design and wind tunnel testing of a size sampling in-situ net system (ssisnetJ Robert Paul Mitchke «*^. ^J^ ^ TtifrVz NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS DESIGN AND WIND TUNNEL TESTING OF A SIZE SAMPLING IN-SITU NET SYSTEM (SSISNET) by Robert Paul Mitchke September 1976 Thesis Advisor E. D. Traganza Approved for public release; distribution unlimited. 7 ns SECURITY CLASSIFICATION OF THIS PAGE (Whan Data £nt»r»d) REPORT DOCUMENTATION PAGE READ INSTRUCTIONS BEFORE COMPLETING FORM t. REPORT NUMBER 2. GOVT ACCESSION NO. 3. RECIPIENT'S CATALOG NUMBER 4. TITLE [VK Submit) Design and Wind Tunnel Testing of a Size Sampling in- situ Net System (SSISNET) S. TYPE OF REPORT * PERlOO COVERED Master's Thesis; September 1976 • PERFORMING ORG. REPORT NUMBER 7. AUTHORS Robert Paul Mitchke «. CONTRACT OR GRANT NUMBERS.) 9. PERFORMING ORGANIZATION NAME ANO AOORESS Naval Postgraduate School Monterey, California 93 9 40 10. PROGRAM ELEMENT. PROJECT, TASK AREA 4 WORK UNIT NUMBERS 1 1. CONTROLLING OFFICE NAME AND AOORESS Naval Postgraduate School Monterey, California 93940 12. REPORT DATE September 1 976 13. NUMBER OF PAGES 94 14. MONITORING AGENCY NAME * AOORESS 1) d. Conical net with nonporous mouth-reducing cone (F = 1) e. Conical net with nonporous casing (F < 1). f. Conical net with nonporous casing and nonporous mouth- reducing cone (F = 1). (from Tranter, 1968) 21 III. METHODS A. WIND TUNNEL TESTING One method of measuring the hydrodynami c characteristics of plankton nets is to construct scale models and to test them in wind or water tunnels. The wind tunnels are partic- ularly suited for this purpose becasue of ease of experimenta- tion, flow visualization, and measurement of the forces acting on the nets. It is for this reason that it was decided to carry out a series of experiments in the low speed wind tunnel of the Mechanical Engineering Department of the Naval Post- graduate School (Plate 1). The tunnel is of open circuit design with its intake in- side the building and exhausting outside. The test section is 51 cm by 71 cm at the center and is 2.4 meters long. The prime mover is a six blade axial fan, located at the down- stream end, and driven by a variable speed 75 horsepower elec- tric motor. The wind speed is continuously variable from 548 m/min to 5486 m/min when the test section is clean, and from about 914 to 4572 m/min (equivalent to 15 and 75 m/min water speed) when the model is installed. The freestream turbulence intensity is controlled at the plenum entrance, followed by up to five interchangeable graded screens and an area contraction ratio of ten to one. The tunnel was equipped with a flow visualization system comprised of a liquid aerosol generator and injection system 22 O) c c +-> T3 0) O) Q. CO +-> 3&&s&^:- •*■ • 23 (Plate 2). The flow of the aerosol particles in front of and around the models have been used to study the flow patterns. This will be described in greater detail later. Evidently, model tests in general and the use of different fluids (e.g. air and water) for the model and prototype re- quire the establishment of model laws in order to be able to correctly interpret the results and to transfer them from one model to another. Fundamentals of fluid mechanics show that (see for example Streeter, 1958) complete similarity requires geometric, kinematic and dynamic similarity of the models. In other words, for the present investigation, this requires that the model and the prototype be geometrically similar and that the model and prototype Reynolds numbers and Mach numbers be identical. It is assumed that there are no free surface effects and the Froude number is excluded from further consideration. Reynolds similarity establishes the correct ratio of the inertial forces to viscous forces in the model and prototype at the corresponding points. Mach similarity, on the other hand, brings into the tests the possible effects of the fluid compressibility and expresses the ratio of the inertial forces to elastic forces. In the present study, the compressibilities of the fluids involved, that is of air and water, are quite negligible. Air shows compressibility effects for body speeds corresponding to Mach numbers of about 0.4 or greater. Water shows compressibility effects for speeds of sound in water or close to it. This, in fact, corre^ sponds to a sound speed of about 4000 feet/sec. Cavitation 24 n»:><*x- "'■*■■»" gr7.yyTvr.ii;;*'1 *m v~j^k~* 9. Plate 2. Liquid aerosol generator and tunnel injection system. 25 and other effects take place long before the compressibility effects come into the picture in collecting plankton (if the collector were ever to travel at such high speeds). Further discussion of the compressibility effects is meaningless and the Mach similarity need not be considered. According to Reynolds similarity, Streeter (1958) used the equation UaDa V D. w = Reynolds number (10) in which U and V are wind and water speeds relative to the collector, D the diameter, and v the kinematic viscosity of - 7 2 the fluid (v . = 9000 X 10 m /min at room temperature and air -7 2 v . = 575 X 10 m /min at 20°C temperature). The indices "a" and "w" denote "air" and "water" respectively to indicate the Reynolds numbers for the model and prototype media. Solving for the speed of air in the wind tunnel, one has: D w (11) w The characteristic dimension is taken as the inlet diameter of the collector without a nose cone, for the prototype D = r w 31.6 cm, and for the model D^ = 7.9 cm, for a model scale of a 1/4. The Reynolds numbers and the corresponding wind and water speeds for the model and prototype respectively are given in Table I. 26 TABLE I. Various wind tunnel air speeds (Ua) and the corre sponding water speeds (V) required to match the Reynolds numbers. Ua wind speed (m/min) Reynolds number (dimensionless) V water speed (m/min) 1560 • 1870 2190 2505 2815 3130 3440 3760 4070 • 4380 137400 164900 192400 219700 247300 275000 302300 330000 357300 385000 25 30 35 40 45 50 55 60 65 70 B. FLOW SPEED MEASUREMENTS The desired model combination of nets, reduction cone and casing was assembled and mounted in the test section of the wind tunnel. The air speed was adjusted to that corresponding the water speed. Photographs were taken of the flow stream lines, i.e. aerosol particles (Plates 6 through 14). A remote controlled hot-wire anemometer was used to mea- sure voltages at various points in front of the different models (Plates 3 and 4). These voltages were recorded on an X-Y plotter (Plate 5), then converted to wind speeds (U) with a the following equation, which is derived from the standard calibration procedure of a hot-wire anemometer probe: 2 2 Ua1/2 * — H" H2) 27 2 I +-> o c o to o Q. +-> o E: to c * s- a; -M O 03 S- i— Q. to c s- 03 +J CD o o > E 5- O) O i— CL >- X LO dhh^MBmE 31 I 0) I U) I ° i c a -a a; i- 32 ... ,~... en 0) I/) o c c o •p- u "O ■1) l_ -C -)-> o CO O) 4-> ^— Q_ 33 QJ c as o o u ai Q. E •r- 00 -a o E 03 en 03 34 CD ■a o m cu Q. E rO 00 CD +-> Q_ 39 where E is the voltage recorded on the X-Y plotter, E is the voltage registered by the anemometer at zero wind speed and y is the anemometer probe characteristic impedance. In the case of one probe E was found to be 5.4 volts and y to be 0.79. A second probe had an E of 3.27 and a y of 0.5. The wind speeds were then converted into corresponding water speeds (V) through the use of Table I. The voltage profile data and corresponding water speeds were tabulated for each system model in the Appendix. The water speed data were used in equation (2) to obtain the filtration efficiency and in equation (9) for mesh approach speed calculations, which in turn was used in equation (3) to obtain filtration pres- sure drop values. These results are tabulated for all models and are listed on the corresponding drawings (Figures 5 through 23). A comparison of the values were made for the purpose of choosing the model that had optimum characteristics 40 2505 M/MIN WIND SPEED, EQUIVALENT TO 40 M/MIN WATER SPEED MEAN SPEED THROUGH MOUTH (mTn) FILTRATION EFFICIENCY Ji5,4_ Ul MEAN SPEED THROUGH MOUTH ("min) 4 7.6 FILTRATION EFFICIENCY LIS. MEAN SPEED THROUGH MOUTH (mTn")__A^x5_ FILTRATION EFFICIENCY L_Q9_ Figure 5. Mouth reduction nose cone models 1, 2 and 3. 41 X !- -z. CD 2 LU _J 2 LU Q o <3- CO o E o h- c^- h- in ^ ^~ LU _J . 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TESTS The effects of filtration efficiency, filtration pressure drop, net filtration ratio and mesh approach speed were in- vestigated by varying the following sampler model parameters: casing length mouth reduction nose cone length and angle speed of tow number of nets net mesh size length of nets clogging of nets Each wind tunnel test, model description and corresponding figures and plates are listed below (data tabulated on figures are based upon prototype dimensions and water speed equiva- lences; the X-Y coordinate system is reference for the hot- wire anemometer probe positions): 1. Nose cone model 1 of 7.6 cm length and 3 1/2° angle (Figure 5 and Plate 6) 2. Nose cone model 2 of 13.5 cm length and 3 1/3° angle (Figure 5 and Plate 7) 3. Nose cone model 3 of 12.6 cm length and 6° angle (Figure 5 and Plate 8) 4. Sampler model A: 15.2 cm, 590 ym simple conical net (Figure 6 ) 60 5. Sampler model B: 48.0 cm, 590 ym simple conical net (Figure 7 and Plate 9) 6. Sampler model C: nose cone model 2 with 22.9 cm, 590 ym conical net attached (Figure 8 and Plate 10) 7. Sampler model D: nose cone model 2 with 30.5 cm, 590 ym conical net attached (Figure 9) 8. Sampler model E: nose cone model 2 with 22.9 cm, 590 ym conical net and 38.1 cm casing attached (Figure 10) 9. Sampler model F: nose cone model 2 with 30.5 cm, 590 ym conical net and 38.1 cm casing attached (Figure 11) 10. Sampler model G: nose cone model 2 with 38.1 cm, 590 ym conical net and 38.1 cm casing attached (Figure 12) 11. Sampler model H: 72.4 cm casing with a 22.9 cm, 590 ym conical net and a 38.1 cm, 103 ym conical net attached (Figure 13 and Plate 1 1 ) 12. Sampler model I: nose cone model 1 with a 22.9 cm, 590 ym conical net, a 38.1 cm, 103 ym conical net and a 72.4 cm casing attached (Figure 14) 13. Sampler model J: nose cone model 1 with a 22.9 cm, 590 ym conical net, a 38.1 cm, 103 ym conical net and a 68.9 cm casing attached (Figure 15 and Plate 12)* 14. Sampler model K: nose cone model 2 with a 22.9 cm, 590 ym conical net, a 38.1 cm, 103 ym conical net and a 68.9 cm casing attached (Figure 16 and Plate 13) 15. Sampler model L: nose cone model 3 with a 22.9 cm, 590 ym conical net, a 38.1 cm, 103 ym conical net and a 68.9 cm casing attached (Figure 17 and Plate 14) 61 16. Sampler model M: nose cone model 2 with two 22.9 cm, 590 ym conical nets and a 38.1 cm casing attached (Figure 18) 17. Sampler model N: nose cone model 1 with a 22.9 cm, 590 ym conical net, a 38.1 cm, 103 ym conical net and a 38.1 cm casing attached (Figure 19) 18. Sampler model 0: nose cone model 1 with a 22.9 cm, 590 ym conical net (one-third mesh area clogged between mouth and apex), a 38.1 cm, 103 ym conical net and a 38.1 cm casing attached (Figure 20) 19. Sampler model P: nose cone model 1 with a 22.9 cm, 590 ym conical net (one-third mesh area clogged at apex), a 38.1 cm, 103 ym conical net and a 38.1 cm casing attached ( Fi gure 21 ) 20. Sampler model Q: 38.1 cm casing with a 22.9 cm, 590 ym conical net (one-third mesh area clogged between mouth and apex), a 38.1 cm, 103 ym conical net attached (Figure 22) 21. Sampler model R: 38.1 cm casing with a 22.9 cm, 590 ym conical net (one-third mesh area clogged at apex), a 38.1 cm, 103 ym conical net attached (Figure 23) 62 Figure 24 is a plot of all different sampler prototypes (vice models) with different combinations of mesh approach speed and pressure drop; the curve demonstrates that a slight increase in approach speed corresponds to a wery drastic increase in pressure drop across the net. This large pressure variable is highly undesirable since the objective is to collect organisms that will be preserved by the sampler rather than possibly destroyed due to high pressure differen- tial across the net. The sampler prototypes at the lower end of the curve are those that were clogged (0, P, Q, R), illustrating the degra- dation in a system's performance as a result. Prototype H is a system with two nets and casing and has low speeds, pressure drop and filtration efficiency (0.37). Prototypes I, J and N are identical with the exception that the casing lengths are 2.9 m , 2.76 m and 1.52 m respectively, a factor that has no observed effect on any of the parameters; these three systems, however, utilized nose cone 1, which proves to be responsible for those systems ' low filtration efficien- cies (each were 0.52). A and B are simple conical nets of length 1.93 m and 0.60 m respectively. Prototypes E, F and G are all systems with reduction cone, casing and only one net (an undesirable feature). Prototypes K, L and M are all systems with reduction cone casing, and two nets; system K has the highest filtration efficiency (0.74) and it is located at a point just before the curve extends into the region of higher pressure drops. 63 3 4 5 6 7 8 v, Mesh approach speed (m/min) 10 Figure 24. Pressure drop (AP) vs. mesh approach speed (v) for each sampling system prototype. 64 The two remaining systems (C and D) are those of a reduction cone and net assembly, which have extremely high approach speed and pressure drops. Prototype K is clearly the optimum system. It has a relatively high filtration efficiency, low approach speed and pressure drop. Its casing houses two nets, both of which have area ratios below 0.2. The total length of the system can be varied by reducing the casing length provided the nets remain protected. 65 V. RESULTS 1. Figure 5 shows that the mouth reduction nose cone model 2 has a higher filtration efficiency than models 1 and 3. 2. Figures 6 and 7 show that an increase in the net length increases filtration ratio, and filtration efficiency but reduces the pressure drop across the net. 3. Figures 8 and 9 show that increasing net length when a nose cone is attached results in an increase in filtra- tion ratio, no change in filtration efficiency and a de- crease in pressure drop. 4. The reduction cones and net assemblies shown in Figures 10 and 11 have higher filtration efficiencies than the corresponding reduction cone, net and casing assemblies shown in Figures 11 and 12. However, the addition of the casing results in a much lower pressure drop. 5. The model shown in Figure 10 has a greater filtration efficiency than those shown in Figures 11 and 12; however clogging rapidly diminishes the filtration efficiencies of nets with lower filtration ratios. 6. The model shown in Figure 18 has a lower filtration effi- ciency than tnat shown in Figure 10 due to the additional net; however the pressure drop is reduced. 7. The net and casing assembly shown in Figure 13 has a lower filtration efficiency than the same assembly with a mouth reduction nose cone attached as shown in Figure 14. 66 10 11 Figures 15, 16 and 17 show that the net and casing assembly with the reduction cone model 2 attached has a higher filtration efficiency than with either cone model 1 or 3 attached. Figure 15 shows that an increase in tow speed increases filtration efficiency; however the increase is not a proportional one. An increase in tow speed from 23.7 m/min to 59.6 m/min resulted in an increase of filtra- tion efficiency of only .09. Figures 15 and 19 show that decreasing the model casing length from 68.9 cm to 38.1 cm has no effect on filtra- tion efficiency. A comparison of Figures 20, 21, 22 and 23 with Figure 19 shows that net clogging results in a lower filtration efficiency. Furthermore, if clogging is concentrated at the apex of the nets the result is a lower filtration efficiency than if the same percentage of clogging occurred nearer the mouth of the nets. 67 VI. DISCUSSION A plankton collection device has been designed and tested that is a combination of relatively optimum physical characteristics, including a high filtration efficiency _ 3 (0.74), a low filtration pressure drop (6.41 X 10 nt), high net filtration ratios (3.18 and 5.40) and a low maxi- mum mesh approach speed (3.63 m/min). The research was initiated by investigating these physi- cal properties associated with the basic conical plankton net and was completed with the study of complex sampling systems. A simple conical net has a filtration efficiency less than 1.0; however with the attachment of a mouth reduc- tion nose cone this figure was increased to greater than 1.0. The nose cone model that was found to result in the highest filtration efficiency was one of 13.5 cm in length with an angle of expansion of 3 1/3°. According to Pankhurst and Holder (1952) the best results are obtained by using a cone with an angle less than 3 1/2°. The length of the nose cone, nets and casing were re- stricted so the scaled-up prototype would be of suitable size. Tranter (1968) points out that the filtration effi- ciency of a net decreases rapidly beyond an area ratio (A/a) of 0.2, which converts into a net minimum side length (for the model) of 19.5 cm or 78 cm for the prototype. Increas- ing the net length beyond this value increases the filtration 68 efficiency and reduces clogging; however, physical restraints have to be imposed due to handling, stowage and weight prob- lems. In the optimum model net, side lengths of 22.9 cm and 38.1 cm were used for the 590 pm and 103 urn nets respectively. So that a size sampling i_n situ net (SSISNET) system could be realized, two nets had to be utilized in series. The mesh size of the front net would be such that all larger plankton would be collected there but the desired sized plankton would pass through and be collected by the rear net for removal and analysis. No more than two nets were tested because the system becomes cumbersome; a system that utilizes more than two nets increases resistance to flow (back pressure) and thus leads to a reduction in filtration efficiency. Aside from the fact that a casing was needed to house the two nets, the casing was found to have several desirable effects on the overall performance of the system, although it did cause a reduction in filtration efficiency. The casing protects the catch and nets and minimizes turbulence; it lends hydrodynamic stability to the system, a factor that could perhaps be further conveniently improved with the addi- tion of fins. The casing also causes a lower pressure drop across the nets. Thus, sampler model K, the encased net sys- tem shown in Figure 16 was chosen because it had the most desirable combination of characteristics, i.e. a high filtra- tion efficiency (0.74), high filtration ratios (3.18 and 5.40), and a mesh approach speed that results in a low pressure differential across the nets (6.41X 10 nt). 69 APPENDIX 70 CM CM i— CTl CM 1^ «3" CT> i — CMCM CM CM CM o c£> o (rt o o o o en -i CO CO CO cmcmcmcococococo CO CO co co CO CO CM > " V c ^ o c o en o Lnco<^>r-.0000 o o O O CO ld r>^ o > f o o o corocricvjN(?00 o o o en r> •vf t— «a- «=r *3- mroc\i<^«a-^-ir)tr) LD ID LO ■^r sr *3" CO -C J 3 IT) un + U3 CM CO loi— coco-^a-t— r->. co co r^» i — «d- CO CO ^* r-^O <* CO «3 i — LT> CT> CM UD vo CM en u-> i— <«o o >- £ II o r-» i-n *tf- CO CO CO CM i — i — o i — i— CM CO CO »w X i CD -o O CU c o u 0) in o J L CN o o 4-> O CU 4- o ^ s- o . 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O > fioiro en CO en en en en en en en co CO CO CO CO CO CO CO co a E <• i/i ^ LO LO O r> CO cnro^DUDOmo CO UD CO CO CO U3 LO r^ CO 0 > | cr> cr> 00 CM "^f LD ID LO ■^r •vT LO LO LO CM r» CO CO £ F en en en on en CM CO i a LO LO + ^ CM CT> LO CM co LO i — CO «3" i — r-» CO CO r--~ i— <3" CO f— LO CO o >- E i^cnn r»- o CM <£> UD CM CTl LO t— CO <^" o II X ^j n^^ LO LO <=a- co en cm i — i — O 1 1 i— CM CO CO 1 1 1 1 1 LO 1 c E E LO CO J L -_>*ArJ' / ! / _i_ CD -a o O) O *- O cx CO O v co <— en' ■«- 4- O S- Q. o to *- 0 > UJ 0) CM LO CO r- ■tf r- CO to CO o CO ^ CM CO r^ CO LO CO CM 1 <3" CN CO CO (wo) A 00 o CO I 91 REFERENCES 1. Aron, W., E. H. Ahlstrom, B. Bary, A.W.H. Be, and W. D. Clarke, "Towing Characteristics of Plankton Sampling Gear," Limnology and Oceanography, v. 10 (3), 333-340, 1965. 2. Neumann, G. and W. J. Pierson, Principles of Physical Oceanography , Prentice-Hall, 1966. 3. Pankhurst, R. C. and D. W. Holder, Wind Tunnel Technique, London, Pitman, 1952. 4. Pope, A. and J. J. Harper, Low Speed Wind Tunnel Testing, John Wiley and Sons, Inc., 1-4, 1966. 5. Smith, P. E. and R. I. Clutter, "Hydrodynamics of Flow and Collection in Plankton Nets", Ocean Science and Ocean Engineering, n. 1, 515 (abstract) , 1965. 6. Streeter, V. L., Fluid Mechanics , McGraw-Hill Book Co., Inc. , 8-9, 1960. 7. Tranter, D. J., "A Formula' for the Filtration Coefficient of a Plankton Net", Australian Journal of Marine and Freshwater Research, v. 18, 113-121, 1967. 8. Tranter, D. J. and A. C. Heron, "Experiments on Filtra- tion in Plankton Nets", Australian Journal of Marine and Freshwater Research, v. 18, 89-111, 1967. 9. Tranter, D. J. and P. E. Smith, "Filtration Performance", UNESCO Monograph on Ocea nographi c Methodology, no. 2, 27-56, 1968. 10. Vannucci, M., "Loss of Organisms Through the Meshes," UNESCO Monograph on Oceanographi c Methodology, no. 2, 77-86, 1968. 92 INITIAL DISTRIBUTION LIST 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11 . Defense Documentation Center Cameron Station Alexandria, Virginia 22314 Library (Code 0142) Naval Postgraduate School Monterey, California 93940 Dr. Eugene D. Traganza Department of Oceanography, Code 68 Naval Postgraduate School Monterey, California 93940 LT. Robert P. Mitchke 7106 Rook Road Houston, Texas 77017 USN Department of Oceanography, Naval Postgraduate School Monterey, California 93940 Oceanographer of the Navy Hoffman Building No. 2 200 Stovall Street Alexandria, Virginia 22332 Code 68 Office of Code 480 Arlington, Naval Research Virginia 22217 Dr. Robert E. Stevenson Scientific Liaison Office, 0 N R Scripps Institution of Oceanography La Jolla, California 92037 Library, Code 3330 Naval Oceanographic Office Washington, D. C. 20373 SI0 Library University of California, San Diego P. 0. Box 2367 La Jolla, California 92037 Department of Oceanography Library University of Washington Seattle, Washington 98105 No. Copies 2 93 12. Commanding Officer Fleet Numerical Weather Central Monterey, California 93940 13. Commanding Officer Navy Environmental Prediction Research Faci 1 i ty Monterey, California 93940 14. Department of the Navy Commander Oceanographi c System Pacific Box 1390 FPO San Francisco 96610 94 Thesis 166837 M646 Mitchke c.l Design and wind tunnel testing of a size sam- pling in-s? tu net system (SSISNET). c.3 Thesis 166837 M646 Mitchke Design and wind tunnel testing of a size sam- /c]J??-^ii^-net astern (SSISNET^ thesM646 Design and wind tunnel testing of a size 3 2768 001 89126 0 DUDLEY KNOX LIBRARY