project 51, which he directed from 1951 to 1957, on the paralic and deltaic sedimentation along the Gulf coast1 . Currently in press is Our Changing Coastlines, written with the late Harold R. Wanless. This book examines the coastline changes around the United States, including Alaska and the Hawaiian Islands, by com- paring early charts and aerial photographs with their modern counterparts. It is a final chapter in a theme which Shepard has pursued throughout his life the geomorphology and classification of shorelines. Early in his career he led the breakaway from the then widely accepted genetic shoreline classification of Douglas Johnson after William Morris Davis' philosophy of historical sequences.

ORIGINAL IDEAS

Among the many original ideas which can be ascribed to Shepard are the following: (1) troughs and fjords of shelves in high latitudes resulted primarily from glacial erosion and not from faulting; (2) the pattern of shelf sedimentation is complex, and beyond the surf zone there is no general gradation of sediments from coarse to fine across continental shelves; (3) submarine canyons are maintained by periodic and sudden removal of clog- ging sediments; (4) the shelf-edge topographic highs and much of the slope relief of the continental margin off Texas are related to salt intrusions; (5) undertow is largely a myth, and rip currents are responsible, instead, for numerous drownings; (6) tsunamis are mostly the direct result of fault displacements rather than of landslides; and (7) there has been no high stand of sea level associated with a climatic optimum during the Holocene.

To Shepard, geology is an observational and descriptive science. He is skeptical of highly sophisticated theoretical analysis and is impatient with oblique contemplation of of the sea from ivory towers. He prefers to overwhelm a problem by an extensive collec- tion of data. Utilizing T.C. Chamberlain's principle of multiple working hypotheses, Shepard, in turn, likes to set up "truth tables," listing the points for or against any idea. His predilection is to jump on his horse (or, rather, ship) and go and see. He develops his views in the field rather than accepting answers recorded in authoritative books, thus "counting the lion's teeth instead of consulting Aristotle."

Of iconoclastic bent, many of Shepard's early writings were directed towards proving that some accepted principle of geology (such as periodic diastrophism) is wrong. His doctoral dissertation on the structural geology of the Rocky Mountain trench proposed that this feature was not a graben, as previously supposed, but even in one place a horst. R.A. Daly and R.T. Chamberlain, his early mentors at Harvard and Chicago respectively, were among those with whom Shepard quickly found reason to disagree. An interesting A10 footnote to this background is that Shepard in 1966 followed Daly as the next American

recipient of the coveted Wollaston Medal of the Geological Society of London. It had been bestowed on Daly in 1942.

SHIPBOARD OBSERVATIONS

Shepard's focus on shipboard observations beginning in the early thirties marked a change of method in marine geology. He had developed an early love for the sea aboard his father's yacht out of Marblehead, Massachusetts. The spark that propelled him into marine geology was his observation that the sediment samples he collected with the yacht off the New England coast strikingly disagreed with the classical dogma that they would become finer grained offshore and toward a "wave base" marked by the shelf break. Once bitten by the taste of the sea, Shepard never returned to classical geology. He kept ties to the land, however, for he became a "green-water" marine geologist, confining his inter- ests largely to the shoreline, the shelf and slope, and especially the precipitous canyons which incised the continental slope. He became a marine geologist and not a geological oceanographer and has treated marine geology as an extension of land geology.

Shepard's canyon studies had modest beginnings a rowboat, a sounding line, and a sextant. With these simple tools, he made repetitive surveys in the nineteen-thirties of several canyon heads along the California coast. His report that some canyon heads had deepened or shoaled within a six-month interval was at first dismissed with a smile. Were they not due to surveying inaccuracies?2 Shepard's findings subsequently have been fully verified. Some of the canyon heads gradually fill with sand and then are periodically cleaned out by some process which still is not fully understood.

Shepard has never been a man with a "greasy thumb" and has little patience with com- plex mechanical gadgets, let alone electronic black boxes. He likes to rely solely upon simple devices which are foolproof and have stood the test of shipboard use. One master- stroke of simple instrumentation was dispatching 2m-high Roger Revelle (later Director

Fig. 2. Francis Shepard inspecting the Westinghouse Deepstar 4000, a deep-research vehicle, just prior to a dive into Mississippi Submarine Trough. Commencing with dives in Cousteau's Diving Saucer in 1964, Shepard has carried out a program of visual studies of submarine canyons. (Photo by Ron Church.)

All

of Scripps Institution of Oceanography) into the surf zone to act as a calibrated wave staff. This interest in simplicity probably in part stems from his involvement in attempting to develop, in the mid-nineteen-thirties a highly touted hydrostatic corer which would utilize the ambient pressure of the deep ocean to drive a core barrel into the bottom. On its first deep trial off California, this device imploded, and all that was recovered was the cable's frayed bitter end. This loss virtually wiped out the instrumentation funds in Shepard's grant for studying canyons off the California coast.

Over the years, the techniques of marine geology have, of course, become ever more sophisticated. By 1966 it was even possible for Shepard to break away from remote sensing and directly inspect the La Jolla Submarine Canyon off California through the portholes of the Cousteau diving saucer. He describes this as "a thrilling experience and the greatest day in my life."

A TURNING POINT IN MARINE GEOLOGY

A turning point in Shepard's career was a $10,000 grant in 1936 from the Penrose Fund of the Geological Society of America for investigating the submarine canyons off California. This was a large grant for those years and the largest ever granted to that date by the G.S.A. With these funds, Shepard was able to use the oceanographic research ship, "E.W. Scripps", for six months, support two student assistants (the authors of this article), and supply the equipment needed. Along with H.C. Stetson's studies during the same period at Woods Hole Oceanographic Institution, this effort founded sea-going marine geology in the United States. A spate of papers resulted from this research, including the monograph, Submarine Topography off the California Coast: Canyons and Tectonic Inter- pretation (GSA Special Paper No. 31, with K.O. Emery). With a follow-on G.S.A. grant, Shepard in 1940 did extensive work in the Gulf of California.

Shepard is perhaps best known for his vigorous espousal of the belief that submarine canyons resulted from river cutting when the continental slopes were exposed due to lowering of sea level as much as 2000m during the Pleistocene. Many sharp exchanges of opinion were published by Shepard and his antagonists, who included Daly and D.W. Johnson, but eventually the turbidity-current origin won the dominating role in the origin of these canyons. To err is human, and Shepard retracted his hypothesis once suffi- cient data accumulated to show that it was not tenable. He now believes that a highly complex set of processes have been at work in submarine canyons, including not only modest sea level lowering and turbidity currents, but also many other types of water cur- rents and mass movements. His recent work has been directed toward learning more about the transportation of sands from shallow to deep water, on cable breaks associated with turbidity currents, and on the scouring of canyon walls by creeping sand masses. In his treatise on submarine canyons, he has modestly written, "The book. . . should be considered only an installment in a continued story."

In association with Hans Suess, Shepard in 1956 made a classic study of the post- glacial rise of sea level using radiocarbon dating. Recently he led a large team investigation to the coral reefs of the west Pacific Ocean, Daly's type locality for his plus-two-meter Holocene high sea level during the so-called Climatic Optimum*. This team found no sup- porting evidence of any such high stand as advocated in recent years by Rhodes Fair- bridge and others.

PROFOUND LOVE OF THE SEA

When not actually at sea, Shepard prefers to work within the sight and sound of the surf. This attachment for the sea cost Shepard the first draft of his textbook on sub- marine geology and nearly his life, as well. In 1946 while writing the manuscript, he was A12 living in a small cottage on the north coast of Hawaii. When the April 1 tsunami, triggered

o o

E

o

A13

by an earthquake in the Aleutian trench, struck, his wife, Elizabeth, quickly retreated to high ground. Shepard himself incautiously remained behind to observe and photograph this rare natural phenomenon. The cottage was completely demolished, the manuscript was washed away, and only by climbing a tree was he able to avoid being washed away by the inundating eighth wave. With characteristic energy and enthusiasm, Shepard (with D.C. Cox and G.A. MacDonald) immediately initiated a now-classic investigation of the coastal effects of that tsunami on the Hawaiian Islands.

Fig. 4. F.P. Shepard as a Navy cadet at Harvard with his future bride, Elizabeth Buchner. World War I ended before Shepard was called to duty overseas.

A14

Surely we can identify Shepard as the first American marine geologist3 . During the late nineteen-thirties, when the submarine-canyon controversy was raging, Shepard was the only participant who had actually ever sounded and sampled a submarine canyon. Shepard's approach has always been direct as he quickly moved to the ocean's edge and grappled intimately with his chosen subject. His overall time at sea must run about five years and there probably are few oceanographers who have spent any more than this on a rolling deck. His wife, Elizabeth, has accompanied him on many of these cruises, espe- cially in recent years, in a supporting role such as monitoring the echo sounder.

HONORS AND RECOGNITION

In 1964 Shepard's students presented him with a book of their papers in his honor entitled Papers in Marine Geology: Shepard Commemorative Volume (Macmillan).4 To keep this effort a secret until published it was given the code name "Project Sextant" in recognition of Shepard's numerous hydrographic surveys in which he utilized this instru- ment. Shepard has received many other honors including an honorary DSc from Beloit College in 1968. In 1968 he was also selected as the San Diego Man of Distinction in rec- ognition of his scientific achievements. From 1958 to 1963 he was President of the Inter- national Association of Sedimentologists and presided over the Association's general meetings at Copenhagen in 1960 and at Amsterdam in 1963. He is a member or fellow of many scientific societies which are too numerous to list here.

A signal honor and token of high regard by his colleagues was the recent establishment of an award in his name by the Society of Economic Geologists. The SEPM has designated it as the Francis P. Shepard Award for Excellence in Marine Geology. It is presented usually annually to an outstanding marine geologist, based on "excellence in marine geology, with primary consideration for excellence in those fields for which Professor Shepard has be- come well known. These fields are the distribution and characteristics of sediments, marine geomorphology, and structure of the continental margins of the world".

Shepard's accomplishments of the past are part of a continuing series. Retirement means little other than providing more unfettered time for marine studies. Judging from the longevity of his parents, Shepard has yet several decades of productivity. We look forward to reading the results of this work.

REFERENCES AND NOTES

1. (see page A10) During this period, one of his students, Harris B. Stewart, composed a poem entitled "An Ode to F.P. Shepard's 100th Reprint* - or, One Sansicle, Please, and No Mud.V

We had drinks and hors d'oeuvres from the platter / The Department was there to a man

It was during a lull in the chatter / That Shepard put forth his new plan.

"If clay and silt are contiguous, / And next to the silt is the sand,

Then 'mud' as a term is ambiguous, / And in consequence should be banned.

If a triangle's used in the riddle, / And sand, silt, and clay juxtaposed,

For the triangle left in the middle, /The term 'sansicle' is proposed."

*(We can excuse this inaccuracy as poetic licence, but in the interest of precise reporting

we must point out that the paper in question (Nomenclature based on sand-silt-clay

ratios. /. Sediment. Petrol, 24(3): 151-158, 1954) was actually his 1 12th.)

2. (see page All) As Shepard's student assistants in these early surveys, the authors of this article must now admit nagging doubts about the validity of these surveys. But, after all, are not apprentice scientists supposed to be skeptics?

3. (see page A14) We have hesitated in referring to Shepard as the "father of marine geol- ogy." However, the venerable Madame Klenova of the U.S.S.R. Institute of Oceanology did so upon the occasion of the International Geological Congress in Mexico City in 1956, when the cold war first had thawed sufficiently for Russian scientists to attend such functions. As they met for the first time, Mme. Klenova warmly remarked, "You are the father of marine geology and I am the mother of marine geology." To this, Elizabeth Shepard replied, "And that, in turn, must make me the concubine."

4. (see page A15) In addition to its 24 papers by his students, this volume contains a biographical foreward about Francis P. Shepard, a "Vita," and a listing of his 141 publi- cations to 1961. A15

52

Reprinted from Nature 229 , No. 5283, 309-312.

Pre-Mesozoic Oceanic Crust in the Eastern Indian Ocean (Wharton Basin)?

by

ROBERT S. DIETZ & JOHN C. HOLDEN

ESSA, Atlantic Oceanographic and Meteorological Laboratories, 901 South Miami Avenue, Miami, Florida 33130

A search for ocean basins underlain by old crust has suggested that the Wharton Basin would be a likely place to investi- gate.

There is now great interest in the search for old Earth's crust, not only for the sake of a better understanding of ocean floor evolution but also because such material would be more highly mineralized and the thick cover of sediments would offer enticing prospects for petroleum. In what follows, by "old crust" we mean merely pre-Mesozoic crust, older than 225 m.y. Even this modest antiquity would, however, antedate the great sequence of events beginning with the breakup and dispersion of Pangaea, which probably commenced in mid- Triassic, 200 m.y. ago1.

The half spreading rates associated with seafloor spreading (that is, the spreading on each limb of a spreading mid-ocean rift) of 1-6 cm per year are suggested by the magnetic anomaly growth lines reaching back over the past 4 m.y. If these rates can be extrapolated linearly back in time to anomaly 32 of Heirtzler et cil.2, about half of the ocean floor is of Cainozoic age (less than 65 m.y.)3 except in special situations; nearly all the remainder must be Mesozoic.

The scientific staff on JOIDES (Deep Sea Drilling Project) leg 6 concluded that the North-west Pacific basin was the oldest part of the oldest ocean4. Upper Jurassic sediments (Tithon- ian, 140 m.y.) were encountered in two cores but, by inference, Lower Jurassic or even Triassic ocean floor might be present closer to the Marianas subduction zone. The Philippine Sea, which lies behind the Japan-Marianas-Palau trench system, was found to be young, probably not older than early Caino- zoic. (In deep sea drilling, the assumption is made that the age of the sediments immediately overlying basement basalts, as indicated by seismic reflexion profiling, is the age of the oceanic crust. This interpretation is reasonable if the crust was emplaced according to the seafloor spreading concept.)

The search for Palaeozoic crust was also a primary aim of the recent JOIDES leg 11 off the eastern United States5. Only mid-Jurassic (about 160 m.y.) strata were found, but this is the oldest rock so far recovered from any ocean basin. This makes it unlikely that the Atlantic commenced opening at the beginning of the Permian and that the peripheral quiet magnetic zone of the Central North Atlantic represents crust emplaced in the 50 m.y. long Kiaman interval of constantly reversed magnetic polarity essentially during the Permian6-7. We agree with Vogt et al." that the magnetic quiet zone represents crustal emplacement during the Triassic. The South Atlantic- is clearly younger than the North Atlantic, and so this entire rift ocean (excluding subplates) is unlikely to contain Palaeo- zoic ocean crust.

It is possible, but perhaps unlikely, that the Arctic Ocea i contains old crust. Apparently there was an ancestral Arctic basin within the framework of Pangaea, which we have named Sinus Borealis (Latin for northern embayment)9. The Eurasian Basin, between the Lomonosov Ridge and Eurasia, must be neo-oceanic, for it contains a central spreading rift, an exten- sion of the mid-Atlantic ridge10. Perhaps the Canadian Basin

contains old crust. But a likely history for the Arctic Ocean is that the Alpha Ridge in the Canadian Basin is a "fossil" but now abandoned spreading rift. This old rift then "jumped" to its present location, splitting off a sector of the Eurasian craton (the Lomonosov Ridge) in the process". This would infer that the oceanic crust of the Canadian Basin is not very old, at least in its northern portion. On the other hand, Churkin's12 interpretation, based on the marginal lower Palaeozoic geosynclines of Alaska and Canada, may be correct. He believes that the oceanic crust of the Canadian Basin must be early Palaeozoic or even Pre-Cambrian.

Seafloor marginal to Antarctica also seems at first to contain sectors of Palaeozoic crust for the following reasons. This continent is surrounded by a rift-megashear system (the pan- Antarctic rift) bounding the Antarctic crustal plate. No trenches are associated with this plate, into which ocean crust is being subducted. It is unique in this respect, for the other major crustal plates North American, South American, Eurasian, African, Indian, Australian, main Pacific and East Pacific plates include a subduction zone. Clearly the Antarc- tic crustal plate has evolved by the outward migration of the pan-Antarctic rift with time. Inside those sectors, where the rift did not initially block out Antarctica's continental slope, areas of old seafloor might be stranded and preserved. The broad sector of West Antarctica which faces the Pacific Ocean seems to offer such a possibility, for this is obviously not a rift margin. A Mesozoic foldbelt, however, a portion of the circum-Pacific orogenic girdle, makes up the periphery of West Antarctica, suggesting that seafloor was once subducted along this margin even if not now. Although volcanic zone extends along the Pacific margin of East Antarctica, the volcanoes are alkaline, not calc-alkaline, and provide no evid- ence for crustal subduction today. Future seismic profiling, however, will probably indicate the former presence of a trench zone there.

Pursuing the question of old crust, attention is drawn to the so-called subplates. The small ocean basins, such as the Sea of Japan, seem to be of prime interest, for they lie isolated and "protected" behind the subduction zones (trenches) where a descending lithospheric plate is being consumed. Geological and heat flow studies, however, suggest that the Japan Sea is also neo-oceanic13. There are Asiatic strata along the inner margin of the Honshu arc, suggesting that Japan was once attached to Asia, but that the Japanese arc subsequently moved outward. Apparently a mid-ocean rift is not a necessity for the emplacement of new oceanic crust, for there are no linear magnetic anomalies in the Japan Sea. The Fuji Basin, behind the Tonga-Kermadec trench, also has been inferred to have young crust14. It seems likely that the small ocean basins of the Pacific which form subplates are generally neo-oceanic.

The Caribbean is another type of isolated subplate which is protected by a subduction zone the east by the Antilles trench and the west by the Central American trench. The crust, however, is probably Mesozoic, not Palaeozoic. It was probably created with extension associated with the initial breakup of Pangaea into North America/Eurasia and South America/Africa in the mid-Triassic1. There is only a small chance that old Pacific floor is trapped within the Caribbean region.

The history of the Gulf of Mexico is an open question

310

NATURE VOL. 229 JANUARY 29 1971

Fig. 1 Reconstruction of the continents into Pangaea before 200 m.y. ago (adapted from Dietz and Holden1).

depending largely on whether it was an arm of the world ocean (Panthalassa), a sinus occidentalism or was created, like the Caribbean, with the initial breakup of Pangaea. Results from JOIDES leg 10 indicate that the central Gulf of Mexico was already deep water in the late Cretaceous (Santonian, 80 m.y.) and the south-east part since Cainomanian time ( 100 m.y.)15. If the Luann salt is a deep water salt laid down with the initial formation of the Gulf of Mexico, its age would be late Triassic or early Jurassic. It seems most likely that the Gulf of Mexico is neo-oceanic, forming in mid-Triassic with the clockwise rotation of the Honduras and Yucatan blocks which rotated outward to form Central America.

Generally regarded as a rift ocean like the Atlantic, the Indian Ocean would seem at first thought to offer little prospect of containing old ocean floor, but its history is much more

complex than the Atlantic. It differs markedly from the Atlantic Ocean in that there was an ancestral Indian Ocean namely, the eastern reaches of Tethys. As well as being a rift ocean, it is of the Pacific type, its northern boundary being margined by a subduction zone the Himalayan-Java trench system. We suggest that the eastern Indian Ocean floor, or the Wharton Basin in the broad sense (as defined by the Ninetyeast ridge, the Java trench, the western Australian margin, and the Diamantina fracture zone), is underlain by pre-Mesozoic crust, for the following reasons.

A generalized reconstruction of Pangaea, adapted from an earlier publication of ours (Fig. 1), shows that the Tethys Sea occupied the region of the Indian Ocean. The region between India and Australia is occupied by a bay of Tethys which we have termed Sinus Australis. A more detailed and precise reconstruction of the continents around Antarctica is shown in Fig. 2, which is quite similar to the assembly offered by Smith and Hallam16. We believe that this reconstruction in essentially correct and provides a basis on which the subses quent history of breakup and continental drift dispersion i- terms of plate tectonics can be reasonably determined and schematized (Fig. 3).

Fig. 3/1 (a Hammer transverse elliptical projection centred on 90 E longitude and 70° S latitude) shows the probable assembly of the continents around the Indian Ocean before continental drift breakup. Regions to the east of Australia and to the west of India are not considered. India and Aus- tralia are joined to Antarctica within the framework of the universal continent of Pangaea before the mid-Triassic, or

- 200 m.y. In Fig. 3/) Antarctica is fixed in position and the geographical coordinates are drawn relative to modern co- ordinates. This is not entirely gratuitous, for Antarctica probably has remained almost fixed with the other continents doing most of the drifting".

Fig. 3B shows the situation in the early Cainozoic or about

45 m.y., just before the detachment of Australia from

Fig. 2

Detailed depiction showing the reconstruction of continents around Antarctica before 200 m.y. ago. Zealand has been broken into two parts along the Alpine fault.

New

NATURE VOL. 229 JANUARY 29 1971

311

Fig. 3 Time sequence diagram showing the breakup and drift dispersion of India and Australia from Antarctica and consequent preservation of old crust in the Wharton Basin.

Antarctica. India had previously been detached from Antarc- tica, drifted far northward and almost reached the Tethyan subduction zone (Himalaya "trench"). The Indian plate was bounded on the west by the Chagos-Laccodive megashear and on the east by the Ninetyeast megashear (rift-trench strike-slip transform faults) and on the south by a rift. Old ocean floor was subducted into the Tethyan trench while new ocean crust was emplaced by seafloor spreading in the "wake" of India on both limbs of a northward migrating rift ("mid- ocean ridge"). Thus a broad swath of Tethys was "repaved". An undersea plateau (possibly a partially differentiated out- pouring of lava of semi-simatic composition) is shown as having come into existence the ancestral Kerguelen Plateau- Broken Ridge highground. It had been incipiently split into two parts by the penetration of the India rift.

Fig. 3C shows the position of the continents and the dis- position of the crustal plates today. According to the magnetic

reversal chronology impressed on the oceanic crust between Australia and Antarctica, these two continents were not detached until the early Cainozoic, for no anomalies older than anomaly 18 (Eocene, -45 m.y.) are present17. Consequently the old Tethyan seafloor, especially Sinus Australis, forming the western part of the Australian plate remains undisturbed. This plate later underwent subduction into the Java trench, but the Wharton Basin remains as unconsumed old crust while new ocean floor is being emplaced between Antarctica and Australia. Also, as we have depicted the drift dispersion of continents in this region, a small sector of old crust has been trapped along the margin of Antarctica near 90° E longitude. The reality of such details of this interpretation depends, of course, on the exact timing and geometry of the breakup.

This treatment considers that both Broken Ridge and the Kerguelen Plateau are of simatic composition. If either or both of these features should be identified as microcontinents

312

NATURE VOL.229 JANUARY 29 1971

there is some evidence that Broken Ridge may be so18 our proposed history would have to be modified. For example, if Kerguelen proves to be young sima while Broken Ridge is old sial, it would most likely have been detached from Antarctica by the rift shown in Fig. 3fl and little, if any, pre-Mesozoic crust would remain stranded adjacent to Antarctica.

We have not treated that portion of the Australian plate in the Pacific Ocean to the east of Australia. However, if the New Zealand subcontinent (a reasonable term as the area of the New Zealand platform is almost as large as India) was once attached to Australia, as seems probable, spreading has occurred between these two sialic platforms such that most of the ocean floor in between must be new.

(An alternative solution to closing the Indian Ocean by our continental drift reconstruction is to place India's east coast against Australia. Such a reconstruction leaves a large triangular mediterranean sea within Gondwana, margined by western India, Africa/Madagascar and Central East Antarctica. We suggest that this inland small ocean basin, if it existed (and we are inclined to doubt it) be termed Mare Gondwanis (Latin for sea of Gondwana). The breakup of this assembly would then involve the insertion of a spreading rift into the centre of this mediterranean and, in turn, would imply that old ocean .floor would now be stranded marginal to parts of India, Africa and Antarctica (from 40°-80° E longitude), the exact sectors involved depending on how the spreading rift was initially inserted. We believe, however, that such a breakup and dispersion history for the Indian Ocean continents is unlikely.)

There is some suggestive evidence that the Wharton Basin is at least of modest antiquity, and its unusual topography sup- ports this interpretation. There are numerous large ridges, marginal plateaus, and blocky highs quite unlike ocean floors elsewhere. This is strikingly revealed by the National Geo- graphic Society's 1967 map of the Indian Ocean floor based on the bathymetric studies of B. C. Heezen and M. Tharp. Sixty million year old basalt has been dredged from Ninety-

east ridge, so that this feature is not young19. Upper Cretace- ous (Turanian) ooze has been cored on the Naturaliste plateau20 and Cretaceous ooze has been recovered from the centre of this basin21. Our interpretation awaits testing by seismic reflexion profiling, dredging, coring and, we hope, drilling by the Deep Sea Sampling Project. If our view is correct, the Wharton Basin is the only broad expanse of pre-Mesozoic seafloor in the world.

Received October 20, 1970.

1 Dietz, R. S., and Holden, J. C, J. Geophys. Res., 75, 26, 4939

(1970).

2 Heirtzler, J., Dickson, G., Herron, E., Pitman, W., and Le Pichon,

X., /. Geophys. Res., 73, 6, 21 19 (1968).

3 Vine, F. J., J. Geol. Education, 18, 2 87 (1970). 1 Geotimes, 14, 8, 13 (1969).

5 Geotimes, 15, 7, 14(1970).

6 Heirtzler, J. R„ and Hayes, D. E., Science, 157, 185 (1967).

7 Emery, K. O., Uchupi, E., Phillips, J., Bowin, C, Bunce, E.,

and Knott, S., Amer. Assoc. Petrol. Geol. Bull., 54, 1, 44 (1970).

8 Vogt, P., Anderson, C, Bracey, D., and Schneider, E., J. Geo-

phys. Res. 75, 20, 3955 (1970).

9 Dietz, R. S., and Holden, J. C, Sci. Amer., 223, 4, 30 (1970).

10 Demenitskaya, R., and Karasik, A., Tectonophysics, 8, 345 (1969).

11 Ostenso, N. A., and Wold, K. I., Intern. Assoc. Geomag. Aeron.

Bull., 24, 67 (1967).

12 Churkin, H., Science, 165, 549 (1969).

13 Fujii, N., Intern. Symp. Mechanical Properties and Processes

in the Mantle, Flagstaff, abstract (1970).

14 Karig, D., J. Geophys. Res., 75, 2, 239 (1970).

15 Geotimes, 15, 6, 11 (1970).

16 Smith, A. C, and Hallam, A., Nature, 225, 139 (1970).

17 Le Pichon, X., and Heirtz, J. R., /. Geophys. Res., 72, 6,

2101 (1968).

18 Francis, T„ and Raitt, R., J. Geophys. Res., 72, 12, 3015 (1967).

19 Bezrukov, P., Krylov, A., and Cernishev, V., Oceanologia, 6,

261 (1966).

20 Burkle, L., Saito, T., and Ewing, M., Deep-Sea Res., 14, 4,

421 (1967).

21 Saito, T., Symp. Micropaleontology of Marine Bottom Sediments

(Special Committee on Oceanic Research, 19, 1967).

53

Reprinted from Geological Society of America Bulletin

82 , 811-814.

ROBERTS. DIETZ ) NO AA, Atlantic Oceanographic and Meteorological Laboratories, 901 South JOHN C. HOLDEN \ Miami Ave., Miami, Florida 33130 WALTER P. SPROLL

Geotectonic Evolution and Subsidence of Bahama Platform: Reply

The preceding discussion by Sheridan of our paper provides a welcome chance to clarify and amplify certain aspects of our views on the evolution of the Bahama plat- form (Dietz and others, 1970).

We agree with Sheridan that our crustal model for the Bahamas is a liberation from the standard concept that all continental regions (defined here as those at or near sea level) need not be necessarily underlain by "mountain roots" a sialic basement com- plex. In particular, we suppose that other marginal plateaus formed at former Y-junc- tions of crustal plates may be thick sedimen- tary accumulations emplaced directly on oceanic crust (such as Demerara marginal plateau) or volcanic accumulations (such as Afar triangle). We are inclined to doubt, however, Sheridan's speculation that the Jurassic Luann salt of the Gulf of Mexico is a shallow-water deposit. More likely it was deposited as a deep-water salt. The recent finding by oil companies that there is 3000 to 4000 m of Miocene salt beneath the Red Sea, without associated marginal facies char- acteristic of evaporites (gypsum and lime- stone), provides a strong case for deep-sea deposition of halite.

We agree that our presumed crustal section beneath the Bahama platform may be un- realistic in that the density chosen for the oceanic crust is too low. Sheridan's proposal for a more probable crustal section, in which he infers the existence of a thick intermediate layer between the normal oceanic crust and the Moho, is certainly an improvement. The problem to be faced, of course, is to some- how fill up with sediments a small ocean basin, or quasi-ocean basin, to sea level with- out grossly violating isostasy so that algal- coral carbonate deposition can gain a foot- hold. We are open to any suggestions for accomplishing this solution.

Sheridan (1969) believes that the deep Atlantic (Blake-Bahama basin) to the east of the Bahama platform was once much shal- lower than now. Results from JOIDES Leg 11 seem to support this point of view to some degree. For example, the Tithonian lime- stones penetrated in Hole 99 just east of San Salvador Island "probably indicate de- position in a relatively shallow pelagic en- vironment," and from Hole 100 nearby, "The nature of these sediments and character of the microfauna suggest a neritic-upper bathyal environment during their deposition" (Scientific staff, 1970). By the sea-floor- spreading concept, all of the floor in a rift ocean was originally generated at the rifted crest of a mid-ocean ridge. Subsequently, these mid-ocean ridges subside, and the original floor is further isostatically depressed by sedimentary loading. The subsidence of the basal sedimentary layers would be the expected history with depression of basal carbonate layers below the modern lysocline (carbonate compensation depth).

We regard as unlikely, however, Sheridan's supposition that the adjacent deep Atlantic has taken part in the full subsidence of the Bahama platform of about 5 km, which would mean that the Blake-Bahama basin was once almost at sea level. We know of no evidence that the Bahama carbonate section mono- clinally dips toward the shelf edge, as do those sections of the Atlantic continental shelf. This dip suggests a coupling between the craton and the ocean floor and suggests regional isostatic compensation. If the Bahama carbonates are really flat lying, the presence of a fault along the platform boun- dary remains probable. Because ocean-floor sedimentary layers are incompetent, we would not expect seismic profiler records to indicate any marked disturbance or drag effect such as would make the fault evident.

Geological Society of America Bulletin, v. 82, p. 811-814, 1 fig., March 1971

811

812 DIETZ AND OTHERS-GEOTECTONIC EVOLUTION, BAHAMA PLATFORM

We caution also that deep-ocean sediments do not recotd latge vertical displacement with clarity, and displaced shallow-water sediments create much confusion. Rather remarkably, with the new chtonology of magnetic reversal anomalies, we can for the first time identify large horizontal shifts of the ocean floor. This stands in sharp contrast to continental geology which is largely blind to horizontal shifts while clearly recording vertical shifts, especially those which penetrate the plane of sea level.

Although the Bahama platform is an aseismic region, this cannot be taken to prove that a normal fault does not exist along the platform margin. Faulting of this type may occur in small increments with little buildup of stress and, as such, would not produce measurable seisms. Also, most of the sub- sidence of the Bahamas occurred in the Mesozoic when the platform was young, with only a small amount of sinking subse- quent to the Eocene.

The dredging of a limestone block with slickensides parallel to bedding from Abaco Canyon by Sheridan, Elliott, and Oostdam (in press) and Sheridan, Berman, and Corman (1971) is most interesting and suggestive, but it does not really constitute a weighty argument favoring an important role for strike-slip tectonics in the Bahama region. The development of this carbonate platform is doubtless complex and defies any simple or single interpretation. Our thoughts on the environmental development of the curious indentations (such as Tongue of the Ocean) was incidental to the main theme. Neverthe- less, it seemed worthwhile to emphasize an aspect of carbonate bank evolution that pre- viously had been overlooked in favor of these re-entrants that were either tectonic or inherited features. We note that "textbook" atolls, whose perfect circularity reflects the circularity of subsided seamount tops, ate rare. Atolls become more irregular with in- creasing size and more and more reflect environmental factors. The Bahama platform is positioned in a strongly asymmetrical part of the Atlantic with respect to planetary currents and tradewinds. The Bahamian islands themselves have marked environ- mental disposition; nearly all are located on the windward side of deep-water passes. We suspect that environmental factors are im- portant and even may dominate in account-

A

a

LEGENO PflEJENT DAV LAND ^

/ Sum-ic rlAB&IN 1000^ . \ NORTH -/*«,«.Tiooofw ' AMERICA

'flj*' TriaaSk ro Rtcewr

/Hi

Figure 1. Formation of the Bahama plat- form following the mid-Triassic opening of the central North Atlantic. Events in the Gulf of Mexico and the Caribbean are left unspeci- fied. Most likely, the region was closed with cratonic blocks which later became Honduras, Yucatan, and the Antilles islands. A. Shortly after rifting, late Triassic. B. After further open- ing, as of mid-Jurassic.

ing for the irregularities of the Bahama platform.

We were aware of the view of Sheridan and othets (1969), that the "Guinea Nose" (a marginal plateau) is underlain by an exten- sion in basement sttuctural arch and, thus, is an integral part of the Aftican craton, but thete is conflicting evidence. On one hand, this intetpretation accords with that of Sougy (1962), who extrapolates his Paleozoic Mautitanides foldbelt across the Guinea Nose. On the other hand, from recent oil company surveys Templeton (in press) believes that this foldbelt bifurcates well inshore of the Guinea Nose and that a syncline lies athwart Sougy's trend and yet is inshore of the Guinea Nose. Templeton shows the pre-Mesozoic

REPLY

813

^winimnir .

surface to be 3000 to 5000 m deep over the Guinea Nose. From their magnetic survey, McMaster and others (1970, p. 161) also specifically question the existence of a west- southwest-trending "Guinea Arch" under- lying the Guinea Nose as proposed by Sheridan. It should be borne in mind, how- ever, that Sheridan, using the seismic refrac- tion method, may have measured Paleozoic structure in sedimentary strata, while McMaster and others measured Precambrian basement effects. We suppose that the pos- sibility remains that the Guinea marginal plateau is a postrift deposition excrescence to the African craton and so, in a small way, a mirror counterpart of the Bahama platform. We would like to offer a novel way in which

one might determine whether or not the Guinea Nose is old craton or postdrift ex- crescence ("new ground"). The ghost out- line of the African margin is rather faithfully reproduced in the mid-ocean rift. Probably the Guinea Nose is sufficiently large to be reflected thus, if it, in fact, was present at the time of breakup (;^ 200 m.y. ago). We have examined the shape of the rift zone where it is intersected by what appears to be the Guinea fracture zone. It appears to re- semble more closely the African margin with the Guinea Nose subtracted rather than added, which supports the idea that it is "new ground." However, detailed survey of the mid-ocean rift is necessary before much cre- dence can be placed in this evaluation.

814 DIETZ AND OTHERS-GEOTECTONIC EVOLUTION, BAHAMA PLATFORM

Some new evidence, that the Bahamas ate a postrift exctescence to North America, follows from the finding of Vogt (written commun., 1970). Magnetic reversal anom- alies created by sea-floor spreading should, and in fact do, generally parallel the margins of North America and Africa. However, the J-series anomalies identified by the Gofar Project of the Naval Oceanographic Office parallel the Atlantic coast, but strike abruptly into the north margin of the Bahama plat- form. Therefore, these spreading anomalies originally may have underrun the Bahama platform and subsequently have been covered by the growth of that platform.

It is also worth noting that the results of JOIDES Leg 11, which drilled in the deep Atlantic off the Bahamas, is consistent with our interpretation (Scientific staff, 1970). The oldest rocks yet found in the Atlantic were recovered just east of San Salvador Island and are estimated to be 160 m.y. old. This obser- vation supports our suggestion that the clastic sediments of the inferred Bahama crypto- basin, undetlying the carbonate cap, must be Late Triassic or Early Jurassic.

REFERENCES CITED

Dietz, R. S.; HoldenJ. C; and Sproll,W. P.

Geotectonic evolution and subsidence of Bahama platform: Geol. Soc. Amer., Bull., Vol. 81, p. 1915-1928, 1970.

McMaster, R. L.; De Boer, J.; and Ashraf,

A. Magnetic and seismic reflection studies on continental shelf off Portuguese Guinea, Guinea, and Sierra Leone, West Africa: Amer. Ass. Petrol. Geol., Bull., Vol. 54, No. 1, p. 158-167, 1970.

Scientific staff. Deep sea drilling project: Leg 11: Geotimes, Vol. 15, No. 7, p. 14-16, 1970.

Sheridan, R. E. Subsidence of continental margins: Tectonophys., Vol. 7, p. 219-229, 1969.

Sheridan, R. E.; Berman, R.; and Corman, D. Faulted limestone block dredged from Blake escarpment: Geol. Soc. Amer., Bull., Vol. 82, No. 1, p. 199-206, 1971.

Sheridan, R. E; Elliott, G. K.; and Oostdam,

B. L. Seismic-reflection profile across Blake escarpment near Great Abaco Canyon: Amer. Ass. Petrol. Geol., Bull., in press.

Sheridan, R. E.; Houtz, R. E.; Drake, C. L.; and Ewing, M. Structure ot continental margin off Sierra Leone, West Africa: ). Geophys. Res., Vol. 74, p. 2512-2530, 1969.

Sougy, J. West Africa fold belt: Geol. Soc. Amer., Bull., Vol. 73, p. 871-876, 1962.

Templeton, R. Geology of the continental margin between Dakar and Cape Palmas: SCOR symposium on Geology of the East Atlantic continental margin, Cambridge, England, March 1970, H.M.S. Stationery Office, London, in press.

Manuscript Received by The Society November 9, 1970

54

Reprinted from Deep Seas Research 18, 441-447

SHORTER CONTRIBUTION

Trou sans Fond submarine canyon: Ivory Coast, Africa

Robert S. Dietz* and Harley J. KNEBELf (Received 10 June 1970; /'/; revised form 16 November 1970; accepted 18 November 1970)

Abstract A bathymetric chart of the Trou sans Fond (Bottomless Hole) submarine canyon off the Ivory Coast, Africa, is presented, based upon a 1400-km survey in 1968 by the O.S.S. Discoverer. The canyon originates with a double head just off the beach and cuts a deep V-shaped furrow across the 30-km-wide shelf, attaining a maximum relief of 450 fm (823 m) near the shelf break. The canyon has a slightly sinuous and rugged relief down the continental slope, indicating an active erosional regime. At 1500 fm (2745 m) where the continental rise commences, the canyon is abruptly offset 20 km to the west, suggesting that the present outer fan valley is a newly developed channel. On the continental rise a depositional regime is indicated by well developed natural levees which have a cross- sectional area 60 times that of the Mississippi in the delta region. The Trou sans Fond appears to be the only canyon which taps the paralic zone between the Cayar Canyon to the north and the Congo Canyon to the south.

INTRODUCTION

In February 1968 the O.S.S. Discoverer, a research ship operated by the National Ocean Survey of the National Oceanic and Atmospheric Administration, surveyed the Trou sans Fond (Bottomless Hole) submarine canyon which lies off the Ivory Coast. Its existence has been known since at least 1846 when it first appeared on a chart published by the French engineer, Bellin. More recently the canyon head has been studied by French engineers for harbor entrance purposes, but its over-all bathymetry remained little known. No mention of it was made, for example, in the excellent mono- graph on the world's submarine canyons by Shepard and Dill (1964). This survey provides for the first time a detailed chart showing its bathymetry to 100 nautical miles offshore. Canyons such as the Trou sans Fond which tap the paralic zone are of unusual geologic interest, as they funnel neritic sediments to the deep ocean floor. By incising the continental shelf almost to the shore, they partially intercept the longshore ' river of sand ' and thus may be called ' sand-eating ' canyons.

The Trou sans Fond is of unusual economic significance in that it provides an access route for deep draft ships to nearshore. Taking advantage of the naturally deep water, the artificial Vridi ship channel was cut in 1952 through the longshore bar to an interior lagoon, making a major regional port and, in turn, creating the practically new city of Abidjan. Presumably owing to flushing of sand into the canyon head, silting-up of the canal entrance has not been a problem; on the contrary, a deepen- ing has occurred over the past 15 years. The canyon head was also the site of an abortive attempt by Georges Claude in the 1930's to create a novel type of power plant which would have utilized the thermal contrast between the cold, deep canyon head waters and the hot lagoonal waters to create a thermal engine. An excellent recent account of the general marine geology of the Ivory Coast continen- tal shelf and the inner portion of the Trou sans Fond was published by Martin (1969). Aspects of physical oceanography and shoreline dynamics have been treated by Varlet (1958).

♦National Oceanic and Atmospheric Administration, Atlantic Oceanographic and Meteorological Laboratories, 901 South Miami Ave., Miami, Florida 33130.

fNow at Department of Oceanography, University of Washington, Seattle, Wash.

441

442

Shorter Contribution

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Fig. 1. Regional geologic setting of the Trou sans Fond canyon. Adapted from Spengler and

Deteil (1966).

Shorter Contribution 443

REGIONAL SETTING

The regional setting of the Trou sans Fond is sketched in Fig. 1. The canyon is cut into a narrow continental shelf about 30-km-wide near the midpoint of a 600-km-wide shallow bight in the African margin extending from Cape Palmas in Liberia to Cape Three Points in Ghana. Although most of the Ivory Coast is a peneplained, early mid-Precambrian shield, a late Mesozoic-Cenozoic basin is present along the shoreline and on the central shelf of the Ivory Coast. Its inner margin is marked by large, down-to-the-basin normal faults. The filling is mostly Cretaceous sediments probably in excess of 5 km thick (Spengler and Deteil, 1966). The creation of this basin is probably related to the shearing and taphrogenisis associated with the continental drift rifting of South America from Africa probably near the end of the Jurassic (Dietz and Holden, 1970).

Some submarine canyons are found off large rivers, but this is not true for the Trou sans Fond, at least today. There are four rivers of moderate size along the Ivory Coast, but they enter estuaries or lagoons, as this is a ria coastline owing to the post-glacial sea level rise. None now reach the strand line, but apparently the Comoe River did so until recently (Martin, 1969). This river is the nearest one to the canyon head, lying 30 km east.

BATHYMETRIC SURVEY

Echograms from 760 nautical miles (1400 km) of trackline were obtained from aboard the O.S.S. Discoverer during February 1968. A Precision Depth Recorder coupled with an Edo transducer was used throughout the survey. This echo sounder is calibrated for an assumed velocity of 800 fm/sec (1463 m/sec), but the soundings were later corrected for velocity variations in the water column due to temperature and salinity. Navigation control was obtained nearshore by visual and radar bearings. Further offshore, positions were maintained by dead reckoning with respect to land ties and celestial fixes, and a constant drift set was assumed. The positional accuracy for the nearshore areas is probably within one nautical mile, while that offshore may be as much as two or three miles, because strong and confusing east-setting currents of the Guinea Current were encountered.

A bathymetric chart contoured at 100-fm intervals is presented as Fig. 2. The canyon commences at the shoreline in an amphitheater-shaped double head, but quickly assumes a deep V-shaped cross section as it incises the continental shelf. It cuts deeply into both the shelf and upper continental slope, attaining a maximum relief near the shelf break of 450 fm (823 m). The sidewall slopes in the steeper portions of the canyon generally average about 15°.

The canyon cuts through four physiographic provinces: the continental shelf, the steep upper continental slope to 1000 fm (1830 m), the more gentle lower continental slope to 1500 fm (2740 m), and the continental rise from 1500 fm to the limit of the survey at 2200 fm. The survey extended for 100 nautical miles offshore, but it is likely that the canyon extends for another 120 nautical miles until it reaches the Guinea abyssal plain at a depth of 2760 fm (5038 m). The long profile of the canyon is concave and is cut normal to the regional slope. At the canyon head, the thalweg declivity attains 1 2 % but quickly decreases to 3%. A steepening occurs near the shelf break to 8%, then decreases to 3-5% across the upper continental slope. The thalweg slope then slowly decreases seaward, being about 1 % in the lower reaches of the continental rise. This canyon has no well developed abyssal cone, but rather cuts across an abyssal fan which forms the upper continental rise. Although clearly erosional across the shelf and upper continental slope, the canyon appears to be dominantly depositional on the continental rise and has developed large natural levees.

Between 1500 and 1900 fm (2745-3477 m), the canyon axis is sharply offset 20 km to the west. This may represent a relatively new course selected by the canyon in seeking a steeper gradient. The former course of the canyon across the continental rise may be marked by a broad channel which lies more exactly along the extended strike of the upper portion of the Trou sans Fond Canyon. Its subdued outline may be due to blanketing pelagic sedimentation since it became inactive.

The stratigraphy of the canyon head probably can be inferred from a deep well drilled in 1959, on shore at Port Bouet but near the canyon, by the Societe Africaine des Petroles (Martin, 1969). This well revealed the following section: 0-71 m, Quaternary, coarse sand; 71-123 m, Miocene, fine sand; 123-706 m, marine Miocene, plastic clay; 706-757 m, Senonian, slightly sandy clay with shell debris; 757-1037 m, Turonian, calcareous sands with sand and clay; 1037-1408 m, Cenomanian, conglomerates, sandstones, calcareous sands, clays with gypsum; 1408-3938 m, Albo-Aptian, fossili- ferous clays, sandstones and gravels, also limestones and arkoses, some lignite. It appears likely that

444

Shorter Contribution

Fig. 2. Bathymetric chart of the Trou sans Fond submarine canyon, Ivory Coast, Africa. Based on 1968 survey by O.S.S. Discoverer, of the National Oceanic and Atmospheric

Administration.

Shorter Contribution 445

the upper portion of the Trou sans Fond Canyon is cut entirely in soft sedimentary rocks of Cretaceous and Cenozoic age.

Our attempt to sample the thalweg of the canyon failed, but suggested firm bottom presumably well swept by turbidity currents. A dredge haul up the west face of the canyon head produced only large blocks of slightly indurated, non-fossiliferous green clay which, from the above stratigraphy, was inferred to be marine Miocene. Martin (1969) also reports only soft sedimentary rocks comprising the canyon wall and an axis of hard sand and gravel. The continental shelf fringing the Trou sans Fond was found to be covered with green mud and silt rich in glauconitized ovoid coprolitic pellets. The shelf is generally smooth and featureless, but interrupted to the west by patches of irregular and hummocky bottom. The high acoustic reflectivity of these patches suggests they contain rocky reefs.

DISCUSSION

Inspection of existing bathymetric charts reveals that Trou sans Fond probably is the only canyon tapping the paralic zone between the Cayar Canyon north of Dakar in Senegal and the Congo Canyon off the Congo River in the Congo. For the sector between the Trou sans Fond and Dakar, this was further established by our own reconnaissance survey of that continental margin. This emphasizes the importance of this canyon as a conduit for funneling neritic sediments onto the abyssal floor. On the other hand, our survey identified numerous large canyons which were either entirely confined to the continental slope or incised the shelf break at the edge of the continental shelf for only a few miles.

A comparison of the Trou sans Fond with the Congo Canyon (Heezen et al., 1964) and the Cayar Canyon (Dietz et al., 1968) is interesting. Both of them are located at the classical positions for submarine canyons which tap the shoreline, the former off a river mouth and the latter upcurrent of a headland. The Congo Canyon enters the estuary of the Congo River, which is second in the world only to the Amazon River in terms of total water flow. A direct relationship between a river mouth and a submarine canyon is nowhere more evident. The principal role of the river presumably has been to supply sediments for turbidity currents rather than for cutting this canyon during lower sea level stands. The Cayar Canyon is positioned north of the prominent headland of Cap Verte, the western- most salient of Africa, toward which sand is transported by strong south-setting longshore currents. The ultimate source of much of this sediment is the Sahara Desert, from which sand has been blown onto the beaches of Mauritania and Senegal by the prevailing northeasterly winds.

We surmise that the Trou sans Fond canyon head has also been cut in response to an abundant supply of sand, although a strong case cannot be made. The Trou sans Fond is located near the center of a broad concavity in the continental margin of Africa, an indentation which pertains to the continental slope as well as the shoreline. It undergoes an abrupt 18° flexure at the canyon head. This shoreline is a region of large waves and plunging breakers creating a high energy regime. Sand transport is largely toward the east, owing to the prevailing swell direction and the east-setting Guinea Current, but this direction at times may reverse nearshore, especially in the subsurface. Under these conditions, sand may tend to accumulate in the center of the bight. The eastward offset of the canyon head from the exact center of this bight may represent a skewness impressed by the prevailing swell direction plus the usual set of the Guinea current (Fig. 1). One may suppose that, were it not for canyon head funneling sand into the deep ocean, the usual shoreline straightening processes would tend to fill in this bight or even create a cuspate foreland at the site of the canyon head. Possibly other factors have played a role as well in localizing the canyon head, such as an easily eroded fault zone, but any such fault remains to be identified.

The Trou sans Fond may be said, in a sense, to extend above sea level because the beach inside the canyon head has an abrupt foreshore, considerably steeper than is normal for the region. A narrow shallow bench, however, separates the brink of the canyon head proper from the beach. Presumably, this is a sand embankment formed in response to the vigorous surf regime.

In the early twentieth century two slumps which carried large volumes of sediment into the canyon head occurred along this shoreline. In 1905 a slump lasting 35 min slowly swallowed a wharf 70 m long upon which were a hundred barrels of cement and a warehouse. The shoreline receded 70 m and formed a small bight 280 m wide and an area formerly 5 m deep deepened to 25 m. Subsequently the strand line was rapidly reshaped by longshore processes. Sand budget surveys prior to modification of the beach environment by the Vridi Canal jetties showed 800,000 m3 of sand moving from the west

446 Shorter Contribution

into the canyon head region of the shoreline but only 400,000 m3 continuing on to the east, indicating a loss of 400,000 m3 of sand to the canyon head (Varlet, 1958).

There is another argument which favors active erosion within the Trou sans Fond canyon head. The abruptness of the shelf break around the world is now generally regarded as having been sharpened by erosional bevelling during the last glacial eustatic lowering of sea level to a depth of about 65 fm (120 m) (Dietz and Menard, 1951). Hence, if a canyon head has not experienced considerable side- wall erosion, a terrace should be etched into the canyon mouth at the shelf break depth, which lies at about 60 fm (110 m) for the Trou sans Fond. No such bench is now present, indicating that it must have been removed by erosion subsequent to the post-glacial rise of sea level.

Canyons which tap the paralic zone, as distinct from those incising the continental slope only, are distinguished by large natural levees on the continental rise. Upon approaching the survey region aboard the Discoverer while still in deep water, the Trou sans Fond was readily detected amongst a wealth of other bottom irregularities by its prominent levees. These levees and the underlying delta fans have a sedimentary volume clearly much larger than can be accounted for by the volume of material eroded from the upper erosional portion of the canyon. This emphasizes the important role of such canyons in conveying shelf and shoreline sediments to the deep ocean floor.

The large size of the undersea leveed fan valleys associated with the lower reaches of submarine canyons is not generally appreciated. For example, profile VII (Fig. 2) across the leveed outer channel of the Trou sans Fond shows a width of 6 km and a depth of 100 m, for a cross-sectional area of 600,000 m2. This is 60 times as large as the cross-sectional area of the Mississippi River below its natural levees in the delta region. Huge volumes of water are needed to overflow such giant channels and create the natural levee system. It would appear that such flows must only be triggered at in- frequent intervals. Perhaps low-volume, high-density turbidity currents are first generated in the can- yon heads and then through turbulent mixing are transformed into flows only slightly more dense than the ambient sea water, but of sufficient volume to overflow, and promote the growth of, the levees. The mode of triggering turbidity flows in a canyon head is largely unknown, but instrumented observations over several years by Inman (1970) in the Scripps submarine canyon off California indicate the existence of current sufficient to initiate strong sand transport.

Little can be said with assurance about the age of the Trou sans Fond Canyon. Its present head, however, must be younger than the Miocene marine claystone through which it is apparently cut and which is not of an open shelf facies. On the other hand, the great scale of the canyon indicates at least moderate geologic antiquity. Some students regard submarine canyon cutting as a Pleistocene process, but it seems more reasonable that ice age low stands of sea level only enhanced the vigor of turbidity currents. The basic processes involved in canyon cutting must have been active since the continental slope was created which, in this particular case, would have commenced with the breakup of the South America-Africa supercontinent in the mid-Mesozoic. Doubtless, the history of this can- yon is complex and involves the switching of channels, the filling of old canyon heads, and the cutting of new ones.

Acknowledgements We thank Captain Lorne Taylor, the officers and crew of the O.S.S. Discoverer for performing this survey. J. P. Pinot and J. R. Vanney of the Institut de Geographic University of Paris, assisted in preparing the bathymetric map of the canyon. Also contributing to the survey were geologists Philippe Bouysse, Carlos Urien, Don Hawkes and Lee Somers.

REFERENCES

Dietz R. and H Menard (1951) Origin of the abrupt change of slope at the continental shelf margin.

Bull. Am. Ass. Petrol. GeoL, 35, 1994-2016. Dietz R., H. Knebel and L. Somers (1968) Cayar submarine canyon. Geol. Soc. Am. Bull, 79,

1821-1828. Dietz R. and J. Holden (1970) Reconstruction of Pangaea: breakup and dispersion of continents,

Permian to Present. /. Geophys. Res., 75, (26) 4939^956. Heezen B., R. Menzies, E. Schneider, W. Ewtng and N. Granelli (1964) Congo submarine

canyon. Am. Ass. Petrol. Geol. Bull., 48, 1126-1149. Inman D. (1970) Strong currents in submarine canyons. Eos, 51 (4) 319 (abs).

Shorter Contribution 447

Martin L. (1969) Introduction a I'etude geologique du plateau continental ivoirien: premiers resultats.

Ivory Coast Center for Oceanographic Research (ORSTOM), No. 034, 163 pp. Shepard F. and R. Dill (1966) Submarine Canyons and other Sea Valleys. Rand McNally Co., 381 pp. Spengler A. and J. Deteil (1966) Le bassin secondaire-tertiare de Cote d'lvoire. In D. Reyre,

editor, Sedimentary basins of the African coasts. Ass. African Geol. Surv., Paris, 108-112. Varlet F. (1958) Le regime de V Atlantique pres Abijan. Inst. Francaise Afrique Noire, Etudes Ebur-

neennes, No. 7, 97-222.

Reprinted from Nature 232 , 20-23

55

Plate Tectonic Evolution of Caribbean-Gulf of Mexico Region

GEORGE L. FREELAND & ROBERT S. DIETZ

National Oceanic and Atmospheric Administration, Atlantic Oceanographic and Meteorological Laboratories, 901 South Miami Avenue, Miami, Florida 33130

A geotectonic history of the American Mediterranean is presented in terms of plate tectonics. The development of this region is presented as seven time sequence reconstructions from past Palaeozoic to present times.

Previous attempts to write a geotectonic history of the Ameri- can Mediterranean (Caribbean-Gulf of Mexico area) based on continental drift models' 3 or, more classically, the foundering of a Palaeozoic landmass4 need revision because of the success of plate tectonics. New data are available from recent land field work5-" and marine surveys12-21. Apparently, the evolution of this region is related to former plate junctions between North America, South America, and Africa and to strike-slip, exten- sional, and compressional motions as the new world drifted westward22. This is the theme of the synthesis presented in this article.

The geotectonic evolution of the American Mediterranean is presented as seven time sequence reconstructions which are azimuthal equidistant projections.

Reconstruction of Drift

Pre-dnft reconstruction: The closure of the Atlantic Ocean at the end of the Palaeozoic according to Bullard et al2i is modified by us (Fig. 1 ) to show the overlaps (in dashed lines) of the Bahama platform, southern Mexico, and Central America on to Africa and South America. In our reconstruction, we have eliminated the overlaps and the oceanic areas by rotations of these cratons (Fig. 2). Three of these, Yucatan24, Honduras- Nicaragua25, and Oaxaca (southern Mexico)9, are underlain by pre-Mesozoic basement. The isthmus of Panama and the Antilles are thought to be neo-cratons ("new ground"), created in Mesozoic-Caenozoic time, and are omitted.

The Bahama platform (more exactly, the Blake-Flonda- Bahama platform) is a crescent-shaped craton with a 3-5 km post-Triassic carbonate capping26. Although the nature of the basement remains unknown, we assume here that it is pre- Mesozoic, thus differing from the neo-cratonic origin of Dietz era/.27. We propose that the south-eastern Bahama spur moved eastward to its modern position along a shear now marked by

the Straits of Florida and the North-east Providence (Bahamas) Channel. This spur would then have originally filled the V-shaped gap between Africa and South America.

Our fit of the Oaxaca craton along western Mexico is speculative, but not unreasonable. In the Bullard tit, southern Mexico south of the Trans-Mexican Volcanic Belt (clearly "old ground")9 overlaps onto South America. The overlapped portion (mostly the Andean foldbelt of north-western Colum- bia) may be partly a marginal Meso/oic accretionary belt2", but the gap created would still be too small to accommodate the Oaxaca craton.

We identify the initial suture of the Gulf of Mexico hy the margin of the mid-Jurassic (Collovian-Oxfordian) basin. Starting from DeSoto submarine canyon, it trends north- westward through southern Alabama and central Mississippi, westward along the Arkansas-Louisiana state line, south- westward around the East Texas Basin, and southward into Mexico29 u. This model is supported by subsurface Tnassic redbeds, located by drilling, which lie just inland from the basin margin12. These presumably represent taphrogenic basins associated with detachment of the Yucatan-Nicaraguan craton.

Although Fig. 2 shows some gaps, the area probably was fully closed originally. Part of the central gap may be inter-

Fig. 1 The Bullard continental drift closure of the Atlantic- Ocean, modified by adding areas of craronic overlap shown in dashed lines. The fit is made at the 500-fm isobath

NATURE VOL 232 JULY 2 1971

21

Fit>. 2 Closure of the \tlantic Ocean and American Mediter- ranean in late Triassic (about 200 my. bp) according to this article. Microcontinents which are later translated are O, Oaxaca; Y, Yucatan: N, Nicaragua-Honduras: and B, south- eastern Bahama platform The northern Bahamas-Blake Plateau area is accommodated by subtracting the neo-cratonic, western Senegal Basin Continental margins are drawn to the 1.000-lm isobath, except where dashed.

Fig. 3 Initial rifting and breakup al the end of the Triable, I SO m.y. HP. Initial movement was rapid Arrows are vectors showing drill relative to Africa South America, which is arbitrarily held lived Hotted bands arc where new oceanic crusl is implaced. the dashed lines are transform laulis and or shear zones. Dotted lines on the continents outline Triassic taphrogeniL basins PR is the pole ol rotation for the North •\merican plate.

mediate crust which has been incorporated, after lectonization, into the nco-cratons of the Greater \nlilles, The western part was squeezed into the Guatemala foldbelt. \\ c would not expect a solution in the form of a simple jigsaw -lit due to the complexity of the problem

Initial breakup Fig, 3 shows the initial opening of the proto- North Atlantic Ocean and the pull-apart of North and South America. This is dated at or alter 2(K1 m.y HP I laic I riassic14) by basalts presumably associated with this rifling1'

The rotation pole of Dietz and Holderr* near south-eastern Spain for the opening of the North Atlantic is used with an

initial clockwise rotation of North America of 10°. South America and Africa remained joined. The split between North and South America was accomplished mostly by the opening of the Gulf of Mexico, with the Yucatan and Honduras- Nicaragua blocks rotating as a single unit about a point near the Isthmus of Tehuantepec. Sinistral shear occurred along northern South America (the El Pilar or South Caribbean shear zone). The Bahama block also started moving north- eastward.

Early Jurassic: Fig. 4 shows the plate positions at early Jurassic time (170 m.y. bp). Laurasia drifted south-westward, accommodated by sinistral shear along the Tethys seaway and the El Pilar fault zone of northern South America. Opening continued in the Gulf of Mexico. The Yucatan-Nicaraguan craton was split, creating the Gulf of Honduras sphenochasm. The Bahama craton lagged behind North America with respect to Africa and thus continued moving north-eastward. As the Gulf of Mexico, Caribbean Sea, and North Atlantic Ocean were small ocean basins at this time, lacking open circulation with the world ocean, deep-water evaporitcs such as the Louann were laid down.

Mid-Jurassic: Fig. 5 shows the plate positions at the end of mid-Jurassic (150 m.y. bp). As North America rotated north- westward, Newfoundland separated from Spain. Continued left-lateral shear occurred along the Tethys and El Pilar zones. The Gulf of Mexico, Caribbean, and North Atlantic remained as intracratonic ocean basins with continued salt deposition.

During the initial Atlantic opening the lack of reversals in the Earth's magnetic field is reflected in the magnetic quiet zone (MQZ). Starting at about 155 m.y. bp, however, reversals created the magnetic anomalies seen in the North Atlantic floor35 The absence of anomalies in the Gulf of Mexico is mostly due to opening during the magnetic quiet time. During the last stages of opening, rapid sedimentation into the rift zone probably prevented rapid chilling of the pillow lavas which record the polarity of the magnetic field.

As the Gulf of Honduras sphenochasm completed its opening, the Yucatan and Nicaraguan cratons assumed their modern positions relative to North America. West of the sphenochasm hinge, the east-west Guatemalan foldbelt was formed, accom- panied by the emplacement of serpentine bodies. Highlands produced by this orogenesis shed a thick sequence of continental and marine Jurassic sediments in Central America25. We propose that this deposition extended the eastern continental margin of the Nicaragua craton and filled the western end of the Gulf of Honduras. This sedimentary wedge would later form the nucleus of the Greater Antilles.

^..

Fip. 4 Blocking out of the American Mediterranean 30 m.y.

after commencement of drift X indicates salt deposits; other

symbols as in Fig. 3.

22

NATURE VOL 232 JULY 2 1971

The formation of the Gulf of Mexico was complete at this stage; the Nicaraguan block had rotated about 2,500 km over 50 m.y., an opening rate of 5.0 cm/yr.

Lower Cretaceous: Fig. 6 shows the plate positions at the end of the Lower Cretaceous (100 m.y. bp). South America separated from Africa at about 135 m.y. bp and became a new plate. Both the North and South American plates encountered subduction zones (trenches) along their western margins which probably had west-dipping Benioff zones. On impingement with the continents, the zones flipped to east-dipping. Marginal orogeny with attendant volcanism ensued.

Soon after South America separated from Africa, Nicaragua separated from South America as a result of the more northerly motion of the North American plate. An open connexion to the Pacific Ocean was established. The Caribbean Sea, thus created, opened wider than it is today. Towards the end of the Lower Cretaceous, the South American plate shifted to a more northerly motion. This resulted in cessation of strike-slip motion along the El Pilar zone and the initiation of subduction, compression, and orogeny along northern Venezuela36.

We propose that the Jurassic sedimentary accretionary wedge within the Gulf of Honduras (the proto-Cayman trench) and under the eastern edge of the Nicaraguan block split away from the Nicaraguan craton on both sides of the proto-Cayman trough to form the nucleus of proto-Cuba and proto-Hispaniola. As North America drifted westward, these blocks lagged behind, drifting north-eastward with respect to North America. Subduction zones formed along their northern margins causing orogeny, metamorphism of the Jurassic sediments, and volcan- ism. Rocks from the central gap in the original fit (Fig. 2) were also incorporated. Later, platform sediments were deposited along the northern edge of Cuba, completing the geosynclinal sequence there.

The Lesser Antilles arc was also initiated as a subduction zone, reflecting the faster rate of westward drift of the North American plate. We suggest that the Aves Ridge, located 250 km west of the modern Lesser Antilles, was the initial arc which was later abandoned by eastward migration of the Benioff zone. The plate boundary between the North and South American plates in the Atlantic Ocean is thought to be marked by several shear zones extending eastward from the Lesser Antilles1.

Mid-Eocene: The Caribbean region attained essentially its modern aspect by the end of the Middle Eocene (45 m.y. bp)

Fig. 6 Positions at the end of the Lower Cretaceous after 100 m.y. of drift. Hatched arrow on North American plate shows the relative motion between the North and South American plates; open arrows show motion relative to Africa as in previous diagrams. Heavy dashed lines are subduction (trench or compression) zones. The Jurassic sediment wedge from Fig. 5 has split off into two parts to form the nucleus of the Greater Antilles. The Lesser Antilles subduction zone is at the Aves Ridge. The Caribbean Sea is seen to be wider than it is today. Venezuelan orogenesis starts.

END OF MIDDLE EOCENE

Fig. 5 The Gulf of Mexico Caribbean near the end of the mid-Jurassic (150 m.y. bp). Note area of Jurassic sediments along the Nicaraguan craton. MQZ is the Magnetic Quiet Zone. Yucatan, Nicaragua, and the south-eastern Bahamas have reached their present position relative to North America Heavy dashed line west of South America is a trench zone

Fig. 7 The end of the mid-Eocene. The plates arc essentially

in their present position The Panama twist is formed due to

differential motion between the North and South American

plates.

(Fig. 7). Cuba and Mispaniola completed their north-eastward relative motion. Additional spreading centres south of the Cayman trough are postulated to have split proto-Hispaniola into further numerous sub-blocks that is, Jamaica, Hispaniola, Puerto Rico, the Virgin Islands and so on whose edges are reflected by intermediate depths. The Beata Ridge may also be one of these. Interaction along the leading plate boundaries and within the Caribbean blocks continued orogeny throughout the Tertiary"117 19. Active subduction beneath the Lesser Antilles arc moved eastward to its modern position during the lioccne. As North America drifted faster than South America, the Caribbean region closed slightly. Continued compression along northern Venezuela and distortion of the Panamanian reuion resulted Vulcanism slowly closed the Isthmus land gap.

NATURE VOL. 232 JULY 2 1971

23

Fig. 8 Present situation. Continued motion between the North and South American plates is accommodated mainly by the Cayman-Puerto Rico shear zones, the Lesser Antilles subduction zone (which has migrated eastward), and a poorly defined shear zone extending eastward from the Lesser Antilles.

Orogeny also continued along the Pacific plate margins, responding to this subduction zone which was pushed westward along the leading continental edge.

Present: Throughout the remainder of the Caenozoic to the Present there was and is continued differential motion, interaction and closure between the two American plates (Fig. 8). We regard these two plates as distinct entities separated mainly by the Cayman-Puerto Rico megashear. Thus, the east-west plate boundary has shifted from the northern margin of South America to the Cayman-Puerto Rican shear zone. The Gulf of Mexico is part of the North American plate, while the Caribbean region is part of the South American plate. The El Pilar zone is mostly inactive today40.

In the Neogene interaction of the North American plate with part of the East Pacific Rise caused separation and northward slippage of Baja California. The Galapagos-Panama ridge- fracture system was created within the East Pacific plate during the last 10 m.y.41.

Consequences of the Model

The foregoing is an attempt to formulate a reasonable plate tectonic history of the Gulf of Mexico/Caribbean region within the context of known geology. Some consequences of our model are as follows.

(1) The age of the sea floor crust of the region would be largely early drift that is, early Jurassic for the Gulf of Mexico and mostly Lower Cretaceous for the Caribbean. There was a large amount of early extension and emplacement of new crust, followed by slight closure during the Tertiary. No Palaeozoic oceanic crust would be present.

(2) The Yucatan and Nicaraguan blocks are clearly old cratons which, by their movement, formed the Gulf of Mexico before the mid-Jurassic period. Movement of these blocks was completed before South America separated from Africa at about 135 m.y. bp. The Caribbean Sea attained a modern aspect by Upper Cretaceous time at 100 m.y. bp.

(3) Both the Greater and Lesser Antilles are regarded as primarily neocratonic (that is, post-breakup in origin). Meta- morphism has obscured the central pre-drift "gap" mateiial which, if present, was incorporated into the eugeosynclinal belts of the Greater Antilles.

(4) The Caribbean area is a subplate presently attached to the South American plate, with little or no movement between them at this time. It is protected from destruction by inward- dipping subduction zones on both cast and west. The Gulf of

Mexico, Yucatan, Cuba, and Bahama areas are parts of the North American plate.

(5) The early differential motion between the North and South American plates was accommodated by a shear zone along the northern margin of South America. The present differential motion is accommodated by shear along the northern Caribbean margin (the Cayman-Puerto Rico trench system), and is much less than during the initial stages of movement.

(6) Unlike the solution from Bullard's fit, the region was fully closed before 200 m.y. bp so that there was no "Mare Occidentalis" western bay indenting Pangaea.

Received March 23 ; revised May 24, 1971.

1 Ball, M. M., and Harrison, C. G. A., Trans. Gulf Coast Assoc.

Geol. Soc, 287 (1969).

2 Carey, S. W., in A Symposium on Continental Drift, 177 (Univ.

Tasmania, Hobart, 1958).

3 MacGillavry, H. J., Proc. Kon. Neder. Akad. van Weten., B, 73,

64(1970).

4 Meyerhoff, A. A., Trans. Gulf Coast Assoc. Geol. Soc, 217 (1967).

5 Almy, jun., C. C, Trans. Gulf Coast Assoc. Geol. Soc, 269 (1969).

6 Bass, M. N., in Tectonic Relations of North Central America and

the Western Caribbean, 283 (AAPG Mem. 11, 1969).

7 Dengo, G., and Bohnenberger, O., in Backbone of the Americas,

203 (AAPG Mem. 11, 1969).

8 Hess, H. H., in Caribbean Geological Investigations, 1 (Geol. Soc.

Amer. Mem. 98, 1966).

9 Kesler. S. E., and Heath, S. A., Bull. Geol. Soc. Amer., 81, 2471

(1970). 10 Khudoley, K. M., Amer. Assoc. Petrol. Geol. Bull., 51, 668 (1967). ' ' McBirney, A. R., and Bass, M. N., in Tectonic Relations of North

Central America and the Western Caribbean, 203 and 269

(AAPG Mem. II, 1969).

12 Bowin, C. O.J. Geophvs. Res., 73, 5159(1968).

13 Bracey, D. R., Geophysics, 33, 950 (1968).

14 Bush, S. A., and Bush, P., Trans. Gulf Coast Assoc Geol. Soc,

281(1969).

5 Chase, R. L , and Bunce, E. T.,J. Geophvs. Res., 74, 1413 (1969).

6 Malloy, R. J., and Hurley, R. J., Geol. Soc Amer. Bull., 81,

1947(1970).

7 Molnar, P., and Sykes, L. R., Geol. Soc. Amer. Bull., 80, 1639

(1969).

8 Rona, P. A., Nature, 224, 141 (1969).

9 Uchupi, E., and Emery, K. O., Amer. Assoc. Petrol. Geol. Bull.,

51,223(1967). 0 Uchupi, E., and Emery, K. O., Amer. Assoc Petrol. Geol. Bull.,

52, 1162(1968). ' Uchupi, E., and Emery, K. O., Woods Hole Oceanog. Inst.

Contrib., 2525 (1970).

2 Dietz, R. S., and Holden, J. C, J. Geophys. Res., 75, 4939 (1970).

3 Bullard, E., Everett, J. E., and Smith, G. E., in A Symposium on

Continental Drift, 41 (Royal Soc, London, Philos. Trans., 1965).

4 Dengo, G., Trans. Gulf Coast Assoc. Geol. Soc, 311 (1969).

5 Mills, R. A., Hugh, K. E., Feray, D. E., and Swolfs, H. C, Amer.

Assoc. Petrol. Geol. Bull., 51, 171 1 (1967).

6 Sheridan, R. E., Draie, C. L., Nafe, J. E., and Hennion, J.,

Amer. Assoc. Petrol. Geol. Bull., 50. 1972 (1966).

7 Dietz, R. S., Holden, J. C, and Sproll, W. P., Geol. Soc. Amer.

Bull., 81, 1915(1970).

8 Jacobs, C, Burgl, H., and Daniel, L. C, in Backbone of the

Americas, 62 (AAPG Mem. 2, 1963).

9 Bayley, R. W.and Muehlberger, W. R., Basement Map of the US

(US Geol. Surv., 1968). 0 deCserna, Z., Bol. Soc. Geol. Mexico, 30, 159 (1969). ' Flawn, P., The Ouachita System (Univ. Texas Pub. 6120, 1961).

2 Scott, K. R . Hayes, W. E., and Fietz, R. P., Trans. Gulf Coast

Assoc. Geol. Soc, 11, 1 (1961).

3 deBoer. J.. Geol. Soc. Amer. Bull., 79, 609 (1968).

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1 20S, 260(1964).

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Geophvs. Res., 76,473(1971).

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J. M., and Robic. R. H., Amer. Assoc. Petrol. Geol. Bull., 37, 690(1953).

7 Bowin. C. O, in Caribbean Geological Investigations, II (Geol.

Soc. Amer. Mem. 9X, 1966).

8 Mattson, P. H.. in Continental Margins and Island Arcs (edit, by

Poole. W. H), 124 (Geol. Surv Canada, 1966). " Whctten, J. T., in Caribbean Geological Investigations, 177 (Geol.

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Reprinted from Interocean '70 2, 65-71

56

Engineering Properties of North Atlantic Deep-Sea Sediments

George H. Keller, National Oceanic and Atmospheric Administration, Atlantic Oceanographic and Meteorological Laboratories, Miami, Florida, USA

Abstract

The engineering characteristics of river, harbor and certain coastal sediments have been investigated since man found it necessary to construct structures such as wharves, jetties and various pile supported platforms. Only during the past decade has some atten- tion been devoted to the engineering properties of deeper coastal water deposits and even more recently to the similar aspects of deep-sea sediments. Initial studies of North Atlantic deposits (upper 10 to 20 m [33 to 66 ft.]) for such properties as shear strength, unit weight, water content, and porosity reveal consider- able variation, yet in some areas there exists a definite correlation between these properties and sediment type, current flow and sea floor topography. With the advent of the U. S. Deep Sea Drilling Project, our knowledge of the sediment blanket covering the ocean basins has been advanced appreciably. Among the many analyses made on the Deep Sea Drilling Project cores are those for water content, unit weight (bulk density) and porosity to depths of 1070 m (3 5 10 ft.) below the sea floor. This program has provided a significant insight into range and variation of these properties to depths greater than has been possible to reach by conventional deep-sea coring techniques. Although some general- izations can be made about the area! distribution and range of certain engineering properties within the surface layers of deep- sea deposits, local lateral variation may be considerable, in some cases exhibiting coefficients of variation as high as 147 percent and more frequently on the order of 30 to 50 percent. To date, we have but little insight into the engineering properties of deep- sea sediments. Before significant data is available to deal with the stability of sea floor deposits both in regard to their foundation characteristics as well as their mass movement, much more regional and detailed sampling is required.

Introduction

Relatively little is known about the engineering properties of deep-sea sediments and as yet only broad generalizations can be made concerning these properties within the upper few meters of the sea floor. An untold number of engineering investigations have been made in river and coastal waters for various projects such as the construction of wharves and jetties or the installation of sub- marine pipelines. Since about 1950 an increasing number of foundation studies have been carried out on the continental shelves in conjunction with the erection of offshore drilling plat- forms. To date, the majority of the engineering studies conducted on deep-sea deposits have been made by marine geologists investi- gating different aspects of the deep ocean environment (Richards, 1961, 1962). A number of these studies have dealt with specific relationships such as sound velocity and mass properties (Hamilton, 1956; Buchan et al., 1967), density variation with depth (Igelman and Hamilton, 1963), consolidation charac- teristics and depositional history (Bryant et al., 1967; Richards and Hamilton, 1967) or have discussed the engineering properties of a local area (Moore and Shumway, 1959; Harrison et al., 1964). Utilizing data from approximately 500 sediment cores (Atlantik - 300, Pacific - 200), Keller (1968) provided the first

regional generalization of the distribution of selected engineering properties in the North Atlantic and North Pacific basins.

Commencing with the U. S. Deep Sea Drilling Project in 1968 an entirely new aspect of these studies has been made possible. This program has provided deep-sea cores from depths as great as 1070 m (3 510 ft.) below the sea floor on which engineering tests have been made for unit weight (bulk density), water content, porosity and relative strength. A discussion of some of these data follow in a later section.

This paper is a discussion of the available engineering properties data for the North Atlantic basin deposits. In addition to presenting the areal distribution of selected properties, it also includes a sec- tion dealing with ultimate bearing capacity of surface materials and the consolidation characteristics of deep-sea sediments. Local variation of engineering properties both laterally and vertically proves to be significant in contrast to some early speculations that deep-sea deposits are homogeneous. These findings, in conjunction with presentation of data from one of the deepest holes yet drilled in the North Atlantic are discussed herein.

Areal Distribution of Engineering Properties Sediment Types

To set the stage for later discussions it is important to visualize the overall types of sediment that occur in the North Atlantic basin. The distribution pattern of bottom sediments as it is known today has been presented in various publications (U. S. Naval Oceanographic Office, 1965; Keller and Bennett, 1968; and Inter- departmental Geophysical Committee of the Academy of Sciences, USSR, 1969). Using the classification of Keller and Bennett (1968) it is seen that much of the North Atlantic is blanketed by calcareous ooze, Fig. 1, which, as used here, is a sediment con- sisting of at least 30 percent calcium carbonate in the form of skeletal material from various planktonic animals and plants. Deposits of terrestrial origin, later reworked by the sea, consti- tute the major sediment type (fluvial marine) along the margin of the basin.These deposits are relatively widespread and extend considerable distances into the basin revealing the strong influence terrestrial drainage has on the sediments of the North Atlantic. Unlike the Pacific basin, the occurrence of "red clay" is not very extensive. Unique deposits of calcareous sand and silt (commonly shell fragments and coralline debris) occur in the area of the Bahama Islands and the Straits of Florida. Although the distribu- tion pattern shown in Fig. 1 is relatively simple, it is highly prob- able that it will increase in complexity as more samples become available. The reader is referred to the study by Keller and Bennett (1968) for a more detailed discussion of the classification used here.

Shear Strength

Shear strength measurements were made on samples consisting primarily of fine grained cohesive material (silty clay and clayey silt) with an occasional stringer of fine sand occurring in some of the cores. Shear strength of this sediment type is a function ot

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cohesion, the angle of internal friction of the material und the effective stress normal to the shear plane, commonly expressed as:

Z{ = c + a tan </>

where c is cohesion, a the effective stress and <p the angle of internal friction. Cohesive, saturated sediments stressed without loss of pore water behave with respect to the applied load as if they were materials without any angle of internal friction (0=0). In which case, shear strength is equal to the cohesion (Tf = c). A more detailed discussion of shear strength can be found in soil mechanics texts such as Taylor (1948) and Scott (1963).

Shear strength measurements were made by either of two methods: unconfined compression test or laboratory vane shear. Testing procedures used to accommodate the relatively weak sub- marine sediments have been discussed by Richards (1961). In the case of the unconfined test, the sediments were considered to be clays or materials behaving like clays and the shear strength was taken as one-half the unconfined compressive strength.

along the Mid-Atlantic Ridge. Available data indicates that a band of low shear strength material may extend in an east-west direc- tion across the Atlantic at approximately 15CN. A definite ex- planation for this occurrence is not readily available without additional data. However, the westward flow of the Equatorial Currents across this portion of the basin may in some way account for the distribution of these relatively low strength sediments. Sediments along this band tend also to possess low unit weights and high water contents.

Sediments east of Greenland display unique properties relative to most of the North Atlantic deposits. Here, shear strengths are some of the lowest yet reported for the North Atlantic and pos- sibly may be attributed to the influx of sediment from Greenland and the Arctic as well as reflecting the general current circulation pattern for this area (Keller and Bennett, 1968). The highest average shear strengths ( 1 ,5 to 2,0 psi [105 to 141 g/cm2]) yet found in the Atlantic are those associated with the calcareous

Figure 1. Sediment distribution in the North Atlantic

Figure 2. Distribution of average shear strength in the North Atlantic

Sediment cores used in this study vary from 30 cm (12 in.) to approximately 7 m (23 ft.) in length. Values of shear strength and water content shown in Fig. 2 and 3 respectively, represent averages of the measured parameter over the entire length of each core. As a rule of thumb, these data can be considered als repre- senting average values for the upper 2,5 m (8 ft.) of the sea floor.

Shear strengths in the upper few meters of the sea floor are found to vary from 0,5 to 2,0 psi (35 to 141 g/cm2). As shown in Fig. 2, much of the basin consists of deposits possessing average shear strengths of 0,5 to 1 ,0 psi (35 to 70 g/cm2). Strengths of less than 0,5 psi (35 g/cm2) are often observed in coastal areas where local drainage or current conditions result in the deposition of relatively weak deposits. Other areas of low shear strength are found associated with the "red clay" deposits and in isolated patches

deposits surrounding the Bahama Islands and on the Blake Plateau off the southeast coast of the United States.

Water Content

Water content is expressed as a percent of the ratio: weight of water to the weight of oven dried solids in a given sediment mass. Laboratory techniques for this determination can be found in most texts dealing with soil mechanics and are not discussed here.

Average sediment water contents for the North Atlantic range from 30 to 175 percent, but more commonly are between 50 and 1 00 percent (Keller and Bennett, 1 968) (Fig. 3). Higher water contents are found in areas influenced by major drainage systems such as off the Mississippi and St. Lawrence rivers. A sizable area of relatively high water content extends from Africa westward to

the Caribbean and may, as noted earlier, possibly be attributed to the general current pattern in this part of the basin. The isolated patches of high and low water content sediments found in the basin may be related to topographic irregularities, which by influencing current conditions have altered the depositional environment on a local basis (Keller and Bennett, 1968). As ob- served in the case of shear strength, the sediments east of Green- land display anomalous water contents relative to those of other portions of the basin. Water contents of less than 50 percent predominate throughout much of the Greenland Sea area.

Unit Weight and Porosity

The distribution of average sediment unit weight (bulk density) and porosity for the North Atlantic has been discussed by Keller and Bennett ( 1968) and will only be summarized here. Unit weights range from 80 to 125 pcf (1,3 to 2,0 g/cc), with the majority of the basin deposits exhibiting values between 95 and

n u

30- 0-

Figure 3. Distribution of average water content in North Atlantic sediments

110 pcf (1,5 to 1,8 g/cc)-. Offshore from large drainage systems (Mississippi and St. Lawrence rivers) densities are commonly below 95 pcf (1,5 g/cc). A prominent feature in the regional distribution of bulk density is a band of relatively low density (78 to 94 pcf [1,2 to 1,5 g/cc]) material characterizing a 350 mile (563 km) wide portion of the sea floor between Africa and the Caribbean in the vicinity of latitude 1 5°N.

Average sediment porosities for most of the North Atlantic seldom exceed 70 percent and more commonly range between 60 and 65 percent. Only in small isolated portions of the basin and in the area influenced by the St. Lawrence River are porosities greater than 80 percent found (Keller and Bennett. 1968). Average porosities of less than 50 percent are relatively rare in the Noth Atlantic.

Ultimate Bearing Capacity

For the engineer concerned with the placement of an installation on the sea floor, the bearing capacity and consolidation charac- teristics of the foundation material must be ascertained. If the load is relatively small, it may only be necessary to determine the bearing capacity in order to know the depth to which a structure or piece of hardware will penetrate the sea floor during the initial installation.

Ultimate bearing capacity is the average load per unit area required to provide failure by rupture of a supporting sediment mass. It is a function of the product of the shear strength and one or more factors, which are dependent on the size and shape of the load as well as the depth of loading. For the purpose of this discussion, a formula for the ultimate bearing capacity of sediment under a strip load (load infinitely long relative to width) at the surface is used for the determination of the values shown in Fig. 4. The general bearing capacity formula for a shallow strip foundation developed by Prandtl (1920) and later modified by Terzaghi (1943) is:

Qc

cNc + 7DNq +

7BN7

(1)

when Qc is the ultimate bearing capacity, 7 the sediment unit weight, B the width of the load, D the depth of the load below the surface, and Nc, N , and N7 are dimensionless factors depend- ent on the angle of internal friction, depth and shape of the foundation and roughness of the base. For the case of a surface load and zero angle of internal friction, the factors N and N7 are equal to unity and zero respectively and equation ( 1 ) is simplified to:

Qc = cNc

90°

(2)

60°

45

5- 15'

ULTIMATE BEARING CAPACITY

Jgf- .3 3 •!' »6 9

^ I 3 .0 I .25

Figure 4. Ultimate bearing capacity values at the sea-floor surface for a strip load

where Nc equals 5,14 according to Prandtl. Other values for Nc are found to be in use by various investigators. Using equation (2) and a selected number of essentially surface (0-5 cm [0-2 in.]) shear strength values, ultimate bearing capacities have been deter- mined for portions of the North Atlantic (Fig. 4).

An example comparing values shown in Fig. 4 with a calculated load will serve to illustrate the significance of these bearing capy- city values. If a strip load whose buoyed weight is 1 ,000 pounds (454 kg) and has a surface area of 400 in2 (2 581 cm2), is placed on the sea floor without impact, the resulting stress on the sedi- ment will be 2,5 psi (176 g/cm2). An ultimate bearing capacity of at least this amount is necessary to prevent a shear failure. As can be seen from Fig. 4, such a load would not cause a shear failure at most of the core sites. This assumes no safety factor is used, which

generally is never the case in actual practice. Depending on the safety factor used, much of the North Atlantic deposits would not be considered capable of supporting the strip load used in this example.

Consolidation Characteristics

Consolidation in the engineering sense refers to the gradual de- crease in volume of a sediment under an imposed load. Consolida- tion characteristics are rather important since they indicate the depth to which a structure or some load will settle into a sedi- ment, and, in conjunction with studies of overburden pressures, they may result in geological conclusions as to the volume of original sediment and the vertical variations of density and poros- ity in the sedimentary deposit. Based on the consolidation test, sediments are usually classified as normally consolidated, under- consolidated or overconsolidated. They are classed as normally consolidated if the present effective overburden pressure is the greatest yet imposed on the deposit; they are said to be over- consolidated if the test indicates that the deposit has been sub- jected to pressures greater than those presently effective. If a deposit has not yet been consolidated under the present pressure, it is considered to be underconsolidated.

A majority of the deep-sea sediments that have been tested for their consolidation characteristics reveal they are slightly over- consolidated (Hamilton, 1964; Bryant et al., 1967; and R ichards and Hamilton, 1967). Although there is little doubt about the validity of the consolidation tests, it is obvious that the deposits have not been subjected to loads greater than their present over- burden pressure nor have they been dessicated. Factual data are not yet available, but a number of investigators have proposed that this unique overconsolidation condition may result from very slow rates of deposition, and "chemical cementation" by inter- particle or ionic bonding {Rittenberg et al., 1963; Hamilton, 1964). This unique property of deep-sea sediments would indicate that they can support greater loads than might have been anti- cipated.

Lateral Variations of Engineering Properties

The earlier figures displaying regional distribution of shear strength and water content may be deceiving in that they suggest that sediments possessing relatively uniform properties extend over large areas of the North Atlantic. In reviewing the available engineering data for deep-sea sediments within the upper 7 m (23 ft.) of the sea floor, Keller and Bennett (1970) reported on the variations of selected properties both for the North Atlantic as a whole as well as for specific sediment types found in the basin, Table 1. These data clearly point out some of the large variations that can be anticipated in this environment.

Variation of engineering properties within a local area have re- cently been examined by Bennett etal. ( 1970). Their study con- sisted of determining certain engineering properties in three sedi- ment cores collected from an area of 400 cm2 (6,2 in.2) in a basin % approximately 2000 m (6560 ft.) deep off the island of Puerto z Rico. Tests were carried out on three corresponding horizons in i each core and a comparison made of the variation among the 2j

measured parameters in these horizons using the statistical ex- pression, "coefficient of variation". As shown in Table 2, a con- siderable degree of variation exists in even such a small area. The greatest variations occurred among such properties as sensitivity (ratio of natural to remolded strength), shear strength and texture, whereas unit weight and grain specific gravity displayed relatively little change. This same discussion included a comparison of data taken from a study by Richards (1964) on four cores collected from an area approximately 0,2 km2 (0,08 mile2) in the northwest

Table 1 . Variation of Engineering Properties for the North Atlantic as a whole (modified from Keller and Bennett, 1970)

y

w

T)

h

St

G

WL

wp

(pcf)

(%)

(%)

(psi)

Max. Min. Ave.

165 78 95

207 15

86

85 32 66

12.9 .01

0.7

88 1

4

2.86 2.45

2.73

109 47

65

38 20

27

Variation of Engineering Properties for Selected Sediment Types in North Atlantic Basin

the

Carbonates

y

w

1

h

St

G

WL

Wp

(pcf)

(%)

(%)

(psi)

Max. Min.

Ave.

114 84 94

132 15 96

78 45

72

Fluv

12.9 0.1

1.1

al Marine

88

1

10

2.86 2.63 2.71

109

77

101

30 26

29

Max. Min. Ave.

165 80 91

188

28

112

80 44 73

10.1 .01

0.9

57

1 4

2.81 2.45 2.67

101 47 85

38 20 29

"Red Clay"

Max. Min. Ave.

127 78 90

207 23

159

85 32 74

3.3 .01 0.6

25 1

9

2.84 2.46 2.54

107 102 105

-

> w

'J

s

unit weight of soil

water content (% dry wt.)

porosity

shear strength

St G WL

Wp

sensitivity

grain specific gravity liquid limit plastic limit

Atlantic. Although covering a much larger area and a different sediment type than that represented by the three cores, the rela- tive degrees of variation were much the same among all seven cores.

Vertical Variation of Engineering Properties

Until recently, sediment cores collected from the deep-sea floor seldom reached lengths greater than 20 m (66 ft.). As a result, very Little is yet known about the variation of engineering properties to any great depth below the sea floor. Certain changes with depth such as increasing shear strength and unit weight and decreasing water content might be anticipated, based on terrestrial studies. Care must be used, however, in applying such generalizations to deep-sea deposits. Detailed studies on the upper few meters of

Figure 5. Variation of selected mass properties with depth in two turbidite sequences

Table 2. Mass Physical Properties and Coefficients of Variation (V*) of three Whiting Basin Cores (modified from Bennet, Keller and Busby, 1970)

Horizon Sampling Interval Water Content (cm) (% dry weight)

Unit Weight (pcO

Core 1 Core 2 Core 3 12 3V 1

2 3V

A 0-8 0-7 0-9 75 66 78 17 97.3 B 8-15 10-17 10-17 67 60 65 11 100.5 C 17-25 17-25 17-26 59 57 63 10 103.0

98.0 96.7 1.3 102.3 101.1 1.8 104.2 101.1 3.0

Grain Specific Gravity Shear Strength Sensitivity (psi)

Liquid Limit (%)

123V 123V 123V

12 3V

2.78 2.77 2.78 0.4 0.3 0.3 0.2 37 3.2 2.7 2.5 25

2.79 2.78 2.78 0.4 0.7 0.6 0.5 33 3.3 5.4 2.8 63 2.78 2.80 2.79 0.7 1.1 2.1 0.8 100 6.2 40.7 7.4 147

34 35 35 3 41 39 37 10

35 34 38 11

Plastic Limit Porosity Sand Silt (%) (%) (%) (%)

Clay

(%)

123V 1 2 3V123V 123

V

12 3V

29 29 28 3 67.8 65.9 68.6 4 42 36 41 15 35 40 37 29 31 31 7 65.6 63.1 64.7 5 29 22 36 48 42 46 40 28 25 31 21 62.6 62.1 64.4 3 29 40 25 46 43 39 45

13 14 14

23 24 22 9 29 32 24 29 28 21 30 35

100 -

o

O

UJ

> I- 400

2s

UJ -—

to I 2; 500

600

UNIT WEIGHT 80 100 120 (pcf)

BREAKS IN CORED INTERVAL

*) coefficient of variation represents a measure of the range of values expressed as ; percent of the median value (Balsley, 1964)

the sea floor indicated that some portions of the ocean basins contain sediments exhibiting considerable degrees of variation with depth (Richards, 1961 ).

Turbidite sequences (layers of relatively coarse material interlaid with fine sediments) are common to many portions of the deep- sea and possess extreme variations among their mass properties within relatively short intervals. Analyses of cored samples from two such deposits clearly attest to this distinctive characteristic. Fig. 5. Richards and Keller (1962) found in their detailed study of a sediment core from off Nova Scotia, that within the uppei 180 cm (71 in.) of the sea floor, water contents varied from 27 to 100 percent.

It was not until 1961, during the United States MOHOLE project, that sediment cores longer than 25 m (82 ft.) were obtained from the sea floor. More recently the U. S. Deep Sea Drilling Project has provided sediment cores from as deep as 1070 m (3 510 ft.) below the ocean floor. Although these samples are disturbed to some degree, it has been possible to make tests for certain en- gineeruig properties of these cores.

The 1961 MOHOLE drilling off Guadalupe Island in the Pacific (28° 59'N, 1 1 30'W) obtained cores through the 1 70 m (558 ft.) of sediment overlying the basaltic basement. At this site water contents ranged from 1 10 percent at the surface to 40 percent at a depth of 170 m (558 ft.) (Rittenberg et al., 1963). There was not, however, a continual decrease in water content with depth. Within the interval 100 to 140 m (328 to 459 ft.) values as high as 120 percent were reported. Hamilton (1964) reported the somewhat surprising finding, that porosity varied little (5 percent) within the 170 m (558 ft.) interval.

20 40 60 80 100 WATER CONTENT (7.DRY WT )

20 40 60 80 POROSITY (%)

Figure 6. Variation of unit weight, water content and porosity with depth at Site 9 (32° 37' N, 59° 10' W) of the Deep Sea Drilling Project

Recent deep-sea drilling in the North Atlantic has contributed significant data on deposits as much as 834,5 m (2737 ft.) below the sea floor (Peterson et al., 1970). Site 9 (32° 37'N, 59° 10' W) of the Deep Sea Drilling Project provides the deepest cored inter- val in the North Atlantic basin yet obtained. Although the hole was not cored continuously, these samples are of the utmost value in any study pertaining to deep-sea sedimentation. Variations with depth of porosity, unit weight and water content have been plotted, Fig. 6, based on the report of Peterson et al. ( 1970). Sur- face values were obtained from unpublished data obtained from short cores collected in the vicinity of Site 9. Porosity and water content tend to decrease with depth. Contrary to the findings of Hamilton (1964) at the Guadalupe site, porosity decreases signifi-

cantly from approximately 82 percent at the surface to 43 per- cent at a depth of 764 m (2506 ft.) It should be noted, however, that there is very little change in porosity below 450 m (1 476 ft.). Unit weight (bulk density) increases gradually with depth, ranging from 1 ,5 g/cc (94 pcf) at the surface to 2,0 g/cc (1 25 pcf) at a depth of 682 m (2237 ft.). An anomalous interval between 204 and 213 m (669 to 699 ft.) is attributed to the interbedding of clay and foraminiferal ooze.

Summary

Investigation of the engineering properties of deep-sea sediments has only received serious consideration in the past ten to fifteen years, and as yet, relatively little has been learned in this area of study. To date, most of the studies have been carried out by marine geologists, who, by applying certain aspects of soil me- chanics, have and are attempting to investigate the various sedi- mentological and environmental characteristics of the unconsoli- dated deposits blanketing much of the sea floor. Thousands of sediment cores have been collected from the North Atlantic, however, relatively few (400 to 500) were obtained for the spe- cific purpose of investigating the engineering properties of sub- marine sediments. Although 400 to 500 cores from an area of approximately 41 X 106 km2 (15,8 X 106 miles2) do not provide representative samples of all the North Atlantic deposits, some generalizations are possible based on these few data:

(a) Calcareous oozes constitute the greatest single sediment type blanketing the North Atlantic basin. Fluvial-marine deposits are the second most abundant sediment type, occurring primarily along the basin margins and in the area between Greenland and Europe.

Although "red clays" are present, they make up only a small percentage of the sediment types found in the North Atlantic.

(b) Average shear strength values for the upper few meters of the sea floor vary from less than 0,5 psi (35g/cm2) to 2 psi (1 40 g/cm2), but more commonly are found to range from 0,5 to 1 psi (35 to 70 g/cm2) over most of the North Atlantic. The highest values yet observed are found in association with the almost pure carbonate deposits of the Bahamas.

(c) Average water contents within the upper 9 to 10 m (30 to 33 ft.) of deep-sea sediments range from slightly less than 50 per- cent to about 175 percent by dry weigth. The majority of the North Atlantic deposits exhibit water contents on the order of 50 to 100 percent.

(d) Unit weight (bulk density) varies from 80 to 125 pcf (1,3 to 2,0 g/cc), but more frequently from 95 to 109 pcf (1,5 to 1,8 g/cc) for the majority of the sediments yet investigated in this basin. Lower densities are commonly found in areas influenced by the debouching of large drainage systems such as the Mississippi and St. Lawrence rivers. Sediment porosities seldom exceed 70 per- cent, but do reach as high as 85 percent in a limited number of areas. More commonly, average porosities are on the order of

60 to 65 percent over most of the basin.

(e) Using the bearing capacity equation for surface loading of a strip load, ultimate bearing capacities were calculated for 22 sites in the North Atlantic. These values ranged from 0,1 to 6,9 psi

(7 to 485 g/cm2), with the majority being 1,5 psi (105 g/cm2) or higher.

Deep-sea sediments are commonly found to exhibit consolidation characteristics similar to those terrestrial deposits classed as slightly overconsolidated. This property is undoubtedly not due to previous loading or desiccation, but may be a result of the very slow rate of deposition taking place in the deep-sea along with possible "cementation" from interparticle or ionic bonding forces.

A few studies of the degree of lateral variation of engineering properties within a local area indicate that rapid changes of these properties often occur over short distances. In one such study of a 400 cm2 (6,2 in.2) area, coefficients of variation (degree of dispersion) were found to be as great as 147 percent and 100 per- cent for sensitivity and shear strength respectively.

Not only are laterial variations important in some areas, but as might be expected, vertical changes in engineering properties can be quite significant even within the upper few meters of the sea floor. Turbidity current deposits, which are found to varying degrees over most of the North Atlantic, exhibit some of the severest variations in mass properties over intervals as small as a few centimeters. Not until the advent of the U. S. Deep Sea Drilling Project have sediment cores longer than 25 m (82 ft.) been collected from the deep sea. Analysis of cored sediments collected during this project to a depth of 834,5 m (2737 ft.) in the North Atlantic ^as provided an insight into the changes of such proper- ties as unit weight, water content, and porosity to this relatively great depth. At drilling Site 9, the most drastic changes in these properties occurred within the upper 40 m (131 ft.) of the sea floor. Water content and porosity decreased considerably as unit weight increased significantly. Below this depth water content decreased continually throughout the cored interval, whereas below a depth of 400 m (1 312 ft.) no significant change in poro- sity was observed. Unit weight increased gradually with depth except in a few intervals where relatively thin layers of contrasting sediments such as foraminiferal ooze caused notable decrease in the unit weight.

The distribution and range of values presented here for selected engineering properties is indeed an over simplification as to the characteristics of deep-sea sediments. We have only begun to study these properties and as with any new investigation there will be continued revisions as more information becomes available.

Acknowledgements

I express my sincere appreciation to Joseph Kravitz of the U. S. Naval Oceanographic Office and Suzanne Bershad of the National Oceanographic Data Center for providing much of the basic data used in this study. Critical review of the manuscript by Louis Butler is gratefully acknowledged.

References

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57

Reprinted from Proceedings Civil Engineering in the

Oceans II, 857.

MASS PROPERTIES OF THE SEA FLOOR IN A SELECTED DEPOSITIONAL ENVIRONMENT

fey

GEORGE H. KELLER1 INTRODUCTION

Man has only begun in the last twenty years to give serious thought to exploiting the sea floor and subsea floor. These interests have progressed gradually from the shoreline to the continental shelf and now, in a few specific areas such as sea-floor mining, into the deep sea. As a result of rapid advances in science and tech- nology, along with man's increasing desire to understand and utilize the marine environment, the new field of ocean engineering has evolved and is fast taking its place beside the other areas of engineering. At this early stage, much of the effort in this field consists of adapting already established engineering principles to the marine environment. This approach has worked reason- ably well for the civil engineer concerned with the soil mechanics or foundation aspects of the sea floor in the relatively shallow waters of the continental shelf. Investigation of the engineering properties of deep-sea deposits has been limited to a small number of studies, generally by marine geologists interested in the depo- sitional processes taking place in the ocean basins.

In contrast to the wealth of soil mechanics data available for terrestrial soils, very little is known about the engineering properties of deep-sea sediments and even less is understood about the influence this unique environment may have on these properties. As might be expected, a number of these properties, particularly in the upper few meters of the ocean floor, differ con- siderably from those reported for terrestrial deposits.

This study was undertaken to investigate the engineer- ing properties of deposits occurring in a somewhat unique deep-sea environment, specifically one consisting of a volcanic cone (seamount) surrounded by the abyssal plain. By examining a number of sediment cores from a small area it was anticipated that not only could the engineering properties be determined, but also ascertain the variation and possible relationship of these properties to the con- trasting topography found at the site. A detailed analysis was made of selected mass properties (cohesion, water con- tent, wet bulk density, texture, porosity, and calcium carbonate content) in order to determine their lateral and vertical variability within the confines of the study area

ESSA, Atlantic Oceanographic and Meteorological Laborato- ries, Miami, Florida 33130

857

858 CIVIL ENGINEERING IN THE OCEANS - II

PREVIOUS INVESTIGATIONS

It is estimated that on the order of 1500 to 2000 sediment cores have been collected from the deep sea for the purpose of studying the engineering properties of sea- floor deposits. Considering the extent to which the sea covers the earth (70 percent), this sampling density clearly points out our lack of information in this environ- ment .

Very few data are available that can be related to the deeper foundation characteristics of the sea floor. This primarily stems from limitations of the sampling techniques presently used by marine geologists to collect deep-sea sediments. Core samples suitable for engineering studies seldom exceed 7m (21 ft.) in length. Studies conducted to date, can only be related to the upper few meters of the sea floor.

The first report on wet unit weight, water content, and shear strength of deep-sea sediments was made by Arrhenius (1952) from his study of a number of Pacific cores collected during the 19l+7-I+8 Swedish Deep-Sea Expe- dition. Shear strength was determined with a fall cone and only relative strengths reported. These values have since been converted to conventional units (Moore and Richards, 1962). Later interest in the engineering prop- erties of submarine sediments stem from the requirements of various military programs for an increased knowledge of the sea-floor environment (Hamilton, 1956; Hamilton, et al., 1956; and Keller, 196*+).

In their efforts to investigate depositional processes or specific characteristics of deep-sea sediments, scien- tists have conducted a number of studies either on specific relationships such as sound velocity and mass properties (Buchan, et al,, 1967), density and depth of burial (Igelman and Hamilton, 1963), consolidation and depositional history (Hamilton, I96W; Richards and Hamilton, 1967) or they have studied the mass properties of a local area (Moore and Shumway, 1959; Richards, 196*+; and Almagor, 1967).

One of the early comprehensive studies on the mass physical properties of deep-sea sediments was that by Richards (1961, 1962) which reported in detail on the test- ing and analysis of 35 sediment cores collected from the north Atlantic, western Mediterranean and north Pacific. This work has provided the basis and impetus for many recent investigations in this field, now referred to as "Marine Geotechnique" (Richards, 1967). As more data have

SEA FLOOR 859

become available, larger scale studies have provided basic engineering properties data on a regional basis, for example, the work of Moore (1962) in the north Pacific. Einsele (1967) in the Red Sea, Bryant and Wallin (1968) in the Gulf of Mexico, and that of Keller and Bennett (1968) who compiled data from approximately 800 cores from the north Pacific and north Atlantic.

Although there is little doubt that considerable instability of the sea floor exists as shown by the occur- rence of numerous slump features and turbidites (graded beds indicative of turbidity flows), only limited informa- tion is available as to the stability of submarine slopes. Terzaghi (1956) presented a lengthy discussion on the various types of failures in submarine slopes, but dealt primarily with the nearshore zone. Moore (1961) investi- gated the shear strength of a number of cores collected from the continental shelf off California. From this study he concluded that submarine sediments were essentially in a stable state on most slopes, except in specialized envi- ronments where the rate of sedimentation was rapid, e.g., deltas and submarine canyons.

An after the fact study of the gullied portion of the San Diego trough by Inderbitzen (1965) presented the characteristic properties of what were reported to be slump deposits. Most recently, Morgenstein (1967) has brought together much of the available information on submarine slumping and has presented a detailed discussion of the mechanics of slumping and the transformation of some such slumps into high density turbidity flows.

STUDY SITE

The setting for this study is 370 km (230 mi.) south- west of San Diego, California in a tectonically active area referred to as the Baja California Seamount province. An abundance of volcanic cones (seamounts) and a micro-relief (*+0 to 100 m [132 to 330 ft.]) of the abyssal sea floor, too rough to permit a generalization regarding depth, characterized this province (Fig. 1). The irregular micro- topography results from tectonic activity, but the specific mechanism such as volcanism or faulting, is not clearly defined. A clear indication of the wide spread volcanism in this area was revealed from a 1,1+00,000 km^ (538,000 mi/) survey of the province by Menard (1959) in which the pres- ence of 1000 seamounts was reported. The eastern margin

860

CIVIL ENGINEERING IN THE OCEANS - II

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o o _

UJ

z

o

CM

*

P

;

o

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SEA FLOOR 861

of this province is bordered by a number of basins and troughs (southern continuation of the continental border- land) which appear to trap sediment being eroded from Baja California (Menard, 1955). Lack of an extensive smooth sediment blanket covering the sea floor, as is found north and south of the province, indicates that little sediment actually bypasses these traps.

Near-bottom currents in the vicinity of the study area trend in a southeast direction at velocities of 2.1+ to if. 10 cm/sec (.08 to 0.1*+ ft. /sec) (Isaacs, et al. , 1966). These investigators also reported similar velocities from the flank of a seamount approximately U8 km (30 mi.) west of the study site. Although their data did not show stronger currents in the vicinity of the seamount they did find, using bottom photographs, that the sea floor was a pavement of pillow lava swept clean of sediment. The occurrence of stronger currents is highly possible since the reported measurements were only for periods of 23.5 to 80.5 hours and during one time of the year.

The actual study area extends over 23,6I+0 km2 (7,200 mi. ) and consists of a prominent seamount rising 2960 m (9768 ft.) above an abyssal plain characterized by a rough micro-relief (Fig. 2). Lack of sufficient bathymetric data precludes the display of this micro-topography. The gentle westerly slope of the sea floor is common to much of the province.

SAMPLING

Twenty sediment cores varying in length from 128 to 320 cm (50 to 128 in.) were collected by the U. S. Naval Oceanographic Office from a small area incorporating a portion of the Pacific abyssal plain and a prominent sea- mount (Fig. 2). Modified Ewing and Kullenberg corers were used, providing samples 6.05 and if. 76 cm (2.38 and 1.88 in.) in diameter respectively (U. S. Navy Hydrographic Office, 1955). The characteristics of these samplers are not ideal for obtaining "undisturbed" material (Richards and Keller, 1961), however, no visible disturbance of the tested por- tions of the cores was noted and the samples were considered on a par with others reported in the literature.

Inert plastic (cellulose acetate butyrate) liners were used in the corers in an effort to reduce chemical reactions between the sediment and the steel barrel and to provide a container in which to transport the sample to the laboratory,

862

CIVIL ENGINEERING IN THE OCEANS - II

3J°5CT

3l°00'h

30° 30'

I22°00'

I2I°00'

120° 30'

FIGURE 2. BATHYMETRIC MAP AND SAMPLE LOCATIONS

SEA FLOOR 863

Since water loss through such a liner can be appreciable (Keller, et al. , 1961), each liner was coated with a micro- crystalline wax after the sample was retrieved.

LABORATORY TESTS

A total of 365 subsamples was tested for selected engineering properties (cohesion, water content, wet bulk density, and grain specific gravity), of these, 207 sam- ples were also analysed for their textural characteristics and calcium carbonate content. Testing procedures for the engineering properties are essentially the same as those established by the American Society for Testing Materials (1958) and have been discussed specifically in regard to submarine sediments by Richards (I96I). Because of the characteristics of this sediment (low cohesion and rela- tively high water content) the standard tests for shear strength were scaled down, but otherwise not altered. The majority of the tests were made with a laboratory-vane shear apparatus (Evans and Sherratt, 19^8 ) and only in a few instances could a modified unconfined compression apparatus be used (Richards, 1961). Undrained shear strength tests were conducted on totally saturated, uncon- solidated sediments. Under these special conditions, shear strength is equal to cohesion, and the strength measured by these tests is a measure of cohesion and is so used here. No corrections have been made for the salt content of the sediment.

Textural determinations were made by the sieving and pipette technique and the analyses for calcium carbonate by the insoluble residue method (Krumbein and Pettijohn, 1938).

Some degree of desiccation or slight disturbance was observed at the ends of almost all the cores. For this reason only those data obtained from the middle portion of the cored interval have been used in this study. The values reported herein are the averages of the respective parameters over the tested portion of the core.

DISCUSSION

The study area consists primarily of an abyssal plain environment with water depths varying from 3712 to ^133 m (12,175 to 13,556 ft.). For the purpose of this study, the abyssal plain is considered to be a relatively flat

864 CIVIL ENGINEERING IN THE OCEANS - II

surface sloping gently to the west, although a micro- topography exists in this area as noted earlier. The sea floor is interrupted in the southwest sector of the study area by a seamount displaying 2960 m (9768 ft.) of relief.

The depositional environment of the site is that of the deep-sea "red clay" deposits, indicating a slow and somewhat uniform rate of sedimentation (few mm per 1000 years). These deposits are terrestrial in origin and are primarily carried in suspension out from the land. Abyssal plain deposits in the study area are texturally quite uniform and exhibit only very minor variation both laterally and with depth (Fig. 3). In 191+ out of the 207 subsamples examined, the median diameter ranged from 1 to 5^ with an average of 2\i. As is commonly found in asso- ciation with "red clays", a silty clay texture predominates in the study area.

Only in those samples taken from the flank of the sea- mount was any noticeable difference observed in the textural characteristics. These sediments were notably coarser than the abyssal plain deposits and were character- ized by a median diameter of Y]\x and a clayey silt texture. The coarser texture is attributed to the winnowing out of a portion of the finer material by currents, along with an increased concentration of calcareous foraminif eral tests which comprise most of the fine sand- and silt-size parti- cles. Although the tests were present in the abyssal plain sediments the relative concentration is considerably higher at the shallow depths of the seamount owing to the lower rate of calcium carbonate solution.

Calcium carbonate content of the surface sediments was low in the abyssal "red clays", averaging about 7 per- cent, but considerably higher (17 percent) on the flank of the seamount (Fig. h) . Microfaunal tests constitute the bulk of the carbonate material, thus the coarser deposits on the seamount correspond to the areas of higher calcium carbonate. A slight decrease in carbonate content is ob- served from east to west on the abyssal plain which may reflect the corresponding gradual increase in water depth in the same direction. The effects of solution at the deeper depths was observed on a number of tests.

Organic carbon analyses of the upper few centimeters of each core revealed an overall average of 0.7*+ percent for the "red clay" and 0.17 percent for the coarser sea- mount sediments. As a general rule, all other things being equal, organic carbon content is directly proportional to

SEA FLOOR

865

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120° 30'

FIGURE 3. MEDIAN DIAMETER AND TEXTURAL DISTRIBUTION.

TEXTURE BASED ON SHEPARD'S (195^) NOMENCLATURE.

866

CIVIL ENGINEERING IN THE OCEANS - II

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SEA FLOOR 867

the concentration of finer particles. It is also found in some instances to have a definite correlation with such properties as cohesion and sensitivity of sediments (Jerbo, 1966).

Specific gravity of the solids varies only slightly in this area, as might be expected for deposits which are not influenced by a number of different source areas. Average values determined for each core range from 2.68 to 2.73. An occasional value as high as 2.93 was found in conjunction with a few thin layers of coarse material (volcanic debris).

Variations in wet bulk density in the area of the abyssal plain are relatively minor and reflect the uniform sediment type comprising most of this portion of the Pacific sea floor. Values range from I.36 to 1.1+2 g/cm^ (8^.9 to 88.6 pcf), which are reasonably close to an average value of l.1!-^ g/cnP (89.9 pcf) reported by Keller and Bennett (1970) for "red clay" deposits. Bulk density values were noticeably higher on the flank of the seamount, varying from 1.57 to 1.70 g/cnP (98 to 106 pcf) with an average of 1.65 g/cm3 (103 pcf). These higher values are attributed to the effects of currents acting on the sea- mount. Winnowing by currents apparently results in the removal of softer (less dense) material and leaving both coarser and denser sediments behind. The distribution pattern shown in Figure 5 clearly reflects the influence pronounced changes in relief have on bulk density.

Water content (percent dry weight) of the deep-sea sediments reveals a gradual increased away from the sea- mount (Fig. 6). Water contents of the abyssal-plain deposits vary from 119 to l'+l percent and do not appear to be influenced by the minor regional changes in topography. The lowest water content values observed (68 percent) occur on the flanks of the seamount, correlating with the coarser and denser sediments also found there.

Although porosity is a calculated value (Terzaghi and Peck, 19^+8) based on other parameters (water content, bulk density and grain specific gravity) it has been included here because of its importance to those investigating the acoustic properties of the sea floor. Porosity was essen- tially uniform throughout the abyssal plain deposits, varying only h percentage points within the study area (Fig. 7). In contrast, the porosity of the seamount sedi- ments was considerably lower (12 to 13 percentage points) than that of the surrounding sea floor.

868

CIVIL ENGINEERING IN THE OCEANS - II

I22°00'

I2I°00'

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30°30'

I22°00

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FIGURE 6. AVERAGE WATER CONTENT OF THE MIDDLE SEGMENT OF THE CORED INTERVAL.

870 CIVIL ENGINEERING IN THE OCEANS - H

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FIGURE 7. AVERAGE POROSITY OF THE MIDDLE SEGMENT OF THE CORED INTERVAL.

SEA FLOOR 871

The distribution pattern for cohesion is not as simple as that shown by the other parameters (Fig. 8), however, a clear distinction exists between the cohesion of abyssal plain sediments and that of the seamount just as has been found for the other properties. Although the other measured parameters appear to show very little variation in the abyssal plain sediments, a noticeable contrast in cohesion is found within these deposits. Much of the area exhibits a cohesion of 60 to 70 g/cm^ (.85 to 1.0 psi) which approximates an average value of ^5 g/cm^ (.6^ psi) reported for "red clay" (Keller and Bennett, 1970). A prominent portion of the sea floor north of the seamount, however, possesses a relatively high cohesion which does not appear to correlate with variations in any of the other measured properties. Sediments on the sea- mount clearly possess higher cohesion as would be anticipated in conjunction with the lower water content and higher bulk densities found there.

CONCLUSIONS

Abyssal plain deposits commonly display rather uniform mass physical properties as nas been shown for a large portion of the north Pacific (Keller and Bennett, 1968). During this study a similar uniformity was observed for the overall sea floor indicating a normal abyssal plain environ- ment. Only in the case of cohesion were anomalous areas of high values observed. Since the other properties measured in this area exhibit no distinct contrast to other portions of the abyssal plain, it is assumed that some other factor has contributed to the zone of higher cohesion. The pres- ence of micro-relief may in some way have affected cohesion yet not have been significant enough to influence the other measured properties. Another possible source for increased cohesion could be local cementation or bonding as a result of pore-water migration. Without considerably more data, a clear explanation for this occurrence is not readily available.

The distribution of the various mass properties is clearly affected by the presence of a volcanic peak rising 2960 m (9768 ft.) above the relatively flat sea floor. As in any dynamic environment a projection above a plain serves to concentrate whatever forces are active in the environment, ocean currents in this case. Samples taken from the flanks of the seamount possess distinctly different characteristics than those of the abyssal plain.

872

CIVIL ENGINEERING IN THE OCEANS - H

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/ J

i

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FIGURE 8. AVERAGE COHESION OF THE MIDDLE SEGMENT OF THE CORED INTERVAL.

SEA FLOOR 873

In viewing the distribution patterns of the various parameters, there is basically little difference found among them. Values tend to increase (grain size, bulk density and cohesion) or decrease (water content and poros- ity) in a radial pattern away from the seamount. Such a pattern would be expected in an area where current veloc- ities are lower away from a topographic high. Relatively higher current velocities acting on the seamount would tend to winnow out much of the finer particles and leave behind both a coarser and denser deposit.

Although micro-relief of ifO-100 m (132 - 330 ft.) exists on the abyssal plain, this scale of relief did not appear to effect the properties of these deposits. This study clearly reveals that a pronounced relationship does exist between the sediment mass physical properties and abrupt changes in relief such as the presence of a seamount on a relatively flat portion of the sea floor.

874 CIVIL ENGINEERING IN THE OCEANS - II

REFERENCES

Almagor, G. , (1967): Interpretation of strength and consolidation data from some bottom cores off Tel-Aviv Palmakhim Coast, Israel: in Marine Geo- technique, Richards, A. F. , Ed., Univ. 111. press, pp. 131-153.

American Society for Testing Materials, (1958): 1958 book of ASTM standards including tentatives, part >+. Philadelphia, Pa., lM-26 pages.

Arrhenius, G. , (1952): Sediment cores from the East

Pacific: Reports of the Swedish Deep-Sea Expedition 19'-+7-191+8, V. 5, No. 1, 227 pages.

Bryant, W. R. , and C. S. Wallin, (1968): Stability and geotechnical characteristics of marine sediments, Gulf of Mexico: Trans. 18th Ann. meeting, Gulf Coast Assoc. Geol. Societies, pp. 33^-356.

Buchan, S. , F. C. D. Dewes, D. M. McCann, and D. Taylor

Smith, (1967): Measurements of the acoustic and geo- technical properties of marine sediment cores: in Marine Geotechnique, Richards, A. F. , Ed., Univ. 111. press, pp. 65-92.

Einsele, G. , (1967): Sedimentary processes and physical properties of cores from the Red Sea, Gulf of Aden, and off the Nile delta: in Marine Geotechnique, Richards, A. F. , Ed., Univ. 111. press, pp. 151+-169.

Evans, I., and G. G. Sherratt, (19^8): A simple and con- venient instrument for measuring the shearing resistance of clay soils: Jour. Sci. Instruments - Physics in Industry, V. 25, pp. Li-ll-1+l1+.

Hamilton, E. L. , (1956): Low sound velocities in high

porosity sediments: Jour. Acoustical Soc. America, V. 28, pp. 16-19.

Hamilton, E. L. , ( 196^-) : Consolidation characteristics and related properties of sediments for experimental Mohole (Guadalupe site): Jour. Geoph. Research, V. 69, pp. L+257-I+269.

Hamilton, E. L. , G. Shumway, H. W. Menard, and C. J. Shipek, (1956): Acoustic and other physical properties of shallow water sediments off San Diego: Jour. Acousti- cal Soc. America, V. 28, pp. 1-15.

SEA FLOOR 875

Igelman, K. R. , and E. L. Hamilton, (1963): Bulk densities of mineral grains from Mohole samples (Guadalupe site): Jour. Sed. Petrology, V. 33, pp. ^7^+- J+yB.

Inderbitzen, A. L. , (1965): An investigation of submarine slope stability: Trans. Conf. on Ocean Science and Ocean Eng. 1965, Marine Tech. Soc. , and Amer. Soc. Limn, and Oceanography, V. 2, pp. 1309-13I^l+.

Isaac, J. D. , J. L. Reid. Jr., G. B. Schick, and R. A.

Schwartzlose, (1966): Near-bottom currents measured in h kilometers depth off the Baja California coast: Jour. Geoph. Research, V. 71, pp. ^297-^303.

Jerbo, A., (1966): Bothnian Clay Sediments - a geological - geotechnical survey: Stockholm, Geotechnical Dept., Swedish State Railways, Bull. 11, 159 pages.

Keller, G. H. , (196^): Investigation of the application of standard soil mechanics techniques and principles to bay sediments: Proc. 1st U. S. Navy Symposium on Military Oceanography, pp. 329-360.

Keller, G. H. , A. F. Richards, and J. H. Recknagel, (I96I): Prevention of water loss through CAB plastic sediment core liners: Deep-Sea Res., V. 8, pp. lt+8-l5l.

Keller, G. H. , and R. H. Bennett, (1968): Mass physical

properties of submarine sediments in the Atlantic and Pacific basins: Proc. XXIII Internat'l Geol. Congress, Sect. 8, pp. 33-50.

Keller, G. H. , and R. H. Bennett, (1970): Variations in the mass physical properties of submarine sediments: Marine Geology, (in press).

Krumbein, W. C. , and F. J. Petti John, (1938): Manual of

Sedimentary Petrography: New York, Appleton-Century- Crofts, Inc., 5^9 pages.

Menard, H. W. , (1955): Deformation of the northeastern Pacific basin and the west coast of North America: Geol. Soc. America Bull. , V. 66, pp. 11^9-1198.

Menard, H. W. , (1959): Geology of the Pacific sea floor: Experientia, V. 15, pp. 205-213.

Moore, D. G. , (1961): Submarine slumps: Jour. Sed. Petrol- ogy, V. 31, pp. 3^3-357.

876 CIVIL ENGINEERING IN THE OCEANS - II

Moore, D. G. , (1962): Bearing strength and other physical properties of some shallow and deep-sea sediments from the North Pacific: Geol. Soc. America Bull., V. 73, PP. 1163-1166.

Moore, D. G. , and G. Shumway, (1959): Sediment thickness and physical properties: Pigeon Point Shelf, Cali- fornia: Jour. Geoph. Research, V. 6h, pp. 367-37I+.

Moore, D. G. , and A. F. Richards, (1962): Conversion of "relative shear strength" measurements by Arrhenius on East Pacific cores to conventional units of shear stress: Geotechnique, V. 11, pp. 55_59.

Morgenstein, N. R. , (1967): Submarine slumping and the

initiation of turbidity currents: in Marine Geotech- nique. Richards, A. F. , Ed., Univ. 111. press, pp. 189-220.

Richards, A. F. , (1961): Investigations of deep-sea sedi- ment cores, I. Shear strength, bearing capacity, and consolidation: U. S. Navy Hydrographic Office Tech. Rept. 63, 70 pages.

Richards, A. F. , (1962): Investigations of deep-sea sedi- ment cores, II. Mass physical properties: IT. S. Navy Hydrographic Office, Tech. Rept. 106 , 1^6 pages.

Richards, A. F. , (196Li): Local sediment shear strength and water content: in Papers in Marine Geology, Shepard Commemorative Volume, Miller, R. L. , Ed., The Macmillan Co., New York, pp. K7h-K8J .

Richards, A. F. , (1967): Marine Geotechnique: Univ. 111. press, 327 pages.

Richards, A. F. , and G. H. Keller, (1961): A plastic- barrell sediment corer: Deep-Sea Res., V. 8, pp. 306-312.

Richards, A. F. , and E. L. Hamilton, (1967): Investigation of deep-sea sediment cores, III. Consolidation: in Marine Geotechnique, Richards, A. F. , Ed., Univ. 111. press, pp. 93-117.

Shepard, F. P., (195*+): Nomenclature based on sand-silt- clay ratios: Jour. Sed. Petrology, V. 21*, pp. 151-158.

Terzaghi, K. , (1956): Varieties of submarine slope fail- ures: Proc. 8th Texas Conf. on Soil Mech. and Found. Eng. Spec. Pub. No. 29, Univ. Texas, Austin, Texas, h2 pages.

SEA FLOOR 877

Terzaghi, K. , and R. B. Peck, (19^8): Soil mechanics in

engineering practice: John A. Wiley & Sons, New York, 566 pages.

U. S. Navy Hydrographic Office, (1955): Instruction manual for oceanographic observations: U. S. Navy Hydro- graphic Office Pub. No. 607, Washington, 210 pages.

Reprinted from The American Association of Petroleum Geologists Bulletin 55_, No. 10, 1719-1729 .

Marine Geophysical Reconnaissance of Continental Margin North of Paria Peninsula, Venezuela1

R. K. LATTIMORE,' L. AUSTIN WEEKS,' and L. W. MORDOCK4

Miami, Florida 33130, 33158, and Seattle, Washington 98102

58

Abstract Marine geophysical observations north of the Paria (Venezuela) Peninsula and westernmost Trinidad have delineated three features that dominate the shallow structural pattern of the shelf: (1) Carupano Sea Valley, which extends eastward along the Paria-Araya shoreline and occupies a structural depression bounded on the south by a major fault system; (2) Cumberland Rise, a locally complex structural and topographic high north of the sea valley; and (3) Tobago Trough, which appears to extend southwest across the shelf almost to the Paria- Trinidad coast. The orientation of the positive elements of Cumberland Rise and the trend of magnetic anomalies that seem to be associated with the Carupano depression suggest that both features may be related to the Lesser Antilles arc. Detritus eroded from the Paria-Araya Penin- sulas is inferred to have been transported eastward through Carupano Sea Valley info Tobago Trough; the Paria shelf has been built upward and northward by sediments which bypassed the valley and were carried directly offshore, over the Cumberland Rise, to be de- posited as foreset beds on an old erosion surface.

The extension of the Lesser Antilles arc southwest into the Paria-Araya shelf is marked by a +60 to +100 mgal free-air gravity anomaly. A shallow igneous intrusive extends from Los Testigos Islands northeast along the trend of this anomaly to the upper continental slope, where the intrusive is truncated by a northwest-southeast fault. The fact that the trends of the arc can be traced well into the Paria shelf militates against the presence of an east-west transcurrent fault between Carupano Sea Valley and the Grenada platform.

Introduction

As part of an Environmental Science Ser- vices Administration program for the investiga- tion of the structure of ocean basins and their margins, marine geophysical observations have been made in an extensive area of the Carib- bean Sea and Atlantic Ocean adjacent to the Paria-Araya Peninsulas of Venezuela, and sur- rounding the islands of Trinidad, Tobago, and Grenada. The results of reconnaissance seis- mic-reflection, bathymetric, gravimetric, and magnetic observations made by USC&GSS Dis- coverer in the summers of 1968 and 1969 will be presented in a series of reports, the first of which are three papers in this issue of the Bul- letin. Our study, which covers measurements made over the Paria-Trinidad shelf and Gre- nada platform between 61°30'W and 63°00/W (Fig. 1), is addressed to two specific objec- tives: (1) determination of the structure of the Paria-Trinidad shelf and its relation to

the Lesser Antilles island arc and the South American continent; and (2) location of the transcurrent or transform fault which, accord- ing to the hypotheses of the "new global tecton- ics" (Isacks et al., 1968), must separat; the Caribbean "plate" from the South American continent.

Previous Study

The earliest marine geophysical observations in the southeast Caribbean were isolated sub- marine gravity measurements made in 1936— 1937 (M. Ewing et al, 1957). In 1947, addi- tional gravity measurements were made along a northwest-southeast traverse of the Paria shelf (M. Ewing et al, 1957). The first detailed bathymetric map of the Paria and Trinidad shelves was published by Koldewijn (1958) as part of a study of the near-surface sediments. Seismic-refraction investigations of the shelf, Tobago Trough, and adjacent parts of the Lesser Antilles arc, conducted by Lamont Geo- logical Observatory in 1955, were reported by J. Ewing et al (1957) and Officer et al (1959). This and subsequent work have been summarized and reviewed by Edgar (1968) and J. Ewing et al (in press).

1 Manuscript received, August 24, 1970; accepted, December 3, 1970.

2 National Oceanic and Atmospheric Administration (NOAA), Atlantic Oceanographic and Meteorological Laboratories.

3 Consultant; formerly. Environmental Science Ser- vices Administration.

4 NOAA, National Ocean Survey, Pacific Marine Center; formerly, seismic-profile officer, USC&GS ship Discoverer.

The writers thank the officers and crew of USC&GS (now NOAA) ship Discoverer, W. W. Doeringsfeld, Jr., William Everard, G. A. Lapiene, Jr., N. J. Malo- ney, Wendell Mickey, and Paul Miller, for their sup- port and cooperation in conducting the field work. G. H. Keller served as chief scientist during part of the survey. Geophysical data were reduced and plotted us- ing programs developed by Paul Grim and Bobby Bas- singer. Sue O'Brien drafted the figures. The paper was reviewed critically by L. W. Butler and B. J. Szenk.

© 1971. The American Association of Petroleum Geologists. All rights reserved.

1719

1720

R. K. Lattimore, L. Austin Weeks and L. W. Mordock

ARAYA-PARIA-TRINIDAD SHELF

SOUNDINGS IN FATHOMS MERCATOR PROJECTION

Fig. 1. Track-line index and bathymetric map, Araya-Paria-Trinidad shelf and Grenada platform. (Sound-velocity corrections were not applied to soundings.)

Methods

Continuous underway seismic-reflection, bathymetric, gravimetric, and magnetic obser- vations were made along the ship's tracks shown on the bathymetric map (Fig. 1). The profiles were run at a nominal speed of 5 knots (9 km/hr); as a result of sea conditions and equipment testing, actual speeds varied from 2 to 9 knots (3.7 to 17 km/hr). Navigational control was by radar range and bearing, visual bearings, and astronomical fixes. The estimated probable error in any ship's position is ± 2 n.mi (±3.7 km).

The seismic reflection profiles were made with a Bolt Associates, Inc., 10-cu in. (164 cc) air gun system with a 25-ft (7.6 m) array of 10 variable reluctance hydrophones. The sound source was fired at 2- or 4-second intervals; the return signal was subjected to a 39-320 Hz bandpass filter and recorded on an Alpine- Muirhead recorder. Interpretative line drawings of representative seismic profiles are presented in Figure 2.

In water depths greater than 100 fm (183 m), soundings were taken with a General In-

strument Corporation "narrow-beam echo- sounding system" which utilizes an electroni- cally-stabilized beam having an effective cone- width of 2%°. Shallow-water soundings were obtained with Raytheon DE-723 fathometer. Soundings are considered accurate to ±1 per- cent (L. G. Taylor, personal commun.). The bathymetric map (Fig. 1) was prepared from published and unpublished data collected by the U.S. Navy and other sources, in addition to our own profiles.

Underway gravity measurements were made with an Askania-Graf seagravimeter mounted on an Anschutz gyro-stabilized platform. The data, corrected for instrumental drift and Eotvos effect5, are presented in the form of free-air anomaly profiles in Figure 3. Although gravity values at track intersections consis- tently were within 10 mgal of each other, dis- crepancies with older data (e.g., M. Ewing et al., 1957) range up to ±20 mgal.

Continuous profiles of earth's total magnetic field were obtained with a Varian Associates,

5 Observed gravity values are relative to Barbados: Seawell Airport f = 978.2997.

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1722

R. K. Lattimore, L. Austin Weeks and L. W. Mordock

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Fia. 3. Free- air gravity anomaly profiles, Paria shelf (AA'-DD') and Grenada platform (JJ'-MM'). From top to bottom, the profiles are arranged from west to east.

Inc., direct-reading proton precession magne- tometer. Critical values were scaled from the graphic record and reduced to residual anoma- lies by using the parameters of the Interna- tional Geomagnetic Reference Field. The mag- netic-anomaly profiles (Fig. 4) are considered to be internally consistent to ±20 y.

Regional Setting

A nearly flat continental shelf, 40-60 n.mi (75-110 km) across, lies where the trends of the Lesser Antilles arc intersect the margin of the South American continent (Fig. 1). This shelf extends from the island of Tobago west- ward beyond 64 °W; it is bounded on the south by the rugged coast ranges of Trinidad and the

Paria-Araya Peninsulas of Venezuela. The coast ranges are breached at Dragon's Mouth, where depths greater than 120 fm (220 m) were measured.

West of Dragon's Mouth, the southernmost part of the shelf is occupied by a shallow valley which Maloney (1967) named the Carupano Sea Valley (Fig. 1). This valley extends from southeast of Isla Margarita due east to about 62 °W, where it opens into a north- to north- east-trending embayment that is considered to be an extension of Tobago Trough (Edgar, 1968). North of the sea valley a broad, very gentle swell can be traced for about 70 n.mi (130 km) east from Isla Margarita; shoals of 10fm(18m)or less occur on this swell south of Los Testigos Islands. We propose the name "Cumberland Rise," for this feature.

The nearly flat part of the Paria shelf termi- nates in a scarp of 50-80 fm (90-150 m) re- lief, which extends east along 11°30'N from 63 °W to approximately 61°40'W. North of this scarp, a gradient of 1:100 or less persists to depths of approximately 400 fm (730 m), where the slope increases by a factor of two or more. Below 700-800 fm (1,280-1,460 m) the smooth slope gives way to a zone of rough, rolling topography.

A platform extends southwest of the island of Grenada to approximately 62 °W, where the sea floor dips abruptly to depths of 300-500 fm (550-910 m; Fig. 1). This platform is sep- arated from the Paria shelf by a broad, asym- metric trough or basin in which depths do not exceed 500 fm (910 m). The floor of this basin generally is smooth and undissected, although shallow channels near the western end of the Grenada platform suggest that local drainage is toward the northwest. On its eastern end, at about 61°40'W, this valley opens into Tobago Trough.

Paria Shelf

Within the depths penetrated by the seismic profile equipment 0.3-0.5 sec two-way travel time the flat continental shelf consists of nearly horizontal stratified rocks. Reflectors near the outer edge of the shelf suggest foreset bedding, and it is clear that the shelf has been built upward and northward by progradation (AA\ BB', DD', JJ', Fig. 2). The shallow sedi- ments of the central and inner shelf are charac- terized by well-defined, subparallel, continuous reflectors; individual beds dip gently and thicken very gradually toward the south (AA\ BB', DD', Fig. 2). Although the sediments

Marine Geophysical Reconnaissance of Venezuela

1723

which make up the shelf are relatively unde- formed, faults of small displacement, open folds, and gentle flexures affect near-surface as well as deeper strata. Few individual structural features are of sufficient magnitude so that they can be traced from one profile to the next.

Coastline Fault System

The abrupt transition from the folded and intruded Mesozoic rocks which form the moun- tainous Paria-Araya Peninsulas (Maxwell and Dengo, 1951; Bucher, 1952; Gonzalez de Juana et ah, 1968) to the nearly horizontal younger strata that comprise the shelf is best explained in terms of major faulting along the shoreline. Fault contact between rocks of the coast ranges and the shelf sediments can be demonstrated in a profile taken through Dragon's Mouth (Bas- singer et al., 1971, this issue of Bulletin). Both profiles east of 62°30'W (CC and DD') show that near-horizontal to north-dipping, com- monly gently folded strata near the coast have been uplifted in relation to apparently equiva- lent, south-dipping sediments farther seaward, a feature that suggests that uplift of the coast ranges has taken place along several faults which form a system oriented generally east- west, parallel with the shoreline.

Carupano Sea Valley

Carupano Sea Valley occupies a structural depression bounded on the south by one or more faults of the coastline system. At 62° 50' W (AA', Fig. 2), this depression is a well-de- fined graben, perhaps 10 n. mi (18 km) across. The graben, or at least the northern bounding fault, can be recognized on the two profiles far- ther east (BB', Fig. 2, and CC), so it may be inferred that the structure extends at least to 62°15'W. At 61°50'W (DD', Fig. 2) the northern fault could not be recognized, but nearly the entire central part of the shelf is tilted southward along a pair of faults that are in line with the presumed southern boundary of the graben. Although Koldewijn (1958) has concluded that sediments derived from the coast ranges since the last glacial period have not yet been moved out of the littoral, the mountainous coastal provinces should supply sufficient detritus to fill the Carupano Sea Val- ley during any extended period of quiescence. Persistence of the sea valley and thickening of individual sedimentary units across faults are strong indications of continuing subsidence.

12°N

Fig. 4. Residual magnetic anomaly profiles, Paria shelf (AA'-DD') and Grenada platform (JJ'-MM'). Dashed lines indicate correlated anomalies whose trends are shown in Figure 6. The shaded area de- notes zone of short-wavelength anomalies which are attributed to shallow igneous intrusive.

Cumberland Rise

Cumberland Rise (Fig. 1) reflects a locally complex, structurally positive feature whose general trend is slightly north of east. At 62°50'W (AA', Fig. 2), the predominant southward apparent dip of the shelf sediments is broken at, and in places reversed along, sev- eral faults of varying sense and amount of dis- placement. At 62°30'W (BB', Fig. 2), an esti- mated 0.35 sec or more of net displacement is distributed along a series of faults south of the axis of the rise; with but one exception, motion along these faults is down-to-the-south, and dis- placement generally increases with depth. Far-

1724

R. K. Lattimore, L Austin Weeks and L W. Mordock

ther east, at 62°20'W down-to-the-south dis- placement is manifested in abrupt, slight in- creases in the south dip component of the sub- surface reflectors; the only significant faults are those which form the graben associated with Carupano Sea Valley. Along 61°50'W (DD', Fig. 2), the sediments dip south from a struc- tural high on the outer shelf at 11°20'N; the only discernible faults v/ould be part of the coastline system. Although topographic relief of Cumberland Rise dies out east of 62°30'W (Fig. 1), the writers suggest that the anticlinal structure at 61°50'W, north of Dragon's Mouth (DD', Fig. 2), is on the main axis of the underlying structure. Alignment of this trend suggests kinship with an older positive structural element that includes Isla Margarita.

Tobago Trough

From seismic-refraction data collected by Lamont Geological Observatory, Edgar (1968) concluded that Tobago Trough extends south- west into the Paria-Trinidad shelf. This conclu- sion is supported by the nearshore bathymetry (Fig. 1) as well as by our geophysical observa- tions. The pronounced negative gravity anom- aly which occurs over the shelf north of Drag- on's Mouth (DD', Fig. 3) is consistent with the

accumulation of a thick column of sediments in the trough, as postulated by Edgar (1968). In the central part of the shelf north of Dragon's Mouth, the seismic profile (DD', Fig. 2) shows 0.2 sec of sediments containing angular to sub- parallel, poorly defined, discontinuous, com- monly curved or arcuate reflectors, sandwiched between sequences of the continuous, well-de- fined reflectors characteristic of the shelf sedi- ments (Fig. 5). The discontinuous, curved re- flectors are believed to represent foreset beds traversed at a small angle to the strike of the slope face. Structures more readily identified as foreset beds were observed at similar depths along profiles at 61°30'W and 61°10'W, 15- 30 n.mi (30-55 km) from the shoreline. The approximate limit of these beds is shown on the "structural" diagram (Fig. 6). The presence of foreset beds interbedded with the normal shelf sediments is considered to be indicative of rapid local subsidence of the central part of the shelf, and also is consistent with incursion of Tobago Trough.

The narrow, —20 to —40 mgal free-air anomaly which is developed over the southern- most part of the shelf east of 62°30'W (CC, DD', Fig. 3) supports the conclusion of Edgar (1968) that a wedge of sediments, 5-7 km

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Marine Geophysical Reconnaissance of Venezuela

63°W 62°

1725

61°W

12°N

11°N-

Fic. 6. Trends and structural patterns of Paria shelf and parts of Tobago Trough and Grenada platform. (Contours are in fathoms.)

(16,400-23,000 ft) thick, extends from To- bago Trough along the Paria coast to 63 °W. The Dragon's Mouth profile (DD', Fig. 3) sug- gests that this minimum is isolated from the broad low associated with incursion of the shelf by Tobago Trough. Bassinger et al. (1971) show that this low is present at 61°30'W.

Sedimentary Framework of Paria Shelf

West of 62 °W the edge of the Paria shelf is built up by at least two distinct sequences of foreset bedding superimposed on each other (AA', BB', JJ', Fig. 2); the younger of these sequences forms the scarp at 11°30'N, de- scribed heretofore. An easily recognized reflect- ing horizon separates the two series of foreset beds; reflectors above this horizon are subparal- lel to angular with respect to those below it. In several localities a slope face developed on the lower sequence can be discerned beneath 0.1- 0.15 sec of younger detritus (e.g., BB', Fig. 2); such fossil scarps lie a few nautical miles land- ward of the present slope. The lower series of sediments is unconformable on broadly folded and intruded older rocks (JJ', Fig. 2). The gently graded terrace in the 200-300-fm (350-550 m) depth range is considered to be a

manifestation of this unconformity, as is the near-level surface of the "basement" ridge at 62°30'W (BB', Fig. 2; Fig. 7). The erosion surface at 200-300 fm (350-550 m) lies far below the generally accepted Pleistocene sea- level minimum, so at least an element of subsi- dence must be invoked to explain its position. Subsidence alone, however, does not account satisfactorily for the near-coincidence of the fossil and present foreset slope faces a re- peated event or, more likely, a cyclic series of events is required.

The structures interpreted as foreset bedding, which suggest subsidence of the central part of the shelf north of Dragon's Mouth (DD', Fig. 2), also suggest that the foreset slope face was oriented at an acute angle to the ship's track (i.e., north or northwest) and that the path of sediment transport across this part of the shelf had a significant east-west component. From these inferences and the evidence of repeated or continuous subsidence of Carupano Sea Val- ley, it may be postulated that sediments derived from the Paria-Araya Peninsulas, and possibly from as far west as Margarita, have been trans- ported east through Carupano Sea Valley to about 62 °W, and then northeast across the

1726

R. K. Lattimore, L. Austin Weeks and L. W. Mordock

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shelf into Tobago Trough. This pattern corre- sponds closely with the distribution of a distinc- tive Holocene heavy-mineral assemblage mapped by Koldewijn (1958: Fig. 8). If this hy- pothesis is valid, intervals of quiescence must be postulated, during which Carupano Sea Val- ley was filled completely and the sediments were transported directly offshore. Detritus car- ried seaward and dumped over Cumberland Rise would have built the edge of the shelf up- ward and seaward, producing sedimentary structures like those seen in the seismic profiles from the western part of the shelf.

Trends of Lesser Antilles Arc

A broad, asymmetric magnetic-anomaly maximum can be traced for about 30 n.mi (55 km) eastward along the edge of the Paria shelf to 62°10'W, where it is abruptly truncated (AA', BB', JJ', Fig. 4). This anomaly is correl- ated with a broad, asymmetric maximum that has been mapped, east of the Grenadine plat- form, by J. Ewing et at. (1960); it probably is related to the island arc and not to the shelf. Data from outside the study area suggest that the irregular maximum which is present over the continental slope at 62°W (MM', Fig. 4), and the increasing values at the northern end of the easternmost track line (DD', Fig. 4) also may be identified with this feature.

The presence of a thick wedge of sediments along the Paria coast strongly suggests that the Carupano Sea Valley depression is structurally continuous with Tobago Trough. However, a pattern of magnetic-anomaly maxima, which in the western part of the shelf seems to coincide with Carupano Sea Valley (BB', CC, DD', Fig. 4), can be traced across the axis of the trough to at least 61°15'W; east of 62°30'W the trend swings slightly north (Fig. 6). If the anomalies are genetically related to the Cam-

Marine Geophysical Reconnaissance of Venezuela

1727

pano Sea Valley depression then this structure, at depth, must extend nearly as far east as To- bago; it is not likely to be part of the present Tobago Trough.

Extension of Trends of Lesser Antilles Arc into Paria Shelf

The presence of "basement" landward of the foreset edge of the shelf at 62°50'W (A A', Fig. 2) was deduced from the presence of undulat- ing, discontinuous, strong reflectors having pro- nounced multiples. These reflectors coincide with a zone of short-wavelength magnetic anomalies, superimposed on a broad maximum which is believed to be related to the island arc (AA', Fig. 4); the short-wavelength anomalies are indicative of a shallow crystalline source, most probably an igneous body. A well-defined basement structure, its top presumably planed off by wave action, is present along 62°30'W (BB', Fig. 2; Fig. 7), north of the foreset slope face at depths of 200-300 fm (350-550 m). In a third locality, the westernmost of four pro- files that were run at right angles to the trend of the Grenada platform, possible basement crops out on the sea floor below 400 fm (730 m; JJ', Fig. 2). The fact that basement in these two profiles also is crystalline is shown by dis- tinctive magnetic signatures which coincide with the structural features (BB', JJ', Fig. 4).

The three occurrences of crystalline base- ment fall on a line which, if extended toward the southwest, includes Los Testigos Islands. Maloney (1967) reported that the largest of these islands consists of a granitic intrusive sur- rounded by younger volcanics. We suggest that the islands and the three profile crossings define a single, essentially continuous, northeast- southwest-trending intrusive igneous body.

The investigation of the Grenada platform included four profiles run on northwest or southeast headings, normal to the long axis of the platform. The westernmost of these profiles (JJ') contains convincing evidence of "base- ment" structure, but the next profile (KB'), taken parallel with and about 5 n.mi (9 km) east of the first, contains no evidence of base- ment, even though the records show penetration of a half-second or more with good resolution. The short-wavelength magnetic anomalies at- tributed to the intrusive do not extend east of 62°20'W (profile JJ') ; instead, the broad low is broken by a distinctive, local maximum which can be traced east-southeastward for about 15 n.mi (28 km; KB', LL', KK", Fig. 4).

The igneous ridge probably disappears at

62°20'W because of a fault. This possibility in- vites speculation that the fault extends south- eastward and also truncates the broad, asym- metric magnetic-anomaly maximum mapped near the edge of the shelf in the western part of the area (e.g., BB', Fig. 4). Such a fault might be confined to the intruded older sedimentary rocks and would not necessarily have any ex- pression in the shallow strata.

The offshore basement ridge and Los Testi- gos Islands are so clearly on strike with the Gre- nada platform and the trend of the Lesser An- tilles arc that truncation of the ridge at 62°20'W and development of a different mag- netic-anomaly pattern are presumed to represent only relatively shallow effects. The gravity anomalies show that the deeper trend of the is- land arc does extend into the Paria shelf. A dis- tinctive + 60 to +100 mgal free-air anomaly, which patently is related to the Grenada plat- form (MM', Fig. 3), can be traced southwest- ward through all three remaining oblique lines (LL', KB', and JJ', Fig. 3) and across the two western north-south lines (BB', AA', Fig. 3), where it coincides with the crystalline basement ridge. The regional study of Bush and Bush (1969) suggests that this anomaly continues across Los Testigos Islands to Isla Margarita where, much reduced in amplitude, it turns al- most due west.

Grenada Platform

The Grenada platform physiographically if not structurally the southern end of the Lesser Antilles arc is a massive core complex overlain by layered sedimentary rocks that range in thickness from 0 to 0.5 sec penetration. The deeper strata usually exhibit variable, commonly comparatively steep apparent dips. The core complex is exposed on the sea floor near the western end of the platform.

A +60 to +100 mgal free-air gravity anom- aly and a broad, fairly smooth magnetic-anom- aly minimum were observed over the western end of Grenada platform (MM', Figs. 3, 4). The free-air anomaly indicates the presence of excess mass and tends to corroborate the exis- tence of a dense, high seismic-velocity "root" beneath the island arc (Edgar, 1968). Observa- tions by other investigators (e.g., J. Ewing et ah, 1960; Bunce et al., 1970) suggest that the magnetic-anomaly profile is not atypical, and that the southern Lesser Antilles platform gen- erally is marked by a fairly smooth, broad min- imum. This minimum can be explained only by the presence of a reversely magnetized body

1728

R. K. Lattimore, L. Austin Weeks and L. W. Mordock

(G. Peter, personal commun.). Local, short- wavelength anomalies mark presumably young- er intrusives.

Inter-Platform Basin

At about 62°05'W northward-dipping sedi- ments of the Paria shelf and slope nearly lap onto the intensely folded layered rocks and core complex of the Grenada platform. The two provinces are separated only by a V-shaped sea-floor valley, no more than 2 n. mi (3.7 km) wide and having perhaps 50 fm (90 m) relief. East of 62°05'W this valley widens into an asymmetric, shallow basin (Fig. 1) which opens into Tobago Trough.

Most of the shallow sediments in the inter- platform basin appear to have been carried across the Paria shelf and dumped over the foreset slope face. Exhibiting a variety of struc- tures indicative of penecontemporaneous de- formation and submarine erosion, they form a wedge 0.2-0.5 sec thick which occupies the floor of the basin (KK", Fig. 2). Detritus from the Grenada platform seems to be restricted to a narrow band near its base.

Summary and Conclusions

The Paria shelf is underlain by more than 1,000 ft (0.3-0.5 sec penetration) of sediments and sedimentary rocks exhibiting subparallel, generally well-defined, continuous reflectors. In general, these beds dip gently and thicken southward; they are cut by numerous faults, commonly of small displacement. Thickening of individual beds across these faults and other evidence attest to continued or repeated epeiro- genic activity.

Three major structural-physiographic ele- ments can be delineated within the Paria shelf. Carupano Sea Valley, which extends eastward along the inner shelf parallel with the Paria-Ar- aya shoreline, occupies a structural depression in places a graben bounded on the south by a zone of faults along which the coast ranges were uplifted. Cumberland Rise, a topographic and locally complex structural high north of the sea valley, is believed to reflect a positive element extending from Isla Margarita east- northeast beyond 62 CW. The southwest exten- sion of Tobago Trough (as shown by Edgar, 1968) is manifested (1) as a shallow embay- ment that extends across the shelf almost to Dragon's Mouth; (2) in a negative free-air gravity anomaly associated with the outer shelf north of Dragon's Mouth; and (3) in the oc-

currence of foreset beds intercalated with "nor- mal" strata, interpreted as representing sudden, local subsidence of the central part of the shelf. East of 62°30'W the distinctive topography of Cumberland Rise disappears, and the associ- ated shallow structures become less complex, probably because of the accumulation of an in- creasingly thick blanket of trough sediments. The overall structural pattern of the shelf sug- gests a block that has been tilted down toward the south along the Araya-Paria-Trinidad coast, and further depressed by Tobago Trough, north of Dragon's Mouth. Our investigations do not exclude the possibility that the Caru- pano Sea Valley depression is a structural ex- tension of Tobago Trough, but magnetic anom- alies, which seem to be associated with the de- pression in the western part of the study area, extend beyond the axis of the trough nearly as far east as Tobago. East of 62°30'W the trend of these anomalies develops a pronounced northward curvature, parallel with the trend of the Lesser Antilles arc.

Of the three major features which comprise the Paria shelf, only Tobago Trough is gener- ally accepted as being part of the island arc sys- tem, but the east-northeast orientation of Cum- berland Rise and the magnetic anomalies asso- ciated with Carupano Sea Valley raise the pos- sibility that the other two elements are more closely related to the arc than to the South American continent. A broad, asymmetric mag- netic-anomaly maximum over the outer shelf west of 62°10'W is correlated with a similar pattern mapped by J. Ewing et al. (1960) north of Grenada; this pattern almost certainly is associated with the arc.

The physiography and shallow structure of the shelf, together with distribution of a Holo- cene heavy-mineral assemblage (Koldewijn, 1958), support a hypothesis that the principal path for sediment eroded from the Paria-Araya Peninsulas has been alongshore through Caru- pano Sea Valley and northeastward across the shelf into Tobago Trough. At such times as the trough or the sea valley was filled to a local base level, detritus was transported directly off- shore; prograding or foreset sediments, depos- ited unconformably on older folded and in- truded sedimentary rocks, have built the edge of the shelf upward and seaward. East of 62 °W, sediments carried over the foreset slope face have been deposited in a comparatively shallow, asymmetric basin that opens on the east into Tobago Trough; this basin constitutes a second route by which detritus eroded from

larine Geophysical Reconnaissance of Venezuela

1729

the Paria-Araya Peninsulas can be conveyed into Tobago Trough.

Geophysical evidence indicates that Grenada platform and by extension the southern Lesser Antilles arc is composed of a relatively uniform, reversely magnetized, crystalline body of rock and a dense, high seismic-velocity "root." Seismic-reflection and magnetic-anom- aly data support the existence of a shallow ig- neous body extending from Los Testigos Is- lands northeast toward Grenada. Although this structure is truncated at 62°20'W (probably by faulting), gravity data substantiate extension of the Lesser Antilles trend into the Paria-Araya shelf; the intrusive body coincides with the trend.

The fact that the trends of the Lesser Antilles and Tobago Trough can be traced well into the Paria shelf implies that any recent transcurrent faulting within the area of investigation could occur only near the Paria-Araya shoreline. If, as is required by the "new global tectonics" (Isacks et al., 1968), the Caribbean plate is sep- arated from the South American continent by a fault along which._great lateral displacement has taken place, this fault if it does not predate the island arc must occur south of 1 1 °N. Evi- dence against this possibility is presented in Bassinger et al. ( 1971, this issue) and discussed by Weeks et al. (1971, this issue).

References Cited

Bassinger, B. G., R. N. Harbison, and L. A. Weeks, 1971, Marine geophysical study northeast of Trini- dad-Tobago: Am. Assoc. Petroleum Geologists Bull., v. 55, no. 10, p. 1730-1740.

Bucher, W. H., 1952, Geologic structure and orogenic history of Venezuela: Geol. Soc. America Mem. 49, 113 p.

Bunce, E. T, J. D. Phillips, R. L. Chase, and C. O. Bovvin, 1970, Lesser Antilles Arc and the eastern margin of the Caribbean Sea: Woods Hole Oceanog. Inst. Contrib. 2288, 36 p.; in press, in A. E. Max-

well, ed., The sea, v. 4: New York, Wiley-Intersci-

ence. Bush, S. A., and P. A. Bush, 1969, Isostatic gravity map

of the eastern Caribbean region: Gulf Coast Assoc.

Geol. Soc. Trans., v. 19, p. 281-285. Edgar, N. T, 1968, Seismic refraction and reflection in

the Caribbean Sea: Ph.D. dissert., Columbia Univ.,

163 p. Ewing, J. I., C. B. Officer, H. R. Johnson, and R. S.

Edwards, 1957, Geophysical investigations in the

eastern Caribbean Trinidad shelf, Tobago trough,

Barbados ridge, Atlantic Ocean: Geol. Soc. America

Bull., v. 68, p. 897-912.

J. W. Antoine, and W. M. Ewing, 1960, Geo- physical measurements in the western Caribbean Sea and in the Gulf of Mexico: Jour. Geophys. Re- search, v. 65, p. 4087-4126.

N. T. Edgar, and J. VV. Antoine, in press, Gulf

of Mexico and Caribbean Sea, in A. E. Maxwell, ed., The sea, v. 4: New York, Wiley-Interscience.

Ewing, W. M., J. L. Worzel, and G. L. Shurbet, 1957, Gravity observations at sea in U.S. submarines Bar- racuda, Tusk, Conger, Argonaut and Medregal: Koninkl. Nederlandsch Geol.-Mijn. Genoot. Verh., Geo!. Ser., v. 18, p. 49-115.

Gonzalez de Juana. C N. G. Munoz J., and M. Vig- nali C, 1968, On the geology of eastern Paria (Ven- ezuela) : 4th Caribbean Geol. Conf. Trans, p. 25-29.

Isacks, B., J. Oliver, and L. R. Sykes, 1968, Seismology and the new global tectonics: Jour. Geophys. Re- search, v. 73, p. 5855-5899.

Koldewijn, B. W., 1958, Sediments of the Paria-Trini- dad shelf; v. 3 of Reports of the Orinoco Shelf expe- dition: The Hague, Mouton and Co., 109 p.

Maloney, N. J., 1967, Geomorphology of the continen- tal margin of Venezuela, Pt. 2, Continental terrace off Carupano: Bol. Inst. Ocean., Univ. Oriente (Cumana, Venezuela), v. 6, p. 147-155.

Maxwell, J. C, and Gabriel Dengo, 1951, Carupano area and its relation to the tectonics of northeastern Venezuela: Am. Geophys. Union Trans., v. 32, no. 2, p. 259-267.

Officer, C. B., J. I. Ewing, J. F. Hennion, D. G. Hark- rider, and D. E. Miller, 1959, Geophysical investi- gations in the eastern Caribbean: Summary of 1955 and 1956 cruises, in L. H. Ahrens et al., eds., Physics and chemistry of the earth, v. 3: New York, Perga- mon Press, p. 17-109.

Weeks, L. A., R. K. Lattimore, R. N. Harbison, B. G. Bassinger, and G. F. Merrill, 1971, Structural rela- tions among Lesser Antilles, Venezuela, and Trini- dad-Tobago: Am. Assoc. Petroleum Geologists Bull., v. 55, no. 10, p. 1741-1752.

59

Reprinted from Nature Physical Science 232 , No. 31,

97-98 .

Deformation of the Sea Floor off the North-west Coast of the United States

GEORGE PETER & OMAR E. DeWALD

NOAA, Atlantic Oceanographic and Meteorological Laboratories, Miami, Florida 33130

A new fracture zone separating the Tufts Abyssal Plain from the moun- tainous topography of the Explorer and Juan de Fuca ridges has been discovered on the basis of the magnetic anomaly offsets. North-east-south-west compres- sion is the likely cause for the rotation, strike-slip faulting, and deformation of the small crustal blocks of the area.

Thirteen east-west tracklines run by NOAA ships during the past few years off the coasts of Oregon and Washington enabled us to identify the magnetic anomaly lineations and to establish their offset pattern west of the Juan de Fuca and Gorda ridges. The magnetic lineation pattern obtained (Fig. 1) reveals a new NW-SE trending fault zone which cuts the magnetic anomalies west of the Juan de Fuca Ridge, and explains the abrupt drop of the sea floor and the disappearance of the rough topography associated with the Juan de Fuca Ridge west of the proposed fault (Fig. 2). The establishment of the anomaly pattern from the Juan de Fuca Ridge to anomaly 7 (ref. 1) closes the gap that existed between the well known pattern near the coast and in the central north-east Pacific2-3.

It is usually considered that magnetic anomaly lineations

Fig. 1 Map of the sea floor magnetic anomaly lineations off the coasts of Washington and Oregon. Zip patterns demon- strate the correlation of the magnetic anomalies across the various fault offsets. Numbers (I) refer to key magnetic anoma- lies. Number 1 (from north to south) is associated with the centre parts of the Explorer, Juan de Fuca, and Gorda ridges.

Fig. 2 Map of the magnetic anomaly offsets (dashed lines) superimposed on a sketch of the bathymetry of the sea floor west of Washington and Oregon. Zip patterns-show the idealized crestal areas of the mid-oceanic ridge segments; dark patches show the major seamounts. The shelf edge is depicted by the 100 fathom isobath (1 fathom=1.83 m). For clarity, contour lines (200 fathom contour intervals) are shown only in depths greater than 1,600 fathoms. Bathymetry is after Chase el a/.14. The new names, Juan de Fuca, Explorer, and Cobb fault zones, were approved by the Board on Geographic Names.

originate from the upper, basaltic part of the oceanic crust and represent strips of rocks which were formed at the centre of mid-oceanic ridges under the influence of the periodically reversing magnetic field of the Earth". As the oceanic crust is younger and has a much simpler tectonic history than the continental crust5, the magnetic lineations acquired by the oceanic crust at the time of its genesis have been preserved through geologic time. Magnetic anomaly maps, therefore, show the offsets of former mid-oceanic ridges and the offsets or deformation pattern of the oceanic crust acquired after its formation.

The Juan de Fuca and Gorda ridges represent short segments of a former mid-oceanic ridge6 which in large part has been obliterated as it migrated eastward and collided with the North American continent17. The origin of the two ridges and the reason for their north-easterly trend have long been a matter of controversy. Various authors have discussed whether the ridges separated and tilted north-east in adjustment to a change in the direction of sea floor spreading7-8, or whether they became offset and rotated as a result of a strike-slip faulting". We believe that the new data (Fig. 3) suggest a solution to this problem.

The magnetic anomaly offset pattern (Fig. I) follows the interpretation of Pavoni'0 and Peter and Lattimore9, and is based on the magnetic anomaly map of Mason and Raff2

1 —"" 1

2, ^^\/j\^Aj^

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Fig. 3 o, Tracklines used for the westward extension of former magnetic anomaly maps. 6, Selected east-west magnetic anomaly profiles showing identification and correlation of the magnetic anomalies. The location of the profiles is shown in a.

south of the Blanco fracture zone, east of the Juan de Fuca Ridge, and east of 134° W in the area north of48°N. In the remaining part of Fig. 1 the magnetic lineations were established on the basis of east-west tracklines which, with the exception of a few cross lines, extend approximately along each degree latitude. A more detailed survey, therefore, may show this area structurally more complex than indicated by this figure.

The new magnetic anomaly data show that anomaly 6 has only minor offsets south of the Sedna fracture zone. The Surveyor fracture zone ends directly west of anomaly 6, and the Blanco fracture zone terminates at the southern tip of the Juan de Fuca Ridge. The magnetic anomaly pattern is continuous west of the Gorda Ridge, but anomaly 5 and a number of anomalies between 5 and 6 are missing west of the Juan de Fuca Ridge. The disappearance of the anomalies occurs along a north-west line which correlates with a sharp 300 fathom (550 m) change in the relief of the sea floor (Fig. 2). To the west of this line lies the Tufts Abyssal Plain with a gentle topo- graphic gradient rising eastward; to the east lies the moun- tainous topography of the Juan de Fuca Ridge. We suggest that this demarcation line trending north-west separating the magnetic lineations and cutting the topography of the Juan de Fuca Ridge at an oblique angle represents a fracture zone, and we named it the Juan de Fuca fracture zone.

The origin of the Juan de Fuca fracture zone is most likely related to the Late Tertiary deformation11 that affected this entire area. It appears in light of the new data that if the Explorer, Juan de Fuca, and Gorda ridges were continuous at the time of the formation of anomaly 5, approximately 10 m.y. ago3, then they must have been in alignment with the segment of anomaly 5 located west of the Gorda Ridge, where the anomaly sequence is uninterrupted. The missing anomalies and the well defined fault-border of the crustal fragments indicate that the deformation involved the rotation, strike-slip faulting, and overthrust of small crustal plates north of the Blanco and Juan de Fuca fault zones, rather than a gradual realignment of the ridges under the influence of a change in the direction of the sea floor spreading. If the magnetic anomalies that were offset by strike-slip faults east of the Juan de Fuca Ridge are aligned, a north-south crustal shortening of 120 km is indicated. The offset of anomaly 5 and the missing anomalies suggest a 200 km westerly displacement and consequent destruction of the crust

along the Juan de Fuca and Blanco fracture zones. Part of the north-south compression has been transmitted to the area of the Gorda Ridge, where the deformation of anomaly 3 near the coastline indicates a north-south compression of 150 km.

North-south compression indicated by the deformation pattern of the magnetic anomalies is in agreement with the relative plate motions derived for the area east of the Juan de Fuca and Gorda ridges7-12. The scatter of earthquakes13 east of the Gorda Ridge also supports the proposed compression of that area, but to the north the distribution of the earthquakes indicates that at the present time the deformation is con- centrated along the Explorer and Blanco fault zones. A more detailed discussion of the plate motions of the area will be presented in another article now in preparation.

We thank B. H. Erickson, NOAA, Pacific Oceanographic Laboratories, for providing most of the magnetic anomaly profiles.

Received July 20, 1971.

1 Pitman, W. C, III, Herron, E. M., and Heirtzler, J. R., J. Geo-

phys. Res., 73, 2069(1968).

2 Raff, A. D., and Mason, R. G., Bull. Geol. Soc. Amer., 72, 1267

(1961); Mason, R. G., and Raff, A. D., Bull. Geol. Soc. Amer , 72, 1259(1961).

3 Pitman, W. C, III, and Hayes, D. E , J. Geophys. Res., 73,

6571 (1968). * Vine, F." J., and Matthews, D. H., Nature, 199, 947 (1963); Vine, F. J., Science, 154, 1405 (1966); Cox, A., Doell, R. R., and Dalrymple, G. B., Science, 144, 1537 (1964).

5 Hess, H. H., in Submarine Geology and Geophysics (vol. 17,

Colston papers) (edit, by Whittard, W. F., and Bradshaw, R.), 317 (Butterworths, London, 1965); Dietz, R. S., Amer. J. Sci., 264, 177(1966).

6 Wilson, J. T., Science, 150, 482 (1965); Menard, H. W., Marine

Geology of the Pacific, 111 (McGraw-Hill, New York, 1964).

7 Atwater, T., Bull. Geol. Soc. Amer., 81, 3513 (1970).

8 Menard, H. W., and Atwater, T., Nature, 219, 463 (1968); ibid.,

222, 1037 (1969).

9 Peter, G., and Lattimore, R., J. Geophys. Res., 74, 586 (1969).

10 Pavoni, N., Pure Appl. Geophys., 63, 172 (1966).

11 McManus, D. A., Marine Geol., 3, 429 (1965); Wise, D. V.,

Bull. Geol. Soc. Amer., 74, 357 (1963).

12 Silver, E. A., Science, 166, 1265 (1969).

13 Tobin, D. G.,and Sykes, L. R.,7. Geophys. Res., 73, 3821 (1968).

14 Chase, T. E., Menard, H. W., and Mammerickx, J., The Institute

of Marine Resources (University of California, 1970).

Primed in Grcal Briiam by Flarepath Printers Limned. Watling Sireel. Colney Streel. St. Albans. Herts

60

Reprinted from The Sea, Vol. 4, Pt. 2, 191-222.

5. MAGNETIC STRUCTURE OF THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN

(June 1968)

George Peter, Barrett H. Erickson, and Paul J. Grim

1. Introduction

The large number of detailed magnetic surveys and exploratory tracklines made during the last decade have contributed significantly to the development of new ideas and to the understanding of the structure and evolution of the oceanic crust. Particularly significant among the methods of study of crustal structure was the Scripps Institution of Oceanography U.S. Coast and Geodetic Survey magnetic-bathymetric survey project off the west coast of the United States (Mason, 1958; Mason and Raff, 1961; Vacquier et al., 1961; Raff and Mason, 1961). It was found that the magnetic anomalies in this area form parallel, north-south trending lineations which are frequently offset as if by lateral faults. Offsets of the magnetic lineations were found to be associated with fracture zones such as the Mendocino; investigation of other offsets led to the discovery of other major fracture zones with well-developed topographic expression. Like the magnetic lineations themselves, the minor offsets appear to lack topographic or even sub-bottom expression; these features, however, generally are considered to reflect internal structure of the oceanic crust or upper mantle. The pattern of the magnetic anomaly lineations therefore can be called the magnetic structure.

Throughout the world, similar magnetic-anomaly lineations have been found to be disposed symmetrically along either side of the axis of the mid-oceanic rises (Vine, 1966; Pitman et al., 1968; Dickson et al, 1968; Le Pichon and Heirtzler, 1968; Heirtzler et al., 1968). The axial symmetry of these magnetic- anomaly lineations and their correlation (within a central crestal zone) with dated magnetic-polarity reversals on land and with the magnetic reversals found in deep-sea cores have given strong support to the hypothesis of crustal evolution through sea-floor spreading (Dietz, 1961; Hess, 1962; Vine and Matthews, 1963; Heirtzler et al., 1966; Ninkovich et al., 1966; Vine, 1966; Cox et al., 1964; Opdyke et al., 1966; Dickson and Foster, 1966).

Detailed studies by McManus (1965), Loncarevic et al. (1966), van Andel et al. (1967), and van Andel and Bowin (1968) have provided insight into the hitherto unknown, complex geology of the crests of the mid-oceanic rises. Although this new information does not directly contradict the hypothesis of sea-floor spreading, it has raised serious questions as to its applicability. Important limitations can be placed on the mechanism of sea-floor spreading by the Y-shaped ridge-junction discovered near the Galapagos Islands (Herron and Heirtzler, 1967; Raff, 1968), by the sediment distribution over mid-oceanic ridges (Ewing and Ewing, 1967), and by the undisturbed sediments in "trans- form fault" zones and trenches (Ludwig et al., 1966; van Andel et al., 1967; Scholl et al., 1968).

191

192

PETER, ERICKSON, AND GRIM

[chap. 4

The purpose of this paper is to describe the magnetic structure of the North- east Pacific and the Aleutian Arc, and to discuss the questions that can be raised in regard to the application of the sea-floor spreading hypothesis within this area. All available data from the Northeast Pacific have been compiled. Magnetic and bathymetric maps for the central Northeast Pacific and the Aleutian Arc that have significant bearing on the discussion are presented, and their implications in regard to crustal genesis are discussed in some detail.

The specific areas under consideration (Fig. 1) represent part of the total systematic coverage under ESSA Coast and Geodetic Survey project SEAMAP (Peter and Stewart, 1965; Peter, 1965; Elvers et al., 1967). Tracks for these surveys comprise a grid of north-south lines approximately spaced at 18 km intervals; irregularly spaced cross-lines were run as checks. Magnetic and bathymetric data were collected with a Varian proton-precession magnetometer and a Precision Depth Recorder, respectively. Accuracies of these measurements are discussed in Peter et al. (1965) and Elvers et al. (1967).

Primary control of the survey was obtained from LORAN-C. Lines run relatively close to the LORAN-C net provided positions along the tracklines with an estimated accuracy of + 1 km. The uncertainty in position increases to the south, although no obvious discrepancies were noted north of 38°N. Between 35°30'N and 38°N, one trackline was rejected and three others were adjusted in a north-south direction by 5 km, based on systematic discrepancies of the magnetic and bathymetric values among adjacent tracklines.

The density of tracklines and the prominence of the lineations are adequate to show all essential details on the magnetic-anomaly contour maps. The trackline density and the contour interval selected are sufficient to delineate the major topographic features. The shortcomings of the 18-km grid, however, are clearly evident in areas of irregular topography or elongated, smaller seamounts and ridges.

150" 170°E 170°W 150" 130"

Fig. 1. Map of North Pacific Ocean: areas of detailed coverage shown in center (A, B, C).

60

Reprinted from The Sea, Vol. 4, Pt. 2, 191-222.

5. MAGNETIC STRUCTURE OF THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN

(June 1968)

George Peter, Barrett H. Erickson, and Paul J. Grim

1. Introduction

The large number of detailed magnetic surveys and exploratory tracklines made during the last decade have contributed significantly to the development of new ideas and to the understanding of the structure and evolution of the oceanic crust. Particularly significant among the methods of study of crustal structure was the Scripps Institution of Oceanography U.S. Coast and Geodetic Survey magnetic-bathymetric survey project off the west coast of the United States (Mason, 1958; Mason and Raff, 1961; Vacquier et al., 1961; Raff and Mason, 1961). It was found that the magnetic anomalies in this area form parallel, north-south trending lineations which are frequently offset as if by lateral faults. Offsets of the magnetic lineations were found to be associated with fracture zones such as the Mendocino; investigation of other offsets led to the discovery of other major fracture zones with well-developed topographic expression. Like the magnetic lineations themselves, the minor offsets appear to lack topographic or even sub-bottom expression; these features, however, generally are considered to reflect internal structure of the oceanic crust or upper mantle. The pattern of the magnetic anomaly lineations therefore can be called the magnetic structure.

Throughout the world, similar magnetic-anomaly lineations have been found to be disposed symmetrically along either side of the axis of the mid-oceanic rises (Vine, 1966; Pitman et al., 1968; Dickson et al, 1968; Le Pichon and Heirtzler, 1968; Heirtzler et al., 1968). The axial symmetry of these magnetic- anomaly lineations and their correlation (within a central crestal zone) with dated magnetic-polarity reversals on land and with the magnetic reversals found in deep-sea cores have given strong support to the hypothesis of crustal evolution through sea-floor spreading (Dietz, 1961; Hess, 1962; Vine and Matthews, 1963; Heirtzler et al., 1966; Ninkovich et al., 1966; Vine, 1966; Cox et al., 1964; Opdyke et al., 1966; Dickson and Foster, 1966).

Detailed studies by McManus (1965), Loncarevic et al. (1966), van Andel et al. (1967), and van Andel and Bowin (1968) have provided insight into the hitherto unknown, complex geology of the crests of the mid-oceanic rises. Although this new information does not directly contradict the hypothesis of sea-floor spreading, it has raised serious questions as to its applicability. Important limitations can be placed on the mechanism of sea-floor spreading by the Y-shaped ridge-junction discovered near the Galapagos Islands (Herron and Heirtzler, 1967; Raff, 1968), by the sediment distribution over mid-oceanic ridges (Ewing and Ewing, 1967), and by the undisturbed sediments in "trans- form fault" zones and trenches (Ludwig et al., 1966; van Andel et al., 1967; Scholl et al., 1968).

191

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193

2. Central Northeast Pacific

A. Bathymetry

In area A (Figs. 1, 2a), there are three distinct bathymetric provinces separated by major fracture zones. South of the Mendocino Fracture Zone, the sea floor is comparatively smooth and has an average depth of 3100 fathoms (5670 m). This area falls under the classification of an abyssal-hill province (Hurley, 1960; Menard, 1964); there is a general east- west trend in the bottom topography which strongly contrasts with the irregular abyssal-hill topography north of the Mendocino Fracture Zone. Two east-west troughs with associated ridges on their northern side cut the ocean floor at 36°10'N and 37°20'N. The troughs and ridges have a relief of approximately 300 fathoms (550 m). A third trough at 37°45'N is bordered by ridges on both sides.

The Mendocino and Pioneer fracture zones cannot be separated. Complex elongated ridges and valleys with steep walls that resemble horsts and grabens extend from 38°N to 39°30'N within this zone (Fig. 3). The central

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194 PETER, ERICKSON, AND GRIM [CHAP. 5

valley of the Mendocino Fracture Zone (Menard, 1964) is the deepest part of the sea floor here. At the western end of Fig. 2a the greatest depth measured was 3525 fathoms (6450 m). In this area all the valleys and ridges of the Mendocino Fault Zone strike 070°.

Between the Mendocino and Surveyor fracture zones (Peter, 1966; Fig. 2a) the abyssal hills are more prominent and there are numerous small seamounts. The sea floor has an average depth of 3000 fathoms (5490 m); this is 100 fathoms (180 m) higher than the sea floor south of the Mendocino Fracture Zone, and 200 fathoms (360 m) lower than the base of the Mendocino ridges.

The Surveyor Fracture Zone has a strike parallel to the Mendocino Fracture Zone and is located at 42°45'N (Fig. 2a). Topographically, it is a 350-fathom (650 m) high ridge, bounded on the northern side by a 200-fathom (360 m) deep trough. Elongated ridges and a generally irregular topography north of the trough appear to be related to the fracture zone. From this area northward to the Aleutian Trench the sea floor is smooth and rises gently to the north.

B. Magnetic Anomalies

The displacement of magnetic anomaly lineations (Mason, 1958; Vacquier et al., 1961) provides a method for the determination of the offsets along the submarine fracture zones. Peter (1966) previously discussed the offsets along the fracture zones of this area. Anomalies 27, 28, and 29 to the north of the Surveyor Fracture Zone and 25 and 26 to the south of it (labelled in Fig. 4) are identified from the spectrum of the world-wide magnetic-anomaly lineations (Pitman et al., 1968) in Fig. 2b. Although it has been found that east of this area the offsets of the magnetic-anomaly lineations and bottom topography generally agree in displacement (Menard, 1964), it has not been determined whether or not a particular type of bottom topography is characteristic of a specific group of magnetic lineations. It is generally agreed that there is no correlation between the individual magnetic-anomaly lineations and the bottom topography. Correlation is not found even between the magnetic data and the rugged topography of the second layer (Drake et al., 1963). Nevertheless these observa- tions only stress the lack of direct, one-to-one correlation; Peter (1966) reported that the minor steplike elevation changes and broad (200-300 km) undulations in the sea-floor topography appear to line up with the strike of the magnetic- anomaly lineations.1

In the area of the Surveyor Fracture Zone, the absence of correlation between the magnetic lineations and the sea-floor topography is well illustrated. Sound- ing and magnetic profiles suggest that this fracture zone forms a border between the smooth, south-southwest dipping, sea floor to the north and the generally horizontal, abyssal-hill province to the south. Yet the magnetic anomalies

1 Recent studies by Talwani et al. (1968) in the area of the Reykjanes Ridge have shown that within a positive or negative magnetic anomaly lineation the variation of the ampli- tude of the anomaly is caused, in general, by changes of the bottom topography. Deep-tow magnetometer observations indicate correlation between trends of the magnetic anomalies and small-scale bottom irregularities (Spiess et al., 1968).

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196 PETER, ERICKSON, AND GRIM [CHAP. 5

(offset by 300 km in a right lateral sense) cross this fracture zone and continue through the two entirely different bathymetric provinces without apparent change in character.

A detailed study of the Murray Fracture Zone indicates that there are elongated magnetic anomalies over the horst-graben pattern of the topography (Malahoff, 1968); in contrast to this, over this area of the Mendocino Fracture Zone magnetic anomalies are absent over even the sharpest ridges. There is a broad, magnetic low over the central part of the fracture zone, but it appears to strike east-west rather than to follow the strike of the topography.

South of the Mendocino Fracture Zone (Figs. 2a, b) the magnetic field is smooth (with the exception of three elongated anomalies over the troughs and ridges described earlier). The magnetic anomalies are strikingly different over each of these features. Over the northernmost feature a positive anomaly is present, over the central feature there is a prominent negative anomaly, and over the southernmost trough and ridge the anomaly consists of both negative and positive parts, disposed in accordance with induced magnetization in the northern hemisphere. None of the anomalies, however, is suggestive of induced magnetization due to the earth's present magnetic field. If simple vertical-sided bodies are assumed as sources, the direction of the dip of the magnetization vector, as judged by the model studies of Heirtzler et al. (1962), is different for each of these features.

3. Abyssal Plain and Trench Southwest of Kodiak

A. Bathymetry

The Aleutian Abyssal Plain (Hurley, 1960) lies between the Aleutian Trench and the Surveyor Fracture Zone (Figs, lb, and 5). The sea floor is essentially flat, with a small southward dip of 2 m/km. A number of knolls and seamounts that vary in heights from a few hundred to over one thousand meters are distributed irregularly throughout the area. The general fabric of the sea-floor topography trends northeast-southwest in the southeastern part of Fig. 5, and northwest-southeast in the southwestern part. At 51°N weak east- west trends are observed; these give way to the northeast-southwest trends at the southern wall of the Aleutian Trench. There is no outer ridge associated with the Aleutian Trench in this area; only a small swell separates the abyssal plain and the trench.

Depths in the trench vary from 3000 fathoms (5480 m) on the east to 3800 fathoms (6960 m) on the west. Although the southern wall of the trench is relatively smooth, the northern wall is irregular with a few benches and welts which persist for great distances (Peter et al., 1965).

B. Magnetic Anomalies

In area A and most of area B (Fig. 1) the magnetic lineations generally strike N18°W. Between 47 °N and 51°30'N these lineations progressively bend

196 PETER, ERICKSON, AND GRIM [CHAP. 5

(offset by 300 km in a right lateral sense) cross this fracture zone and continue through the two entirely different bathymetric provinces without apparent change in character.

A detailed study of the Murray Fracture Zone indicates that there are elongated magnetic anomalies over the horst-graben pattern of the topography (Malahoff, 1968); in contrast to this, over this area of the Mendocino Fracture Zone magnetic anomalies are absent over even the sharpest ridges. There is a broad, magnetic low over the central part of the fracture zone, but it appears to strike east-west rather than to follow the strike of the topography.

South of the Mendocino Fracture Zone (Figs. 2a, b) the magnetic field is smooth (with the exception of three elongated anomalies over the troughs and ridges described earlier). The magnetic anomalies are strikingly different over each of these features. Over the northernmost feature a positive anomaly is present, over the central feature there is a prominent negative anomaly, and over the southernmost trough and ridge the anomaly consists of both negative and positive parts, disposed in accordance with induced magnetization in the northern hemisphere. None of the anomalies, however, is suggestive of induced magnetization due to the earth's present magnetic field. If simple vertical-sided bodies are assumed as sources, the direction of the dip of the magnetization vector, as judged by the model studies of Heirtzler et al. (1962), is different for each of these features.

3. Abyssal Plain and Trench Southwest of Kodiak

A. Bathymetry

The Aleutian Abyssal Plain (Hurley, 1960) lies between the Aleutian Trench and the Surveyor Fracture Zone (Figs, lb, and 5). The sea floor is essentially flat, with a small southward dip of 2 m/km. A number of knolls and seamounts that vary in heights from a few hundred to over one thousand meters are distributed irregularly throughout the area. The general fabric of the sea-floor topography trends northeast-southwest in the southeastern part of Fig. 5, and northwest-southeast in the southwestern part. At 51°N weak east- west trends are observed ; these give way to the northeast-southwest trends at the southern wall of the Aleutian Trench. There is no outer ridge associated with the Aleutian Trench in this area; only a small swell separates the abyssal plain and the trench.

Depths in the trench vary from 3000 fathoms (5480 m) on the east to 3800 fathoms (6960 m) on the west. Although the southern wall of the trench is relatively smooth, the northern wall is irregular with a few benches and welts which persist for great distances (Peter et al., 1965).

B. Magnetic Anomalies

In area A and most of area B (Fig. 1) the magnetic lineations generally strike N18°W. Between 47°N and 51°30'N these lineations progressively bend

. 5. Bathymotric map of area B (Fig. 1). Contour interval 50 fms (1 fm = 1.83 m), except in areas of large gradients in which the interval is increased (from Elvers et al., 1967).

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN

197

+500 -500

I 1 1

GAMMAS

Fig. 6. Illustration of the offset of the magnetic -anomaly lineations across the Amlia and Adak fracture zones (location of profiles shown in Fig. 12) (from Grim and Erickson, 1969).

sharply westward, and their general strike becomes N83°W (Fig. 7). Anomaly 32B (see Fig. 4 for identification) bends first, at the south-west part of Fig. 7; anomaly 25 is the last lineation that clearly bends westward. The east-west lineation along 53°30'N and the south-east limb that projects from it may be anomaly 24. The new strike represents an abrupt change in orientation of 65° for all these anomalies.

The control for the magnetic map is shown in Fig. 8, and discussed in detail by Elvers et al. (1967). To demonstrate the continuity of the anomalies around the bend, a number of north -south magnetic lines from this area are compared to east-west lines in Fig. 9. It is shown that along the profiles the character of the anomalies changes abruptly at the bend. The entire group of lineations is present on the westernmost profile (Fig. 9, profile 1).

One of the most pronounced differences between the east-west and north- south portions of the lineations is the higher amplitude of the anomalies along the east-west segments. Model studies (Heirtzler et al., 1962) indicate that the change in orientation of the lineations with respect to magnetic north (which changes approximately from 30 to 70° across the bend) is not sufficient to

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN

197

Fig. 6. Illustration of the offset of the magnetic-anomaly lineations across the Amlia and Adak fracture zones (location of profiles shown in Fig. 12) (from Grim and Erickson, 1969).

sharply westward, and their general strike becomes N83°W (Fig. 7). Anomaly 32B (see Fig. 4 for identification) bends first, at the south-west part of Fig. 7; anomaly 25 is the last lineation that clearly bends westward. The east-west lineation along 53°30'N and the south-east limb that projects from it may be anomaly 24. The new strike represents an abrupt change in orientation of 65° for all these anomalies.

The control for the magnetic map is shown in Fig. 8, and discussed in detail by Elvers et al. (1967). To demonstrate the continuity of the anomalies around the bend, a number of north-south magnetic lines from this area are compared to east-west lines in Fig. 9. It is shown that along the profiles the character of the anomalies changes abruptly at the bend. The entire group of lineations is present on the westernmost profile (Fig. 9, profile 1).

One of the most pronounced differences between the east-west and north- south portions of the lineations is the higher amplitude of the anomalies along the east-west segments. Model studies (Heirtzler et al., 1962) indicate that the change in orientation of the lineations with respect to magnetic north (which changes approximately from 30 to 70° across the bend) is not sufficient to

Rig. 7. Magnetic total intensity anomaly map of area B (Fig. 1). Contour interval is 100

gammas (from Fivers ot al., 1967).

198

PETER, ERICKSON, AND GRIM

[CHAP. 5

160

Fig. 8. Trackline chart of area B (Fig. 1). Small course changes are not shown (accuracy + 3 km).

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN

199

32B

32A

31 30

29 28 27

26 25

46l

48fc

50c

52^ i

26 25

148 c 1

146° __l

144' L_

142'

L_

E

200

0

200

r200

- 0 —200

140°

Fig. 9. Illustration of the westward bend of the magnetic -anomaly lineations. Selected north-south profiles (upper half) are compared to two east-west profiles (lower half) run along 35°30'N and 36°30'N. Location of N-S profiles is shown in Fig. 8.

account for the increase in amplitude of the positive anomalies. The change in orientation in certain parts of the area would provide an adequate explanation for the change in amplitude of the negative lineations. In other parts, however, the change in amplitude is either greater or much less than that which would be expected from the model studies.

The decrease of distance between anomalies 26 and 27 after these lineations bend westward, is also quite prominent. By contrast, the distance between 31 and 32B increases considerably. The decreased distance between anomalies 26 and 27 seems to be at the expense of the broad, generally negative area directly east of 27; the extra distance between anomalies 31 and 32B apparently is taken up by two additional, small lineations (Fig. 6c).

200 PETER, ERICKSON, AND GRIM [CHAP. 5

A narrow, positive and negative lineation also is developed north of the east-west segment of anomaly 25. If the prominent east-west lineation along 53°30'N is anomaly 24, the distance between 24 and 25 is greatly increased after the westward bend. Furthermore, if the northwest-southeast trending, positive anomaly at 52°N, 156°W, is part of anomaly 24, then there is an apparent break in this lineation at 52°30'N. A similar break of anomaly 32A is seen just before it bends westward. A more detailed survey would be necessary to adaquately determine the smaller internal fractures and the discontinuities of these lineations.

4. Aleutian Trench and Outer Ridge (164°W to 180°W)

A. Bathymetry

Area C (Fig. 1) includes the Aleutian Trench and outer ridge. The weakly developed, east-west trending ridges on the outer swell southwest of Kodiak continue westward and their relief increases progressively. By 172°W a typical outer ridge of moderate relief is present (Fig. 10).

At 172°40'W, a north-south depression cuts through the outer ridge. West of this depression there are a number of seamounts and the relief of the outer ridge is greater than it is to the east. The seamounts on the western side of this depression mark the location of the north-south trending Amlia Fracture Zone (Grim and Erickson, 1969; Hayes and Heirtzler, 1968). No indication of this fracture zone is seen in the trench; however, the change in trend of the Aleutian Arc may be related to it.

Another depression, with a less pronounced relief and a somewhat irregular shape, crosses the southern part of the outer ridge at 177°20'W. This depression marks the general location of the Adak Fracture Zone (Grim and Erickson, 1969). There is no appreciable difference in the topography of the outer ridge on opposite sides of this fracture zone, nor is there any evidence of a fracture zone on the trench floor. The offset of the depression between the Aleutian Terrace and the Aleutian Arc (Nichols and Perry, 1966), however, may be related to this feature. This offset approximately 30 km appears to be expressed as a reduction of the width of the Aleutian Terrace.

Adak Canyon to the north is approximately in line with the Adak Fracture Zone, and is probably another expression of it. The canyon separates strikingly different topography on either side. A generally smooth shelf on the east changes to chaotic topography, riddled with numerous smaller canyons, on the west. The eastern wall of Adak Canyon trends north-south; it is quite steep and has the appearance of a fault scarp.

B. Magnetic data

Westward extension of the magnetic anomaly lineations is shown in Fig. 11. Correlation of the magnetic lineations across the Amlia and Adak fracture zones is demonstrated in Fig. 6 (location of profiles is shown in Fig. 12).

o o

o o

J2

O

I

u •z o +-<

a

o U

o

ft

ft

08

Pi

c* fe

202

PETER, ERICKSON, AND GRIM

[CHAP. 4

-}-450

165°

Fig. 12. Trackline chart of area C (Fig. 1) (after Grim and Erickson, 1969).

The anomalies terminate abruptly at the axis of the trench; traces of anomalies 24, 25, and 26, however, appear to cross the trench and extend over the Aleutian Terrace (Fig. 6a, profiles P, Q, and R). The east- west trend of the isogamma lines north of the trench between the Amlia and Adak fracture zones may also represent vestiges of the east- west magnetic lineations.

Generally, the magnetic field is smooth over the trench, but short- wavelength anomalies are found in shallow water near the islands where the tracklines cross the top of the Aleutian Ridge. Hayes and Heirtzler (1968) report that no traces of the lineations can be found in the Bering Sea north of the Aleutian Islands.

The location of the Amlia and Adak fracture zones was determined by the offset of magnetic lineations. The Amlia Fracture Zone offsets most lineations in a left-lateral sense by 230 km. The offset of anomalies 32A and 32B is only 140 km. The difference in offset is the result of two small anomalies (Fig. 6c, box) that are developed between anomalies 31 and 32 A east of the Amlia Fracture Zone.

Anomalies 25 and 26 are not seen on profiles N and M (Fig. 6c); they seem to disappear where they cross the axis of the Aleutian Trench. Similarly, anomalies 27 and 28 disappear in the trench east of the Amlia Fracture Zone. Anomalies 29 through 32B do not cross the trench. These anomalies have the same

Fig. 11. Magnetic total-intensity anomaly map of areas B and C (Fig. 1). Contour interval ia 100 gammaa.

202

PETER, ERICKSON, AND GRIM

[CHAP. 4

-J- 45°

165°

Fig. 12. Trackline chart of area C (Fig. 1) (after Grim and Erickson, 1969).

The anomalies terminate abruptly at the axis of the trench; traces of anomalies 24, 25, and 26, however, appear to cross the trench and extend over the Aleutian Terrace (Fig. 6a, profiles P, Q, and R). The east-west trend of the isogamma lines north of the trench between the Amlia and Adak fracture zones may also represent vestiges of the east-west magnetic lineations.

Generally, the magnetic field is smooth over the trench, but short-wavelength anomalies are found in shallow water near the islands where the tracklines cross the top of the Aleutian Ridge. Hayes and Heirtzler (1968) report that no traces of the lineations can be found in the Bering Sea north of the Aleutian Islands.

The location of the Amlia and Adak fracture zones was determined by the offset of magnetic lineations. The Amlia Fracture Zone offsets most lineations in a left-lateral sense by 230 km. The offset of anomalies 32 A and 32B is only 140 km. The difference in offset is the result of two small anomalies (Fig. 6c, box) that are developed between anomalies 31 and 32 A east of the Amlia Fracture Zone.

Anomalies 25 and 26 are not seen on profiles N and M (Fig. 6c); they seem to disappear where they cross the axis of the Aleutian Trench. Similarly, anomalies 27 and 28 disappear in the trench east of the Amlia Fracture Zone. Anomalies 29 through 32B do not cross the trench. These anomalies have the same

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN 203

amplitude on both sides of the Amlia Fracture Zone; anomalies 25 through 28, which disappear in the trench, have a uniformly lower amplitude west of the Amlia Fracture Zone.

The offset of the magnetic anomalies across the Adak Fracture Zone is 30 km left-lateral. Figure 6b clearly shows the offset of anomalies 25 and 26. Data from Hayes and Heirtzler (1968) further support this offset, although these authors offer a different interpretation of the fracture pattern of this area.

The offset at 178°30'E was interpreted from data published by Hayes and Heirtzler (1968). The offset at 176°30'E was adopted from their interpretation.

5. Magnetic Structure of the Northeast Pacific Ocean

A. General Pattern

The Northeast Pacific constitutes an especially satisfactory area for the study of the geophysical implications of the magnetic anomalies because of the excellent survey coverage. An interpretation of the magnetic data available at the time of the writing of this article is assembled in Fig. 4. Most data are taken from published maps and profiles, unpublished data are presented through the courtesy of R. H. Higgs, U.S. Naval Oceanographic Office, and W. C. Pitman III and D. E. Hayes, Lamont-Doherty Geological Observatory.

The magnetic-anomaly lineations are numbered according to the system of Pitman et al. (1968). For most of the area shown in Fig. 4, the magnetic lines were mapped by detailed systematic surveys (18 km grid or closer); where the pattern of lineations was established from a few isolated tracklines, these tracks are indicated by black circles. For the schematic representation of the fracture zones, heavy lines are used. Dashed lines represent the possible exten- sion of the anomalies and the fracture zones in areas in which control is poor or not available.

The magnetic lineations of the Northeast Pacific can be separated into the following three groups or "magnetic structural provinces":

1. The coastal pattern ("crestal anomalies" of Heirtzler and Le Pichon, 1965) is found east of anomaly 7 (or east of anomaly 10 between the Pioneer and Murray fracture zones) and is cut by numerous northwest-southeast and northeast-southwest faults.

2. The central pattern, between anomalies 7 and 21 (10 and 21 between the Pioneer and Murray fracture zones) consists only of north -south trending lineations. This pattern is cut by east-west faults that apparently are confined to these lineations.

3. The western pattern extends from anomaly 21 through anomaly 32B. It strikes northwest-southeast and bends abruptly as it approaches the Aleutian Trench. This pattern is also cut by fault zones that are nearly perpendicular to the lineations.

The orthogonal relationship between the faults and the lineations of the central and western patterns is especially striking in the case of the Surveyor

204 PETER, EKICKSON, AND GRIM [CHAP. 5

and the Mendocino fault zones; these clearly change trend toward the south- west at the beginning of the general area of the western pattern (Fig. 4).

Differences between the three patterns are further illustrated in Table I. The distance between a chosen lineation of the coastal group and one of the

Table I

Anomalies

Latitude

Distance (km)

5-10

52°N

775

48°N

675

46°N

525

41°N

880

10-20

56°N

440

52°N

575

48°N

685

45°N

740

41°N

840

35°N

870

30°N

1570

25-32B

45°N

590

41°N

585

35°N

590

central group is highly irregular. The central anomalies gradually widen to the south; the distances among the western lineations are generally unchanged. In Table I, anomalies 10 and 20 were chosen for the measurements because they have been observed in the northern part of the area shown in Fig. 4, as well as in the area between the Pioneer and Murray fracture zones.

Although there are small internal changes, the overall width of the western lineations is the same even after they bend westward. At the Amlia Fracture Zone, however, the distance between anomalies 25 and 32B has decreased to 460 km. Westward of the Amlia Fracture Zone this distance appears to remain constant.

The large increase in the distance between anomalies 10 and 20 at 32°N is the result of the disturbed zone south of the Murray Fracture Zone that is described by Raff and Mason (1961).

Lineations 22 through 24 are somewhat irregular. As in the central group, the distances separating them increase to the south, but they strike parallel to the western group. These anomalies, therefore, can be considered to form a transitional zone between the central and western patterns. Definition of the exact nature of this transition zone must await further studies.

B. Coastal Pattern

The coastal pattern is the most complex of the three provinces. Part of the area mapped by Mason and Raff (1961) was resurveyed by Lattimore et al.

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN 205

(1968) with a less dense line spacing. The similarity of the results from the two surveys proves that the complex, faulted, magnetic pattern, in fact represents complex tectonic activity in the coastal areas, and is not simply a function of the more detailed coverage as might be expected.

North of the Mendocino Fracture Zone the fault pattern is actually much more complex than can be shown in Fig. 4. There are a large number of faults between Vancouver Island and anomaly 5 along the trends shown here. Numerous small, east-west faults east of the Juan de Fuca Ridge, and northeast- southwest and northwest-southeast offsets in the Gorda Ridge area, were depicted by Pavoni (1966). Most of the faults shown here were also indicated by Raff and Mason (1961) and others.

The dashed arrow that indicates right-lateral motion along the Mendocino Fracture Zone at its eastern end (Fig. 4) represents the eastward movement of the Gorda block (area between the Mendocino and Blanco fracture zones westward limit is approximately 135°W) which caused the separation of the Juan de Fuca and Gorda ridges postulated by Peter and Lattimore (1969). They assumed that the northeast-southwest trending magnetic lineations of this area originally were oriented north-south in conformance with the overall pattern of lineations, and that the Juan de Fuca and Gorda ridges at one time were part of a continuous ridge.

The offsets of anomalies 3 and 3' east of the Juan de Fuca Ridge argue against an original transform-fault relationship along the Blanco Fracture Zone (i.e., original offset of the two ridges) because no comparable ridge crest is present from which anomaly 3' could have originated by spreading (Pavoni, 1966; Peter and Lattimore, 1969). A relative eastward motion of the Gorda block is postulated in preference to an overall westward displacement of the crustal blocks north of the Blanco Fracture Zone. If realignment of the anomaly bands is made with respect to the anomalies of the Gorda block, a number of lineations east of the Juan de Fuca Ridge would fall under the Washington- Oregon coast, with the ridge crest and central anomalies located under Van- couver Island. Unless the continent was farther eastward at that time, these anomalies would have had to emerge from under the continent. If they were under the continent, they probably would have been "erased." This phenom- enon seems to occur today along the margins of the continents.

The coastal anomaly group is not seen between the Mendocino and Pioneer fracture zones. Anomaly 9 [and possibly 8 (not shown)] occurs adjacent to the continental slope.

None of the prominent (numbered) anomalies of the coastal group are present between the Pioneer and Murray fracture zones. The somewhat distorted anomaly 10 of the central group sharply abuts the northeast-southwest trend- ing, short-wavelength lineations that presumably belong to the coastal group. The absence of anomalies 9, 8, and 7 is a curious phenomenon which seems to occur nowhere else in the Northeast Pacific.

The northwest-southeast fault at 35°N and 123°W is quite clear on the magnetic-anomaly map of Mason and Raff (1961); the exact identity of the

206 PETER, ERICKSON, AND GRIM [CHAP. 5

coastal group of lineations is not known (triple line and double line), therefore their offset cannot be determined.

Magnetic expression of the Murray Fracture Zone toward the east ends between anomalies 9 and 7. Data are too scarce to present a good case for offset of the coastal anomalies along the extension of the Murray Fracture Zone. Small, left-lateral offsets inferred within the coastal pattern (Fig. 4), however, seem to align with left-lateral faults on the Channel Islands.

Anomalies 9, 8, and 7 are present south of the Murray Fracture Zone. Unfortunately, available data do not extend to the coastline, so only the edge of the coastal pattern is shown in Fig. 4.

C. Central Pattern

The "central pattern" has been surveyed in detail only in the area between the Pioneer and Murray fracture zones. However, since there are numerous tracklines over this pattern throughout the Northeast Pacific the north-south trend of the magnetic anomalies and the location of the east-west fracture zones (with the exception of the two northern ones) are sufficiently established.

Many of the east-west fracture zones are clearly restricted to the central pattern. Major fracture zones, like the Surveyor, Mendocino, Pioneer, and the Murray, seem to cross the western pattern as well. According to Menard (1967), some of these extend across the greater part of the Pacific basin. Even among these major fracture zones, the Surveyor and the Murray appear to terminate on the east at the eastern edge of the central pattern. The same may hold for the Mendocino and Pioneer fracture zones; this cannot be determined because south of these faults the eastern edge of the central pattern is not reached before the magnetic pattern and the faults reach the continental slope. The east- west fault at 37°N (Bassinger et al., 1969) ends east of anomaly 13, where two north- east-southwest faults seem to offset the magnetic anomalies.

The generally smaller offset of anomaly 7 at the eastern edge of the central pattern and the offsets of anomaly 6 are shown in Fig. 4 as hypothetical northwest-southeast faults. The interpretation of the offsets by these northwest- southeast faults, with the exception of the fault at 49°N and 135°W, is not necessary if differential movements (crustal compression or extension) are postulated at the eastern termination of the east-west faults.

From detailed surveys (Vacquier et al., 1961 ; Lattimore et al., 1968) the east- west fault at 37°N is known to terminate at 127°W against a northeast-south- west fault that, in turn, apparently cuts the crustal block between the Pioneer and Murray fracture zones. Some of the magnetic lineations are clearly offset across the east- west fault; others seem to bend and give the impression of plastic drag (Fig. 13, from Bassinger et al., 1969). Although the sediment cover is only 200 m, there is no topographic expression of this fault (L. A. Weeks, personal communication).

The western end of the east-west fault is not known. The offset of anomaly 21, designated as the westernmost of the central pattern, is generally the same as the rest of the lineations. A further puzzle is that no obvious topographic

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN

Fig. 13. Magnetic total- intensity anomaly map with interpretation of the magnetic offsets. Area is located between the Pioneer and Murray fracture zones (from Bassinger et al., 1969).

evidence exists where the faults either disappear or run into faults of different motions at the edges of the central pattern.

D. Western Pattern

The essential characteristics of the western magnetic pattern are described in the discussion of the magnetic maps for areas A, B, and C of Fig. 1. Thus only- possible modes of origin of the bend in the magnetic lineations [or, as called by Elvers et al. (1967), the "Great Magnetic Bight"] are presented here.

Some of the possible explanations for the existence of the bend in the lineations are the following:

1 . The magnetic lineations, as discrete geological structures within the earth's rigid crust, were straight at one time. Subsequently the crust was broken up and bent westward.

2. The magnetic lineations were straight at one time. When they were bent westward, the crustal material responsible for the lineations behaved like pliable plastic so that crustal break did not occur.

208

PETER, ERICKSON, AND GRIM

[CHAP. 5

3. The magnetic anomalies were formed [as postulated by the Vine and Matthews (1963) hypothesis] along two separate, mid-oceanic ridge axes (one trending northwest-southeast, the other east-west) both of which have been obliterated since their formation.

4. The magnetic anomalies were formed [as postulated by the Vine and Matthews ( 1 963) hypothesis] along an approximately northwest-southeast and an east-west trending, mid-oceanic ridge axis, located along anomaly 32B (Pitman and Hayes, 1 968). As the younger lineations were formed these ridge crests migra- ted northward and eastward, leaving behind the successively younger crustal elements represented by the magnetic lineations north and east of 32B. The two ridge crests disappeared under the Aleutian Arc and the North American Continent.

5. The anomaly lineations represent a global stress or fracture pattern in the crust (possibly intruded by mantle rocks), so that the magnetic pattern (including the bend) formed "in place" (Mason, 1958; Raff and Mason, 1961; Peter, 1965 and 1966; Elvers et al., 1967).

6. The magnetic-anomaly lineations are related to geological entities located in the upper mantle and in the lower part of the oceanic crust. The magnetic bend may have formed as differentiated mantle kept filling a void created by crustal fracture. The shape of the crustal fracture and the direction of the tension that caused the fracture have determined the shape of the bend.

Arguments can be raised against both the plastic (case 2) and the rigid (case 1) behavior of the magnetic lineations. The relative straightness for thousands of kilometers, the usual fracture type offsets [although draglike phenomena are observed in places (Bassinger et al., 1969)], and the small internal fractures within individual blocks seem to support the idea that the anomalies are caused by rigid geological bodies. Yet, as Fig. 14 illustrates, the bend could not have occurred by rotation of two rigid crustal blocks. Part A (Fig. 14) represents a crustal block with two magnetic lineations. Parts B and C demon- strate that if the crust is bent as a rigid block, either crustal opening or crustal compression must occur. In the area of the bend, neither topographic nor magnetic data support such a possibility.

■4— h

(a) (b) (c) (d)

Fig. 14. Development of crustal opening and compression in case of rotation of rigid blocks.

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN 209

Part D shows that overthrust of blocks must occur if the anomalies "spread" at right angles away from two segments of a ridge that forms an angle (case 3). For this case, one may consider the right edge of drawing D as the spreading source; the overlapping part is shown by dashed lines.

Case 5 is unlikely in view of the well demonstrated axial symmetry and global occurrence of the magnetic lineations.

The "migrating ridge" hypothesis (case 4) of Pitman and Hayes (1968) is a possible explanation for the formation of the bend. This, together with the last explanation above (No. 6) is treated in detail in connection with the discussion on the origin of the magnetic lineations.

6. Magnetic Structure Origin of Magnetic Lineations

A. Proposed Hypotheses

A comprehensive summary on the possible geological origin of the magnetic lineations was given by Bullard and Mason (1963) in Volume 3 of The Sea. Some of their observations have a direct bearing on the origin of the magnetic lineation pattern and are shown in Table II.

Table II

1. There is no correlation between bottom topography and magnetic lineations.

2. There is no difference in seismic velocities between areas of positive and negative lineations.

3. Oceanic crust appears to be rigid; there are large displacements without distortion of the lineations.

4. Orthogonal relationship between the magnetic lineations and major fracture zones may indicate common origin.

5. Anomaly sharpness indicates that the upper surface of magnetic body is not deeper than 1 km below sea floor.

6. Pattern disappears below continents; anomalies erased by combined effect of tempera- ture and pressure.

7. Fracture zones are younger than the magnetic pattern.

Bullard and Mason (1963) listed three possible explanations for the origin of the lineations: (a) isolated magnetic bodies (such as lava flows) within the second layer; (b) elevated folds or fault blocks in the main crustal layer; and (c) zones of intrusion of mantle material.

The most commonly accepted explanation for the origin of the lineations is the Vine and Matthews (1963) hypothesis which is a corollary to the sea-floor spreading concept of Hess (1962, 1965) and Dietz (1961). According to this hypothesis, at the axis of the mid-oceanic ridges the crust is broken apart by convection currents and the basaltic material that fills the break acquires a magnetization in the direction of the existing magnetic field of the earth as it cools through the Curie point. As the earth's magnetic field periodically reverses

210 PETER, ERICKSON, AND GRIM [CHAP. 5

polarity (Cox et al., 1964), a sequence of normally and reversely magnetized rocks, symmetrical about the ridge axis, comes into existence and slowly spreads away from the ridge crest.

As another corollary of the sea-floor spreading hypothesis, Wilson (1965[a], 1965[b]) suggested that offsets of mid-oceanic ridges do not represent actual displacements, but that the opening in the crust (along which the mid-oceanic ridges and magnetic lineations subsequently formed) was offset originally. He postulated that, as the sea floor spreads away from the ridge crests, the motion along the planes which connect the offset portion of the ridge crests is actually opposite in direction to that which would be indicated by strike-slip faulting. He called this motion transform faulting and used it to explain both the earth- quake activity concentrated along the planes which join the offset ridge crests, and the relative absence of earthquakes along the extensions of the faults that lie beyond the ridges that they join.

B. Sea- floor Spreading

Some of the data in direct support of the original sea-floor spreading and transform -fault concepts are listed in Table III; data opposed to these hypoth- eses are summarized in Table IV. Comparison of these two tables indicates

Table III

1. Magnetic lineations are generally parallel to mid-oceanic ridges.

2. Magnetic lineations are symmetrical about the axis of mid-ocean ridges.

3. The same spectrum of lineations and axial symmetry is present in association with all tectonically active mid-oceanic ridges.

4. The sequence of positive and negative lineations which extend from the ridge-axis to a distance approximately 160 km, agrees with the sequence of normal and reverse polarities of the earth's magnetic field in the past fovir million years. (Measured on dated volcanic rocks on land and on deep-sea sediment cores.)

5. Earthquake mechanism studies corroborate the motion required by transform faulting.

6. The age of sediments (based on available samples) indicates general increase from the ridge crest to the flanks.

that an important part of the facts that argue against sea-floor spreading are based on sediment structure and distribution, and on sea-floor topography. If the main source of the magnetic lineations lies within a 1- or 2 -km thick basaltic layer which overlies the main " serpentinite " crustal layer (Vine and Wilson, 1965; Vine, 1966), offsets of the magnetic pattern, of either the transcurrent or transform kind, should be reflected in the sediment structure. In the Northeast Pacific, where the sediment overlying the second layer is relatively thin [145-680 m thick according to Hamilton (1967)] these offsets should be indicated on the sea floor.

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN 211

Table IV

1. Over 1 km of undisturbed, horizontally bedded sediments were found in the trough of the Vema Fracture Zone which is considered to be an active transform fault.

2. Numerous magnetic offsets, some "dated" by the magnetic time scale as less than two million years old, show no disturbance of either sea-floor topography or sub-buttom sediments.

3. Most trenches studied are either unfilled or filled with undisturbed sediments.

4. The topography and petrology of the upper flanks of the ridges are of a different origin from those of the ridge-crest.

5. Magnetic lineations cross morphologic province boundaries without ajjparent change in character.

6. Magnetic anomalies over the ridge-crests differ in amplitude and wavelength from those over the flanks.

7. The magnetic structure of the Northeast Pacific indicates three phases of tectonic activity.

8. Most faults of the Northeast Pacific do not meet the definition of transform faults.

If the offsets either preceded the sediment deposition or started very recently the above arguments are not necessarily valid . However, according to Vine ( 1 966 ) , motion along the offsets (such as transform faults) has been uniform since the Cretaceous. Based on this assumption, a geomagnetic time scale has been proposed in which anomaly 32B is "dated" as 72 million years old (Vine, 1966, Heirtzler et al., 1968).

East of the Juan de Fuca Ridge a northeast-southwest strike-slip fault offsets a group of magnetic-anomaly lineations by 100 km (Fig. 4). According to the geomagnetic time scale, the youngest lineation offset (anomaly 3) is two million years old, therefore a 5 cm/yr motion is required along the fault during Late Pliocene and Pleistocene (Peter and Lattimore, 1968). Seismic-reflection studies of this area indicated no sediment disturbance in the area of this fault (Hamilton and Menard, 1968).

On the basis of these arguments it appears that the "marine" geomagnetic time scale is questionable, and/or the magnetic lineations are likely to originate below the second layer so that their offset is not necessarily reflected in the upper part of the crustal column.

Near the axis of mid-oceanic ridges the geomagnetic time scale is supported by a number of observations (Table III), therefore its validity may be accepted within the "coastal pattern." A pause in sea-floor spreading, and consequently a rejection of the time scale outside the area of the ridge crests ("coastal pattern' j, was suggested by E\, ing and Ewing (1967) on the basis of the abrupt increase m sediment thickness at the edge of the ridge crests. The three different patterns in the magnetic structure (Fig. 4) strongly support the idea of three separate episodes of tectonic activity, and since the length of the pauses cannot be determined, the extrapolation of the geomagnetic time scale outside the crestal area of mid-oceanic ridges is not justified.

212 PETER, ERICKSON, AND GRIM [CHAP. 5

The suggestion that the magnetic anomalies originate below the second layer is contrary to the conclusion reached by Bullard and Mason (1963) who state that the upper surface of the magnetic bodies should be no deeper than 1 km below the sea floor. Additionally, deep-towed magnetometer data indicate large-amplitude, short-wavelength anomalies near the sea floor (Mudie and Harrison. 1067; Spiess et al.. 1968; and Spiess and Mudie, Part I, Chapter 7). In order to satisfy all observations it is suggested that small intrusives (dikes) in the second layer could be responsible for the short-wavelength, large amplitude anomalies, and that the major bodies (as possible sources of these intrusives) may lie deeper.

The existence of a magnetically quiet zone at continental margins and trenches may be interpreted as support of this suggestion. Model computations, like those reported by Hayes and Heirtzler (1968), indicate that if the magnet- ized bodies are part of the second layer, the down-bow of the crust indicated by seismic data at the Aleutian Islands is not sufficient to account for the abrupt elimination of the anomalies over the Aleutian Trench. If, however, the magnetic bodies lie in the lower part of the crust or in the upper mantle as suggested here, the 3-6-km crustal down- warp may be sufficient to either carry the temperature of the magnetic bodies above the Curie point or cause sufficient metamorphism that their magnetization is erased (Bullard and Mason, 1963; Table II).

The crossing of the magnetic lineations over major morphologic provinces without a change in character, the apparent "drag" effect on certain lineations (mapped across fault A in Fig. 13), the relatively young offset of the magnetic lineations east of the Juan de Fuca Ridge without deformation of sediments, the irregular junction of the "central pattern" with the neighboring magnetic patterns (Fig. 4), and the abrupt termination of large east- west faults without sub-bottom or bottom topographic expression all support the prob- ability of a deeper source of the magnetic lineations whereby the magnetic offsets do not necessarily indicate the offset of the entire crustal column. This interpretation suggests that in certain cases small offsets of the deeper magnetic layer can be compensated for within the overlying crustal layers in such a manner that noticeable offsets do not necessarily occur near the top of the second layer. The combination of offsets and drags of the lineations across fault A in Fig. 13 may be the result of the interaction between the deeper crustal layers that represent the proposed compensation.

Seismic refraction measurements in the Northeast Pacific (Shor, 1962; Shor et al., 1968) indicate normal oceanic crust in the areas of the "central" and "western" magnetic patterns; over the Gorda and Juan de Fuca ridges (i.e., over the "coastal pattern") the crustal velocity is slightly higher, the mantle velocity is below normal, and the ridges appear to represent the surface expression of the upraised crust and mantle. Shor et al. (1968) concluded that the structure of the Juan de Fuca and Gorda ridges is the same as that of the East Pacific Rise. Gravity anomalies over oceanic ridges [summarized by Worzel (1965)] further reflect unique crustal structure. As Heirtzler and Le

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN 213

Pichon (1965) noted, short-wavelength magnetic anomalies seem to be associ- ated with the anomalous-mantle zone in the area of the ridge crests. It can be concluded, therefore, that the "coastal pattern" in the Northeast Pacific is associated with the anomalous crustal structure, and that it alone represents segments of the present East Pacific Rise.

Although uplifted by the present East Pacific Rise, the normal oceanic crust to the west does not appear to be a part of it structurally (Fig. 4). Both reference to the areas of the central and western magnetic patterns as "ridge flank," and the extension of the East Pacific Rise to the edge of all lineations (anomaly 32B) as proposed by many investigators, are unwarranted. It is suggested that the change of the magnetic lineations from broad, even- amplitude anomalies to short-wavelength anomalies at the edge of the "coastal pattern," is related to a change in crustal structure, rather than to more frequent reversals of the earth's field alone as Vine (1966) proposed.

A modification of the sea-floor spreading hypothesis, namely, the possibility that the ridge crest itself migrates, was raised by Pitman and Hayes (1968). These authors proposed that a Y-shaped junction of ridge crests initially existed southwest of the present bend in the anomaly lineations. Convection currents that upwelled along this junction carried the ridge crests along with them (northward and eastward) until the convection pattern was "stifled" by the Aleutian Trench. If the corollary assumptions of this hy- pothesis are valid, a simplified magnetic pattern (Pitman and Hayes, 1968; Fig. 4) may be explained. Modifications are necessary, however, to incorporate the detail shown in Fig. 4.

Morgan (1968) suggested that the earth's surface is broken up into large rigid blocks bounded by rises, trenches, or faults, and that these blocks rotate about each other with respect to several "poles." The mid-oceanic rises are not associated with deep-seated convection currents, but instead represent new crust created where two blocks separate. Dikes a few kilometers in width and, perhaps 100 km deep are formed in this way and magnetized according to the existing polarity of the earth's field. With continued tension, the dikes are split down the middle, new material is injected, and a symmetrical pattern of magnetic anomalies is created. Although Morgan's (1968) hypothesis may not account for all the detail of the magnetic structure derived here for the North- east Pacific, his suggestion that the ridge crests are independent of the location of the convection cell is a significant departure from the original sea-floor spreading hypothesis.

C. Transform faults

Beyond question, many of the faults in the "coastal pattern" are not trans- form faults; many make a small angle with the ridge crests and some are bounded by other faults. Especially in the area of the Juan de Fuca Ridge, fault patterns are clearly incompatible with the concept of transform-faulting (see Morgan, 1968, Fig. 2). By definition, a transform fault must cross all magnetic lineations; none of the faults in the "coastal pattern" and only a few

214 PETER, ERICKSON, AND GRIM [CHAP. 5

in the "central pattern" meet this criterion. The Murray and Surveyor fracture zones clearly stop near the eastern edge of the "central pattern"; the other east-west faults of the "central pattern" do not extend into the westernmost lineations. The Pioneer and Mendocino fracture zones appear to cross the "western" and "central" patterns but terminate near the continental margin before the "coastal pattern" develops. The proposition that the Mendocino and Murray fracture zones may be transform faults (Wilson, 1965[a]; Vine, 1966) is also open to question on the basis of their linear extent across the entire Pacific basin (Menard, 11)67).

If transform faults (cutting all three magnetic patterns) did exist in the area of Fig. 4, the "coastal pattern" could have evolved into the "central pattern" and this, in turn, into the "western pattern" through lateral spread- ing. The bend in the "western pattern," the development of extra lineations in part of the east-west segment of the "western pattern," and the fact that the "central pattern" does not bend, together with the arguments derived earlier, require modification of the sea-floor spreading hypothesis and its twro corollaries —the Vine and Matthews (1963) and the transform-fault hypotheses (Wilson, 1965[a], 1965[b]) in their application to the East Pacific area. Present-day, transform -fan It motions (Sykes, 1967) do not necessarily prove that the ridge crests were originally offset. Once the offset has taken place (e.g., by transcurrent faulting) active growth of the individual ridges would produce relative motion along the fault plane connecting the ridge crests that is in accord with transform-fault motion.

D. Interpretation

In previous portions of this paper, it is suggested that the main source of the magnetic lineations may lie below the second layer. It has been demon- strated that because of the absence of the required overlap of lineations the bend in the magnetic anomaly bands could not have originated by crustal spreading from two stationary ridge crests. The characteristic internal fault system of the three magnetic patterns could not be derived from one another through simple lateral spreading, and it has been suggested that the three patterns probably are associated with three episodes of tectonic activity. The interpretation of the genesis of the lineations and their offset pattern must combine these deductions with the world-wide occurrence of the magnetic lineations in association with mid-oceanic ridges, and their general symmetry with respect to the ridge crests.

These latter observations suggest that there is a definite relationship between the magnetic lineations and the ridges. Two reasonable explanations may be offered for the axial symmetry of the magnetic anomaly bands: (a) an "active" system of intrusives at the ridge crest that forces the crust aside [Vine and Wilson (1965) suggest that this takes place in the second layer]; and (b) a "passive" system of intrusives that are simply filling a void created by the opening of the crust. In the first explanation the ridge crest is directly tied to the up welling and dynamic motion of the convection currents. The second

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN

215

explanation is based on crustal tension alone, that is, there is no restriction on the mechanism that may cause the crustal tension. Among possible mechanisms are polar shift, earth-expansion, and the suggestion of Morgan (1968) that tension is produced by rotation of large crustal blocks.

Since the existence of the bend in the "western pattern" demands that the lineations cannot be pushed aside by subsequently formed younger lineations (Fig. 14d), the ridge crest is considered here not as a dynamic, moving part of the oceanic crust but as a passive part formed as the result of crustal tension. The mid-oceanic ridges are seen as "scars" in the earth's crust. The anomalous mantle and crustal structure below the ridge crest is believed to be caused by differentiation and volcanic processes occurring in response to the fracturing of the crust. It is only in the sense of "cause and effect" that the proposed "passive ridge-crest" hypothesis is different from the process of crustal generation described by Hess (1965).

If the earth's crust as a whole is under tension (earth-expansion), fracturing of the crust, differentiation processes in the upper mantle, and the filling of the void created by fracturing with differentiated mantle rocks and volcanics could account for both the existence of mid-oceanic ridges and the axial symmetry of the magnetic lineations. Figure 15b illustrates the formation of the magnetic bend according to this hypothesis: as the crust on the two sides of the fracture is pulled apart, differentiated mantle material fills the gap and becomes "welded" to the crust. Continued tension breaks this "dike" in the center where it is hottest and may be only partially solidified at depth (Morgan, 1968). With further tension, under the influence of a periodically reversing magnetic field (Vine and Matthews, 1963), magnetic lineations could be formed symmetrically about the center of the crustal break.1

/

v////////////////////////////,

fa)

(b)

(c)

Fig. 15. Development of Y-shaped ridge junction, magnetic bend, and ridge offset through crustal tension.

1 Symmetrical lineations can be produced not only by normally and reversely magnetized blocks, but also by nonmagnetic blocks intermixed with magnetized blocks in the formation cycle. This may be an especially attractive assumption for the older lineations.

216 PETER, ERICKSON, AND GRIM [CHAP. 5

If, in Fig. 15b, one side of the fracture is stationary and only the other side is being pulled away, the appearance is that of a "migrating ridge" such as described by Pitman and Hayes (1068) and Morgan (1968). Crustal tension in three directions (or in two directions away from a stationary block) is shown in Fig. 15a; this case is applicable to the Y-shaped ridge junction reported near the Galapagos Islands by Herron and Heirtzler (1067) and Raff (1068).

It should be noted that with a "passive" ridge crest the problem of lateral compression seen in connection with spreading (Fig. 14d) does not exist since the lineations are not spreading away from a ridge crest; they are "welded" to the lower crust and upper mantle, which are under tension and pulling apart. Thus the lineations, together with the receding crust, are moving away from the center of the ridge and give the impression of a spreading ridge. Both "active" and "passive" ridge crest hypotheses imply that the lineations are progressively older away from the center of the ridge crest.

Figure 15c illustrates how crustal tension can cause the "transform-fault" motion between the offset portions of ridge crests that Sykes (1067) noted.

Application of the observations in the preceding paragraphs to the specific case of the Northeast Pacific suggests that the "western pattern" is related to an early phase of tectonic activity, that is, to a predecessor of the East Pacific Rise. During this period, the inferred crustal opening probably followed the tectonic grain of the North American Cordillera with its westward bend in Alaska (Fig. 15b). Development of the "western pattern" was followed by a pause in the tectonic activity; during this time the opening healed over com- pletely. Renewed crustal tension, probably with a predominant east-west component, may have been manifested in a crustal break along a "zig-zag" pattern (Fig. 15c). The intrusives represented by the anomalies of the "central pattern" would have formed in north-south openings in the crust. These openings may have been connected by east-west planes of dislocation that could be described as transform faults. During the second period of quiescence, these fractures healed over so that with renewal of east-west tensional forces the crust yielded along a slightly different pattern. The present East Pacific Rise is related to this last phase of tectonic activity. The pattern, which probably originally conformed to the north-south orientation of the "central pattern," apparently was broken up by northeast-southwest and northwest-southeast fractures subsequent to its formation. If the inferences of McManus (1065) and Peter and Lattimore (1060) are assumed, this breaking-up occurs as the result of the Late Tertiary to Recent coastal orogeny.

The deep source of the magnetic lineations postulated in this paper permits some faulting of the magnetic lineations without the disruption of bottom topography or the sedimentary section. Thus the occurrence of undisturbed sediments east of the Juan de Fuca Ridge that Hamilton and Menard (1068) reported does not present a contradiction to the proposed interpretation. The passive ridge hypothesis, coupled with earth-expansion, is especially attractive when one considers the undisturbed sediments and the lack of obvious com- pressional phenomena on the ocean floor at the continental margins.

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN 217

7. Magnetic Structure Origin of Aleutian Trench

A. Proposed Hypotheses

In this section the previously derived interpretation is applied to the problems of the origin of the Aleutian Trench as seen from the point of view of the two major hypotheses: the tensional- and compressional-origin hypotheses.

The hypotheses are not reviewed in detail. A comprehensive treatise on the tensional hypothesis was given by Worzel (1965); a summary of data on trenches with emphasis on their compressional, convection-current origin was given by Fisher and Hess (1963).

According to the tensional hypothesis, the trenches are considered to be down-faulted parts of the oceanic crust. The negative, isostatic anomalies that characterize the trench areas are explained in terms of mutual interaction of the island arc, trench, and outer-ridge systems. Shor (1965) suggested that the Aleutian Trench formed as a direct result of the loading of the island arc on the oceanic crust; the isostatic imbalance of the trench is attributed to the elastic behavior of the oceanic crust.

The argument for the compressional origin is also based on the negative isostatic anomalies associated with the trenches. According to this theory, static-mass imbalances in the area of the trench should be compensated for in a relatively short time; since the negative isostatic anomalies indicate that this has not occurred it is presumed that a dynamic force, such as compression caused by convection currents or drag induced by them, is preventing the trench from adjusting to isostatic equilibrium.

B. Interpretation

The mechanical conditions that might be expected to exist if the oceanic crust is moving under a curved trench driven by convection currents have been illustrated by Fisher and Hess (1963; Fig. 16). Geological structural trends similar to f-f, illustrated in Fig. 16, should conform to the arcuate shape of the trench on both sides. The east-west trends of the magnetic-anomaly lineations in the vicinity of the Aleutian Trench are in sharp conflict with these logical expectations. The apparent north-south (as opposed to radial) trend of the fracture zones associated with the Aleutian Trench further implies structural independence.

Data collected in the area of the Aleutian Trench indicate that (a) traces of some magnetic lineations extend over the Aleutian Terrace; (b) those lineations that intersect the trench east of the Amlia Fracture Zone have reduced amplitudes west of the fracture zone; and (c) the fracture zones have no obvious topographic expression in the trench floor, but they may be related to changes in trend on the Aleutian Ridge.

If it is assumed that the sea floor is rigid and that it has been carried deep below the trench and island arc by a descending convection current, vestiges of the lineations and general, weak east-west trends of the anomalies

218

PETER, ERICKSON, AND GRIM

[CHAP. 5

Fig. 16. Postulated mechanical situation in which the crust moves into a curved trench (from Fisher and Hess, 1963).

should not exist over the Aleutian Terrace; instead, the anomaly trends either should follow the curvature of the island arc or should not be seen at all.

The fact that anomalies 25 through 28 (the only ones that intersect the trench east of the Amlia Fracture Zone) are much reduced in amplitude west of the fracture strongly suggests that the reduction in amplitude is related to the trench formation. If the island arc and trench were superimposed on an exist- ing, unfaulted magnetic pattern, then such loading might depress the lower part of the crust below the Curie point isotherm, or to such a temperature that metamorphism would cause alteration of mineralogy. In this manner part of the magnetization could have been erased. Before complete suppression of the anomalies took place, transcurrent faulting could have carried the crust away from the influence of the island arc, thus preserving the lineations in their diminished form. If, on the other hand, the Amlia Fracture Zone is assumed to be a transform fault and the only movement of the sea floor was northward, there is no explanation for the uniformly reduced amplitude of that particular group of anomalies.

Northward movement of the sea floor would also require that the sea-floor topography of the outer ridge be carried into the trench; the drift of guyots into the Aleutian Trench has been proposed by Menard and Dietz (1951), and the drift of guyots from the Darwin Rise to the Gulf of Alaska by Hess (1965).

THE ALEUTIAN TRENCH AND NORTHEAST PACIFIC BASIN 219

Yet, the high relief of the outer ridge does not continue onto the south wall of the Aleutian Trench.

If the structures that cause the magnetic anomaly lineations lie mainly in the lower part of the crust and upper mantle, the relatively "quiet" magnetic zone of the trenches and continental margins is to be expected because crustal down-bow may be sufficient to carry the lower crust-upper mantle into such temperatures that its magnetization is erased.

Vine (1966) and others suggested that the fracture pattern off the Washington- Oregon coast is the result of the westward drift of the North American con- tinent and the change in the direction of sea-floor spreading during the Pliocene. It was further assumed that as a result of this new direction of spreading the crust of the entire North Pacific ocean has been moving northwestward, and causing the formation of the Aleutian Trench. Recent studies of earthquake first motions by Isacks et al. (1968) support this interpretation, and together with the distribution of sediments in the North Pacific (Ewing et al., 1968), imply that the Aleutian Trench may be as young as Late Tertiary.

If the Aleutian Trench is Tertiary or younger, and the western half of the Aleutian Arc is dominated by strike-slip faulting (Isacks et al., 1968), then the existence of a well-developed trench along the western half of the arc may be questioned because no appreciable underthrusting could have taken place in the last ten million years.

Pitman and Hayes (1968) have proposed that the Aleutian Trench was formed by the underthrusting of a northward moving sea floor which ended in the Paleocene; Ewing and Ewing (1967) suggested that there was a 10-million- year pause before the renewal of sea-floor spreading in the Pliocene. These suggestions raise the question of whether or not the elapsed time before the latest phase of spreading would have been sufficient for isostatic rebound of the trench, if the cause of trench formation is underthrusting.

Whether there has been an "early" trench or not, however, the north- westward motion of the sea-floor in the last 10 million years should have created measurable differences in the development of the two halves of the Aleutian Trench.

These considerations, together with the magnetic structure of the Aleutian Arc and the Northeast Pacific, complement our earlier conclusions and suggest that the Aleutian Trench has been formed as the result of crustal downfault or down-bow rather than underthrust of the ocean floor.

Acknowledgments

The U.S. Coast and Geodetic Survey ships Pioneer and Surveyor collected the systematic SEAMAP data. For additional data and manuscripts not published at the time of writing this paper, we are indebted to R. H. Higgs, U.S. Naval Oceanographic Office, and W. C. Pitman, III, D. E. Hayes, and J. I. Ewing, Lamont-Doherty Geological Observatory. Several colleagues, es- pecially O. E. DeWald and the late A. B. McCollum deserve credit for their help in working on SEAMAP data.

220 PETER, ERICKSON, AND GRIM [CHAP. 5

We are grateful to R. K. Lattimore and H. B. Stewart, Jr. for many helpful discussions and critical review of the manuscript.

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(abstract). Trans. Amer. Geophys. Un., 46, 196. Shor, G. G., P. Dehlinger, H. K. Kirk, and W. S. French, 1968. Seismic refraction studies

off Oregon and northern California. J. Geophys. Res., 73, 2175-2194. Spiess, F. N., B. P. Luyendyk, and J. D. Mudie, 1968. Geological observations of abyssal

hills using a deeply towed instrument package (abstract). Trans. Amer. Geophys.

Un., 49, 213-214. Sykes, L. R., 1967. Mechanism of earthquakes and nature of faulting on the mid-oceanic

ridges. J. Geophys. Res., 72, 2131-2153. Talwani, M., C. Windisch, and M. Langseth, 1968. Recent geophysical studies on the

Reykjanes Ridge (abstract). Trans. Amer. Geophys. Un., 49, 201. Vacquier, V., A. D. Raff, and R. E. Warren, 1961. Horizontal displacement in the floor

of the Pacific Ocean. Bull. Geol. Soc. Amer., 72, 1267-1270. van Andel, Tj. H., J. B. Corliss, and V. T. Bowen, 1967. The intersection between the Mid- Atlantic Ridge and the Vema fracture zone in the North Atlantic. J. Marine Res.,

25, 343-351. van Andel, Tj. H., and C. O. Bowin, 1968. Mid-Atlantic ridge between 22° and 23° North

latitude and the tectonics of mid-ocean rises. J. Geophys. Res., 73, 1279-1298. Vine, F. J., 1966. Spreading of the ocean floor: New evidence. Science, 154, 1405-1415. Vine, F. J., and D. H. Matthews, 1963. Magnetic anomalies over oceanic ridges. Nature,

199, 947-949. Vine, F. J., and J. T. Wilson, 1965. Magnetic anomalies over a young oceanic ridge off

Vancouver Island. Science, 150, 485-489. Wilson, J. T., 1965[a]. A new class of faults and their bearing on continental drift. Nature,

207, 343-345. Wilson, J. T., 1965[b]. Transform faults, oceanic ridges, and magnetic anomalies southwest

of Vancouver Island. Science, 150, 482-485. Worzel, J. L., 1965. Deep structure of coastal margins and mid-oceanic ridges. Colston

Papers, 17, 335-359.

61

Reprinted from Deep-Sea Research 18_, 321-327.

Bathymetry off central northwest Africa*

Peter A. RoNAf

{Received 13 July, 1970; revised and accepted 3 September 1970)

Abstract A preliminary bathymetric chart of an area about 106 km2 extending from Cap Blanc, Mauritania, to the abyssal hills near 30°W, was constructed from about 8000 km of sounding tracks recorded by the USNS Gibbs in 1968 plus other earlier soundings. Major unnamed U-shaped sub- marine canyons attain widths of 85 km and a relief of 700 m where they cross the continental slope and upper continental rise between 20° and 25°N; narrow V-shaped canyons attain widths of 10 km and a relief of 300 m between 18° and 20°N.

Comparison of bottom morphology with patterns of atmospheric and oceanic circulation suggests that wind transport of sediment derived from North Africa is a major process in shaping the Cape Verde Plateau.

INTRODUCTION

About 8000 km of sounding tracks recorded by the USNS /. W. Gibbs in 1968 were combined with earlier soundings to construct a preliminary bathymetric chart which delineates the northern edge of the Cape Verde Plateau, major submarine canyons, and specific topographic features between the continental shelf and the abyssal hills near 30°W (Fig. 1). Previous bathymetric charts, based on a low density of sounding tracks, outline an unusually wide continental rise off central northwest Africa con- tiguous with the Cape Verde Plateau (Fig. 2) (U.S.N. Oceanographic Office, 1952, 1961; International Hydrographic Bureau, 1958; Heezen and Tharp, 1968).

Navigation on the Gibbs was performed by Omega with an estimated positional accuracy of ± 5 nm (Zuccaro and Rona, 1968). Soundings were made with a 12 kHz 60° full beam width Edo UQN sonar transducer and recorded on a Raytheon 192 Precision Fathometer Recorder.

submarine canyons

Submarine canyons of major dimensions, either absent or less completely shown on prior charts, occur on the continental slope and upper continental rise between 18° and 26°N (Fig. 1). Seismic reflection profile A-A' parallel with the lower con- tinental slope (Fig. 3) records U-shaped canyons with axes at 180, 225, 350 and 470 km which range in shoulder-to-shoulder width between 35 and 85 km and in floor-to- shoulder relief between about 350 and 780 m (Table 1). Each is underlain by a succes- sion of buried troughs to at least 1-5 km (1*5 sec) acoustic penetration. These are directly below the canyon axis at 470 km and are offset 10-20 km south of the axes at 225, and 340 km. The sediment-water interface of the intercanyon areas (divides

♦The field work was supported by the Office of Naval Research under Contract Nonr-266 (84). Reproduction in whole or in part is permitted for any purpose of the United States Government.

tNOAA Atlantic Oceanographic and Meteorological Laboratories, 901 South Miami Avenue, Miami, Florida 33130.

321

322

Peter A. Ron a

30° W

20°W

-|0°N

Fig. 2. Regional bathymetric chart showing the relation of the area in Fig. 1 (outlined) to the Cape Verde Plateau (U.S.N. Oceanographic Office, 1961 ; Dietz et al., 1969). Directions of ocean surface currents (arrows) and a current velocity contour (< 25 cm/sec) (U.S.N. Oceano- graphic Office, 1965, Figs. 1-5) are indicated. Envelopes are shown of most frequent dust fall occurrence (ship) (after Folger, 1970, Fig. 1) and of a dust storm photographed by ESSA 5 satellite on 7 June, 1967 (satellite) (Prospero et al., 1970, Figs. 3 and 4). The locations of sedi- ment cores (A153-158, A180-47, V17-158) (Ericson et al, 1961) and of an atmospheric dust sample collected aboard H.M.S. Vidal on 17 January, 1965 are also shown (Folger, 1970).

Table 1 . Submarine canyons which cross the continental slope off Cap Blanc, Mauri- tania measured from precision echo-sounding records made with a 12 kHz 60° total

beam width sonar transducer.

Canyon shoulder-to-

Maximum

shoulder distances

Width

Width

Depth N.

Depth S.

Depth

floor-to-

along profile A- A'

shoulders

floor

shoulder

shoulder

floor

shoulder

(Fig. 3) (km)

(km)

(km)

(m)

(m)

(m)

relief {m)

144-145

1

0-5

2200

2190

2225

35

145-205

60

15

2190

1770

2550

780

206-208

2

0-5

1790

1765

1915

150

210-245

35

10

1750

1775

2100

350

230-232

2

1

2120

2100

2210

110

265-305

40

5

1710

1885

1950

240

305-385

80

25

1885

1855

2550

695

390-425

35

10

1860

1605

2020

415

425-510

85

25

1605

1720

2290

685

470-473

3

0-5

2240

2230

2350

120

520-523

3

2

1815

1790

1900

110

531-534

3

1

1885

1900

2050

165

538-540

2

1

1945

1945

2160

215

541-542

1

0-5

1980

1940

2140

200

556-566

10

9

1805

1810

1875

70

582-585

3

1

1805

1825

1990

185

604-611

7

1

1765

1875

2065

300

622-623

1

0-5

1935

1950

2080

145

628-630

2

1

1925

1960

2070

145

649-5-6500

0-5

0-25

1960

1920

2080

160

651-652

1

0-5

1935

1960

2060

125

Bathymetry off central northwest Africa

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Peter A. Rona

between canyons including walls) are convex-up and are generally underlain by sub-parallel convex-up strata. Smaller narrow V-shaped canyons are situated on the crests of intercanyon areas at 145 and 207 km and are nearly centered within U-shaped canyons at 231 and 471 km. A succession of narrow (< 10 km wide), steep-walled, roughly V-shaped canyons with flat floors is present off Cap Timiris between 510 and 630 km.

SEAMOUNTS

Major seamounts known off Cap Blanc are Echo Bank and Papp Seamount based on soundings and nomenclature of the British National Institute of Oceano- graphy (International Hydrographic Bureau, 1968) and Tropical Bank (Inter- national Hydrographic Bureau, 1958) contoured from Gibbs sounding tracks (Fig. 1). Tropical Bank consists of two distinct peaks at nearly equivalent depths aligned NW-SE with a common base deeper than about 2000 m below sea level, rather than a single peak as previously shown (U.S.N. Hydrographic Office, 1952). The 9-km wide summit of the southeastern peak* is nearly flat with local protuber- ances, possibly coral, which rise up to about 25 m above the 999-m summit (Fig. 4). This is less than the previous minimum depths of 1696 m (U.S.N. Hydrographic Office, 1952) and 1055 m (Internationa.. Hydrographic Bureau, 1958). A bench about 0-5 km wide indents the northeast side at about 1050 m below sea level.

NE OKM

Fig. 4. Minimum depth bathymetric profile across the summit of Carmenchu Peak on Tropical Bank. A bench faces northeast at about 1050 m below sea level. Vertical exaggeration is

about 20 : 1.

DISCUSSION

Knowledge of geological processes considered important in the shaping of the more thoroughly investigated continental margin off eastern North America is helpful in the interpretation of the morphology on the northwest African continental margin. Submarine canyons on the continental slope off Cape Hatteras are inferred

*I propose to name this southeastern summit of Tropical Bank ' Carmenchu Peak ', in honor of Me. del Carmen Piernavieja y Oramas of Las Palmas, Canary Islands, Spain.

Bathymetry off central northwest Africa 325

to have developed by depositional upbuilding of the walls (intercanyon areas), while the channels were maintained over sites of original incision by sediment transport processes (Rona, 1970). Some of the original incisions off Cap Blanc appear to have been structurally controlled at the intersections of oceanic fracture zones with the continental margin (Rona, 1969). As off Cape Hatteras, the canyons off Cap Blanc are underlain by buried troughs and the intercanyon areas by convex-up strata sub-parallel with the sediment-water interface. The similarity in the formations implies that similar processes have been active in the development of canyons on the continental slopes on both sides of the Atlantic. The scale differs, the canyons on the continental slope off Cap Blanc attaining about twice the relief and several times the width of those off Cape Hatteras (Table 1 ; Rona et al, 1967). As canyon relief is inferred to be constructural, the differences in relief indicate that higher rates of sediment accumulation have prevailed off Cap Blanc.

The Cape Verde Plateau forms a roughly triangular salient encompassing the Cape Verde archipelago with base extending along the continental shelf from about 12° to 22°N and apex reflected as far as 1000 km seaward to the 4575-m isobath (Figs. 1 and 2). Continental rise isobaths inflect around the northern and southern flanks of the Cape Verde Plateau delineating a broad central ridge between Cap Blanc and Dakar which converges toward the Cape Verde Islands. Seismic reflection profiles reveal sediment in excess of 2 km (2 sec) with the acoustic character of stratified lutite (silt and clay size) beneath this ridge (Fig. 3 ; Lowrie and Escowitz, 1969, Kane 9 D,E,F). The smoothness of the residual magnetic field along the continental slope (Fig. 3) also indicates the presence of a thick sedimentary column. The 700-m relief of Cayar Canyon where it crosses the continental slope off Dakar (Fig. 2) (Dietz et al, 1968) is comparable to that of canyons off Cap Blanc (Table 1), suggesting that relatively high rates of sediment accumulation have affected the entire landward margin of the Cape Verde Plateau. Post-glacial rates of accumulation of lutite cored from the wall of Cayar Canyon are 20 cm/ 1 000 y (Ericson et al, 1961, core A 180-47, Table 5).

Wind-borne dust has frequently been observed off northwest Africa from sea- level to several kilometers above sea-level by ships (Folger, 1970), aircraft (Prospero and Carlson, 1970), and satellites (Prospero et a/., 1970). A striking spatial cor- relation exists between the shapes and areas of the envelope of most frequent dust falls and the Cape Verde Plateau (Fig. 2). This correlation suggests a possible genetic relation between the pattern and volume of eolian sediment transport and sediment deposition on the Cape Verde Plateau. On the basis of similarities of composition, texture, and consideration of air parcel trajectories of the prevailing trade winds, silt and clay-sized material has been traced from North African soils to the dust envelope off northwest Africa (Folger, 1970; Prospero et al, 1970), to surface sea water samples (Folger, 1970), and finally to deep-sea sediments (Folger, 1970). The ratios of clay minerals measured in tops of sediment cores from the Cape Verde Plateau (Biscaye, 1965, cores A153-158, V17-158) are similar to those collected from the adjacent atmosphere (Fig. 2) (Folger, 1970, Fig. 9, Table 3). Cores recovered from the Cape Verde Plateau contain lutite (Ericson et al, 1961, A180-51, 53, 56) with the exception of those from the floor of Cayar Canyon which contain sand (A180-49, 50), probably derived from the adjacent shelf where sand predominates (McMaster and Lachance, 1968).

326 Peter A. Rona

Oceanographic conditions immediately underlying the dust envelope favor the persistence of the fallout pattern as particles settle from the sea surface, through the water column, to the bottom. The velocity of surface currents, affecting perhaps the upper 200 m, is less than 25 cm/sec in an area over the Cape Verde Plateau (Fig. 2). The deep thermohaline circulation is predicted to be weak and diffuse on the eastern boundary of the North Atlantic (Wust, 1957; Defant, 1961) and direct observations indicate negligible near bottom currents at present (Lowrie et ah, 1970). The irregular topographic relief of the Cape Verde archipelago would further act to trap sediment on the bottom. The amount of atmospheric fallout might be expected to decrease away from the sediment source, which corresponds with the seaward narrowing and apparent thinning of the sedimentary apron that forms the Cape Verde Plateau. The northeast orientation of the bench observed on Tropical Bank (Fig. 4) indicates that the bench was cut by surf driven from the present prevailing wind direction and suggests that an eolian sediment transport system may have been in effect long enough to shape the Cape Verde Plateau and prograde the continental rise.

Acknowledgements William P. Osborn, formerly with Hudson Laboratories of Columbia University, assisted with the bathymetric chart. Henry S. Fleming of U.S. Naval Research Laboratory gave helpful encouragement. Dr. A. S. Laughton of the British National Institute of Oceanography provided charts of Echo Bank and Papp Seamount. Conversations with Drs. Louis W. Butler and George H. Keller of NOAA were valuable. Dr. Robert S. Dietz and Paul J. Grim of NOAA constructively criticized the manuscript. Ernest L. Bergeron, Consular Agent of the U.S., facilitated matters when the Gibbs made port in the Canary Islands. Captain Raymond E. Salman and the officers and crew of the USNS /. W. Gibbs provided splendid co-operation.

REFERENCES

Biscaye P. E. (1965) Mineralogy and sedimentation of recent deep-sea clay in the Atlantic

Ocean and adjacent seas and oceans. Bull. Geol. Soc. Am., 76, 803-831. Defant A. (1961) Physical Oceanography. Macmillan, New York, Vol. 1, 729 pp. Dietz R. S., H. J. Knebel and L. H. Somers (1968) Cayar submarine canyon. Bull. Geol.

Soc. Am., 79, 1821-1828. Ericson D. B., M. Ewtng, G. Wollin and B. C. Heezen (1961) Atlantic deep-sea sediment

cores. Bull. Geol. Soc. Am., 72, 193-286. Folger D. W. (1970) Wind transport of land-derived mineral, biogenic, and industrial

matter over the North Atlantic. Deep-Sea Res., 17, 337-352. Heezen B. C. and M. Tharp (1968) Physiographic diagram of the North Atlantic Ocean.

Spec. Pap. Geol. Soc. Am., 65, revised. International Hydrographic Bureau (1958) Carte Generate Bathymetrique des Oceans,

4th edition, Monaco. International Hydrographic Bureau (1968) Sheets 103, 104, 128, 129 for the Carte

Generate Bathymetrique des Oceans, Monaco. Lowrie A. and E. Escowitz, editors (1969) Kane 9. U.S.N. Oceanogr. Off. Global Ocean

Floor Analysis Res. Data, Ser. 1, 1-971. Lowrie A., W. Jahn and J. Egloff (1970) Bottom current activity in the Cape Verde and

Canaries Basin, Eastern Atlantic. Trans. Am. geophys. Un., 51, 336. Matthews D. J. ( 1 939) Tables of the velocity of sound in pure water and sea water. Admiralty,

Hydrographic Department, London, 52 pp. McMaster R. L. and T. P. Lachance (1970) Northwestern African continental shelf sedi- ments. Marine Geol., 7, 57-67 (1969). Prospero J. M. and T. N. Carlson (1970) Radon-222 in the North Atlantic trade winds:

Its relationship to dust transport from Africa. Science, 167, 974-977. Prospero J. M., E. Bonatti, C. Schubert and T. N. Carlson (1970) Dust in the Caribbean

atmosphere traced to an African dust storm. Earth Planet. Sci. Letters, in press.

Bathymetry off central northwest Africa 327

Rona P. A. (1969) Seismic reflection profiles from northwest African continental margin

between Canary and Cape Verde islands (abs.). Trans. Am. geophys. Un., 50, 21 1. Rona P. A. (1970) Submarine canyon origin on upper continental slope off Cape Hatteras.

/. Geo!., 78, 141-152. Rona P. A., E. D. Schneider and B. C. Heezen (1967) Bathymetry of the continental rise

off Cape Hatteras. Deep-Sea Res., 4, 625-633. U.S.N. Hydrographic Office (1952) Bottom Contour Chart 0305 N, 1st edition. U.S.N. Oceanographic Office (1961) The world. H. O. Misc., 15, 254-257. U.S.N. Oceanographic Office (1965) Oceanographic atlas of the North Atlantic Ocean,

Section I Tides and Currents. USNOO Pub. 700. 75 pp. Wust G. (1957) Stromgeschwindigkeiten und Strommengen in den Tiefen des Atlantischen

Ozeans. Wiss. Ergebn. dt. Atlant. Exped. ' Meteor ', 6 (2), 261-^20. Zuccaro A. and P. A. Rona (1968) Omega navigation performance off northwest Africa

during operation no. 267, April 23-May 28, 1968. Tech. Rept. Columbia Univ. Hudson

Lab., 153, 36 pp. (unpublished manuscript).

62

Reprinted from Geotimes

deep-sea salt diapirs

The case for deep-sea salt diapirs is alive and well in spite of reports to the contrary. Leg 14 of the Deep Sea Drilling Project (February 1971 Geo- times) obtained evidence from 2 drill- ing sites off northwest Africa support- ing the existence of deep-sea salt de- posits. At both Sites 139 and 140, in water depths of 3,047 and 4,483 m, on the middle and lower continental rise, the sediments showed marked sa- linity gradients (38 to 75 ppt in 665 m penetration at Site 139; the salinity of sea water is generally about 35 ppt). These 2 sites are situated where I have interpreted the presence of possible salt diapirs from geophysical data and regional geologic considerations (Rona, 1969, Nature, v. 224, p. 141- 143: American Association of Petro- leum Geologists Bulletin, v. 54, p. 129- 157). The diffusion rates of ions in saturated unconsolidated sediments are so high ( Vi to %o of diffusion rates in free solution according to Manheim (1970, Earth and planetary science letters 9, p. 307-309) that a signifi-

8 GEOTIMES May 1971

cant source concentration at depth is required to maintain the observed sa- linity gradients. The salinity gradients observed off northwest Africa are com- parable to those in sediments over salt deposits in the Gulf of Mexico (Man- heim & Sayles, 1970, Science, v. 170, p. 57-61).

The Leg 14 report emphasizes the drilling of a basalt body at Site 141, 200 km north of the Cape Verde Islands, that was interpreted as a salt diapir (Schneider & Johnson, 1970, AAPG Bulletin, v. 54, p. 2,151-2,169, figure 8). The hypothesis of deep-sea salt diapirs should not be judged on evidence from this single site but should await more evidence including publication of the Leg 14 salinity studies. The model which I postulated of the early Atlantic as an evaporite basin restricted by the Late Triassic/ Jurassic positions of the drifting con- tinents remains reasonable. Peter A. Rona

NOAA, Atlantic Oceanographic & Meteorologic Laboratories Miami, Fla.

63

Reprinted from Nature 231 , 179-180.

Depth Distribution in Ocean Basins and Plate Tectonics

In this article I shall show that relationships between the movement of lithospheric plates1-3 and the depths of the sea floor are leading towards a quantitative theory of the distri- bution of oceanic depths, and that some predictions can be made. Several principal lithospheric plates have now been recognized; their relative motion over the mantle is described by a rotation of one plate relative to an adjacent plate4-6. The rotation requires two parameters to locate the pole of relative rotation, and one to specify the magnitude of the angular velocity. The direction of spreading is along small circles concentric about the pole of rotation and the velocity of spreading varies as the sine of the distance (measured in degrees of arc) from that pole, to a maximum at a distance of 90° along the equator of rotation. The angular velocity of rotation is the same everywhere. In the Atlantic Ocean the fracture zones between about 60° N and 10° S are very nearly small circles centred about a pole near the southern tip of Greenland (62 ±5° N, 36 ±2° W), and the spreading rates approximately agree with the velocities required for the opening of the North Atlantic about this pole1,3.

Examination of the topography of the sea floor and spreading rates in the central region of the world system of mid-ocean ridges shows that the width of the ridge7, the local topography8, and the thickness of layer 2 of the oceanic crust8 seem to be related to the spreading rate in the following way. (1) Slow spreading (1-2 cm yr-1) away from the ridge centre is asso- ciated with a narrow ridge, a central rift, adjacent rift moun- tains and a thick layer 2. (2) Fast spreading (3-4.5 cm yr-1) is associated with a wide ridge, subdued topography (no central rift) and a thin layer 2. (3) The volume of lava dis- charged in layer 2 per unit time and unit length along the crest of the whole active system is relatively constant regardless of the spreading rate. Thus, topography and the thickness of layer 2 can be predicted if the rate of spreading is known.

An examination of topographic profiles perpendicular to various sections of the world mid-ocean ridge system supports the inference that topography is a function of spreading rate9. The relationship between the slope of ridge flanks and the spreading rate from the ridge crest to magnetic anomaly No. 5 at a distance corresponding to 107 yr was formulated from this series of profiles so that, by knowing the spreading rate, the slope can be calculated9. The faster the spreading rate within an episode of spreading, the lower the topographic slope and roughness, measured over a distance corresponding to the crust generated during that episode. The decrease in

180

0

1,000 2,000 3,000 4,000 5,000 6,000 7,000

I ' I

ft ~*~ ' X

I «•»!

Latitude (north)

Fig. 1 Depth distribution at the inner margin of the High Fractured Plateau province and marginal basins1 ' of the northern Mid-Atlantic

Ridge (R, I-IV" ; E, I, J10). A vertical bar indicates variations where the topography is too irregular to determine a unique depth. The

dashed line is part of a sine curve varying from maximum elevation (zero depth) at the latitude of the North Atlantic pole of rotation

(62° N, ref. 1) to minimum elevation (maximum depth) at the equator of rotation, 90° to the south.

topographic slope with increasing spreading rates is a result of the greater length of layer 2 crust generated per unit time, as well as an almost linear decrease in the absolute elevation of the crest of the ridge associated with the thinning of layer 2.

From the lithospheric plate motions1 ~3 and the relationships between spreading rate and sea floor topography7-9, it follows that the depth of a mid-ocean ridge crest increases from a maximum elevation (zero reference depth) near the pole of rotation with the sine of the distance from the pole, and the slope of its adjacent flanks decreases with the reciprocal of the sine of the distance from the pole of rotation of the two litho- spheric plates the boundaries of which form the ridge. The limiting case of zero slope and zero elevation (maximum depth) along the equator of rotation never occurs because it would require an infinite rate of sea floor spreading.

Sufficient data exist to test this hypothesis over about 40° of latitude in the North Atlantic. The depths of the Mid- Atlantic Ridge, measured at the inner margin of the High Fractured Plateau province, decrease between 49° and 12° N and this decrease may be approximated by a sine curve originat- ing at the latitude of the pertinent North Atlantic pole of rotation (62° N) (Fig. 1, and see ref. 1). The variation in depths about the sine curve is a result of the irregular topo-

Distar.ce from rift valley of Mid- Atlantic Ridge (km) 0 100 200 300

s.ooo-1

Fig. 2 Half-profiles perpendicular to the crest of the Mid- Atlantic Ridge. The High Fractured Plateau and Flank pro- vinces are represented by straight line segments fitted through the mean topographical values with slopes as indicated'0. The topographic step between provinces is evidence of a lapse in sea floor spreading which occurred simultaneously ending about 107 yr ago10.

graphy of the ridge crest transected by numerous fracture zones. The southward decrease in crestal elevation and slope of the ridge flanks is apparent in profiles perpendicular to the ridge axis (Fig. 2). To measure depth and slope, the irregular topography of the High Fractured Plateau and Flank provinces was fitted with straight line segments through the mean topo- graphical values. The depth of both provinces progressively increases and the slope decreases with distance from the pole of rotation. A marked topographic step between the High Fractured Plateau and the Flank provinces is evidence of a discontinuity in sea floor spreading, when the ridge subsided during a spreading lapse ending about 107 yr ago10 (a dis- continuity of zero spreading would result in a vertical topo- graphic step of infinite slope). The progressive southward increase in the width of the High Fractured Plateau province is consistent with the increase of spreading rates with distance from the pole of rotation.

The maximum depth along the axes of the basins on the east and west margins of the Mid-Atlantic Ridge increases away from the pole of rotation, measured between 55° N and 12° N (Fig. 1). The axes of maximum depth can be approxi- mated by sine functions, with the exception of an anomalous decrease in depth along the part of the western basin adjacent to the Lesser Antilles island arc, where special structural conditions prevail. The increase in depth at the axes of the marginal basins is less than that at the ridge crest, so that their respective sine curves converge towards the equator of rotation.

The observation that the increase in depth at the ridge crest and at the axes of the marginal basins can both be described by sine functions, originating near a pole of rotation and con- verging towards the equator of rotation, indicates that depth distribution is maintained as the sea floor spreads bilaterally away from the crestal region and subsides on the ridge flanks. The hypothesis presented here helps to explain the correspond- ence between depth and latitude in the oceans, because the poles of lithospheric plate rotation tend to lie near the Earth's rotational axis.

I thank D. C. Krause for a constructive review.

Peter A. Rona National Oceanic and Atmospheric Administration, Atlantic Oceanographic and Meteorological Laboratories, Miami, Florida 33130

Received April 16, 1971.

1 Morgan, W. J., J. Geophys. Res., 73, 1959 (1968).

2 McKenzie, D. P., and Parker, R. L., Nature, 216, 1276 (1967).

3 Le Pichon, X., J. Geophys. Res., 73, 3661 (1968).

4 Holmes, A., Trans. Geol. Soc. Glasgow, 18-3, 559 (1931).

5 Hess, H. H., Petrologic Studies: A Volume in Honour of A. F

Buddington, 599 (Geol. Soc. Amer., 1962).

6 Dietz, R. S., Nature, 190, 854 (1961).

7 Vogt, P. R., and Ostenso, N. A., Nature, 215, 810 (1967).

8 Menard, H. W., Science, 157, 923 (1967).

9 Le Pichon, X., and Langseth, jun., M. G., Tectonophysics, 8, 319

(1969).

10 Schneider, E. D., and Vogt, P. R., Nature, 217, 1212 (1968).

11 Heezen, B. C, Tharp, M., and Ewing, M., Special Paper 65

(Geol. Soc. Amer., 1959).

Reprinted from Geology Bulletin No. 5, 25-29

MARINE GEOPHYSICAL OBSERVATIONS OF THE EASTERN PUERTO RICO-VIRGIN ISLANDS REGION

by

Robert B. Starr and Robert G. Bassinger Atlantic Oceanographic Laboratories, Environmental Science Services Administration, Miami, Florida 33130

Abstract

During early May 1966, a combined bathymetric, seismic reflection profile, and total magnetic field inten- sity investigation was conducted of the area south and east from Puerto Rico to the Virgin Islands, using precise Hi- Fix navigation control. Except for the exceptionally shallow, flat area of the Puerto Rico-northern Virgin Islands platform, the bathymetry indicates a very irregular submarine topography of basins and block faults. The disturbed magnetic signature over the platform indicates at- or near-surface sources. South of the platform three basins with appreciably different depths were delineated. Sub-buttom reflectors within these basins indicate evi- dence of recent deformation. Bordering these basins to the south, a broad ridge with peaks at least as shallow as 500 fathoms, except for the shoaler Grappler Bank, extends west from St. Croix. A minor magnetic expression was evident over the ridge, but none was noted for Grappler Bank.

Introduction

The Puerto Rico-Virgin Islands shelf and St. Croix Ridge with the intervening Virgin Islands Trough1 are at the eastern end of the Greater Antilles sector of the An- tilles Arc. The area and tracklines are shown in Figure 1 .

This study was conducted from the USC&GSS "Whiting" in 1966. Observations consist of 1,1 80 nautical miles of hydrographic soundings, continuous seismic re- flection profiling, and total magnetic-field intensity observations at a nominal line spacing of 4.6 nautical miles. Ship's position was determined with Hl-FIX elec- tronic navigation. Additional lines of hydrography and magnetics were obtained by the USC&GSS "Explorer" in 1965 and one line of hydrography and seismic reflection profiling by the USNS "Lynch" in 1 967.

Results

Bathymetry

For convenience of discussion, the bathymetry of the Puerto Rico-Virgin Islands region may be divided into five provinces on the basis of their morphology. From north to south these are ( 1 ) south slope of the Puerto Rico Trench (north slope of the shelf), (2) Puerto Rico-Virgin Islands shelf, (3) Virgin Islands Trough, (4) St. Croix Ridge, and (5) north margin of the Venezuelan Basin. These provinces have an east-west trend throughout the study area.

1 The names "Virgin Islands Trough" vice "Virgin Islands Basin," "Grappler Seamount" vice "Grappler Bank," "St. Croix Ridge," "Whiting Basin," and "Whiting Seamount" were approved by the U.S. Board of Geographic Names, September 19, 1968.

The upper portion of the south slope of the Puerto Rico Trench (Fig. 2) consists of a short, steep scarp of about 20° terminating between depths of 80 and 940 fathoms. At this point the slope abruptly changes to a gradient which it maintains to the limit of the tracklines. A "V"-shaped depression in this slope at about 65°05'W suggests a submarine canyon.

The Puerto Rico-Virgin Islands shelf is nearly a featureless plain except for the islands and isolated banks and reefs. The northern half, however, averages approxi- mately 15 fathoms deeper than the shallower southern half. From our traverse west of Culebra Island, this depth difference appears to be associated with a fault. Donnelly (1965) relates this declivity between St. Thomas and Culebra to post-Pleistocene faulting.

From the character of the sounding records the steep walls of the Virgin Islands Trough appear to be much rougher than mapped, with spurs intersecting a bottom of discontinuous, relatively flat areas. Southeast of Puerto Rico a small basin (Whiting Basin) is defined by the 1 ,000-fathom isobath. This basin is separated from the trough by a north-south ridge connecting the Puerto Rico-Virgin Islands shelf with Whiting Seamount. East of the basin the trough deepens to a small plain at 2,200 fathoms which is partially separated from the main floor of the trough (PI. 1). The main floor is outlined by the 2,400 fathom isobath (PI. 1 and Fig. 2).

The St. Croix Ridge extends westward from St. Croix to Investigator Bank. West to 65°35'W, the ridge consists of an irregular row of discontinuous highs with northeast-trending spurs. Our soundings indicate that the deepest passage over the ridge occurs between 65°25'W and 65°30'W, and appears to be a little over 1,000 fathoms.

West of 65°35'W,the St. Croix Ridge has a different character from that to the east. It consists of three inter- connected peaks: Whiting Seamount, Grappler Seamount, and Investigator Bank. Summits of these are much shallower than the crest of the ridge in the east ; the top of Grappler Seamount is only 35 fathoms, for instance, and no consistent trend of the isobaths is apparent.

The north slope of the Venezuelan Basin appears to have a uniform gradient. Except for minor irregularities, the slope averages between and 7°. It decends from the St. Croix Ridge to somewhat over 2,700 fathoms in the southeastern part of the area (PI. 1 ).

Sub-Bottom Profiling Results

Seismic reflection results shown in the cross-section (Fig. 2) are form lines showing approximate penetration based on the instrument calibration velocity of 4,800 fps. The quality of the reflection records varied widely throughout the area. Penetration of the south slope of the Puerto Rico Trench was excellent. Several reflectors were observed, decreasing in number and thickness downslope (Fig. 2).

Trans. Fifth Carib. GeoL Cont, GeoL Bull. No. Queens College Press, May 1971.

26

On the shallow Puerto Rico-Virgin Islands shelf, the hard bottom and multiple reflectors limited the profiler results. However, on the lines northeast of Vieques Island, sufficient penetration was obtained to identify southeast- dipping strata as far as three miles offshore ( Fig. 3). South- east of St. Thomas, an anticline was crossed with its limbs dipping northeast and southwest (Fig. 4). In addition, numerous small scarps were crossed. Similar features have been interpreted by Donnelly ( 1 965) as fault scarps.

No significant sub-bottom reflectors were recorded along the walls of the Virgin Islands Trough owing pos- sibly to the lack of sediment on the steep walls. The bottom of the trough, however, consists of good reflec- tors. These reflectors are flat lying or dip to the south away from a low, northeast-trending ridge which crosses the floor of the trough at 65°05'W. The contacts of the sediments of the trough bottom with the walls are in all cases abrupt and discontinuous. The walls appear to be fault scarps and the trough a graben (Fig. 2) as earlier suggested by Meyerhoff( 1927) and Whetten ( 1 966).

On the St. Croix Ridge, the eastern sector has southerly dipping strata on the northern ends of the spurs, but no reflectors were apparent on the main crest of the ridge (Fig. 2) or on the seamounts of the western sector. The profiler record of the top of Grappler Seamount is similar to that of the Puerto Rico-Virgin Islands shelf.

No discernible sedimentary strata were found on the northern slope of the Venezuelan Basin. However, the basin itself provided some of the deepest reflected pene- trations recorded (up to 0.7 sec). On the reflection records the boundary between the basin and the north slope can be placed at an apparent fault scarp (Fig. 2). The abrupt discontinuous contact of the basin sediments with the north slope, and the slump structures with multiple slip planes on some of the sections indicate this boundary to be a fault line. A fault at this general location has been inferred by Meyerhoff (1927) and Donnelly ( 1 964).

Magnetics

Over the southern slope of the Puerto Rico Trench and the northern edge of the Puerto Rico-Virgin Islands shelf the magnetic anomalies are of long wave length and small amplitude (PI. 2 and Fig. 2). This suggests that the sources of the anomalies are broad relative to their thick- ness and are probably at a moderate depth.

The magnetic pattern of the Puerto Rico-Virgin Islands shelf proper consists of belts of high amplitude, short wave-length anomalies (Fig. 2) which are more or less parallel to the margins of the shelf. Some of these anomalies are directly associated with known intrusivesin the islands and most of them probably reflect the occur- rence of near-surface intrusive bodies (Renard, 1967).

The linear magnetic low in the wall of the Virgin Islands Trough (PI. 2) which coincides with the break in the slope east of Vieques Island suggests the possibility of a fault. This could be an extension of the major east-west fault zone of northern Puerto Rico (Briggs and Akers, 1965;Mattson, 1966).

East of 65°35'W a slight, linear, east-west magnetic high with a corresponding magnetic low to the north is apparently associated with the St. Croix Ridge. A promi- nent low immediately southeast of St. Croix may be

related to the coastal plain graben found there (Ceder- strom, 1950; Whetten, 1966). The western sector of the ridge has noticeable anomalies which correlate with Whiting and Grappler seamounts. To the south, the northern edge of the Venezuelan Basin appears to have a relatively featureless magnetic pattern.

References

1. Briggs, R.P., and Akers, J. P., 1965, Hydrogeologic map of Puerto Rico and adjacent islands: U.S. Geol. Survey Hydrol. Inv. Atlas HA-1 97.

2. Cederstrom, D.J., 1950, Geology and ground-water resources of St. Croix, Virgin Islands: U.S. Geol. Survey Water Supply Paper 1067, 117 p.

3. Donnelly, T.W., 1964, Evolution of eastern Greater Antillean island arc: Am. Assoc. Petroleum Geolo- gists Bull., v. 48, p. 680-696.

4. 1965, Sea-bottom morphology

suggestive of Post-Pleistocene tectonic activity of the eastern Greater Antilles: Geol. Soc. America Bull., v. 76, p. 1291-1294.

5. Mattson, P.H., 1966, Geological characteristics of Puerto Rico: p. 124-138 in Continental margins and island arcs, ed. Poole, W. H.: Geol. Survey Canada Paper 66-15, Ottawa, Queens Printer, 486 p.

6. Meyerhoff, H.A., 1927, The physiography of the Virgin Islands, Culebra, and Vieques: N.Y. Acad. Sci. Scientific Survey of Porto Rico and the Virgin Islands, v. 4, pt. 2, p. 145-219.

7. Renard, V., 1967, Virgin bank: Correlation of mag- netism and gravity with geology: Ph.D. Thesis, Rice University, 1 1 1 p.

Whetten, J.T., Virgin Islands: 177-239.

1966, Geology of St. Croix, U.S. Geol. Soc. Am. Memoir 98, p.

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CONTINENTAL TERRACE AND DEEP PLAIN OFFSHORE CENTRAL CALIFORNIA

L.AUSTIN WEEKS* and ROBERT K. LATTIMORE

Environmental Science Services Administration, Atlantic Oceanographic and Meteorological Laboratories, Miami, Fla. 33130, U.S.A.

(Received 21 April, 1970)

Abstract. Seismic-reflection profile investigations of the California continental terrace and Deep Plain, between 35 °N and 39 °N, support the hypothesis that the continental shelf and slope consist of alternating blocks of Franciscan and granitic-metamorphic basement overlain by varying thick- nesses of younger sediments. North of 37 °N, the seismic profiles confirm the distribution of turbidites shown by other workers. A significant proportion of the sediments on the middle and lower con- tinental rise, south of 37 °N, appears to be unrelated to the present Monterey deep-sea canyon system.

Near 39 °N the ridge which forms the topographic axis of the Delgada deep-sea fan consists of a thin cover of acoustically-transparent sediment unconformably overlying a thick sequence of turbi- dites; the southern part of this ridge is composed of well-defined short reflectors of highly variable dip. The ridge is incised by a steep-walled, flat-floored valley which follows a nearly straight course across its eastern flank. Among possible explanations for this pattern is uplift of the sea floor beneath the ridge.

Our data and investigations of others indicate that acoustic basement north of 38°40'N is at least 0.5 sec (two-way travel time) shoaler than it is south of Pioneer Ridge; when present, the ridge may represent as much as 0.5 sec additional basement relief. This structural pattern probably does not extend east of 127°40'W, although the magnetic expression of the ridge persists to 127°W.

Disappearance of the distinctive abyssal hills topography from west to east within the area of investigation usually can be attributed to burial by turbidites. Normal 'pelagic' sediments form a veneer, rarely more than 0.15 sec thick, which conforms with the basement topography; some loca- lities are devoid of discernible sediment.

1. Introduction

The first regional investigation of the sea floor off central California was part of a study of the entire California coastal margin by Shepard and Emery (1941); along with maps and descriptions of the shelf and slope, their paper includes hypotheses on the evolution of the more important physiographic features. Menard (1955) gave the name, "Deep Plain of the northeastern Pacific", to the area bounded by the Mendoci- no and Murray fracture zones (Figure 1), and described the area in the context of the tectonic framework of the entire northeastern Pacific basin.

Systematic marine geomagnetic observations in the area bounded by the Mendocino and Murray fracture zones have been reported by Mason (1958), Vacquier et al. (1961), Mason and Raff (1961) and others. A detailed bathymetric map of the continental margin, prepared by H. W. Menard, was published in Heezen and Menard (1963, Figure 12) and in more complete form in Winterer et al. (1968, Figure 7). Soundings and bottom samples taken across Santa Lucia Bank and the shelf offshore San Fran-

* Present address: 13720 SW 78th Ct., Miami, Fla. 33158, U.S.A.

Marine Geophysical Researches 1 (1971) 145-161. All Rights Reserved Copyright © 1971 by D. Reidel Publishing Company, Dordrecht - Holland

65

146

L.AUSTIN WEEKS AND ROBERT K.LATTIMORE

cisco as part of a regional investigation of the continental slope have been reported by Uchupi and Emery (1963). Curray (1965) has described seismic-reflection profiles of the continental shelf and slope between Santa Lucia Bank and Cape Mendocino. In addition to these regional investigations, there is an extensive literature dealing with individual features within the Deep Plain.

Fig. 1.

In 1965 and 1966, as part of the Environmental Science Services Administration - U.S. Coast and Geodetic Survey contribution to the international Upper Mantle Project, systematic marine geological and geophysical studies were made of the area between 35° and 39° North Latitude, extending from the California coast to 133° West Longitude - the offshore extension of the U.S. Trancontinental Geophysical Survey (TGS) (U.S. Upper Mantle Committee, 1965, p. 115). The TGS investigations included continuous geomagnetic measurements, soundings, and gravity observations along east-west lines spaced at 18-km intervals (Lattimore et al., 1968a, b) as well as the collection of deep-sea cores and heat-flow measurements (Burns and Grim, 1967). The results of the TGS seismic-reflection profile reconnaissance, made by USC&GSS Surveyor in April and May, 1966, are presented in this report.

CONTINENTAL TERRACE AND DEEP PLAIN OFFSHORE CENTRAL CALIFORNIA 147

2. Methods

Continuous seismic-reflection profiles were made along a series of east-west lines, spaced at 50-60 km intervals, extending from the California coast to the base of the continental slope; at 36 °N and 39 °N, the lines were extended to 130°W (Figure 2). Additional traverses were run to construct a northeast-southwest profile which inter- sects the continental slope near Pioneer Seamount, and a northwest-southeast profile running roughly along the 4000-m isobath. The seismic profiles were made with a 20,000-joule Rayflex 'arcer' fired at 4-sec intervals; the return signal was subjected to a 70-120 Hz-bandpass filter. Normal survey speed was about 12 km/hr but the vessel's speed was slowed as necessary to obtain acceptable records in heavy seas.

Ship's position was determined with the U.S. Navy Satellite Navigation System, fixes being obtained at irregular intervals averaging once every two hours. This con- trol was supplemented with LORAN and other conventional means of determining position. The probable error in any smooth-plotted ship's position is estimated to be less than 2 km.

The deepest continuous reflector on the seismic records usually was selected as the top of the basement. Beneath the sediments of the upper continental rise and in other localities where there was no distinctive reflector, the top of the basement was picked at a level below which there were no returns suggestive of bedding, so long as this level was well within the limits of penetration of the signal. 'Basement' thus represents only the shoalest acoustically-opaque rock and the nature and lithology of the base- ment would be expected to vary from place to place. In the continental rise, the top of the basement seems to be generally equivalent with the top of the seismic second layer as determined by refraction measurements (Mason, 1958, p. 328 and Figure 2; Menard, 1964, Figure 3.3; Winterer et «/., 1968, Figure 6).

3. Results and Discussions

As has been noted, the deep-sea portion of the area of the Transcontinental Geophys- ical Survey investigation falls within the "Deep Plain of the northeastern Pacific" (Menard, 1955, p. 1158). Generally, the Deep Plain is about 1.5 km deeper than the Ridge-and-Trough Province north of the Mendocino Escarpment, and about a half- kilometer deeper than the Baja California Seamount Province south of the Murray Fracture Zone (Menard, 1960, Figure 2); its main characteristic is that it is relatively featureless in comparison with the two provinces which adjoin it.

The results of the TGS seismic reflection observations are presented as interpreta- tive line drawings in Figure 2. The locations of the illustrated profiles are shown on the accompanying bathymetric map (Figure 2) which has been redrawn from one prepared by the authors for the Transcontinental Geophysical Survey report (Latti- more et ah, 1968b).

Because of the size of the area of study and the diversity of geologic features within it, it is convenient to divide the TGS area into five provinces, and to include in the

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discussion of each province a review of the results and conclusions of earlier investi- gators. The five areas are: (1) continental terrace (shelf and slope); (2) continental rise south of 37 °N; (3) Delgada deep-sea fan; (4) Pioneer Ridge; and (5) abyssal hills (Figure 1 ).

A. CONTINENTAL TERRACE

North of Cordell Bank, the TGS investigation and the study reported by Curray

(1965) show that the continental shelf is composed of a thick sequence of moderately to intensely deformed strata, in some localities overlain by beds which are gently arched and cut by faults of small vertical displacement (see Curray, 1965, Figure 2). The continental slope is made up of a series of fault blocks, in which evidence of stratification can be found in the surface sediments down to depths of approximately 1800 m (A A', Figure 2).

The area from Cordell Bank south to Pioneer Seamount, which for convenience will be referred to as the Farallon platform, is characterized by an unusually wide shelf (in comparison with the shelf to the north and south) and by relatively minor incision of the shelf by sea valleys. The width and morphology undoubtedly are attributable to the presence of relatively resistant rock beneath the edge of the shelf and the upper slope (BB', Figure 2; Curray, 1965, Figure 3). A thick section of folded strata lies to landward of this resistant block ; the present sea floor has been cut across both units, presumably by Pleistocene wave erosion (Curray, 1965, p. 798).

Between Pioneer Seamount and Monterey Canyon, the edge of the continental shelf is made up of at least a half-second of folded sedimentary rocks but a well-defined basement block, cut by faults, can be recognized under the middle continental slope at depths of 800 m or more (CC, DD', Figure 2; Curray, 1965, Figure 4).

From Monterey Canyon south to 35 °N, the edge of the shelf consists of no more than a half-second of folded sedimentary rock (EE\ FF', GG', Figure 2). These strata are overlain by younger sediments which thicken landward (to at least 0.7 sec at 36 °N) and have been tilted and faulted. Off Point Sur (EE', Figure 2), at a depth of 1000 m (approximately 1.5 sec), folded strata which make up the edge of the shelf are in fault contact with a basement block that forms the middle continental slope. Off Cape San Martin (FF', Figure 2) and on Santa Lucia Bank (GG', Figure 2), the base- ment can be traced from beneath the edge of the shelf toward the shoreline; both basement and some of the overlying sediments are cut by faults. The continental slope is made up of fault-blocks of basement rock, in some places thinly covered by sedi- ments.

The presence of basement beneath the outer continental shelf and upper slope was first established by Curray (1965), who concluded that basement rocks comprise an essentially continuous ridge extending from 35°30'N to 39°30'N, with the possible exception of a zone north of Point Arena (Curray, 1965, p. 799 and Figure 1). Page

(1966) suggested that, like the Coast Ranges, the California shelf and slope may be made up of blocks of a granitic-metamorphic complex alternating with blocks under- lain by Franciscan rocks. The Franciscan includes a flysch sequence ranging in age

152 L. AUSTIN WEEKS AND ROBERT K. LATTIMORE

from Late Jurassic to Late Cretaceous; the granites are overlain unconformably by Upper Cretaceous and Paleocene strata (Taliaferro, 1951, p. 117). Page (1966, Figure 1 ) also proposed that the Salinian block - granodiorite basement bounded roughly by the Nacimiento and San Andreas faults - extends beneath the continental shelf northwest of Monterey Bay. South of Monterey Bay and west of the Nacimiento fault, sediments of the shelf are underlain by the Franciscan core complex (Page, 1966, Figure 6). The results of our investigations are entirely consistent with the hypothesis of Page (1966). Furthermore, because the trends of the Salinian block are slightly to the west of the shoreline, Franciscan basement would be expected to occur west of the shelf break, north of 36°30'N (Figure 3); the presence of faulted basement blocks beneath the slope at 36°50'N (DD', Figure 2) and 37°20'N (CC\ Figure 2) has been noted.

B. CONTINENTAL RISE SOUTH OF 37 °N

The thalwegs of the more important sea valleys on the lower continental slope and continental rise, inferred by the authors from the TGS fathograms, are shown on the bathymetric map (Figure 2).

The existence of a tight meander in the Monterey deep-sea valley system, at 36°15'N, 122°50'W (map, Figure 2), was first established by Shepard (1966, Figure 1); he also showed that the valley which drains southward from the meander just east of 123°W does not breach the wall of the main canyon. South of 36 °N, what is presumed to be the main channel of the Monterey system trends somewhat east of south toward the flank of Davidson Seamount, as has been shown by Dill et al. (1954, Figure 2); a secondary valley branches off to the southwest. South of 35°30'N the main channel also swings southwestward and breaks up into a number of distributary channels.

Although the TGS investigation included east-west bathymetric profiles at approx- imately 18-km intervals, Pioneer Canyon could not be traced beyond the base of the continental slope. The depressions delineated by the 3800-, 4000-, and 4200-m isobaths between 36 °N and 37 °N (Figure 2) are marked by a number of valleys; although some of these are fairly well-developed, no single valley could be traced from one bathymetric profile to the next.

Throughout the area south of 37'30'N, two distinct types of internal structure can be recognized in the sediments of the continental rise. The first is characterized by near-horizontal, continuous reflectors which are independent of structural relief of the basement or underlying strata, and usually form a smooth sea-floor profile, con- cordant with the regional gradient. On the upper and middle continental rise, these sediments form floodplain-like deposits which rise tens or even hundreds of meters above the regional level of the sea floor, and extend laterally from the axes of deep-sea valleys for a hundred kilometers or more. Such deposits often are impounded by local topographic highs (124°25'W, 126°50'W, FF', Figure 2). In the transition zone be- tween the typical profile of the abyssal hills and the smooth profile of the continental rise, continuous reflectors can be seen to fill-in between the hills, forming broad, flat- floored valleys (127°20'W, 127°50'W, BB', Figure 2); disappearance of the abyssal

CONTINENTAL TERRACE AND DEEP PLAIN OFFSHORE CENTRAL CALIFORNIA

153

Fig. 3.

hills topography from west to east across the lower continental rise usually can be attributed to burial by this type of sediment. There is little doubt that these strata are turbidites (Hamilton, 1967, Figure 10a).

The second type of sedimentary structure is characterized by 'soft' reflectors, often

154 L.AUSTIN WEEKS AND ROBERT K.LATTIMORE

with variable dip, which commonly extend for no more than 2-3 km along the profile. Sea-floor outcrops of these strata frequently coincide with reversals or marked changes in the regional depth gradient (124°30'W-125°W, HH', Figure 2) and often with a zone of 'rough' topography (124°40'W-125°W, FF'; 37°N, JJ', Figure 2). Perhaps the most significant characteristic of these reflectors is that they are to some degree conformable with structural relief of the basement. An extensive blanket of sediments containing zones of these discontinuous-conformable reflectors occurs south of 37 °N at depths greater than 4000 m(124°15'W-124°25'W, DD', 124o30'VV-125°30'W, HH', Figure 2); the zones range in thickness from 0.4 sec upwards. The presence of isolated valleys in this area has been noted; despite the presence of such valleys, however, it is impossible to relate these strata to any known major deep-sea channel system. South of 36°15'N, similar deposits extend landward to the 3800-m isobath (JJ', Figure 2); the seismic profiles show that they are overlain by near-horizontal, floodplain-like turbidites which are associated with the Monterey deep-sea valley system. In some localities, well-bedded, horizontal strata fill in valleys and other depressions in the discontinuous-conformable sediments.

From consideration of their areal distribution, conformability, and relationship with the overlying turbidites, it seems likely that strata containing the discontinuous- conformable reflectors are composed predominantly of deposits formed in the deep ocean by some means other than turbidite sedimentation. If these deposits can be attributed to normal ('hemipelagic') sedimentary processes operating in the deep ocean, the sediment column in any given locality would consist of varying admixtures of 'normal' allogenic-abyssal and turbidite sediments; distinctive internal structures would be expected only if one process or the other were predominant. A second pos- sibility is that the discontinuous-conformable strata originally were horizontal, and have been involved in post-depositional tectonic activity.

Regardless of the origin of the discontinuous-conformable reflectors, their nature and distribution militate against their having been derived from the present Monterey deep-sea valley system. These investigations suggest that deposits clearly associated with the Monterey system actually may comprise only a relatively small part of the blanket of sediments on the middle and lower continental rise between 35 °N and 37 °N.

C. DELGADA DEEP-SEA FAN

The topographic axis of the Delgada deep-sea fan is a broad, roughly symmetrical ridge which originates at the base of the continental slope north of Delgada Canyon (Shepard and Emery, 1941, Chart IV) and extends southwest to about 38°15'N (Figure 2). Two deep-sea valleys lie southeast of this ridge, between its axis and the base of the continental slope. Both valleys run generally south-southwest from where they enter the area (39 °N) to about 38 °N, where they swing southwest and apparently break up into a number of smaller distributary channels; one of these channels can be traced as far as 37 °N, 126°30'W (Figure 2).

Between 39 °N and 38°10'N the westernmost of the two deep-sea valleys follows a nearly straight course across the eastern flank of the axial ridge, and its valley seems

CONTINENTAL TERRACE AND DEEP PLAIN OFFSHORE CENTRAL CALIFORNIA 155

to have been incised into the ridge. South of 38°15'N, where the relief of the ridge disappears, the channel begins to meander and constructional levees are present. This valley is considered to be a member of the Delgada Canyon system (Figure 1).

Between 39 N and 38 °30'N, the eastern channel apparently occupies a broad, shal- low valley, 10 km or more across, with relief on the order of 30 m. At depths greater than 3800 m, this channel has a well-defined V-shape with relief of 40 m or more. Bathymetric profiles between 38°20'N and 37°50'N show an asymmetric valley whose cross-sections are consistent with the meandering course shown on the map (Figure 2); levees first appear south of 38°10'N, at depths of about 3900 m.

Of the several sedimentary 'units' which can be distinguished in the Delgada deep- sea fan, by far the most important in terms of volume are the turbidites. These deposits cover the upper continental rise between 37°30'N and 39 °N (BB', AA', Figure 2) and extend into the abyssal hills as far west as 128°W (BB', Figure 2), in some localities beyond 128°30'W (Ewing et a/., 1968, Figure 7). As far south as 36 °N, turbidite strata west of 126°30'Wmay be part of the Delgada deep-sea fan (FF', HH', Figure 2). As has been shown by Menard (1964, plate) a tongue of turbidites, 20-40 km wide, extends along the base of Pioneer Ridge at least as far west as 133°W. Stratified, horizontal sediments were noted on seismic-reflection profile crossings of Pioneer Ridge between 132°W and 133°W, and Naugler and Perry (personal communication) describe a typical turbidite sequence from a core at 38°30'N, 132°W.

At 38°50'N (AA', Figure 2), the western slope of the ridge which forms the topo- graphic axis of the fan consists of 0.1-0.2 sec of sediments lying unconformably upon a thick sequence of near-horizontal strata that appear to be continuous with the tur- bidites at the base of the continental slope. Extensive areas of the western slope are characterized by a 'hummocky, terrain in which low (15-25 m) hills, sinusoidal in section, occur at regular 1-2 km intervals along the profile. An example of this topo- graphy can be seen in Profile AA' (Figure 2), where the hummocks are developed in near-surface sediments which lie unconformably on the turbidites. Within the uppor- most 0.1-0.2 sec of these sediments only a single reflector can be discerned - a nearly continuous surface which is parallel with the present sea floor and which follows the relief of the individual hummocks. The hummocky structure and the absence of horizontal reflectors make it extremely unlikely that the near-surface sediments are turbidites; probably, they are normal deep-ocean allogenic deposits, or 'pelagic' sediments in the broad sense.

The southern end of the ridge consists of 0.4-0.6 sec of sediments in which the reflectors are discontinuous and highly contorted (37°55'N-38°30'N, JJ', Figure 2). These chaotic reflectors apparently have been observed also by Truchan et al. (1967, p. 126) as "'cross reflections' exhibiting large apparent dips" covering an area from the Delgada Channel (probably the eastern valley) to 38°30'N and 125°35'W. Land- ward of this valley, these authors noted, the sub-bottom strata are nearly horizon- tal.

The 'cross reflections' differ in several important respects from the discontinuous- conformable reflectors described in the preceding section. Although short, the 'cross

156 L.AUSTIN WEEKS AND ROBERT K.LATTIMORE

reflections' are distinct and well defined. In contrast with the soft, discontinuous reflectors, which may show sub-parallel orientation and commonly reflect basement relief, the 'cross reflections' may be highly angular with respect to one another, and usually are independent of relief of the basement. Significantly, the 'cross reflections' are clearly associated with a major deep-sea valley system, as has been established by Truchan et al. (1967, p. 126) and is illustrated in Profile JJ' (Figure 2).

The relation of the 'cross reflections' to sea floor stream channels, and their internal structure and independence of basement relief suggest that the southern part of the axial ridge (JJ', Figure 2) is composed of fossil channel levee and scour-and-fill deposits. The suggestion that these are slump deposits or submarine landslides derived from the shelf to the east is unsatisfactory in view of their distance from the base of the continental slope, their areal extent (Truchan et al., 1967, p. 126) and the present gradient of the ridge, which is a maximum of 20 m/km.

To summarize the preceding paragraphs, near 39 °N the ridge which forms the topographic axis of the Delgada deep-sea fan consists of a succession of turbidites overlain unconformably by 'normal' allogenic-abyssal sediments. To the south, both give way to the 'cross reflections' which may have formed by reworking of older sedi- ments. The eastern slope of the ridge is deeply incised by a stream valley that follows a fairly straight course across it, forming an acute angle with the axis of the ridge near 38°15'N (Figure 2). Clearly, this pattern of sedimentation and valley morphology cannot be explained in terms of a static environment; some element of tectonic activity must be invoked to explain it.

Uplift of the continental shelf north of 39 °N might have increased the gradient of an existing drainage system to the point that its valley would have been incised into the axial ridge; the deepened channels would have contained all sediment moved through the drainage system, so that 'normal' allogenic-abyssal sediments could have accumulated on the flanks of the ridge undiluted by turbidite deposits. An equally acceptable, alternate explanation for the incised valley and the accumulation of 'normal' deep-ocean sediments is uplift of the sea floor beneath the ridge, proper. If it may be further postulated that this uplift began in the north and progressed south- ward, several other major features of the area also are accounted for. The course of any major deep-sea valleys, prior to the uplift, may have been normal to the continental slope, and a thick sequence of turbidites built seaward across the continental rise. Uplift of the ridge, progressing from north to south, would have diverted the channels southward, exposing older sediments to erosion and reworking. Beyond the area of uplift the channels, once again under influence of the regional topographic gradient, would swing westward and erosional relief of the valleys would disappear. The south- eastward migration of the channels across the southern half of the ridge would account for formation of the 'cross reflections' and, particularly, for the fact that they seem to occur only to seaward of the distributary valleys (Truchan et al., 1967, p. 126). The wedge of turbidites shown in Profile AA' (Figure 2) is simply an erosional remnant covered by subsequent normal deep-ocean sediments. Tectonic activity associated with uplift of the ridge also would account for displacements of the basement, often

CONTINENTAL TERRACE AND DEEP PLAIN OFFSHORE CENTRAL CALIFORNIA 157

accompanied by distortion of overlying continuous reflectors, which are found in the middle continental rise north of 37J30'N.

The ridges which extend westward from the base of the continental slope at approx- imately 37°15'N and 37°30'N (Figure 2) enclose a basin which may be receiving little if any terrigenous sand (Uchupi and Emery, 1963, p. 427; Wilde, 1965, Figures 9-11) despite proximity to the drainage system which empties into the Pacific through the Golden Gate. Just north of the ridge at 37°05'N, the sediments are no thicker than 0.3 sec (HH', Figure 2). Along the axis of the basin, at 37°20'N, a seismic record of marginal quality (not shown) suggests a maximum of 0.6 sec and a minimum of 0.2 sec of sediment overlying an extremely irregular basement surface. At least the upper 0.2-0.3 sec of these sediments are turbidites.

D. BASEMENT TRENDS IN THE CONTINENTAL RISE

The ridges which extend westward from the base of the continental slope at 37°05'N and 37°30'N are only two of at least five topographic features with marked east-west orientation which occur on the upper continental rise north of 37 °N (Figure 2). Profile HH' (Figure 2) suggests that the ridge at 37°05'N reflects basement structure; the presence of knolls on the distal ends of the ridges at 37°45'N and 38°10'N supports the conclusion that the ridges are primarily basement structures.

Although there is no correlation between these east-west trends and the magnetic- anomaly pattern north of 37 °N (see Mason and Raff, 1961, Figure 2 ; Lattimore et al. 1968a), the ridges all seem to end at about 124°40'W, which coincides with the axis of the easternmost 'typical' deep-ocean magnetic anomaly lineation. This anomaly, whose north-south trend truncates the anomalies of the upper continental rise between 36 °N and 38°30'N, also coincides with the western flank of another low ridge (defined by the 4000-m isobath) that extends due south from approximately 37 °N to 36°30'N (Figure 2). From Profiles HH' and J J' (Figure 2), it may be seen that at least the north- ern tip of this north-south ridge reflects structural relief of the basement.

These observations suggest that there is, in fact, a relationship between the magnetic anomalies and the structure of the upper continental rise; for example, the crust may change from typical oceanic to intermediate at 124°40'W.

E. PIONEER RIDGE

The TGS seismic-reflection investigation of Pioneer Ridge was limited to a profile along the ridge at 38°50'N (AA', Figure 2) and two north-south crossings west of 130 °W (not shown). These profiles, together with those of Ewing et al. (1968, Figure 7) and Winterer et al. (1968, Figures 2-5), yield some idea of the gross structure of this feature. West of 126°W, the general level of the basement north of 38°40'N is about 0.5 sec higher than beneath the continental rise and abyssal hills to the south (compare AA' and BB', Figure 2; Winterer et al., 1968, Figures 2a-2c). The ridge which usually occurs on the southern margin of this uplifted block, west of 127°30'W, represents an additional 400 m or 0.5 sec of basement relief.

West of 127°30'W the basement associated with Pioneer Ridge can be described in

158 L. AUSTIN WEEKS AND ROBERT K. LATTIMORE

terms of short-wavelength features of low, regular amplitude, which are morphologi- cally similar to the structure of the abyssal hills (AA\ Figure 2; Winterer et al, 1968, Figure 2d). East of 127°W, relief of the basement appears to be irregular and of greater amplitude, and the pattern more nearly resembles the basement structure found beneath the middle and upper continental rise (Figure 2).

Although the 'magnetic structure' of Pioneer Ridge extends at least as far east as 127°W (Mason and Raff, 1961, PI. 1) topographic relief on the ridge does not extend beyond 127°40'W (Figure 2) and it is obvious from the profiles shown by Winterer et al. (1968, Figure 2) that the gross structure of the feature changes marked- ly, near the meridian. The bathymetric data compiled from the TGS investigation suggest that the low ridge at 126°W, defined by the 4000-m isobath, has an east- northeast trend (Figure 2), but the map prepared by Menard (Winterer et al., 1968, Figure 7) shows this ridge as being oriented almost east-west, and Winterer et al. present data in support of the idea that the feature is a continuation of the Pioneer trend.

Profile AA' (Figure 2) shows that terrigeneous sediments, mostly turbidites, extend along the north slope of Pioneer Ridge for about 300 km west of the base of the con- tinental slope. At 127°W, 0.2 sec of horizontally-stratified deposits overlie thinner, acoustically-transparent beds which are conformable with the bedrock topography. West of 127°30'W acoustically transparent sediments predominate. Between 127°30'W and 128°30'W such deposits average 0.3 sec in thickness, or about double the average thickness of pelagic sediments on the abyssal hills south of the ridge. The north-south profile of Ewing et al. (1968, Figure 7) shows that at 128°30'W these same sediments thicken to the north. These data support the hypothesis of Winterer et al. (1968, p. 518) that sediments in the northern part of the Delgada fan may be at least partially derived from north of the Mendocino Escarpment.

F. ABYSSAL HILLS

At a distance of 400-500 km from the base of the continental slope the distinctive, parabolic profiles of the abyssal hills emerge from beneath a waning cover of terri- genous sediments. Within the abyssal hills province, maximum relief is found in ridges and seamounts along the northern and eastern margins; these stand 600 m or so above the surrounding sea floor (Figure 2). Otherwise, the entire province east of 1 33 °W falls in the 4600-5400 m depth range (Lattimore et al, 1 968). Relief on individ- ual hills seldom exceeds a few hundred meters, and width along the base generally is 2.5 km or less. Slope gradients approaching 10 per cent are not uncommon.

The basement structure of the abyssal hills typically is covered by a conformable mantle of acoustically-transparent sediments, undoubtedly equivalent to the 'pelagic' sediments of Hamilton (1967, p. 4202). This mantle rarely is more than 0.15 sec thick, and zones in the southwestern part of the study area are completely devoid of per- ceptible sediments (FF', Figure 2).

As may be expected, turbidites do not vanish abruptly from the sediment column. Almost every east-west profile contains a transition zone, up to 1 50 km wide, in which basement features covered with a conforming mantle of acoustically-transparent

CONTINENTAL TERRACE AND DEEP PLAIN OFFSHORE CENTRAL CALIFORNIA 1 59

sediments rise above horizontal, stratified sediments filling adjacent lows (FF', Figure 2). Flat-floored valleys suggesting turbidite sedimentation are common through- out the area of investigation.

4. Summary

The Transcontinental Geophysical Survey seismic-reflection profiles support the hypothesis that the gross patterns of the geology of the Coast Ranges of California are present beneath the continental shelf and slope. In particular, the broad, fiat con- tinental shelf from Pigeon Point north to Cordell Bank may be attributed to the occurrence of a crystalline ridge along the edge of the shelf; Page (1966, Figure 1) has suggested that this is an extension of the Salinian block that forms the basement beneath the Coast Ranges south of Monterey Bay. The more deeply-incised continen- tal shelf and less precipitous upper continental slope south of Monterey Canyon are believed to reflect the presence of the Franciscan basement complex overlain by a sequence of folded and faulted sedimentary rocks, as also suggested by Page (1966, Figure 6). Basement blocks beneath the middle and lower continental slope, north of 37 °N, may be a continuation of the Franciscan complex.

On the continental rise south of 37 °N, the course of the Monterey deep-sea valley has been traced south and southwest from the meander at 36°15'N, 122°50'W, mapped by Shepard (1966, Figure 1). Pioneer Canyon could not be traced beyond the base of the continental slope.

Turbidites on the continental rise are characterized by near-horizontal, continuous reflectors; they tend to be concordant with the regional topographic gradient and independent of structural relief on the strata or basement beneath them. On the upper rise, south of 37 °N, these sediments form floodplain-like deposits clearly associated with the distributary system of the Monterey deep-sea valley.

Below 3800-4000 m a significant proportion of the sediment column is characterized by 'soft', discontinuous reflectors which tend to be conformable with structural relief of the basement and cannot be related to any known deep-sea valley system; in places, these strata are overlain unconformably by horizontally-stratified turbidites. While the origin of these discontinuous-conformable reflectors is uncertain, it is clear that they are not related to the present Monterey deep-sea valley system.

Turbidite deposits which are related to the Delgada deep-sea fan comprise the continental rise north of 37°30'N; turbidites cover abyssal hills east of 128°W, and extend south of 36°.N. A tongue of turbidite strata extends along the base of Pioneer Ridge at least as far west as 133°W, as shown by Menard (1964, plate). Our investiga- tions show that turbidites occur also north of Pioneer Ridge, between 126°50'W and 127°20'W.

Near 39 °N the ridge which forms the topographic axis of the Delgada deep-sea fan consists of a sequence of turbidites overlain unconformably by 0.1-0.2 sec of normal allogenic-abyssal or 'pelagic' sediments. The southern end of this ridge is made up of 'cross reflections', probably the same as those observed by Truchan et al. (1967), which we interpret as having resulted from submarine scour-and-fill or rework-

1 60 L. AUSTIN WEEKS AND ROBERT K. LATTIMORE

ing of older sediments. The ridge is incised by a valley with steep walls and a flat floor, which follows a nearly straight course southwestward across it. Although the struc- ture of this ridge implies a change in the sedimentary environment in response to tectonic activity, several alternative explanations can be offered which are consistent with the available data. The preferred explanation is that the ridge has undergone uplift progressing from north to south.

A pattern of abrupt changes in depth-to-basement, which is associated with the sedimentary ridge, could be related to epeirogenic activity. An alternate explanation is offered by Winterer et al. (1968, pp. 510-514), namely, that the structure of Pioneer Ridge extends into or beneath the sedimentary ridge.

The low east-west ridges on the upper continental rise north of 37 °N are con- sidered to be indicative of basement structure. While there is no direct correlation be- tween these trends and the magnetic anomaly pattern (Mason and Raff, 1961, Plate 2; Lattimore et al., 1968a) neither these trends nor the magnetic anomaly pattern of the upper continental rise extend west of 124°40'W - the axis of the easternmost 'typical' deep-ocean magnetic anomaly.

A broad picture of the basement structure associated with Pioneer Ridge can be drawn from our investigations, the profile published by Ewing et al. (1968, Figure 7) and the report of Winterer et al. (1968). North of 38°40'N the basement stands about 0.5 sec higher than the basement beneath the sea floor to the south. When present, the topographic ridge which runs along the southern margin of this raised block represents an additional 0.5 sec of basement relief. That this structural pattern is modified east of 127°40'W is indicated by the bathymetry as well as by the seismic-reflection inves- tigations of Winterer et al. (1968, Figure 2). The TGS data neither support nor contra- dict the inference of Winterer et al. (1968) that the Pioneer trend extends eastward from 127°40'W beneath the sediments of the Delgada fan. Our data and that of Ewing et al. (1968) do substantiate the proposal of Winterer et al. that 'pelagic' sediments on Pioneer Ridge may have been derived partially from north of the Men- docino Escarpment.

Seismic-reflection observations in the abyssal hills reveal that conformable, acous- tically-transparent 'pelagic' sediments rarely exceed 0.15 sec in thickness; in the south- western part of the area they do not appear at all.

Acknowledgements

The authors thank S. P. Perry (ESSA, Pacific Oceanographic Research Laboratories), J. M. McAlinden and C. X. G. Fefe (U.S. Coast and Geodetic Survey) and F. M. Edvalson (U.S. Naval Oceanographic Office) for providing supplementary data on the deep-sea cores and bathymetry within the TGS area. G. F. Merrill and F. P. Sauls- bury (ESSA, Atlantic Oceanographic and Meteorological Laboratories) supervised cartography and drafting of the figures. The manuscript was critically reviewed by L. W. Butler, G. H. Keller, and G. Peter (ESSA, Atlantic Oceanographic and Meteo- rological Laboratories).

CONTINENTAL TERRACE AND DEEP PLAIN OFFSHORE CENTRAL CALIFORNIA 161

References

Bums, R. E. and Grim, P. J.: 1967, 'Heat Flow in the Pacific Ocean off Central California', J.

Geophys. Res. 72, 6239-47. Curray, J. R.: 1965, 'Structure of the Continental Margin off Central California', N. Y. Acad. Sci.

Trans., Ser. II 27, 794-801. Dill, R. F., Dietz, R. S., and Stewart, H.: 1954, 'Deep-Sea Channels and Delta of the Monterey

Submarine Canyon', Bull. Geol. Soc. Am. 65, 191-94. Ewing, J., Ewing, M., Aitken, T., and Ludwig, W. J. : 1968, 'North Pacific Sediment Layer Measured

by Seismic Profiling'; 147-173 in Knopoff, L., Drake, C. L. and Hart, P. J. (eds.), 'Crust and

Upper Mantle of the Pacific Area', Am. Geophys. Un. Geophys. Mon. 12, 522 p. Hamilton, E. L.: 1967, 'Marine Geology of Abyssal Plains in the Gulf of Alaska', J. Geophys. Res.

72, 4189-4213. Heezen, B. C. and Menard, H. W.: 1963, 'Topography of the Deep-Sea Floor'; 233-280 in Hill,

M. N. (ed.) The Sea 3, New York, Interscience, 963 p. Lattimore, R. K., Bassinger, B. G., and DeWald, O. E.: 1968, 'Transcontinental Geophysical Survey

(35°-39°N) - Magnetic map from the Coast of California to 133°W Longitude', U.S. Geol. Surv.

Misc. Geol. Inv., Map I-531-A. Lattimore, R. K., Bush, S. A., and Bush, P. A.: 1968, 'Transcontinental Geophysical Survey

(35°-39°N)- Gravity and Bathymetric Map from the Coast of California to 133°W Longitude',

U.S. Geol. Surv. Misc. Geo!. Inv., Map I-531-B. Mason, R. G.: 1958, 'Magnetic Survey off the West Coast of the United States between Latitudes

32° and 36 °N and Longitudes 121° and 128°W, Geophys. J. Roy. Astron. Soc. 1, 320-29. Mason, R. G. and Raff, A. D.: 1961, 'Magnetic Survey off the West Coast of North America, 32 °N

Latitude to 42 °N Latitude', Bull. Geol. Soc. Am. 72, 1259-66. Menard, H. W. : 1955, 'Deformation of the Northeastern Pacific Basin and the West Coast of North

America', Bull. Geol. Soc. Am. 66, 1149-98. Menard, H. W : 1960, 'Possible Pre-Pleistocene Deep-Sea Fans off Central California', Bull. Geol.

Soc. Am. 71, 1271-78. Menard, H. W.: 1964, Marine Geology of the Pacific, McGraw-Hill, New York, N.Y., 271 p. Page, B. M.: 1966, 'Geology of the Coast Ranges of California', 255-76, in Bailey, E. H. (ed.),

'Geology of Northern California', Bull. Calif. Div. Mines and Geology 190, 508 p. Shepard, F. P. and Emery, K. O.: 1941, 'Submarine Topography off the California Coast: Canyons

and Tectonic Interpretation', Geol. Soc. Am. Spec. Paper 31, 171 p. Shepard, F. P.: 1966, 'Meander in Valley Crossing a Deep-Ocean Fan', Science 154, 385-86. Taliaferro, N. L.: 1951, 'Geology of the San Francisco Bay Counties', 117-50, in 'Geologic Guide- book of the San Francisco Bay Counties', Bull. Calif. Div. Mines 154, 392 p. Truchan, M., Windisch, C. C, and Hamilton, G. R.: 1967, 'Detailed Bathymetric and Seismic

Reflection Survey of a Portion of the Delgada Deep-Sea Fan and its Channel' (abs.), Am. Geophys.

Un. Trans. 48, 126-27. Uchupi, E. and Emery, K. O.: 1963, 'The Continental Slope between San Francisco, California and

Cedros Island, Mexico', Deep-Sea Res. 10, 397^147. U.S. Upper Mantle Committee: 1965, United States program for the international Upper Mantle

Project: Progress report - 1965: Washington, D.C., Nat. Acad. Sci. - Nat. Res. Council. Vacquier, V., Raff, A. D., and Warren, R. E.: 1961, 'Horizontal Displacements in the Floor of the

Northeastern Pacific Ocean', Bull. Geol. Soc. Am. 72, 1251-58. Wilde, P.: 1965, 'Recent Sediments of the Monterey Deep-Sea Fan', Univ. California (Berkeley),

Hydraulic Eng. Lab. Tech. Rept. HEL-2-13. Winterer, E. L., Curray, J. R., and Peterson, M. N. A.: 1968, 'Geologic History of the Intersection

of the Pioneer Fracture Zone with the Delgada Deep-Sea Fan, Northeast Pacific', Deep-Sea Res.

15, 509-20.

66

Reprinted from The American Association of Petroleum Geologists Bulletin 55_, No. 10, 1741-1752 .

Structural Relations Among Lesser Antilles, Venezuela, and Trinidad-Tobago1

L. AUSTIN WEEKS,3 R. K. LATTIMORE,' R. N. HARBISON,8 B. G. BASSINGER," and G. F. MERRILL3

Miami, Florida 33158

Abstract More than 2,500 n. mi (4,630 km) of seismic reflection profiling, gravity, magnetics, and bathymetric data were collected in the southeastern Caribbean by the ESSA Coast and Geodetic Survey ship Discoverer in 1968-1969.

A review of the structural geology of the southeastern Caribbean and the South American continent in conjunc- tion with the ESSA data supports a relatively simplistic explanation for the geologic structure. The Barbados Ridge is a greatly fractured anticlinorium, supported by "basement" rocks, and consisting of two parallel arches with a central syncline. The Lesser Antilles volcanic arc, the Tobago trough, and the Barbados anticlinorium are traceable into the Venezuelan and Trinidadian shelves (South American continent).

An analogy between the Caribbean and Indonesian island arcs shows the validity of the concept of continua- tion of continental mobile belts into island arc systems. The mobile belt and the island arc system are analogous manifestations of orogeny in different crustal types. Evi- dence is against wrench faulting, with its implication of vast horizontal movements of individual blocks. The island arc structural belts and the mobile belts of the continent are interrelated, gradational, and interlocked.

Introduction

In 1968 the ESSA ship Discoverer began a continuing geophysical study of the southern Lesser Antilles, the Venezuelan and Trinida- dian shelves, and the Barbados Ridge.

The primary purpose of this study is to de- termine the structural configuration of the Lesser Antilles island arc system and its rela- tion to the South American continent. Previ- ously, the senior writer and others conducted a similar study in the Andaman Sea during the International Indian Ocean Expedition in 1964 (Peter et al, 1966; Weeks et al, 1967). Simi- larities between the Andaman-Nicobar Islands and the Lesser Antilles led to a similar though expanded study of the Caribbean eastern mar- gin.

This paper is a synthesis of the ESSA data

1 Manuscript received, August 24, 1970; accepted, December 3, 1970.

2 Consultant, 13720 SW 78th Court.

'National Oceanic and Atmospheric Administration (NOAA), Atlantic Oceanographic and Meteorological Laboratories.

© 1971. The American Association of Petroleum Geologists. All rights reserved.

presented in the preceding papers in this Bulle- tin by Lattimore et al. (1971) and Bassinger et al. (1971), and of the known structural geol- ogy of the island arc system and the northeast- ern part of the South American continent. A structural analogy between the Lesser Antilles and Indonesian arcs is presented.

Ths 1969 study area was bounded by long. 58°30'-63°W and lat. 10°-12°30'N. Within that area more than 2,500 n. mi (4,630 km) were covered by seismic reflection profiling, gravimeter, magnetometer, and echo sounding observations. Additional gravimetric, magnetic, and bathymetric data were collected along vari- ous transects of the area. Figure 1 shows ba- thymetry and track lines within the study area.

Structural Belts

An interpretative cross section across the Lesser Antilles island arc system from the Ven- ezuela basin through the Aves Ridge, Lesser Antilles, Barbados anticlinorium, and interven- ing troughs (Grenada Trough, Tobago Trough, Central syncline) is shown in Figure 2. The vertical scale is exaggerated to show the struc- tural features more clearly.

Venezuela Basin

The west end of the section (Fig. 2) starts in the eastern Venezuela basin, on the west flank of the Aves Ridge. According to Edgar (1968; Fig. 3 this report), there are about 2 km (1V4 mi) of sediments, of velocity less than 5 km/ sec (3.1 mi/sec), within the central part of the Venezuela basin, thickening to about 5 km (3.1 mi) on the western flank of the Aves Ridge. Sediments are thinnest within the central part of the basin and thicken toward the flanks of the basin in all directions. Ewing et al. (1967) showed that the sediments of the Venezuela ba- sin are flat and undisturbed, indicating a lack of deformation or tectonic activity within the block. The basin as a unit has had a relatively stable tectonic history with only minor defor- mation around the edges of the plate. It is seis- mically inactive. Ewing et al. (1967) con- cluded that stability of the Caribbean subbasins

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seems to preclude sea-floor spreading or hori- zontal movement, implying rather a dominant role of vertical movements instead.

Aves Ridge

The Aves Ridge is considered to be part of the island arc system, as its gross characteristics relate more to the arc than to the Venezuela basin. Sediments on the east flank of the ridge plunge unconformably beneath younger turbi- dites of the Grenada Trough (Edgar, 1968). The unconformable relation between older folded beds and younger relatively flat-lying de- posits is characteristic of the basinal areas of the double island arc system (Fig. 2). In addi- tion, the Carib beds of the Venezuela basin are not identified east of the western flank of the Aves Ridge. These sediments are the deep-wa- ter deposits identified over much of the Carib- bean west of the Aves Ridge (Ewing et al., 1967).

Bunce et al. (1970) showed a generalized crustal structure section from the Venezuela basin to the Atlantic Ocean. The crust thickens considerably in the eastern Venezuela basin, under the Aves Ridge and the rest of the island arc system, and does not thin again until the Atlantic Ocean is reached. Aves Ridge is, there- fore, part of the thickened crust of the island arc system. Depth to mantle is roughly the same in the eastern Venezuela basin and the Atlantic Ocean, just east of the Barbados Ridge or anticlinorium.

The Aves Ridge is aseismic, nearly neutral in gravity, and approximately enclosed by the 1,000-fm (1,830 m) isobath. The only segment of the ridge above sea level is Aves Island, a

small, low 3-m (9.9 ft) maximum feature cov- ered by calcareous sediments. Bedding strikes N70E, and dips toward the north and south (Maloney et al., 1968). This strike is subparal- Iel with strikes normal to the arc system found in Barbados and Grenada (Lesser Antilles). Dredging on the ridge has produced basalt (Hurley, 1966), glassy flows and brecciated rocks of possible eruptive origin (Marlowe, 1968), and much granite (recent cruise of R/V Eastward). The latter cruise dredged over 2 tons of light-colored granitic rocks from more than 50 locations along the ridge.

Aves Island has been decreasing slowly in size since the last century, and a slow epeiro- genic subsidence of the whole ridge may be in- dicated. Such subsidence after positive eleva- tion in tectonic trends is quite widespread (e.g., Weeks et al., 1967).

Grenada Trough

East of the Aves Ridge is the Grenada Trough (Fig. 2). Sedimentation in the Grenada Trough is distinct from that in the Venezuela basin. From the Grenada Trough eastward, flank sediments off the positive areas dip be- neath the relatively flat sediments of the inter- vening Grenada and Tobago Troughs (negative areas within Barbados anticlinorium). The deeper parts of the Grenada Trough are east of the structural axis of the basin; therefore, asymmetry is eastward, toward the Atlantic Ocean. The unconformity between flank sedi- ments dipping into the trough and the younger flat-lying beds is typical of the negative areas in the arc system. Edgar (1968; Fig. 3, this re- port) shows 4-7 km (2.5-4.4 mi) of sedi- ments, a greater thickness than in the Venezu- ela basin.

Volcanic Arc

The volcanic arc of the Lesser Antilles forms a long graceful curve, convex toward the At- lantic. The arc is also asymmetric, with topo- graphic slopes steeper on the west.

Volcanic activity in the Lesser Antilles has continued into recent geologic time, whereas it ceased in the Greater Antilles (except Hispanio- la [MacDonald and Melson, 1969] during the Eocene (MacGillavry, 1970). MacGillavry considered that this cannot be explained by a quiescent episode of ocean-floor spreading. Ac- cording to Lewis (1968, p. 44-45) the "Basal- tic rocks occurring in the Lesser Antilles are directly comparable to chemical composition and mineralogy with basalts from other circum-

Lesser Antilles, Venezuela, and Trinidad-Tobago

1745

oceanic islands and from orogenic belts on the continental margins. Basalts of this type, characterized by a high alumina and low alkali content, are distinct from olivine tholeiites of the ocean basins and from alkali basalts of the intraoceanic islands."

Earle (1924, 1928), describing the southern Antilles, mentioned folding in Grenada that is approximately east-west, similar to strikes found on Aves Island, Barbados, and Trinidad. More recently, Martin-Kaye and Saunders (1962) described an upper Eocene sedimentary series (Tufton Hall Formation) in northern Grenada. The series consists of several hundred feet of folded, repetitively bedded graywacke and shale, with a fauna suggesting deposition at bathyal depth. It is tempting to correlate these deposits with the lower Scotland Group of Bar- bados (Baadsgaard, 1960), also considered to have been deposited at bathyal depth and folded with a pronounced northeast-southwest strike. Marine limestone at 180 m (600 ft) of elevation attests to later epeirogenic uplift in Grenada.

The most volcanically active segment of the arc is near the center, as the most recent vol- canism is restricted to that part. The synchro- nous eruption of Soufriere (St. Vincent) and Pelee (Martinique) in 1902 indicates a deep common origin.

Seismically, the Lesser Antilles overlie a zone of intermediate depth earthquakes (Sykes and Ewing, 1965). Most of the hypocenters are confined to a zone about 50 km (31 mi) wide, dipping about 60 °W.

Tobago Trough

East of the volcanic arc is the Tobago Trough, whose surface is about 500 fm (915 m) shallower than the Grenada Trough (Fig. 2). The trough is elliptical, asymmetrical toward the east, with the deeper parts near the Barba- dos anticlinorium (Fig. 1). The topographic axis is east of the structural axis, which contin- ues southwest, depressing the Paria shelf (Figs. 1, 3). The total area of the Tobago Trough, even including the part on the Paria shelf, is less than half that of the Grenada Trough. This is a result of its termination on the north by a structural feature, herein termed the "St. Lucia- Barbados cross-warp" (Fig. 5).

The ESSA data indicate that younger, rela- tively flat-lying sediments unconformably over- lie folded sediments which plunge under the Tobago Trough from both sides. Major contri- bution of sediment is from the south and per-

ANDAMAN SEA

, MOBILE BELTS

(Continent) 5 4 3 2 1

CARIBBEAN SEA

Fig. 4. Double island arc system structural belts as seen in Andaman Sea (Indonesian Arc) and Eastern Caribbean (Lesser Antilles). See Table 1 for descrip- tion of specific belts. Belts: 1. stable platform; 2. back- deep; 3. inner volcanic arc; 4. interdeep; 5. outer sedi- mentary arc and/or foredeep (trench).

haps southeast, with smaller amounts from the Lesser Antilles. Sediment thickness exceeds 10 km (6.2 mi, Fig. 3). Minimum thickness of sediments of similar velocities is 4 km (2.5 mi) at the southwest end of the Paria shelf, just off the Araya-Paria Peninsulas (Pilar block), reaching the maximum of more than 10 km (6.2 mi) on the northeast, just west of, and in- cluding Barbados. Tobago Trough sediments are now more than five times as thick as those in the Venezuela basin, having thickened grad- ually eastward across the island arc system (Fig. 3).

Barbados Anticlinorium

The Barbados anticlinorium was described earlier as a double ridge with a central syncline or trough. The Central syncline surface is somewhat above the general level of the To- bago Trough. However, the Tobago Trough is larger than the Central syncline in areal extent and volume. Sediment isopachs based on re- fraction data are oriented approximately east- west, with thickening northward toward Barba- dos (Fig. 3).

The inference of a southern source of supply for Barbados and the Tobago Trough is strong. East-west structural lineations in the Pilar block, and in some structures on Barbados it- self, parallel the isopachs in every respect.

The seismic profiles suggest that the base- ment of the West ridge (Barbados anticlino-

1746

Weeks, Lattimore, Harbison, Bassinger and Merrill

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Lesser Antilles, Venezuela, and Trinidad-Tobago

1747

rium) plunges northward under the island of Barbados, a plausible phenomenon in view of the northward thickening of sediments (Fig. 3). The folded sediments of the East ridge and of the generally higher West ridge also plunge un- der the younger flat-lying sediments of the Cen- tral syncline.

Thus, the section from the Venezuela basin across the Barbados anticlinorium (Fig. 2) shows essentially a typical double island arc system. At the west is the Venezuela basin; at the east, the Atlantic basin; the apex is at the inner volcanic arc of the Lesser Antilles. Even where the outer sedimentary arc ceases to exist north of the Barbados anticlinorium, alternation of positive and negative structures prevails. Basins and ridges are approximately equidistant in their spacing. The Barbados anticlinorium is at about the same distance from the Lesser An- tilles as the Aves Ridge. One cannot but believe that an overall pattern of structural "waves" is involved in the development of this double arc.

Island Arc Structure, Development, and Analogies with Indonesian Arc

A structural development very similar to that of the Caribbean island arc was noted in the Indonesian island arc by Weeks et al. (1967) and a direct comparison can be made (Fig. 4). The Indonesian arc in the Andaman Sea area and the Lesser Antilles arc of the eastern Ca- ribbean are both double arc systems, in that both inner volcanic and outer sedimentary arcs are represented. The terminology used by the senior Writer in the Andaman Sea, following that of van Bemmelen (1949), is equally appli- cable to the eastern Caribbean (Fig. 4; Table 1). Its advantage lies in its simplicity of terms, which are self-explanatory.

Both the Indonesian and Lesser Antilles is- land arc systems are characterized by inner vol- canic arcs, outer sedimentary arcs, backdeeps, interdeeps, and foredeeps present or former

Abbreviations :

CR = Curacao ridge

G =Grenada Is.

LR =Los Roques Is.

SL-B =St. Lucia-Barbados cross-warp

0=Orchila Is.

B = Barbados Is.

C = Caracas

To =Tobago Is.

Bl =Blanquilla Is.

NTA = North Tobago anticline

LH =Los Hermanos Is.

ETS =East Tobago syncline

A =Aves Is.

WR =West ridge

M =Margarita Is.

CS =Central syncline

LF=Los Frailes Is.

ER =East ridge

LT = Los Testigos Is.

trenches (Fig. 4). Table 1 lists the similarities in structure and gravity of the several arcuate belts in both the Andaman Sea and the eastern Caribbean.

The pattern of development in an island arc system is one of growth toward the ocean plate, not only normal to the arc but, in certain re- spects, also axially. Growth in both directions, normal and axial to the arc, occurs over a con- siderable period of time, or a diastrophic cycle. The cycle includes periods of orogeny and epeirogeny, as well as relaxation and/ or exten- sional collapse. In the sense that double arcs are continuations of continental orogenic belts, the axial growth is quite evident, but axial growth within the outer island arc-foredeep belts of the system proper is becoming increas- ingly apparent. Axial growth explains the dual roles and interrelations between the outer sedi- mentary arc and the foredeep or trench (belt 5, Fig. 4).

The development of the outer sedimentary arc is of greatest interest in defining the interre- lations not only of the outer sedimentary arc with the foredeep or trench, but also of the outer arc-foredeep with the orogenic belt of the continent. It is the key to the interlocking rela- tion between the continental crust and the in- termediate or oceanic crust. It is a mutual rela- tion that is gradational in nature axially, rather than normal to the arc system.

The writers believe that a double island arc system is a continuation of a continental mobile belt. In the Indonesian arc the orogenic belt of the Himalayas-Arakan Yoma (western Burma) continues by gradation into the Indian Ocean via the Andaman-Nicobar-Mentawai islands, or the outer sedimentary arc. At the distal end of the outer island arc the foredeep or trench be- comes prominent (belt 5, Fig. 4). As shown in Table 1, the outer island arc is most completely developed where the foredeep is not and, con- versely, the foredeep is best developed where the outer island arc is not. It is apparent that one cannot develop except at the expense of the other; hence, they must be mutually interre- lated and gradational. The outer arc is the posi- tive manifestation of the foredeep (negative feature). Both the foredeep and the outer island arc contain sedimentary rocks. Abyssal deposits of Barbados, the Oceanic Group (Baadsgaard, 1960), are testimony to the earlier foredeep na- ture of the outer arc in that area. In addition, the Eocene deposits in Barbados are flyschlike turbidites laid down under submarine condi- tions. The Eocene sediments of the Andaman-

1748

Weeks, Lattimore, Harbison, Bassinger and Merril

Table 1. Double Island Arc System Belts (See Fig. 4)

Area

E. Caribbean

Andaman Sea

1 . Stable platform

(a) plate from which arc system radiates

(b) formerly involved in arc system, but now stable area

2 . Backdeep

(a) basin behind, or on concave side of inner volcanic arc

(b) part of arc system farthest from ocean plate

3. Inner volcanic arc

(a) positive gravity

(b) intermediate earthquake belt

(c) older feature than outer sedimentary arc

(d) asymmetry toward ocean plate

4. Interdeep

(a) between outer sedimentary arc and inner volcanic arc

(b) absent where no outer arc present

5 . Outer sedimentary arc

(a) negative gravity

(b) occurs near continental end of island arc

(c) found where trench is absent or buried

(d) youngest feature of arc system

(e) asymmetry toward ocean plate

(f) folded, faulted, and thrusted

(g) shallow earthquake belt

(h) structural history closely related to forcdeep

6 . Foredeep (or Trench)

(a) frontal to outer arc, where present, or to inner volcanic arc

(b) negative gravity, where outer arc absent

(c) trench where frontal to inner volcanic arc

(d) youngest part of arc system

(e) occurs along axis of outermost arc system farthest from continent

(f) least expression where frontal to outer arc (older); most expression where frontal to inner volcanic arc (younger)

(g) shallow earthquake belt

Venezuela basin piate and Aves Ridge

Grenada Trough on concave side of inner volcanic arc

Lesser Antilles

Tobago Trough

Barbados anticlinorium

Depressed structural belt just in front of Barbados anticlinorium

Malay Peninsula

Andaman Sea area on concave side of inner volcanic arc

Barisan Range (Sumatra)- Narcondam and Barren Islands

Negative structural belt between Andaman-Nicobar Islands and Barisan-Narcondam-Barren arc

Andaman-Nicobar-Mentawai Islands

Depressed structural belt just in front of Andaman-Nicobar- Mentawai Islands

Nicobar outer arc grade from coarse terrestrial deposits on the continental end of the belt near- est Burma to marine carbonates on the distal end of the outer arc. Infill and attendant facies changes take place from the continental end of the arc to the distal end. Hurley (1966), refer- ring to his work in the Aleutian Trench, pointed out a similar situation there.

In Indonesia the continuation of the conti- nental orogenic belt through the outer sedimen- tary arc is uninterrupted. However, in the southeastern Caribbean the Pilar block acted in some degree as a rigid wall. Toward the eastern end of the Pilar block, rigidity appears to de- crease, and it is there that the outer sedimen- tary arc manifests itself. The analogy between the Indonesian arc and eastern Caribbean is still good, if one accepts the fact that the Pilar block is an exception to the general rule. This block is an old geologic feature which has be- come involved in a much younger orogenic belt-island arc development, and therefore it has acted as a partial deterrent to the more nor-

mal gradation, such as that in Indonesia and elsewhere.

The outer arc-foredeep relation is not contin- uous in the axial sense, but more en echelon, with some overlap of two structures (belt 5, Fig. 4). In both Indonesia and the eastern Ca- ribbean it can be seen that the distal end of the outer sedimentary arc lies within or concave to the foredeep (Fig. 4). There is evidence of a buried foredeep lying outside the Andaman-Ni- cobar chain (Weeks et al., 1967), a great dis- tance from its more obvious expression as the Java trench. The en echelon expression or par- tial overlap of the two features is explained by the fact that the arc system is growing not only axially but also normal to the arc. Infill and ele- vation of the foredeep into an outer arc from the continental end are closely related to its con- current development normal to the arc and to- ward the ocean basin. Undoubtedly, the devel- opment normal to the arc demands a much greater period of geologic time than axial infill and elevation. Hence, the two are still mutually

Lesser Antilles, Venezuela, and Trinidad-Tobago

1749

interrelated, but development in two directions creates the en echelon or overlap effect.

The en echelon effect of complete island arc systems is very evident in the western Pacific- Asian region. Arcs overlap, are concentric with each other, bifurcate, and may even be super- imposed. Tectonic trends on the Asian conti- nent exhibit remarkable proximity in some arcs, without major fracturing.

In summary, the double arc grows in two di- rections— normal (toward the ocean basin), and axial to the arc. Axial growth is from the continental end (mobile belt) of the outer arc toward its distal equivalent, the foredeep. The foredeep is, therefore, a younger structure than the outer sedimentary arc. Normal to the arc, the youngest feature is the outer arc or fore- deep (belt 5, Fig. 4), and the oldest features are the backdeep and stable plate (belts 1, 2; Table 1, Fig. 4).

Tectonic Map and Interpretation

A tectonic map of the southeastern Carib- bean and adjacent areas is shown in Figure 5. It is based on marine data from ESSA and other sources, and on the geology of the conti- nent and certain islands.

The simplistic approach in the tectonic map reflects the view that the geologic history of this area can be explained without recourse to vast horizontal wrench faults or differential plate movements. Continuation of double island arc system belts into continents has been substanti- ated (Indonesian, Aleutian, Scotian, and Antil- lean). The arc belts have in places modified the structural trends of the continental margin, as on the Paria shelf.

It was noted in reviewing the geologic litera- ture that the prevalence of cross trends in the arc system appeared to be the rule rather than the exception. These trends are more or less at right angles or normal to the arcs, and include not only faults but folds and even thrust faults. A summary of the cross trends found in the lit- erature includes the following.

1. A fracture zone at the southeastern limit of the Los Roques Trench, north of the Nether- lands Antilles, curves sharply across the inter- rupted arc of the Aves Ridge-Netherlands An- tilles. The axis of the Eastern Venezuela basin makes a double change in trend just south of the southeastern terminus of the Los Roques Trench, and suggests the existence of a cross trend of some type, approximately at right an- gles to the coast near Barcelona, Venezuela.

2. Northwest-striking cross fractures, nor-

mal to the arc, occur in the Los Testigos Is- lands, which the ESSA data show to be a con- tinuation of the Lesser Antilles inner volcanic arc. The islands consist of granites and volcanic rocks, Testigo Grande being a granitic intrusive body, bordered by younger volcanic rocks (Maloney, 1967). The Los Frailes Islands, along the same arc between Margarita and the Testigos, are a northwest-trending en echelon set of islands parallel with the eastern coast of Margarita.

3. The Los Hermanos Islands, just east of La Blanquilla Island, are oriented somewhat normal to the trend connecting the Blanquilla- Hermanos platform and the Aves Ridge. A sea- mount, 13 n. mi (24 km) southwest of La Blanquilla, also is oriented northwest-southeast, normal to the major trend. A basin between the seamount and the island of La Blanquilla like- wise has a northwest-southeast orientation (Maloney, 1966, 1968).

4. Aves Island, the only part of the ridge above sea level, is arched with an axis approxi- mately N70°E, and dips north and south (Ma- loney et al., 1968). This general east-west ori- entation has been noted by prior workers.

5. The folds and thrusts exposed in eastern Barbados are oriented more or less east-west, normal to the outer island arc trend. The St. Lucia-Barbados cross-warp, whatever its true nature, also is normal to the arc trend.

6. In Grenada, the southernmost island of the Lesser Antilles, several anticlines and syn- clines have fold axes in an approximately east- west direction. These folds cross the arc trend, and are similar to those in Barbados.

7. Tobago Island consists of isoclinally folded schist and phyllite in the northern third of the island. These trends are east-northeast, contrary to the northeast strike of the island.

Undoubtedly many other examples exist, but those listed are sufficient to emphasize the fact that cross fractures and/ or folds are far from uncommon.

The type of movement that has occurred along the El Pilar fault zone is very important in solving the tectonics of the region. The writ- ers consider movement along the El Pilar and the northern fault zones to have been primarily vertical, and if any horizontal movement has occurred, it is relatively minimal. Vast horizon- tal movement of the magnitude of hundreds of miles is not supportable by field data.

1. Work by Potter (1968) shows that much of the literature has been theoretical, based on previous lack of field investigations. His map-

1750

Weeks, Lattimore, Harbison, Bassinger and Merrill

ping in the Northern Range of Trinidad has provided data for examining movement on the El Pilar fault. Evidence is good for vertical dis- placement of up to 6,000 ft (1,830 m) on the El Pilar and on the Brasso Seco faults, but there is no evidence for lateral movement. In addition. Potter noted that lateral movement since late Pliocene is not suggested by the posi- tions of buried Plio-Pleistocene alluvial fans.

2. ESSA data from the Dragon's Mouth east to 59°W merely indicate a very clean high-an- gle to vertical break, between the Pilar block and the sediments on the south (Bassinger et al., 1971 ). Lack of a wide gouge zone, expecta- ble in a wrench fault, is quite conclusive. Al- though the near-vertical trace of the fault at the surface is indicated, it is not unlikely that the plane of the fault at depth may become shal- lower and dip north, as shown in published cross sections of Trinidad's structure (Kugler, 1961). At least this type of fault is consistent with other field data in Trinidad. The ESSA data further indicate the possibility that the El Pilar fault either becomes deeply buried or ceases to be a fracture east of 58°30'W.

3. Detailed field work along the El Pilar fault by Metz (1964) in the central Araya-Pa- ria Peninsulas provides the evidence against large-scale strike-slip displacement, (a) The Cutacual Formation (Lower Cretaceous), only locally developed, crops out on both sides of the fault; this facies does not occur elsewhere, and therefore cannot have been displaced; (b) the same light-colored facies of the San Anto- nio Formation (Upper Cretaceous) also is found on either side of the fault, suggesting de- position in the same lithic province; and (c) the east-northeast-trending belt of the upper Cantil Formation (Lower Cretaceous) contin- ues across the fault into the metamorphic belt on the north. Metz considered that, if any wrench faulting has taken place, it is minor, and recently (personal commun) Metz has even further reduced his estimate of wrench movement to 5 km (3.1 mi) or less.

4. The El Pilar and the now discounted Southern Caribbean faults have been consid- ered as logical zones for possible right-lateral wrench movement. However, as Mencher (1963, p. 84, 85) pointed out in reference to the El Pilar, the actual field evidence for such extensive faulting and movement in Venezuela is limited and very little surface evidence of the fault exists in Trinidad. The age of the origin of the fault is uncertain, but some of the move- ment must be post-Cretaceous, as Cretaceous

rocks are affected, but Miocene to Holocene sediments overlapping the fault are not. Mencher concluded that, if such faults were not pre-Tertiary, they could not have played an important part in much of the tectonic history of Venezuela.

It is concluded that the El Pilar is no more than a vertical displacement fault, possibly a high-angle thrust at the surface, which contin- ues east to about 58°30'W. It may continue even farther, but is either deeply buried or be- comes inactive toward the east. If the El Pilar changes its east-west trend and becomes the frontal fault of the Barbados anticlinorium, it would indicate a reactivation of the fault as part of the arc system. This also would mean that the mobile belt continued around the east- ern end of the Pilar block.

An analysis of the tectonic map (Fig. 5) shows two overall trends which have interacted. The old east-west trend, exemplified by the Pi- lar block and El Pilar fault, has somewhat modified and directed the arcward continuation of the continental mobile belt, with a trend more north than due east, into the island arc system. The fold and fault trends south of the Pilar block have an east-northeast trend and terminate against the block. The trends on the north have a similar east-northeast trend and terminate against the block at their southwest- ern ends; some are subparallel with the block. The general strike of the folds is, therefore, ap- proximately the same north and south of the block. Only at the extreme west end of the Pi- lar block do trends continue around it, and it is possible that the same is true at the east end of the block.

Several extensional collapse features along the Pilar block are indicated, particularly in the Cariaco basin and the Dragon's Mouth. The abrupt turn in the southeastern part of the Los Roques Trench, the collapse of the Cariaco ba- sin, and the abrupt twists in the axis of the Eastern Venezuela basin near 65 °W long, sug- gest the presence of a possible tectonic cross feature. West of 66°W long, the strike of the coastal features is compatible with the merger of the continental orogenic belt-island arc sys- tem. The trends interrupted by the southeastern end of the Los Roques Trench continue west for some distance before merging with the oro- genic belts of western Venezuela and Colombia (west of Fig. 5). The Pilar block seems to lose its identity, or to become involved in the trend of the merged orogenic systems from Caracas westward.

Lesser Antilles, Venezuela, and Trinidad-Tobago

1751

Fold and fault patterns south of the Pilar block indicate the probability that three seg- ments of the block once stood higher in eleva- tion, resulting in gravity-slide thrusting toward the southeast. These three areas are the Caracas (Caribbean Ranges), Cariaco (Araya-Paria Peninsulas), and North Range (Trinidad) areas. Sliding toward the southeast, normal to the folding, is suggested most strongly south of these three localities. Considerable thrusting is found in northern Guarico state, Venezuela, south of Caracas; the Serrania del Interior, south of Cariaco; and throughout Trinidad, south of the Northern Range. Wrench faults, of limited displacement, such as the Los Bajos fault of southwestern Trinidad, also occur in the Serrania del Interior, possibly merging into southeastward-directed thrusts at their limits. These faults are found south of the potentially higher areas. The high areas were undoubtedly much reduced by erosion prior to development of more recent phases of the arc system off- shore.

Summary

The results obtained during this study, in conjunction with the known structural geology of the region, show the following.

1. Sediments flanking the positive ridges of the southeast Caribbean island arc system are overlain unconformably by relatively undis- turbed beds in the intervening troughs. In the Tobago Trough and the Central syncline (Bar- bados anticlinorium), an unconformity sepa- rates the folded strata of the positive elements from the flat-lying younger beds of the negative elements. Considerable elevation of the outer parts of the arc has occurred since folding ceased, as shown by the presence of reefs on Barbados at an elevation of 1,100 ft (336 m) above sea level. A period of folding was followed by one of epeirogeny.

2. Several cross features, normal to the trend of the arc system, appear to be quite common. Collapsed areas, such as in the Drag- on's Mouth and the zone between the Grenada platform (Lesser Antilles) and Testigos-Mar- garita platform, occur within the area of study.

3. The Barbados anticlinorium, or outer sed- imentary arc of the island arc system, is a fea- ture consisting of two positive elements (West and East ridges), separated by a negative ele- ment (Central syncline). "Basement" rocks support the two ridges and lie more than 1.5 sec of acoustic penetration below the Central syncline. Other subsidiary or modifying fea-

tures, such as the North Tobago anticline and the East Tobago syncline, belong to the folded and faulted outer sedimentary arc.

4. The Lesser Antilles, or inner volcanic arc, is traceable onto the Paria shelf, continuing into the Testigos-Margarita platform. The con- tinuation is confirmed by seismic reflection pro- filer and gravity data, but not by the bathyme- try.

5. The Tobago Trough extends across the Paria shelf, depressing it with a large volume of sediments. The trend appears to end subparallel with the Pilar block. This observation is sup- ported by seismic-reflection profiling, bathyme- try inside the 100-fm (183 m) isobath, and re- fraction data. Evidence for a southern source of sediments both for the trough and Barbados is very strong.

6. Evidence shows that the Pilar block is an old structure which has partly modified the junction of the island arc system with the conti- nent. The block is essentially a horst, bounded on the north and south by fault zones. The northern fault zone is traceable from the west- ern end of the Araya Peninsula to the edge of the eastern Trinidadian shelf, where it cannot be distinguished from the fracture system at the junction of the East ridge and the Pilar block. In all likelihood, the fault zone north of the Pi- lar block consists of a series of en echelon frac- tures. Although the individual faults may strike east-northeast, the fault zone strikes essentially east-west. The El Pilar is traceable farther east, because a "basemenf'-sediment contact is easy to detect seismically. It is traceable east to 58°30'W, although there is considerable ques- tion as to whether it continues as a fault, be- cause it may be deeply buried by sediments from the south.

Both the El Pilar and northern fault zones may cross the Cariaco basin and be present north and south of the coastal ranges near Ca- racas. This would be the most logical projec- tion, and Figure 5 reflects this inference.

7. The evidence in the southeastern Carib- bean does not support the concept of wrench faulting, with its implication of vast horizontal movements of individual blocks. The Southern Caribbean fault, long hypothesized as the southern margin of the Caribbean plate, simply does not exist. Nor is the EI Pilar a wrench fault, inasmuch as most field data show its movements to have been vertical with only a small wrench component.

8. The structural geology of the region can be explained in a simplistic manner. The island

1752

Weeks, Lattimore, Harbison, Bassinger and Merrill

arc structural belts and the mobile belts of the continent are interrelated, gradational, and in- terlocked.

9. An analogy between the southeastern Ca- ribbean and the Andaman Sea arcs shows the logic in an extension of a continental mobile belt into an island arc system. Except for the modifying influence of the Pilar block, the two island arc systems are surprisingly similar.

References Cited

Baadsgaard, P. H., 1960, Barbados, W. L: exploration results 1950-1958, in Structure of the earth's crust and deformation of rocks: 21st Internat. Geol. Cong. Rept., Copenhagen, pt. 18, p. 21-27.

Bassinger, B. G., R. N. Harbison, and L. A. Weeks, 1971, Marine geophysical study northeast of Trini- dad-Tobago: Am. Assoc. Petroleum Geologists Bull., v. 55, no. 10, p. 1730-1740.

Bunce, E. T., J. D. Phillips, R. L. Chase, and C. O. Bowin, 1970, The Lesser Antilles arc and the eastern margin of the Caribbean Sea: Woods Hole Oceanog. Inst. Contrib. 2288, 36 p.; in press, in A. E. Max- well, ed., The sea, v. 4: New York, Wiley Tntersci- ence.

Earle, K. W., 1924, Geological survey of Grenada and the (Grenada) Grenadines: St. George's, Grenada, Govt. Printing Office, 9 p.

1928, Report on the geology of Saint Vincent

and the neighbouring Grenadines: Kingston, Ja- maica, Govt. Printing Office, 65 p.

Edgar, N. T., 1968, Seismic refraction and reflection in the Caribbean Sea: Ph.D. thesis, Columbia Univ., 163 p.

J. I. Ewing, and J. Hennion, 1971, Seismic re- fraction and reflection in Caribbean Sea: Am. Assoc. Petroleum Geologists Bull., v. 55, no. 6, p. 833-870.

Ewing, J. I., M. Talwani, M. Ewing, and T. Edgar, 1967, Sediments of the Caribbean: Internat. Conf. Tropical Oceanog. Proc, Miami Univ., 1965, p. 88- 102.

Hurley, R. J., 1966, Geological studies of the West In- dies: Canada Geol. Survey Paper 66-15, p. 139— 150.

Kugler, H. G., 1961, Geological map of Trinidad and geological sections through Trinidad: pub. for Petro- leum Assoc. Trinidad, Zurich, Orell Fussli, and Lon- don, E. Strand.

Lattimore, R. K., L. A. Weeks, and L. W. Mordock, 1971, Marine geophysical reconnaissance of con- tinental margin north of Paria Peninsula, Venezuela: Am. Assoc. Petroleum Geologists Bull., v. 55, no. 10, p. 1719-1729.

Lewis, J. F., 1968, Composition, origin and differentia-

tion of basalt magma in the Lesser Antilles (abs.), in Abstracts of papers: 5th Caribbean Geol. Conf., Virgin Islands, July 1-5, 1968, p. 44-45.

MacDonald, W. D., and W. G. Melson, 1969, A late Cenozoic volcanic province in Hispaniola: Carib- bean Jour. Sci., v. 9, nos. 3-4, p. 81-90.

MacGillavry, H. J., 1970, Geological history of the Ca- ribbean: Nederlandse Akad. Wetensch. Proc, ser. B, v. 73, no. 1, p. 64-96.

Maloney, N. J., 1966, Geomorphology of continental margin of Venezuela, pt. 1, Cariaco basin: Univ. Oriente, Inst. Oceanog. Bol., v. 5, no. 1, 2, p. 38-53.

1967, Geomorphology of continental margin of

Venezuela, pt. 2, Continental terrace off Carupano: Univ. Oriente, Inst. Oceanog. Bol., v. 6, no. 1, p. 147-155.

C. Shubert, J. I. Marlowe, and A. T. S. Ramsay,

1968, Geology of Aves Island, Venezuela (abs.), in Abstracts of papers: 5th Caribbean Geol. Conf., Vir- gin Islands, July 1-5, 1968, p. 50-51.

1968, Geology of La Blanquilla Island with

notes on Los Hermanos Islands, eastern Venezuela (abs.), in Abstracts of papers: 5th Caribbean Geol. Conf., Virgin Islands, July 1-5, 1968, p. 49-50.

Marlowe, J. I., 1968, Geological reconnaissance of parts of Aves Ridge (abs.), in Abstracts of papers: 5th Caribbean Geol. Conf., Virgin Islands, July 1-5, 1968, p. 51-52.

Martin-Kaye, P. H. A., and J. B. Saunders, 1962, An upper Eocene formation in Grenada, West Indies (abs.): 3d Caribbean Geol. Conf. Prog., Kingston, Jamaica, p. 29-30.

Mencher, E., 1963, Tectonic history of Venezuela, in Backbone of the Americas: Am. Assoc. Petroleum Geologists Mem. 2, p. 73-87.

Metz, H. L., 1964, Geology of the El Pilar fault zone, state of Sucre, Venezuela: Ph.D. thesis, Princeton Univ., 102 p.

Peter, G., L. A. Weeks, and R. E. Bruns, 1966, A re- connaissance geophysical survey in the Andaman Sea and across the Andaman-Nicobar Island arc: Jour. Geophys. Research, v. 71, p. 495-509.

Potter, H. C, 1968, Faulting in the Northern Range of Trinidad (abs.): 23d Internat. Geol. Cong. Rept., Prague, p. 95.

Sykes, L. R., and M. Ewing, 1965, The seismicity of the Caribbean region: Jour. Geophys. Research, v. 70, p. 5065-5074.

Tomblin, J. F., 1968, Geochemistry and genesis of Lesser Antillean volcanic rocks (abs.), in Abstracts of papers: 5th Caribbean Geol. Conf., Virgin Is- lands, July 1-5, 1968, p. 74-75.

van Bemmelen, R. W., 1949, The geology of Indonesia, v. 1A: The Hague, Govt. Printing Office, 732 p.

Weeks, L. A., R. N. Harbison, and G. Peter, 1967, Is- land arc system in Andaman Sea: Am. Assoc. Petro- leum Geologists Bull., v. 51, no. 9, p. 1803-1815.

67

Reprinted from Proceedings of the Miami Workshop on Remote Sensing, March 29-31, 1971, 133-148.

STUDIES OF OF SOLAR

CLOUD AND SATELLITE PARAMETERIZATION IRRADIANCE AT THE EARTH'S SURFACE

Ki rby J . Hanson

National Oceania and Atmospheric Administration Atlantic Oceano graphic and Meteorological Laboratories

Miami, Florida

INTRODUCTION

Whe uate the this can during t During t (mostly cent of however , surface figures at Swan on the d only 1 . 2 the type for para

n cloud

i r r a d i

be see

he four

hese mo

cirrus)

that re

the at

is very

1 and 2

I si and

ay with

percen

of cl o

meteri z

s are ance n fro -mon t nths , but c e i v e tenua

1 ow .

whi c ( C a r i

deep t of u d i n e i ng s

thin by on m sol h per the a

yet d on ti on An h sho bbean

trop the c ss as urf ac

(sue ly a ar i r iod f verag the s cl ear is la examp w the )• T i cal 1 ear-

wel 1 e i rr

h as c i smal 1 a r a d i a n c rom Sep e s ky c o 1 a r i r

days . rge and le of t

sol ar he inte con vect day val

as the adi ance

rrus ) t moun t . e data tember- overage r a d i a n c When c the i r his is i r r a d i a prated ion ( 0 c ue (Oct amount

hey te An ex at Can Decemb was 1 e was 1 ouds radian i 1 lust nee on daily tober ober A is i m

nd to atten ample of ton I s 1 and er, 1960. 0/10th 85-90 per- are thick , ce at the rated in

two days i r r a d i a n c e 30 ) was ) . Thus , portan t

133

(1968) to apply to Canton Island: 1. Q = Q

Q = Q,

Q = Q,

Q = Q,

Q = Q,

Q - Q,

Q Q

(1 .0-0. 71 C) (Kimball . 1928)

(0.803-0. 304C-0.458C2) (Back, 1956)

(1-0.655C) (Savino-Angstrom

(Budyko, 1956))

(1-0.39C-0.38C2) (Berliand, 1960)

(l-0.0006Ct3) (Laevastu, 1960)

(1-0. 0895C+0. 00252a' ) (Tabata, 1964)

A

0. 884-0. 552C ) op

(Quinn, 1969)

where : Q

Q,

!A

op

a1

total incoming solar irradiance,

total incoming solar irradiance with a clear sky,

total solar irradiance on a horizontal surface at the top of the atmosphere,

proportion of sky covered with clouds (0-1.0),

cloud cover in tenths (1-10),

cloud amount in Oktas (1-8),

proportion of sky covered with opaque clouds (0-1.0),

midmonth solar altitude in degrees.

Oct. U, 1^66 - 670(cal/cm2) Oct. 30, l<) 66 - 8(cal/cm2)

II 12 13 14

True Solar Time ( Hrs.)

Figure 1

Solar irradiance curves for Swan Island. Values are integrated daily total irradiance (cal/cm2 ) .

134

OCTOBER 4, 7966

OCTOBER 30. 1966

Figure 2. Satellite photos of Central Amerioa3 the Gulf of Mexico, and the western Caribbean. Swan Island is located at l7°Ni 84°W. The photos correspond to the two days (radiation curves) shown in figure 1.

These empirical equations have been araphed and illustrated in figure 3 to show the wide range of transmi ttance values for a particular value of cloud cover. Moreover, the functional re- lationships differ depending on the proposed formula used: in four cases a linear relationship has been found, but in others second- and third-order polynomials are illustrated.

Another difficulty with parameterization using cloudiness is that the result depends on the time scale over which the cloud and irradiance data are averaged. An example of this is shown in figures 4 and 5. In both illustrations, curves 3 and 5 are shown as limiting curves. Mean atmospheric transmi ttance and mean cloudiness averaged over daily periods are shown in figure 4, and averaged over annual periods are shown in

135

Cloudiness (tenths)

Figure 3. Atmospheric transmittance vs. cloudiness by var- ious authors (see text) as summarized by Quinn (1968).

10

I I

1

l i 1 - i 1

s Total Sky Cover / Miami Fla

"^^_

\

\

X

\

""-«

i> , Opaque Sky Cover ^;*1^/ Miami, fla

-

\.

'

\

■s \ \

\\ \

\\ \ \ \ \ .

\

\3 \

N

10

Cloudiness (tenths)

Figure 4. Atmospheric transmittanoe vs. cloudiness for Miami, Florida, based on daily values of irradiance and cloudiness .

136

Cloudiness (tenths)

Figure 5. Atmospheric transmittance vs. cloudiness for Miami, Florida, based on annual values of irradianoe and cloudiness .

figure 5. The transmittance values are obtained as the ratio of the solar irradiance at the earth's surface to the extra- terrestrial irradiance. Both figures 4 and 5 are based on data from Miami, Florida. From these figures it is clear that the time scale of averaging the data changes both the position and the shape of the parameterization curve. This may offer a partial explanation for the wide variety of curves in figure 3 which undoubtedly are based on a variety of time scales.

It is apparent from more than 40 years of effort by many investigators that there are certain shortcomings in quantify- ing solar irradiance from cloudiness. This paper is to look at the accuracies of simple parameterization ques (which include surface-observed cloudiness) and pare these with parameterization accuracies based on tive satellite data.

an attempt techni - to com- quanti ta-

2. PARAMETERIZATION METHODS

There are many applications for calculated values of solar irradiance at the earth's surface and, presumably, each

137

of these applications has a certain requirement for accuracy. Thus, it is important to be able to state quantitatively the predictability of surface irradiance. The followinq sections discuss the use of simple techniques for calculating surface irradiance as well as the use of quantitative satellite data for this purpose.

2.1 Long-Term Mean Irradiance

The most simple technique for determining the surface irradiance is to use the long-term (climatic) mean irradiance

T the cl Fl ori d standa for bo tabl e di ance are av v i a t i o on an nearly standa for sh the eq strong

0 test i mati c a , and rd dev th 1 oc

1 , sho to be

eraged fi is 3 hourly an or rd dev orter uatori ly att

the v

mean ,

15 ye

i a t i o n

ati ons

w (as

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. On

. 5 per

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time s

al dry

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zone

na cl o

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resu ed) t n the ly ba f the tanda tude s are

beca (2° S u d i n e

of observ ken 18 ye nton Isla ad i ance o Its, in t he standa

time sea sis at Mi

observed r d d e v i a t 1 arger .

somewhat use Canto . lat. ) a ss .

ed i r ars o nd an n var he le rd de 1 e ov ami ,

i rra ion i For C

smal n Isl nd is

radian f data d cal c i o u s t ft-han v i a t i o er whi the st di ance s 30.5 anton ler (p and is less

ce da

from

ul ate

ime s

d col

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ch th

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1 oca

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ta from Miami , d the cales umns of i r r a - e data d de- re as , ent -- d, the ul arly ted in ted by

These values in the left

hand ii

section of table

1 might be termed the "natural variance" of irradiance that occurs on various time scales. In this respect they represent an upper limit -- against which various parameterization tech- niques should show improvement.

2.2 Surface-Observed Cloudiness

A commonly observed meteorological parameter is total sky cover, which is the amount of sky obscured by clouds of any discernable thickness. Because it is commonly available, we have used this parameter to determine a functional rela- tionship between cloudiness and irradiance and have calcu- lated the variance of observed irradiance values from function generated irradiance values. (This is commonly called "vari- ance of the residuals after regression".) The same Miami

138

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139

and Canton Island data were used, and the results are shown in tne middle section of table 1. It can be seen that standard deviation increased with shorter time scales, and the values are less than those determined from the climatic mean. The major improvement in predictability (over the climatic mean) is in the shorter time scales. For example, for Miami, the standard deviation decreases from 27.3 to 17.7 percent on the daily ti me scale.

Thus, it appears that simple cloud parameterization of irradiance is most useful for applications which require cal- culations on time scales of a week or less.

2.3 Satellite-Observed Irradiance

Based on the principle of conservation of energy, it is possible to calculate the absorption of radiation by the at- mosphere as a residual, in cases where satellite and surface irradiance measurements are available (Hanson et al . 1967). However, in the present case it is not atmospheric absorption that is desired, but irradiance at the surface. Thus, the residual calculation is surface irradiance -- which requires satellite irradiance measurements and a quantitative estimate of atmospheric absorption.

We have used this method to establish the accuracy with which surface irradiance may be determined. The result, with dependent data, shows that for the United States on a monthly scale (June, 1966) the standard deviation of surface irra- diance is 3.2 percent (table 1). This is smaller by a factor of three than the standard deviation of the irradiance from the long-term mean. This satellite data technique is yet to be tested with independent data.

The method used in this technique is to determine the atmospheric absorption of irradiance (I„) as a residual in

lo = ^"^g + h + h

(1)

where

I = incident extraterrestrial solar irradiance,

I = solar irradiance at earth's surface,

L = irradiance reflected to space,

a = surface reflectance (albedo).

140

Dividing ( 1 ) by I gives

where

1 = qa + qr + qg(1"a)

(2)

qa = W

the fraction of incident sunlight absorbed i n the atmosphere ,

^r " V:o

the fraction of incident sunlight reflected to space ,

«g = I/[o'

the fraction of incident sunlight transmitted by the atmosphere to the earth's surface.

The right-hand term in (2) is the fraction of the incident irradiance which is absorbed at the earth's surface; this will

be denoted as q

Then

1 = q + q + q ^a ^r Me

(3)

Equation (3) simply shows the partitioning of solar radiation which is incident on the earth's outer atmosphere.

The following sections show how the individual irradiance terms were determined.

2.3.1 Irradiance at Upper Boundary

In this study, the irradiance, I , was calculated from

i0 = y>vr)2 cos^

(4)

The solar constant, I , was taken as 2.0 cal/cm2 min, r and

r are the mean and actual earth-sun distances, and c, is the time- integrated solar zenith angle at the subsatellite point

2.3.2 Irradiance at the Earth's Surface

The irradiance, I , was obtained from measurements by the National Weather Service network of pyranometer stations which

141

measure the broadband (0.3-2.5 urn) solar irradiance. These data are avaiable from the National Climatic Center (NOAA, 1966). Corrections have been made to the measurements in order to account for degradation of the sensors at some sta- tions. The background information for determining those cor- rections was obtained from Stark (1971). Surface reflectance, a, values for the United States were obtained from the summer season surface reflectances reported by Kung et al . (1964). The resulting surface absorption of irradiance, q , over the

United States is shown in the lower portion of figure 6 and is expressed as the fraction of incident extraterrestrial irradiance.

2.3.3 Irradiance at the Upper Boundary

The upwelling irradiance at satellite height, IR, was

observed by the MRIR (broadband solar) sensor on NIMBUS II.

The irradiance was determined from MRIR radiance data by methods described by Raschke and Bandeen (1970). The earth's

reflectance at satellite height, q , is given in the upper

half of figure 6. There is a high negative correlation be- tween q and q , as is evident in figure 6.

2.3.4 Irradiance in the Atmosphere

a res

Values of atmospheric absorption, I. i dual using (1) and the values of a,

were cal cul a ted as I , I , and ID from

U 0 K

the sources indicated above. The resulting q values are

a

shown in the upper half of fiaure 7. The distribution of q

shows high absorption in the east -- particularly the south- east -- as expected from water-vapor distribution. This latter value is shown in the lower part of figure 7 and has been calculated from mean monthly temperature and water- vapor (vertical) distributions. Optical depth of water vapor, u, was calculated from:

u =

1

Tw dp

(5)

where g is the acceleration of gravity at the earth's surface w is the mixing ratio of water vapor, and p is pressure. The integration was carried out to approximately 300 mb . Optical pathlength values, t, (in lower fig. 7) have been determined

142

Figure 6. Distributions of fractional reflectance 3 q j of earth/atmosphere and fractional

absorption of the earth ' s surf ace 3 q 3 for June, 1966.

143

Fractional Absorption Atmosphere ne, 1966

^"^-Vvp? cp \ .

Figure 7. Distributi

on of fractional absorption by the atmosphere, q ^ and optical pathlength of

water vapor for June, 1966.

144

from these u values, from the change in optical pathlength due to varying solar zenith angles, 5, and from the effect of diffuse radiation beneath clouds. The latter effect was introduced in the following way:

t = (l-c)(.86u* + .14(1. 66u)) + c(1.66u)

(6)

where c is the mean monthly cloudiness and u* is the opti cal pathlength with clear skies,

i* =

u sec i>

(7)

A diffusivity factor of 1.66 has been used as the optical pathlength under diffuse light conditions due to clouds.

The resulting t values, mapped in figure 7, show a

pattern very similar to the atmospheric absorption, q .

a

There are low values for optical pathlenqth in the western

United States and higher values in the east and southeast.

In comparing these two distributions, it appears that qa

a

values in the northeastern quarter of the United States are

higher than expected from water vapor along -- and may be a

result of industrial or other pollution. The strong depend

ence of q on t is clear from figure 7. a

In figure 8, the dependence of q 3 on t is shown in a

a

scatter diagram. The qa values are related to t by

a

117 + .031t* In t

(8)

where the constants have been determined by least squares fit. The variance of the residuals from the function values is .00101. Thus, the standard deviation of the residuals is 3.2 percent.

In this case we have determined I„ as a residual in (1). However, it is also possible to use the measurement of I n and a knowledge of I and In (calculated from (8)) in

K 3 O A

order to parameterize I over the United States. This has been done, and the calculated I values and observed (dependent

145

0.50

<

40

- 0 30

20

U.S. Network June . 1966

2 3 4 5

Optical Pathlength of Water Vapor (cm)

Figure 8. Fractional absorption of solar radiation by the atmosphere q 3 vs. optical path- length of water vapor based on the U.S. network of pyranometer and radiosonde stations and on NIMBUS II broadband solar (MRIR) data for June 1966.

data) values of I have a standard deviation of 3.2 percent

9 The significance of this fact, as shown in table 1, is that the satellite parameterization of I shows improvement by

factors of 2 and 3 over the other two techniques.

SUMMARY

This study has shown that there are difficulties and shortcomings with relatively simple techniques for parameter- izing solar irradiance from (1) long-term climatic radiation data, and (2) cloud observations from the earth's surface. One difficulty is that there is a wide range in the results of empirically determined irradiance values (from cloudiness) depending on the equation used (i.e., the author selected). A second difficulty is that both the form and the constants of the empirical equation depend on the time scale over which the data are averaged.

146

In an attempt to determine the accuracy of these two parameterization techniques, we have used 18 years of data from Miami, Florida, and 15 years from Canton Island. The result (table 1) shows that the longer time scales have the smallest errors. The use of surface-observed cloudiness to parameterize the surface irradiance shows only slight im- provement over the natural variance that occurs. On shorter time scales, the improvement is somewhat more significant than on the longer time scale. The use of satellite data for parameterizing surface irradiance on a monthly time scale shows improvement by a factor of about 3 over the natural variance that occurs.

REFERENCES

Beriland, T.G. (I960), Metodika Kl imatol ogi cheski kh Raschetov Summarnoi Radiatsii (Method of CI i matol ogi cal Calculation of Global Radiation), Meteor, i Gidrol. 6, 9-12.

Black, J.N. (1956), The distribution of solar radiation over the earth's surface, Archiv. Meteorol . Geophys. Bioklim. B7, 165-189.

Budyko, M.I. (1956), The Heat Balance of the Earth's Surface, Gi drometeorol ogi cheskoe Izdatel'stvo Leningrad (transl. by Office of Tech. Services, U.S. Dept. of Commerce, Washington, D.C., 1958, 259 pp).

Cox, S., and S. Hastenrath (1970), Radiation measurements over the equatorial central Pacific, Monthly Weather Rev. 98, 823-832.

Hanson, K.J., T.H. Vonder Haar, and V. Suomi (1967), Reflec- tion of sunlight to space and absorption by the earth and atmosphere over the United States during the spring 1962, Monthly Weather Rev. 95_, 353-362.

Kimball, H.H. (1928), Amount of solar radiation that reaches the surface of the earth on the land and on the sea, and methods by which it is measured, Monthly Weather Rev. 56 , 393-398.

Laevastu, T. (1960), Factors affecting the temperature of the surface layer of the sea, Soc. Sci . Fennica, Commen- tationes Phys. Math. 25, 1-135.

147

NOAA (1966), CI imatologi cal Data - National Summary, Natl. Climatic Data Center, Asheville, N.C.

Quinn, W.H. (1969), A study of several approaches to com- puting surface insolation over tropical oceans, J. Appl. Meteorol . 8, 205-212.

Raschke, E., and W. Bandeen (1970), The radiation balance of the planet earth from radiation measurements of the satellite NIMBUS II, J. Appl. Meteorol. 9, 215-238.

Tabata, S. (1964), Insolation in relation to cloud amount and sun's altitude, Univ. of Tokyo, Geophysics Notes 17, 202-210.

148

68

Reprinted from Journal of Geophysical Research 76,

No. 18, 4172-4180 .

Airborne Measurements of the Total Heat Flux from the Sea

during Bomex

E. D. McAlister

University of California at San Diego Scripps Institute of Oceanography, La Jolla, California 92037

William McLeish

Environmental Science Services Administration Atlantic Oceanographic and Meteorologic Laboratories, Miami, Florida 33130

Ernst A. Corduan

University of California at San Diego Scripps Institute of Oceanography, La Jolla, California 92037

Airborne measurements of the total heat flux from the sea were successfully made during the Barbados oceanographic and meteorological experiment in May 1969. The values found at night ranged from 0.05 to 0.45 cal cm"2 min"1 and are half-hour averages over contiguous strips of ocean 1.6 km long and 75 meters wide. These are the first airborne measurements of this oceanic factor and the method used is new.

A total of 1021 calories of solar energy is stored during the daylight hours of one aver- age day in the top 30 meters of the world's oceans. This energy is released during a 24-hour cycle and thus is important to the dynamics of the ocean. It represents the total energy available to the marine atmosphere from below and so has a direct bearing on meteorological predictions. No direct method of measurement of this total heat loss has previously been dem- onstrated.

For the past several years at Scripps Insti- tution of Oceanography, the authors have at- tempted to fill this need by developing an air- borne infrared-optical method. The principle of this method depends on the physical properties of water, namely its absorption coefficient for infrared radiation and its molecular heat con- ductivity. The system developed measures the vertical temperature gradient in the top 0.1 mm of the sea surface wherein the heat flow is dom- inated by molecular conduction [McAlister and McLeish, 1969]. The total heat flow may be determined from this temperature gradient and the heat conductivity of sea water. A two-wave-

Copyright © 1971 by the American Geophysical Union.

length infrared radiometer was developed for this purpose.

The use of an airborne digital data reduction system was of major importance in this system. This combined with continuous calibration of detector sensitivity allowed measurement of water temperature to 0.01 °C and the tempera- ture difference between the two depths to 0.003°C. It is believed that the accuracy in reading water temperature is set by the mer- cury thermometer used in calibration, which could be read to 0.01 °C.

This accuracy is reached only after determin- ing atmospheric losses caused by absorption, scattering, and emission by flying at different altitudes and extrapolating the data to zero altitude, i.e., the sea surface. The radiation from the sky is continuously measured and used to remove reflected sky radiation from the beam coming from immediately below the water surface. Details of the two-wavelength radiometer, the digital data recorder, calibra- tion, operation, calculation procedures, and the effect of sea state are described in McAlister and McLeish [1970]. The calculation pro- cedure is repeated here and one day's records are analyzed later to illustrate the calculation

4172

Heat Flux

4173

of total heat flux and sea-surface temperature. The infrared radiance from the water sur- face at night Iw is the sum of two parts: h(l r) from immediately below the water sur- face and Is r from the sky by reflection from the water surface, i.e.,

Iw = Iu(l - r) + ls-r (1)

where Iv and Ia are the underwater and sky radiation intensities and r is the reflectivity of the water surface. The radiometer compares this total with that from the reference black- body IB- The radiometer uses two wavelength bands, 3.4 to 4.1 /x (channel 1) and 4.5 to 5.1 /jl (channel 2), which effectively isolate radia- tion coming from depths of 0.0075 cm and 0.0025 cm in the water. The reflectivity for the wavelengths used in channel 1 is rt 0.0268 and in channel 2 the reflectivity is r2 = 0.0210. In channel 1 the comparison of intensity from the water with that from the reference black- body is

(la, ~ Is)

_ (Iw, - IBl) ~ (h, - h,)-r, ^ A ,y (1 - r,) and in channel 2 it is

(la. ~ h,)

(Jw, - //»,) - (Is, - js^tll _ A (3) (1 - r2) The difference in intensity coming from the two depths is then

Iv, ~ la, = A, - A2 (4)

The temperature difference in the water at the two depths is therefore

AT = (Al - A2)C

(5)

where

C

((TBl) - (TBJ)/((IBl) - </*.» (6)

and (IB,), (Ib,), (TBi), and (TBa) are the aver- age intensities and temperatures for the two reference blackbodies during the time interval of interest. This approximate relation holds with sufficient accuracy when water temperature and the blackbody temperatures are no more than or 3°C apart. After AT is evaluated for a particular exercise the total heat flux is calculated

by multiplying the coefficient of heat conduc- tivity of sea water by the vertical temperature gradient.

The actual temperature at the two depths cannot be obtained as accurately as the dif- ference in temperatures, equation 5. This is because the temperature of the water surface flown over does change a few hundredths of a degree centigrade during the half hour or more of time necessary to obtain several read- ings at three or more altitudes. Also, since the difference in radiation intensity coming from the two depths (equation 4) changes very little (a small fraction of 1%) for a 0.1 °C change in water temperature (say, from 300.0°K to 300.1 °K) the temperature difference as ob- tained from equation 5 is accurate.

The Trials at Barbados

During May of 1969 at Barbados scientists from several oceanographic institutions made use of Scripps' Floating Instrument Platjorm (Flip) to measure the latent heat flux, sen- sible heat flux, and the factors influencing the magnitude of these heat losses. This offered an opportunity for comparison with values meas- ured simultaneously by the total heat flow radiometric system.

The equipment and crew were flown to Bar- bados in Scripps' DC-3 aircraft. The system was assembled and recalibrated to verify its condition after the flight from San Diego.

Flip was stationed 200 miles east of Barba- dos. Flights near it were made when weather and operating conditions permitted. These flights were at night to avoid solar interference with readings from the shorter wavelength channel (3.5 to 4.1 fi). Safety regulations that were adopted required a lateral separation of 300 meters from Flip. Consequently a racetrack course was flown, the downwind leg being 300 meters north of Flip and the upwind leg 300 meters south.

Data was tape recorded during 24 sec of each leg, which gave information on a 1.6-km strip on the sea which averaged 75 meters in width. 26,000 readings of 10 parameters were recorded during each pass. The flights were made at 50, 100, and 150 meters altitude to correct for atmospheric attenuation [McAUster and McLeish, 1970]. Usually 16 to 24 passes by Flip were made during a period of from

4174 McAlister, McLeish, and Corduan

TABLE 1. Computer printout of 30- sec averages

DEC. SEAU) III SKYI1) BB 121 Sfi4(?1 66 II) SKY m BB 121 I8e(ll 168(21

DEC. 9 1091. 0<i 1898,94 2841.34 1851.90 1923.30 1942.14 2654.62 1678.42 212. IT 1407.33

AVG.

TEMP. 9 27.995 27.291 28.262

AVC.

DEC. 10 1665.97 1997.00 277?. 4fc le49.28 1947.44 1971.23 2617.25 1907.40 275.59 1466.70

SVG.

TEMP. 10 28.060 27.340 28.309

AVC.

DEC. 11 1876.61 1185.20 2635.95 1837.71 1940.77 1961.43 2671.24 1898.28 258.95 1454.42

AVG.

TEMP. 11 28.002 27.327 28.299

A VS.

DEC. 12 1853.44 lt61.10 2761. B9 1816.11 19C6.32 1933.50 ?5tl.22 1871.03 258.75 1438.78

AVG.

TEMP. 12 28.029 27.327 28.287

AVG.

DEC. 13 1863.76 1871.05 2806.24 lR26.e7 le93.78 1920.17 75^6. 86 1859.41 278.99 1437.53

AVG.

TEMP. 13 28.053 27.343 28.286

AVG.

OEC. 14 1958.30 116'j.42 27H4.56 1421.71 1977. 5e 1994.48 2603.85 1933.22 317.16 1462.60

AVG.

TEMP. 14 28.010 27.373 28.306

AVG.

OEC. 15 1900.21 1907.02 2861.19 1862. <3 1936.15 1954.25 26H4.4A 1893.82 244.26 1382.84

AVG.

TEMP. 15 29.011 27.316 28.243

AVG.

DEC. 16 1853.96 1858.08 2793.82 1814.4? 1903. C9 1921.34 2614.61 1861.69 341.23 1461.46

AVG.

TEMP. 16 28.019 27.392 26.305

AVG.

DEC. 17 1878.85 1887.36 2828.32 1843. CO 1110. ec 1933.83 2641.84 1873.75 275.55 1389.29

AVG.

TEMP. 17 28.050 27.340 28.246

AVG.

OfcC. 1H 1342.90 1354.76 2693.51 1M2.C2 ie53.85 1923.75 2511.77 1863.65 217.09 1331.49

AVG.

TEMP. 18 28.045 27.295 28.203

AVG.

DEC. 19 1913.10 1925.65 2532.79 1883.36 1945.05 1972.99 2426.26 1913.70 309.50 1412.35

AVG.

TEMP. 19 27.997 27.367 28.266

AVG.

DEC. 20 1945.03 1953.21 2828.69 1909.44 1941.08 1958.49 2632.18 1899.71 282.05 1396.89

AVG.

TEMP. 20 28.021 27.345 28.254

AVG.

OEC. 21 1888.39 1893.17 2848.46 1849.59 1912.94 1928.09 2656.76 1868.22 265.53 1375.34

AVG.

TEMP. 21 27.981 27.332 28.237

AVG.

OEC. 22 2048.00 2048.00 2048.00 2048. CO 2048.00 2048.00 2048.00 2048.00 2048.00 2048.00

AVG.

TEAR. 22 28.725 28.725 28.763

Heat Flux

4175

40 minutes to 1 hour. These provide an aver- age value of total heat flux from the strip of ocean 1.6 km long and 75 meters wide.

Flights were made when weather permitted a night rendevous with Flip. The Flip was be- ing towed to a new location from May 20 to 23, consequently no flights were made then. From May 19 to May 29, seven flights were

made as shown in Table 3. The flight on May 29 was made in cooperation with ESSA planes. Flip was departing Barbados on this date. During all of these flights there were scattered low clouds, 300 to 600 meters and a secondary layer at middle altitudes. These cloud condi- tions were uniform for all of the flights. Dark- ness prevented detailed cloud description.

TABLE 2. Computer printout of radiation intensity differences

CHANNEL 1

CHANNEL 2

R1C. (S(D-BB(l)l - ((SKYI2I-BBI III*. 02681

(S(2)-BB(ll 1 - ((3KYI2I-

2

-33.22*2

2

-3*. 1212

3

-35.2994

3

-36.252-.

4

-33. 423*

4

-34.3258

5

-35.7298

5

-36.6945

6

-35.4512

6

-36.4084

7

-37.5697

7

-38.5841

a

-35.6011

8

-3-6.5623

9

-33.1563

9

-34.0515

10

-34.4929

10

-35.4242

11

-32.0701

11

-32.9360

12

-32.4824

12

-33.3594

13

-32.3531

13

-33.2266

1<V

-30.0462

1*

-30.8574

15

-32.4354

15

-33.3111

16

-29.1973

16

-29.9862

17

-33.7277

17

-34.6334

18

-34.3385

18

-35.2656

19

-28.8214

19

-29.5995

20

-31.6429

20

-32.4972

21

-30.3818

21

■531.2021

47.7200

45.6900

44.ieco

45.21C0 44.4900 43.6500 44.3600

43.5eC0

-21.7335 -25.5144

-33.3133 -24.48S9

-38.4351 -27.0927

-42.2011 -30.8148

-43.10E0 -31.4974

-46.0594 -34.9672

-35.0295 -26.1607

-33.8021 -25.3289

-37.3564 -28.3480

-35.5660 -27.1464

-40.7821 -30.2761

-<.0.60C5 -29.9654

-29.6968 -22.2458

-33.4340 -24.9850

-32.8087 -24.3693

-37.flle2 -28.3429

-42.24e4 -30.59e4

-37.4587 -27.12CO

-31.5575 -23.8523

-30.4521 -22.4997

29

. 57C0

56

.5000

58

.7800

60

.OBCO

59

.9300

6 0.

. 38CO

b!

48C0

63

.7200

63,

,e300

65,

. 15C0

6?

,4700

60,

, 76C0

61 ,

,26C0

60.

,4300

S>J.

6500

60.

caco

59,

S0CO

'.9.

2900

58.

7800

59.

8700

BBUI)'.0210>

ALT. IN

Ai"Ao

METERS

1 2

^.7966

150

-8.6068

-.8118

-11.7626

-.8548

100

-7.2331

-.8818

-5.8796

-.8967

50

-4.9110

-.9231

-3.6169

-.9484

150

-10.4016

-.9717

-8.7227

-.9686

100

-7.0762

-.9720

-5.7875

-.9599

50

-3.0833

-.9431

-3.2612

-.9330

150

-8.6116

-.9275

-8.3261

-.9132

100

-5.6169

-.9081

-6.2955

-.9086

50

-4.6672

-.8996

-2.4795

-.9090

1 CA

-8.6449

-.9050

■8.7024

4176

McAlister, McLeish, and Corduan

Experimental Results

The operation of the system is illustrated by a set of computer print-outs of magnetic tape records obtained during the Barbados exercises (Bomex) on May 26, 1969, and interpretation of these records. As mentioned previously the losses in the atmospheric path to the sea are determined by two flights, each at three alti- tudes: 50 meters, 100 meters and 150 meters. These are made in a series of flights in a racktrack course around Scripps vessel Flip. Successive flights of 26 sec (yielding data for ^1.6 km of sea surface) were made upwind 300 meters north of Flip and then downwind 300 meters south of Flip. On May 26, from 1743 to 1838 LT 20 fly-bys were made and the computer print-out of the average of a part of the 100-entry record is shown in Table 1, along with the blackbody temperatures and the water surface temperature from channel 1. Note that the water temperature is between the blackbody temperatures. Each one of the entries in this table is the average of 2600 in- dividual readings. Notice the small variations in temperature of the blackbodies and of the water at a 0.075-mm depth, the latter being the average temperature for a 1.6-km path on the sea surface. (Details of these tempera- ture calculations are given later.)

The computer (CDC 3600) is programmed to calculate A^ and A2> the right-hand members of equations 2 and 3. Some of the steps in this calculation are printed out by the computer in Table 2. The first column is the record (flight) number, the second column is IVl IBl, the third column is IBl IB,. The fourth column is IUt IBl (channel 2), the fifth column is IBi IBa (channel 2), the sixth column is TB, TBl in degrees centigrade, the seventh column is flight altitude, and finally in column 8 is Ai A2 in intensity units.

The first number in column 2 is the numer- ator of equation 2. The next number down (also record 2) is the above number divided by (1 rj which makes it Aa. Numbers in the third and fifth column are the intensity differences in channels 1 and 2 for the temperature differ- ences (column 6) between the two blackbodies. The first number in column 4 is the numerator of equation 3. The next number down this column is the first one divided by (1 r2)

and multiplied by the sensitivity ratio of col- umn 3 over column 5. This number is A2. Column 7 is the altitude of the flight in meters. Column 8 is Ax Aa (equation 4) for the dif- ferent altitudes of flight, column 7. A progres- sive change in intensity difference from the two water depths (column 8) is apparent as the sea surface is approached in equal steps of 50 meters. These values of Ai A2 are plotted against altitude in Figure 1. Each value plotted here is an average and is derived from 5200 readings in the two channels. The circled points are average values for the different flight alti- tudes and are derived from some 21,000 read- ings for the 150-meter altitude and 16,000 readings for the 100- and 50-meter altitudes.

The intercept at zero altitude shows a dif- ference of 0.75 intensity units. Using equation 6, C (the calibration constant) is calculated from the average of the numbers in column 6 divided by the average of the numbers in column 3. This ratio is 0.0208 °C per intensity unit in channel 1 for the exercise. The average temperature difference between the depths of 0.025 mm and 0.075 mm during this time in- terval is obtained from equation 5 and has a value of 0.75 X 0.0208 = 0.016°C.

The heat flow equation

Q = K AT/d per unit area

gives the amount of heat energy flowing up- wards as

0.086 X 0-016 0.0050

= 0.27 cal cm min"

LU UJ O Q

Z ID

£ l 10 -

50 IOO

ALTITUDE - METERS

150

Fig. 1, Intensity difference received at altitude versus altitude.

Heat Flux

4177

This then is the average value of heat flux from the sea surface for the period 1743 to 1838 LT on May 26, 1969, near the latitude and longitude of Flip, 13.57 N and 56.33 W.

Table 3 shows the average sea-surface tem- perature and average heat flux obtained for the useful flights made at Barbados. Column 3 shows average values of wind speed at a 2-meter altitude as measured on Flip and kindly sup- plied by K. Davidson, University of Michigan. These are averages over the time intervals indi- cated in column 2. The sea-surface tempera- tures shown are average values for the time interval indicated. The average deviation in temperature is shown below each value. The average temperature for individual fly-bys of five of these exercises are shown in Tables 4 and 5.

The heat flux result for the May 26 exercise (calculated as shown above) is the second entry in Table 3. The May 27 results are calculated in detail in McAlister and McLeish [1970, page 2702]. The results for May 24 and May 29 are

obtained in exactly the same way from tape records for these dates. The May 29 exercise was flown nearer to Barbados and also nearer to vessels participating in Bomex. The strong radar pulses from these vessels interacted with our electronic system a good part of the time so that only fragmentary records were obtained. These fragments, however, did enable a value of 0.4 cal cm"2 min"1 to be calculated.

The comments column in Table 3 gives some indication of weather conditions, especially for the first three exercises listed. The negative results for May 25 were caused by radar inter- ference nearly 100% of the time. On May 19 the wind was very gusty, so much so that the air- craft could not maintain a constant altitude, and there was no way to correct for this. In the early exercise on May 24 the power supply for the electronic system became so 'noisy' that no useful data could be obtained. The aircraft returned to Barbados, the power supply was repaired, and a late flight on that date gave the results shown in the first entry in Table 3. The

TABLE 3. Total Heat Flux Results

Date (1969)

Local Time

Sea Surface

Wind Speed Temperature cm sec"1* °Ct

Heat Flux

Results t cal cm-2 min-

Comments

May 24

1827-1858

612

27.77 ±0.02

0.05

Intermittent rain

May 26

1740-1838

890

28.06 ±0.02

0.27

Rain nearby

May 27

0446-0552

830

27.71 ±0.02

0.45

Best weather

May 29

1724-1834

28.44

0.4

Radar interference 90% data lost

May 25

1746-1838

650

27.61 ±0.13

Negative

Radar interfer- ence

May 19

1804-1855

795

27.96 ±0.02

Negative

Heavy weather. Altitudes uncer- tain

May 24

0654-0724

770

28.08 ±0.05

Negative

Internal interfer- ence from power supply

May 28

0553-0623

830

27.84 ±0.07

Negative

Gusty winds; spray below 75 meters

* Data from Flip.

t Average over a 1.6-km strip 75 meters wide.

4178

McAlister, McLeish, and Corduan

May 28 exercise gave no heat flux results be- cause of wind-blown spray encountered at the 75-meter altitude. This prevented an accurate extrapolation of data to the sea surface.

The comparison of heat flux results shown in Table 3 with simultaneous measurements by others on Flip did not materialize. The only comparison that can be made was to data ob- tained on Flip the week before, which ranged in value from 0.15 to 0.40 cal cm"2 min"1. This range compares favorably with values in Table 3, but the measurements were not simultaneous. The May 29 value of 0.4 cal cm"2 min"1 may be compared to a simultaneously obtained value of 0.3 cal cm"2 min"1 reported in a private com- munication by Dr. B. Bean of ESSA. Laboratory measurements in a wind-water tunnel [Mc- Alister and McLeish, 1969] show an experi- mental error in heat flux for this system of ±8%.

Sea-Surface Temperatures

McAlister and McLeish [1970] showed that the use of an airborne digital data recorder, con-

TABLE 4. Sea-Surface Temoeratures

TABLE 5. Sea-Surface Temperatures

May 19, 1969 14.43 N, 57.32 W

May 24, 1969 13.57 N, 56.30 W

Surface Surface

Local Time Temp. °C Local Time Temp. °C

1804 06 08 12

14 16 18 20

25 27 30 32 35 .'57 41 43 45 47 50 53 1855

27.94

0.95

0.95

0.94

0.98 28.00 27.96

0.98 28.01 27.95

0.98

0.98

0.97

0.94

0.95

0.96

0.94

0.94

0.95

0.90 27.92 27.96 ± 0.02

0700 04 OS 12 17 20 22 24

0728

1827 31 33 40 43 45 47 50 53 55

1858

.05

28.05

0.09

0.16

0.20

0.05

0.04

0.06

0.07 27.99 28.08 ±

27.79

0.77

0.84

0.78

0.75

0.78

0.78

0.77

0.69

0.74 27.75

27.77 ± .02

May 26, 1969 13.57.3 N, 56.33 W

May 27, 1969 13.58 N, 56.37 W

Surface Surface

Local Time Temp. °C Local Time Temp. °C

1743 46 49 52 55 57

1801 03 06 09 13 16 20 22 26 28 32 35

1838

28.09

0.07

0.11

0.08

0.10

0.10

0.04

0.08

0.03

0.04

0.06

0.05

0.05

0.04

0.07

0.06

0.01

0.06 28.02 28.06 ± 0

.02

0446 49 52 55 59

0502 06 08 11 14 17 20 24 27 30 33 37 40 43 46 49

0552

27.70

0.70

0.70

0.67

0.69

0.72

0.69

0.69

0.70

0.73

0.75

0.75

0.74

0.73

0.72

0.74

0.71

0.73

0.70

0.74

0.70 27.71

27.71 ± 0.02

tmuous calibration of detector sensitivity, and the data reduction methods employed provided an accuracy in temperature measurement of 0.01 °C. These factors also allowed measure- ment of the temperature difference between the two water depths to 0.003°C. This accuracy is reached in a 30-sec averaging period, i.e., while the aircraft is flying 1.6 km at constant altitude over the ocean. (Thermistor drift found after 6-months use caused an error of 0.004 in tem- perature values.)

In Table 1 there are two rows for each fly-by (record number). The lower one is labeled AVG. TEMP, (average temperature) and the two temperatures on the right are of black- bodies 1 and 2 obtained from the numbers immediately above and calibration charts. The average sea-surface temperature for that 1.6 km of flight is shown to the left. These sea- surface temperatures are obtained as follows: for record 21 in Table 2 we find the entry (lower one) 31.202 which is a value for the right-hand member of equation 2, i.e., the

Heat Flux

4179

radiation intensity difference between the sea readings and the readings on blackbody 1. The radiometer sensitivity for record 21 is the ratio of the temperature difference between the two blackbodies and their intensity reading differ- ence in column 3, i.e., 0.905/43.58 or 0.0208°C per unit intensity. The product 0.0208 X 31.202 = 0.649°C is the temperature difference between the sea and blackbody 1 . Table 1 shows an average temperature for blackbody 1 of 27.332°C. So 0.649 + 27.332 or 27.981°C is the average sea-surface temperature for that record, which is printed out by the computer in Table 1 for record 21. The average sea-sur- face temperature for each record in Table 1 is calculated by the computer in the same way.

The effect of surface roughness and waves (i.e., sea state) on these temperature readings is discussed by McAlister and McLeish [1970] on page 2701. Here the studies of others and the 25° beamwidth of the radiometer that was used lead to the conclusion that as a first approxi- mation the ocean is 'essentially flat' even up to high wind speeds. This can be visualized by noting that the radiometer beam averages the intensity received over one or two wavelengths of ocean waves so the effect of positive and negative slopes tends to cancel. If the relation between reflectivity and angle of incidence were linear, the effect of equal elements of positive and negative wave slopes would exactly cancel under conditions where the effective sky radia- tion is constant with angle from the zenith. For a range of ±15° the reflectivity versus angle is nearly linear (departs a maximum of three parts in 100 from linear). Also for a uniform overhead sky its radiation is quite uniform out to 30° from zenith. Thus the assumption of a 'flat' ocean is a good first approximation, the limits of which will have to be set by consider- able experience. The distribution of wave slopes (including capillaries) is somewhat different downwind compared to upwind so that a definite lack of symmetry exists. The procedure followed in these airborne measurements of making an equal number of flights upwind and downwind is believed to cancel out this wind effect. Evi- dence for this belief can be seen in Figure 1 where the experimental points are seen to cluster in a group above the line and another group below this line. In Table 2 the even flights are upwind and the odd flights are downwind. Of

these ten pairs of flights six gave results where upwind and downwind were on opposite sides of the line drawn, two were nearly equal in value while two were opposed to the first six. This shows evidence of a cancellation of the wind effect as mentioned above.

With this in mind it is interesting to examine the sea surface temperatures off Barbados for the time periods shown in Table 3. Five of these flights are shown in Tables 4 and 5. Each entry in these tables gives the time of the start of each 30-sec pass and the average sea surface temperature for the strip flown over. These values were obtained from the 3.5 to 4.1 fi channel where atmospheric absorption is least. Plotting the values as a function of altitude of observation, an absorption correction of + 0.012°C for each 50-meter increase in alti- tude was found. This correction was used to obtain values shown in Tables 4 and 5.

Most of the time Flip was being held against wind and current by a tug so there was little overlap in the one-mile strips of ocean from one pass to the next. In other words, each pass was most of the time over a new strip of ocean but these strips were not far apart. The latitude and longitude for each exercise are shown in these tables.

Examination of entries in these tables reveals an interesting constancy in average tempera- ture of these one-mile strips of ocean surface under Barbados conditions. Surface tempera- ture changes from one day to the next were noted but for periods of an hour at night the temperature stays remarkably constant. The average deviation in temperature is shown and for four of the five periods it is only ±0.02°C. No previous measurements of sea-surface tem- perature have been made which show the accu- racy and area coverage (a 1.6-km strip) that are reported in Tables 4 and 5. This type of temper- ture measurement should be better for correla- tion with oceanic and meteorologic factors than isolated bucket temperature measurements.

Tests are in progress to study the possibility of shipborne use of the heat flow system. Here, so near the sea surface, atmospheric attenuation is quite small and correctable from meteorologi- cal data. A protective housing and stabilized platform have been made. This usage, if found possible, would enable longer time surveys at much less expense.

4180 McAlister, McLeish, and Corduan

Limitations of the Present System Summary

The present procedure of flying at three alti- tudes to obtain corrections for atmospheric attenuation is very time consuming. A modifica- tion of the radiometer's optical system to view the ocean at 20° and 60° from the vertical would provide two optical path lengths to the sea from one altitude. With adequate system sensitivity they should be sufficient for attenua- tion corrections. This would be a major re- design of the optical system.

Daytime operation with the present wave- lengths used in channel 1 is not possible because of solar energy reflected from the sea. Design of a system for day and night operation is diffi- cult but not impossible.

Sky conditions very different from those found at Barbados have been encountered near San Diego which interfere with the operation and linearity of the preamplifier system. These con- ditions are a clear cold night sky with small scattered low clouds. Under these conditions the clear sky signal, (/8ky IB), may be 20 times that from the water, (Iw IB), and it may vary ±50% from second to second. Lab- oratory tests duplicating these conditions show the amplifier system to become erratic and to depart from linearity in measuring intensity differences. The sky conditions at Barbados for all exercises showed a maximum variation in sky signal of 5%. Further tests of the amplifier sys- tem show that it departs from linearity when the clear sky to cloud signal variation reaches ±15%.

An initial solution of this electronic problem is under study. This is to attenuate the sky signal about an order of magnitude by intro- ducing a fixed impedance to the feedback loop input of the preamplifiers when the rotating mirror brings the sky radiation onto each de- tector. Airborne tests of this solution are en- couraging. Here it is necessary to write a new program for the tape records to bring the sky signal back to its unattenuated value before proceeding with the calculations. If this does not solve the scattered cloud problem then an improved preamplification system will be neces- sary. This would be a major undertaking.

Participation in the Bomex trials during May 1969 resulted in airborne measurements of the total heat flow from the sea. The values found at night ranged from 0.05 cal cm"2 min"1 on May 24 to 0.45 cal cm-2 min-1 on May 27. Measurements of heat flux made from Flip the week before in the same location show a range from 0.15 to 0.40 cal cm"2 min-1. Thus the range of values found by conventional methods from Flip and the airborne system agrees well but the measurements were not simultaneous. Lab- oratory tests of the airborne system show an error of ±8%.

A new order of accuracy in measurement of sea surface temperature has been demon- strated. It surpasses the accuracy of oceano- graphic mercury thermometry for sea surface temperature.

A redesign of the optical system is possible to shorten the time for one measurement. Also, a preamplifier improvement to include a wider range of sky conditions is under test.

These tests at Barbados have demonstrated the feasibility of airborne measurement of total heat flux with the present system. A thorough 'at sea' calibration is still lacking and further redesign is necessary before this development can be considered complete.

Acknowledgments. We are indebted to Bomex management organization and its operations team for fitting our needs so smoothly into a very com- plex exercise.

This research was supported by the Office of Naval Research, codes 461 and 481, Naval Ocean- ographic Office code 7007, and National Science Foundation, Atmospheric Sciences Section, under grants GA-1491 and GA 11975.

References

McAlister, E. D., and W. McLeish, Heat transfer in the top millimeter of the ocean, J. Geophys. Res., 74, 3408, 1969.

McAlister. E. D.. and W. McLeish, A radiometric system for airborne measurement of the total heat flow from the sea, Appl. Opt., 9, 2697, 1970.

(Received October 10, 1970; revised March 18, 1971.)

Reprinted from Journal of Atmospher ic Sciences 2 8 ,

No. 3, 429-435.

69

Measurements of Microwave Emission from a Foam-Covered, Wind-Driven Sea

W. NORDBERG, J. CONAWAY, DUNCAN B. ROSS1 AND T. WlLHEIT

Goddard Space Flight Center, Greenbell, Md. (Manuscript received 13 October 1970. in revised form 11 January 1971)

ABSTRACT

Measurements were made from aircraft of the 1.55-cm microwave emission from the North Sea and North Atlantic at surface wind speeds ranging from less than 5 to 25 m sec-1. Brightness temperatures in the nadir direction increased almost linearly with wind speed from 7 to 25 m sec-1 at a rate of about 1.2C (m sec-1)-1. At 70° from nadir the rate was 1.8C (m sec-1)-1. This increase was directly proportional to the occurrence of white water on the sea surface. At wind speeds <7 m sec-1, essentially no white water was observed and brightness temperatures in the nadir direction were ~120K; at wind speeds of 25 m sec-1 white water cover was on the order of 30% and average brightness temperatures at nadir were ~142K. Maximum brightness temperatures for foam patches large enough to fill the entire radiometer beam were 220K.

1. Introduction

Considerable interest has been devoted to the quanti- tative measurement of sea surface roughness, on a global scale, from spacecraft and to the possible deriva- tion of surface winds from these measurements (NAS Summer Study, 1969). For this reason, we measured the microwave emission at 1.55 cm over the North Atlantic and the North Sea in March 1969 over a wide range of sea surface, wind and cloud conditions in order to establish a quantitative relationship between the emission and the sea state and to delineate parameters such as surface winds, foam cover, wave height and cloud cover that would affect this relationship.

Earlier measurements (Nordberg el al., 1969) over the Salton Sea have shown that the microwave emis- sion, observed at all nadir angles from to 50° and at a wavelength of 1.55 cm, is considerably greater from a rough water surface than from a smooth one. Stogryn (1967) had predicted that increases in micro- wave emission from rough water could be observed only at nadir angles >30°. However, Stogryn's calcula- tions were addressed primarily to the effect of the large- scale wave geometry on the emission and did not, for example, account for foam and spray. We have there- fore conducted these observations at high wind speeds and extensive foam cover to investigate further this discrepancy between theory and earlier observations.

2. Description of experiment

Measurements were made from the NASA Convair 990 airborne observatory. Primary instruments carried by the aircraft were as follows :

1 Present affiliation : NOAA Air-Sea Interaction Laboratory, Miami, Fla.

1) A radiometer measuring horizontally polarized radiation at 1.55 cm wavelength within a 2.8° diameter field of view which was scanned perpendicularly to the aircraft's flight path over a nadir angle range of ±50°. The same instrument was used in the Salton Sea obser- vations; it was built by the Space Division of Aerojet General Corporation (Oister and Falco, 1967).

2) A laser geodolite of the Spectra-Physics Corpora- tion to measure the ocean wave height spectrum.

3) An infrared radiometer, similar to the Medium Resolution Infrared Radiometer (MRIR) flown on Nimbus satellites (Nimbus III User's Guide, 1969), to determine the sea surface temperature from emission measurements at wavelengths between 10.6 and 11.6 (j.m.

4) Standard airborne navigation systems, both Doppler and inertial, with which wind speed and direc- tion at the aircraft altitude were measured.

5) A Vinton 70-mm camera, pointing at nadir with a square field of view of about 68°, to photograph sea surface and cloud conditions.

In addition, the aircraft carried standard instrumen- tation for altitude, attitude, speed, and ambient tem- perature measurements and auxiliary cameras. A non- scanning, nadir viewing, 3-cm microwave radiometer with a field of view of about 13°X 13° was provided by the Jet Propulsion Laboratory for comparison with the 1.55-cm measurements.

The aircraft was based at Shannon, Ireland. Two flights, averaging 5 hr each, were made over the North Sea, and four flights, equally long, covered a region of the North Atlantic between Iceland and Ireland. In general, passes were made over each area of interest at several altitudes between 120 and 12,000 m to differ- entiate the effects of atmospheric and surface emission.

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Table 1. Summary of meteorological conditions and microwave emission temperatures for six overwater flights.

Case

Date (March 69) Time (GMT) Location

A 10

1321

Atlantic

Off Shannon

B

13

1247

Atlantic Ship J

C

13

1117 Atlantic Ship I

D

10

1430 Atlantic Ship I

E

19

1023 North Sea 57°N 3°E

F

14

1453

North Sea

59°N 1°30'E

Wind speed (m sec-1)

<5

6

13

16

17

25

Significant wave height (m)

<1

6.0|

3.9

5.0

4.0

7.8

Foam cover (%) Whitecaps Streaks Total

4.2 3.5

7.7

5.6 6.9

12.5

6.0

17.4 23.4

5.0 27.0 32.0

Temperature (°C) Sea surface Air surface

9

10 (est.)

10

11

9

7

9

5

2 2

4

2

Cloud altitude (m) Base Top

2000 2300

clear clear

300 2100

800 2000

600 2000

150 5000

Brightness temperature (CK) High altitude* Low altitude

128** 120

118

127

138

132

138

132

148 142

* Measured within 30 min of time shown. ** Over Irish Sea at 1212 GMT. f All swell, no wind waves.

Surface wind speeds ranged from calm to 25 m sec-1. They were obtained from surface anemometer obser- vations and/or by extrapolation of the aircraft measured ambient wind speeds at the lowest flight altitudes under the assumption that wind speed decreased exponen- tially toward the surface (Ross et al., 1970). Where both were available no significant discrepancy was noted. This assumption was applied to all cases shown in Table 1, except case E. In that case, examination of reduced geostrophic winds and ship reports led us to assume that the wind speed increased from the height of the aircraft to the surface. We are very much in- debted to Prof. Vincent Cardone of New York Uni- versity for pointing this out to us. A similar increase in wind speed with decreasing altitude was observed during the Salton Sea flight. However, in the absence of surface observations, it was not deemed appropriate to depart from the winds observed at 200 m, the mini- mum aircraft altitude, for our approximation of the sur- face winds. In this case, it is recognized that the true surface wind speed could be considerably higher. For the Atlantic Ocean and North Sea observations, the accuracy of the surface wind speed determinations is judged to be within 3 m sec-1.

Cloud conditions, observed visually and photo- graphically from the aircraft, ranged from clear to stralocumulus overcasts with moderate rain, over the numerous sea surface targets selected for the flights.

The 10-11 jum equivalent blackbody temperatures were taken to be equal to the sea surface temperature when measured with the infrared radiometer at the lowest altitudes. Temperatures ranged from 10C at 50N over the Atlantic to 2C over the coldest part of the North Sea.

Sea state varied from calm, with no whitecaps, tc significant wave heights of ~8 m with over 30% coverage by foam with extensive streaking. Significant wave heights were determined by analysis of the wave spectra observed with the laser geodolite. The foam coverage was determined from photographs of the sea surface with a digital densitometer. The method con- sists of numerically computing the areas on the photo- graphs above and below a chosen brightness threshold such that whitecaps, foam streaks and undisturbed sea can be differentiated quantitatively. These parameters are listed in Table 1. Due largely to the subjective nature of the choice of the thresholds, the accuracy of» this method is limited to about 15% of the value ob- tained. Percentages for each case are averages resulting from several consecutive photographs due to the vari- ation in the foam cover between individual frames.

Whenever possible, sea state, temperatures and winds measured with the aircraft were compared with the observations obtained from ocean vessels I and J (59N, 19W and 53N, 20°30'W, respectively) and with analyses made by the Irish Meteorological Service at Shannon Airport. There was never any significant dis- crepancy among these data. A complete log of all llights, including environmental and meteorological observations was compiled by Griffie et al. (1969). The specific conditions for which microwave measurements are reported here arc summarized in Table 1.

3. Results

Brightness temperatures measured at 1.55 cm during six low-altitude passes over the Atlantic and North Sea at wind speeds ranging from less than 5 to about 25 m sec-1 were selected to illustrate their dependence on

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1429 1432 10 l-

431

19 MAR

1323 1116

13 MAR 1119

1432 1020

1023 1449 I-

14 MAR

1452 1455

TIME (GMT)

1427 1430

14 MARCH

Fig. 1. Instantaneous brightness temperatures measured in the nadir direction vs time. Plot (a) corre- sponds to case A in Table 1, plots (b)-(e) to cases C-F. All brightness temperatures in (a)-(e) were observed from heights of > 'ISO m. Brightness temperatures in (f) were observed from a height ~5500 m over approximately the same location as (e).

wind speed and foam cover (Fig. 1). The recorded radiometer output was converted to radiances taking into account the calibrations performed on board the aircraft during each scan with two reference loads, one stabilized at 330K and another terminated in a liquid nitrogen dewar. Antenna and radiometer character- istics, including effects of radiation received by the antenna through side lobes outside the 2.8° diameter instantaneous field of view which were measured in the laboratory and against a known sky background prior to and after the expedition, were also taken into ac- count in this conversion. The resulting radiances are expressed as brightness temperatures (°K) and are plotted in Fig. 1 for the nadir viewing positions only. The radiometer field of view scanned from 50° left of nadir to 50° right of nadir, once every 2 sec. Thus, the traces shown in Fig. 1 consist of one data point per 2 sec. They cover time segments corresponding to the sea, cloud and wind conditions listed in Table 1.

The plotted brightness temperatures (Tb) result from three radiation components received by the radiometer radiation emitted to the aircraft by the sea surface, radiation emitted to the aircraft by clouds and atmospheric water vapor, and atmospheric radia- tion reflected toward the aircraft by the sea surface :

TB = eTWTH+(l-€)TSTH+ I TA(h)(dT/dh)dh, (1)

where Tw is the water surface temperature, Ts the sky

brightness temperature, TA the atmosphere tempera- ture, r the atmosphere transmissivity, e the surface emissivity, h height above surface, and H aircraft altitude. The first, second and third terms of (1) cor- respond to surface emission, reflected atmospheric radiation, and atmospheric emission, respectively.

The cases listed in Table 1 were chosen such that atmospheric conditions, including cloud cover, were generally similar. In each of these cases, there was no measurable precipitation from the prevailing broken stratocumulus clouds. Somewhat denser cloud cover encountered during higher wind speeds was almost compenstated for by the lower atmospheric tempera- tures prevailing in these cases. For example, we have computed that the reflected radiation component for cases A and B of Table 1 (thin clouds but warm atmosphere) contributed ~9.5C to the measured brightness temperature, while for cases E and F (thicker clouds, but cold atmosphere) this contribution was ~11C. Thus, for the conditions listed in Table 1, the reflected component due to T s can be assumed to be nearly constant, with variations certainly remaining smaller than 3C. Also, the directly received emitted atmospheric radiation was negligible when the aircraft was at low altitudes (150-200 m), since there were no clouds below the aircraft, and the transmissivity was very near unity between the aircraft and the surface. In those cases, the integral term in Eq. (1) approaches zero.

Measurements of TB were also made from high altitudes (> 5000 m) for the same conditions and gener-

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i r

X ATLANTIC, NORTH SEA

SALTON SEA «

10 20

WIND SPEED (m/sec)

30

Fig. 2. Brightness temperature differences between observations made at wind speeds <5 m sec-1 and higher wind speeds as a function of wind speed.

ally within less than 30 min of the times listed in Table 1. Brightness temperatures were 6-8C higher (depend- ing on sea surface roughness) than corresponding bright- ness temperatures observed at the low altitudes. In each case, these increases relative to the low-altitude passes account quite precisely for the emitted atmo- spheric radiation term and for the decrease of th from unity to about 0.95. The comparison between low- and high-altitude observations confirms our assertion that the measurements shown in Fig. 1 were obtained under comparable atmospheric and cloud conditions.

At this wavelength, the measured brightness temper atures are essentially independent of the sea surface temperatures within the observed range, because e varies inversely with the surface temperature such that iTw in Eq. (1) is nearly constant. Differences between the measured brightness temperatures for the various cases of Table 1 are then almost entirely due to dif- ferences in sea surface roughness. Brightness tempera- ture differences between the lowest wind condition (case A) and each of the other cases were computed and plotted vs surface wind speeds in Fig. 2. A system- atic increase in emission with increasing wind speed is clearly evident. The rate of increase is ~1.2C (m sec-1)-1. A qualitatively similar result was obtained from the data taken over the Salton Sea in 1968. This previously unpublished datum is from the same series of measurements discussed by Nordberg et al. (1969). The apparent quantitative disagreement with the 1.2C rate of increase for the North Atlantic and North Sea measurements is not deemed significant because of the large wind speed uncertainty in the Salton Sea case.

Measurements for the nadir direction only were plotted in Figs. 1 and 2. At larger nadir angles, up to 70°, we have observed proportionally larger rates of increase. Fig. 3 shows brightness temperatures as a function of nadir angle for a low and for the highest

wind speeds listed in Table 1. Although the radiomete antenna scanned only to nadir angles up to 50°, wi were able to observe radiation from nadir angles up t< 80° during banking of the aircraft. The two solid curve: in Fig. 3 were obtained by smoothing brightness tern perature averages at each nadir angle for periods o 10-20 sec during which the aircraft bank angle wai held constant at 30°. The brightness temperature rat< of change with wind speed increased from 1.2C (rr sec-1)-1 at nadir to ~ 1.8C (m sec-1)-1 at 70° from nadir This is qualitatively in accord with observations b\| Hollinger (1970), who reported an increase from 0.8C (m sec-1)-1 at 30° from nadir to 1.4C (m sec-1)-1 al 70° from nadir, for a much lower wind speed range.

The dashed curve in Fig. 3 was computed for the atmospheric and sea surface temperature conditions observed for case B, but for a specular sea surface. The absolute brightness temperatures measured at nadir for case B were ~ 15C lower than the computed tem- peratures (dashed curve). We believe that this dis- crepancy is largely due to errors in the absolute calibra-, tion of the radiometer and indicates that all brightness

2 130

120

z 110

I

o

80 -

-20

20 40

NADIR ANGLE (degrees)

Fig. 3. Brightness temperatures averaged for 10-29 sec time periods, for each antenna scan angle during 30° aircraft banks, vs nadir angle for case B of Table 1 (lower curve) and case F of Table 1 (upper curve). Absolute brightness temperatures were normalized to computations for smooth sea (dashed curve) at nadir. The dashed curve shows computed brightness temperatures for atmospheric and sea surface temperatures encountered in case B but for a smooth, specular sea surface.

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temperatures measured with this instrument should be corrected by about + ISC. This correction was made for the brightness temperatures plotted for cases B and F in Fig. 3. The relative calibration of the instrument was maintained at about ±1.5C throughout all flights.

Comparison of the slope of the dashed curve with the slope of curve B shows that the decrease of brightness temperatures with nadir angle is much steeper for a theoretical, specular and smooth water surface than for real water surfaces, even at low wind speeds. This suggests that the small-scale roughness intro- duced even by very low winds causes a considerable brightness temperature increase at large nadir angles. The slopes of curves B and F differ much less than those of curve B and the smooth water curve. This suggests that the rate of brightness temperature increase with nadir angle diminishes at the higher wind speeds. How- ever, there remains a brightness temperature increase of at least 22C with wind speed at all nadir angles, as shown by the offset of curve F compared to curve B. This offset could be caused by the greater emission from white water such as foam and spray which would produce nearly the same brightness temperature in- crease at all nadir angles, depending only on the amount of foam cover.

Fig. 2 shows that a nearly linear brightness temper- ature increase with wind speed occurs above a threshold of ~7 m sec-1. The measurements at 6 m sec-1 (case B) show no increase of Tb over the measurements at less than 5 m sec-1 (case A). There is no evidence of any brightness temperature difference between cases A and B despite the fact that the sea surface was very smooth for case A while extremely large swells (6 m) but no whitecaps were observed for case B. Monahan (1969a) has reported an abrupt increase in whitecap coverage and spray density at 7 m sec-1 and Cardone (1969) has computed that the energy available for whitecap pro- duction at wind speeds <7 m sec-1 is practically negligible. This suggests that the increase of microwave emission with wind speed, shown in Fig. 2, is related mainly to the occurrence of white water (foam and spray). At lower wind speeds, where foam does not occur, the brightness temperature measured at all nadir directions is independent of wind speed. Foam has been suspected previously as a cause for increased microwave emission (Williams, 1969; Droppleman, 1970).

Further evidence of the dependence of the micro- wave emission on foam cover can be found in the rapid brightness temperature fluctuations with time, shown in Figs, lc-le. In Fig. Id, for example, the average brightness temperature is ~132K, but, instantaneous spikes frequently reach 140K and two spikes exceed 155K. Fig. le, which corresponds to winds of 25 m sec-1, shows many more of these spikes. In this case, the average brightness temperature is ~142K, but instantaneous spikes exceeding 150K occur about every 30 sec. Several of these spikes range between 175 and

Fig. 4. Photographs with a 70-mm camera taken in the nadir direction at surface wind speeds of 16 m sec-1 (a) and 25 m sec-1 (b), corresponding to cases D and F, respectively, in Table 1.

190K. From the photographs there is a strong implica- tion that these spikes are caused by foam patches on the sea surface.

We have analyzed the instantaneous brightness tem- peratures measured at all scan angles over a period of 20 min, approximately centered on the time corre- sponding to Fig. le. to determine the amplitude and frequency of brightness temperature spikes. We found that the maximum amplitude was ~220K for seven spikes which occurred during that period. One such spike was clearly coincident with the immense foam patch photographed in Fig. 4b. The radiometer scanned the scenes shown in Fig. 4 from left to right, with the

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I 1 I l

5ALT°N SEA 1 FROM J

X ATLANTIC - NORTH SEA { PH°T°S /

D SINGLE FOAM PATCHES /

/ + WHITECAP MODEL /

CARDONE (1969) /

<\/

ox-

0

y

40 60

% FOAM COVER

100

Fig. 5. Brightness temperature differences between observations made at wind speeds less than 5 m sec-1 and at higher wind speeds as a function of foam cover as estimated from photographs, from the analytical model of Cardone, and from single foam patches covering the entire microwave radiometer beam.

aircraft having flown from bottom to top. Since the position of the scans on the photographs are not known exactly, and since at low altitudes scans were not con- tiguous, the foam patches may not always have filled the antenna field of view entirely. We assume that this occurred only when the maximum brightness tempera- tures of 220K were measured.

The photographs of Fig. 4 were taken over sea states corresponding to the brightness temperature measure- ments in Figs, lc and le, respectively. Aircraft altitudes ranged from 120 to 450 m. Fig. 4b was observed from 120 m and extends over about 200 m from top to bottom. The foam estimates (Table 1) were made from time series of photographs similar to those shown in Fig. 4. The increasing amounts of both foam patches and streaking with wind speed are quite apparent from Table 1. We assume that such streaking and foam patches, which were small relative to the radiometer field of view, raised the measured brightness tempera- tures uniformly throughout each scan, but that the largest patches of foam produced the temperature spikes which were more than 70C above the average. It is, therefore, very important that estimates of foam coverage, as they relate to the microwave emission, include the effect of both foam patches and streaking. This has been attempted with the estimates of total foam cover listed in Table 1.

The brightness temperature spikes seen in Figs. Id and le were not observed when the aircraft was at higher altitudes, where each foam patch covered an area much smaller than that resolved by the instantan- eous field of view of the radiometer. Fig. If shows brightness temperatures measured from 5500 m in the vicinity where the photograph of Fig. 4b and the measurements shown in Fig. le were made. No large spikes are evident in this case. At the aircraft height of

120 m (Fig. le) each scan spot covered an area with a diameter of ~ 7 m, while at the aircraft height of 5500 m (Fig. If) the diameter of the area covered was -275 m. In the latter case, brightness temperatures show a much smoother pattern with no significant spikes be- cause the characteristic diameter and spacing of the largest foam patches were less than ~ 100 m (Fig. 4b) and individual patches were not resolved by the radiometer.

Brightness temperature differences were plotted vs foam coverage in Fig. 5, as determined from the photo- graphs (solid line). There is a similar increase of bright- ness temperature with foam cover, as there is with wind speed. However, the rate of increase obtained from the small-scale, single foam patch measurements, each repre- senting 100% foam cover (dashed line), is considerably greater than the rate determined from the large-scale observations derived from the photographs for less than 40% foam cover (solid line). There are two possible explanations for this discrepancy :

1) The estimates of streaking which account for a large portion of the white water coverage as determined from the photographs (Table 1) are subjective, though internally consistent. Thus, foam cover as determined from the photographs may have been overestimated. This is also suggested by the fact that if foam cover is taken from Cardone's (1969) model, corrected for salt water after Monahan (1969b), brightness temperature increases are consistent with the rate obtained for 100% foam cover (dashed line) which is independent of the estimates made from the photographs. The uncertainty of estimating Whitewater coverage from photographs and the possibility of overestimating foam cover has been pointed out recently by Blanchard (1971).

2) Another possibility is that the total white water estimates made from the photographs are correct but that the effect of the streaks on the microwave emission is smaller than the effect of the whitecaps which produce the 100% foam cover spikes. In this case, the agreement with Cardone's model would be purely coin- cidental. Further microwave measurements under con- trolled conditions of foam and streaking should resolve this point.

It is noteworthy that the Salton Sea measurements made on 5 June 1968 are generally consistent with the North Sea and Atlantic measurements with regard to brightness temperature dependence on both wind speed and on foam cover.

Preliminarv results from the 3-cm radiometer, flown simultaneously with the other instruments, indicate that the brightness temperature increase at this wave- length is about 8C for a wind speed increase from calm to 13 m sec-1. Beyond 13 m sec-1 there is only a negligi- ble increase in brightness temperature. However, because of calibration uncertainties, the 3-cm measure- ments cannot be considered as firm as those at 1.55

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cm. We are indebted to Messrs. F. Barath and J. Blinn of the Jet Propulsion Laboratory and A. Edgerton of Aerojet General Corporation for making this, as yet unpublished, information available to us.

4. Conclusions

There is a definite increase in the thermal emission at 1.55 cm from the sea surface with increasing wind speed. On the average, this increase amounts to about 22C in the nadir direction and 32C at 70° from nadir for a wind speed increase from 7 to 25 m sec-1. For very low wind speeds, up to about 7 m sec-1 when foam cover is negligible, there is no increase in bright- ness temperatures. Compared to calm sea states, brightness temperatures are ~100C higher when foam patches covering the radiometer field of view are ob- served. We conclude that the increased emission at 1.55 cm from a wind-driven sea surface is primarily due to white water cover, while the effect of the wave slope geometry is negligible. The microwave emission at 1.55 cm from the sea surface is therefore a sensitive indicator of white water coverage and of wind speed at all nadir angles, at least to 50°.

We believe that an important parameter involved in the interaction between air and the sea surface, namely, the energy expended in the production of white water, can be inferred from microwave brightness tempera- ture measurements provided that: 1) the consistent relationship between white water occurrence and wind speed reported here is confirmed; and 2) microwave measurements are made at various wavelengths, both polarizations, and over a large range of nadir angles to separate the various effects of foam cover, cloud cover, and atmosphere and sea surface temperatures on the microwave emission.

Results from the observations reported here might provide a basis to test further developments or re- visions of analytical models relating microwave emis- sion to sea surface roughness.

Acknowledgments. There were several dozen indi- viduals without whom these observations would not have been possible. We are unable to name all of them,

but we acknowledge their dedicated contributions gratefully. We are especially indebted to the NASA pilots and flight crew of the CV 990 observatory for carrying out the demanding flight operations that were required for these observations, to Mr. Earl Peterson of the NASA Ames Research Center for organizing the expedition, and the Irish Meteorological Service for providing excellent weather forecasts and analyses to support our flight operations.

REFERENCES

Blanchard, D. C, 1971: Whitecaps at sea. /. Atmos. Sci., 27 (in press).

Cardone, V. J., 1969: Specification of the wind field distribution in the marine boundary layer for wave forecasting. Geo- physical Science Lab., New York University, Rept. TR69-1.

Droppleman, J. D., 1970: Apparent microwave emissivity of sea foam. J. Geophys. Res., 75, 696-698.

Griflee, L., J. Ledgerwood, D. Hill and W. E. Marlatt, 1969: Support data for NASA Convair 990 meteorological flight IV. Dept. Atmos. Sci., Colorado State University, Ft. Collins, 83, pp.

Hollinger, J. P., 1970: Passive microwave measurements of the sea surface. /. Geophys. Res., 75, 5209-5213.

Monahan, E. C, 1969a: Freshwater whitecaps. J. Atmos. Sci., 26, 1026-1029.

, 1969b: Laboratory comparisons of freshwater and salt

water whitecaps. /. Geophys. Res., 74, 6961-6966.

NAS Summer Study, 1966. Useful applications of earth-oriented satellites. Summer study on space applications, National Academy of Sciences, Washington, D. C.

Nimbus III User's Guide, 1969: Staff Members, Nimbus Project, NASA, Goddard Space Flight Center, Greenbelt, Md.

Nordberg, W., J. Conaway and P. Thaddeus, 1969: Microwave observations of sea state from aircraft. Quart. J. Roy. Meteor. Soc, 95, 408.

Oister, G, and C. V. Falco, 1967: Microwave radiometer design and development. Final Rept., Contract NAS5-9680, Aerojet- General Corp., Space Division, El Monte, Calif.

Ross, D. R. V. Cardone and J. Conaway, 1970: Laser and micro- wave observations of sea surface conditions for fetch limited 35 to 50 knot winds. IEEE Trans. Geoscience Electronics, GE-8 (in press).

Stogryn, A., 1967: The apparent temperature of the sea at micro- wave frequencies. IEEE Trans. Antennas Propagation, AP-15, 278.

Williams, G. F., Jr., 1969: Microwave radiometry of the ocean and the possibility of marine wind velocity determination from satellite observations. J. Geophys. Res., 74, 4591-4594.

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Reprinted from IEEE Transactions on Geoscience Electronics GE-9 , No. 4, 197-198.

Introductory Remarks.

SEA-AIR INTERACTION INSTRUMENTATION

Problems of the interaction between the atmosphere and the ocean have confronted man ever since he left his homestead in the urge to expand his horizon and to conquer new frontiers. In his search for food and the riches of his environment, he had to master the winds, waves, and ocean currents; and these factors are primarily the result of air-sea interaction. More recently, the less obvious, but perhaps in many respects equally important, aspects of air-sea in- teraction have been stressed, namely, the influence of the ocean on the atmosphere in producing weather and climates. This is reflected in the present effort to gain a better understanding of the processes occurring at the sea surface and in the adjoining boundary layers in order to better parameterize the major exchanges of momentum, heat, and moisture.

The importance of the oceans to the global environment lies in the fact that more than two-thirds of the surface of this planet is covered by water with its very special and unique physical properties. This has profound effects on the atmosphere, since most of the energy received from the sun is absorbed by the water. Again, most of this absorbed energy in the water is released in the form of latent heat during the evaporation process. Thus the ocean provides a large portion of the moisture supply to the atmosphere and heats the atmosphere when the latent heat of evaporation is freed upon con- densation of water vapor in the atmosphere. This heat represents the main fuel which drives the atmospheric circulation. It is therefore no surprise that large-scale experiments, such as the 1969 Barbados Oceanographic and Meteorological Experiment (BOMEX), have been conducted recently to investigate air-sea interaction processes. Others are planned for the future, such as those within the framework of the Global Atmospheric Research Program (GARP), which are designed to investigate how air-sea processes relate to large- and small-scale convective atmospheric systems.

Recently, advances have been made in several problem areas. Numerical atmospheric circulation models have been successfully coupled through air-sea interaction with ocean circulation models. Correlations between positive sea surface temperature anomalies in the Northern Pacific and dry and cold winters in the Eastern portion of the United States have been found, suggesting a strong large-

scale interaction between ocean and atmospheric circulation patterns.

Obviously, such large-scale investigations require data coverage on the global scale. Although the general climatological coverage has been obtained from data collected during the last hundred years by merchant and other ships, vast areas outside the regular shipping lanes are poorly covered. With the development of indirect sensing techniques and man-made satellites and the considerable effort spent in technology, global coverage for observing ocean surface parameters such as temperatures, salinity, waves, winds, tides, and ocean cur- rents appears possible. Present planning for oceanographic satellites is concentrated on the feasibility of obtaining many of these pa- rameters from space.

On the other hand, direct and indirect sensing techniques to be employed from surface platforms also need further development in order to provide ground truth ,i\»\ to investigate the important processes that govern air sea exchanges. A most pressing need exists to obtain a better understanding of planetary boundary layer dy- namics. Here, Doppler radar and acoustic sounding techniques seem to be the most promising tools for studying the three-dimensional structure of the boundary layer of the air. Some pertinent work on related problems may be found in the Prodizedings of the IEEE (Special Issue on Remote Environmental Sensing, April 1969).

This issue, then, is organized in three parts: direct sensing of the boundary layer structure, remote sensing of the sea surface parame- ters, and laboratory studies of the water surface perturbed by waves and foam.

The paper by Garstang el al. provides an excellent summary and description of the marine atmospheric boundary layer and some of the transfer processes germane to the subcloud layer. Although some previous boundary layer observations exist, mainly over land and made from high towers, the technique described in this paper is a ship-deployed instrumented platform capable of providing unique time-series data from the atmospheric boundary layer over the ocean. Somewhat more limited in its use (nearshore areas) is a tracking system, described in the paper by Dunkel el al., which permits wind profiles to be observed in the atmospheric boundary layer using rapid releases of pilot balloons. This system has been successfully

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IEI E TRANSACTIONS ON GEOSCIENCE ELECTRONICS, OCTOBER 1471

applied in an experiment just concluded over the Grand Bahama Banks. Some 400 wind profiles have been obtained in conjunction with other pertinent observations.

The next two papers deal with remote sensing of ocean waves. In his paper, league describes a technique by which long wavelength directional wave spectra can be observed for an area of several hun- dred kilometers offshore using LORAN A transmissions. This tech- nique may prove a convenient way to monitor offshore wave condi- tions. The paper by Chadwick and Cooper shows that with presently available radar technology it should be possible to estimate wave heights, at least from aircraft. Through functional relationships between wind speed, letch, and duration, possibly wind speed could be estimated by this technique.

Finally, a very important problem in the application of indirect microwave teciniques is the knowledge of the emissivity of foam and bubbles, which are generated extensively by breaking waves and strong winds. Williams, in his paper, presents results of labora- tory experiments that will be helpful in the interpretation of micro- wave data.

In closing, I would like to emphasize that the collection of papers in this issue represents a small sample of present scientific endeavors in the field of air-sea interaction. It is gratifying to see that a sig- nificant effort is now being made to bring to bear the advances in technology of the last 10 or 20 yeats in helping to solve our environ- mental problems.

Fe:odor Ostapoff, Guesl Editor

Feodor Ostapoff was born in Danzig on March 19, 1925. He studied physics, mathematics, and chemistry at the University of Marburg, Marburg, Germany, and received the German equivalent of the B.S. degiee in physics in 1949. He studied physical oceanography at the University of Kiel, Kiel, Germany, and re- ceived the M.S. degree in physical oceanography from New York University, New York, N. Y., in 1957.

In 1959 he joined the U. S. Weather Bureau as a Research Scientist and was engaged in Antarctic research. Since 1964 he was heavily involved in the coordination and implementation of the Federal air- sea interaction program, especially after the formation of the Environmental Science Services Administra- tion. This program culminated in the Barbados Oceanographic and Meteorological Experiment in 1969, which he helped plan and organize. Presently he holds the position of Director of the Sea-Air Interaction Laboratory of the National Oceanographic and Atmospheric Administration.

Mr. Ostapoff is a member of the American Geophysical Union and American Meteorological Society, serving on the Committee on the Interaction of the Sea and Atmosphere. He is also a member of Sigma Xi. He also serves the Cooperative Investigations of the Caribbean and Adjacent Region (CICAR), an international program with some 15 nations participating and sponsored by the Intergovernmental Oceanographic Commission of UNESCO, as Assistant International Coordinator (Meteorology) ap- pointed by the World Meteorological Organization.

71

Repr inted from Proceedings of the Symposium on Investigations and Resources of the Caribbean Sea and Adjacent Regions , 137 -145 .

OCEAN-ATMOSPHERE INTERACTION IN THE CARIBBEAN SEA VIEWED FROM THE O C E A NOG R A P HI C SIDE

Feodor Ostapoff

1. INTRODUCTION

The title of my paper is rather broad and while listening to my colleagues yesterday and today it became obvious that many aspects of ocean-atmo- sphere interactions have been discussed directly or indirectly.

Perhaps the most direct visual evidence of the effects of the atmosphere on the sea surface are the waves and wavelets which have been the subject of intense study for the past 200 years. The same driving forces establish the general circulation of the ocean. As early as 1686, Halley concluded that the surface circulation of the ocean is wind driven. Today the theory of wind driven ocean circulation has advanced to a considerable degree of sophistication. In addi- tion the ocean is heated and cooled at the surface, in other words , its heat sources and sinks are essentially at the same geopotential , forming dis- tinct water mass characteristics. The strength of the heat and salinity sources and sinks is de- termined by climatic conditions on the globe. Once the water masses are formed at the sea surface due to heating, cooling, evaporation and precipitation, ice formation and melting, they will seek their equilibrium position in the ocean ac- cording to their density. Combination of the wind driven mode and the internal pressure distribution then spreads these water masses with their speci- fic characteristics through the oceans, modifying them through turbulent mixing. Thus, Wiist and Gordon (1964) identify in the Caribbean Sea four "core layers" : the sub-tropical underwater, the sub-Antarctic intermediate water, the North Atlantic deep water, the Caribbean bottom water. In this sense then, we must recognize an ocean- atmosphere interaction process in the Caribbean Sea. Although direct effects forming the water masses occur in remote areas perhaps tens or hundreds of years earlier, these are the large- scale (in time and space) interactions.

Figure 1 (after Wyrtki , 1967) illustrates the distribution of the main water masses at the sea surface and boundaries between these water masses. Clearly, the area of our topic is influ- enced by a very complicated and complex mecha- nism .

At the other end of the spectrum , we recog- nize small-scale interactions - perhaps it would be better to call them "first order" interactions - which act locally and are highly variable. Consi- derable research has been done in this field during the past few decades. The importance of this re- search lies in the fact that neither of the large- scale phenomena can be fully understood without an intimate knowledge of the first order interac- tion, nor can specific characteristics such as the sea surface temperature and salinity, the mixed layer depth and the thermocline be treated theo- retically in a satisfactory way. Let us first briefly discuss these first order interactions.

2. BASIC PROCESSES ACROSS THE SEA SURFACE AND THEIR SIGNIFICANCE

The exchange across the sea surface involves a number of important quantities.

They can be classified in three main catego- ries, as shown in Figure 2.

(1) Momentum exchange

(2) Heat exchange

(3) Mass exchange

Momentum exchange is one of the most impor- tant interaction quantities from the oceanographic point of view, as discussed above. While the mo- mentum loss by the atmosphere is of perhaps neg- ligible consequence to the atmospheric circulation, it represents the major force which generates and maintains surface waves and drives local and major ocean currents. Indeed, the early results in ocean dynamics are based on the momentum exchange process. In this connexion we need only mention Ekman's work.

The total heat exchange can be differenti- ated depending on the process involved. First of all, 80% of the short-wave radiation received from the sun at the ocean surface is absorbed in the top layer of the ocean. Long-wave radiation is emitted from the ocean's surface a. absorbed partially in the atmosphere. Sensible h.-at is ex- changed by conduction due to the difference in temperatures between the two media. But most importantly, the ocean is cooled by evaporation of water, resulting in latent heat exchange. This

138

Feodor Ostapoff

Figure 1. Distribution of the main water masses at the sea surface and boundaries between these water masses.

process and the associated water transport from the ocean to the air is of utmost importance from the energetic point of view to the generation and maintenance of the atmospheric circulation, in- cluding hurricanes and tropical storms. Evapo- ration and precipitation, of course, determine also to a large extent the salinity distribution in the ocean.

The most important masses exchanged at the surface are water vapour (in conjunction with the exchange of latent heat) , the return of water in the form of rain (thereby releasing latent heat in the atmosphere) , salt and gases. The latter are again instrumental in important physical processes in the atmosphere.

In view of the complexity and the numerous modes of interaction, we will discuss in the fol- lowing only a few of the important oceanographic processes which seem particularly suited for study in the Caribbean Sea - our main topic today.

3.

PRECIPITATION AND THE PRESSURE FIELD IN THE OCEAN

An often neglected but apparently important effect is that of precipitation which, in these latitudes, is more localized and more intense than in other parts of the world ocean.

Last summer, the USC&GS ship "Discoverer" (Figure 3) occupied a station some 60 miles east of Barbados for about 2 months, more or less

continuously. Three-hourly surface salinities (bucket) were observed and six -hourly STD lower- ings were made. During a heavy rain shower, the surface salinity dropped abruptly by 0.7 to 1 part per thousand for about 24 hours, while the 10 me- tre salinity followed a longer-term trend (Figure 4).

The implication for dynamic height calcula- tions , the basis for all geostrophic calculations , seems considerable.

Let us perform a hypothetical experiment in our minds as follows : we calculate dynamic depths for one of the regular stations which were obtained during the expedition. Then we replace the surface salinity value by a value of one part per thousand less than the original observation. Using standard oceanographic procedures, and not knowing how deep this lens is , the calculation was made for the usual standard depths of 0 , 25, 50,

MOMENTUM HEAT

MASS

Figure 2. Air-sea interactions.

Ocean-atmosphere interaction in the Caribbean sea

139

Figure 3.

S o/oo

17 AUGUST 196S

Figure 4. Surface bucket salinities (solid line) and 10 meter salinities (circles) 60 miles east of Barbados.

75, 100 metres etc. Comparing the two calcula- tions, one finds at 25 metres a difference of 2 dyn. cm. between the two "stations". Moreover, if the two "stations" were 30 miles apart (and such variability in rain may very well occur in those latitudes) an additional "current" of about 2 knots would result in these low latitudes.

4. THE EFFECT OF HURRICANES ON TEM- PERATURE STRUCTURES IN THE TOP LAYERS OF THE OCEANS

Next, I wish to discuss the effects of hurricanes on the ocean, a very pertinent subject if we con- sider the Caribbean Sea. Possibly, an opportunity will present itself to continue research along those lines .

In 1964, when Hurricane Hilda cross the Gulf of Mexico an opportunity arose to study the direct effects of a hurricane on the thermal structure of the open ocean. Leipper (1967) had surveyed the area prior to the passage of the hurricane. When the hurricane traversed the area a new expedition

140

Feodor Ostapoff

§f »r

»r M'

HILDA CRUISE DATA MERCHANT SHIPS DATA- INADEQUATE DATA

Figure 5. Sea-surface temperature, after Hilda. October 1-13 inclusive. Including Cruise Hilda and BCF data (shaded area > 28° ; stippled area < 25°). [After Leipper, 1967]

was quickly organized and remarkable data obtained.

Figure 5 shows the sea surface temperature distribution after Hilda. The general surface temperature prior to Hilda was about 29°C. A lowering of about 6°C was observed. Even more remarkable are the vertical temperature profiles. An example is given in Figure 6.

If upwelling due to divergence induced by the wind stress is the process responsible for lower- ing the surface temperature , then the water may have come to the surface from about 60-80 metre depths.

Figure 7 shows the density distribution along the same cross section as in Figure 6.

The gross features of upwelling can easily be explained by Ekman's wind drift theory. The transport in the Ekman layer is outward from the centre of the storm , producing divergence from the centre up to the distance of maximum winds and convergence further out. Therefore, upward motion is indicated left and right of the eye with maximum vertical velocity at the radius of maxi- mum winds and downward motion at the outer fringes of the storm (about twice the radius of maximum wind stress). Now, since the storm is radially symmetric, the hurricane should leave one cold water trace at the surface. However, in low latitudes and with an east-west propagation of the storm two upwelled regions may be generated

Ocean-atmosphere interaction in the Caribbean sea

141

POSITION OF HURRICANE EYE

STA. NO. 15

V VWv

Figure 6. Depth of isotherms in section across path, after Hilda. [After Leipper, 1967]

due to the difference in Coriolis parameter (every- thing else being equal). For a storm of 30 miles radius of maximum winds, the Coriolis parameter could change almost by 10%. Such an effect has not been clearly observed yet, but all our mea- surements were taken in the Gulf of Mexico. A more elaborate transient .(although with a station- ary storm) numerical model has been developed by J.J. O'Brien and R.O. Reid (1967) and J.J. O'Brien (1967) which agrees with major parts of the observations.

Present technology permits the rapid collec- tion of sea surface temperatures from aircraft using infra-red radiation thermometers. Fur- thermore, expendable bathythermometers have been developed for use from aircraft. Indeed, expendable salinity -temperature probes are in the offing.

Examples of radiation temperature observa- tion in the wake of Hurricane Betsy in 1965 are given in Figures 8 and 9. These data were ob- tained by J. McFadden (1967) from ESSA research aircraft. While data obtained from a ship must be

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Figure 7. Depth of contours of density anomaly 0", across path, after Hilda [After Leipper, 1967J

composite in nature (anywhere from 8 to 14 days) the aircraft can span the same area within a few hours. With the additional technique of sampling temperature and salinity vertically a powerful research tool becomes available. Not only can the detailed structure of the ocean be explored on a synoptic basis , but this technique also enables study of the important question of the relative permanence of the observed changes.

This could be accomplished by repeated flights over the hurricane path to obtain a time history of the event. The Caribbean Sea may be ideally suited to investigate these questions and bring us closer to understanding strong interactions and the response of the ocean to these interactions.

5. MODELLING OF EXCHANGE PROCESSES

Finally , I wish to touch briefly on a recent effort in modelling exchange processes. This work is being carried out primarily by J. Pandolfo with support of the Sea Air Interaction Laboratory.

The model represents a complex local simu- lation of the atmosphere -ocean planetary boundary layer (Pandolfo and Brown, 1967; Pandolfo and Atwater , 1968) which extends from depths of a few hundred metres (say 400 m) in the ocean layer to heights of about a kilometre in the atmo- spheric layer. The principal processes are the eddy fluxes , mixing due to wind induced waves at the sea surface and radiative heating, which de- pends on cloud cover.

At the sea surface the following conditions are imposed: continuity of eddy shearing stress, con- tinuity in the velocities in both media , continuity in temperature , saturation of the air by water vapour , and a balance between evaporation and

142

Feodor Ostapoff

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Figure 9. Sea-surface temperature distribu- tion 15 September 1965. [After McFadden, 1967]

Ocean-atmosphere interaction in the Caribbean sea

143

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^*^

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MODEL

1100 1600 2100 0200

Figure 10. [After Pandolfo, 1968

MODEL

^x x DEFANT

1100 1600 2100 0200 0700 LT

Figure 11. [After Pandolfo, 1968]

salinity. Conditions at the top and bottom of the model are prescribed.

A few examples may illustrate the presently available results although the full power of the model has not yet been explored.

The agreement between the two curves is quite satisfactory. In particular the occurrence of the maximum and minimum agrees very well, both in the salinity and temperature curves. (Figures 10 and 11). It is noteworthy that the salinity maximum follows the temperature maxi- mum by about 3 hours. Also, the small secon- dary salinity maximum is reproduced in agree- ment with observations. This secondary maxi- mum is related to maximum vertical mixing in the ocean, which occurs at the same time.

The observed diurnal salinity amplitude is about five times larger than the computed value. This indicates a deficiency in the model, possibly due to the fact that at this time precipitation had not been incorporated.

The vertical temperature and salinity distri- bution is shown in Figure 12. The initial temper- ature and salinity profiles were assumed linear. Again the calculated temperature profile com- pares quite favourably with observations obtained this summer (1968) on the Discoverer. The Dis- coverer data shows a mixed top layer of 15 to 17 metres. The model calculates a mixed layer depth of 20 metres. The temperature difference between 20 metres and 100 metres amounts to 4.5°C. Observations showed a difference of 3°C. The salinity profile disagrees with observations , not so much in the mixed layer as in the complete lack of the salinity maximum at about 100 metres. Clearly a single station model incorporating local processes cannot simulate such phenomena as water mass advection.

The vertical current distribution at one par-

-10

-20

-30

-40

I "50

-60

-70

-80

-90

O Temperature X Salinity

-i 1 1 i x-o

A

X -t X X -6)

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xo

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s<o/0o>

35.400 35.420 35.440 35.460 35.480 35.^00 -100 I dt 1 1 1 1

294

295

296 297 T(°K)

298

299

300

Figure 12. Oceanic temperature and salinity profiles at one time step in the run JB1 ; 0530 LST. [After Pandolfo, 1968]

144

Feodor Ostapoff

l (cm sec ')

Figure 13. Wind current hodographs at one time step in the simulation run JB1 ; 0930 LST. [After Pandolfo, 1968]

ticular time step in the integration is shown in Figure 13. Variations with inertial periods are superimposed on the current vector.

The mean angle between surface current direction and the surface wind direction is about 30°.

This model is being further developed, prin- cipally to expand areawise and to include advec- tive processes in the ocean and the atmosphere. An observational programme could be carried out during Cicar to utilize the model in further understanding changes occurring in the near sur- face layers of the ocean.

6. CLOSING REMARKS

In closing, I would like to emphasize that I have only touched briefly on a few problems which may

40 be interesting or important to oceanographers if

we concern ourselves with the air -sea interaction problem in relationship to oceanography.

Many problems of interaction are of a funda- mental nature and can be studied anywhere in the world ocean. However, we must still distinguish between climatic regimes which may favour one 7~ exchange process over the other, making the v choice of an experimental area an important one g if we want to isolate and study one aspect of inter - action. This is certainly true as far as our sister science, meteorology is concerned, where con- vective processes are a predominant process in low latitudes while air mass modification may be studied better in regions where drastic differen- ces in air masses occur. In oceanography con- vective mixing may be the predominant process of high latitudes where deep water masses are formed.

The Caribbean Sea has been studied exten- sively if we consider large-scale exchanges from the meteorological point of view. Essentially, the meteorological island network surrounding the Caribbean Sea has been utilized b,y applying continuity considerations. We need to mention only the works by J. Colon (1963), Malkus (1962), Hastenrath (1967) and Rasmusson (1967 and 1968). Evidently, this work could continue in support of the planned Cigar activities. Within this frame- work specific problems may be studied for which the Caribbean Sea may present itself as a natural laboratory.

In closing I would like to quote a few words from J. Malkus (1962) which may be worth rem- embering when planning our future work. She writes : "Rarely, but often enough to be of ines- timable value, nature herself performs an ex- periment under partially controlled conditions , as we have seen in some of the trade wind cases; one of the main skills of the earth scientist lies in being able to recognize and exploit these, using them to guide his measurement programmes and as a framework within which to relate the results . "

REFERENCES

Colon, F.A. 1963. Seasonal variations in heat flux from the sea surface to the atmosphere over the Caribbean Sea. Journ. Geoph. Res. , 68, 5, p. 1421-1430.

Defant , A. 1961. Physical Oceanography , New York, Pergamon Press, 2 vols.

Hastenrath, S.L. 1967. Diurnal fluctuations of the atmospheric moisture flux in the Carib- bean and Gulf of Mexico area. Journ. Geoph. Res. , 72, p. 4119-4130.

Leipper , D.F. 1967. Observed ocean conditions and Hurricane Hilda , 1964. Journ. Atmos. Sci. , 24, p. 182-196.

Malkus, J.S. 1962. Large-scale interactions , The Sea (ed. M.N. Hill), V, 1 , p. 88-294, Interscience Publ. , New York, J. Wiley & Sons.

McFadden , J.D. 1967. Sea surface tempera- tures in the wake of Hurricane Betsy (1965). Monthly Weath. Rev. , p. 299-302.

Ocean-atmosphere interaction in the Caribbean sea

145

O'Brien, J.J.: Reid, R.O. 1967. The non-linear response of a two layer , baroclinic ocean to a stationary, axially symmetric hurricane, Part I. Upwelling induced by momentum transfer. , Journ. Atmos. Sci. , p. 197-207.

O'Brien, J.J. 1967. The non-linear response of a two layer, baroclinic ocean to a station- ary, axially symmetric hurricane: Part II. Upwelling and mixing induced by momentum transfer. Journ. Atmos. Sci. , p. 208-215.

Pandolfo, J.P.: Atwater , M. A. 1968. Varia- tions of diurnal and inertial period in a phy- sical-numerical model of the atmosphere- ocean planetary boundary layer. Final Re- port, 7046-321 , Contract E-120-67(N). Hartford, Conn. , The Travelers Research Center , Inc. ,

Pandolfo, J.P. : Brown, P.S. Jr. , 1967.

Inertial oscillations in an Ekman layer con- taining a horizontal discontinuity surface. Journ . Mar. Res. , 25, p. 10-28.

Rasmusson, E.M. 1967. Atmospheric water vapour transport and the water balance of North America : Parti. Characteristics of the water vapour flux field. Monthly Weath. Rev. , 95, p. 403-426.

Rasmusson, E.M. 1968. Atmospheric water vapour transport and the water balance of North America : Part II. Large-scale water balance investigations. Monthly Weath. Rev. 96, p. 720-734.

Wust, G. : Gordon, A. 1964. Stratification and

circulation in the Antillean -Caribbean basins. Part I. Spreading and mixing of the water types. New York and London, Columbia University Press, 201 p.

Wyrtki, K. 1967. Water masses in the oceans and adjacent seas, in: International Dic-

tionary of Geophysics (gen . Pergamon Press.

ed. K. Runcorn).

72

U.S. DEPARTMENT OF COMMERCE National Oceanic and Atmospheric Administration

Environmental Research Laboratories

NOAA Technical Memorandum ERL AOML-15

TESTS OF MODIFIED RADIOSONDE HYGRISTOR DUCT

Willard W. Shinners Gerald E. Putland Peter B. Connors

Atlantic Oceanographic and Meteorological Laboratories Miami, Florida December 1971

TABLE OF CONTENTS

PAGE

1 . I NTRODUCT I ON

2 . AIR FLOW TESTS

3 . FL I GHT TESTS k. CONCLUSION 5. REFERENCES

1

3

5

6

10

TESTS OF MODIFIED RADIOSONDE HYGRISTOR DUCT

Willard W. Shinners, Gerald E. Putland, and Peter B. Connors

To evaluate a modified configuration of the National Weather Service's radiosonde humidity duct, wind tunnel and flight tests were made by the Sea-Air Interaction Laboratory. Results indicate the new design to be greatly improved over the previous type with respect to ventilation and radiational heating.

1 . INTRODUCTION

The VIZ Corporation provided the NOAA Sea Air Interac- tion Laboratory several newly designed hygristor housings or ducts for wind tunnel and flight tests similar to the origi- nal tests by SAIL reported in NOAA Technical Report 19^-AOML ^ "Some Tests on the Radiosonde Humidity Error." The 1970 report indicated the ventilation in the area of the hygristor was reduced about 70% from ambient air flow, and the trans- 1 ucency and reflective characteristics of the plastic duct permitted considerable solar heating of the hygristor resulting in significant humidity errors.

The newly designed duct provides a much larger opening or air scoop than the prior design. The air passes through a restricted section holding the hygristor, and as a result

the air movement is accelerated. Air entering the scoop of

2 2

58 cm area passes through the restricted area of 23 cm

cross-section with over 100% increase in speed from the scoop

area to the exit of the hygristor chamber (fig. 1). A black

covering under the top and at the bottom of the hygristor

section is highly effective in reducing direct and reflected

solar heating of the hygristor.

Figure 1. New design of NWS hygristor duct. Cover removed

2. AIR FLOW TESTS

Tests were conducted in SAIL's wind-water tunnel facility, (NOAA Tech. Memo ERL AOML-12). The facility provides an air chamber 70 by 90 cm in c ross -sec t i on and 610 cm in length. Air flow was 5-2 mps - about the rate of ascent of a radio- sonde. A Pitot tube and a The rmo-Sys terns , Inc., hot wire (constant temperature anemometer) model 1050 was used to monitor air flow rates.

The duct with a carbon hygristor in place was placed in the wind tunnel and a series of readings at 1 -cm spacing were made along line A-B (fig. 1). The probe was even with the top of the side wall of the scoop. Table 1 lists these values .

Table 1. Air flow at air scoop entrance

mps

Cm Left 5 k

Center 1 0 1

Cm Ri ght k 5

1.9 2.0 2.0 2.1 2.1 2.1 2.2 2.2 2.2 2.2 2.0

■B

The data give an average value of 2.1 mps for air enter- ing the air scoop along A-B. This is kQ% of the ambient 5-2 mps flow rate in the tunnel. Measurements were made up-wind from the duct air scoop at a distance of 7-6 cm, where a speed of 3-6 mps was recorded. At a distance of 15-2 cm upwind the speed was h.k mps.

Measurement of the air flow right at the hygristor posed a problem due to the probe support and connecting cables. Since the cross sectional area is nearly constant and uniform in dimensions from the air scoop to the discharge orifice, the assumption was made that the air speed at the hygristor would be essentially the same as in the discharge area. Measure- ments were made at 1 cm intervals from the center line along line C-D. Table 2 presents average values.

Table 2. Air flow in discharge orifice

Cm Left 5 k

Center 1 0

Cm Right 3 4 5

mps 5-3 5-4 5-4 5-0 4.4 4.8 4.1 5-2 5-0 5.0 4.9

The mean value across the discharge orifice was 5.0 mps, over SS% of ambient flow in the wind tunnel.

Since lee or down-wind turbulence could affect the air flow through and past the duct, a 403 mc radiosonde, without the thermistor out-rigger or strap was included for a second series of measurement.

Values in Table 3 were obtained 2 cm above the air scoop at 2-cm intervals along line A-B.

Table 3- Air flow 2 cm above air scoop with radiosonde

Cm Left Center Cm Right 4 2 0 2 4

A B

mps 2.9 2.6 2.4 2.4 2.6

A mean value of 2.6 mps is obtained from the above data. The higher value at 2 cm above the orifice is consistent with the increase in speed-up wind.

Measurements across the exit orifice provide the f o 1 1 ow i ng :

Table 4

Wind speed at discharge orifice -duct with radiosonde

Cm Left Center Cm Right 4 2 0 2 4

C D

mps 5.4 4.6 4.2 5-0 5-4

A mean value of k .9 mps results for flow through the duct. A recheck of air flow up-wind of the duct resulted in identical values to those obtained prior to the inclusion of the full radiosonde in the tests. The 0.1 mps difference (5-0 and k .S mps) does not appear significant, and the exper- imental procedure followed does not indicate a change in ven- tilation rate when the duct and radiosonde are combined (i.e., without the thermistor or webbed strap in place).

3. FLIGHT TESTS

To determine the effectiveness of the new duct under operational conditions, several flights were made at Miami. Releases were made close to solar noon In order to expose the duct to maximum radiotonal effect. Air mass characteris- tics were typica of the trade winds, with a warm moist layer the first several hundred meters, then an inversion and rela- tively dry air above. Two radiosondes were flown on the same train, one with the older duct configuration and one with the new design. A further comparison was made with the vertical duct used by SAIL (Ostapoff, et al., 1970) and the new design. Figure 2 thru 6 present the comparative relative humidity values as obtained by the dual flights.

Figure 2 indicates differences as high as 20% in rela- tive humidity with the difference varying up to 830 mb . The sonde with the new duct showed lower relative humidity above this level. Scattered clouds and the resultant shading may account for the variability at the lower level. The reversal above 825 nib, where the standard sonde indicated higher hu- midity, has been observed before (Brousaides and Morrissey, 1971); however, a confirmed explanation is not available.

A maximum difference of 32% in RH at 835 mb appears in figure 3 with the newly designed duct configuration giving a 97% RH value. Figures k and 5 are typical of comparative flights in which solar heating was substantially reduced and

ventilation of the hygristor improved relative to the standard sonde.

Figure 6 presents curves for the new NWS duct and a vertical tube used by SAIL (Ostapoff, et al., 1970). The sondes were observed to swing through a large arc during the first few minutes of flight, and it is suspected that some solar heating as well as reduced ventilation in the tube may account for the differences in RH during the early part of the f 1 i ght .

k. CONCLUSION Based on these wind tunnel and flight tests, the new National Weather Service radiosonde duct virtually eliminates the solar heating problem found in the previous duct config- uration. The problem of thermal lag should also be reduced to a considerable extent with the increased ventilation rate.

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5. REFERENCES Broussaides, F. J., and Morrissey, J. F. (1971), Improved

measurements with a redesigned radiosonde humidity duct,

Bulletin AMS , 2, No . 3 . McLeish, Wm . , Berles, R., Everard, W., and Putland, G. (1971),

The SAIL 6-m wind-water tunnel facility, NOAA TM ERL

AOML- 1 2 . Ostapoff, F., Shinners, W., Augstein, E. (1970), Some tests

on the radiosonde humidity error, NOAA TR ERL I9A-AOML k.

10

USCOMM ML

PENN STATE UNIVERSITY LIBRARIES