< ae tay te The Concrete Engineer's Handbook : A CONVENIENT REFERENCE BOOK For All Persons Interested In Cement, Plain and Reinforced Concrete, Building Construction, Architecture, Concrete Blocks, Mill Building, Office Building, Fireproof Houses, Etc. = BY International Correspondence Schools SCRANTON, PA. ia) , aN ~ \ — Ist Edition, 12th Thousand, 2d Impression \ : Weoaairvoi, PA. #) Z-) INTERNATIONAL TEXTBOOK COMPANY Z 1912 — CopyRiGHt, 1911, By INTERNATIONAL TEXTBOOK COMPANY ENTERED AT STATIONERS’ HALL, LONDON Att RicHTs RESERVED PRINTED IN THE UNITED STATES 7 {i ; ~ os a Ne eS ee Ss Ko n —— _ See PREFACE The publishers have not attempted in this work to produce a condensed cyclopedia cover- ing the broad field of concrete engineering, but they have aimed to present to the public a handy reference book convenient to carry in the pocket—a pocketbook in reality—and con- taining rules, formulas, tables, and diagrams that are often used and needed by architects, concrete engineers, inspectors, superintendents, foremen, carpenters, contractors, draftsmen, designers, house owners and prospective house owners; in fact, every one engaged in any pro- fession or trade connected with building of con- crete, or in any way interested therein. The aim of the publishers has been to select from the vast amount of material on hand only that portion which is most likely to be used in connection with daily work, or which will be most frequently consulted. Although the treat- ment of some subjects is of necessity brief, it has been the aim to so distribute the space available that it would cover the more important subjects as fully as possible. It has been found impracticable to give tables for the strength of concrete beams and slabs, because the stresses employed are subject to city regulations. Until the large cities adopt uniform requirements, such tables cannot come into general use. The tables selected throughout this work are those most in demand, and the applications of the rules and iii iv PREFACE formulas are shown in many cases by practical examples and solutions, together with expla- nations. The material is conveniently arranged for ready reference. Particular attention has been given to the weights of various materials. Most tables on weights are incomplete and it is often necessary to search some time before the weight of any particular material can be ascertained. It is hoped that this volume will obviate tedious work of this kind. The section on tests of cement will be found to contain useful information that is usually found only in special treatises on the subject. INTERNATIONAL CORRESPONDENCE SCHOOLS, July, 1911. Scranton, Pa. ve i a = a ere Ti a i sil AO POO RET PRT ‘ PE EN PONT rr, rar Phe Te TPT a INDEX A Accelerated test, 213. tests for soundness, 360. Accidental load, 56. Aggregate, Definition of, 2 other than sand, 231. Selection of, 232. Size of, 231. Specifications for, 368. Aggregates, Comparative value of different, 234. Allowable live load on floors in different cities, 63. Analysis of cement, 229. Angles having equal legs, oo of standard, 54. having unequal legs, Prop- erties of standard, 158. or arcs, Measure of, 2 Apparatus for fineness tests, for specific-gravity tests, 225 Arc, Length of, 51. Arch, Reinforced-concrete, 306. ee eas of angles and, Area of circle, 50. of circular segment, 52. of ellipse, 51. of parallelogram, 51. of rectangle, 51. of ring, 52. of sector of circle, 51. of peuece of circular ring, of surface of cone, 53. of surface of cylinder, 52. of surface of frustum of cone, 53. of surface of frustum of cylinder, 53. Area of surface of frustum of rectangular pyramid, of surface of parallelo- piped, 55. of surface of prism, 55. of surface of rectangular pyramid, 54. of surface of sphere, 53. of. trapezoid, 51. of trapezium, 51. of triangle, 51. Areas and weights of square and round bars, 253 Irregular, 55. of circles, Circumferences and, 10. Argillaceous sand, 197. Australian woods, Table of weight of, 79. Avoirdupois weight, 3. Axis by means of the prin- ciple of moments, Lo- cating neutral, 97. Neutral, 97, 143. B Bar, Columbian, 262. Corrugated, 257. De Mann, 255. Diamond, 260 Hyatt, 255. iron, Plain, 254. iene 258. ahn cup, 257. Kahn trussed, 260. Longitudinal column, 250. Main reinforcement, 250. Monolith steel, 261. of special construction, Quad, 255. Ransome, 256. Rerolled, 254. Shear, 250. vi INDEX . Bar, Shrinkage, 250. Siamese, 255. Spiral, 256. Splice, 250. Square-twisted, 256. Square-twisted lug, 257. Staff, 255. Table of properties of cor- rugated, or Johnson, 258. Table of properties of Diamond, 260. Table of properties of Kahn cup, 257. Table of properties of Ransome, , Table of properties of square-twisted lug, 258. Table of properties of Thacher, 259. Table of properties of universal, 259. Tension, 250. Thacher, 255, 259. ie-, 250. Trus-Con, 261. Trussed, 250. 263 Unit, 255. Universal, 258. Weights and areas of a square and round, 253. Barrett specifications for waterproofing, 345. Batch mixers, 347. Beam and girder, Bearings for a concrete, 332. Concrete T, 298. Continuous, 99. Continuous concrete, 294. Deflection of, 174 Formula for design of a, 167. Roca for deflection of 172. Lends suddenly applied on, 176. Plain concrete, 282. Rectangular concrete, 291. Reinforced-concrete, 290. Restrained, 100. Shear on, 104. Simple, 99. Beam sockets, 328. Weight of, 170. Beams, Bending moments of, 110. Continuous, 120. Diagram for bending mo- ment on, 114. fixed at both ends, 100. Forces acting on, 99. Formulas for maximum shear and bending mo- ment of, 116 Homogeneous, 129. Loads on, 100 over equal spans, Bend- ing moments for con- tinuous, 120. over equal spans, Reac- tions for continuous, Positive and negative shear on, 105. oe age of standard I, Reactions on, 100. reinforced at top and bottom, 295. Shear diagrams of, 107. Styles of, 99. Bearing value of foundation soils, 311, 313. Bearings for concrete beams and girders, sire: -moment diagram, 4. moment for continuous beams over equal spans, -moment formulas, 167. moment of beams, For- mulas for maximum shear and, 116. moments, 110. stress in Sceee bt Table of, 284. stress of various materials, Table of, 283. Bigelow socket, 328. Bituminous concrete, 230. membranes, 345 Boiler, Instructions for start- ing and managing a, 255. Boiling test, 218. Bolts, all forms clamp, 338. Bond and shear, 300. Brace for wall forms, 341. Brayton reinforcement, 280. Brick facing, 327. ; masonry, Crushing strength of, 288. Briquet, Form for, 217. Methods of making a, 218. r Storage of, 218. 4 Table of tensile strength 3 of a cement, 221 with Building details, 322. laws, 357. material, Strength of, 124. material, Table of weight of, 59. Built-up section, 98. P C Calcareous sand, 197. Calcination, 192. Cantilever foundations, 318. Capacity, Measure of, 5. Carlin cube mixers, 347. re column, Wood and, -iron columns, 183. -iron columns, Dimensions of standard connections to, 190. ; -iron columns, Safe load E on, F Cement, 194. : Accelerated test for, 213. Accelerated tests for j soundness of, 360. ; and sand, 192. Apparatus for fineness test for, 223. ; Apparatus eat Ld 4 Say ory } specific- _ gravity tests on, 225. | Boiling test for, 213. R 3 * for briquet, Form for, 217. briquet, Methods making, 218. briquets, Storage of, 218. briquets, Table of tensile strength of, 221. of INDEX vii Cement, Chemical analysis of, 229. Constancy of volume of, 229. Fineness of, 229. for waterproofing, 344. Hard set of, 222. Improved, 195. Initial set of, 222. Inspection of, 229. mortar, Materials required per cubic yard of, 203. Measurement of expan- sion of, 211. Method of making fine- ness test on, 224. Method of making specific- gravity test on, 226. Mixed, 195. Molds for, 218. mortar, 201. mortar, Table of tensile strength of, 204. -mortar tests, Sand for,217. mortars, Lime and, 199 Natural, 194. Normal consistency of, 216. Normal test of, 211. Packages for, 228. Portland, 194. Properties of, 195, Protection of, 229. Puzzolan, 194. Results of tests for sound- ness of, 215. Results of time of setting tests on, 223. Sand, 195. Secondary tests for, 221. Set of, 229. Slag, 195. specifications, 227, 367. Steam test for, 214. Table of requirements of high-grade, 228 -testing machine, 219. Tests for fineness of, 223. Tests for specific gravity of, 225. Tests for tensile strength of, 215 viii INDEX Cement, Tests of natural and slag, Tests on, 208. setae -of- setting test for, Weight of hydraulic, 196. Cementing material, 192. Center of gravity, 95. of grauy of plane figures, 9 Centering for concrete, 333. Pigaer rp loaded columns, 2 Channels, Properties of standard, 151. Chatelier flask, Le, 225. Chemical analysis of cement, 29. Cinder concrete, 230. Circle, Area of, 10, 50. Circumference of, 10, 50. Chord of, 52. Diameter of, 50. Radius of, 50. Sector of, 51. Segment of, 52. Circular ring, ‘Surface of, 53. ring, Volume of, Circumference of circle, 50. and areas of circles, 10. Cities, Unit working values of concrete allowed by various, 240. a bolts, Wall forms for, Clamping device for forms, Clay, Waterproofing by add- ing lime or, 343 Clinton wire cloth, 268. Coarse sand, 198 ockburn mixer, 352. Cold yoga Concreting in, weather, Laying mortar in, Collapsible forms, 336. Coloring of mortar, 208. Columbian bar, 262. Column, Cast-iron, 187. Centrally loaded, 285. Concrete, 285. Column, Dimensions of standard connections to cast-iron, 190. - Eccentrically loaded, 288. Eccentrically loaded con- crete, 306. footings, Placing rein- forcement in, 314. formulas, 187. reinforcement, Empirical rules for straight, 304. reinforcement, Hooped, reinforcement, Straight, rods, Longitudinal, 250. Safe load on a cast-iron, 8. Spread footings for out- side, Table of constants for a rectangular wooden, ties, 250. Wood and cast-iron, 179. Common limes, 193 stp erin , Granulometric, of forces, 88. Compressive strength of brick masonry, 288. eins of concrete, 233, strength of stone and stone masonry, 287. stress, 122. ‘Concentrated load, 100. Concrete allowed by various cities, Unit working values of, 240. arches, Reinforced-, 306. beam, ‘Continuous, 294. beam, Rectangular, 291. beams and girders, Bear- ing for, 332. beams, Plain, 282. beams reinforced at top and bottom, 295. Bituminous, 230. by weight, Proportioning, 235. Cinder, 230. INDEX ix Concrete columns, 285, 302. columns, Eccentrically loaded, 306. Comparative value of dif- » ferent aggregates used in, 234. Compressive strength of, 233. Cost of, 357, 364. Crushing strength of, 286. po 285 Dry, 236. Effect of fire on, 237. Effect of thermal changes in, 238. Effect of vibration on,238. Fastenings in, 327. for waterproofing, Mixing of, 342. Fuller’s rule for quantities for, 242 Lime, 230. Materials used for, 230. measurer and feeder, Gil- braith, 353. Medium, 285. Methods of measuring in- gredients for, 242. mixer, Cockburn, 352. mixer, Continuous, 351. » mixer, Cube, 347 mixer, Drake, 351. mixer, Quantitative, 353. mixer, Ransome, 348. mixer, Smith, 349. mixer, Starting and opera- ting, 356 mixers, 347. mixers, Operation of, 354. Mixing and working of, 242. Mixing of, 246. Moduli of rupture of, 284. Plain, 230. Properties of, 237. Quantities for, 244. Specifications for, 357, 367. Stone, 230. T beams, 298. oe or gderarags strength of, ° Transverse strength of, 284. Concrete, Usual proportions of material for, 235 Water for, 236. Waterproofing of, 342. Wet, 2 with new, Joining of old, 247 Working stresses of, 238. Concreting at high temper- atures, 246. in freezing weather, 247. Cone, Frustum of, 53. Surface of, 53. Volume of, 53. Connection to cast-iron col- umns, Dimensions of standard, 190. Consistency, Normal, 216. Constancy. of volume, 210. of volume of cement, 229. Construction and finish of form work, 333. Cornice, 343. Continuous beam, 99, 120. beams over equal spans, ae moments for, beams over equal spans, Reactions for, 119. concrete beam, 294. inserts, 330. mixer, 351. Conversion of inches to fest, Table of, 14 tables, 6. Chord, Length of, 52. Cornice construction, 343. Cornices and eaves, 325. Corrugated bar, 257. ohnson, bar, Table of properties of, Cost data, 364. of concrete, 357 Crushing strength. of brick masonry, 288. strength of concrete, 286. strength of stone and stone masonry, 287. Cube mixers, 347. mixers, Carlin, 347. root, 27. Cubes and squares, 28. x INDEX Cubic measure, 2. Cu » 4 ings reinforcement, Cup bar, Kahn, 257. bar, Table of properties of Kahn, 257. y Curing, Definition of, 236. Cylinder, Frustum of, 53. Surface of, 52. A Volume of, 52. Damp concrete, 285. Dead load, 56. Decimal equivalents, 14. Decimals of a foot for each fraction of an inch, 14. Deflection of beams, 174. of Sen Formulas for, De Mann bar, 255. tit = of beams, Formulas or, : of concrete structural members, 282. of footings, Formulas for, Details, Building, 322. ape borg Bending moment, Shear, 107. Diameter of circle, 50. Diamond bar, 260. bar, Table of properties of, Dimension of standard con- nections to cast-iron columns, 190. of standard T rails, Prop- erties and principal, 166. Disposition of loads, 8 Distributed load, 100. Double reinforced - concrete beam, 295. Drake mixer, 351. Dry concrete, 236. measure, 3. Dryer, Sand, 199. E Eaves and cornices, 325. seasrat waged loaded column, Eccentrically loaded concrete columns, 306 Elastic properties, 123. Electrically welded fabric, 268. j Elements of usual sections, Ellipse, Area of, 51. Perimeter of, 51. Elongation, 122. Ultimate, 124. *Eminently hydraulic lime, 194. Empirical rules for straight reinforcement, 304. Equivalents, Decimal, i} of Fee to feet, Table of, Rate sen: and involution, Expanded metal, 263. metal, Herring-bone, 266. metal, Kahn, 265. metal, Table of properties of, 264. metal, ce of properties of Kah sea pe ‘Meaiipeivialt of, F Binion Electrically welded, Lock-woven wire, 267. Tie-locked wire, 267. Fabricated system of rein- forcement, 277. Facing, Brick, 327. Factor of safety, 124. Failure, rere tie to re- sist lines of, 2 Farm products, Table of weight of, 71. Fastenings in concrete, 327. Fat lime, 193. Feebly hydraulic lime, 194. Ferroinclave, 267 Field inspection, 208. operations, 347 Fine sand, 198. Fineness of cement, 229. test, Apparatus for, 223 “Ss ll Mi tli ee Ne a INDEX xi Fineness, Test for, 223. ee, ee of making, Finish of form work, Con- struction and, 333. : Fire on concrete, Effect of, Fixed at both ends, Beam, 100. Flask, Le Chatelier, 225. Floor and test load, 368 systems, Forms for, 334. Floors in different cities, Table of allowable live loads on, 63. Foot for each fraction of an inch, Table of decimals of a, 14. ! a Formula for design of a, : for outside columns, Spread, 315. Placing teinforcement in a column, 314. Spread, 314. Force of wind, Table of velocity and, 82. Representation of a, 87. Forces, 87. acting on beams, 99. Composition of, 88. Moment of, 93. Parallelogram of, 88. Resolution of, 91. Resultant of several, 89. Triangle of, 89. Form, Braces for wall, 314. Clamping devices ‘for a, 340. Collapsible, 336. constructed of planks, for floor systems, 334. Partly collapsible, 337. Plank holders 8 a, 340. Spandrel wall, 341 bi clamp bolts, Wail, 38. with wire ties, Wall, 338. work, work construction and . finish, 333. Formula, Bending moment, 167. for cast-iron columns, 187. for deflection of beams, for design of beams, 167. for long posts, 181 Formulas, 16. for maximum shears and bending moments of beams, 116. Foundation, Cantilever, 318. soils, Bearing value of, 311,313. Foundations, 311. Frames, Pin-connected gir- der, 278. Freezing weather, Concret- ing in, 247. weather, Laying mortar in, 206 Frustum of cone, 53. of cylinder, 53. of prism, Volume of, 55. of rectangular pyramid, Surface of, 54 of rectangular pyramid, Volume of, 54. bias rule for quantities, G Gabriel system of reinforce- ment, Gilbraith measurer and feeder, 353. Girder frames, Pin-con- nected, 278. Girders, Bearings for con- crete beams and, 332. sae? aia composition, Gravity, Center of, 95. Grouting, 207. Gyration, Radius of, 142. H Hancock insert, 328. Hard set, 222. Heat changes in concrete, Effect of, 238. xii INDEX Helix, oan of, 52. Herring- bone expanded metal, 266. High-carbon steel, 252. temperatures, Concreting at, 246. Homogeneous beams, 129. Hooke’s law, 123. Hooped column reinforce- ment, 302, 305. Hot Ne sa Concreting in, Hyatt bar, 255. Hydrated lime, 193. Hydraulic cement, Weight of; 196 lime, 193. vE I beams, Properties of, 148. Imperviousness, Effect of strength and, 234. Improved cement, 195. Inch, Table of decimals of a aot for fraction of an, Inertia, Moment of, 129. Ingredients for concrete, Methods of measuring, 242. Proportioning of, 234. Initial set, 222. Insert, Continuous, 330. Hancock, 328. Inspection, Field, 208. of cement, 229. Integral method of water- proofing, 342. Involution and evolution: lron column, Wood and cast-, 179. columns, Cast-, 187. column, Dimensions of standard connections to cast-, 190. column, Safe load on cast-, Plain bar, 254. Irregular areas, 55. Jennings-Steinmetz socket, 328. Johnson bar, 258. _ bar, Table of properties of, 258. Joining old and new work, 247. K Kahn cup bar, Table of properties of, 257. expanded metal, Table of properties of, 265 Stes of reinforcement, Ths trussed bar, 260. L Lath, Herring-bone metal, Law, Hooke’s, 123. for steel, 361. for walls, 361. Laws, Building, 357. Laying mortar in freezing weather, 206. Le Chatelier flask, 225. Legs, Properties of standard ener having equal, Properties of standard angles having unequal, 158. Length of arc, 51. of chord, 52. of helix, 52. of spiral, 54. Lengths, Measure of, 5. Lime and cement mortars, 199. Common, 193. concrete, 230. Fat, 193. Hydrated, 193. Hydraulic, 193. Meager, 193. mortar, 200. or clay, Waterproofing by adding, 343. Poor, 193. Pe ae ee hlmvehlCh eh Stt:™~S~; SL INDEX xiii Lime, Rich, 193. Slaked, 193. Linear measure, 1. Lintel and spandrel construc- tion, 322. Liquid measure, 3. Live load, 56, 61. loads on floors in different cities, Table of, 63. Load, Accidental, 56. Concentrated, 100. Dead, 56. Distributed, 100. Floor and test, 368. from floor to floor, Re- duction of live, 86. Live, 56, 61. on cast-iron columns, Safe, 188. on floors in different cities, Table of allowable live, 63. Snow, 56. Suddenly applied, 176. Table of wind, Uniform, 100. Wind, 56. Wind and snow, 81. Loading testing machine, Rate of, 220. Loads, Disposition of, 85. in structures, 56. on beam, 100. Locating neutral axis by means of the principle of moments, 97. sugges wire fabric, Long posts, 181. -ton weight, 3. ce are column rods, Loop truss, Cummings, 278 Loose-rod system of rein- forcement, 269. Low temperature, mortar at, 206. Lug De r, Square-twisted, Laying bar, Table of properties of twisted, 258. M Machine, Rate of loading testing, 220. Testing, 219. Main reinforcing rods, 250. Masonry, Crushing strengch of brick, 288 Crushing strength of stone, 287. Material, Cementing, 192. required per cubic yard of mortar, 203. Strength of building, 124. Table of weight of build- ing, 59. Table of weights of mis- cellaneous, 68. used for concrete, 230. i 2 fas proportions of, Mathematical tables, 10. Mathematics, 16. Matrix, Definition of, 230. Maximum shears and bend- ing moments of beams, Formulas for, 116. McCarty separator, 340. Meager lime, 193. Measure, Cubic, 2. Liquid, 3. of angles or arcs, 2. of capacity, 5. of length, 5. of surface, 5. of volume, 5. of weight, 6. Square, 2. Surveyor’s, 1. Surveyor’s square, 2. Measurement of expansion, of moments, 93. Measurer and feeder, Gil- braith, 353. Measures, Weights and, 1. Measuring ingredients, Method of, 242. Mechanics, 87. Medium concrete, 285. xiv «INDEX Medium steel, 252. Membrane method of water- proofing, 345. Mensuration, 49. Merchandise in bulk, Table of weight of, 64. Merrick system of reinforce- ment, 274. Metal, Expanded, 263. Herring-bone expanded, Kahn expanded: 265. reinforcement, Sheet-, 267. Table of properties of expanded, 264. Table of properties of Kahn expanded, 265. Metallic reinforcement, Characteristics of, 252. Metals, Table of ultimate strength of, 126. Tables of weights of vari- ous, 67 Metric capacity, 5. conversion tables, 6. lengths, 5. surface, 5. system, 4. volume, 5. weight, 6. Mild, or soft, steel, 252. Miscellaneous materials, Table of weights of, 68. reinforcement, 280. Mixed cement, 195. Mixer, Carlin cube, 347. Cube, 347. Cockburn, 352. Concrete, 347. Continuous, 351. Drake, so aay of concrete, Quantitative, 353. Ransome, 34 Smith, 349. : ae and operating a, Mixing and working of con- crete, 242. concrete for waterproof- ing, 342 Mixing of concrete, 246. Mixtures, Sand and its, 197. Moduli of rupture of con- crete, Table of, 284. aoe of rupture, 124, Section, 145. Molds for mortar, 218. Moment, Diagram for bend- ing, 114 for continuous beams over equal spans, Bending, 120. formulas, Bending, 167. Measurements of, 93. of beams, Formulas for maximum shear and bending, 116. of forces, 93. of inertia, 129. Resultant, 95. Moments, Bending, 110. Locating neutral axis by means of the principle of, 97. Negative and positive, 94. Monolith steel bar, 262. Mortar briquets, Method of making, briquets, Storage of, 218. Cement, 201. Coloring of, 208. Consistency of, 216. in freezing weather, Lay- ing, 206. Lime, 200. Lime and cement, 199. Materials required per cubic yard of, 2! Molds for, 218. Retempering of, 206. Shrinking in, 207. Table of tensile strength of cement, 204. test, Sand for, 217. Mushroom system of rein- forcement, 275. N Natural and slag cement, Tests of, 227. .---. ”_ Oe eee ——— os ee S.”,:CmCrC( .mhlhl eo INDEX xv Natural cement, 194. Needle, Vicat, 222. Negative and positive mo- ments, 94. shear, Positive and, 105. Neutral axis, 97, 143 axis by means of the prin- ciple of moments, Lo- cating, 97. New, Joining of old concrete with, : Normal consistency, 216. tests, 211. strc pressure, Table of, oO Old and new work, Joining, 247. Operation of mixers, 354. Ordinarily hydraulic lime, Outside columns, Spread footings for, 315. Pr Package for cement, 228. Paraffin for waterproofing, Parallelogram, Area of, 51. of forces, 88. Duke vie ta Surface of, Volume of, 55. Percentage of voids, 197. _ Perimeter of ellipse, 51. Philippine wood, Table of weights of, 79. Joie girder frames, Pit sand, 197. Plain bar iron, 254. concrete, 230. Plane figures, Center of vity of, 96. pe om constructed of, holders for forms, 340. Polygons, Regular, BD. Poor lime, 193. Portland cement, 194. perment, Specifications for, Positive and negative mo- ments, and negative shear, 105. Post, Long, 1 hort, Table of constants for a rectangular wooden, 184. Wooden, 179. Powers, roots, and recipro- cals, 31. Preparation of sand, 199. Pressure, Table of normal wind, 83. Primary tests, 210. Principal dimensions of standard T rails, 166. Prism, Surface of, 55. Volume of, 55. Volume of frustum of, 55. Prismoid, Volume of, 53. Properties and principal dimensions of standard T rails, 166. of rolled ‘steel shapes, 146. of sections, 129. of standard angles having equal legs, 154 of standard angles having unequal legs, 158. of standard channels, 151. of standard I beams, 148. of T bars, 164. of Z bars, 162. Property, "Plastic, 123. of cement, 195. of concrete, 237. of sand, 197. Proportion of materials, Usual, 235. at ca by weight, of ingredients, 234. Proportions of ingredients for concrete, 244. Protection of cement, 229. Purpose and classification of cement tests, 210. Puzzolan cement, 194. Pyramid, Surface of frus- tum of rectangular, 54. Surface of rectangular, 54. Xvi INDEX Pyramid, Volume of frus- tum of rectangular, 54. Volume of rectangular, 54. Q uad bar, 255. uantitative mixer, 353. uantities for concrete, Table of, 244. Fuller’s rule for, 242. R Radius of circle, 50. of gyration, 142. il, Properties and prin- cipal dimensions of standard, 166. Ransome bar, 256. bas. — of properties of, mixer, 348. Rate of loading testing machine, 220. Reactions for. continuous beams over equal spans, 119. on beams, 100. Reciprocals, 30. Powers, roots, and, 31. Rectangle, Area of, 51. weceaesar concrete beam, pyramid, Surface of, 54. pyramid, Surface of frus- tum of, 54. pyramid, Volume of, 54. pyramid, Volume of frus- tum of, 54 wooden posts, Table of eonstants for, 184. Reduction of live loads from floor to floor, 86. Regular polygons, 55. Reinforced at top and bot- o> Concrete beam, -concrete arches, 306. -concrete beam, 290. -concrete column, 302. sags iE Brayton, Reinforcement, Characteris- tics of metallic, 252. Cummings, 278. defined, Parts of steel, 250. Elements of steel, 248. Empirical rules for straight column, 304. si system of, Gabriel system of, 274. Hooped column, 302, 305. in column footings, Pla- cing, 314. Kahn system of, 271. Loose-rod system of, 269. Merrick system of, 274. Mushroom system of, 275. of PO ere construction, gpa oat girder, 278. Plain bar, 254. Shear frame, 279. Sheet-metal, 267. Square- and _ triangular- mesh wire, 268. Straight column, 302. Structural shapes used for steel, 263. to resist lines of failure, 251 Trussit, 267. Types of steel, 254. Unit system of, 277. Visintini, 281. Reinforcing rods, Main, 250. sted. Specifications for, Representation of a force, 87. Rerolled bars, 254 Resolution of forces, 91. Restrained beams, 100. Resultant moment, 95. of several forces, 89. Retempering of mortar, 206. Rich lime, 193. Ring, Area of, 52. River sand, 197. Rod, 1» vongitudinal column, Main reinforcement, 250. of eigen construction, INDEX Rod, Plain iron, 254. Shear, 250. Shrinkage, 250. Slab, 250. Splice, 250. Tension, 250. Tie-, 250. Trussed, 250. Weights and areas of a square and round, 253. Rolled sections, Values for standard, 136. shapes, Pro; mes Paar 146. Roof y dara f, 56: Root, Cube, 2 Square, i Roots, and reciprocals, Pow- ers, 31. Round bars, Weights and areas of square and, 253. Rule, ior quantities, Fuller’s Rules yar operating mixers, Rupture, Modulus of, 124, 179. of concrete, Table of moduli o Ss Safe load on cast-iron col- h of ‘concrete, 328. Safety factor, 124. Sampling, 209. Sand and cement, 192. and its mixtures, 197. Argillaceous, 197. Calcareous, 197. cement, 195. Coarse, 198. dryer, 199. Fine, 198. for mortar test, 217. Granulometric composi- tion of, 198. sas op Consistency of, Percentage of voids in, 197. XVii Sand, Pit, 197. , Preparation of, 199. Properties of, 197. River, 197. Silicious, 197. a, 197. Secondary tests, 210, 221. Section, Built-up, 98. modulus, 145. Rootes. Elements of usual Properties of, 129. Values for rolled, 136. Sector of circle, 51. Segment of circle, 52. Selection of aggregates, 232. Separator, McCarty, 340. Set, Hard, 222. Initial, 222. of cement, 229. hier test, Results of time- oO - Shapes, Properties of rolled ste Shear and bending moment of beams, Formulas for maximum, 116. and bond, 300. bar, 250. diagram, 107. frame reinforcement, 279. Negative and _ positive, 105. Vertical, 104. Shearing stress, 122. a? pace reinforcement, -steel socket, 330. Short posts, 180. Shot machine, 219. Shrinkage bar, 250. in mortars, 207. Siamese bar, ig Side of triangle, Silicious me, HE “gr Simple beam, 9 Size of nota yodl 231, Slab rods, 250. Slag cement, 195. cement, Tests of natural and, 227. Slaked lime, 193. XVil Smith mixer, 349. Snow and wind load, 81. load, 56. Socket, Beam, 328. Bigelow, 328. Jennings-Steinmetz, 328. Sheet-steel, 330. Unit, 328. Soft, or mild, steel, 252. Soil, Bearing value of a foundation, 311, 313. Soundness, Accelerated tests or, 360. Results of tests for, 215. Tests for, 210. Span, Definition of, 99. Spandrel and lintel construc- tion, 322. wall forms, 341. Spans, Bending moment for continuous beams over equal, 120. Reactions for continuous beams over equal, 119. cian apa herksten Bars of, Specific-gravity tests, Appa- tatus for, 225. gravity, Tests for, 225. -gravity tests, Method of making, 226 Sees for aggregates, for cement, 227, 367. for concrete, 367. for floor and test load, 368. for reinforcing steel, 368. for Sige 7 omen ait Bar- rett, 345. Sphere, Surface of, 53. Volume of, Spiral bar, 256. Length of, 54.° Splice rod, 250. Spread footing for outside columns, 315 footings, 314. Square and -round bars, My ay and areas of, measure, 2. INDEX Square measure, Surveyor’s, -mesh wire reinforcement, 268 : root, 26. -twisted bars, 256. -twisted lug bar, 257. wooden posts, Table of constants for, 184. Squares and cubes, 28. Staff bar, 255 Standard angles having equal legs, Properties of, 154. angles legs, Pro c hannels, having unequal Slee of, 158. roperties of, pesaieal to cast-iron columns, Dimensions of, 190. : I he egg Properties of, rolled sections, Values for, rolled steel shapes, Prop- erties of, 146. T rails, Properties and peoctpat dimensions of, 16 Starting and managing boil- ers, Instructions for, and operating a mixer, 356 Steam test, 214. Stearate, Waterproofing with meta ic; 3 Steel angles, having equal legs, Properties of, 154. angles having unequal legs, Properties of, 158. bar, Monolith, 262. ware es Properties of, High carbon, 252. I beams, Properties of, 148. Laws for, Medium, "252. Plain bar, 254. reinforcement, Character- istics of, 252. oe i , INDEX xix Steel reinforcement defined, of, ; reinforcement, Elements of, 248. F teinforcement of special construction, 255. reinforcement, Structural shapes used for, 263. oe uaa Types of, ' shapes, Properties of rolled, 1 socket, Sheet-, 330. Soft, or mild, "252. : Specifications for fein- forcing, 368. T bars, Properties of, 164. T rails, Properties and pepcipat dimensions of, z bars, Properties of, 162. Stirrup, 250 Stone and stone masonry, Crushing strength of, 287 concrete, 230. Storage of briquets, 218. Straight column reinforce- ment, 302 Strain, Unit, 122. Strain and stresses, 121. Strength and impervious- ness, Effect of, 234. of brick masonry, 288. of building material, 124. of cement _ briquets, Table of tensile, 221. of concrete, Compressive, of concrete, Crushing, of concrete, Safe, 238. of concrete, Table of transverse, 284. of concrete, Table of ultimate, 241. of metals, Table of ulti- mate, ‘ of stone and stone ma- sonry, Crushing, 278. Sltrength of various ma- terials, Table of trans- verse, 283. of wood, Ultimate, 128. Tensile, 122. Tests for tensile, 215. i, Result of tensile-, Ultimate, 124. Stress, Compressive, 122. Shearing, 122. Unit, 122. Stresses and strains, 121. of concrete, Working, 238. SAE CoureRs, Terra-cotta, Structural members, Design of concrete, 282 shapes used for steel rein- forcement, 263. —- aneyee, Properties of, Structures, Loads in, 56. Suddenly applied load, 176. ullivan pressed steel plank holder, 340. Superficial ‘method of water- proofing, 344 Surface, Measure of, 5. of circular ring, 53. of cone, 53. of cylinder, 52. of frustum of cone, 53. of frustum of cylinder, 53. of frustum of rectangular pyramid, 54. of amir sae Area of, of prism, 55. of rectangular pyramid, of sphere, 53. Surveyor’s measure, 1. square measure, 2. Sylvester process of water- proofing, 343. System, Metric, 4. 4 T bars, Properties of, 164. beams, Concrete, 298. xx fasteners, 327. -headed bolt for continu- ous insert, 330 rail, Properties and prin- cipal dimensions of standard, 166. Table of allowable live loads on floors in different ‘cities, 63. of areas and weights of square and round bars, 253. of avoirdupois weight, 3. of bearing value of differ- ent foundation soils, of bending moments for continuous beams over equal spans, 120. of circles, 10. of comparative value of different aggregates used for concrete, 234. of compressive strength of concrete made of dif- ferent-sized stone, 233. of constants for rectangu- lar wooden posts, 184. of crushing strength of concrete, 286. of crushing strength of brick masonry, 288. of crushing strength of stone and stone ma- sonry, 287. of cubic measure, 2. of decimal equivalents, 14. of decimals of a foot for “0 fraction of an inch, 4, of dimensions of standard connections to cast-iron columns, 190. of dry measure, 3. of elements of usual sec- tions, 130. of formulas for deflection of beams, 172. of formulas for maximum shears and bending mo- ments of beams, 116. INDEX _T-headed bolt for concrete | Table of linear measure, 1. of liquid measure, 3. of live loads, 62. of long-ton weight, 3. of materials required per cubic yard of mortar, of measure of angles or arcs, of measure of capacity, 5. of measure of lengths, 5 of measure of surface, 5. of measure of volume, 5 of. measure of weight, 6. of moduli of rupture of concrete, 284. of moduli of rupture of various materials, 283. of powers, roots, and reciprocals, 31. of properties of standard channels, of properties of corru- eae or Johnson, bar, of properties of diamond bar, i of properties of expanded metal, 264 of properties of Kahn cup bar, of properties of Kahn expanded metal, 265. of properties of Ransome bars, of properties of square- twisted lug bar, 258. of properties of standard angles having equal legs, 154. of properties of standard angles having unequal legs, 158. of properties of standard T rails, of properties of T bars, 164. of properties of Thacher bar, 259. of properties of universal bar, of properties of Z bars, 162. INDEX xxi | Table of quantities for con- crete, 244 of reactions for continuous beams over equal spans, 19. of reduction of live loads from floor to floor, 86. of requirements of high- grade cement, 228. of safe loads on cast-iron columns, 188. of square measure, 2. of standard I beams, 148. of surveyor’s measure, 1. of surveyor’s square meas- ure, 2. of tensile strength of ce- ment briquets, 221, of tensile strength of ce- ment mortar, 204. of troy weight, 3. of ultimate strength of concrete, 241. of aoe strength of metals, of unit a a values of concrete allowed by various cities, 240. of velocity and force of wind, 82. of ultimate strength of wood, F of values for standard rolled sections, 136. of weight of Australian wood, 79. of weight of building material, 59. of weight of hydraulic cement, 196. of ‘weight of merchandise in bulk, 64. of weight of Philippine wo of weight of roof trusses, of weights of farm prod- ucts, 71. of weights of various metals, 67. of weights of oo ous materi Table of weights of wood, 74. Tables, Conversion, 6. Mathematical, 10. Temperature changes in con- crete, Effect of, 238. Laying: mortar at tlow, 206. Tensile strength, strength of Coane bri- quets, Table of, 221. strength of cement mortar, Table of, 204. sah test, Results of, strength, ae for, 215. Tension bar, 250 Terra-cotta string - courses, 327. Test, Accelerated, 213, 360. Apparatus for fineness, Apparatus for specific- gravity, 225. Boiling, 213. for fineness, 223. for soundness, 210. se ena, Results of, for specific gravity, 225. for tensile strength, 215. loads, Floor and, 368. Method of making specific- gravity, 226. Method of making the fineness, 224. Normal, 211. of natural and slag ce- ment, 227 on cement, 208. Primary, 210. Per ae. and classification Result of tensile- strength, Results of time-of-setting, 223. Sand for mortar, 217. Secondary, 210, 221. Steam, 214. Time-of-setting, 221. Testing machine, 219. Seay one Rate of loading, “Xxii INDEX Thacher bar, 255, 259. ig aia of properties of, Thermal changes in concrete, Effect of, 238 Tie-bar, 250. Column, 250. 2 a wire fabric, 267. 1 forms with wire, . 38. Time-of-setting test, 221. MsetOing test, Results of, 3: Ton weight, Table of long-, 3. Transverse strength of con- crete, Table of, 284. strength of various ma- terials, Table of, 283. Trapezium, Area of, 51. Trapezoid, Area of, 51. Triangle, Area of, 51. Dimensions of, 50. of forces, 89. Triangular-mesh wire rein- forcement, 268 Troy weight, 3. Trussed bar, Kahn, 260. bars, 250. Trus-Con bar, 261. Trusses, Weight of roof, 56. Trussit reinforcement, 267. Twisted bars, Square-, 256. lug bar, Square-, 257. lug bar, Table of proper- ties of square-, 258. U bar, 263. Ultimate elongation, 124. strength, 124. strength of concrete, 241. se i ha metals, Table fe) strength of wood, Table 128. Uniform load, 100. Unit bar, 255. socket, 328. strain, 122. stress, 122. system of reinforcement, 277. Unit working values of con™ crete allowed by vari- ous cities, 240. Universal bar, 258. jg ener of properties of, Vv Velocity and force of wind, Table of, Vertical shear, 104. Vibration on concrete, Effect of, 238. Vicat needle, 222. Visintini reinforcement, 281. Voids, Definition of, 230 Percentage of, 197. Volume, Constancy of, 210. Measure of, 5. of cement, Constancy of, 229. of circular ring, 53. of cone, 53 of cylinder, 52. of frustum of cone, 53. of frustum of cylinder, 53. of frustum of prism, 55. of frustum of rectangular pyramid, 54. of parallelopiped, 55. of prism, 55. of prismoid, 53. é of z TOCHRRUIAT pyramid, of sphere, 53. of wedge, 53. Ww Wall forms, Braces for, 341. forms, Spandrel, 341. forms with clamp bolts, forms with wire ties, 338. Walls, Laws for, 361 Water for concrete, 236. Waterproofing, Barrett spe- cifications for, 345. by adding lime or clay, Cements for, 344. INDEX Waterproofing, method o Membrane ‘‘iathed of, 345. Mixing concrete for, 342. of concrete, 342. Paraffin for, 344. Superficial method of, 344. Sylvester process of, 343. Waxes for, 344. with metallic stearates, Integral 44, Waxes for waterproofing, 344 Weather, Laying mortar in freezing, 206. Wedge, Volume of, 53. Weight, Avoirdupois, 3: Measure of, 6. of Australian wood, Table of, 79. of beams, 170. of building material, Table of, 59. of farm products, Table of, of fires cement, 196. of merchandise in bulk, « Table of, 64. of miscellaneous materials, Table of, 68. of Philippine woods, Table of, 79. of roof trusses, 56. of various metals, Table of, 67. of wood, Table of, 74. Proportioning by, 235. Table of long-ton, 3. XXiii Weight, Troy, 3. Weights and areas of square and round bars, and measures, l. Mise! fabric, Electrically, Wet concrete, 285. Wind and snow load, 81. load, 56. pressure, Table of normal, Table of velocity and force of, 82. Wire cloth, Clinton, 268. fabric, Lock-woven, 267. fabric, Tie-locked, 267. reinforcement, Square- and triangular-mesh, 268. nas forms with, Nivee and cast-iron column, Table ‘of weight of Austra- lian, 79. Table ‘of weight of Philip- pine, 79. Table of weights of, 74. Ultimate strength of, 128. Wooden posts, 179. posts, Table of constants for rectangular, 184. Working of concrete, Mixing and, 242. stresses of concrete, 238. Z T bars, Properties of, 162. The Concrete Engineer’s Handbook USEFUL TABLES WEIGHTS AND MEASURES LINEAR MEASURE BS inches (Gin?)s os ots ho PD IO0b i os cok oc ae he caewteee SB OCCr oie cnc Oo ee 1 VAIO as had oe werk nee Wsth PARAS Se ose ato crecce aiscee ord POO ac avesicid os, slerataelareretor tele MO" F008 oS ke si sons vote mL POTIONG::. 5 2 eure dte oe ees S~ furlongs: 3.7. cs ss cee ee miles Fk ee hats ee in. it. yd. rd. fur. mi. 36= 3= 1 198= 165= 55= 1 7,920= 660= 220= 40=1 63,360 = 5,280 = 1,760 =320=8= 1 SURVEYOR’S MEASURE (le Gs SO 1k SC: Seen eee gee ES OS eg Se PEN Bf . :: SUNS See ERE. A 4 rods 100 links Ie Aaa eiehs is Moree, Se CAGED dacs, heri ehe a aie nie ch. 66 feet OO CHAM koe gael we oe MIG, Bor ve oe eclea curee ik 1 mi. =80 ch. =320 rd. =8,000 li. = 63,360 in. 2 ; USEFUL TABLES SQUARE MEASURE 144 square inches (sq. in.). =1 square foot..........sq. ft. 9 square feet...........=1 square yard......... sq. yd. 304 square yards......... .=1 square rod.......... sq. rd. .160 square rods.......... eet BOTS is “sh cscaiwre 4, Re cued ERE 640 acres... 25..0.....=1 square mile; 2.6... sq. mi. sq.mi.A sq. rd. sq. yd. sq. ft. sq. in. 1=640 = 102,400 = 3,097,600 = 27,878,400 = 4,014,489,600 SURVEYOR’S SQUARE MEASURE 625 square links (sq. li.)....=1 square rod.......... sq. rd. LG equiare TOGSR. osm os =1 square chain........sq. ch. Meee he ata: ee <= lacre. . i eidia bis soe 640 acres. Nae =] sue. aie Vict sq. mi. 36 square ‘niles 6 | mi. , SUAS) 6 ice 1 tOWNERID: £25 cess. a eed Tp. 1 sq. mi. =640 A.=6,400 sq. ch. =102,400 sq. rd. = 64,000,000 sq. li. The acre contains 4,840 sq. yd., or 43,560 sq. ft., and is equal to the area of a square measuring 208.71 ft. on a side. CUBIC MEASURE . 1,728 cubic inches (cu. in.) =1 cubic foot...........cu. ft. 27° cubic feet.......5.:. =1 cubic yard..... 2%. cu. yd. Pao voubic feet... 6... 5's Sons we NCOP sos ae eae seit sik so OCS 24? cubic feet........... asl PORCt en pace es eared se es 1 cu. yd.=27 cu. ft. = 46,656 cu. in. MEASURE OF ANGLES OR ARCS GO Seconds (") 2. etal oid PE ie iss ke ee le ee 60 minutes...............=1 degree. . > AR A 4 90 degrees. 2). on... ed et ele or ‘ igdraanie” oO 360 degrees.... Hivve ee = icirele,« Es ae ee 1 cir. = 360° = 21,600’=1, aes 5,000” USEFUL TABLES 3 AVOIRDUPOIS WEIGHT 437.5 grains EAE ....-=1 ounce. inet ne ary IOs 16 ounces. . Venger’ Phin tonne: oS 24,61: 100 pounds.. =] hundredweight Gives ett cwt. 20 cwt., or 2.000 Ib.. at ton. seks 1 T.=20 cwt. = 2,000 tice —32,000 oz. = ia 000, 000 ¢ gr. The avoirdupois pound contains 7,000 gr. LONG-TON TABLE 16 ounces. . Rete -=1 pound.. seks Se 112 ae : =] himdesiweisht:. . -cwt. 20 cwt., or 2,240 Ib.. Dts Sh wes eon Sok Rukh ae TROY WEIGHT Se oradins (O°) 26.0 voce se sts send hae scattered tstete gee pwt. 20 pennyweights........... =} ounce. . cates phate detous enn Oe 12 ounces..... .=1 pound.. A Pees | ° 1 Ib. eaty OZ. 7. =240 pwt. =5, 760 Pe DRY MEASURE Ptnts CDG). scnate occ eee ee QUAL b sete ce a piesa aes PA CIUAT RG eee ahs Sines tise cies of peck:... <.(4:.. “s pk 4 DOCKS. 5335.50. «'s see) bushel ie yeas weaeces bu. i ha. pe as =32 qt. =64 pt. The U.S. struck bushel contains 2,150.42 cu. in. =1.2444 cu. ft. By law, its dimensions are those of a cylinder 18} in. in diameter and 8 in. deep. The heaped bushel is equal to 1} struck bushels, the cone being 6 in. high. The dry gallon contains 268.8 cu. in., being 4 struck bushel. For approximations, the bushel may be taken at 1} cu. ft.; or 1 cu. ft. may be considered # bushel. The British bushel contains 2,218.19 cu. in. = 1.2837 cu. ft. = 1.032 U. S. bushels. LIQUID MEASURE Be GINS (SP) ois osc. 0'0,.5 5.5100. A DUR ora otis A ineio sees, bese PVPS sas esaad bs ae on to CGURTEs Ss wo ores casea we oatetlts Mr erCHUAT EG a. eons, Nec aie a4 oa LION a org tented ena oe oe 314 gallons. . ave .=1 barrel.. ditawe Sa ceeee 2 barrels, or © 63 mations: =] ideation © . -hhd. 1 hhd.=2 bbl. =63 gal. = 252 qt. =504 pt. =5, 016 gi. 4 USEFUL TABLES The U. S. gallon contains 231 cu. in. =.134 cu. ft., nearly; or 1 cu. ft. contains 7.481 gal. The following cylinders con- tain the given measures very closely: Diam. Height Diam. Height Gill... ... .12 in. 3 in. Gallon.... 7 in. 6 in. Pint. .....34 in. 3 in. 8 gallons 14 in. 12 in. ual. cc.s)s 34 in. 6 in. 10 gallons 14 in. 15 in. When water is at its maximum density, 1 cu. ft. weighs 62.425 lb. and 1 gal. weighs 8.345 lb. For approximations, 1 cu. ft. of water is considered equal to 74 gal., and 1 gal. as weighing 84 lb. The British imperial gallon, both liquid and dry, con- tains 277.274 cu. in. =.16046 cu. ft., and is equivalent to the volume of 10 lb. of pure water at 62° F. To reduce British to U.S. liquid gallons, multiply by 1.2. Conversely, to convert U. S. into British liquid gallons, divide by 1.2; or, increase the number of gallons one-fifth. THE METRIC SYSTEM The metric system is based on the meter, which, according to the United States Coast and Geodetic Survey Report of 1884, is equal to 39.370482 in. The value commonly used is 39.37 in., and is authorized by the United States govern- ment. The meter was originally intended to be one ten- millionth of the distance from the pole to the equator, measured on a meridian passing near Paris. This distance was carefully calculated, and a standard meter bar made and deposited among the archives of France, at Paris. It has since been discovered that the original calculations were at fault and the standard meter is somewhat short of one ten-millionth of the earth’s quadrant. Nevertheless, the error is so small that it was not considered necessary to change the standard to make it correct, and the original meter length is still preserved. There are three principal units—the meter, the liter (pro- nounced ‘‘lee-ter’’), and the gram, the units of length, . capacity, and weight, respectively. Multiples of these units USEFUL TABLES 5 are obtained by prefixing to the names of the principal units the Greek words deca (10), hecto (100), and kilo (1,000); the submultiples, or divisions, are obtained by prefixing the Latin words deci (zs), centi (xs), and milli (xgo0). These prefixes form the key to the entire system. The abbrevi- ations of the principal units of these submultiples begin with . a small letter, and those of the multiples begin with a capital letter. MEASURES OF LENGTH 10 millimeters (mm.).......=1 centimeter............ cm. 10 centimeters........4.... = ] decimeter.............dm. 10 Gecimetets:.. i005 is 6c.cc ed meter: 5. sce sare HEE Ae 10‘ meters ii. 6... Ssed ca os OE detameter. 65022... DRG 10 decameters.............=1 hectometer...........Hm. 10 hectometers............ =1 kilometer... ......... Km. MEASURES OF SURFACE (NOT LAND) 100 square millimeters (sq. mm.)............=1 square centimeter. ..sq. cm. 100 square centimeters. ....=1 square decimeter...sq. dm. 100 square decimeters......=1 square meter........sq. m. MEASURES OF VOLUME 1,000 cubic millimeters (cu. mm.)...........=1 cubic centimeter... .cu. cm. 1,000 cubic centimeters..... =1 cubic decimeter ....cu. dm. 1,000 cubic decimeters...... =] cubic meter......... cu. m. MEASURES OF CAPACITY 10 miliititers: (ml.).. 2... cenfiliter:. oo 5605. oes sels EO Centahters.:5 . 5 20c.s occ osic SE 2 OCHMEOR. cae ec sce 26 pGke MA ECTILOTS Fo vcarine: cic vie 31 wv 0 EL AIROP. Lainie wercle sue soa Oky POPHCOES otc tec ast satis arose e DL ORRNGED, cao cacn aenk secs 10 decaliters: ...4.2255.6.... <= 1 Heotoliter. osc cxreess 2 Hl. 10 peatediters. Se ee eae =1 kiloliter.. rete Fans <6 The liter is equal to the volume ae oa 1 cu. ben - 6 USEFUL TABLES MEASURES OF WEIGHT 10 milligrams (mg.)........=1 centigram............. -Cg. IO\centigrams. 65) .ss6066 om. =) decigram:: 2.3. cantdhienewaes MO Gecivrarmms: =.\fr, bes deed gram...) 2s sh ee 40 GF808 Ail athicen wii = Lidetagram:.. is 4.2 as ID decagrams. ose via. 5.08 =] hectogram............Hg. 10: hectograms............. =1 kilogram........ Kg. or kilo 1,000 kilograms............ Cay We ic) + Ee Be pay aes Pes bal The gram is the weight of 1 cu. cm. of pure 3 distilled ‘ents at a temperature of 39.2° F.; the kilogram is the weight of 1 liter of water; the ton is the weight of 1 cu. m. of water. CONVERSION TABLES By means of the tables on pages 8 and 9, metric measures can be converted into English, and vice versa, by simple addi- tion. All the figures of the values given are not required, four or five digits being all that are commonly used; it is only in very exact calculations that all the digits are necessary. Using table, proceed as follows: 1,828.8 Change 6,471.8 ft. into meters. Any number, as 121.92 6,471.8, may be regarded as .6,000+400+70+1 21.336 +.8; also, 6,000=1,0006; 400=100X4; etc. .3048 Hence, looking in the left-hand column of the .2438 upper part of the table, page 8, for figure 6 (the 1,972.6046 first figure of the given number), we find opposite it in the third column, which is headed Feet to Meters, the number 1.8287838. Now, using but five digits and increas- ing the fifth digit by 1 (since the next is greater than 5), we get 1.8288. In other words, 6 ft. = 1.8288 m.; hence, 6,000 ft. = 1,000 X 1.8288 = 1,828.8, simply moving the decimal point three places to the right. Likewise, 400 ft.=121.92 m.; 70 ft. =21.336 m.; 1 ft.=.3048 m.; and .8 ft.=.2438 m. Adding as shown above, we get 1,972.6046 m. Again, convert 19.635 kilos into pounds. The 22.046 work should be perfectly clear from the explana- 19.8416 tion given above. ‘The result is 43.2875 lb. 1.3228 The only difficulty in applying these tables lies .0661 in locating the decimal point. It may always be .0110 found thus: If the figure considered lies to the 43.2875 left of the decimal point, count each figure in ———— USEFUL TABLES P 7 order, beginning with units (but calling unit’s place zero) until the desired figure is reached; then move the decimal point to the right as many places as the figure being considered is to the left of the unit figure. Thus, in the first case above, 6 lies three places to the left of 1, which is in unit’s place; hence, the decimal point is moved three places to the right. By exchanging the words ‘‘right’”’ and ‘“‘left,’’ the statement will also apply to decimals. Thus, in the second case above, the 5 lies three places to the right of unit’s place; hence, the decimal point in the number taken from the table is moved three places to the left. USEFUL TABLES CONVERSION TABLE ENGLIisH MEAsuRES INTO METRIC Metric Metric Metric Metric Eng- ia Inches to Feet to Pounds to | Gallons to Meters Meters los Liters 1 .0253998 .38047973 .4535925 3.7853122 2 .0507996 .6095946 -9071850 7.5706244 3 .0761993 .9143919 1.3607775 | 11.3559366 4 .1015991 1.2191892 1.8143700 | 15.1412488 5 .1269989 1.5239865 | 2.2679625 | 18.9265610 6 .1523987 1.8287838 | 2.7215550 | 22.7118732 7 .1777984 2.1335811 3.1751475 | 26.4971854 8 .2031982 2.4383784 | 3.6287400 | 30.2824976 9 .2285980 2.7431757 | 4.0823325 | 34.0678098 10 .2539978 3.0479730 | 4.5359250 | 37.8531220 Metric Metric Metric Metric Eng- Square Square Cubic Pounds per lish Inches eet Feet Square Inch to to to to Kilo per Square Square Cubic Square Meters Meters Meters eter 1 .000645150 | .092901394 | .028316094 108 aes 2 .001290300 | .185802788 | .056632188 | 1,406.16482 3 .001935450 | .278704182 | .084948282 | 2,109.24723 4 .002580600 | .371605576 | .113264376 | 2,812.32964 5 .003225750 | .464506970 | .141580470 | 3,515.41205 6 003870900 | .557408364 | .169896564 | 4,218.49446 7 004516050 |. .650309758 | .198212658 | 4,921.57687 8 005161200 | .748211152 | .226528752 | 5,624.65928 9 .005806350 | .836112546 | .254844846 | 6,327.74169 10 .006451500 | .929013940 | .283160940 | 7,030.82410 USEFUL TABLES CONVERSION TABLE Metric MEasurRES INTO ENGLISH English English English English Metric Meters to Meters to Kilos to Liters to Inches Feet Pounds Gallons 1 39.370432 | 3.2808693 | 2.2046223 .2641790 2 78.740864 | 6.5617386 | 4.4092447 .5283580 3 118.111296 | 9.8426079 | 6.6138670 -7925371 4 157.481728 | 13.1234772 8.8184894 | 1.0567161 5 196.852160 | 16.4043465 | 11.0231117 | 1.3208951 6 236.222592 | 19.6852158 | 13.2277340 | 1.5850741 7 275.593024 | 22.9660851 | 15.4323564 | 1.8492531 8 314.963456 | 26.2469544 | 17.6369787 | 2.11343822 9 354.333888 | 29.5278237 | 19.8416011 | 2.3776112 10 393.704320 | 32.8086930 | 22.0462234 | 2.6417902 English English English English 4 Metric Square Square Cubic — eed Meters Meters Meters M 2 pas eter to to to to Pounds per Square uare Cubic Squ ri Inches eet Feet tack 1 1,550.03092; 10.7641034, 35.3156163 .001422310 2 3,100.06184 21 ‘5282068 70.6312326 .002844620 3 4,650.09276 32.2923102 105.9468489| .004266930 4 6,200.12368 43.0564136) 141.2624652 .005689240 5 7,750.15460| 53.8205170| 176.5780815) .007111550 6 9,300.18552) 64.5846204' 211.8936978 .008533860. 7 |10,850.21644| 75.3487238 247.2093141)| .009956170 * 8 |12,400.24736|) 86.1128272 282.5249304| .011378480 9 |13, '950.27828| 96. 8769306 317.8405467 .012800790 10 15, 500.30920 107.6410340 353.1561630 .014223100 10 USEFUL TABLES MATHEMATICAL TABLES CIRCUMFERENCES AND AREAS OF CIRCLES FROM 1-64 TO 100 Diam. | Circum. area ‘Diam. | Circum. Area oy 0491 .0002 4 12.5664 | 12.5664 a 0982 .0008 4 12.9591 | 13.3641 is 1963 .0031 4 13.3518 | 14.1863 i 3927 .0123 43 13.7445 | 15.0330 .0276 4 14.1372 | 15.9043 + 7854 0491 4 14.5299 | 16.8002 Ye 0767 4 14.9226 | 17.7206 ¥ 1.1781 1104 4 15.3153 | 18.6555 1.3744 1503 5 15.7080 | 19.6350 q 1.5708 1963 5 16.1007 1.7671 2485 5 16.4934 | 21.6476 a 1.9635 3068 5# 16.8861 | 22.6907 4h 2.1598 3712 5 17.2788 | 23.7583 12.1737 | 11.7933 9 28.2744 | 63.6174 USEFUL TABLES TABLE—(Continued) il Diam Circum Area Diam. | Circum. | Area 9 28.6671 | 65.3968 19 61.2612 | 298. 9 29.0598 | 67.2008 19 62.0466 | 306.355 9% 29.4525 | 69.0293 20 62.8320 | 314.160 9 29.8452 | 70.8823 204 63.6174 | 322.063 9 30.2379 | 72.7599 204 64.4028 | 330.064 9 .6306 | 74.6621 207 65.1882 | 338.164 9 31.0233 76.589 21 65.9736 | 346.361 10 31.4160 78.540 214 66.7590 | 354.657 104 32.2014 82.516 214 67.5444 | 363.051 HH 32.9868 86.590 212 .3298 | 371.543 10 33.7722 90.763 22 69.1152 | 380.134 11 34.5576 95.033 224 69.9006 | 388.822 114 35.3430 99.402 224 0.6860 | 397.609 11 36.1284 | 103.869 222 71.4714 | 406.494 11 36.9138 | 108.43 23 72.2568 | 415.477 12 37.6992 | 113.098 23+ 73.0422 | 424.558 124 38.4846 | 117.859 234 73.8276 | 433.737 12 39.2700 | 122.719 232 74.6130 | 443.015 12 40.0554 | 127.677 24 75.3984 | 452.390 13 8 132.733 244 6.1838 | 461.864 13} 41.6262 | 137.887 244 76.9692 | 471.436 13 42.4116 | 143.139 243 77.7546 | 481.107 13 43.1970 | 148.490 25 8.5400 | 490.875 14 .9824 | 153.938 25 79.3254 .742 14} 44.7678 | 159.485 25 80.1108 | 510.706 14 45.5532 | 165.130 25 80.8962 | 520.769 14 46.3386 | 170.874 26 81.6816 0.930 15 47.1240 | 176.715 26 82.4670 | 541.190 15} 47.9094 | 182.655 26 83.2524 | 551.547 15 6 188.692 26 84.0378 62.003 15 49.4802 | 194.828 27 84.8232 | 572.557 16 50.2656 | 201.062 2734 85.6086 | 583.209 16} 51.0510 | 207.395 274 86.3940 | 593.959 16 51.8364 | 213.825 272 87.1794 4.80 16 52.6218 | 220.354 28 87.9648 | 615.754 17 53.4072 | 226.981 28} 88.7502 | 626.798 17} 54.1926 | 233.706 284 89.5356 | 637.941 17 54.9780 | 240.529 287 90.3210 | 649.182 17 55.7634 | 247.450 29 91.1064 | 660.521 18 56.5 254.470 293 91.8918 | 671.959 18} 57.3342 | 261.587 2 92.6772 4 184 .1196 | 268.803 29 93.4626 | 695.128 182 58.9050 | 276.117 30 94.2480 | 706.860 19 59.6904 | 283.529 304 95.0334 | 718.690 194 60.4758 | 291.040 304 95.8188 | 730.618 12 USEFUL TABLES TABLE—(Continued) Diam. | Circum Area Diam. | Circum. Area 303 96.6042 742.645 | 42 131.947 | 1,385.450 31 97.3896 754.769 | 424 132.733 | 1,401.990 314 98.1750 766.992 | 424 133.518 | 1,418.630 314 98.9604 779.313 | 422 134.303 | 1,435.370 312 99.7458 791.732 | 43 135.089 | 1,452.200 32 100.5312 804.250 | 434 135.874 | 1,469.140 32} 101.3166 16.865 | 434 6.660 | 1,486.170 32 102.1020 829.579 | 432 137.445 | 1,503.300 32 102.8874 842.391 44 .230 | 1,520.530 33 103.673 855.301 44} 139.016 | 1,537.860 334 104.458 868.3 444 139.801 | 1,555.29 334 105.244 881.415 | 44? 140.587 | 1,572.81 33% 106.029 894.620 | 45 141.372 | 1,590.43 34 106.814 907.922 | 454 142.157 | 1,608.16 -84} 107.600 921.323 | 454 142.943 | 1,625.97 34 108.385 934.822 | 452 143.728 | 1,643.89 34 109.171 420 | 46 144.514 | 1,661.91 35 109.956 962.115 | 464 145.299 | 1,680.02 354 110.741 975.909 | 464 146.084 | 1,698.23 354 111.527 89.800 | 462 146.870 | 1,716.54 352 112.312 | 1,003.790 | 47 147.655 | 1,734.95 36 113.098 | 1,017.878 | 474 441 | 1,753.45 36+ 113.883 | 1,032.065 | 474 149.226 | 1,772.06 364 114.668 | 1,046.349 | 472 150.011 | 1,790.76 362 115.454 | 1,060.732 | 48 150.797 | 1,809.56 37 116.239 | 1,075.213 | 484 151.582 | 1,828.46 374 117.025 | 1,089.792 | 484 152.368 | 1,847.46 374 117.810 | 1,104.469 | 48? 153.153 | 1,866.55 372 118.595 1,119.244 49 53. 1,885.75 38 119.381 1,134.118 491 154.724 | 1,905.04 38} 120.166 | 1,149.089 | 494 155.509 | 1,924.43 384 120.952 | 1,164.159 | 493 156.295 | 1,943.91 38} 121.737 | 1,179.327 | 50 157.080 | 1,963.50 39 122.522 | 1,194.593 | 504 158.651 | 2,002.97 394 123.308 | 1,209.958 | 51 160.222 | 2,042.83 | 124.093 | 1,225.420 | 514 161.792 | 2,083.08 39 124.879 | 1,240.981 52 3 2,123.72 40 125.664 { 1,256.640 | 524 164.934 | 2,164.76 40+ 126.449 12725 53 166.505 | 2,206.19 404 127.235 | 1,288.250 | 534 168.076 | 2,248.01 403 128.020 | 1,304.210 |] 54 169.646 | 2,290.23 41 128.806 | 1,320.260 | 544 171.217 | 2,332.83 41} 129.591 1,336.410 55 172.788 | 2,375.83 41 130.376 | 1,352.6 554 174.359 | 2,419.23 41 131.162 | 1,369.000 | 56 175.930 | 2,463.01 USEFUL TABLES 13 TABLE—(Continued) Diam. | Circum -Area Diam. | Circum. Area 564 177. 2,507.19 784 246.616 | 4,839.83 57 179.071 | 2,551.76 79 248.186 | 4,901.68 574 80. 2,596.73 794 249.757 | 4,963.92 58 182.213 | 2,642.09 80 251.328 | 5,026.56 584 183.784 | 2,687.84 804 252.899 | 5,089.59 59 185.354 | 2,733.98 81 254.470 | 5,153.01 594 186.925 | 2,780.51 814 256.040 | 5,216.82 60 188.496 | 2,827.44 82 257.611 5,281.03 604 190.067 | 2,874.76 824 259.182 | 5,345.63 61 191.638 | 2,922.47 83 260.753 | 5,410.62 614 193.208 | 2,970.58 834 262.324 | 5,476.01 62 194.779 | 3,019.08 84 263.894 | 5,541.78 624 196.350 | 3,067.97 | .844 265.465 | 5,607.95 63 197.921 | 3,117.25 85 267.036 | 5,674.51 634 199.492 | 3,166.93 854 268.607 | 5,741.47 64 201.062 | 3,217.00 86 270.178 | 5,808.82 644 202.633 | 3,267.46 864 271.748 | 5,876.56 65 204.204 | 3,318.31 87 273.319 | 5,944.69 654 205.775 | 3,369.56 874 274.890 | 6,013.22 66 207.346 | 3,421.20 88 6.46 6,082.14 664 208.916 | 3,473.24 884 278.032 | 6,151.45 67 210.487 | 3,525.66 89 279.602 | 6,221.15 674 212.058 | 3,578.48 894 281.173 | 6,291.25 68 213.629 | 3,631.69 90 282.744 | 6,361.74 684 215.200 | 3,685.29 904 284.315 | 6,432.62 69 216.770 | 3,739.29 91 285.886 | 6,503.90 694 218.341 | 3,793.68 914 287.456 | 6,575.56 70 219.912 | 3,848.46 92 289.027 | 6,647.63 704 221.483 | 3,903.63 924 290.598 | 6,720.08 71 223.054 | 3,959.20 93 292.169 | 6,792.92 714 224.624 | 4,015.16 934 293.7 6,866.1 72 226.195 | 4,071.51 94 295.310 | 6,939.79 724 227.766 | 4,128.26 944 296.881 7,013.82 73 229.337 | 4,185.40 95 298.452 | 7,088.24 73% | 230.908 | 4,242.93 954 300.023 7,163.04 74 232.478 | 4,300.85 96 301.594 | 7,238.25 744 234.049 | 4,359.17 964 303.164 7,313.84 75 235.620 | 4,417.87 97 304.735 | 7,389.83 754 237.191 | 4,476.98 974 >| 306.306 | 7,466.21 76 238.762 | 4,536.47 98 307.877 | 7,542.98 764 240.332 | 4,596.36 984 9. 7,620.15 as 241.903 | 4,656.64 99 311.018 | 7.697.71 774 243.474 | 4,717.31 994 312.589 7,775.66 78 245.045 | 4,778.37 | 100 314.160 | 7,854.00 14 USEFUL TABLES DECIMAL EQUIVALENTS 1-64 | .015625 | 17-64 | .265625 | 33-64) .515625 | 49-64! .765625 1-32 | .031250|] 9-32/| .281250]17-32| .531250] 25-32) .781250 3-64 | .046875]| 19-64 | .296875 | 35-64} .546875 | 51-64) .796875 1-16 | .0625 - 312500} 9-16) .562500} 13-16 | .812500 5-64 | .078125} 21-64 | .328125 | 37-64] .578125 | 53-64} .828125 3-32 | .093750] 11-32 | .843750 | 19-32 | .593750 127-32 | 843750 7-64 | .109375| 23-64 | .359375 |] 39-64! .609375 155-64 | .859375 1-8 |.125000] 8-8 |.375000}] 5-8 | .625000] 7-8 | .875000 9-64 | .140625] 25-64 | .390625 | 41-64 | .640625 157-64 | .890625 5-32 | .156250| 13-32] .460250 | 21-32! .656250 |29-32 | .906250 11-64 |.171875| 27-64| .421875 | 43-64] .671875 |59-64 | .921875 3-16 | .187500] 7-16} .487500} 11-16) .687500 }15-16 | .937 13-64 | .203125] 29-64) .453125 | 45-64! .703125 161-64| .953125 7-32 |.218750]| 15-32 8750 | 23-32) .718750 {31-32 750 15-64 | .234375]| 31-64 | .484375| 47-64) .7343875 |63-64| .984375 1 250000} 1-2 3-4 |.7 1 BT DECIMALS OF A FOOT FOR EACH 1-32 INCH Inch 0” Sh 2” 3” 4” 5* 0 .0833 1667 | .2500 | .3333 4167 ay .0026 | .0859 1693 | .2526 | .8359 | .4193 vs .0052 | .0885 1719 | .2552 | .3385 | .4219 ¥ .0078 | .0911 1745 | .2578 | .8411 | .4245 .0104 | .0937 1771 .2604 | .3437 | .4271 fs 0130 | .0964 1797 | .2630 | .3464 | .4297 is 0156 | .0990 1823 | .2656 |! .3490 4323 az .0182 | .1016 1849 | .2682 | .3516 | .4349 4 .0208 | .1042 1875 | .2708 | .3542 | .4375 = .0234 | .1068 901 2734 | .3568 | .4401 ¥s .0260 | .1094 1927 760 | .3594 | .4427 4 .0286 | .1120 1953 2786 | .3620 | .4453 2 .0812 | .1146 | .1979 | .2812 | .3646 | .4479 AR .0339 1172 | .2005 | .2839 | .3672 | .4505 6 .0365 1198 | .2031 .2865 | .8698 | .4531 AB .0391 1224 | .2057 | .2891 .3724 | .4557 Py .0417 1250 | .2083 | .2917 | .38750 | .4583 Ay .0443 1276 2109 | .2943 | .3776 | .4609 Ys .0469 1302 2135 | .2969 | .3802 | .4635 43 .0495 1328 2161 -.2995 | .8828 | .4661 3 0521 .1354 2188 | .3021 0804 | .4688 §4 .0547 | .1380 2214 | .3047 | .8880 | .4714 so .0573 | .1406 2240 | .8073 | .38906 | .4740 33 .0599 | .1432 2266 | .8099 | .8932 4766 USEFUL TABLES DECIMALS OF A FOOT FOR EACH 1-32 INCH—(Continued) 15 Inch 0” 1” 2" 3” 4” 5” 0625 | .1458 | .2292 | .3125 | 3958 | .4792 ii 0651 | .1484 | .2318 | .3151 | .3984 | .4818 i 0677 | .1510 | .2344 | .3177.| .4010 | .4844 Fy] 0703 | .1536 | .2370 | .3203 | .4036 | .4870 % (0729 | .1562 | .2396 | .3229 | .4062 | .4896 rt) 0755 | .1589 | .2422 | .3255 | .4089 | .4922 33 0781 | .1615 | .2448 | 3281 | .4115 | .4948 iu 0807 | .1641 | .2474 | 3307 | .4141 | .4974 DECIMALS OF A FOOT FOR EACH 1-32 INCH Inch 6” | 7” 8” | 9” 10” | 11” 0 .5000 | .5833 | .6667 | .7500 | .8333 | .9167 ce 5026 | .5859 | .6693 | .7526 | .8359 | .9193 =a 5052 | .5885 | .6719 | .7552 | .8385 | .9219 * 5078 | .5911 | .6745 | .7578 | .8411 | .9245 4 5104 | .5937 | .6771 | .7604 | .8437 | .9271 dr 5130 | .5964 | .6797 | .7630 | .8464 | .9297 Ys 5156 | .5990 | .6823 | .7656 | .8490 | .9323 a 5182 | .6016 | .6849 | .7682 | .8516 | .9349 4 5208 | .6042 | .6875 | .7708 | .8542 | 9375 & 5234 | .6068 | .6901 | .7734 | .8568 | .9401 Ys 5260 | .6094 | .6927 | .7760 | .8594 | .9427 Ht 5286 | .6120 | .6953 | .7786 | .8620 | .9453 3 5312 | .6146 | .6979 | .7812 | .8646 | .9479 # 5839 | .6172 | .7005 | .7839 | .8672 | .9505 a 5365 | .6198 | .7031 | .7865 | .8698 | .9531 ii 5391 | .6224 | .7057 | .7891 | .8724 | .9557 $ .5417 | .6250 | .7083 | .7917 | .8750 | .9583 a 5443 | .6276 | .7109 | .7943 | .8776 | .9609 ¥s 5469 | .6302 | .7135 | .7669 | .8802 | .9635 bey 5495 | .6328 | .7161 | .7995 | .8828 | .9661 5 5521 | .6354 | .7188 | .8021 | .8854 | .9688 # 5547 | .6380 | .7214 | :8047 | .8880 | 9714 rm 5573 | .6406 | .7240 | .8073 | .8906 | .9740 34 5599 | .6432 | .7266 | .8099 | .8932 | .9766 3 5625 | .6458 | .7292 | 8125 | .8958 | .9792 rr} 5651 | .6484 | .7318 | .8151 | .8984 | .9818 i 5677 | .6510 | .7344 | .8177 | .9010 | 9844 .5703 | .6536 | .7370 | .8203 | .9036 | .9870 % 5729 | .6562 | .7396 | .8229 | .9062 | .9896 ra) 5755 | .6589 | .7422 | 18255 | .9089 | .9922 8 ‘5781 | .6615 | .7448 | .8281 | .9115 | :9948 ae 5807 | .6641 | .7474 | -8307 | .9141 } .9974 16 MATHEMATICS MATHEMATICS FORMULAS ={+[- :(Vx /+):-]}= The term formula, as used in mathematics and in techni- cal books, may be defined as a rule in which symbols are used instead of words; in fact, a formula may be regarded as a shorthand method of expressing a rule. Most persons having no knowledge of algebra regard for- mulas with distrust; they think that a person must be a good algebraic scholar in order to be able to use formulas. This idea, however, is erroneous. As a rule, no knowledge of any branch of mathematics except arithmetic is required to enable one to use a formula. Any formula can be expressed in words, and when so expressed it becomes a rule. Formulas are much more convenient than rules. They show at a glance all the operations that are to be performed; they do not have to be read three or four times, as is the case with most rules, to enable one to understand their meaning; they take up less space, both in the printed book and in one’s notebook, than rules; in short, whenever a rule can be expressed as a formula, the formula is to be preferred. It is the intention in the following pages to show ‘how to use such formulas as are likely to be encountered in ‘‘hand- books,”’ or other works of like nature. The signs used in formulas are the ordinary signs indica- tive of operations and the signs of aggregation. All these signs are used in arithmetic, but, to refresh the reader’s memory, their nature and uses will be explained before . proceeding further. The signs indicative of operations are six in number, viz.: +,—, X, +, |, and Vv. The sign (+) indicates addition, and is called plus; when placed between two quantities, it indicates that the two quantities are to be added. Thus, in the expression 25+17, the sign (+) shows that 17 is to be added to 25. MATHEMATICS 17 The sign (—) indicates subtraction, and is called minus; when placed between two quantities, it indicates that the quantity on the right is to be subtracted from that on the left. Thus, in the expression 25—17, the sign (—) shows that 17 is to be subtracted from 25. The sign (X) indicates multiplication, and is read times, or multiplied by; when placed between two quantities, it indi- cates that the quantity on the left is to be multiplied by that on the right. Thus, in the expression 25X17, the sign (xX) shows that 25 is to be multiplied by 17. The sign (+) indicates division, and is read divided by; when placed between two quantities, it indicates that the quantity on the left is to be divided by that on the right. Thus, in the expression 25+ 17, the sign (+) shows that 25 is to be divided by 17. Division is also indicated by placing a straight line between the two quantities. Thus, 25 | 17, 25/17, and 23 all indicate that 25 is to be divided by 17. If both quantities are placed on the same horizontal line, the straight line indicates that the quantity on the left is to be divided by thaton the right. When one quantity is below the other, the straight line between indicates that the quantity above the line is to be divided by the one below it. The sign (WV) indicates that some root of the quantity to the right is to be taken; it is called the radical sign. To indicate what root is to be taken, a small figure, called the index, is placed within the sign, this being always omitted when the square root is to be indicated. Thus 25 indicates that the square root of 25 is to be taken; ~25 indicates that the cube root of 25 is to be taken; etc. NOTE.—As the term ‘‘quantity’’ is a very convenient one to use, it will be defined. In mathematics the word guantity is applied to any- _ thing that is to be subjected to the ordinary operations of addition, subtraction, multiplication, etc., when it is desired not to be more ex- plicit and not to state exactly what the thingis. Thus, the terms ‘‘two or more numbers,’’ or “‘two or more quantities’? may be used. How- ate Head word quantity is more general in its meaning than the word number. The signs of aggregation are four in number, viz.: : (), (], and { 3 respectively called the vinculum, the paren- thesis, the brackets, and the brace. They are used when it is 18 MATHEMATICS desired to indicate that all the quantities included by them are to be subjected to the same operation. ‘Thus, suppose that the sum of 5 and 8 is to be multiplied by 7, and that the addition is to precede the multiplication. Any one of thefoursignsof aggregation may be employed toindicate the operation. Thus, 5+8X7, (5+8) X7,[5+8]X7, {5+8} X7 The vinculum is placed above the quantities that are to be treated as one quantity and subjected to the same operations. While any one of the four signs may be used as shown above, custom has restricted their use somewhat. The vincu- lum is rarely used except in connection with the radical sign. Thus, instead of writing {/(5+8), {[5+8], or 1 {5+8} for the cube root of 5 plus 8, all of which would be correct, the vinculum is nearly always used, 45 +8. In cases where only one sign of aggregation is needed (except, of course, when a root is to be indicated), the parenthesis is always used. Hence, (5+8) x7 would be the usual way of expressing the product of 5 plus 8 by 7. If two signs of aggregation are needed, the brackets and parenthesis are used, so as to avoid having a parenthesis within a parenthesis, the brackets being placed outside. For example, [(20—5)+3]X9 means that the difference between — 20 and 5 is to be divided by 3, and this result multiplied by 9. If three signs of aggregation are required, the brace, brackets, and parenthesis are used, the brace being placed outside, the brackets next, and the parenthesis inside. For example, { [(20—5)+3]x9—21} +8 means that the quo- tient obtained by dividing the difference between 20 and 5 by 3 is to be multiplied by 9, and that 21 is to be subtracted from the product thus obtained, and the result divided by 8. Should it be necessary to use all four signs of aggrega- tion, the brace would be put outside, the brackets next, the parenthesis next, and the vinculuminside. For example, {\(20—5+3)x9-21]+8}%12. The reason for using the brace in this last instance will be explained, as it is not . generally understood. MATHEMATICS 19 When several quantities are connected by the various signs indicating addition, subtraction, multiplication, and division, the operation indicated by the sign of multiplication must always be performed first. Thus, 2+3X4 equals 14, 3. being multiplied by 4 before adding to 2. Similarly, 10+2X5 equals 1, since 2X 5 equals 10, and 10+ 10 equals 1. Hence, in the preceding case, if the brace were omitted, the result would be 4; whereas, by inserting the brace, the result is 36. Following the sign of multiplication comes the sign of division in its order of importance. For example, 5—9+3 equals 2, 9 being divided by 3 before subtracting from 5. The signs of addition and subtraction are of equal value; that is, if several quantities are connected by plus and minus signs, the indicated operations may be performed in the order in which the quantities are placed. There is one other sign used, which is neither a sign of aggregation nor a sign indicative of an operation to be per- formed; it is (=), and is called the sign of equality; it means that all on one side of it is exactly equal to all on the other side. For example, 2=2, 5—3=2, 5X (14—9) =25. Having described the signs used in formulas, the formulas themselves will now be explained. First, consider the well- known rule for finding the safe load that a rectangular white-oak post will carry, which may be stated as follows: From unity subtract 1 one-hundredth of the dividend obtained by dividing the length of the post in inches by the least dimension of its cross-section in inches. Multiply the remainder by 1,000 times the area of the post section in square inches. The result is the safe load the post will carry. This rule is rather complicated, and it can be greatly simplified by putting it in the form of a formula. An examination of the rule will show that three quantities (viz., the area of the section, the length, and the least dimension of the cross-section) are involved. Hence, the rule might be expressed as follows: Safe load = 1,000 X area of section in square inches x ( << length in inches ) 100 X least dimension of cross-section in inches 20 _ MATHEMATICS This expression could be shortened by representing each quantity by a single letter. Thus, representing the safe load by W, the area of the cross-section of the post in square inches by A, the length of the post in inches by L, the least dimension of its cross-section in inches by D, and substi- tuting these letters for the quantities that they represent, the preceding expression would reduce to Bik, W=1,000X AX (i~Taep): a much simpler and shorter expression. This last expression is called a formula. As a further example, consider the rule as explained on page 300 for finding the safe resisting moment of a rein- forced-concrete beam, which is as follows: Multiply the area of the steel reinforcement in square inches by the distance from the center of the steel to the top of the beam. Multiply the product by 13,760. The result is the safe resisting moment of the beam in inch-pounds. In this case, let M represent the safe resisting moment in inch-pounds; a, the area of the steel, in square inches; and d, the distance, in inches, from the center of the rein- forcement to the top of the beam. Then, the preceding rule may be expressed by the following formula: M = 13,760 XdXa The formula just given shows, as was stated in the begin- ning, that a formula is really a shorthand method of express- ing a rule. It is customary, however, to omit the sign of multiplication between two or more quantities when they are to be multiplied together, or between a number and a letter representing a quantity, it being always understood that when two letters are adjacent with no sign between them, the quantities represented by these letters are to be multiplied. Bearing this fact in mind, the formula just given can be further simplified to M = 13,760da The sign of multiplication, evidently, cannot be omitted between two or more numbers, as it would then be impossible to distinguish the numbers. A near approach to this, how- ever, may be attained by placing a dot between the numbers MATHEMATICS 21 that are to be multiplied together, and this is frequently done in works on mathematics when it is desired to economize space. In such cases it is customary to put the dot higher than the position occupied by the decimal point. Thus, 2°3 means the same as 2X3; 542*749-1,006 indicates that the numbers 542, 749, and 1,006 are to be multiplied together. It is also customary to omit the sign of multiplication in expressions similar to the following: aX Vb+c, 3X (bc), (b+c) Xa, etc., writing them avb+c, 3(b+c), (b+c)a, etc. The sign is not omitted when several quantities are included by a vinculum, and it is desired to indicate that the quantities so included are to be multiplied by another quantity. For example, 3Xb+c, b+cXa, Vb+cXa, etc., are always written as here printed. Before proceeding further, it may be well to explain one other device used by formula makers, and which is apt to puzzle one who encounters it for the first time. It is the use of what mathematicians call primes and subs., and what printers call superior and inferior characters. As a rule, formula makers designate quantities by the initial letters of the names of the quantities. For example, they represent moment by M, stress by s, length by /, etc. This practice is to be commended, as the letter itself serves in many cases to identify the quantity that it represents. Some authors carry the practice a little further and represent all quantities of the same nature by the same letter throughout the book, always having the same letter represent the same thing. Now, this practice necessitates the use of the primes and subs. above mentioned when two quantities have the same name, but represent different things. Thus, consider the word moment as applied to beams. The safe moment equals the ultimate moment divided by the factor of safety. If it is decided to designate all moments by M, it will be necessary to make a distinction between the M that refers to safe moment and the M that refers to ultimate moment. This may be effected by designating the safe moment as Ms, and the ultimate moment as Mx. The formula may then be written M.= , in which F equals the factor of safety. 22 MATHEMATICS The main thing to be remembered is that when a formula is given in which the same letters occur several times, all like letters having the same primes or subs. represent the same quantities, while those which differ in any respect represent different quantities. Thus, in the formula R= i +Io+I3+I4 Gb AE. aes R represents the radius of gyration of a section composed of four parts; J;, Jo, J3, and I4 represent the moment of inertia of the respective parts about the same axis around which R is taken; and A represents the total area of the section. It is very easy to apply the above formula when the values of the quantities represented by the different letters areknown. All that is required is to substitute the numerical values of the letters, and then perform the indicated oper- ations. Thus, suppose that the values of Jj, Io, Iz, and I4 are 4.2, 3.6, 7.5, and 9.8, respectively, and that A is equal to 8 sq. in. Then, the value of R may be found by substi- tuting in the above formula; thus, nf Pate er SSS UE Apes , : R=\ 3 = 5 = ¥8.1375 =1.77 in. Attention is called to one or two other facts relating to formulas. 160 sometimes occur, the heavy line Expressions arenes to = 660 25 ; indicating that 160 is to be divided by the quotient obtained by dividing 660 by 25. If both lines were light, it would be impossible to tell whether 160 was to be divided by = or whether Ba irensbo be divided: Sy BS aks Inkter rahe 160 were desired, the expression would be written a In every case the heavy line indicates that all above it is to be divided by all below it. In an expression like ct 660° +35 the heavy line is not neces- MATHEMATICS ° 23 sary, because it is impossible to mistake the operation that Re to bs petioanek. But, ance 74 Seat Os 25 25 175-900 is substituted for 7+0°, the heavy line becomes necessary in order to make the resulting expression clear. Thus, 160. _—«:160_~—_—i160 7880 175+660 835 25 25 25 Fractional exponents are sometimes used instead of the radical sign; that is, instead of indicating the square, cube, - fourth root, etc. of some quantity, as 37, by 37, 437, 437, etc., those roots are indicated 372, 373, 374, etc. Should the numerator of the fractional exponent be some quantity other than 1, this quantity, whatever it may be, indicates that the quantity affected by the exponent is to be raised to the power indicated by the numerator; the denominator is always the index of the root. Hence, instead of expressing the cube root of the square of 37 as 4372, it may be expressed 37%, the denominator being the index of the root; in other words, 4372 =373. Likewise, Va +a%b)3 may also be writ- _ten (1 +a%)3, a much simpler expression. Several examples showing how to apply some of the more difficult formulas will now be given. The area of any segment of a circle that is less than (or equal to) a semicircle is expressed by the formula wa CG =h) . 860 2 . in which A =area of segment; r =3.1416; r=radius; E=angle obtained by drawing lines from the center to the extremities of arc of segment; c=chord of segment; and h=height of segment. EXAMPLE.—What is the area of a segment whose chord is 10 in. long, angle subtended by chord is 83.46°, radius is 7.5 in., and height of segment is 1.91 in.? SoLtuTion.—Applying the formula just given, 2 A ="rE_¢ a _ 3.1416 TK 88 6 10 7 5 — 1.91) = 40.968 — 27.95 = 13.018 sq. in., nearly 24 MATHEMATICS The area of any triangle may be found by means of the following formula, in which A=the area, and a, b, and ¢ represent the lengths of the sides: a2+b2—¢2 1-bNo-(=5=) ExAaMPLE.—What is the area of a triangle whose sides are 21 ft., 46 ft., and 50 ft. long? SoLtuTion.—In order to apply the formula, assume that a represents the side that is 21 ft. long; b, the side that is 50 ft. long; and c, the side that is 46 ft. long. Then substituting in the formula, -) fa PBR 2 _ 504 —( P+502—462\2 Ams Ve ( )- ay 2x50 4 _50 441 +2,500—2,116 \2 825 2 Vsti - ( 100 ) =25 441 (3) = 25 V441 — 8.25? = 25 V441 — 68.0625 = 25 V372.9375 = 25 X 19.312 = 482.8 sq. ft., nearly The above operations have been extended much further than was necessary in order to show every step of the process. The Rankine-Gordon formula for determining the least load in pounds that will cause a long column to break is in which P=load (pressure)in pounds; S= ultimate strength, in pounds per square inch, of material composing column; A=area of cross-section of column, in square inches; gq=a factor (multiplier) whose value depends on the shape of the ends of the column and on the material composing the column; 1=length of the column, in inches; G=least radius of gyration of cross-section of column. The meaning of the term G is explained on page 142. ExAMPLeE.—What is the least load that will break a hollow steel column whose outside diameter is 14 in., inside diam- eter 11 in., length 20 ft., and whose ends are flat? SoLuTIonN.—For steel, S=150,000, and g= for flat- 1 25,000 MATHEMATICS 25 ended steel columns. The area of the cross-section A = .7854 (d,2—d>?), d, and dz being the outside and inside diam- 2 eters, respectively; 1=20X12=240 in.; and Gute Substituting these values in the formula, Pus SA _ 150,000 X .7854(142— 112) as 2 - 1 2402 1+4¢3 1 +95 000 *T2@ +10 16 150,000 X 58.905 _ 8,835.750 _ -- tue es INVOLUTION AND EVOLUTION By means of the table on pages 31-48 the square, cube, square root, cube root, and reciprocal of any number may be obtained correct always to five significant figures, and in the majority of cases correct to six significant figures. In any number, the figures beginning with the first digit (a cipher is not a digit) at the left and ending with the last digit at the right, are called the significant figures of the number. Thus, the number 405,800 has the four significant figures, 4, 0, 5, and 8; and the number .000090067 has the five significant figures 9, 0, 0, 6, and 7. The part of the number consisting of its significant figures is called the significant part of the number. Thus, in the number 28,070, the significant part is 2807; in the number .00812, the significant part is 812; and in the number 170.3, the significant part is 1703. In speaking of the significant figures or of the significant part of a number, the figures are considered in their proper order, from the first digit at the left to the last digit at the right, but no attention is paid to the position of the decimal point. Hence, all numbers that differ only in the position of the decimal point have the same significant part. For example, .002103, 21.03, 21,030, and 210,300 have the same significant figures 2, 1, 0, and 3, and the same significant part 2103. The integral part of a number is the part to the left of the decimal point. 26 MATHEMATICS It will be more convenient to explain first how to use the table for finding square and cube roots. } Square Root.—First point off the given number into periods of two figures each, beginning with the decimal point and proceeding to the left and right. The following numbers are thus pointed off: 12703, 1/’27'03; 12.703, 12.70/30; 220000, 22/00/00; .000442, .00’04’42. Having pointed off the number, move the decimal point so that it will fall between the first and second periods of the significant part of the number. In the preceding numbers, the decimal point will be placed thus: 1.2703, 12.703, 22., 4.42. If the number has only three (or less) significant figures, find the significant part of the number in the column headed u; the square root will be found in the column headed Vx or ~ Vi0n, according to whether the part to the left of the decimal point contains one figure or two figures. Thus, 4.42 =2.1024, and V22= 10 X 2.20=4.6904. The decimal point is located in all cases by reference to the original number after pointing off into periods. There will be as many figures in the root preceding the decimal point as there are periods preceding the decimal point in the given number; tf the number is entirely decimal, the root is entirely decimal, and there will be as many ciphers following the decimal point in the root as there are cipher periods following the decimal point in the given number, Applying this rule, ‘220000=469.04 and .000442 = .021024. The operation when the given number has more than three significant figures is best explained by an example. EXxampPLe.—(a) ¥3.1416=? (6) V2342.9=? SoLuTION.—(a) Since the first period contains only one figure, there is no need of moving the decimal point. Look in the column headed n?2 and find two consecutive numbers, one a little greater and the other a little less than the given number; in the present case, 3.1684= 1.782 and 3.1329 = 1.772. The first three figures of the root are therefore 177. Find the difference between the two numbers between which the given number falls, and the difference between the smaller MATHEMATICS 27 number and the given number; divide the second difference by the first difference, carrying the quotient to three decimal places and increasing the second figure by 1 if the third is 5 or a greater digit. The two figures of the quotient thus determined will be the fourth and fifth figures of the root. In the present example, dropping decimal points, in the remainders, 3.1684—3.1329 =355, the first difference; 3.1416 — 3.1329 =87, the second difference; 87 +355 = .245+, or .25. Hence, V3.1416=1.7725. (b) 2342.9=? Pointed off into periods, the number appears as 23’42.90, and by moving the decimal point, the number appears as 23.4290; the first three figures of the root are 484; the first difference is 23.5225—23.4256=969; the second difference is 23.4290 — 23.4256 = 34; 34+969 = .035+, or .04. Hence, V¥2342.9 = 48.404. Cube Root.—The cube root of a number is found in the same manner as thesquare root, except the given number is pointed off into periods of three figures each. The following numbers would be pointed off thus: 3141.6, 3/141.6; 67296428, 67'296/428; 601426.314, 601’426.314; .0000000217, .000’000’021’700. Having pointed off, move the decimal point so that it will fall between the first and second periods of the significant part of the number, as in square root. In the above numbers the decimal point will be placed thus: 3.1416, 67.296,428, 601.426314, and 21.7. If the given nimber has but three (or less) significant figures, find the significant part of the number in the column headed u; the cube root will be found in the column headed Vn, 410, or W100, according to whether one, two, or three figures precede the decimal point after it has been moved. Thus, the cube root of 21.7 will be found oppo- site 2.17, in column headed Vi0n, while the cube root of 2.17 will be found in the column headed Vn, and the cube root of 217 in the column headed +100n, all on the same line. If the given number contains more than three significant figures, proceed exactly as described for square root, but use the column headed n3. ExampLe.—(a) ¥,0000062417=? (b) 4%50932676=? 28 MATHEMATICS SoLtuTion.—(a) Pointed off into periods, the number appears as 000’006’241’700, and by moving the decimal point the number appears as 6.2417. The number falls between 6.22950 = 1.848 and 6.33163 =1.853; the first differ- ence is 10213; the second difference is 6.24170—6.22950 = 1220; 1220+10213=.119+, or .12, the fourth and fifth figures of the root. The decimal point is located by the rule previously given; hence, 40000062417 =.018412. (b) ~50932676=? As the number contains more than six significant figures, reduce it to six significant figures by replacing all after the sixth figure with ciphers, increasing the sixth figure by 1 when the seventh is 5 or a greater digit. In other words, the first five figures of 450932700 and of 450932676 are the same. Pointed off into periods, the | number appears as 50’932’700, and by moving the decimal point, the number appears as 50.9327, which falls between 50.6530 =3.703 and 51.0648=3.71%; the first difference is 4118; the second difference is 2797; 2797+ 4118=.679+, or .68. The integral part of the root evidently contains three figures; hence ~V50932676=370.68, correct to five figures. Squares and Cubes.—If the given number contains but three (or less) significant figures, the square or cube is found in the column headed u? or 3, opposite the given number in the column headed u. If the given number contains more than three significant figures, proceed in a manner similar to that described for extracting roots. To square a number, place the decimal point between the first and second signifi- cant figures and find in the column headed Wn or Vi0n two consecutive numbers, one of which shall be a little greater and the other a little less than the given number. The remainder of the work is exactly as heretofore described. To locate the decimal point, employ the principle that the square of any number contains either twice as many figures as the number squared or twice as many less one. If the column headed V¥10” is used, the square will contain twice as many figures, while if the column headed Nn is used, the square will contain twice as many figures as the number squared, less one. If the number contains an integral part, the principle MATHEMATICS 29 is applied to the integral part only; if the number is wholly decimal, there will be twice as many ciphers following the decimal in the square or twice as many plus one as in the number squared, depending on whether V10n or Vn column is used. For example, 273.42? will contain five figures in the integral part; 4516.2? will contain eight figures in the integral part, all after the fifth being denoted by ciphers; .002945322 will have five ciphers following the decimal point; .0524362 will have two ciphers following the decimal point. EXxAMPLE.—(a) 273.422=? (6) .0524386?2=? SoLuTION.—(a) Placing the decimal point between the first and second significant figures, the result is 2.7342; this number occurs between 2.73313 = V7.47 and 2.73496 = V7.48 in the column headed Vu. The first difference is 2.73496 — 2.73313=183; the second difference is 2.73420— 2.73313 =107; and 107+183=.584+, or .58. Hence, 273.42? =74,758, correct to five significant figures. (b) Shifting the decimal point to between the first and second significant figures, the number 5.2436 is obtained. This falls between 5.23450 =: V27.4 and 5.24404= 27.5. The first difference is 954; the second difference is 910; 910+954 =.953+, or .95. Hence, .0524362=.0027495, to five sig- nificant figures. A number is cubed in exactly the same manner, using the column headed ©n, Vi0n, or Vi00n, according to whether the first period of the significant part of the number contains one, two, or three figures, respe tively. If the number con- tains an integral part, the number of figures in the integral part of the cube will be three times as many as in the given number if column headed ¥100n is used; it will be three times as many less 1 if the column headed 410n is used; and it will be three times as many less 2 if the column headed Wn is used. If the given number is wholly decimal, the cube will have either three times, three times plus one, or three times plus two, as many ciphers following the decimal as there are ciphers following the decimal point in the given number. ExAMPLE.—(a) 129.6843=? (6) .764423=? (c) .0324253=? SoLuTION.—(a) Placing the decimal point between the 30 MATHEMATICS first and second significant figures, the number 1.29684 is found between 1.29664= 2.18 and 1.29862= 12.19. The first difference is 198; the second difference is 20; and 20+198 =.101+, or .10. Hence, the first five significant figures are 21810; the number of figures in the integral part of the cube is 3X3—2=7; and 129.6848=2,181,000, correct to five sig- nificant figures. (b) 7.64420 occurs between 7.64032 = 1446 and 7.64603 = 447. The first difference is 571; the second difference is 888; and 388+571=.679+, or .68. Hence, the first five significant figures are 44668; the number of ciphers following the decimal point is 3X 0=0; and .764423 = .44866, correct to five significant figures. (c) 3.2425 falls between 3.24278= 134.1 and 3.23961 = 34.0. The first difference is 317; the second difference is 289; 289+317=.911+, or .91. Hence, the first five sig- nificant figures are 34091; the number of ciphers following the decimal point is 3X 1+1=4; and .0324253 = .000034091, correct to five significant figures. Reciprocals.—The reciprocal of a number is 1 divided by the number. By using reciprocals, division is changed into multiplication, since a+b=t—axe, The table gives the reciprocals of all numbers éxpressed by three significant figures correct to six significant figures. By proceeding in a manner similar to that just described for powers and roots, | the reciprocal of any number correct to five significant figures may be obtained. The decimal point in the result may be located as follows: If the given number has an integral part, the number of ciphers following the decimal point in the reciprocal will be one less than the number of figures in the integral part of the given number; and if the given number is entirely decimal, the number of figures in the integral part of the reciprocal will be one greater than the number of ciphers following the decimal point in the given number. For example, the reciprocal of 3370= .00029- 6736 and of .00348 = 287.356. When the number whose reciprocal is desired contains more than three significant figures, express the number to POWERS, ROOTS, AND RECIPROCALS 31 3 r—) | alkane anlanll alll anll aall aalh aula Serre Creo Seeee seas j ‘01489 | 3.20936 | 1.00990 | 2.17577 | 4.68755 | 970874 ‘0816 | 1.12486 | 1.01980 | 3.22490 | 1.01316 | 2.18278 | 4.70267 | .961539 1025 | 1.15763 | 1.02470 | 3.24037 | 1.01640 | 2.18976 | 4.71769 | .952381 -1236 | 1.19102 | 1.02956 | 3.25576 | 1.01961 | 2.19669 | 4.73262 392 x a é - -4161 | 1.68516 | 1.09087 | 3.44964 | 1.05970 | 2.28305 | 4.91868 | .840336 -4400 | 1.72800 | 1.09545 | 3.46410 | 1.06266 | 2.28943 | 4.93242 | .833333 4641 | 1.77156 | 1.10000 | 3.47851 | 1.06560 | 2.29577 | 4.94609 | .826446 4884 | 1.81585 | 1.10454 | 3.49285 | 1.06853 | 2.30208 | 4.95968 | .819672 1.5129 | 1.86087 | 1.10905 | 3.50714 | 1.07144 | 2.30835 : 97319 | .813008 1.5625 | 1.95313 | 1.11803 | 3.53553 ~1.07722 | 2.32080 5.00000 -800000 1.5876 | 2.00038 | 1.12250 | 3.54965 | 1.08008 | 2.32697 | 5.01330 | .793651 1.6129 | 2.04838 | 1.12694 | 3.56371 | 1.08293 | 2.33310 | 5.02653 | .787402 1.6384 | 2.09715 | 1.13137 | 3.57771 | 1.08577 | 2.33921 | 5.03968 | .781250 1.6641 | 2.14669 | 1.13578 | 3.59166 | 1.08859 | 2.34529 | 5.05277 | .775194 -6900 6 5.06580 1.7161 2.24809 1.14455 | 3.61939 | 1.09418 | 2.35735 | 5.07875 | .763359 1.7956 | 2.40610 | 1.15758 | 3.66060 | 1.10247 | 2.37521 | 5.11723 | .746269 1.8225 | 2.46038 | 1.16190 | 3.67423 | 1.10521 | 2.38110 | 5.12993 | 740741 1.8496 | 2.51546 | 1.16619 | 3.68782 | 1.10793 | 2.38696 | 5.14256 | .735294 1.8769 | 2.57135 | 1.17047 | 3.70135 | 1.11064 | 2.39280 | 5.15514 | .729927 1.9044 | 2.62807 | 1.17473 | 3.71484 | 1.11334 | 2.39861 | 5.16765 | .724638 1.9321 | 2.68562 | 1.17898 | 3.72827 | 1.11602 | 2.40439 | 5.18010 | .719425 -9600 | 2.74400 | 1.18322 | 3.74166 | 1.11869 | 2.41014 | 5.19249 | .714286 1.9881 | 2.80322 | 1.18743 | 3.75500 | 1.12135 | 2.41587 | 5.20483 | .709220 2.0164 | 2.86329 | 1.19164 | 3.76829 | 1.12399 | 2.42156 | 5.21710 | .704225 2.0449 | 2.92421 | 1.19583 | 3.78153 | 1.12662 | 2.42724 | 5.22932 | .699301 2.0736 | 2.98598 | 1.20000 | 3.79473 | 1.12924 | 2.43288 | 5.24148 | .694444 2.1025 | 3.04863 | 1.20416 | 3.80789 | 1.13185 | 2.43850 | 5.25359 | .689655 2.1316 | 3.11214 | 1.20830 | 3.82099 | 1.13445 | 2.44409 | 5.26564 | .684932 2.1609 | 3.17652 | 1.21244 | 3.83406 | 1.13703 | 2.44966 | 5.277 680272 2.1904 | 3.24179 | 1.21655 | 3.84708 | 1.13960 | 2.45520 | 5.28957 | .675676 2.2201 | 3.30795 | 1.22066 | 3.86005 | 1.14216 | 2.46072 | 5.30146 | .671141 SEE55 GESES SSREAS KESSS SSENS GRGSA 2.2500 | 3.37500 | 1.22474 | 3.87298 | 1.14471 | 2.46621 | 5.31329 | .666667 32 POWERS, ROOTS, AND RECIPROCALS dn | Vion | *i00n 3 3 to 3 on) + | 3 2.2801 | 3.44295 | 1.22882 | 3.88587 | 1.14725 | 2.47168 | 5 2.3104 | 3.51181 | 1.23288 | 3.89872 | 1.14978 | 2.47713 | 5.33680 2.3409 | 3.58158 | 1.23693 | 3.91152 | 1.15230 | 2.48255 | 5.34848 F . a 1.15480 | 2. 5.36011 2.4025 | 3.72388 | 1.24499 | 3.93700 | 1.15729 | 2.49332 | 5.37169 2.4336 | 3.79642 | 1.24900 | 3.94968 | 1.15978 | 2.49866 | 5.38321 oe agBge ee 3 s Ned 2 nw 8 _ w z w s s @ w & Fs & 2 oo : 7) s meee 3 a 2 S on 2.7225 | 4.49213 | 1.28452 | 4.06202 | 1 118167 | 2.54582 5.48481 2.7556 | 4.57430 | 1.28841 | 4.07431 | 1.18405 | 2.55095 | 5.49586 4,65746 | 1.29228 | 4.08656 | 1.18642 | 2.55607 | 5. 2.8224 | 4.74163 | 1.29615 | 4.09878 | 1.18878 | 2.56116 | 5.51785 2.8561 | 4.82681 | 1.30000 | 4.11096 | 1.19114 | 2.56623 | 5.52877 2.8900 | 4.91300 | 1.30384 | 4.12311 | 1.19348 | 2.57128 | 5.53966 5.00021 | 1.30767 | 4.13521 | 1.19582 | 2.57631 | 5.55050 - « & aRSs2 see i) g hs mH BF oO =] el ad 5 : be 3 a —J = S i) 2 g or & z co co 60 6 Biss 3 12.3201 14,2129 14.7456 14.8225 14.8996 14,9769 54.8720 55.3063 55.7430 56.1819 56.6231 57.0666 57.5125 1.91050 1.91311 1.51974 1 re 1.56322 3.27418 8.31714 3.32017 3.32319 3.32621 3.32922 3.34716 3.35014 3.35310 5607 7.27479 7.28108 7.28736 363 7.33723 7.34342 7.34960 7.85576 7.36192 7.36806 251889 POWERS, ROOTS, AND RECIPROCALS 37 : 1 n? n3 Nn 41002 = 16.0801 | 64.4812 | 2.00250 7.37420 | .249377 16.1604 | 64.9648 | 2.00499 7.38032 | 248756 6.2409 | 65.4508 | 2.00749 7.38644 | 248139 16.3216 | 65.9393 | 2. 739254 | 247525 16.4025 | 66.4301 | 2.01246 739864 | 1246914 16.4836 | 66.9234 | 2.01494 7.40472 | .2 16.5649 | 67.4191 | 2.01742 7.41080 | .245700 16.6464 | 67.9173 | 2.01990 7.41686 | .2 16.7281 | 68.4179 | 2.02237 7.42291 | 1244499 16.8100 | 68.9210 | 2.02485 7.42896 | 1243902 16.8921 | 69.4265 | 2.02731 7.43499 | 243309 16.9744 | 69.9345 | 2.02978 7.44102 | 242718 17.0569 | 70.4450 | 2.03224 7.44703 | 242131 17.1396 | 70.9579 | 2.03470 7.45304 | 241546 17.2225 | 71.4734 | 2.03715 7.45904 | 240964 17.3056 | 71.9913 | 2.03961 7.46502 } .240385 17.3889 | 72.5117 | 2.04206 7.47100 | .239808 17.4724 | 73.0346 | 2. 7.47697 | 239234 17.5561 | 73.5601 | 2.04695 7.48292 | _238664 17.6400 | 74.0880 | 2.049 "48887 | .238095 17.7241 | 74.6185 | 2.05183 7.49481 | .237530 1 75.1514 | 2.05426 7.50074 | 1236967 17.8929 | 75.6870 | 2.05670 7.50666 | 236407 17.9776 | 76.2250 | 2.05913 7.51257 | .235849 18.0625 | 76.7656 | 2.06155 7.51847 | 1235294 18.1476 | 77.3088 | 2.06398 7.52437 | 284742 18.2329 | 77.8545 | 2.06640 7.53025 | .234192 18.3184 | 78.4028 | 2.06882 7.53612 | 1233645 18.4041 | 78.9536 | 2.07123 7.54199 | |233100 4.30 | 18.4900 | 79.5070 | 2.07364 7.54784 | 1232558 4.31 | 18.5761 | 80.0630 | 2.07605 7.55369 | 232019 4.32 | 18.6624 | 80.6216 | 2.07846 7.55953 | 231482 4.33 | 18.7489 | 81.1827 | 2.08087 7.56535 | 230947 4.34 | 18.8356 | 81.7465 | 2.08327 757117 | .230415 4.35 | 18.9225 | 82.3129 | 2.08567 7.57698 | (229885 4.36 | 19.0096 | 82.8819 | 2. 7.58279 | 229358 4.37 | 19.0969 | 83.4535 | 2.09045 7.58858 | |228833 4.38 | 19.1844 | 84.0277 | 2.09284 7.59436 | 228311 4.39 | 19.2721 | 84.6045 | 2.09523 7.60014 | .227790 4.40 | 19.3600 | 85.1840 | 2.09762 "60590 | |227273 4.41 | 19.4481 | 85.7661 | 2.10000 7.61166 | .226757 4.42 | 19.5364 | 86.3509 | 2.10238 7.61741 | 1226244 4.43 | 19.6249 | 86.9383 | 2.10476 7.62315 | 225734 4.44 | 19.7136 | 87.5284 | 2.10713 7.62888 | 1225225 4.45 | 19.8025 | 88.1211 | 2.10950 7.63461 | .224719 4.46 | 19.9916 | 88.7165 | 2.11187 7.64082 | .224215 4.47 | 19.9809 | 89.3146 | 2.11424 7.64603 | 223714 4.48 | 20.0704 | 89.9154 | 2.11660 7.65172 | 223214 4.49 | 20.1601 | 90.5188 | 2.11896 7.65741 | 222717 4.50 | 20.2500 | 91.1250 | 2.12132 "222292 38 POWERS, ROOTS, AND RECIPROCALS SS a BS, 15 n? n3 Nn | ~vVion| Wn | Mion|*i00n| — 3 20.3401 | 91.7339 | 2.12368 | 6.71565 | 1.65219 | 3.55953 | 7.66877 | .221730 20.4304 | 92.3454 | 2.12603 | 6.72309 | 1.65341 | 3.56215 | 7.67443 | .221239 20.5209 | 92.9597 | 2.12838 | 6.73053 | 1.65462 | 3.56478 | 7.68009 | .220751 20.6116 | 93.5767 | 2.13073 | 6.73795 | 1.65584 | 3.56740 | 7.68573 | .220264 20.7025 | 94.1964 | 2.13307 | 6.74537 706 | 3.57002 | 7.69137 | .219780 8 SEBh Basta SkseHd SeRke aeeee seeee ares Nw rent a3 | 21.0681 | 96.7026 | 2.14243 | 6.77495 F ; 865 21.1600 | 97.3360 | 2.14476 | 6.78233 | 1.66310 | 3.58305 | 7.71944 | .217391 21,2521 | 97.9722 | 2.14709 | 6.78970 | 1.66431 | 3.58564 | 7.72503 | .216920 21.3444 | 98.6111 | 2.14942 | 6.79706 | 1.66551 | 3.58823 | 7.73061 | .216450 21.4369 | 99.2528 | 2.15174 | 6.80441 | 1.66671 | 3.59082 | 7.73619 | .215983 21.5296 | 99.8973 | 2.15407 | 6.81175 | 1.66791 | 3.59340 | 7.74175 | .215517 21.6225 | 100.545 | 2.15639 | 6.81909 | 1.66911 | 3.59598 | 7.74731 | .215054 21.7156 | 101.195 | 2.15870 | 6.82642 | 1.67030 | 3.59856 | 7.75286 | .214592 bp en ys 6.83374 | 1.67150 | 3.60113 | 7.75840 | .214133 ‘ 2.1 d F ‘ 21.9961 | 103.162 | 2.16564 | 6.84836 | 1.67388 | 3.60626 | 7.76946 | .213220 22.0900 | 103.823 | 2.16795 | 6.85565 | 1.67507 | 3.60883 | 7.77498 | .212766 22.1841 | 104.487 | 2.17025 | 6.86294 geben 3.61138 | 7.78049 | .212314 21 i 22.5625 | 107.172 | 2.17945 | 6.89202 | 1.68099 | 3.62158 | 7.80245 | 210526 22.6576 | 107.850 | 2.18174 | 6.89928 | 1.68217 | 3.62412 | 7.80793 | .210084 © 22.7529 | 108.531 | 2.18403 | 6.90652 | 1.68334 | 3.62665 | 7.81339 | .209644 22.8484 | 109.215 | 2.18632 | 6.91375 | 1.68452 | 3.62919 | 7.81885 | .209205 22.9441 | 109.902 | 2.18861 | 6.92098 | 1.68569 | 3.63171 | 7.82429 | .208768 23.0400 | 110.592 | 2.19089 | 6.92820 | 1.68687 | 3.63424 | 7.82974 | .208333 23.1361 | 111.285 | 2.19317 | 6.93542 | 1.68804 | 3.63676 | 7.83517 | .207900 23.4256 | 113.380 | 2.20000 | 6.95701 | 1.69154 | 3.64431 | 7.85142 | .206612 23.5225 | 114.084 | 2.20227 | 6.96419 | 1.69270 | 3.64682 | 7.85683 | .206186 23,6196 | 114.791 | 2.20454 | 6.97137 | 1.69386 | 3.64932 | 7.86222 | .205761 23.7169 | 115,501 | 2.20681 | 6.97854 | 1.69503 | 3.65182 | 7.86761 | .205339 23.8144 | 116.214 | 2.20907 | 6.98570 | 1.69619 | 3.65432 | 7.87299 | .204918 23.9121 | 116.930 | 2.21133 | 6.99285 | 1.69734 | 3.65682 | 7.87837 | .204499 24.0100 | 117.649 | 2.21359 | 7.00000 | 1.69850 | 3.65931 | 7.88374 | .204082 24,1081 } 118.871 | 2.21585 | 7.00714 | 1.69965 | 3.66179 | 7.88909 | .203666 24.2064 | 119.095 | 2.21811 | 7.01427 | 1.70081 | 3 66428 | 7.89445 | .203252 24.3049 | 119.823 | 2.22036 | 7.02140-| 1.70196 | 3.66676 | 7.89979 | .202840 24,4036 | 120.554 | 2 22261 | 7.02851 | 1.70311 | 3.66924 | 7.90513 | .202429 24,5025 | 121.287 | 2.22486 | 7.03562 | 1.70426 | 3.67171 | 7.91046 | .202020 24.6016 | 122.024 | 2.22711 | 7.04273 | 1.70540 | 3.67418 | 7.91578 | .201613 24,7009 | 122.763 | 2.22935 | 7.04982 | 1.70655 | 3.67665 | 7.92110 | .201207 24.8004 | 123.506 | 2.23159 | 7.05691 | 1.70769 | 3.67911 | 7.92641 | .200803 24.9001 | 124.251 | 2.23383 | 7.06399 | 1.70884 | 3.68157 | 7.93171 | .200401 25.0000 | 125.000 | 2.23607 | 7.07107 | 1.70998 | 3.68403 | 7.93701 | .200000 : . TREAD RPP R A PPR PD SSSR FLSSS SSELS GS POWERS, ROOTS, AND RECIPROCALS 39 3 N10 n a . 8 a2aes g 30.3601 30.4704 30.5809 30.6916 30.8025 30.9136 31.0249 31.1364 31.2481 31.3600 31.4721 34, noe 174.677 eos _ 193, 101 194.105 195,112 196.123 197.137 198.155 199.177 200.202 205.379 206.425 207.475 : 35797 2.36008 2.36220 2.36432 2.36643 2.38747 2.38956 2.39165 2.39374 2.39583 2.39792 2.44745 2.44949 7.61577 7.62234 1.77051 1.77157 1.77263 1.78108 1.78213 1.78318 1.78422 1.78527 1.78632 1.78736 1.79876 1.81712 3.83495 3.83721 3.83948 3.84174 3.87532 8.21303 8.21797 8.22290 8.22783 8.23275 8.23766 8.24257 8.24747 8.41554 8.42025 8.42494 8.42964 8.43433 173913 173611 172117 171821 -171527 171233 -170940 POWERS, ROOTS, AND RECIPROCALS 41 5 | n na n3 Nn 4n | 40n|*i00n = 6.01 | 36.1201 | 217.082 | 2.45153 1.81813 | 3.91704 | 8.43901 | .1 6.02 | 36.2404 | 218.167 | 2.45357 1.81914 | 3.91921 | 8.44369 | .166118 6.03 | 36.3609 | 219.256 | 2.45561 1.82014 | 3.92138 | 8.44836 | .165888 6.04 | 36.4816 | 220.349 | 2.45764 1.82115 | 3.92355 | 8.45308 | .165568 6.05 | 36.6025 | 221.445 | 2.45967 1.82215 | 3.92571 | 8.45769 | .165289 6.06 | 36.7236 | 222.545 | 2.46171 1.82316 | 3.92787 | 8.46235 | .165017 6.07 | 36.8449 | 223.649 | 2.46374 1.82416 | 3.93003 | 8.46700 | 164745 6.08 | 36.9664 | 224.756 | 2.46577 1.82516 | 3.93219 | 8.47165 | 1164474 6.09 | 37.0881 | 225.867 | 2.46779 1.82616 | 3.93434 | 8.47629 | .164204 6.10 | 37.2100 | 226.981 | 2.46982 1.82716 | 3.93650 | 8.48093 | .163934 6.11 | 37.3321 | 228.099 | 2.47184 1.82816 | 3.93865 | 8.48556 | .163666 6.12 | 37.4544 | 229.221 | 2.47386 1.82915 | 3.94079 | 8.49018 | .168399 6.13 | 37.5769 | 230.346 | 2.47588 183015 | 3.94294 | 8.49481 | .163132 6.14 | 37.6996 | 231.476 | 2.47790 1.83115 | 3.9 8.49942 | .162866 3.15 | 37.8225 | 232.608 | 2.47992 1.83214 | 3.94722 | 8.50404 | .162602 6.16 | 37.9456 | 283.745 | 2.48193 1.83818 | 3.94936 | 8. 162388 6.17 | 38.0689 | 234.885 | 2.48395 '83412 | 3.95150 | 8.51324 | .162075 6.18 | 38.1924 | 236.029 | 2.48596 1.83511 | 3.95 ‘51784 | 161812 6.19 | 38.3161 | 237.177 | 2.48797 1.83610 | 3.95576 | 8.52248 | .161551 6.20 | 38. 238,328 | 2.48998 1.83709 | 3.95789 | 8.52702 | .161290 6.21 | 38.5641 | 239.483 | 2.49199 1.88808 | 8.9 8.53160 | .161031 6.22 | 38.6884 | 240.642 | 2.49399 1.83906 | 8.96214 | 8.53618 | .160772 6.23 | 38.8129 | 241.804 | 2.49600 1.84005 | 8.96426 | 8.54075 | .160514 6.24 | 38.9376 | 242.971 | 2.49800 1.84103 | 3.96639 | 8.54532 | .160256 6.25 | 39.0625 | 244.141 | 2.50000 1.84202 | 8.96850 | 8.54988 | .160000 .26 | 39.1876 | 245.314 | 2.50200 1.84300 | 3.97062 | 8.55444 | .159744 "27 | 39.3129 | 246.492 | 2.50400 1.84398 | 8.97273 | 8.55899 | .159490 "28 | 39.4384 | 247.678 | 2.50599 1.84496 | 3.97484 | 8.56354 | .169236 6.29 | 39.5641 | 248.858 | 2.50799 1.84594 | 3.97695 | 8.56808 | .158988 6.30 | 89.6900 | 250.047 | 2.50998 1.84691 | 3.97906 | 8.57262 | .158730 6.31 | 39.8161 | 251.240 | 2.51197 1.84789 | 3.98116 | 8.57715 | .158479 6.32 | 39.9424 | 252.436 | 2.51396 1.84887 | 8.98326 | 8.58168 | .158228 6.33 | 40.0689 | 253.636 | 2.51595 1.84984 | 8.98536 | 8.58620 | 157978 6.34 | 40.1956 | 254.840 | 2.51794 1.85082 | 8.98746 | 8.59072 | .157729 6.35 | 40.8225 | 256.048 | 2.51992 1.85179 | 3. 8.59524 | .157 6.36 | 40.4496 | 257.259 | 2.52190 1.85276 | 8.99165 | 8.59975 | .157238 6.37 | 40.5769 | 258.475 | 2.52389 1.85373 | 3.99374 | 8.60425 | .156986 6.38 | 40.7044 | 259.694 | 2.52587 1.85470 | 3. 8.60875 | .156740 6.39 | 40.8321 | 260.917 | 2.52784 1.85567 | 3.99792 | 8.61825 | .156495 6.40 | 40.9600 | 262.144 | 2.52982 1.85664 | 4. 8.61774 | .156250 6.41 | 41.0881 | 263.375 | 2.53180 1.85760 | 4.00208 | 8.62222 | .156006 6.42 | 41.2164 | 264.609 | 2.53377 1.85857 | 4.00416 | 8.62671 | .155763 6.43 | 41.3449 | 265.848 | 2.58574 1.85953 | 4.00624 | 8.63118 | .155521 6.44 | 41.4736 | 267.090 | 2.53772 1.86050 | 4.00882 | 8.63566 | .155280 6.45 | 41.6025 | 268.336 | 2.53969 1.86146 | 4.01039 | 8.64012 6.46 41.7316 | 269.586 | 2.54165 1.86242 | 4.01246 | 8.64459 | .154799 647 | 41.8609 | 270.840 | 2.54362 1.86388 | 4.01453 | 8.64904 | .154560 6.48 | 41.9904 | 272,098 | 2.54558 1.86434 | 4.01660 | 8.65350 | .154821 6.49 | 42.1201 | 273.359 | 2.54755 1.86530 | 4.01866 | 8.65795 | .154088 6.50 | 42.2500 | 274.625 | 2.54951 1.86626 | 4.02073 | 8.66239 | |153846 42 POWERS, ROOTS, AND RECIPROCALS n2 n3 Vn | ion| Wn | Vi0n|*i00n 3 42.3801 | 275.894 | 2.55147 | 8.06846 | 1.86721 | 4.02279 | 8.66683 42.5104 | 277.168 | 2.55343 | 8.07465 | 1.86817 | 4.02485 | 8.67127 42.6409 | 278.445 | 2.55539 | 8.08084 | 1.86912 | 4.02690 | 8.67570 42.7716 | 279.726 | 2.55734 | 8.08703 | 1.87008 | 4.02896 | 8.68012 42,9025 | 281.011 | 2.55930 | 8.09321 | 1.87103 | 4.03101 | 8.68455 43.0336 | 282.300 | 2.56125 | 8.09938 | 1.87198 | 4.03306 | 8.68896 43.1649 | 283.593 | 2.56320 | 8.10555 | 1.87293 | 4.03511 | 8.69338 43,2964 | 284.890 | 2.56515 | 8.11172 | 1.87388 | 4.03715 | 8.69778 43.4281 | 286.191 | 2.56710 | 8.11788 | 1.87483 | 4.03920 | 8.70219 43,5600 | 287.496 | 2.56905 | 8.12404 | 1.87578 | 4.04124 | 8.70659 43.6921 | 288.805 | 2.57099 | 8.13019 | 1.87672 | 4.04328 | 8.71098 43.8244 | 290.118 | 2.57294 | 8.13634 | 1.87767 | 4.04532 | 8.71537 43.9569 | 291.434 | 2.57488 | 8.14248 | 1.87862 | 4.04735 | 8.71976 44,0896 | 292.755 | 2.57682 | 8.14862 | 1.87956 | 4.04939 | 8.72414 44,2225 | 294,080 | 2.57876 | 8.15475 | 1.88050 | 4.05142 | 8.72852 44,3556 | 295.408 | 2.58070 | 8.16088 | 1.88144 | 4.05345 | 8.73289 44,4389 | 296.741 | 2.58263 | 8.16701 | 1.88239 | 4.05548 | 8.73726 44.6224 | 298.078 | 2.58457 | 8.17313 | 1.88333 | 4.05750 | 8.74162 44,7561 | 299.418 | 2.58650 | 8.17924 | 1.88427 | 4.05953 | 8.74598 44,8900 | 300.763 | 2.58844 | 8.18535 | 1.88520 | 4.06155 | 8.75034 45.0241 | 302.112 | 2.59037 | 8.19146 | 1.88614 | 4.06357 | 8.75469 45.1584 | 303.464 | 2.59230 | 8.19756 | 1.88708 | 4.06558 | 8.75904 45.2929 | 304.821 | 2.59422 | 8.20366 | 1.88801 | 4.06760 | 8.76338 45.4276 | 306.182 | 2.59615 | 8.20975 | 1.88895 | 4.06961 | 8.76772 8.77205 45.6976 | 308.916 | 2.60000 | 8.22192 | 1.89081 | 4.07364 | 8.77638 45.8329 | 310.289 | 2.60192 | 8.22800 | 1.89175 | 4.07564 | 8.78071 45.9684 | 311.666 | 2.60384 | 8.23408 | 1.89268 | 4.07765 | 8.78503 46.1041 | 313.047 | 2.60576 | 8.24015 | 1.89361 | 4.07965 | 8.78935 46.2400 | 314.432 | 2.60768 | 8.24621 | 1.89454 | 4.08166 | 8.79366 46.3761 | 315.821 | 2.60960 | 8.25227 | 1.89546 | 4.08365 | 8.79797 46.5124 | 317.215 | 2.61151 | 8.25833 | 1.89639 | 4.08565 | 8.80227 46.6489 | 318.612 | 2.61343 | 8.26438 | 1.89732 | 4.08765 | 8.80657: 46.7856 | 320.014 | 2.61534 | 8.27043 | 1.89824 | 4.08964 | 8.81087 46.9225 | 321.419 | 2.61725 | 8.27647 | 1.89917 | 4.09164 | 8.81516 47.0596 | 322.829 | 2.61916 | 8.28251 | 1.90009 | 4.09362 | 8.81945 47.1969 | 324.243 | 2.62107 | 8.28855 | 1.90102 | 4.09561 | 8.82373 47.3344 | 325.661 | 2.62298 | 8.29458 | 1.90194 | 4.09760 | 8.82801 47.4721 | 327.083 | 2.62488 | 8.30060 | 1.90286 | 4.09958 | 8.83229 47.6100 | 328.509 | 2.62679 | 8.30662 | 1.90378 | 4.10157 | 8.83656 47.7481 | 329.939 | 2.62869 | 8.31264 ; 1.90470 | 4.10355 | 8.84082 47.8864 | 331.374 | 2.63059 | 8.31865 | 1.90562 | 4.10552 | 8.84509 48.0249 | 332.813 | 2.63249 | 8.32466 | 1.90653 | 4.10750 | 8.84934 48.1636 | 334.255 | 2.63439 | 8.33067 | 1.90745 | 4.10948 | 8.85360 48.3025 | 335.702 | 2.63629 | 8.33667 | 1.90837 | 4.11145 | 8.85785 48.4416 | 837.154 | 2.63818 | 8.34266 | 1.90928 | 4.11342 | 8.86210 48.5809 | 338.609 | 2.64008 | 8.34865 | 1.91019 | 4.11539 | 8.86634 48.7204 | 340.068 | 2.64197 | 8.35464 | 1.91111 | 4.11736 | 8.87058 48.8601 | 341.532 | 2.64386 | 8.36062 | 1.91202 | 4.11932 | 8.87481 49.0000 | 343.000 | 2.64575 | 8.36660 | 1.91293 | 4.12129 | 8.87904 NAARAM APAMA MAAA® AAAAM ABAAH ARHHR PAADHR PHARA BAAAHA HAI2aH SSSSE FLESL SSSRR SLSSS SBS AKRSNA SSRAFZ HSPBSS SSRSAIF ARFSSS & or & o wo So a 4 ~r nw S S a fo +) be oa - _ % co & ~ —] =I _ & POWERS, ROOTS, AND RECIPROCALS 43 3 n? nt | va |vion| % | *on|*ioon| 2 49.1401 | 344.472 | 2.64764 | 8.37257 | 1.91384 | 4.12325 | 8.88327 | .142653 49.2804 | 345.948 | 2.64953 | 8.37854 | 1.91475 | 4.12521 | 8.88749 | .142450 49.4209 | 347.429 | 2.65141 | 8.38451 | 1.91566 | 4.12716 | 8.89171 | .142248 aaaasa SN ANa8a As9g88 ANAS AAA 49.5616 Lay tn 2.65330 | 8.39047 | 1.91657 | 4.12912 | 8.89592 | .142046 49.7) B 2.65518 | 8.39643 | 1.91747 | 4.13107 | 8.90013 | .141844 49.8426 | 351.896 | 2.65707 | 8.40238 | 1.91838 | 4.13303 | 8.90434 | .141643 P 2.65895 | 8 1.91929 | 4.13498 | 8 141443 50.1264 | 354.895 | 2.66083 | 8.41427 | 1.92019 | 4.13695 | 8.91274 | .141243 50.2681 | 356.401 | 2.66271 | 8.4: 1.92109 | 4.13887 -141044 50.4100 | 357.911 | 2.66458 | 8.42615 | 1.92200 | 4.14082 | 8.92112 | . 8 3 52.1284 | 376.367 | 2.68701 | 8.49706 patois 4.16402 | 8.97110 | .138504 52.4176 | 379.503 | 2.69072 | 8.50882 | 1.93455 | 4.16786 | 8.97988 | .138122 52.5625 | 381.078 | 2.69258 | 8.51469 | 1.93544 | 4.16978 | 8.98351 | .137931 52.7076 | 382.657 | 2.69444 | 8.52056 | 1.93633 | 4.17169 | 8.98764 | .137741 SB Beuish BERGE REERE BESS8 ReRSS 48 REBRE BRE SSE55 SEESE S83 52.8529 | 384.241 | 2.69629 | 8.52643 | 1.93722 | 4.17361 | 8.99176 | .137552 53.5824 | 392.223 | 2.70555 | 8.55570 | 1.94165 | 4.18315 | 9.01233 | .136612 1 s . : 4. 08156 | . 2500 | 421.875 | 2.73861 | 8.66025 1.95748 | S216 | 9.08560 -133333 POWERS, ROOTS, AND RECIPROCALS 3 ne Nn 1007 SS SSS93 sae88 sees sees Be SSRIS SFBVS SSSAS SRESA 1.73 Bae & © &esse & SCNAAT ATTA Aaa S8eee 58.5225 58.6756. 58.8289 58.9824 59.1361 59.2900. 59.4441 59.5984 59.7529 59.9076 60.0625 60.2176 60.3729 60.5284 60.6841 61.6225 61.7796 61.9369 63.5209 423.565 447.697 449.455 451,218 452.985 454,757 456,533 458.314 472.729 474,552 476.380 478.212 480.049 491.169 493.039 494.914 502.460 504.358 506.262 508.170 510.082 512,000 2.74044 2.74226 2.74408 2.74591 2.74773 2.74955 2.77669 2.77849 2.78029 2.78209 2.78388 2.78568 2.78747 2.78927 2.79106 2.79285 2.79464 2.79643 2.79821 2.80000 2.80179 2.80357 2.80535 2.80713 2.80891 2.81069 2.81247 2.81425 2.81957 2.82135 2.82843 8.71780 8.72353 8.72926 8.73499 8.74071 8.74643 8.75214 8.80341 8.80909 8.81476 8.82043 8.82610 8.83176 8.83742 8.91628 |. 8.92188 8.92749 8.93308 8.93868 8.94427 1,96523 1.97040 1.97126 1.97211 1.97297 1.97895 1.97980 1.98065 1.98150 1.98234 1,98319 1.98911 4.22651 4.22838 4.23024 4.23210 4.23396 4,23582 4,23768 4.23954 4.25248 4.28177 4.28359 4.29265 4.29446 4.29627 4.29807 4.29987 4.30168 4.30348 4.30528 4.30707 4.30887 9.08964 9.09367 9.09770 9.10173 9.10575 9.14179 9.14577 9.14976 9.15374 9.15771 9.16169 9.16566 9.16962 9.17359 9.17754 9.18150 9.18545 9.18940 9.19335 9.19729 9.20123 9.20516 9.22087 9.22479 9.22871 9.23262 9.23653 9.24043 9.24433 9.24823 9.28318 POWERS, ROOTS, AND RECIPROCALS 45 rat 1 n n3 Nn |Vi0n| Wn | MOn| oon 2 8.01 513.922 | 2.83019 | 8.94986 | 2.00083 | 4.31066 | 9.28704 | .124844 8.02 615.850 | 2.83196 | 8.95545 | 2.00167 | 4.31246 | 9.29091 | 124688 8.03 517.782 | 2.83373 | 8.96103 | 2.00250 | 4.31425 | 9.29477 | .124533 8.04 519.718 | 2.83549 | 8. 2.00333 | 4.31604 | 9.29862 | .124378 8.05 521.660 | 2.83725 | 8.97218 | 2.00416 | 4.31783 | 9.30248 | 1124224 8.06 523.607 | 2.83901 | 8.97775 | 2.00499 | 4.81961 | 9.80633 | .124070 8.07 25.558 | 2.84077 | 8.98332 | 2.00582 | 4.32140 | 9.31018 | .123916 8.08 527.514 | 2.84253 | 8.98888 | 2. 4.32818 | 9.31402 | .123762 8.09 529.475 | 2.84429 | 8.99444 | 2.00747 | 4.82497 | 9.31786 | .123609 8.10 531.441 | 2.84605 | 9.00000 | 2. 4.32675 | 9.32170 | .123457 8.11 533.412 | 2.84781 | 9.00555 | 2.00912 | 4.32858 | 9.32553 | .123305 8.12 535.387 | 2.84956 | 9.01110 | 2.00995 | 4.33031 | 9.32936 | 123153 8.13 537.368 | 2.85132 | 9.01665 | 2.01078 | 4.33208 | 9.33319 | .123001 8.14 539.353 | 2.85307 | 9.02219 | 2.01160 | 4.33386 | 9.33702 | .122850 8.15 641.343 | 2.85482 | 9.02774 | 2.01242 | 4.33563 | 9.34084 | 1122699 8.16 543.338 | 2.85657 | 9.03827 | 2.01325 | 4.83741 | 9.84466 | .122549 8.17 545.339 | 2.85832 | 9.03881 | 2.01407 | 4.33918 | 9.34847 | .122399 8.18 547.343 | 2.86007 | 9.04434 | 2.01489 | 4.34095 | 9.35229 | 1122249 8.19 549.353 | 2.86182 | 9.04986 | 2.01571 | 4.34272 | 9.35610 | .122100 8.20 551.368 | 2.86356 | 9.05539 | 2.01653 | 4.3 9.35: 121951 8.21 553.388 | 2.86531 | 9.06091 | 2.01735 | 4.34625 | 9.36370 | .121808 8.22 565.412 | 2.86705 | 9.06642 | 2.01817 | 4.34801 | 9.36751 | 121655 8.23 557.442 | 2.86880 | 9.07193 | 2.01899 | 4.34977 | 9.37130 | .121507 8.24 559.476 | 2.87054 | 9.07744 | 2.01980 | 4.35153 | 9.37510 | 1121359 8.25 561.516 | 2.87228 | 9.08295 | 2.02062 | 4.35829 | 9.37889 | {121212 8.26 563.560 | 2.87402 | 9.08845 | 2.02144 | 4.35505 | 9.38268 | .121065 8.27 565.609 | 2.87576 | 9.09395 | 2.02225 | 4.35681 | 9.38646 | 120919 8.28 567.664 | 2.87750 | 9.09945 | 2.02307 | 4.35856 | 9.39024 | .120773 8.29 569.723 | 2.87924 | 9.10494 | 2.02388 | 4.36032 | 9.39402 | |120627 8.30 571.787 | 2.88097 | 9.11043 | 2.02469 | 4.36207 | 9.39780 | {120482 8.31 573.856 | 2.88271 | 9.11592 | 2.02551 | 4.86382 | 9.40157 | .120337 8.32 575.930 | 2.88444 | 9.12140 | 2.02632 | 4.36557 | 9.40534 | .120192 8.33 578.010 | 2.88617 | 9.12688 | 2.02713 | 4.36732 | 9.40911 | .120048 8.34 580.094 | 2.88791 | 9.13236 | 2.02794 | 4.36907 | 9.41287 | .119904 8.35 582.183 | 2.88964 | 9.13783 | 2.02875 | 4.37081 | 9.41663 | .119761 8.36 584.277 | 2.89137 | 9.14330 | 2.02956 | 4.87255 | 9.42039 | .119617 8.37 586.376 | 2.89310 | 9.14877 | 2.03037 | 4.37480 | 9.42414 | .119474 8.38 588.480 | 2.89482 | 9.15423 | 2.03118 | 4.37604 | 9.42789 | 119332 8.39 590.590 | 2.89655 | 9.15969 | 2.03199 | 4.37778 | 9.43164 | .119190 8.40 592.704 | 2.89828 | 9.16515 | 2.03279 | 4.37952 | 9.43539 | .119048 8.41 594,823 | 2.90000 | 9.17061 | 2.03360 | 4.38126 | 9.43913 | .118906 8.42 596.948 | 2.90172 | 9.17606 | 2.03440 | 4.38299 | 9.44287 | |118765 8.43 599.077 | 2.90345 | 9.18150 | 2.03521 | 4.38473 | 9.44661 | .118624 8.44 601.212 | 2.90517 | 9.18695 | 2.03601 | 4. 9.45034 | .118483 8.45 603.351 | 2. 9.19239 | 2.03682 | 4.38819 | 9.45407 | 118343 8.46 605.496 | 2.90861 | 9.19783 | 2.03762 | 4.38992 | 9.45780 | .118203 8.47 7.645 | 2.91033 | 9.20826 | 2.03842 | 4.39165 | 9.46152 | 118064 8.48 609.800 | 2.91204 | 9.20869 | 2.03923 | 4.39338 | 9.46525 | 117925 8.49 611.960 | 2.91376 | 9.21412 | 2.04003 | 4.39511 | 9.46897 | 117786 8.50 614.125 | 2.91548 | 9.21954 | 2.04083 | 4.39683 | 9.47268 | .117647 ROOTS, AND RECIPROCALS 3 Vn N10 n Vn P 90 90 G0 go 00 GO 00 GO OO ae monn Konno or ZSS2 SSSIS APSA @omca@m 90 90 G0 go Go SSR2aa & Nad URas PON COOMA OP ON Resse Sezne 9 Sp & Go be Oo se saaa Om Cobo {oc 00 GD GOOD GD ODED BODG~O MaMmGMD WMMMO MoDG~MM SSeS8 72.4201 13.2736 73.4449 73.6164 73.7881 73.9600 74,1321 74.9956 75.1689 75.3424 75.5161 75.6900 76.3876 76.5625 16.7376 77.6161 17.7924 77.9689 78.1456 718.3225 78.4996 18.6769 78.8544 79.0321 79.2100 79.3881 644.973 647.215 649.462 651.714 681.472 683.798 695.506 697.864 700.227 702.595 704.969 107.348 709.732 712,122 714.517 716.917 719,323 721.734 724,151 726.578 729,000 2.91719 2.94279 2.94449 2.94618 2.94788 2.94958 2.95127 2.95804 2.95973 2.97489 2.97658 2.98161 2.98329 2.98496 2.98664 2.98831 2.98998 2.99166 2.99333 2.99500 9.22497 9.23038 9,23580 9.24121 9.24662 9.25203 9.32738 9.33274 9.38616 9.39149 9.39681 9.40213 9.40744 9.41276 2.04163 2.04243 2.04323 2.04402 2.04482 2.04562 2.04641 2.04721 2.04801 2.04880 2.04959 2.05039 2.05118 2.05197 2.05276 2.05750 2.05828 2.06924 2.07002 2.07080 2.07157 2.07235 2.07313 2.07390 2.07468 2.07545 2.07622 2.07700 4.41571 4,41742 4.41913 4.42084 4.42254 4.42425 4.42595 4.42765 4.42935 4.43105 4.44627 4.44796 4.44964 4.45133 4.45301 4.45469 4,45637 4.47476 4.47642 4.47808 4,47974 4,48140 1 9.48752 9.49122 9.53175 9.53542 9.53908 9.54274 9.54640 9.55006 9.55371 9.55736 9.56101 9.56466 9.56830 9.57194 9.57557 9.57921 9.58284 9.58647 116279 116144 115473 115340 11111 / POWERS, ROOTS, AND RECIPROCALS 47 3 n2 n3 Wn | Vion| *n | MOn|Moon| = i=) 1 www eae -48306 | 9.65847 | .110988 -48472 | 9.66204 | .110865 9. 1 48803 | 9.66918 | .110620 "9025 | 741.218 | 3.00832 | 9.51315 | 2.08393 | 4.49968 | 9.67274 | .110497 82.0836 | 743.677 | 3.00998 | 9.51840 | 2.08470 | 4.49134 | 9.67630 | .110375 WwWWwWO Www SSS8 & dad el ire leer OCOARD OK ONK SO BEE Bi bo -~ . & 82.2649 | 746.143 | 3.01164 | 9.52365 | 2.08546 | 4.49299 | 9.67986 | .110254 J 9. - . 108342 é .03974 | 9.61249 | 2.09841 | 4.52089 | 9.73996 | .108225 791.453 | 3.04138 | 9.61769 | 2.09917 | 4.52252 | 9.74348 | .108108 85.7476 | 794.023 | 3.04302 | 9.62289 | 2.09992 | 4.52415 | 9.74699 | .107991 85.9329 | 796.598 | 3.04467 | 9.62808 | 2.10068 | 4.52578 | 9.75049 | .107875 86.1184 | 799.179 | 3.04631 | 9.63328 | 2.10144 | 4.52740 | 9.75400 | .107759 86.3041 | 801.765 | 3.04795 | 9.63846 | 2.10219 | 4.52903 | 9.75750 | .107643 86.4900 | 804.357 | 3.04959 | 9.64365 | 2.10294 | 4.53065 | 9.76100 | .10752T . . Beeb #8ee & GESSE SERRE & 86.6761 | 806.954 | 3.05123 | 9.64883 | 2.10370 | 4.53228 | 9.76450 107411 Ns 4.53390 J J A z . 4.54038 -106838 87.7969 | 822.657 | 3.06105 | 9.67988 | 2.10821 | 4.54199 | 9.78543 | .106724 843.909 | 3.07409 | 9.72111 | 2.11419 | 4.55488 | 9.81320 | :105820 89.4916 | 846.591 | 3.07571 | 9.72625 | 2.11494 | 4.55649 | 9.81666 | .105708 ~ =a ses 849.278 | 3.07734 | 9.73139 | 2.11568 | 4.55809 | 9.82012 | .105597 ’ 9.73653 | 2. A 16 90.0601 | 854.670 | 3.08058 °. 74166 | 2.11717 | 4.56130 | 9.82703 | .105374 90.2500 | 857.375 | 3.08221 | 9.74679 | 2.11791 | 4.56290 | 9.83048 | .105263 48 POWERS, ROOTS, AND RECIPROCALS vion| %m | tion|*ioon| + 9.75192 | 2.11865 | 4.56450 | 9.83392 | 105158 3 4 3 a 22 8 S 3 S & Ss Ra 3 e 4.56930 91.2025 | 870.984 | 3.09031 | 9.77241 | 2.12162 | 4.57089 | 9.84769 | .104712 91.3936 | 873.723 | 3.09192 | 9.77753 | 2.12236 | 4.57249 | 9.85113 | .104603 91.5849 | 876.467 | 3.09354 | 9.78264 | 2.12310 | 4.57408 | 9.85456 | .104493 91.7764 | 879.218 | 3.09516 | 9.78775 | 2.12384 | 4.57568 | 9.85799 | .104384 91.9681 | 881.974 | 3.09677 | 9.79285 | 2.12458 | 4.57727 | 9.86142 | .104275 92.1600 | 884.736 | 3.09839 | 9.79796 | 2.12532 | 4.57886 | 9.86485 | .104167 F 4 -10000 | 9. 2.12605 | 4.58045 | 9.86827 | .104058 92.5444 | 890.277 | 3.10161 | 9.80816 | 2.12679 | 4.58203 | 9.87169 | .103950 . ts 03842 92.9296 | 895.841 | 3.10483 | 9.81835 | 2.12826 | 4.58521 | 9.87853 | .103734 93.1225 | 898.632 | 3.10644 | 9.82344 | 2.12900 | 4.58679 | 9.88195 | .103627 WOOHOO OOWOOO Owoowoo Ba2z Reese sesse are s g & é wo © s s 93.8961 | 909.853 | 3.11288 | 9.84378 | 2.13194 | 4.59312 | 9.89558 | .103199 ‘ 2.13267 | 4.59470 | 9.89898 | .103093 ” = i) © -~ co} I as fr) = ao bd = © Syste tate Salata tay OOOOO COoOwww CHAR Tmwwe : 9. . < 94,8676 | 924.010 | 3.12090 | 9.86914 | 2.13560 | 4.60101 | 9.91257 | .102669 95.0625 | 926.859 | 3.12250 | 9.87421 | 2.13633 | 4.60258 | 9.91596 | .102564 95.2576 | 929.714 | 3.12410 | 9.87927 | 2.13706 | 4.60416 Hp ben 102459 A 9.92274 95.8441 | 938.314 | 3.12890 | 9.89444 | 2.13925 | 4.60887 | 9.92950 | .102145 96.0400 | 941.192 | 3.13050 | 9.89949 | 2.13997 | 4.61044 | 9.93288 | [102041 96.2361 | 944.076 | 3.13209 | 9.90454 | 2.14070 | 4.61200 | 9.93626 | .101937 96.4324 | 946.966 | 3.13369 | 9.90959 | 2.14143 | 4.61357 | 9.93964 | .101833 96.6289 | 949.862 | 3.13528 | 9.91464 | 2.14216 | 4.61513 | 9.94301 | .101729 96.8256 | 952.764 | 3.13688 | 9.91968 | 2.14288 | 4.61670 | 9.94638 | .101626 97.0225 | 955.672 | 3.13847 | 9.92472 | 2.14361 | 4.61826 | 9.94975 | .101523 97.2196 | 958.585 | 3.14006 | 9.92975 | 2.14483 | 4.61983 | 9.95311 | .101420 97.4169 | 961.505 | 3.14166 | 9.93479 | 2.14506 | 4.62139 | 9.95648 | .101317 ‘ 964.430 | 3.14325 | 9.93982 | 2.14578 | 4.62295 | 9.95984 | .101215 97.8121 | 967.362 | 3.14484 | 9.94485 | 2.14651 | 4.62451 | 9.96320 | .101112 98.0100 | 970.299 | 3.14643 | 9.94987 | 2.14723 | 4.62607 | 9.96655 | .101010 98.2081 | 973.242 | 3.14802 | 9.95490 | 2.14795 | 4.62762 | 9.96991 | .100908 98.4064 | 976.191 | 3.14960 | 9.95992 | 2.14867 | 4.62918 | 9.97826 | .100807 98.6049 | 979.147 | 3.15119 | 9.96494 | 2.14940 | 4.63073 | 9.97661 | .100705 98.8036 | 982.108 | 3.15278 | 9.96995 | 2.15012 | 4.63229 | 9.97996 | .1 9.97497 | 2.15084 | 4.63384 | 9.98331 | .100503 99.2016 | 988.048 | 3.15595 | 9.97998 | 2.15156 | 4.63539 | 9.98665 | .100402 4009 9.98499 | 2.15228 | 4.63694 | 9.98999 | .100301 © CLwowLo SSR Saxn: 99 2 oe Sezee z = © Peosos es « S88 &esse S33 8 s nt o Cc & o 1 o oe — oO S a J ° J 1002 99.8001 | 997.003 | 3.16070 | 9.99500 | 2.15372 | 4.64004 | 9.99667 | .100100 3.16228 | 10.0000 | 2.15443 | 4.64159 | 10.0000 | .100000 Seoews woos ss S s s 3 MATHEMATICS 49 six significant figures (adding ciphers, if necessary, to make six figures) and find between what two numbers in the column headed B the significant figures of the given number fall; then proceed exactly as previously described to deter- mine the fourth and fifth figures. EXxAMPLE.—(a) The reciprocal of 379.426 = ? (b) — 7004853 4692 > =? SoLuTion.—(a) .379426 falls between 878788 = 5, nial 380228-= 57. The first difference is 380228—378788 = 1440; the second difference is 380228 — 379426 =802; 802 + 1440 = .557, or .56. Hence, the first five significant figures are 26356, and the tect of 379.426 is .0026356, to five significant figures. (b) .469200 falls between .469484 = si and .467290 = sir The first difference is 2194; the second difference i . <3 C 1 a is 284; 284+ 2194=.129+,or.13. Hence, 9004602 ~ 2131.3, correct to five significant figures. MENSURATION In the following formulas, unless otherwise stated, the letters have the meanings here given: D=larger diameter; d=smaller diameter; R=radius corresponding to D; r=radius corresponding to d; p=perimeter of circumference; C=area of convex surface=area of flat surface that can be rolled into the shape shown; S=area of entire surface=C-+area of the end or ends; A=area of plane figure; m7=3.1416, nearly=ratio of any circumference to its diameter; V =volume of solid. The other letters used will be found on.the cuts. 50 MATHEMATICS CIRCLE p=nd=3.1416d p=2nr =6.2832r p=2VrA =3.5449 VA A 4A ac aaae ay QUES aeee) Te Siete oe d=2 A =1.1284VA Satie De "=n 6.9832 1°92? r= (4 =.5642Va - A =72 = .7854d2 A=nr2=3.1416r2 _?r_pd A= 2a. 4 TRIANGLES D=B+C E+B+C=180° B=D-C E'+B+C=180° "L, EISE B'=B The above letters refer to angles. sa a right triangle, c being the’ hypotenuse, = ae a= Nc2 b= V2 C= an acute angle of an nie triangle. = Va?+b?—Qbe + “pa Na2— ¢2 c=length of side opposite an obtuse angle of an oblique-angled _triangle. c= Va2+b2+ 2Qhe h= Va2— For a triangle inscribed in a semicircle; i. e., any right triangle, MATHEMATICS 51 @26 4 dik ,—-eP_@ Cte a:b+e=e:a=h:c 6 th thie For any triangle, bh A=y = tbh b a2+b2—¢2\2 saree ee RECTANGLE AND PARALLELOGRAM Ao x TRAPEZOID / A=th(a+b) . TRAPEZIUM Divide into two triangles and a trapezoid. A=bh'+4a(h' +h) +4ch; or, A=34[bh’+ch+a(h’+h)] Or, divide into two triangles by draw- ing a diagonal. Consider the diagonal as the base of both triangles, call its length /; call the altitudes of the triangles 4, and 2; then A=3(hi +h) ELLIPSE pean Pte (D—d)? AWA 2 8.8 MMM A = {Dd=.7854Dd SECTOR a, A=3lr rrE A= 360 7 .008727r2E fi 1=length of arc *The perimeter of an ellipse cannot be exactly determined without a very elaborate calculation, and this formula is merely an approxima- tion giving fairly close results. - MATHEMATICS SEGMENT A =4lr—c(r—h)] = sag at) RING wT A =7(D?—d?) CHORD c=length of chord c2 + 4h2 ¢2 c=22hr—h2 p= S28 3 , approximately HELIX Tc construct a helix: , 1=length of helix; fC n=number of turns; Pe e t= pitch. a pR ES 2 to t= ee 32d. l=nWNnr2d2+2 Oe seeks rick +2 CYLINDER C=ndh S=2rrh+2rr2 =ndh +50 V=arh= adh p*h V= "7, = .0796p% MATHEMATICS 53 FRUSTRUM OF CYLINDER h=4 sum of greatest and least heights C=ph=tdh S=ndh+ 7 +area of elliptical top V=Ah=30h CONE Wi C=3rdl=nrl h S=nrl + ar2= ar V2 + h2+ wr? i md? h _.7854d*h _ p%h — 9 amie bar Seine Goes 6 FRUSTUM OF CONE C=4(P+p)=51(D +d) S=5(D +d) +43(D?+d?)] V=5(D2+Dd +a) Xth = .2618h(D?-+ Dd +?) SPHERE S = 1d? = 4nr? = 12.5664r? V =}a3 = grr? = .5236d3 = 4.18887 CIRCULAR RING D=mean diameter; R=mean radius. S = 4n2Rr =9.8696Dd V =2n2Rr2 = 2.4674Dd?2 WEDGE V =twh(a+b+c) - Ao PRISMOID A prismoid is a solid having two parallel plane ends, the edges of which are connected by plane triangular or quadri- lateral surfaces. 54 MATHEMATICS A=area of one end; a=area of other end; m=area of section midway between ends; l=perpendicular distance between ends. V=4l(A+at+4m) The area m is not in general a mean between the areas of the two ends, but its sides are means between the correspond- ing lengths of the ends. Approximately, V= Ate REGULAR PYRAMID | P=perimeter of base; A=area of base. To obtain area of base, divide it into triangles, and find their sum. The formula for V applies to any pyramid whose base is A and altitude h. FRUSTUM OF REGULAR PYRAMID a =area of upper base; A=area of lower base; p=perimeter of upper base; P=perimeter of lower base. C=4l(P+>) S=4l(P+p)+A+t+a V=3n(A+a+ VAa) The formula for V applies to the frustum of any pyramid. LENGTH OF SPIRAL I= (2<7) n=number of coils; ="n\—> 1 =length of spiral; 1 =7(R2—1?) Bar ' MATHEMATICS 55 PRISM OR PARALLELOPIPED C=ph S=ph+2A ey a> 0 Ge eet amy, qf For prisms with regular polygon as bases, p=length of one side X number of sides. To obtain area of base, if it is a polygon, divide it into tri- angles, and find sum of partial areas. FRUSTUM OF PRISM If a section perpendicular to the edges is a tri- angle, square, parallelogram, or regular polygon, yasum of lengths of edges ~ number of edges REGULAR POLYGONS Divide the polygon into equal triangles and find the sum of the partial areas. Otherwise, square the length of one side and multiply by proper number from the following table: Kit HM X area of right section. Name No. Sides Multiplier Triangle... 2. cc03°8 .433 — DOUATG. na er ve 4 1.000 (/ \ Pentagon. ......5-..°8 1.720 Hexagon......... 6 2.598 \ y), Heptagon. «i: ¢,.::6 7 3.634 ——— Octagon... 14065. 4.828 NOnagOns ssc. 9 6.182 Decagon......... 10 7.694 IRREGULAR AREAS Divide the area into trapezoids, triangles, parts of circles, etc., and find the sum of the partial areas. If the figure is very irregular, the approximate area may be found as follows: Divide the figure into trapezoids by equidistant parallel lines b, c, d, etc. The lengths of these lines being measured, then, calling a the first and m the last length, and . y the width of strips, area=(F"+b-+c-+etc. +m) 56 LOADS IN STRUCTURES LOADS IN STRUCTURES The loads that a structure has to carry may be divided into five classes namely, the dead load, the live load, the accidental load, the snow load, and the wind load. The dead load is the weight of the materials of which the structure is composed, as the weight of the beams, columns, walls, floors, and the like. The live load is the weight of the various articles in the building that are not part of the structure itself, such as furniture, material stored, if the building is a storehouse, the occupants of the building, light machinery, etc. The accidental load is one whose application is doubtful or whose magnitude is great and its effect local. As exam- ples of such loads may be classed the load that would be generated if the ropes of an elevator broke and the safety device was suddenly brought into action, and the load that ' would be created on a stairway in a mill if there was a panic among the employes, as during a fire. As an accidental load may also be classed such loads as would be caused by an especially heavy office safe or piece of machinery. Many engineers no longer consider an accidental load. The load that would come from an extra-large crowd, as on a stair- way in a fire, they class as part of the liveload. Such loads as would occur from a large safe, they usually class as part of the dead load, because the safe would be too heavy to be moved. Therefore, only that part of the structure in the vicinity of the safe need be strengthened. The snow and wind loads are, as the names imply, loads that are caused respectively by snow and wind. DEAD LOADS WEIGHT OF ROOF TRUSSES The dead load must be calculated for each member of a structure by means of tables that give the weights of build- ing materials, such as those on pages 59-61. However, it LOADS IN STRUCTURES 57 is often desirable to know the approximate weight of roof trusses before the actual size of the members has been cal- culated. In such cases, the following empirical formula may be used: ; W=aDL ( 1+ a) in which W is the approximate weight of the truss, in pounds; a, a constant—for wood .5, for steel .75; D, the distance, in feet, from center to center of trusses; and L, the span of the truss, in feet. It is sometimes desirable to know the approximate weight of roof truss per square foot of roof surface. It will be noted that this is not the same thing as per square foot of hori- zontal surface, since the roof slants. If x is the angle between the rafter and the chord, L the span of the truss in feet, and w the approximate weight of the truss per square foot of roof surface, then y= eo +L) cos x 10 in which a is .5 for wooden trusses and .75 for steel trusses. ExaMPpLeE.—Determine the weight, per square foot, that must be added to the weight of a roof covering to provide for the weight of the principals, the steel trusses in this case having a span of 72 ft. and a rise of 18 ft. SoLuTION.—The angle between the rafter and the chord may be found from the formula tan x= ——=H8=.5, corre- _ sponding to an angle x of 26° 34’. Substituting the values of a, L, and cos x in the preceding formula, .75 (10+72) cos 26° 34’ .75xX82xX.8944 w= 10 = 0 = 5.5 lb. The following table has been calculated from the preceding formula. This table gives the weight that must be added to a square foot of roof covering to provide for the weight of the principals, or trusses. The slope of the roof is in each case given in terms of its “‘pitch,’’ which is here taken as the ratio of rise to span. Thus, a $ pitch is such a slope that the rise of the truss is one-third the span of the truss. LOADS IN STRUCTURES 58 OF'9 b0'9 co'G | SZZ hb | OSO'F | FFL | 98TO'S| O08 $0°9 02'S 0gs | 809% | Ges'e | 9Ec's | 60GS'z| GZ 69'S LE°¢ 66% | Shor | OON'S | SzE'E | E897! O02 veg €0°9 89> | LL6E | SLES | OTE | SSIgs) gg 86'P OL'P Lev | GIZ’s | OST'S | 216s | S4tES| O09 oOF 98°F 90°F | LHP'S | G26S | HOLS | TOST'S| g¢ ee any oe oe 2 COST LF c0'P PLE | G8I'ES | 00LS | 96'S | FZI0'S| OG 16'S 69'S eve | L166 | SLPS | 88S | LFPST| GPF 9c°¢ cee GUS | 699% | OSS'S | O80 | OLZ9T| OF 06'S 60'S 18% | 988% | S20 | SLZ8'T | S609 | gE S8'% 89'S OS'S | Ié1@ | OOST | F99T | 9TFPET| OF | LQ°F Z0'F bLZS | S8lE | O0OLS | 96F'S | FZIO'SZ! OS |) 80°F 08's ros | GOO'S | OSG'S | LEES | 9006T| Gz 62'S | 8s 68§ | 868% | OOPS | SIZS | S88ZT| OL 9¢o°E ges oS | gos | OSSS | O8OS | OLLO'T ¢9 oes el'é 16% | GZS | COOLS | IFET | Zg9C'T 09 80'S 16% OLS | 862° | OS6T | GOST | FESFT| g¢ ee a oer ae poom C8 89'S OS'S | IZtS | OOST | FOOT | 9TFET! OS 19% 9F'% 62'S | SFET | OSOT | SSS | 86201) Ft LEG bo 80° | 89ZT | OOST | Z8ET | OSITT| OF ELS 10% LST | 169°C | OSET | SST | Z900'T cE 06'T 6LT 99'T | FIPT | OOST | GOTT | HF68 0€ |. Wud $ UU | [MU F YU F MW F Yd F UW T SSHIL JO JozoVIVyy) 7 79297 uedg er aoRjng jJooy jo yooy orenbg sed spunog ERTS yam SassnuL fOOU AO LHOIGM ALVWIXOUddV LOADS IN STRUCTURES WEIGHT OF BUILDING MATERIALS PER CUBIC FOOT 59 Name of Material Average Weight Pounds Pounds per per Cubic Inch} Cubic Foot Asphalt-pavement eeope an. Acree 130 Bluestone. . ae 160 Brick, best pressed. . 150 Brick, common and hard. r25 Brick, paving. Ae 150 Brick, soft, inferior. . 100 Brickwork, in lime mortar (average) 120 Brickwork, i in cement mortar (aver- 13h Brickwork, pressed brick, thin joints 140 Cement, Portland, packed. . poe tay, A 100 to 120 Cement, natural, packed. . 75 to 95 Concrete, LE, ee as 105 Concrete, eden Bee Sas 140 Concrete, slag. . 135 Concrete, stone. . ee 140 Concrete, reinforced (average). a 150 ‘Earth, dry and loose.. 72 to 80 Earth, dry and moderately rammed 90 to 100 Be ipetriok: one Seed 2c Re 150 Granite: 2655. 165 to 170 Gravel.. eS LZ tor1 25 Iron, cast. . Save Sis: > .260 450 Iron, wrought. . 207 480 Limestone. . 146 to 168 Marble. . -168 Masonry, squared granite. or lime- stone. 165 Masonry, granite or limestone rubble 150 Masonry, granite or limestone dry LUDDIey, esis oy . :- Nfs 138 Masonry, sandstone. . 145 Mineral wool. . j 12 Mortar, hardened. . 90 to 100 Prick, ground, loose, ‘or small ee . 53 Ouie eee ground, thoroughly shaken. sekere 75 Sand, pure quartz, dry.. 90 to 106 60 LOADS IN STRUCTURES WEIGHT OF BUILDING MATERIALS PER CUBIC FOOT (Continued) Average Weight Name of Material Pounds Pounds er Per Cubic Inch} Cubic Foot Sandstone, chew hed 139 to 151 Slate.. Mins 160 to 180 Snow, fresh fallen. 5 to 12 Steel, structural. . .283 489.6 Terra cotta. 110 2 os Saba masonry work. . 112 Tile. . Suita Nite 110 to 120 WEIGHT OF BUILDING MATERIALS PER SQUARE FOOT Average Weight Name of Material Pounds per Square Foot SINGE6 aca 2.91 NoraSisiwi 2.36 a ce ee ae : : : Oy Secas ae 54 Corrugated (24-in.) galvanized iron Nae Bat >. 127 No: 26 <<. .99 NO 275.6 .93 NG 28.6356 .86 Corrugated galvanized iron, No. 20, severaae Rona gs of side lap, unboarded. 24 per roofing, 16-oz., standing seam. 14 Reh and pitch, without bape: ee 3 tell 4 in. thick. . 12 Hemlock sheathing, ‘1 in. thick. . 2 Lead, about 4 in. thick.. 6 to8 Lath-and- plaster ceiling (ordinary) .. Seats 6 to 8 Mackite, 1 in. thick, with plaster. . Ais PSs 10 LOADS IN STRUCTURES 61 WEIGHT OF BUILDING MATERIALS PER SQUARE FOOT (Continued) Average Weight c Pounds Name of Material Per uare oot Neponset roofing felt, two layers. . ete faye 4 Spruce sheathing, 1 in. thick.. Sphate.e te eG 2 ¢ in. eid ey 1.81 ¥e,in. thick. . bree 2.71 ?} SRG oss oe 3.62 Slate, single thickness{ $ in. thick...... 5.43 in. thick 7.25 $ in. thick. . 9.06 # in. thick.. : ol «10:87 hingles, common, 6 in. X 18 in., 5 in. ‘to weather. 2 Sruene of glass, ts to }in., including f frame....| 4to10 Slag roof, four-ply.. Ate 4 Steel roofing, standing seam. 1 Tiles, Spanish, 144 in. X 103 i in., 7 hj in. to ‘weather 84 Tiles, plain, 104 in. x6} in. xs in., ee in. to weather. ; 18 White-pine “sheathing, 1 in. thick. . 2 Yellow-pine sheathing, 1 in. thick. . 3 Gravel roof and four-ply felt.. 54 Gravel roof and five-ply felt. . : 6 peers, three-ply ready (asphalt, rubberoid, reat 3 to Bodie ‘wooden, ‘with 12- to 16- ft. span. Ay 2 Chestnut or maple sheathing, 1 in. thick........ 4 Ash, hickory, or oak anest eet 1 in. thick.. 5 Sheet iron, ae in. apaaen Seas 3 Thatch.. ; dcusvera eats + kik 6.5 LIVE LOADS If the live load consists of heavy material, such as mer- chandise in a warehouse, and if the amount of this material and its location are known, the live load is usually calculated from the table of weights of materials given on pages 64-81. If, however, the structure is to be used as a dwelling, a hotel, 62 LOADS IN STRUCTURES or a warehouse for general merchandise the character of which is yet unknown, it is customary to assume the live load to be a certain number of pounds per square foot of floor space and to design the structure for this load. The following table gives the loads per square foot of aoe space often employed: LIVE LOADS PER SQUARE FOOT IN BUILDINGS Character of Building © Pounds Dwellings. . ¢ 8b bea ASG ER otis. che 70 Offices. . Loe 7 Hotels and apartment houses... ye 7 Theaters. . Sashes 120 Churches. . eek 120 Ballrooms and drill ‘halls. rae 120: Factories...... PRR from 150 up Warehouses...........0sscsecceeee from 150 to 250 up The load of 70 lb. will probably never be realized in dwellings; but inasmuch as acity house may at times be used for some purpose other than that of a dwelling, it is: not generally advisable to use a lighter load. In a country ‘house, a hotel, or a building of like character, a live load of 40 lb. per sq. ft. of floor surface is ample for all rooms not used for public assembly. For assembly rooms, a live load of 100 1b. will be sufficient. If the desks and chairs are fixed, as in a schoolroom or a church, a live load of more than from 40 to 50 lb. will never be attained. Retail stores should have floors proportioned for a live load of 100 lb. and upwards. Wholesale stores, machine shops, etc. should have the floors proportioned for a live,load of not less than 150 lb. per sq.ft. The floors of printing houses and binderies should be proportioned for a live load of at least 250 lb. per sq. ft. Special provision should be made in such floor systems tor heavy presses, trimmers, and cutters, and the beams should be proportioned for twice the static load likely to occur from such machines. The static load in factories seldom exceeds from 40 to 50 Ib. per sq. ft. of floor LOADS IN STRUCTURES 63 surface; therefore, in the majority of cases, a live load of 100 Ib. is ample. The conservative rule is, in general, to assume loads not less than those just given, and to propor- tion the beams so as to avoid excessive deflection, Stiffness is as important a factor as strength. ALLOWABLE LIVE LOADS ON FLOORS IN DIFFERENT CITIES Pounds per Square Foot Character of Building New : Phila- Vani Chicago delphia Boston Gerretse for gs as- semb Sulidings “for ‘ordinary stores, light manufac- turing, and light storage| 120 100 120 Dwellings, apartment houses, tenement houses, and lodging houses. . 60 40 70 50 Office buildings, first floor} 150 100 100 100 Office eae above 90 100 120 150 first floo Public buildings. ‘except schools. . 150 Roofs, pitch less than 20°. . 50 25 30 25* Roofs, pitch more than 20° 30 25 30 25* Schools or places of in- struction. 75 80 Stables or carriage ‘houses less than 500 sq. ft. in Grea .. 75 40 Stables or carriage “houses more than 500 sq. ft. in area . 75 100 Stores for heavy ‘materials, Bercnoes, and _fac- sake tdetec a) DO 150 250 Sidewalks. Shea otal COU. NOTE.~In the table the values given for roofs are for snow and wind loads. Inthe last column, the roof loads marked with the aste- risk (*) do not include the wind load; the building laws of Boston require that a proper allowance for the wind load exerting a presfure of 30 lb. persq. ft. of vertical surface shall be made in designing roofs- 64 LOADS IN STRUCTURES In proportioning the live loads on floors, the engineer cannot always exercise his own judgment, for if the building is to be erected in a large city, the live load must comply with the building laws. As such laws are not uniform in the several cities the table on page 63 is given to show the stip- ulated live loads in the four largest cities in the United States. . WEIGHTS OF MERCHANDISE, IN BULK, FOR CALCU- LATING LIVE LOADS Measure- Bi dere aog ments eights ; g . 9 ® Name of Material Ee. 23 a3 ahsisze oj Px} 2 pS | 8 Oe, 5 ee 5 oe Bom ay Oo ay A Cotton, etc.: Bale of commercial cotton | 8.10/44.20| 515 64 | 12 Bale of.compressed cotton | 4.10/21.60) 5 134 | 25 Bale of American Cotton Co.. -| 4.00/11.00|} 263 66 | 24 Bale of Planters Compress Co. . .| 2.30] 7.20) 254 | 110 | 35 Bale of jute... Seite ai gre Gia alata 2.40} 9.90} 300 | 125 | 30 Bale of jute lashings...... 2.60/10.50| 450 | 172 | 43 Bale of manila...........| 3.20/10.90} 280 88 | 26 Bale of hemp............| 8.70|34.70} 700 81 | 20 Bale OF Sisal Sie, Sais ss 5.30/17.00| 400 75 | 24 Cotton Goods: Bale of unbleached jeans. .| 4.00/12.50|} 300 75 | 24 Piece of duck. . -| 1.10) 2.30) 75 33 Bale of brown sheetings. .| 3.60)10.10) 235 65 | 23 Case of bleached sora wae 4.80)11.40) 330 69 | 29 Case of quilts... 2 . | 7.20)19.00} 295 41 16 Bale of print cloths....... 4, 9.30) 175 44] 19 Case of prints............ 4.50/13 420 93 | 31 Bale of ebitignte 3.30) 8.80) 325 99 | 37 Burlaps.... 130 30 cle bagging. . 1.40} 5.30) 100 71} 19 Wheat in bags. . 4.20) 4.20) 165 39 ; 39 Flour in barrels on side. 4.10) 5.40) 218 53 | 40 : | LOADS IN STRUCTURES WEIGHTS OF MERCHANDISE, IN BULK, FOR CAL- CULATING LIVE LOADS—(Continued) 65 Measure- Approximate ments eights N f Material g, |¥ go (8 ateri “ad tu “3 ° 3 Bam | BO") SE |B) Om aS a |s Grain—Continued Flour in barrels on end. 3.10) 7:10) 218; 70] 31 COPED AGS sa. oc reste hoc .60} 3.60; 112} 31] 31 Corn meal in barrels.....| 3.70} 5.90} 218; 59 | 37 Oats inibags: «. .biccuaans 3.30} 3.60} 96; 29 | 27 Bale of clover hay........ 5.00/20.00} 284; 57 | 14 Bale of clover Beye snlenal compressed . 12751 -6.25|) 225). Flo} 24 Bale Gt Straw aces oceoen es 1276) 3225) 100) “52°19 Bale of tow . Bi lousicte Selo ES TOL Oncol LON “SOulnace Bale of excelsior ero cel Lt Olcoseol LOO -S7-41) ao Rags in Bales: gs on Be linen. 8.50/39.50} 910] 107 | 23 White cotton.. Suse Oe 140700! “7151 “78-) “18 ISTOWit COLLON sic soo oes: 7.60/30.00} 442; 58 15 Paper ee: ...-| 7.50;384.00| 507; 68 15 ee A ee 16.00\65.00} 450; 28 Z oolen Cee 7.50/30.00} 600} 80 | 20 He ore 2.80/11.00} 400; 143 | 36 Wool: Bale, East India. . 3.00)/12.00} 340] 113 | 28 Bale, Australian. . ..-| 5.80/22.00] 385; 66] 15 Bale, South American. ..-| 7.00/34.00/1,000;} 143 | 29 Bale, Oregon. ...| 6.90133.00] 482; 70 | 15 Bale, Cali ifornia. 7.50133.00} 550/ 73 17 Bag of woo | ie 5.00/30.00} 200! 40 7 Sack of scoured wool. . 5 Woolen Goods: Case of flannels. . se aac] 1.00]/12..70| - 220) 40°) 17 Case of flannels, heavy .--| 7.10115.20} 330; 46/1 22 Case of dress goods....... 5.50/22.00) 460; 84] 21 Case of cassimeres........ 10.50/28.00} 550] 52 | 20 of underwear........ .30/21.00} 350} 48 | 17 Case of blankets. . .. .110.30/385.001 450) 44); 13 Case of horse blankets... . 4.00)14.00} 250 18 66 LOADS IN STRUCTURES © Were OF MERCHANDISE, IN BULK, FOR CAL- CULATING LIVE LOADS—(C ontinued) Measure- ND Enea ments eights g, i2 g Name of Material Bo jf. .| 9 |Be|2. tte) wo} yeoorey) ZG eee ee we eee Sah epaderell ‘joyooly 82 ewe eo eo oe Seep tistey uwtory yeooreyg 69T “* “ee we ** MOTTOA ‘leyseqely $e trees esceeee se eno WOsy TeOOlEYy) IZI Trrctsterss ress *saqnys ‘ayseqery Z9 re eusedureyy GIL ee ‘oLmnydms ‘PPy 9CI oo Oe ewe ce ee te Bete eeecrene aed) 16 ‘‘oroydsoyd * (PPV SIOSGG [09884 4 Be ee 8 + Sg ‘ZeIs ‘quaures) 9L ‘ “OLtqia ‘PPV 00T 9108 |""°*'’*'** °° ot pexoed ‘Beys ‘yuouted PO ee do as “(u0TyoospAy) oryeLmur ‘PPV 6901 Gp |" °° °° ******‘asooy ‘TemnzeU ‘yuaTIE, 6 “opony ‘PHY C6 01 CL ***pexyoed ‘Temyzeu ‘yueuled 99 ‘ooo ‘phy spunog spunodg yoo s1qng yoo s1qnag aor 5 Pe nl [elsozeyy Jo owen jeer Mage TeHoyeW Jo oureNy aseloAy aseloAy STVIMALVA SQOANVTIAOSIN AO SLHOIDM AOVAAAV 69 LOADS IN STRUCTURES eeoeo ee ees Sr Nain teehee ae sy LL CPO LO! LS OOr sone ess ease 2) 2 PSRs SUAS Trrrrtescceseceses Burgi ‘sadeg ‘Buiddvim ‘rodeg ** 1 *3J00q ‘pesopuayeosedns Jodeg eee . ee eeeee *preoqMelys ‘rodeg eoeoe ee eeee ov eeeee "smou ‘sodeq “eplueul ‘todeg a ee ed PrIvOg-JOY} eI] ‘rode eee re eeee **300q, peleapusyeo ‘rodeg *(971ZeUWIaY) UOIT 4jos ‘210 " * @}HeuseUT) uost prey ‘aI0 sislerereleWieie ste) sie si4igiest e040 oyeu ‘HO eoeere reer eer ev eeeese ourjuadin3 ‘TO tneis sis esncieserw aa $610 bi 6:0 “QATTO ‘10 "***peesuyy ‘TO cece “ToqN eevee eon sce ee er re ee eeeese -eyyyden Freee rere ee eter er cece es -oUOASTTTAL (bie: SIN A aU N ioe etelacuienele gedeteie Gis 4/6 014 BOT eeeeveea oe ee * O1[Se yl **pouroyeo ‘ayisouse yy cooere ee ee eevee ‘ayeuogieo ‘vIsousey[ Trees ceessssapid ur ‘afos ‘s0y}8eT 40D 6:8. 6 6-8 8 OO. 8:e 816 *AIOAT eee ve eveeorsrerveeeeeeeeene *sSB[SUIST eeeevovecs Te ce eccesssssaqqns Btpuy eee vere eoeee se ee ceeeers ‘90T ee @ owe Sere Eee sisie)2 2° i*/° sO PUO TA UsO LH eeere eo eo ne ee ee oe eeeeore ee oe oe oe oe oe ee oe ee esr eeee ee ee ew ores OOT °F 06 66 97 28 08 93 ZL rts wom a te ty eee Ae Se et a ho ik * ‘ato eq BUlOH ‘ummsd Ax) eee ee eee **eyoied %44N+) 0 Ge O00 ea. 6.07 Cie) Ble 01 @.6 prjos ‘rapmoduns) 656 5), 6:8) 50 10.6 0: 4 08'S: 6 “uaxeys ‘Iopmodunr) * *@SOO] ‘sepmoduns) PRR ee oe oe “* “yeyeur uns) : tees eeeeeeeseorqere UNS a6 rele. Greveisco'e) 9.6) 0i8iie9'='4ie 9u0}spulss) O36" 60 S708 668, mt 9SOO0] ut ‘sstour) eee vere ee ee eeeee uOUTUIOS ‘sstaur) eee . eee ee quit ‘sseyy * ee uouwlul09 ‘SSB]L) ce cece cece ce veces SCE Nt i eee CW ek ak . ‘+ redsppy SiS) 6 646 6G 16, O'S Rise’ do 86 oe Ss ‘1943 Soe: CIEE goa . "*phnur asuap oF!] ‘qyed - pr Burmoy | ‘qos ayy ‘Yweq "AjozeI9 pout powues “UIBO] uOUIWIOD ‘qyeg *uayeVys ‘UIBO] UOUIUWIOD ‘yyseg eri: asoo] ‘UIBOT UOUTUIOD ‘YWIeW wie isieiecsless\alvie(ainis's!siefs uaul JO PMOID eae "SUfOHS Uy ‘ured u03407¢ cece ccoee *“umpunsoy . ei oan rad. sites Undo 0:6, 6 OS 60710106: 0, Bed 0. 5's. asOo] ‘ayog 70 LOADS.IN STRUCTURES Z9 es ee @e “SOUL M, 90L O} 06 D6 BaD ~ pees 18 "* guoqeyey M. idk: Sac aie “ peLtp- T1984 ‘eppuy 250M ‘4T8S 89 o> * +p UL A CP see eee *OSIBOO “4TeS 0g 0} 0Z *qeod Io ‘ ty I&t see ee . * ** “ee eewe *Ioyodyfes OLT se eeees ely, PZL * *9U04SU944OR e9 nek ess eT oP -- erueyy ‘odor gg "xo JO > outed ‘MOTB IL, 69 . “UTSO ISt yoorq ‘oye y CoOL “ond | ‘wourUt0S ‘2y7en. CSI ‘Inydms Lg **eu04s soruIng OOT Be lst bie Se ats S-s' se De le ae Ole, resnsg OLT SA Rae *AtAYdIOg 6S **to0euLIEdS OFT RES eS ee *osequini[d LEP sourz Io ‘raqjeds 08 see eee meee 4880 ‘sq3eq jo J04SeId OLT *-guo0ysde0g aL ee ee "youd ZI Cov es ce eresssscvesene uwOUIWIOO *I0G OIL * *snroydsoyd PLI SESE RA ren rp ae **-o9RIG a eo umndo130g ZOL ff ee. . eenee *saTeys og O} 0z eer ee ew ee eee posseidur0o ‘AIp ‘qeog spunog spunog yoo o1qnag 4yOO,F oIqn eeiea [evozey jo owen : oS aioe . [eHoyeWy JO owen eseIIAY aBvIOAY (panu1iu0)—STVIMALVW SNOANVTTAOSIN AO SLHOIAM AOVUAAAV LOADS IN STRUCTURES ge “surazs UFTA sodvir) OF ; *SpOIIBY) re ; ‘ saLIteqasoor) OF é “yopout un ‘odnopeiue?) CF \(paasuly) peasxe|y SF ; "pees AreuB) gg “UO4yNUT JO IBY OF “oseqqey 6g “S80y Jo ey 6S Pe Regd tie 8g goed 20 78a 68 Sine * “qeoq Mong 89 “S337 og oe ae = paos UIOD-WOO1 Eg Ze ‘*sque1n) Il sees "sseiZ aulolg 62 ““sq1sFoquvs) 91 jana _Uelg CZ Soren or Gaicre * * paast0}}0/) Il so “paas sseis-on|g ge ay eey areas “ peajoqun ‘Teaut WIOD rE “‘sottsoqenig Lg Ct ey ee Ce De ge Oa *pestoq ‘jeour AOD Se * “SoLlieq soe CP ea *porpeys ‘u10d 0s - pos poomsvssog gg aan toa ‘paysnyun ‘qoo a4} UO UO) bP . "S}00G 9¢ "rte tts" paysny ‘qoo ey} wo W105 19 : : * *XBMSoog 8P ** paas JOAO[) 1g -“poqlous ‘s0nme5 ‘subg $9 a ‘Iaplg SP “our ‘suvog es Srey aioe tcrets ey. ge wh “Age ep eeeeeeeeee seganuasayy Ze * "pees addy OF see ee cece eeeeees ssatraUy 0Z “poup ‘sojddy og e aceiecaie arent * sao) ge ‘sojddy spunog spunodg yoo, a1qng [elioyep Jo oweN yoo s1qng [eHoyeR JO owen sod 7310 \\ Jad 74310 M SLOnNdOdd WUVA JO SLHSIGM AOVAAAV LOADS IN STRUCTURES 72 ee qoo 9y4 uo ‘uroodog 6S ed ‘°° "DIeyT 9c ee u1oodog 08 Ce toyse[d puey 4 ee eee oe SEUSS So ag QP ereeene seog ZS eee cw eo ee ee eens ****sspis wosuyO 68 TIAN LS eae 91 ste tesesesss “Daas SsBis-aAT WeLeIT SI dae : ‘synuveg CF se eres*-OZTeur IO ‘UIOD UeIpUy 9% FE eS ‘pojeod pue pep ‘sayoved 68 Bnet ee "pees sseis ueiiesunyy OF ata se ayitt ‘souveg OF coe eee cece se * “ysIpesasioH] 8g eee **sdrusieg 16 ee *AQUOPT 92 = Br tac ge 6h ee Autwoyy he " "pees Ssvis-psreyoIO OF ee sqynu ALIOYOIG CP “SU ce eee ere ee ee ee eer ee ee ee eee poos dwey 9Z *s72@0 9 Bae 2 4les s 9.906 09-08: - BELIOSSRI sre Ef tZ ee ee --pavisny oF ee MOU ul ‘JaAO]O ‘ABH 8Z Be sy ‘pavcuseq asounde ft TTA ‘74 setters -Dagsarduro0d ‘JOA0]O ‘AeYy OF eee eevee ee THN FI eee ee we weeeree “sereq ur *IQAO ) ‘ACT ¢9 “ATEN 98°9€ - ae “SeTeq passe. u09 Ze ge oak emanp Cin -21qn0p eoupuryas ul ‘eyyeyre ‘ACE se “@STB09 “ssul]PPlAL €9°SS ‘ *sayeq pesseidur0o Lg “Teo “ejqnop semMsuejzoes Ul ‘eyyeyte ‘ACE x4 “MPN FS PT OF SST)" ig aps ul “exreste ‘ABH $9 * -QUIrT oF sete eeeee "SBABNE) spunodg spunog yOOy 9Iqny TeboyeW JO owen yoo oIqng TeBoqyeyT JO oureNy Jod 1y310 Jod Jy 310M (panuuuod)—SLondodd WAVA dO SLHOIGM AOVAAAV LOADS IN STRUCTURES “eo - -sqnuyeM er +++ pags SSBIB-IOAT2A ‘sdiuin * *sooPeUIOL, “ paas Ay,OULL “sole Bios. 91d 8 pee (050.14) 616 85.050 ‘poos auvo-se8NS “Sottaq MeI}S Sar gs sesianeeses (agg ue Bens (doy ye ae ae Siete seis S5eisi eis OTT wotetisel, e «6, @6 sre ee cece ss saggms ‘S90}810g oe eens stresses soqruMm ‘se0zepOd —— 2 Sere oy = LOADS IN STRUCTURES 74 *soTqe} os 94} UI WOATS SON[LA OY] 0} Poppe oq ISNuUI pooM 94} UT peurejuOS o1Njslou Jo oSejuao10d oyY “*TS-64 S9Sed uo spoom ueI[eIIsnYy pue ourddryiyg 10} sojqe} oyeredeas 90g ‘*poom uae13 10j ou pue poom Aip AIdA IO} ae S2TqQe} BuUIMO]T[O] 943 pue Sty} Ul Sz4SsTAM oY L *SUIEIUOD FI 9IN}S[OU! yo JUNOUIe Oy} UO AJasIe] Spusdap poomM jo }YSIOM OY L—ALON CZ eek MSN VE Bow Sera SSeS SOUL IOREE ‘repedg LP eowoeve ee ee ee ee wee eens q90MS ‘qolig &Z% Riese ASS SACS tS Fee OURO. \TEDery ce Te a es Be ele Te per ‘yorg GS eee ee one eee “OPITTM erusOHTe) ‘repag 1g eeeoee ee eevee "OUI M 10 ‘roded ‘yollg GZ Sil ed I SASS Tae ate cea ad 88 yf edjeyeg 91 Pr ee ee ee ee) ereqeyyogd LZ ie. & 0. 6 6 4 8 eee ‘ueeq uevIpUy Io ‘edjeyeg aP ee eo e@ceeeneeeseseee yooog 9¢ SENSI SIE UH ae MES BP RE oy Ew 1g eeeeeeeoe ere eeeesreee ee eee 901} Avg cE eoenrevoeeee “91OWUIBOAS Io ‘poomuoyyng 8% eevee see nese ee era ere eee eee poomsseg CZ beeen rere eeee ee ees saniraqaing 2z a hee We re Se ala are ooqueg iste) Rie h SSR = se A Se SS. oes SOOT OMe LZ Ua eh 2s See [9 8-8: 8 ay SRE ee 1% cr eseecereseese ss saggms ‘oAoHOng 6g eo ee ee eros oo ee sees reese ou M ‘Sy 8% ARAN, Sas SNR OL. 8 SORE), OOM TEL Se eeneeee re eoee ree eee ‘por ‘ysy LS ore ersneeo ee ee eee * *youely ‘poomxog cE eaeesreere ee ee oe eeeeeeee uoso1l ‘UsV es se ee Stay Es 1) 5 9-8 OTT ‘poomxog 6 eoerneeroereeaoeee eer eeeeree ee usool ‘UsV £9 . oe ee eree *por ‘uelizelg ‘poomxog PP . ° Pa ee ee ee en]{q ‘UsyV 9% eee ‘o[deu poAavoa]-yse Io ‘rape xog 6 eseeeeeweeoeeeen ee eeeeeees yoryq ‘UsV 69 o4 EP oes ee we eeseee (9014 I9A9J) wns anid 61 eee oe ee ere ew ee ewww ee ee “SYA soqiy CF “ee ee eo werner (poomuolt) yooeq, eng Z sesevceenvnenee ee eeeen ee eeeeeeer eddy OP BLY ER are tae ast eee 6 ok SONA: Osteh oP exe sveseveeveeeeeeverveoeeeeeee Jeply spunog spunodg OO dIqng yoo. oIqn yod Fut Ah eel jo wey en Pichtok eel JO oweN esvIBAY aBVIIAY Aud ‘SdqOOM AO LHOIGM LOADS IN STRUCTURES a eres CR eee ; ese eet hai fice of tf. eeeeoe eee ecceoe ‘OJOIIg Ooreon “-ysruedg ouluse wan "9013 enyso eed ‘AIOYOUT “gnu 1 39900ut ‘ALOMOY * *yooyweyy "uO MEPL pote? (your uvonowy) soeseunnoey] cheat *700MS ‘une) ‘mos ‘ums * "0033.00 ‘uins) * -qreayuees£) Sa) may oie) “ouTyM ‘It Nalaou B ‘oyjouryed * woysuryse M ‘ued ‘pooma[ppeg * 901} VBURIO peas ‘asuelOC (oesalieg « oyut eemares ysHig Woly 4sBvog sy19eq) i ‘eo ee eee 78 LOADS IN STRUCTURES &% * "9033 enysof to ‘eo0n K GZ sr oq ‘Qnuye A os “ystuedg ‘MO 9¢ Cie Ne RC ee ee a "‘UBISIOg ‘qnuye 6P “yong ‘MOK SP ee “* “UeITeIT ‘qnuyle Mm Zo . *eInie xX 9g ee “Ysijsuq ‘qnuye M 1B “yoeiq ‘MOTIELM, ce "Tr r ttt tts SBISSBOII) ‘qnuye M 9% " * POOMa7TY M Se. ae "eid ‘qnuye MA 92 “eqyese M €8 *901} OUIA Spunod spunog yooy s1qng 4oo,F dIqn Foc vuse Ry sol], JO oWIeN i oe eis sol], JooweN BBPIIAY WBBIOAY (panuyuo))—xXad ‘SdOOM JO LHOIGM ; LOADS IN STRUCTURES 79 WEIGHT OF PHILIPPINE WOODS, DRY Sati dgoalt wa Name of Tree Cubic eet Name of Tree Cubie poet Pounds Pounds Acle 37 EANGIR SS ee ca 44 Amuguis 43 Lumbayao..... 35 Apitong., Ack 22.s.+ 41 Macaasin....... 44 Aranga.... 154 Malasontol..... 40 Balacat.... Malugay....... 40 Balacbacan ..... 34 Mayapis........ 25 Bansalaguin..... 53 Molave......... 49 BSAHUVO S355 o0eusc) « 33 Buse t.ie si 36 Batitinan : 49 Palo Maria..... 39 1 3 9 PR err Be 49 Sacat 37 WSIANEAS 2: ic ids0 58 27 WaSalt 36 iis css 55 Dungon.. 49 Supa;.... 45 Guijo.... 43 Tanguile....... 30 BTL oc setetsiek ccvsjes 6 47 TIMNGalos wics-4 05-0 48 Lauan by 2s age ee §2 WEIGHT OF AUSTRALIAN WOODS, DRY Ae bi beac Name of Tree hha a Wer Pounds Acacia dealbata (silver wattle)................ 57 Acacia decurrens (common wattle) . 47 Acacia implexa.. 44 Acacia melanoxylon. (blackwood; lightwood). . 47 Acacia mollissima (silver wattle). . 50 Acacia pycnantha (golden wattle)... 52 Acacia salicina. . Te weittnre Bees 48 Araucaria cunninghamii (pine). ilasatniwWa sitet ere 45 Aster argophyllus (musk tree)................. 40 Banksia integrifolia (coast honeysuckle tree) . 50 Banksia marginata (common honeysuckle tree) . 38 Banksia serrata (heath honeysuckle tree). . : 50 Callitris verrucosa anata PRE pine, or cypress). . shes ; : 43 NOTE.—On account of the unsettled nomenclature of Australian woods, this table gives botanical names, with common names, so far as possible, in parenthesis after the botanical name. 80 LOADS IN STRUCTURES WEIGHT OF AUSTRALIAN WOODS, DRY—(Continued) Name of Tree Castanaspermum australe (black bean) ........ Casuarina torulusa (forest oak) ............000. Casuarina quadravalvis (drooping she seat Cedrela australis (cedar). ............8.cceeees Ceratopetalum apetalum (coachwood) . ss wee ey Dacrydium cupressinum (rimu)............... ' Dissiliaria baloghioides (teak) ....... ra re Dysoxylon muelleri (red bean) ................ gelpsonp dm amygdalina regnans (mountain ash ppermint tree).. ; ed yptus botryoides (biue’ gum, Gippsland mahogany, or bastard mahogany).. ee ep'dsns Eucalyptus corymbosa (bloodwood). .......... Eucalyptus corynocalyx es ced ene STS Eucalyptus diversicolor (karri Shee SSLa ae 2 Eucalyptus globulus (blue gum).. Ree re Eucalyptus gomphocephala (tuart).. 5 Racaoee goniocalyx (bastard box, ‘spotted m).. inapalspties haewastowa (spotted gum).. ; Eucalyptus a eicaaonge (canary hia ig white box, or gray ; Eucalyptus laxetioieas (slaty gum). sake arelenad. seats Eucalyptus leucoxylon (iron bark, red seebieeo or black iron bark).. ee Eucalyptus longifolia Gwollybute tree). Ae eT ae Eucalyptus maculata pote PUM) ck cows oe ha'as Eucalyptus marginata (jarrah)........--+-+++-- Eucalyptus melliodora root es DOK). cna taas a5 va Eucalyptus microcorys (tallow wood).. ; Eucalyptus obliqua (messmate, stringy ‘bark).. Eucalyptus pilularis (blackbutt, or flintwood). . Eucalyptus piperita sem coring ate stringy bark tree)..... ’ Eucalyptus resinifera (mahogan SM Slain Abe eee Eucalyptus robusta (swamp m oan). SEAS hICAr Eucalyptus rostrata (red gum tree). ate BATS Eucalyptus saligna (gray gum)...............: Eucalyptus siderophloia (iron bark). . .Eucalyptus sieberiana (iron bark, "gumtop stringy bark, mountain ashes)............... woke eight per Cubic Foot Pounds SI2SSS FS SSRERSSS LOADS IN STRUCTURES 81. WEIGHT OF AUSTRALIAN WOODS, DRY—(Continued) | Sha Name of Tree Cube Rad Pounds Eucalyptus tereticarnis (flooded gum).......... 68 Eucalyptus viminalis (manna sees tree, a Croaeroe gum, or white gum tree)..... 43 Eugenia smithii (myrtle) . 57 Exocarpus cupressiformis (native cherry ‘tree).. 50 Fagus cunninghamii (evergreen Deech or native myrtle). . aly idroian a7 45 Hakea leucoptera (water tree). 51 Heterodendron preroliieas;: ate 53 Lomatia fraseri . : 42 Melalenca decussata. . 59 Melalenca econ ape 62 Myporum insulare.. 51 Myrsine variabilis. . 45 Panax murrayi (palm panax).. 22 Pimelea microcephala. 55 Pittosporum bicolor (white wood)... 48 Pomaderris apetala (hazel).. 48 Prostanthera lasianthas {mmiet tree).. 51 ean acuminatum (native peach ‘or quan- xi Bantatasn persicarium (native sandalwood). cracciece 47 Senecio bedfordii (native dogwood)........... 56 Syncarpia laurifolia (turpentine) .............. 63 Tristania conferta (brush or white ‘bpr).- Bratend cleats 67 Tristania neriifolia yan a) hs oe 63 Viminaria denudata . : 39 SNOW AND WIND LOADS In calculating the weights on roofs, the snow load must be included. When the rise of the roof is under 12 in. per ft. of horizontal distance, the snow load is estimated at 12 lb. per sq. ft.; for roofs of a rise of more than 12 in. per ft. of horizontal distance, assume the snow load to be 8 lb. persa. ft. In northern climates, such as that of Canada, snow loads 50% greater than the preceding should be assumed. The wind pressure depends on the velocity with which the air is moving. United States government tests have 82 LOADS IN STRUCTURES determined that the pressure per square foot on a vertical surface is approximately represented by the formula p= .00492V2, in which p is the pressure, in pounds per square foot, of ver- tical surface, and V is the velocity of wind, in miles per hour. Careful records, extending over a period of years, show that the velocity of the wind seldom attains 100 mi. per hr.— probably not more than once in the lifetime of a structure. The following table was calculated by means of the pre- ceding formula. Though the table indicates that for 100 mi. an hr. the pressure per square foot is nearly 50 lb., modern practice often allows only 40 lb. per sq. ft. for large surfaces. VELOCITY AND FORCE OF WIND, IN POUNDS PER SQUARE FOOT, ON A VERTICAL SURFACE Force Miles | Feet | Feet oe Strength of Wind pr per per ae our |Minute | Second Square Foot Hardly perceptible........ 1 88 |. 1.47 .005 J bl 5 364 440 ‘bas ust perceptible......... he : } 4 352 5.78 .079 Gentle breeze............. 5 440 7.33 .123 . 10 880 14.67 .492 Pleasant breeze........:6. 15 1,320 22.00 | 1.107 Briskwale, . bo. « 52.w:do asnwde 20 ,760 29.33 | 1.968 25 2,200 36.67 | 3.075 FRIGH RVIIG Fo patel RF a ck hele 30 2,640 44.00 | 4.428 35 3,080 51.33 | 6.027 40 3,520 58.67 | 7.872 Very high wind........... 45 3,960 66.00 | 9.963 PRETO N ee an geal oars ae Se 50 4,400 73.33 | 12.300 60 5,280 88.00 | 17.712 Great stormyn.. ss sete ee bee's 70 6,160 | 102.67.) 24.108 80 7,040 | 117.33 | 31.488 Hurricane or cyclone......} 100 8,800 | 146.67 | 49.200 Curved and flat surfaces not in a vertical plane are sub- jected to less pressure than flat vertical surfaces. The pres- LOADS IN STRUCTURES 83 sure on a cylindrical surface is about one-half the pressure on a flat surface having the same width as the diameter of the cyl- inder and the same height. If p’, Fig. 1, represents the direction and strength of the wind pressure against the roof abc, it isthe normal component p that must be ascertained in order to calculate the total pressure nor- mal to the roof, or to determine the stresses in the members of a roof frame or truss. The other component py is acting upwards and in a direction parallel with the slope. The latter force is not taken into consideration. The wind, which is usually supposed to exert a horizontal pressure of 40 lb., strikes the roof at an angle; consequently, the pressure p, normal to the slope, is less than 40 lb. The full discussion of the relation between p’ and »p is somewhat more complex than the one given here, however. What has been said shows in a general way why »p is more nearly equal to »’ when a roof is steep than when a roof is flat. In the design of roof trusses, a horizontal wind pres- sure of 40 Ib. is usually assumed. NORMAL WIND PRESSURE FROM HORIZONTAL PRES- SURE OF 40 LB. PER SQ. FT. Fic. 1 Horizontal Per Pitch, Wind Pressure Rise per Sere Aa Proportion | Normal to Slope poe ‘Horizontal of Rise Pounds per Inches to Span Square Foot 4 18° 26’ 4 23.00 4.8 21° 48’ 26.11 6 26° 34’ 29.82 8 33° 41’ 33.93 12 45° QO’ 37.71 16 53° 8! 39.02 18 56° 19’ 39.33 24 63° 26/ 1 39.75 84 LOADS IN STRUCTURES All necessary data for calculating the wind pressure on a roof with any one of the customary pitches and a horizon- tal wind pressure of 40 lb. per sq. ft. are given in the table on page 83. The diagram shown in Fig. 2 facilitates the finding of the normal pressure » for the usual slopes and for horizontal wind pressures of 20, 30, and 40 lb. per sq. ft. 70 i Pitch Lid dee ba ae eo 60° Pitch 4 a 4 & eeure <0 N ¥ genes -t 7. i.e SEUU EEE ADELE ~ £02 30 Wind Pressure Normil to Slope of Roof in Pounds Per Square Foot Fic. 2 The values of the normal pressure for a given slope and a horizontal wind pressure of 20, 30, or 40 lb. may be found as follows: Assume that the normal pressures on a roof hav- ing an angle with the horizontal of 40° is to be determined. Proceed along the horizontal line marked 40° until it inter- sects the curve marked 20 lb., which represents a horizontal wind pressure of 20 lb. The point of intersection indicates the normal pressure p, the value of which is found by draw- ing an imaginary vertical line to the base line, which is marked off in pounds of pressure per square foot. It is - LOADS IN STRUCTURES 85 found that the normal pressure p amounts to 18.2 lb. per sq. ft. Proceeding in the same manner, it is found that for horizontal pressures of 30 and 40 lb., the normal pressures are 27.3 and 36.4 lb. per sq. ft., respectively. In Fig. 3, the normal force » has been resolved into its two components, p, and py, the former acting in a horizontal direction and the latter in a vertical one. The force pz tends to push the roof in a direction parallel with the wind, while the force p, tends to depress the roof or, in some cases, to press it sidewise. In open sheds, where the wind is liable to strike the inner, far Fic. 3 side of the shed roof, the effect of the force », must be con- sidered, as its tendency would be to lift the roof. DISPOSITION OF LOADS In warehouses where all floors are likely at any one time to be fully loaded, the beams, girders, columns, and founda- tions are always proportioned for the entire live and dead loads. However, where the building exceeds four or five stories in height and is used for any other purpose except storage, as, for instance, a modern office building, it is cus- tomary to assume that certain members, while proportioned for the entire dead load, carry only a certain percentage of the live load. In an office building, or similar structure, it is highly improbable that all the floors or all parts of the same floor will be fully loaded at the same time, and in view of this fact it is considered good practice, while proportioning the floor- beams for the full live load, to calculate only say 90% of the live load on the girders and columns. It is customary to proportion the columns supporting the roof and the top floor for the full live load. The live loads on the columns, in each successive tier, from the floor above is reduced 10% until 50% of the live load is reached, when such reduced loads are used for all the remaining floors to the basement. 86 LOADS IN STRUCTURES The economy obtained by this disposition of the live load is observed from the following table, which gives the dis- tribution of the assumed live loads on the columns in the several tiers of an eighteen-story office building. REDUCTION OF LIVE LOADS FROM FLOOR TO FLOOR Floors a a, = .90a za za on AGS 2a Roof 20 20.00 20 20.00 18 60 60.00 80 80.00 17 60 54. 140 134.00 4.3 16 60 48 .60 200 182.60 8.7 15 60 43.74 260 226 .34 12.9 14 60 39.37 320 265.71 17.0 13 60 35.43 380 301.14 20.8 12 60 31.89 440 333 .03 24.3 11 60 30.00 500 363 .03 27.4 10 60 30.00 393 .03 29.8 9 60 30.00 620 423 .03 31.8 8 60 30.00 680 453 .03 33.4 7 60 30.00 740 483 .03 34.7 6 60 30.00 513.03 35.9 5 60 30.00 860 543.03 36.9 4 60 30.00 920 573.03 37.7 3 60 30.00 980 603 .03 38.5 2 60 30.00 1,040 633 .03 39.1 1 60 30.00 1,100 663 .03 39.7 The following may serve to explain the data given in the table: a represents the live load on each floor, in pounds per square foot; a; the live load on each floor, in pounds per square foot, reduced by 10%, as a;=.90 a; 2a, the sum of all live loads, in pounds per square foot, on a column from all floors above, if no reduction is made; and 2a,, the sum of all live loads, in pounds per square foot, on a column from all floors above, if 10% reduction is made. The theoretical percentage of saving resulting from the reduction of 10% on the upper floors is found by the for- za— za —. These percentages of saving are given in ul mula Sa the last column of the table. MECHANICS 87 It should be understood that each column of a building supports a given floor area, and that the load coming on each column will depend on the extent of this area multiplied by - the live load, in pounds per square foot of floor. Each column carries not alone this load, but also the loads trans- mitted directly from column to column. Thus, the column supporting the fifteenth floor supports also four other columns above with all their loads. While this system of graduating the live loads on the columns from floor to floor is generally practiced, the amount of reduction at each floor is a matter that depends on the judgment of the designer. The percentage of reduction is often fixed by city building laws, with bbe us the designer must comply. MECHANICS FORCES Two forces may be compared when the three following facts about each force are known: (1) The point of applica- tion, or point at which the force acts; (2) the direction of the force or line along which it acts; and (3) the magnitude of the force when compared with a given standard. In engineering work in America, the unit of force is always taken as the pound. Representation of a Force.—A force may be represented by aline. Thus, in Fig. 1, let A be the point of application of the force, let the length of the line AB Tepresent its magnitude and line of action to any convenient selected scale, as, for Fie. 1 instance, 1 in. equals 10 lb., and let the arrowhead indicate the direction in which the force acts. Then the line AB fulfils the three required conditions in regard to point of application, direction, and intensity, and the force is fully represented. z & 88 MECHANICS COMPOSITION OF FORCES If several forces act on a body, and if they are replaced by a single force that has the same effect in moving the body through space as the several forces combined, the single force is called the resultant of the several forces; and, conversely, the several forces are called the components of the single force. The process of finding the resultant when the various components are known is called the composition of forces. _ Parallelogram of Forces.—When */ “two forces act on a body at the same time and at the same point, but at different angles, their final effect may be obtained as follows: In Fig. 2, let A’ be the com- SO1n. 4 ~— c mon point of application of the bcs hae two forces, and let AB and Fic: 2 AC represent the magnitude and direction of the forces. Let, for instance, the line AB repre- sent the distance that the force AB would cause the body to move in a certain length of time; similarly, let AC represent the distance that the force AC would cause the body to move in the same length of time, when both forces are acting separately. A fundamental law of mechanics states that the motion is proportional to the force applied, and, therefore, while AB and AC represent the magnitude of the forces to some scale, they are also proportional to the distances these forces would move the same body in the same length of time. The force AB, acting alone, would carry the body to B. If the force AC were now to act on the body, it would carry it along the line BD, parallel to AC, to a point D, at a distance from B equal to AC. Join C and D, then CD is parallel to AB and ABDC isa parallelogram. Draw the diagonal AD. The body will stop at D, whether the forces act separately or together, but if they act together, the path of the body will be along AD, the diagonal of the parallelogram. More- over, the length of the line AD represents the magnitude of a force, which, acting at A in the direction AD, would cause the body to move from A to D; in other words, AD, measured to the same scale as AB and AC, represents the magnitude MECHANICS 89 and direction of the combined effect of the two forces AB and AC. The force represented by the line AD is the resultant of the forces AB and AC. Suppose that the scale used was 50 lb. to the inch; then, if AB=50 lb. and AC=623 Ib., the length of AB would be 50+50=1 in., and the length of AC would be 62.5+50=1}4in. If the line AD measures 1? in., the magnitude of the resultant, which it represents, would be 13 X 50 =87}3 Ib. Therefore, a force of 874 Ib., acting on a body at A, in the direction AD, will produce the same result as the combined effects of a force of 50 lb. acting in the direction AB and a force of 624 lb. acting in the direction AC. Triangle of Forces.—Let Fig. 3 represent a parallelogram of forces. AB and AC are the two component forces and AD is theresultant. Now, to find this resultant AD without drawing the entire parallelogram, first lay off AB, and then from the point B lay off BD ee equal to AC and parallel to its line of action; then, draw AD, which completes the triangle ABD and makes it unnecessary to draw AC and CD. Or, the force AC could be drawn first, and then from C, the line Fic. 3 CD, thus completing the triangle ACD and not drawing AB and BD. Ineither case, it is seen that, if desired, the result- ant of two forces can be found by drawing a triangle instead of a parallelogram. Resultant of Several Forces.—When three or more forces act on a body at a given point, their resultant may be found as follows: Find the resultant of any two forces; treat this resultant as a single force, and combine it with a third force to find a second resultant. Combine this second resultant with a fourth force, to find a third resultant, etc. After all the forces have been thus combined, the last resultant will be the resultant of all the forces, both in magnitude and direction. The order in which the forces are taken is immaterial. 90 MECHANICS ExamPLe.—Find the resultant of all the forces acting on. the point O, Fig. 4, the length of the lines being proportional to the magnitude of the forces, SoLuTion.—Draw OE parallel and equal to AO, and EF parallel and equal to BO; then OF is the resultant of these two forces, and its direction is from O to F. Consider OF as replacing OF and EF, and draw FG parallel and equal to CO; OG will be the resultant of OF and FG; but OF is the resultant of OE and EF; hence, OG is the resultant of OE, EF, and FG, and likewise of AO, BO, and CO. The line FG, parallel to CO, could not be drawn from the point O to the right of OE, for in that case it would be opposed in direction to OF; but FG must have the same direction as OF. For the same reason, draw GL parallel and equal to DO. Join O and L, and OL will be the resultant of all the forces AO, BO, CO, and DO (both in magnitude and direction) acting at the point O. If L’O is drawn parallel and equal to OL, and having the same direction, it will represent the effect produced on the body by the combined action of the forces AO, BO, CO, and DO. For brevity, the terms forces AO, BO, etc. and resultants OF, OG, and OL have been used in this solution. It should be remembered, however, that these are merely lines that represent the forces in magnitude and direction, MECHANICS 91 In Fig. 4 the forces OE, EF, etc., all point in the same direction; that is, a body at O acted on by these forces in succession would move from Otol. The resultant therefore acts from O to L, and not from L to O, This line of reason- ing will give the direction of the resultant in a force diagram. In Fig. 4, the forces were taken in the order AO, BO, CO, and DO. However, the magnitude and direction of the resultant OL would be the same, no matter in what order the forces were taken. RESOLUTION OF FORCES Since two forces can be combined to form a single redeteat force, a single force may also be treated as if it were the resultant of two forces whose joint action on a body will be the same as that of a single force. Thus, in Fig. 5, the force OA may be resolved into two forces, OB’ and B’A. It will be observed that one resultant force may have an innumerable number of combinations of components. Instead of OB’ and B’A, Fig.5,OB” or B’” A orOB'”’ and B’”’A may be taken as components. It is cus- tomary, however, to make 32” OB’ and B’A perpendicu- lar to each other, as pe SN shown in the illustra- ? < tion. Fic. 5 Frequently, the positiony magnitude, and direction of @ certain force are known, and it is desired to know the effect of the force in some direction other than that in which it acts. Thus, in Fig. 6, suppose that OA represents, to some scale, the magnitude, direction, and line of action of a force acting on a body at A, and weet pee ece eee ee eo 4 that it is desired to know what Fic. 6 effect OA produces in the direction BA. From A draw a line AB in the required direction; from O draw a line per- pendicular to AB. Then BA is the component required. on oo $ o°* a 92 MECHANICS It is necessary, of course, that OB be at right angles to BA, so that all the effect of OA in the required direction may be represented by BA and none of it by OB. Thus, OB’ and B’A, although components of OA, and although one of them is in the required direction, would not be a correct solution of the problem because, besides B’A, OA exerts some more effect in the line BA, namely, a part of OB’ is in that direc- tion with an amount BB’. ExaMPLE.—If a body weighing 200 Ib. rests on an inclined plane whose angle of inclination to the horizontal is 18°, what force does it exert perpendicular to the plane, and what force does it exert parallel to the plane, tending to slide it downwards? SoLutTion.—Let ABC, Fig. 7, be the plane, the anette A being 18°, and let W be the weight. Draw a vertical line Fic. 7 Fic. 8 FD=200 1b., to represent the magnitude of the weight. Through F draw FE parallel to AB, and through D draw DE perpendicular to EF, the two lines intersecting at E. FDis now resolved into two components, one FE tending to pull the weight down the incline, and the other ED acting as a perpendicular pressure on the plane. On measuring FE with the same scale by which the weight FD was laid off, it is found to be about 61.8 lb., and the perpendicular pres- sure ED on the plane is found to measure 190.2 Ib. _ As it is often necessary to resolve a force into two com- ponents at right angles to each other, a simple method of solution is employed. In Fig. 8, let OA be the force it is desired to resolve into two components at right angles to. MECHANICS 93 each other. Through O as a center draw an indefinite line XX’ in the required direction of one of the components, and through the same center O draw the indefinite line Y Y’ in the direction of the other component. Then XX’ and YY’ are at right angles to each other, since the components to be found are to be at right angles to each other. The line XX’ is commonly called the XX’ axis, or simply the X axis, and the line YY’, the YY’ axis or the Y axis. From A draw a line perpendicular to the X axis, as Aa’, and also a line perpendicular to the Y axis, as Aa”. Then Qa’ is the component force in the direction of XX’ and Oa” is the other component in the direction of YY’. When the components Oa’ and Oa” are horizontal and vertical, as in the present case, they are called, respectively, the horizontal component and the vertical component of the force OA. ; ‘ MOMENTS OF FORCES DEFINITIONS AND MEASUREMENTS In Fig. 1, W is a weight that tends to fall—that is, to act downwards—with a force of 10,000 lb. It is well known that if some fixed point, as a, not in the line along which the weight W acts, is con- nected with the line of action 4 of W by a rigid arm, so that jj Hi W pulls on one end of this | arm while the other end is |i//-% firmly held at a, the pull of as W will tend to turn, or rotate, [im the arm about the point a. It is also known that the tendency to rotate is directly proportional to the magni- tude of the force, provided the arm remains of the same length, and directly proportional to the length of the arm, if the force remains constant. In general, therefore, the rotative- effect is proportional to the Fic. 1 94 MECHANICS product of the magnitude of the force and the length of the lever arm. This product is called the moment of the force with respect to the point in question. Thus, in Fig. 1, the moment of the force W with respect to the point a is the product obtained by multiplying the magnitude, 10,000 Ib., by the perpendicular distance, 10 ft., from the point a to the line of action of W. The point a, Fig. 1, that is assumed as the center around which there is a tendency to rotate, is called the center, or origin, of moments. : The perpendicular distance from the center of moments .- to the line along which the force acts, is the lever arm of the force, or the leverage of the force. Since the unit of force is the pound, and the ordinary unit of length is the foot, the unit of moment will be a derived unit, the foot-pound (abbreviated to jt.-lb.), and moments will usually be expressed in foot-pounds. In Fig. 1, for example, the moment of the force W with respect to the point ‘a is 10,000 X 10=100,000 ft.-Ib. The moment of a force may be expressed in inch-pounds (in.-lb.), foot-pounds, or foot-tons (ft.-T.), depending on the unit of measurement used to designate the magnitude of the force and the length of its lever arm. For instance, if the magnitude of a force is measured in pounds, and the lever arm through which it acts in inches, the moment will be in inch-pounds; again, if a force of 10 T. acts through a lever arm of 20 ft., the moment of the force is 10 X 20 = 200 ft.-T. Positive and Negative Moments.—In order to distinguish between the directions in which there is a tendency to produce rotation, the signs + and — may be used. Thus if a force tends to produce right-hand rotation, that is, rota- tion in the same direction as the hands of a clock, it is called positive, and its moment takes the sign +; a force that tends to produce rotation in the opposite direction is called neg- ative, and its moment takes the sign —. The selection of one direction for positive and another for negative is merely an arbitrary distinction to show that the directions are opposite. It has, however, been adopted by engineers, and should always be used as given. MECHANICS 95 Resultant Moments.—In Fig. 2 is shown a lever com- posed of two arms at right angles to each other, and free to turn about the center C. A force A acts on the horizontal arm in such a manner that it tends to produce left-hand rotation, its moment being 10X5=50 ft.-lb., which, since it tends to produce left-hand rotation, will be ealled negative. Another force B, whose moment with respect to the center C is 12X3=36 ft.-lb., tends to produce right-hand rotation. B-12 Bt: i. \ —5 ft. pe Bowes Fic. 2 Therefore, —50+36=—14 ft.-lb., which is the resultant moment, and has the same turning effect as the two moments already given. If, instead of the two forces just considered, there is a body that is acted on by any number of forces whose moments about a given center are known, the resultant moment of these forces will be the algebraic sum of the moments of the given forces. CENTER OF GRAVITY The center of gravity of a body, or of a system of bodies, or forces, is that point at which the body or system may be balanced, or it is the point at which the whole weight 96 MECHANICS of the body or bodies may be considered as concentrated. If the body or system were suspended from any other point than the center of gravity, and in such a manner as to be free to turn about the point of suspension, it would rotate until the center of gravity reached a position directly under the point of suspension. Center of Gravity of Plane pistes: —If the plane figure has one axis of symmetry, this axis passes through its center of gravity. If the figure has two axes of symmetry, its center of gravity is at their point of intersection, The center of gravity of a triangle lies on a line drawn from a vertex to the middle point of the opposite side, and at a distance from that side equal to one-third the length of the line; or it is at the intersection of lines drawn from the ver- texes to the middle of the opposite sides. The perpendicular distance of the center of gravity of a triangle from the base is equal to one-third the altitude. The center of gravity of a parallelogram is at the inter- section of its two diagonals; Soerenee ae it is midway between its sides. The center of gravity of an auseulae jour-sided figure may be found as follows: First divide it, by a diagonal, into two triangles and join the centers of gravity of the triangles by a straight line; then, by means of the other diagonal, divide the fig- ee) ure into two other triangles, and a ! join their centers of gravity by e another straight line; the center of gravity of the figure is at the intersection of the lines joining the centers of gravity of the two sets of. triangles. Another method by which to A locate the center of gravity of an irregular four-sided figure is illus- Fic. 3 trated in Fig. 3. Draw the diag- onals ac and bd, and from their intersection e¢, measure the distance to any vertex, as ae. From the opposite vertex, lay off this distance, as at cf. Then from f, draw a line to MECHANICS . 97 one of the other vertexes, as fd, and bisect this line as at g. Connect g and b and lay off one-third of its length from g at the point hk, This point is the center of gravity of the The distance of the center of gravity of the surface of a half circle from the center is equal to the radius multiplied by .424, Neutral Axis.—The neutral axis of a flat or plane figure may be considered as any line passing through the center of gravity. This definition of neutral axis is correct for use in the mechanics of ordinary materials. However, in speaking of the neutral axis of reinforced-concrete beams, something else is meant, This will be explained later. The location of the horizontal neutral axis, that is, a horizontal line through the center of gravity of a plane figure, is of great importance in engineering. Of course, if the center of gravity is located, the horizontal neutral axis can be located easily; but, as a rule, the horizontal neutral axis is located without first locating the center of gravity. Locating the Neutral Axis by Means of the Principle of Moments.—A convenient method of locating the neutral axis is based on the principle that the moment of any plane figure, with respect to any given line as an axis or origin of moments, is equal to the product of its area by the perpen- dicular distance from the center of gravity of the figure to the given axis, Let M represent the moment; A, the area of the figure or section; andc the perpendicular distance from center of gravity of figure to given axis. Then, M M=AXce andc= A If necessary, the figure may be subdivided; then the moment of the figure is equal to the sum of the moments of its separate parts with respect to the same axis. Designa- ting the areas of the subdivisions by the letters a, a’, a”, etc. and their moments by m, m’, m”, etc., then the preceding formula becomes m+m’+m”, etc. c= at+a’+a’”, etc. 98 MECHANICS Built-Up Section.—Fig. 4 shows a section of the rafter member of a large roof truss formed of a 3” X16” web-plate and a 3” X12” flange plate, the two joined by two 4” X 4” X }” angles. It is desired to know the distance from the neutral axis of the section to the top edge of the flange plate. By means of the principles given, the centers of gravity of the two rectangular plates are easily located as shown. The centers of gravity of the angles might also be located by applying the rule given in the preceding paragraph; this, however, is unnecessary because the position of the center of gravity can be obtained directly by referring to the tables of the properties of rolled sections furnished by the various steel manufacturers. By referring to any of these tables, the center of gravity of a 4”X4”X4” angle is found to be 1.18 in, from the back of a flange, thus giving the distance 1.18 + .875=1.555, or about 144, in. from the top edge of the flange plate to the axis through the centers of gravity of the angles, From the same tables it is also found that the area of the section of a 4” 4” 4” angle is 3.75 sq. in. The area of the section of the flange plate is 3X12=4.5 sq. in., and of the web-plate, 3 16=6 sq. in.; the area of the whole section is therefore 2X 3.75+4.5+6=18 sq. in. MECHANICS 99 The moments of the areas of the separate sections, with respect to the line ab, are as follows: Flange plate, 45X %&= 84 Two angles, 2X3.75X14#=11:70 Web-plate, 6X82 =50.25 Total, 62.79 The distance c from the top edge of the flange plate to the neutral axis de of the section is therefore 62.79 +18=3.48 in. FORCES ACTING ON BEAMS STYLES OF BEAMS A beam that has two points of support, one at each end, as shown in Fig. 1, is known asa simple beam, The distance between the points of sup- port is called the span. A beam that has more & than two supports, as Fic. 1 shown in Fig 2, is known asa continuous beam. The point of support of the middle support is con- sidered to be at its cen- ter, as at a. Continuous beams, except in rein- forced-concrete work, have not found much favor among engineers in the Fic. 3 last few years. A cantilever beam is one with only one sup- port, which is at the middle, or any part of a beam that projects out beyond its support. A common form of cantilever is shown in Fig.3. This beam projects from a wall or some other solid structure and has no support at its outer end. Fic. 2 Fic. 4 100 3 MECHANICS _ When a beam is rigidly held, or fixed, at both ends, as shown in Fig, 4, it is called a restrained beam, or, more com- monly, a beam fixed at both ends. LOADS ON BEAMS The forces due to the weights that a beam supports are known as loads. If the whole load is applied at one point, or practically one point, it is called a concentrated load; if it extends over a portion of the beam, it is called a distributed load; and if it is equally distributed over the beam, so that each unit of length has the same load, it is called a uniform load. There are certain methods by which such loads may be represented graphically. These methods may best be illus- trated by referring to Fig. 5, which shows a simple beam, Starting at the left, the point of the arrow shown at R; is the point of support. The Fic. 5 arrow a represents a concentrated load. At bb’ is shown a uniformly distributed load, of a certain number of pounds per foot of beam, that extends from b tob’. Atc,d, and f are shown other concen- trated loads similar to the one at a. From ¢ to é’ is a distrib- uted load, represented by the shaded triangle under ee’, that starts from nothing at e and increases to a given number of pounds per foot of beam ate’. At gg” is a distributed load, _ starting from nothing at g and increasing to a maximum at g’, and then decreasing to nothing at g”. At Ro is shown the right-hand support. REACTIONS A beam with any loads it may carry is held up by the supports; that is, the beam presses on its supports at the ends, The supports resist this pressure and prevent the beam from falling. This upward force exerted by each support is known as the reaction. There are two facts susceptible to proof in regard to a beam: (1) The resultant of all the forces acting on a body MECHANICS 101 or beam must be zero, and (2) the resultant moment of all the forces about any point must be zero. The forces acting on a beam are the forces due to loads on the beam and the weight of the beam itself, if that is con- sidered, and then there are the reactions of the supports on the beam. Now, all the loads act vertically downwards and the reactions act vertically upwards. They are therefore parallel; and as they are opposite, the sum of the loads must equal the sum of the reactions. A beam with two supports will be considered. The sum of the reactions is known from the loads, but the value of each reaction is not known. To find this, it is necessary to resort to the second condition, namely, that the resultant moment of all the forces about any point must be zero. Any point can be assumed, but it is found convenient to choose the reaction of one support as the point about which to take moments, The moment of the reaction at the point is zero, because the arm of the moment is zero. It is there- fore necessary that the sum of the moments of the loads about one point of support and the moment of the other reaction about the same point shall equal zero, ass. =: ~) : J i 3 3 $ ] — + 27 ft-—-— | — —— — —-19 st- — + — — aan p——8 ft— { i rt ere RESET oa z b, Fic. 6 A practical example will now be considered. In Fig. 6 let it be required to find the reactions R, and R2 at the points of support aand b. (In all the subjoined problems, R; and Rz represent the reactions.) The center of moments may be taken at either R; or Ro. Let the point b be taken in this case. The three loads are forces acting in a downward 102 MECHANICS direction; the sum of their moments, in foot-pounds, with respect to the assumed center, may be computed as follows: 8,000X 5= 40000 6,000 x 19=114000 2,000X27= 54000 Total, 208000 This is the total negative moment about the pointb. The positive moment about this point is of course R, X30. Since the resultant moment is zero, the positive moment must equal the negative moment, or 208,000=30 R; or R; = 208,000 +30 =6,9334 lb. The sum of all the loads is 2,000+ 6,000+ 8,000 = 16,000 lb. This is also the sum of the reactions. Therefore, R2=16,000—6,9334 =9,066% Ib. In this problem, the weight of the beam itself has been neglected. EXAMPLE 1.—What is the reaction at Rz in Fig. 7? SoLuTION.—In computing the moment due to a uniform, or evenly distributed, load, as at a, the lever arm is always considered as the distance from the center of moments to <_- 20 ft. $ $-127¢ sono te parirunnt no bok ety LIA zy Yi st tintzorm tout _ 10 ft: ! 30 ft. Ry Rez Fic. 7 the center of gravity of the load. The amount of the uni- | form load a is 3,000 X 10 =30,000 1b., and the distance of its center of gravity from R; is 13 ft. Therefore, the moments of the loads on this beam about Rj, in fopspeunes, are as follows: 30,000 X 13=3 90000 4,000 4= 16000 9,000 xX 20=180000 Total, 586000 MECHANICS 103 This is the sum of the moments of all the loads about R,, asacenter. The leverage of the reaction Re is 30 ft. Hence, the reaction at Re is 586,000 +30 =19,5334 Ib. 000 1b. per running ft. 6 ft. ExAamMPLE 2.—A beam is loaded as shown in Fig. 8. Com- pute the reactions R; and Ro. SoLuTion.—Consider, say Ro, as the center of moments. Then, the negative moments of the loads about Ro, in foot- pounds, are 20,000 X 27=5 40000 2,000X12= 24000 3,000X 8= 24000 Total, 588000 Now, the positive moments of the loads about Re, in foot- pounds, are 1,000 X6X3=18000 5,000X6 =380000 . Total, 48000 The resultant moment of the loads about Rz is negative and is —588,000+ 48,000 = —540,000 ft.-lb.; 540,000+30 = 18,000 lb., which is the value of Rj. The sum of the loads is 20000 2000 3000 6X1,000= 6000 5000 36000 R2=36,000 — 18,000 = 18,000 1b. 104 MECHANICS VERTICAL SHEAR In any beam, as for instance the one shown in Fig. 9, there are forces—either loads or reactions—acting both upwards and downwards. In this figure, the left-hand reaction Ry mes R, RF, Fic. 9 acts upwards and tends to push the end of the beam up. On account of the strength of the beam, however, the end remains stationary. If the beam were suddenly cut on the line ab, the left-hand portion of the beam would move up in relation to the right-hand portion. This action of the forces on a beam in tending to make the surfaces at any imaginary section slide past each other, from its similarity to a shearing action, is called shear. Consider now the beam shown in Fig. 10. Since the loads are symmetrically applied, each reaction is equal to 40 1b. or one-half the total load on the beam. Considering therefore, — —-- 3} — —— 9 S < < < s s — 3 3 A) a} ~) ‘EA yada le ie R, Ry Fic. 10 any transverse section of the beam between R; and the point of application of the load u, it is evident that the part of the beam at the left of this transverse section is subjected to an upward thrust of 40 lb., while the part at the right is sub- jected to an equal downward thrust. The result is a shear- MECHANICS 105 ing action at this place, the magnitude of which is equal to the reaction R,. This shearing action is resisted by the strength of the fibers of the beam at the section under con- sideration. When the point of application of is reached, the effect of the upward force R; is partly balanced by the downward force of 10 lb. due to the load m. Any section between the points of application of m and m is therefore subject to a shearing stress equal to the difference between the reaction R; and the load n, or 40—10=30 1b. In the same way, it fol- lows that the shearing stress for any section between m and o is 40—(10+15)=15 lb. For any section, as cd, between the points of application of o and p, the shearing stress is 40—(10+15+15)=0. In other words, it is a section in which there is no shear. — Positive and Negative Shear.—For convenience, it is cus- tomary to call the reactions, or forces, acting in an upward direction, positive, and the loads, or downward forces, nega- tive. Since the difference between the sums of the positive and negative numbers representing a given set of values is called their algebraic sum, it follows that the shear for any section of a. beam is equal to the algebraic sum of either reaction and the loads between this reaction and the trans- verse section under consideration. In speaking of the shear at a certain section of a beam as being positive or nega- tive, it is simply meant that the resultant of the forces acting on the portion to the left of the section under con- sideration is either positive or negative. If a transverse section of a simple beam is taken near the left reaction and the forces acting on the part of the beam at the left are considered, it will be seen that their resultant acts upwards. The shear at this section is there- fore called positive shear. If, however, a section near the right reaction is taken, the resultant of the forces at the left of this section is found to act downwards, and in conse- quence the shear is called negative. It is also evident that there is a section between the two where the resultant of the forces changes from positive to negative. At such a section the shear is said to change sign. 106 MECHANICS It can readily be seen that in a cantilever beam the con- ditions are somewhat reversed; that is, in a beam having one support at the middle, the shear in the part to the left of the section taken to the left of the support is negative, while if the section is taken to the right of the support, it is positive. Like in a simple beam, however, there is an intermediate point where the shear changes sign. 3 ~ . $ ds ~~ 3s $ =e Fic. 11 ExamMPLe.—At what point in the beam loaded as shown in Fig. 11 does the shear change sign? SoLuTIon.—Compute the reaction R; as follows: With the center of moments at Re, the moments of the loads, in foot-pounds, are 9,000 X 10 90000 4,000 X 26 =104000 3,000 X 10K 17=510000 Total, 704000 The reaction at R, is therefore 704,000 +30=23,4662 Ib. Proceeding from R;, the first load that occurs is c of 4,000 Ib. Then, 23,4662—4,000=19,4662 1b. The next load that occurs on the beam is the uniform load of 3,000 lb. per running ft. There being altogether 30,000 lb. in this load, it is evident that the load will more than counteract the remaining amount of the reaction R,; the point where the change of sign occurs must consequently be somewhere in that part of the beam covered by the uniform load. The load being 3,000 lb. per running ft., if the remaining part MECHANICS 107 of the reaction, 19,4663 1b., is divided by the 3,000 Ib., the result will be the number of feet of the uniform load required to counteract the remaining part of the reaction, and this will give the distance of the section, beyond which the result- ant of the forces at the left becomes negative, from the edge of the uniform load at a; thus, 19,466%+3,000=6.49 ft. The distance from R, to the edge of the uniform load is 8 ft. The entire distance to the section of change of sign of the shear is, therefore, 8+ 6.48 = 14.48 ft. from Rj. Shear Diagram.— It is sometimes necessary to plot the shear of the forces acting on a beam in a diagram known as the shear diagram. In order to illustrate how this may be —_1f.-— -—— Renee Bft—|- 3 ft d oe be (a) | Fic. 12 done the beam shown in Fig. 12 (a), the span of which is 12 feet, will be considered. Since the beam is symmetrically loaded, each reaction is equal to one-half the sum of the 400 + 1,200+ 400 2 =1,000 lb. The shear at R; is equal to the reaction, or 1,000 Ib. To plot the diagram, proceed as follows: Draw a line ab to any convenient scale to represent the length of loads; that is, each reaction is equal to 108 MECHANICS the beam, This line will also represent the base, or datum, line of the shearing forces, positive values being laid off above and negative values below the base line. The shear at R, being positive and equal to 1,000 lb., draw from a upwards a vertical line ac equal to 1,000 Ib., according to any convenient scale. From c draw to the same scale as ab a horizontal line cd equal to 3 ft. Ordinates drawn from — —25 ft — 3 ft. Tih —<«érn— B Ua aia ft ii tere | | * g s TD 6852 1b. Z Y, Fic. 13 any point on the line ab to cd will be of equal lengths, show- ing that the shear retains the value of 1,000 lb. from the reaction R; to the first load of 400 lb. At this point the shear is reduced by the load of 400 1b.; therefore, from d, draw downwards a vertical line de of a length corresponding to 400 lb., as shown in the diagram. The shear is then uniform until the central load is reached, and may be represented by the distance of the line ef from MECHANICS 109 the line ab, namely, 600 lb. At this point the shear is reduced by 1,200 lb., shown on the diagram by the line fg, and becomes negative. At the third load, counting from the left, the shear is still further reduced by 400 lb., and is represented by the line 4z in the diagram. From this load on to the right-hand reaction the shear is negative in sign and equal to 1,000 lb. This right-hand reaction drawn from j to b closes the diagram. It may now be seen that to find the shear at any point ina beam it is necessary to draw an ordinate from the corre- sponding point on the line ab and to measure the length of the part included in the shaded diagram with the correct. scale. For instance, if it is desired to ascertain the shear and its sign at the point k, draw a perpendicular line km crossing the shear diagram. The length /m measured by the scale selected for the shear will show that the shear at this point is 600 lb., and, as lm is located below the base line ab, the shear is negative. As a general example, the shear diagram of the beam shown in Fig. 138 may be plotted. As the load here is not symmetrical, it is first mecessary to calculate the reactions R, and Ry. The positive moments about the left-hand end of the beam, in foot-pounds, are: 500X 3= 1500 (1,000 X6)X 8= 48000 200xX 9= 1800 1,000X15= 15000 5,000 X 21=105000 Total, 171300 The total negative moment is R2X25. Therefore, Re =171,300+25=6,852 1b. The sum of the loads is 500 + (1,000 x 6) + 200+ 1,000+5,000 = 12,700 Ib. R, is there- fore equal to 12,700—6,852 =5,848 Ib. The plotting of the shear diagram shown in Fig. 13 may now be started. Draw the line ab equal to the length of the beam; ac equal to R;, or 5,848 lb.; cd, horizontally, equal to 3 ft.; de, vertically downwards, equal to 500 Ib.; and éf, horizontally, equal to 2 ft. From a on ab lay off 9 ft., as 110 MECHANICS at p. The shear at this point, just to the left of the con- centrated load, is +5,848—500—(1,0004)= +1,348 Ib. This value laid off above ab gives the point g. Draw fg. From g lay off vertically downwards 200 1b. to the point h, From a, on the line ab, lay off 11 ft., as at g. The shear at q is +5,848—500— (1,000 x 6)—200= —852 1b. From gq lay off, vertically, 852 lb. to 7, downwards in this case because the shear is negative. Join h and 7. If correctly drawn, hi should be parallel to fg. From 7 draw 7 horizontal and equal to 4 ft.; from 7 draw jk vertically downwards, equal to 1,000 lb.; from k& draw kl horizontally, equal to 6 ft.; from / draw lm vertically downwards, equal to 5,000 Ib.; and from m draw mn horizontally, equal to 4 ft. Then, if the diagram is correctly constructed, bn should be vertical and equal to Ro, or 6,852 1b. Then acde...mnb is the shear diagram, and ordinates drawn from any point on ab across the diagram will, when measured by the proper scale, indi- cate the shear at that section, which is positive if above the line ab and negative if below it. BENDING MOMENTS In order to illustrate the method of calculating the bend- ing moment, or the moment of a force that tends to bend a beam, the beam shown in Fig. 14 will be considered. At the point a is a joint, or hinge. It is evident that when loads w Pie | 1 ee ase —— saree mat Re Fic. 14 are applied, as shown by the arrows, the beam will bend at the joint and take the position indicated by the dotted lines; or, to be more exact, will bend still farther until it falls off the supports entirely. The loads and reactions (and weight of the beam itself, if this is considered) are what cause the beam to bend. Con- MECHANICS 111 sidering the portion of the beam to the left of the joint, this portion moves clockwise, and the moment that moves it is therefore positive. The magnitude of the moment tending to move the left-hand part of the beam is R,l—Wh, since the load W acts in the opposite direction to R,. It will thus be seen that no matter in what part of the beam the joint a is placed, the beam will collapse. There- fore, it is evident that in any beam carrying loads, these loads and the reactions exert a moment at any transverse section that tends to bend the beam. It is only on account of its own strength that a beam does not break. A beam is therefore designed to withstand the bending moment of the forces acting on it, and for this reason the engineer must at all times be able to find this moment. With a simple beam the bending moment (considering, as usual, the part to the left of the section) is always positive, while with cantilever beams it is negative. ee oft: 3ft---+-—6ft.—_— 00 lb. per ft. $ 3 6 24 ft. R, R2 Pre 15 As an illustration, the bending moment around various sections of the beam shown in Fig. 15 will be considered. It is of course first necessary to find the reactions, so that the moments may be calculated. To find Re, take moments about R;. The positive moments, in foot-pounds, are 1,000X3= 3600 (800 X9)xX103= 75600 2,000X18= 36000 Total; 115200 The span is 24 ft. Therefore, Ro=115,200 +24 =4,800 Ib. The sum of the loads is 1,200+ (800 X 9) +2 000 = 10,400 Ib. Therefore, R; = 10,400 — 4,800 = 5,600 lb The bending moment at any section of the beam may now ‘be found. For example, find the bending moment around 112 MECHANICS point a directly under the first load. The moment here, on the left-hand part of the beam, is R,xX3 = 5,600X3 = 16,800 ft.-lb. f Then find the moment on the left-hand portion of the beam around point b. Here the positive moment is R, x 104, or 5,600 X 104 = 58,800 ft.-lb. There are, however, two neg- ative moments acting, and these must be subtracted from the positive moment in order to get the resultant moment. One of these moments is that due to the concentrated load of 1,200 1b., and the other is that due to the part of the dis- tributed load to the left of the pointb. The negative moment of the concentrated load is therefore 1,200 X 74 =9,000 ft.-Ib. The portion of the distributed load considered is 800 44} =3,600 lb. Its moment arm may be considered to extend from the point b to the center of the portion under consid- eration, or 44+-2=24ft. Its moment is therefore 3,600 x 24 = —8,100 ft.-lb. The resultant moment of the left-hand section about b is therefore 58,800 —9,000—8,100= + 41,700 ft.-Ib. The bending moment about ¢ is 5,600 18—1,200X15 — (800 X 9) X 74 = 100,800 — 18,000 — 54,000 = + 28,800 ft.-lb. The bending moment of the forces acting on a beam, tending to break it at any section, may be calculated from either end of the beam. It is customary to call the bending moment positive if it tends to turn the left-hand part in the direction of the hands of a clock, and negative if it tends to turn it in the opposite direction. However, the moment may be calculated from either end, remembering that if it is calculated from the right-hand end the bending moment acts in an opposite direction and will therefore receive a sign opposite to that given the left-hand end of the beam. As has been stated, the reason a beam does not break is because its strength at any transverse section is sufficient tc resist the moment of the forces about that section. It has also been shown that the bending moment is different at different points along a beam. It is therefore important to find out around what point the forces acting on a beam exert their maximum moment, and then, by the method already given, to find this maximum moment. MECHANICS 113 The point where the shear on a beam changes sign, that is, changes from positive to negative, or from nega- tive to positive, is the point around which the maximum bending moment occurs. The point where the shear on a cantilever beam changes sign, that is, the point around which the moment is maximum, is always at the point of support. Sometimes, the shear will change from positive to negative or vice versa two or more times on a beam, and each sec- tion, when the shear is zero, must therefore be investigated . to determine around which point the maximum moment occurs. Fig. 16 shows an example of this kind. To solve this example, it is first necessary to find the reactions. The moments of the loads about R;, in foot-pounds, are as follows: 500 2=1000 800X 5=4000 300 x 14=4200 Total, 9200 R2X10 = 9,200 ft.-lb.; R.=9,200+10= 920 1lb.; and Ry = 500+ 800+ 300 — 920 =680 Ib. veri I At R;, the shear is + 680 lb.,and at 2 ft. from the left-hand end the shear changes from +680 to 680—500= +180 Ib. At 5 ft. from the left-hand end, the shear changes from +180 to 180—800= —6201b. This, therefore, is one place where the shear changes sign. Under the reaction Re, the shear changes from —620 to 920—620= +300 Ib., and this is therefore another point where the shear changes sign. There are therefore two places to be investigated for maximum bending moment, one 5 ft. from the left-hand end and the other 10 ft. from the left-hand end. The bending moment about the point 5 ft. from the left-hand end is 114 MECHANICS 680 X 5—500 X3=+1,900 ft.-lb., and that about the point . 10 ft. from the left-hand end is 680 10—500 X8—800X5 = —1,200 ft.-lb. It is thus seen that the greater of the two maximum bending moments occurs about the point 5 ft. from the left-hand end. | Bending-Moment Diagrams.— The bending moments that act at various points of a loaded beam may be repre- sented graphically in the same manner in which the shear- ing forces were shown. For example, a beam 50 ft. long s » i) $ S ~- SW, W. = 1 s 2 ~ ~) A . S ) ~ ~ ) 3 : ~ bo) ~ " t) o te < zi ———-~------ Pus. 17 supports two concentrated loads of the magnitudes and in the positions indicated in Fig. 17. Now, assuming that Fig. 17 (a) is drawn to scale, draw the horizontal line ab and produce the lines indicating the reactions and concentrated loads until they intersect line ab at a, c,d, and b. By cal- culating the moments about the left-hand reaction, the moment for the load W, is found to be 10,000 X 10= 100,000 ft.-lb. and that for We, 6,000 25=150,000 ft.-lb. The 100,000 X 150,000 reaction Rp» is therefore 50 =5,000 lb., and reaction R; is 10,000 +6,000 — 5,000 = 11,000 Ib. MECHANICS 115 The bending moment at W; is 11,000 X 10 =110,000 ft.-lb., and that at We is (11,000 « 25) — (10,000 x 15) = 125,000 ft.-Ib. Lay off the line cc; to any convenient scale to represent the bending moment at W,, and at dd; to represent that at We. Connect points a, c,, dj, and b, as shown, and the dia- gram is complete. As another illustration, assume that it is desired to plot the bending-moment diagram of the beam shown in Fig. 18. This beam is 50 ft. long and has a uniform load of 1,000 lb. per running ft. First, divide the beam into any number of smaller parts, each, for instance, 10 ft. long, and then find the bending = LY — R,=25000 Lb. moment for each of these parts. In this instance, the reactions R; and Rp» are each equal to one-half the total load, or 50,000+2=25,000 lb. The bending moment at c is (25,000 X 10) — (1,000 X 10 * 5) = 200,000 ft.-lb.; at d it is (25,000 X 20) — (1,000 X 20 X 10) = 300,000 ft.-lb. Inasimilar manner, it will be found that the bending moments at points e and f are 300,000 and 200,000 ft.-lb., respectively. On laying off these bending moments at ¢)C2, d,do, etc. and " connecting points a,c)... b, the diagram is complete. The FORMULAS FOR MAXIMUM SHEAR AND BENDING MOMENTS ON BEAMS : Maximum | Maximum Case Method of Loading Shear Moment —— J ——__— I i w| Ww Wl wi II Ww <2 \ Wasi net Il = at 3 S wy 2W1 3 wi Vv Ww. ep VI \ “dln = WwW we VII © i ALR eg Ae Fe eae id ue eon, ae ; ; roe bs Watches Sees ape PE a ee Pe ee x | et ony = “ a, — : ; 116 TABLE—(Continued) | Maximum Case | Method af Loading a ‘a. @ 2 8 XII “ a XI b a ud - as Ww : 2 52W1 XIV = “405 w XV i HW Wi a ae | =e EE Ys sw aw N - ‘ 4 5 NS Ww Wl cibad Ni % = oy ie XVIII XIX xX 117 118 | MECH ANICS outline of this diagram, however, is only approximately cor- rect. To find its true form, the beam should be divided into an infinite number of parts, in which case the lines acy, c,d}, dé, 171, and 7;b would be parts of a curve, shown dotted, instead of a series of short, broken lines. MOMENT TABLES The methods of finding the shear and maximum moment occurring in simple and in cantilever beams have been explained. In these calculations the weight of the beam itself, if of wood or steel, is often omitted. The various unusual loadings were also considered, and the method of finding the maximum bending moment was explained. These methods will be found usefiil if such cases ever arise. However, in practice the loads on the beams are often more uniform, and if the weight of the beam itself is neglected, the formulas given in the accompanying table may be used. Beams with fixed ends or even with one end fixed and one simply supported are also given in the table. In each case in the table, the total load on the beam, in pounds, is denoted by W. If there are two separate and WwW equal loads on the beam, each one is called 4) so as to make the total load W. If the load is uniformly distributed over the entire length of the beam, the load per foot will be W +length of beam, in feet. The length of the beam is denoted by/. If J is taken in inches, the moment will be in inch-pounds; but if taken in feet, the moment will be in foot-pounds. The usual method of indicating loading is adopted. A simple support under a beam is shown by the conventional arrow, while a cantilever or a beam fixed at the ends is shown as in Case I or XVII, respectively. Cases XV and XVI indicate a beam fixed at one end and supported at the other. The maximum shear on a cantilever or on a beam fixed at the end depends somewhat on the method of holding it in the wall and the length that extends into the wall. How- ever, the maximum shears given in the table are correct MECHANICS «119 for usual cases. In Case XX, two values are given fér both shear and bending moment, and the maximum of the two values obtained must be the one used. The sign of the shears or bending moments has not been put in the table, but it can be told by inspection whether they are positive or negative, as every-day experience should enable the engi- neer to determine whether the loads will bend the beam up or down. The point of maximum shear is marked on the beam at the point a, while maximum bending moment is at the REACTIONS FOR CONTINUOUS BEAMS OVER EQUAL SPANS (Coefficients of W) Num- Number of Each Support Spans ah 2d | 3d! 4th} 5th eth | 7th| 8th| 9th| 10th 2 % | 4e) # 3 vo | 33 | 46 | ws 4 33 | 38 | 38 | | 38 5 48 | 43 | 34 | 34 | 43 | 3 6 | tor 43d /482| 18F| 402 | 108 | woe (Moc rabcraberabesabcsabeeabe sibs y3 8 | 385/443 |558| 388 | 338 | F848 | HS | 398 | 388 9 580 $30) $86 355/348 | 345 | $38| 343| $93) 33 = point b. In some cases, either of these values may reach its maximum at two or more places, in which case it is so marked. The following example will serve to show the use of the table: ExaAMPLE.—A simple beam on a span of 13 ft. 24 in. carries a uniformly distributed load of 85 lb. per ft. What is the maximum shear and the maximum bending moment devel- oped? 120 MECHANICS *SoLuTION.—The length of the beam, reduced to feet, is 13.2083. The total load W is therefore 85 13.2083 =1,122.7055, say 1,123 lb. Referring to Case XI, the max- W 1123 imum shear = A a =561.51lb. Likewise, the maximum bending moment is wl 43 1,123 X 13.2083 8 8 = 1,854,115, say 1,854, ft.-Ib. CONTINUOUS BEAMS When a single beam extends over three or more supports ‘it is said to be continuous. The bending moments produced are very different from those in an ordinary beam. For this reason, the treatment of this class of beams must be con- sidered separately. BENDING MOMENTS FOR CONTINUOUS BEAMS OVER EQUAL SPANS (Coefficients of W1) saa: Number of Each Support ber of Spans! 1<¢ | 2d | 3d | 4th! 5th| 6th| 7th| sth| 9th| 10th 2 0 |4/)0 3 0 \zvo\rs| 0 4 | 0 | ds \as| Hs | 0 5 0 | as \se| ds | as | 0 6 0 |Yor|\rer|roq|1eq|fox| 0 7 | 0 |site rede] ree || ave |r| 0 g | 0 | atelaite| aie |aie| aie | atte) ates 0 9 O | sehr state | seo | sAe'o | so | sto | s*z#o| sao) 0 The first of the tables, on page 119, gives the coefficients for the reactions of the beam at its supports. The value given in the table multiplied by W, which represents the load per span, will give the reaction. By knowing the reactions STRESSES AND STRAINS 121 and the loads per foot, the shear at any section may be found. The coefficient from the second table multiplied by WI, which represents the load per span and the length of span, will give the negative bending moment over each support. As the maximum moment occurs over a support, it is seen, by referring to the table, where this moment will be. If the coefficient given in this table is multiplied by the load in pounds and the span in feet, the result will be in foot-pounds; but if the span is taken in inches, the result will be in inch- pounds. To illustrate the method of using the tables, the following example will be assumed: EXxaMPLE.—A beam of three spans is supported by four reactions. Each span is 11 ft. The beam carries a load of 2,000 lb. per ft. (a) What will be the amount of the end reactions? (b) What is the greatest bending moment pro- duced? SoLuT:on.—(a) The load W supported by each span is 2,000 X 11=22,000 lb. From the first table, the reaction at each end support is equal to y45 W. Substituting these values, the reaction at each end is equal to 39% 22,000 ==8,800 lb. (b) The greatest bending moment occurs at the inter- mediate supports; from the second table, this moment is equal to yy WI, or yp X 22,00 X 11 = 24,200 ft.-Ib. STRESSES AND STRAINS STRESS It is evident that the weight of the materials composing a building and its contents produces forces that must be resisted by the different members of the structure. The action of these forces has a tendency to change the relative position of the particles composing the members, and this tendency is, in turn, resisted by the cohesive force in the materials, which acts to hold the particles together. The internal resistance with which the force of cohesion opposes the tendency of an external force to change the relative position of the particles of any body subjected to a load is called a stress; or, stress may be defined as the load 122 STRESSES AND STRAINS that produces an alteration in the form of a body, and this alteration of form is called the strain. — In accordance with the direction in which the forces act with reference to a body, the stress produced may be either tensile, compressive, or shearing. Tenstle stress is the effect produced when the external forces act in sucha direction that they tend to stretch a body. Compressive stress is the effect produced when the tendency of the forces is to compress the body. Shearing stress is when the forces act so as to produce a tendency for the particles in one section of a body to slide over the particles of the adjacent section. When a beam is loaded in such a manner that there is in it a tendency to bend, it is subjected to a bending stress. In this case, there is a combination of the three stresses already mentioned (tension, compression, and shear) in different parts of the beam. The unit stress (called, also, the imtensity of stress) is the name given to the stress per unit of area; or, it is the total stress in a tie-rod, column, or the like divided by the area of the cross-section. Let P represent the total stress, in pounds; A, the area of cross-section, in square inches; and s, the unit stress, in pounds per square inch. Then, P om FOF P=As STRAIN When a body is stretched, shortened, or in any way — » deformed through the action of a force, the deformation is called a strain. Thus, if a rod were elongated + in. by a load of 1,000 1b., the strain would be yy in. Within certain limits, to be given hereafter, strains are proportional to the ~ stresses producing them. Unit strain is the strain per unit of length or of area, but is usually taken per unit of length and called, for tension, the elongation per unit of length. If the unit of length is taken as 1 in., the unit strain is equal to the total strain divided by the length of the body in inches. STRESSES AND STRAINS 123 Let / represent the length of the body, in inches; e, the ' deformation, in inches; and gq, the unit strain. Then, e q=7, OF e=lq ELASTIC PROPERTIES It can be proved by experiment that when a certain unit stress is created in a substance, a certain definite unit strain is developed. If the unit stress is doubled, it will be found that the unit strain also has doubled; that is, the alteration of shape or the strain in a body is proportional to the force applied to that body. This experimental fact is known as Hooke’s law. When a certain stress is created in a body a certain strain is produced. When the stress is removed, the body returns to its original shape, provided the unit stress has not been too great. For each substance, however, there is a certain maximum unit stress that the substance will stand and still return to its originai shape after the external forces are removed. This unit stress is called the elastic limit of the material. If a body is strained beyond the elastic limit, it will maintain a permanent distortion, or set, even after the strain forces are removed. Hooke’s law, which is almost exact for most materials below the elastic limit, does not hold good for these materials above the elastic limit, as the strain increases much more rapidly than the stress. Thus, if the unit stress is doubled beyond the elastic limit, the unit strain will be more than doubled. The unit stress that is so great that the strain increases greatly with very little increment of stress is called the yield point. For all prac- tical purposes, with many materials the yield point com- mences at the elastic limit. To restate Hooke’s law, the ratio of the unit stress to the unit strain for any substance is constant below the elastic limit. This ratio of unit stress to unit strain is called the modulus of elasticity, or coefficient of elasticity, which will be represented by the symbol E. It is Ss E=- q 124 STRESSES AND STRAINS From this equation, when s and E are known, g may be found; that is, if the modulus of elasticity of a certain sub- stance and the unit stress are known, the unit strain can readily be found. STRENGTH OF BUILDING MATERIALS The ultimate strength of any material is that unit stress which is just sufficient to break it. The ultimate elongation is the total elongation produced - in a unit of length of the material by a unit stress equal to the ultimate strength of the material. The modulus of rupture differs from the ultimate tensile or compressive stress, but is a quantity, something like it, that is used in calculating the strength of beams. Its use is discussed under the heading Homogeneous Beanis. ; FACTOR OF SAFETY A value that is taken for the ultimate strength of any material is an average value of a number of experiments made on the material. As it is impossible to get two sam- ples of the same material exactly alike, so is it also impos- sible to get two samples with the same ultimate strength. It is therefore customary in design to avoid stressing a material up to its ultimate strength or even up to its elastic limit. The factor of safety, or, as it is sometimes called, the safety factor, is the ratio of the ultimate strength of the material to the load that, under usual conditions, the material is called on to carry. Suppose that the load required to rupture a piece of steel is 5,000 lb., and that the load it is called on to carry is 1,000 lb.; then, the factor of safety may be obtained by dividing the 5,000 lb. by the 1,000 Ib. Thus, 5,000+1,000=5, which is the factor of safety of this material. Another factor to be considered in selecting materials is deterioration, which is due to various causes. In metals, there is corrosion on account of moisture and gases in the atmosphere. Wood is subject to decay from either dry or wet rot, caused by local conditions; it may, like iron and steel, be STRESSES AND STRAINS 125 subjected to fatigue, produced by constant stress due to the load it may have to sustain. The preceding reasons are sufficient to require the factors now adopted by conservative constructors in all engineering work. These factors are 3 to 5 for structural steel, and 6 to 10 for cast iron. Stone and brick are very unreliable and a high factor of safety should therefore be used. Usually, the factors employed are 10 for compressive stresses, 15 for tensile stresses, and from 10 to 20 for bending stresses. Some engineers, however, do not use such high factors. Stone- work or brickwork is even more unreliable than stone or brick themselves, but the same factors are often employed. Usually, however, the strengths of stonework and brickwork, instead of being given as ultimate strength, are arranged in tables to give the safe, or allowable, stress per square inch or per square foot. This value embodies its own factor of safety. Concrete is another material that sometimes requires a high factor of safety. In reinforced-concrete work a factor varying from 4 to 6 is usually employed, although some engineers use a higher one. Ordinances in various cities throughout the country govern the allowable load that building materials should carry. A structure withstanding shocks or containing rapidly vibrating machinery is more liable to fail than one in which the loads are quiet, even if the latter has the greater loads. Therefore, in designing a structure to withstand vibrating loads or shocks, the designer, to make the structure safe, uses a larger factor of safety. Usually, this factor averages from two to three times the ordinary factors, except those for timber, which need not as a rule be increased. The average ultimate strength of various metals and woods are given in the accompanying tables. STRESSES AND STRAINS 126 000'000‘8T 000'0T | 000‘09 rsrttss**payveuueun ‘orp raddog 000‘000‘ST 000‘9¢ iA * (Buryeoyos 4q - pauaajos) peyeouue ‘aim Iaddog 000°000'0T | 000‘ZZ | 000‘0E | 000'9 000'F% (000° ‘OF) "4880 ‘1oddoj ‘ : 000‘0¢ 0000 Pas ae aK '3 **s3JOq, ‘reddo5 000 009'% 000‘0OF 000‘99 ee uIqo ‘ezuolg 000 000 FI 000'FZ 000‘0S ee ee ee ee *roydsoy ezuoilg ES ve 000°08 | 000‘09 000‘0ZT * ‘esouvsuBUl ‘ezuolg 000°000 OT | 000'S¢ 000°0T | 000‘%E (000°02) "rts" Teqour uns ‘ezuorg 000°¢2 000'0ZT veeese sess uInUTUMe ‘azuorg ~ 000‘000‘FT OO0'GTn BOO Oe. 4 — me.. fet Cras sees --poyeouuedn ‘QIIM SSPIg 000‘0¢ coe ween see ee * (Burwoyos Aq pauasjos) peyeouue ‘oirm sseig 000°000°6 | 000'0Z | 000‘98 | 000‘9 000'bZ (00008) ee ‘sselg /4aGg0 pun ‘azuorg ‘ssvag 000‘'22 000‘0F ee ee ee a es jexoru ‘umnurWn{y 000°000'TT 000‘ZT | 00¢'9 000°ST 000‘ZT ***Teposeuruto0o *‘wnUTWnyy SmnutMmn) yp ‘ a ploryselq -dn sur quit uors jo snnpoy | jo oer -reayg sae BosUeL | -soidw05 -npoyw HONI FUVNOS UAd SANNOd NI ‘SIVLAW AO SHLONAUNIS ALVWILIN ANVUAAV 127 STRESSES AND STRAINS *sqisuo] [eulst1o UL woTONpes %oT Buronposd spor ozeoIpul sosayqjuaied uy pasojoue senjea uolssoiduoy) —HLON 000'000'ET 000'000'F 900‘000‘08 000‘000'08 000‘000‘08 000‘0006z 000‘000'6z 000‘000'6Z 000‘000'08 000'000'T 000'000'9z 000000'2Z 000‘000‘Sz 000‘000'ST 000°000'ZT 000‘09 000°FS 000‘02 000'8F 000'F 000‘0F 000‘08 000‘0¢ 000'8% 000°09 000‘0F 000‘0F 000'8T 000°9 000'¢ o0g's 000'F9 000‘'9¢ 000'02 009'T 000° 000'0¢ 000‘¢E 000'ST (000‘02) (000‘9) 000‘F9 000'8F 000‘9F 000‘08 "ey oak ee eS ee eye sissies is eaeD ‘QUIZ “- phat Si ger ary 0 Soe) Cae AE ASO UL FT ‘9uLZ pun UL] ae pestoduiey [etoods ‘allm [904¢ ‘sespiiq uorsuadsns J0j ‘alta [9041S See gE AE giqionsd ‘asim Je01S " peyeouueun ‘QIIM [9039S * (Buryvayer ‘sq pansies) peyeouue ‘OIIM 19938 ere maria es wnt peu ‘jeanjons3s ‘1994S Jp ato “30s ‘TeanjonJ4s ‘1993S *SBUIYSED ‘[904G a4 4nqmndy D ISDI 4 > ne id peor ; ‘"4sBo ‘peay ipoay] phase “sieq paljored ‘qysno1m ‘dOd] ae ‘sodeys ‘yysnoim ‘UOosy "* pelsouusun ‘aIIM UOIT * (Buyyvoyar 4q pouaisos) peeouue ‘oJIM UOIT “payesns10 ‘uol] “sureyo wos] v4 *yseo ‘UOlT STRESSES AND STRAINS 128 v v a 9 P ¢ c OL jen nepali a inate cee Ayoyes Jo 104,0e J 000'00Z'T |000°S 1 ie ASP WERE | MATS sae idee ctitt sonids vrusoyiyeg __ | 00% | 000'00Z - |00S'F | 009 | 000‘F rE tee Eh eS Ng "poompes wrusOsITeD 000.2 | 009 | 000 000 T 000°¢ | 006 | 000‘F 00¢‘s8 "ynuysey9 00¢‘T | OOF | 000'00Z |000'F| 002 | O0S‘E | nOS‘¢ 000'2 “sepa P 000 006 000 ¢ 002 000 ¥ 000‘¢ 000‘9 | ssor &9 00g 3 | OgE | 000006 009 | 009 | 000'F 000‘9 * *yOTUIE 000 € | 00% | 000.002 T 000% | 00L | 000% | a00‘9}00¢ | 000'8 |": it ea ue sonidg 000 0€T T |000 ¢ | 008 000'F 000‘'¢ | 00¢ | 000'8 |°**(euld AemsIon) ould pay 000°F | 00% | 000002 T |000'9 | 000'T| COS'F | 000‘9}00¢ | 0006 |" ** ‘auld MOTeA Jee|-3104S : 00¢ | 000:00F'T |000'S| 008 | 00S'F | OOL‘S 000'S. }°°"." “ay sepsnoqd 000‘¢ | 009 | 000‘00S‘1 |000‘Z | OOFT| O00'S | 000'2| 009 | OD0'ZT | °° *” ‘guid eIB aoe “1095 3 io Jeor- -Bu0] uleyynog 000'Z | 00% | 000‘000'T |000‘F |o0z | 003'E | oog‘s| 00g | 0002 ‘guid azIy 000'F | 008 | G00'00S'T |000'Z | 000‘Z| 000‘E | QDD‘Z | 000‘ | 000‘ZT "#80 OUI 8aoa > ry > [B45 o| @ > P| 3) we |Su| 2 Bezel ge | § | < ¢ ad AS 84/98 lsy38) 2a | & S & Q ba oat 1a Dep - a ~ QO | 3 Gf | sa] o |--= Oo | 9 a 5 So go| 3 3 2 Joquiny, JO pury iy tie a 5B | CUBIS UM 3 8 suLeeyg @SIOASUBLL, uotsserduros uorsuay, HONI @AVNOS Ad SANNOd NI ‘SOOM JO SHIONAUIS ALVWILTIO ANVAAAV HOMOGENEOUS BEAMS 129 HOMOGENEOUS BEAMS PROPERTIES OF SECTIONS MOMENT OF INERTIA The strength and the stiffness of a beam depend on vari- ous factors. For instance, the load that a beam can bear depends on the material of the beam, on the manner in which the load is applied, and on the length and cross-section of the beam. As to the area of the cross-section, the strength does not depend on that area itself, because, as every-day experience shows, a plank used as a beam will sustain a greater load when placed edgewise than when placed on its broad side, although it has the same area in both cases. The strength of a beam depends on the manner in which the area is distributed or disposed with respect to the neutral axis of the cross-section. The effect of the cross-section is measured by a quantity that depends on such disposition or distribution of area, and is called the moment of inertia of the cross-section with respect to the neutral axis. The moment of inertia of a plane figure has really nothing to do with the property of matter known as inertia, and as here used it is simply the name for a certain constant depending on the shape of the cross-section of a beam. It is not a moment as the word is generally understood, and it might have been called anything so far as the structural engineer is concerned, but it has received its name from some relations in higher mathematics where it is derived. This quantity must be considered simply as a constant that has been found suitable for use in certain formulas for the design of beams, which will be explained later. The following table, entitled Elements of Usual Sections, contains, in the column marked J, the moments of inertia of the shapes of beam sections commonly used in practice. The axis in each case passes through the center of gravity, and is designated neutral axis in the table for reasons that will be explained later. The square may be regarded as a . £ oe ZY oe’ I; —-= 97 pees ve Soren a 2 £ taeaean Pp ePq 2P 9 g—p=9 eee Pq pz zi Zn 9 zi é v 6g = = pg = D p lott = == 2 zD ete D9 ZI Fos : aoa Y yD — 5p yo — p Che 4 Sasse ZIKn 9 zi z Yj D 6gz° = = es p Dp = =2 zo by ss I 19 puv 2 7N va as nae u0}}09¢g Jo V I 77*% so 3 or So]}!U101}xq 0} | uUOT}OEg u01}0eg UOdeIAD Jo sninpoyy uonoeg | nasa] sIxy [e1jnoN | jo Bory snipey jo JUSTO |W WIOIy s0ueysIG SNOILOGS IvaSN dO SINAWATH 130 Pp 6bo° = ps l= ; ep goo = |" 99 == 2 eo: £ pP Pp zp a v UIs g + ZI \ ae es (o zUIS 29 + z 901829 +02 809zP] » Soop 9 ° |wgs00¢7)—| 2 FIS 2 + 7800p Pq x » 2800 ire Pq —™ (cP + 29)9 cP+cfn9 | (cP +29)9| e+ e%r oa Pg aP 29 P 2 1 ('p 19 — p qg)zt ?9 z1 z “a= peN p—sP9 |pa—epa PS ia ae ee cole 9 ZI 2 a py cP eP 9 pe re 131 b ze ¢? 7 So" = Pg S34 = Ps gP 9 900° = i) <= v , eP Qu P PQu p bzo* =! 4 . a Z ZI ° a! p 400° ve 6° = CCI ce F- = (b — » £)z61 J uzSi't pip — ult =2 | 2? 8 9 — gu On Seeger ph PE orn t 2p it 9— zt ¥9 — zu 6 pez = -- = 19 eP u p ) Ip — 60° = Ip— 6¢o’ = (z P zP) : Pp (s Sy 8 (51? %) 0 eae Sgt = Pp —yP) a , k (c'P — ¢P)4 12 pue 2 = =4 Le sIxy e Gage N Ores ao V re) Ipey 1309 is 1x nON jO Bol S| jo juomojW WO.Ly] e1sIq Vv (panuyuo))—SNOILOGS TVOASA dO SINANATI a oa— s9V — 9—-qQ= J; “+4 e pas mite (?—9)4 —- Ut e952 [ety ts eee PQ [(? — 9)¥ — Pa\erN 6 - : ? eee ne ett See = es —9)4¥— x a | of Y + 9 Sz of U + 99 Sz is P4 (2 — ¢)¥ — paler Brees = a P9 (7 — 9) Z se e\e & coud pas (7 = @)e% — eP 9 da ee aris 34 — ¢P@ PX PX Saas dix we 19 +19 gh (1g + 9)9 . g pga Si A (2'9 + *99 + 29)ey 2 = 009 es te JA (19 + g)oe P ae PX gag if t an 2'g + 99" + 0@ z'g+ 'ggh+ 29 ae Gceae” (Stg+2y+sgQ)e_ reer e(S — 9) (2 — 19) Vere [ (6—2)(9—19) ~ FAG (Stg+ay+sQgje . ] 7 el = 1) 9— 9)— C= Pe) G="a)e 1u+89 a(S — 9) (7—9)— Pa+e9 eld + 279 | lair yi £ (Quy +sq)e 19 —p se—D)G—0) | pee P=) (7 —9)— war IN kB ‘ Baaereee Ne ea e99+_7 . rat [= 9s + P7ley P9 G9 * eae (2 — 9)s+ (7 — 9)eS + oP? | (?— 9)eS + ¢P? eI P Pi eS + ¢P? T 12 puev 2 Lit so W01}09¢ Jo V 7 7 jana wrtent eniecesel 0} | uonsag m0}}00g cope: 10 snipe [eunpoyeuonoas| MOSY.emoet | "Sy winaay” | Jo Sony (panuz7“0))—SNOILOAS TVOSN dO SINAWATA HOMOGENEOUS BEAMS 135 particular case of a rectangle whose base b and altitude d are equal. The value of the area A is given in the second column. The distance c, given in the third column, is the dis- tance of the most remote part of the figure from the neutral axis. The section modulus and radius of gyration, the character of which will be explained later, are given in the last two columns. EXxAMPLE.—What is the area, the distance from the neutral axis to the extremities of the section, and the moment of inertia about the neutral axis of the section illustrated in Fig. 1? SoLuTion.—Referring to the table, it will be seen that }; =4 in., b>=104 in., andd=7in. Therefore, the area is b+b, en un Sent 2 Likewise, the distance from the neutral axis to the longer parallel side is b+2b,'d 10.5+2X4 7 = X -—=2.977 in. Oth Ss WOSME- 8 , The distance c, which is the distance of the neutral axis from the shorter parallel side, is b+2b d 44+2X10.5 7 — X—=4.023 in. eet 8 1 eee S As a check, c; +c should equal d, or 7in.; thus 2.977+ 4.023 =7.000 in., which indicates that the preceding solution is correct. ‘The moment of inertia is found by the formula __6?+,4bb; +b;? 36 (b+5;) Substituting values for the letters in this formula, 10.5°+4X10.5X4+4 = X 73 =193.348 36 X (10.5 + 4) In general, it one of the values of ¢ and ¢; is found by means of the formula, the other may be found by subtracting the Bicod = 50.75 sq. in. ye or =) > — —+ e . s+ a9 e uit es (R+5)(@-9)+ oss na Oe Te eed ve oa > S+7)7 [ Gre ) (4¥—P)at Roe aY¥ —P)?+(¥— Pee gi eI y+| Stic + Bis ee ‘ He teale? | eh vl vf PQ (72 + Hee —@%) . 2% : ae one + Pa i CE Q)E og, 79+ (M+ '92)2 as e(? = 9) (?— 9) 2 9 +22 — 2)? (Ge TD)E He hs G— aE go +(9 + wey e Gm Use A e(? —9)(? —P)— 990+ ¢(2—2)2 gf —7D+_0 U2 €)8 a 19 pue 2 ‘u0I1}09g Jo O¥g O . i sixy seiiaae jo JuoWO WW Ls aoa oomasiiel Y *eesy TO}}08$ SIXY [B1]NON Wolg souej}sIq SNOILOUS CATION CUVANVIS WHOA SHATVA 126 ge [27 + 97) + ee 4 +=, 4+ 275 + c + 1) pnexy fo vI4LVer i (ae je Gest Oh W[(22 —2 a? rs (A= 2) = te) t — 1/2 eden sae =22)] »zsoo £ vp UIs ,J — 9 S007 a= OF = 2) ee? al — 2 )F £ WA tee aed dame — yz » 9[3UY 94} 9OJMJ, Jo JUSSUL,], Fea * 4-1/4 SIXV ‘elj10euy Jo JUOWO;, ig “eiyJouy ‘ uo1j09 be S 8 ri a[(2 — 2)2 + 9) zi e(7@ — 9)!” — 9Q0 V9 In — 9) — Iu + s)t alt | (2 — PE)(? oe —ypuet heen’ yb Bote tee GEF WH sge+("—gst Cee Oe 4 poet SLM | 7 9) + Ti a Wl —+4 3P@ (2 )se +2 stk a © pus.? “woRIS vy ‘Bory u01}08g I JO ¥Oug 0} S[xy [e1JNON Woig 99uK}sIq a-4 SIX ‘BIJ19U] Jo UOMO, (panuzj“0)-SNOILOAS’ CATION GUVANVIS YOA SANTIVA YP lace fh »zsoo zi (7 — gP) (eg —79) p gulls 7 — v ,809 ,/ ler "9 + ef + OT PPI mn [2(72 + "2)2 + el? a TE — 27 9 [ve + geyrzgesqut CL e712 + ¢'2'15 + 995 882 ZI 9 eae ST ae , Thm S12 L » O[SUY OY} SIM JO JOBUBL | ehiouy jo juowow | 4-, sixy ‘epiouyjojweuoy =| FHS % 140 HOMOGENEOUS BEAMS known one from d. Thus, after having calculated c; in this example, c would be equal to d—cy =7—2.977 =4.023 in., which value corresponds to the one found by means of the formula. Many of the beams used in building construction are made of steel. These steel beams are rolled with various cross- sectional shapes, from which they derive their names. These shapes are standard; that is, they are rolled to con- form to certain sizes that have been adopted by many of the large steel companies. In the first column of the accom- panying table, entitled Values for Standard Rolled Sections, are shown the cross-sections of the various structural shapes. The first section shown is known as an angle with equal legs; the second, as an angle with unequal legs; the third, as a channel; the fourth, as a bulb beam; while the fifth, sixth, and seventh sections are known, respectively, as anI beam, a T bar, and a Z bar. In this table is given the moment of inertia for each sec- tion about at least two axes, both of which pass through the center of gravity of the section; that is, the moments of inertia are given always with respect to neutral axes. The moments of inertia with respect to different neutral axes are, in general, different, and as a rule there is one neutral axis about which the moment of inertia is less than it is about any other. With the channel, bulb beam, I beam, and T bar, the smallest moment of inertia is about the axis y’—y’, or the vertical axis. However, with both styles of angles and with the Z bar, there is another moment of inertia about a neu- tral axis, not horizontal nor vertical, that is smaller than the moment of inertia about any other neutral axis; that is, in certain work, more particularly in the design of columns, it is necessary to know about what neutral axis the moment of inertia will be smallest. It is also necessary to know what this moment of inertia will be. Therefore, in the section of the angle with equal legs, the section of the angle with unequal legs, and the Z-bar section, the moment of inertia is also given for the oblique axis giving the smallest moment of inertia. The position of this neutral axis is found by higher mathematics. With the angle with equal legs, this 3) elle HOMOGENEOUS BEAMS 141 oblique neutral axis y’-y’ makes an angle of 45° with the horizontal. With the angle section with unequal legs and with the Z-bar section, this oblique neutral axis y’—y” makes an angle a with a vertical line. Instead of giving this angle direct, it is more convenient to give a value for the trigono- metric tangent of twice the angle, and this is done in the last column of the table. The formulas given in the table are long and difficult to use. The values of the properties of various structural- steel sections have therefore been calculated for all the standard sizes of angles, channels, etc. that are ordinarily manufactured. The tables containing these values will be found on page 147, where their use will be explained. In the two tables just given, the moment of inertia is taken about the neutral axis. Sometimes, however, it is desirable to find the moment of inertia of the section about some axis other than the neutral axis. This may be accom- plished as follows: Let A represent the area of any section; J, the moment of inertia with respect to an axis through the center of grav- ity of the section; Ix, the moment of inertia with respect to any other axis parallel to the former; and », the distance ' between axes. Then, Ix=I+Ap? EXxAMPLE.—Determine the moment of inertia of a triangle with respect to its base (see fourth section of the table entitled Elements of Usual Sections). SoLuTIon.—The distance between the base and the neutral axis c, is 4 d, the area is 4 bd, and J=y, bd. Then, by the preceding formula, bd? bd? ba = 2=—_ — ae Ix= 95 bd? +4 bd X (4 d) a6 Tame Many sections may be regarded as built up of simpler parts; they are called compound sections. For example, a hollow square consists of a large square and a smaller square; the T shown in the table entitled Elements of Usual Sections consists of two slender rectangles, one horizontal and one - vertical. 142 HOMOGENEOUS BEAMS The moment of inertia of a compound section with respect to any axis may be found by adding, algebraically, the moments of inertia, with respect to the same axis, of the component parts of the figure. - ExaMPLE.—Find the moment of inertia of the Z bars shown in Fig. 2, about the neutral axis X’X, the dimensions being as shown. SoLuTION.—The figure may be divided into the three rect- angles efgh, e’f'g'h’, and jgig’. The moment of inertia of efgh about an axis i = 1, through its center of e gravity and parallel to I X'X is yy a'f; that of - t+ e’f'g'h’ about an axis through its center of — gravity and parallel to X'X is also yy a’. The distance between this Lt gt! = axis and the X’X axis be e is 4 (b—2. The mo- ment of inertia of the rectangle efgh and also Fic. 2 of the rectangle e’}’g’h! ; about the axis X’X is then, 7 a’f#+a’t [4 (0—f)]?. The moment of inertia of the rectangle jgig’ about the axis X’X is 7 tb?. The moment of inertia of the entire figure is, therefore, 2{ rr a’+a't[t (b—OP} +r 8 Expanding and reducing this expression, ab3— a’ (b — 2t)8 oh => 2 . + - | | HE | | | > | | | | x Sear &, sf-- y T= RADIUS OF GYRATION The radius of gyration of a section with respect to an axis is a quantity whose square multiplied by the area of the section is equal to the moment of inertia of the section with respect to the same axis. If 7 and J denote, respectively, _HOMOGENEOUS BEAMS 143 the radius of gyration and the moment of inertia of a sec- tion, and A the area in square inches, then, Arz=T, fi h =< [— whence rT y A The last column of the table entitled Elements of Usual Sections gives radii of gyration corresponding to the mo- ments of inertia given in the fourth column. The radius of gyration of a section, or figure, may be found directly from its moment of inertia by means of the formula just given. For example, the radii of gyration for the rectangle and the hollow square in the table just referred to are found as follows: For the rectangle, r= Vib bd? + bd --2—= 280d Vi2 For the hollow square, a? + a;? r= Vis (at— a4) + (@2— 0,2) = ery NEUTRAL AXIS If, in a cantilever loaded as shown in Fig. 3, any point x on the center line ab is taken as a center of moments. and a WH > S i 1 Y i Yj ‘pes : 1." Pe SR Oe Vee. ET’ / Eres, H } —— nN 7 ~~ a ft RE re . > / peas } d ee ‘ ~ ‘ eee Fic. 3 section made by a vertical plane cd through this center is considered, it will be evident that the moment of the force due to the downward thrust of the load tends to turn the end of the beam to the right of cd around the centerx. The 144 HOMOGENEOUS BEAMS measure of this tendency is the product of the weight W multiplied by its distance from cd, and, since this tendency is the moment of a force that tends to bend the beam, it is called the bending moment. A further inspection of Fig. 3 will show that through the bending action of the load the upper part of the beam is subjected to a tensile stress, while the lower part is sub- jected to a compressive stress. Fig. 3 also shows that the greater the distance of the par- ticles in the assumed section above or below the center x, the greater will be their displacement. In other words ae WY at Sit REA | IS 41 8H I f' Ze D’ Fic. 4 since the stress in a loaded body is directly proportional to the strain, or relative displacement of the particles, it fol- lows that the stress in a particle of any section is propor- tional to its distance from the center line ab, and that the greatest stress is in the particles composing the upper and lower surfaces of the beam. In Fig. 4, let ABCD represent a cantilever. A force F acts on it at its extremity A. This force will tend to bend the beam into something like the shape shown by A’BCD’. It is evident from what has preceded that the effect of the force F in bending the beam is to lengthen the upper fibers and to shorten the lower ones. Hence, the upper part A’B is now longer than it was before the force was applied; that is, A’B is longer than AB. It is also evident that D/C is shorter than DC. Further consideration will show that there must be a fiber, as SS”, that is neither lengthened nor short- HOMOGENEOUS BEAMS 145 ened when the beam is bent; that is, SS”=S’S”. A line drawn through this fiber SS” when the beam is straight is called the neutral line, and the horizontal plane in which this line lies is known as the neutral surface of the beam. The neutral line corresponds to the center line ab, Fig. 3, on which the center of moments x was taken. The line s,s2, which passes through any beam section, as abcd, Fig. 4, at the neutral line, perpendicular to the direc- tion in which the beam bends, is called the neutral axis. It is shown in works on mechanics that the neutral axis always passes through the center of gravity of the cross-section of a beam made of uniform material. Thus, in a beam, it is evident that the neutral axis of any section is a horizontal line at which the fibers composing the beam are neither stretched nor compressed. The axis is horizontal because it is at right angles to the direction of the load, which, in structural problems, usually acts down- wards. It so happens that in a beam made of one material, this line will pass through the center of gravity of the sec- tion. It is for this reason that the neutral axis has been spoken of as a line through the center of gravity of a section. It happens, however, that in many beams made of two materials, as, for example, concrete and steel, the neutral axis—that is, the horizontal line along which the particles of the beam are neither stretched nor compressed—does not pass through the center of gravity of the section. SECTION MODULUS The modulus of a section of a beam is equal to the moment of inertia of the section about its neutral axis divided by the distance from the outermost fiber in that section to the neutral axis. This fiber may be either above or below the neutral axis, and it is immaterial whether the beam is a simple beam, a cantilever, or any other kind of beam. If the moment of inertia of a section about its neutral axis is represented by J, the distance from the neutral axis to the outermost fiber by c, and the section modulus by S, then iT c 146 HOMOGENEOUS BEAMS EXAMPLE.—Prove the formula for the modulus of a section as shown in Fig. 5 to be correct as given in the table on page 133. SoLutTion.—According to the table, the moment of inertia 2 of F the section is aneEar® 3. Itisa question whether ¢ or c, is the longer. However, on examining the values L—» given for these two quantities ‘eawieoe in the table, it is seen that they rN et are the same, with the exception i pa ‘’ of the first part of the numerator. Uy = For cj, this part of the numer- % ator is b+2b,, while for ¢ it is Wi b:+2b: “In Fig 5, bas: greater than b;; therefore, b:+2b is a na, 5 greater than b+2b,, and it fol- lows that c is greater thanc,. Accordingly, the formula is I bh 4bbi + Oi) 5 b+2b a ~¢€ B86(b+b) bth 3 _ Cabby +b?) B b+b) 3_ B+ Abi +b? oy 36 (6+b:) (b+ 2b) d 12 (b; +20) which is the same as the one given in the table. PROPERTIES OF ROLLED-STEEL SHAPES The table of values for standard rolled sections already given shows various cross-sections of steel beams. Each one of these beams is made in various sizes and weights. On account of the confusion that ensued from using beams of different sizes from different manufacturers, the latter agreed to adopt standard sizes, which are known as American standard. Therefore, knowing the dimensions of the section of any beam that is rolled according to the American stand- ard, the properties of the section may be found by using the table already given. This table, however, while quite accu- rate, is inconvenient to use, because the formulas it con- tains are long and complicated. The following tables of properties of standard sections are therefore given to diminish the labor required in beam design. i HOMOGENEOUS BEAMS 147 The first of the following tables gives the properties of standard I beams. The bevel on the inside of the flange is always made 1 to 6. The same bevel is also used for channels. The tables dealing with I beams and channels give two columns dealing with the deflection, or sag, of beams. The use of these columns will be explained on page 174. The other values given in the tables will be readily understood. Fic. 6 Frequently, steel beams are built up of several steel sec- tions riveted together. To find the strength of a beam of this kind it is first necessary to determine the moment of inertia of the entire section about its neutral axis. This is done by the methods previously described on page 97, but it may probably be best illustrated by an actual problem. PROPERTIES OF STANDARD I BEAMS OCS NHOD gy |, |S828 SESE ha 2 f 89 = Bxo Aga | $8 | ° S83 888s BQ PSS SSse 3A E SIs $333 oO v ND 2 a 3 Os _ Fe ON A poor a) ako) ee aeae - S88 3338 soyoul “YSIeM UF — |eseelouy punog yoeq re ~ | soygam jossu | ~|8 5 -yory, |, JO asvoiouy ; ; o| supuy eestxy |. | BARB SBSE — | ‘aoIyetA4 Jo snipey | * ae Kea ; ee §9R5 o | PU sgsy |. | HHS NOSS ‘eIqIouy JO JuUomOy; | B ZTOTOO00" OTTTO000" 61210000" O¢ET0000° 29F 10000" SZ8T0000° L9Z0T000° 6800000" 0€900000° 82900000" ¢¢900000° 6900000" ¥1600000° OFTTOO00 OTZ1T0000° 68210000" P9ETOOOD 6E8T0000" 08610000° ZF TZ0000" 9620000" ¢€se0000" T9¢E0000° 36TS0000° 86920000" ZT¥90000° 60° €€0° L¢0° SFO" 640° 690° . ~ © oO té we = Ses Sess FNNN AAR re COnmN FTNOM DONH WSO BH ANN AND ott WHOK CNnHOO Nan ANN ANN comme moe doses Ode MOM WATE ASCSS SWVTooD woe Hi5S NOW CD000D ONO MMOD HH OHH HH tin Not odas 156 WHOK OKHO NOAA 9193 OOO PY DMDOHDHD AONOM AOA DON ANN AAS NOD Bato COON SEY aoe NNN MMH WSO 149 ZS000000° | €8000000° 8Z'T |$o S| 66'°8 | 86119 62E'% ¥S000000° | FE000000° ‘OE T OL LF) 60° 6 |F Z6T/0 60E'S 9S000000° | S8000000° T€'T |OL SF) 02'6 |S 98T\F 8Ea‘z% ZS000000° | 9€000000° eel iSe' Fr) TE°6 |Z OST S LOLS 09000000° | ZE000G00' | €ZI0° | 98'T |\98'ZF| 9F'6 6 EZLT/Z 280% 86000000° | T9000000° LIT |S3° 08) 89°2 |6 9ST 8°896'T ZOTO0000° | ¥9000000° 61 T |¥0'62| OL 2 |0' ZST\8 612 T 90T00000° | 99000000" STO" 1Z'T [98°22] €8'°2 |O LIT\S'69T'T GET00000° | #8000000" 60° T |Z9' FZ) 69°9 |F ZOT|Z 126 TPIOOOOO’ | 88000000" Il T |Z¥ $3] 62°9 16°26 |S T88 8F100000° | Z6000000° EIT |8E°3s| 16°9 |S 6 |S TFS 9ST00000° 86000000" 910° | ST 'TI6L' 12; 20°2/F' 88 9962 T€Z00000° | FFTOO000' TOT |ZT ST] Z¢°S |S TZ |9'sEe €~Z00000° | ZST00000° €0°T |90'° ZT] 29 GIT'S9 |O TTS 2SZ00000° | T9TO00000° vO'T |¥0'9T! $2°9 |¢' FO |F' ESP éLECO000" | OZ TOO000' 40°T |60 ST] 28°9 18°09 |8'ocPr T8Z00000° | 9ZTO0000° 020° +=| 80'T |Z9'FI| 96'S 16'S |S THF G0S00000° | 9TE00000° 96° |S6°OT| 29°F |O' TR |6 StS PFSO0000' | OFS00000' 66° {Z0°OT!] TZ'F /0' 88 |€'8sz% ¢ZS00000° | 09800000" Gc0° TOT |0¢°6 | €8° F/O 9E [SSIS iN { 4 ad 4 Ss I 0 oma) IDI 191939191 ~OCOOGD OOO RKRKRK | q SEK SeSSS 19 O11) © SSS88 S888 S88 8888s YSRi3S eo BSS oth) 9 OD st bol! (panuyuo))—SWVAd I GUVGNVIS AO SAILNAdOUd 150 PROPERTIES OF STANDARD CHANNELS 151 Q2x PN a ae oe Say a| 3 = 3 or ag ue O00 ted ae #25 392 «| 38 oa Yio Asa Pa 38 z ESS 333 5 SS SSS soyuy “343M UT 2 x eo jesveiouy punog yoeq| _ fez) S ™ | soy qa jo ssau 2 se -Yory J, JO asearouy ‘ao ro aan +tHO 68 S| et ey oe ee See JajuaZ jo s0ueysiq souo "6-G SI "a martN 191900 = OES) jo aa Re fe ee o | seyouy “g-esrxy |. | RAN RIS | “‘snmpow uonseg | 4) ss souou ‘6-G SIXY i noe ND es soa i jojuowo, | ™ RAS a soyouy “J-] sixy nas Ba3 = : ‘uoleiADy jo snipey | * ea sae sSayouy =*J-] sixy SS Sy eae o | SPU Try | | Skt ere ‘eIyJauy JO JUaUIOW, SHAN ote 2 hte «| #838 88k esueLy JO YPM See Aes Soyouy OO W100 * | gam Jo ssouyoryy Gee gee cx: m sayouy erenbg)—| « ase ep ope UO0r4deg JO voy | winied mimic Tie aed S22 888 - Soy ie opened NS puueyy jo yidaq 0920000 ° |29T0000° 6S° | 09° | IT’ T/gz°s | 94'°S| 6 IT |B" 2h | Z9°S| 8S" |Ss"9 |Sz'Tz| 8 €8Z0000° |£2T0000° 2° | 09° | ZO'T|T0'S | 8°S| OIL |8 "eh | €9°S| GF" |TS"S |Sz'8T/ 8 T1€0000° |%610000° 99° | 19° | 96° |8Z°T | 68°S| 0°01 66 | HP'S] OF |8L° |SS°9T| 8 ¢6£0000° |91Z0000° 9¢° | 29° | 48° |9¢'T | 86°S|0°6 |0'98 | GE°s| Te" |FO'F |S2"eT| 8 #820000" |0%Z0000"| 280° | 89° | e9° | 6L° /ee'T | OT S| T's jess | 9s°s| oe jGe's |Sz°TT| 8 $4£0000° |%€Z0000° gg | 99° | 96° [ost | 68°%|9°6 |Z ee | ISS} e9° |I8'S |e2"6T) 2 T1¥0000° | 490000" gg’ | 9¢° | 28° |Z9°L | bF°S|9'8 |Z°0E | Th'S| ES" [20'S |Ss" ZT! Z 4G%0000° |98Z0000° eg° | 2G° | 62° |OP'T | 09'S 8°L |Z°2e | 08°S| Sh |PE'F |S2°FT) 2 %190000° | TZE0000° eg° | 2G° | TZ |6L°T | 69°S|6'9 |Z°bS | 0Z°S| ZE" |09"S |Ss°ST| 2 8820000" |89¢0000°| ZO" | so | 6G | 9° [86° | SL°Z|0'9 |T'IS | 60°S| Te [GBs \g2°6 | 4 9£90000° | 460000" gg" | @¢° | HL° |8%°T | 20°} S°9 |o°6T | 8a°S| 9G" |9G°F J0G"ST| 9 4120000° |8%0000° eg’ | e¢° | g9° |20°T | €t'3| 8S [E°4T | 91'S] FH" |S8"E |00'ST| 9 1@80000° |§1S0000° og’ | eg" | 29° |gg° | 12'S} O°g |T'ST | F0'S| ZE" |60'E |0G'OT| 9 €930000°|2620000°| 670" | ZS° | #° | OG jOL’ | FE'S| EF [OST | Z6'T| 03° |8E"s |00'8 | 9 €611000 °|9%20000° Ig’ | 6h | ¥o° [28° | GZ°T| Sb |b'OT | FO'S| SF \8e's [OS TT) 66£1000 ° |280000° 8h | 6h | oh [69° | S8'T| S's |6°8 | 68'T| Se" [So's |00'6 |g $L91000"|9FOT000"| 690° | 6h | OG | 8e° [8h | S6'T| O'S [FL | SLT] BI’ [€6'T jOg'9 |g iN N f % Poa? 00 ig tet Yan, an eae i a | Vv . (panu1juo))—STANNVHO GUVANVIS 40 SHILaadoudd 152 6200000 ' *|6100000° 9800000" 24600000" Z01T0000° 0Z10000° 9810000" 8910000" 9810000" 92T0000° *|8610000° "18910000" |¥9T0000° 8100000" TG00000° *|6600000° ’ | #600000" *|$%00000° *|6€00000 ° 1900000 2900000 6600000: 9T T0000" 0TT0000° 0Z0° gZ0° 6c0° €€0° AA HAAR BANNAN MMO OO HH HAAN ANMOM WINING WOE CDODCDCD ODCDCDEDOD WN AAHH wdudwnsINw NID WENO HOOD wKeMOr-W MADr~ AYONM AOOMD OMAN AANN ANAM AooedeDed epedeDeDED00 OTN WGHNOS ONw S| Og" SESE SSESSE 153 154 PROPERTIES OF STANDARD ANGLES HAVING EQUAL LEGS HOMOGENEOUS BEAMS soyouy ou e-¢ SIxy ‘uoyeiy | +} AR SAS jo SHIpey 4seeT : = get ~ | oe NNo = o-G SIXV YW} oo Sess ‘SnINPpo|W wor99g yeqey 3° See S| sesmy ‘enon [|X| SS S55 jO JUOWIOW 4S¥oT seyout = ‘“xedy 20 MID @ | [PUloIX” WO APAPID | & CIO a es jo Iajueg jo s0ueysIq bods Seiad | AN SOD os J-[ stxy ie) SAE ee ‘UOI}eIAL) JO SNIPER Sogou EX 538 3 I-] sixy A SS ee ‘sn[npoy, UorjoeGg ppict S2 883 o [-[ stxyv ~ o o se Oo ‘elyiouy Jo JuoMIO;, seyouy = “Ba’T jo me ont 9 | YOVCG WOOL AYACID Jo |; & NAN coded I9juNg jo souRisIq soyouy erenbs 2a Aas “| — uomseg jo vary =| * * spunog OD WN yoo Jod 4ySI0 he we seyouy ssoUHOY.L, “oe ae ue seqouy a re SUOISUsTIG, x| XX XXX . . 8 CC 155 HOMOGENEOUS BEAMS “HHHAN Sete FWSM MOVAWMOA NODWHOOH ONOKHMNO FBHODOOErNM . “-* FAN FANN NANO HIS Notts otis ON wD ctenlSe wtonlSivelinianl® oitealinten Sen olotealirieelSn aftvelSrtenf cele min il ean ion icn NANANANAN XX KK KK KKKK KKKKKK KKKKKK KKKKKKK Rt rn ttdtrdciedcindss cotnothetocettonectin ON ON OY SS SS SSS SSS SS NNNANNN Sl a ae Bh oe ee ce ee ee oe oe | Tt IRIN coheeochnethen coherence 156 HOMOGENEOUS BEAMS 5 O00 D ODOM ARWOWWr ES SEBBESSS SESSSESSSS RARERRE “~—o-_ NOrtoorn dad COh-RO1ID WOMODO 3 om YS5SLLR3 RESSSShnes Nod HAD z ss oes oe Be ce Be | So oe Re oe Be S 5 6) ANANANN DOM E89 BOP KANONO a 3 we SSRBS33a8 SABBOH rONws | ree SHANNA rr NNANN 2 NORAD OH OOMOMDN19N 00 atheros I % ANRRG Os SBS ID 1D 1D OOO COOK so Sesser etre ee ee a ee Se Oo Oe eB oe Be | B MNHMHOMDMH OEHPOWWHMONN WOMANS |. | SSERESRH SSSSSSSESS ARAAA ro) Se Be Be Oe Oe ee Oh oe | trie DHAMMOEROS DNOAMVWnGnMOD lS Blond F ”n BRRSSUSs AAMHOWAHNG ASLSAS ty 5 eo Oh oe | SSS SAM NNN SeHHAA i HHOONAMAT MOHRDODAHRMNMOMM HORoON Oly AWKRANAHOOHD HONOAMSANIODQ hMMYOMOH S| BAH AHNNNAN ANMMMAHHIN MAHHNOoO (=) TSESAR SVS OAHODONONA NHOOWD rey DHDARHAD SSOSCSSAAAAe HAAN e Soe | sk ho A ad Sasser & HOR HINO O OADIODMAHRDMO WORIND ai«a SVAILSES SHONSAMBGON Soras fs TMHANNMOOD ANNMOOHHINID NANO H AAA HHI CMADMAHOWS KIC CCCI ODED WOMHASHA OOM C9 WO OO MN wag ~ Se Oe oe Oe ee oe oe | a S| | teeeeeneeert eeeicmetiarttiie Rentals a. a asain cl ; x MOODODODODEDODOD MDODODODODODCDCDODOD HH HH Hi eH 3 KKK KKK KK KK KKK KK KKK KK KKK CD OD OD OD OD OD OD CD —_eoreieanieandoiriniceicmicesioy SH SH SH SH RSSSSRE snjnpoy uorjoag «MN | o|] peppy Beemy |. | Seren al ‘eljiauy JO JuomIoyY =| aa soyouy “say Jeqr1o0y OD 190 O @ | jo yoeg wor AACE) ® REZRLRS JO Jo}zU9d JO a0uR4SIq. a seyouy ‘“J-[ sixy j SSSB5RS uoesAy josnipey |; ~j} ** ttt? ~| sur visxy |, | RASSSR6 snmnpoy uoysag «=» |] WP NS : RE BAHFS ef PP U | EL ey. [eee eIjJoul JO JUSMIO;Y seyouy “Sey Jasuo7y jo mist re wo | Yoeg worg AqtAeIL) JO | & BESBSES Jajued JO sourysig «| Swerems — |_| gBSRREA UOlz}IG jo voly Ses HNN spunog peepee bak! oo 300.7 ad 34319 \\ S| cds oon Soyouy z * oh Ssouyoy treed = soyouy BL ANANAAA suOISUSUIG, x eee ee eae 159 HOMOGENEOUS BEAMS Sessa Sse Se oe ee oe oe oe oe | NAA ANNA CNCOCO HH ODO OO a at et iS Ree FARRAR RNR RRR RRR RRS eS St et et SS PSSRSGSNS SRSRBeS 288 RAR BRANNAN NOD CD 08 eet TOS omc Stet to Oo FANNING HANNAN n0Ned AAD CO Cd st tt Se SSS Se . HIDORDAS HORDAOCHNM OKRAQOHANMHDO WOOOMIONH KHANH AOO SH ODN WHIOOrn OO = efErior {Snel cio IS ee Ero revallonorfSnelepe — dtelSetor{S melee IRAN NNN EN RIRIRN Rea OD OD OD CD OD CD OD CD OD «OVD CVD. CVD. CD) OVD CVD) CVD) CVD) CVD. CD. pe a ee ANAANAN AANAAANAANAN mommammccnoe DEDEK DOSS ES hE EES KOK OE. - DEDEDE OEE KODE. RAIA OD OD OD OD OD OD OD 160 HOMOGENEOUS BEAM. s 9L° | G8h° | 6S'T | F9'% |06'8 | S9'T ‘92° | $8h° | 09'T | 62'S |8Z°2 | I9'T ZL’ | 68° | 19'T | P6'T 109'9 | 69° T v9" | T€E° | $9°T | SZ°F |82 °F] S8'T ¥9° | 988° | SS'L | OFF |186'EST| 98'T 09° | OFS" | SS°L | OL 'F ISL 'SL| P8'T v9" | ShS° | 99°T | 98'S [8S SI! Z8'T v9" | 6FE° | LO°L | So's |ZE'IT| O8'T GQ” | €SE° | 8S°T | €2°S |S OT! 22°T G9° | LSE" | 6ST | 16'S |Sh'6 | S2Z'°T g9° | 198° | 09°T | 89'S |Sh'S | ELT S9° |79E° | 19°L | F2°S |ZE°2 | OL'T 99° | 89€° | I9'T | 68'T 192°9 | 8O'T ¥9° | Z2TS° | 0Z'T | GO"S |GZ°2 | OFT ¥9° | 8TS° | 1Z°L | 248°S |SE°L | FFT v9" | b29° | 2ST | 89'S |86'9 | ZE'T v9" | 66S" | GST | 6F'S |6h'9 | 6E'T v9" | PES" | $S°T | 08'S |E0'9 | ZE'°T ¥9° | 8ES° | HST | 60'S |g¢e'¢ | SEe'T $9° | Sho" | SSL | 68°T [So's | Ee'T $9" | LPG" | SS°T | 8O'L leo '°F | OF 'T v9° | TSG" | 9S°L | OFT |96'E | S2'T G9° | PSG" | 4Z'T | SS°T Ise’ | 92'T at D Ted iS WI * S FANANN OCs HANNAN NoseseOsED NODES ys _ pie . . . NANO HHISID ANd Noo <8 AMOARHOWDONMMD NWMOMOrMHMIAN to rim fSrelSeeeawtnte oaenltnaliaartimenane ene riirdouden caepapenenarenenenen apeneparedenenenaneD saG0e0 xXKMK KKK KKK KK KKK KK KKK KKK SH SHH SH SH HH 991919191291910191N)- 10101) mM DXq (panuyuo))—sSoaT TVNOANN ONIAVH SATONV GUVAGNVIS JO SAILUAdOUd 161 HOMOGENEOUS BEAMS 06'I DDHDDMDD AHH UD UD AD AD UD O22 QD RRS SRN NNN Re Ese IS Ree Oe oma be ee ee oe ee oe ee | NOOO WH AD HOW IOOOOORN Mat HoONND FR ANNAAAANAAN THA ANNNNAAN orto) roe Oo} . BRANNAN RFRA BANANA NOOO OD Sea chienhben hl DOOD 0D SHH SH HH tt tt tt xxKKKKKKK KK KKK KKK KKK MK KK KKK KKK | ID1DIDIDIDIHINID OOOOOGOGOOOO OOOGOOOOOSO UEP GOO HIT CIGWHGHOOOM WGHOGOMNHHBASS ONDMOMOKA HNOMAROWONMA MMNNHOWOHNRO sooleaeoreliSeit? aeentenelenrfiae eRe etonll rele fate ree HHAGHOON HHTHHOCOMN OD HHAHOGHOONNDA AMINA Ret Rdtidciniindinditnd ics OD OD OD OD OD OD OF OD OD CFD CD CFD OD OY) OD OD — PROPERTIES OF Z BARS oy STARS 12 23 S 3 BBS3s et Sond oe 64 S55585 en ae es OMAIOD re o = 9A by z= Raases SAS x eS |" |388833 Hes footie Pits tibcoteer ito soyouy 2 gg sy ‘uoneso |4 | BBSBRE jo snipey 4seo7T SSSKSu S| o[suy jo juesuey | 8 SSSRRS me «| seyour ‘g-gsxy |. | SaAnSaas + | ‘uoneity jo snipey | |) o| seuou, “e-ssIxy |» | RSRSSR | ‘snp poy, woryzoesg wet cal of wane ; rt HON 19 19 00 OPEL Ee RLY, Ceo ‘eljlouy JO JUSMIOWW VOD OD SH SHAD oo | SMU T-rsixy |. | ANSON ‘UOIZVIAL) JO SNIP i wlcob eee N Or OOD pe | CHOSE. CO F-T SEW SRZISS ; sn[npoyy, wor49eg HAAN ACD oD : roesee ©. | PU iar sey) |_| SEM ‘elzIouy JO JUSWIO;, CI O0 9 SH Hid seyouy oienbs < a FRRSA is UO0I}DaG JO valy PUAN CD oD tH spunog Ss ee “| 00,7 red 34310 Ca ae seyouy ‘sse7y pue | | © | qo Jo ssouxoryy, “teeter tel soyouy 4, 8 403} eH bal rs ssa’J Jo y4sue’T NANA AA vai, 4 +e 42 ra tJeg jo yjdoq " | coadencaen es | 162 660000 ° €€0000° FLO000" > om . @) ib aoe ce - . ANAAAAAAA AA MANN NCO ANNO MOH Amott HA oe) ie 6 ie Joie ete eee wt ah odd pod et vot hed al cal aol pad ed AeA oad ae NARA RH Ob AIHOWMWReN OID WM WAMMOOT YT ROmHOr oO ww HiDQiQoOO OH SSSassSSS BESS oo hoe oe hoe oe hee hoe hoe hon ee hn hee LD SH HO tH OD cose NAODOMD 1909 HO WINDOW Oro Woyoor 18’? ON N 2 ko rie os, ~~ NANN BANNAN NODO . WON N HSB MRONONROH INWAAMBOAnH Cos Te ee oe] CD OD OD CD OD OD OD OY) OD OD OD OD CD OD OD CD CVD CD CD OD OD OD OD . Eee ree ete te ecto eee iv See nten face ev nate “2 OD OD OD Sees = oO oD wivefinice Srinelieiarfine efiaterl® tele eter Entel 164 PROPERTIES OF T BARS EouaL LeEcs HOMOGENEOUS BEAMS oo | soyour “e-gsixy |. | AARAR FS | ‘uonerdyjosnipey; ~} *° "7" . ca | soppuy “eesey |, | SSSS5 AR “| ‘snmpow uonosg |] "°° RF ~| swur sesmy |, | 58883 28 | ‘eysouy jo yuomow |] *} «+++ = o| smu risxy |, | 38888 38 | ‘uonersy josnipey] ~} *s 6 *: aire o> | sul ‘s-rsKy |, | 8885S Aw sninpoy woseg | “}] «s** oe o | SU ‘THrsixy |, | SSSSS HF elyieuy jo yueuiow |~ | - ae a soyouy ba ‘eSUPTy JO opisyn BoD oO On on WOIy ALIAPIN a FS ee JajUag jo s0ue4sIq < seyouy erenbs < eee: ie WOI49aG jo eoly Bin ih® BO rad eae rita neetee 4OOWT Jed 14310 M Senne ot sayouy se | MBSR Sts fete W194 g| 88sse gs JO SSOUMSY TL, | > | rtoukctubiuks ls g soyout —| Fe | Bate etm i Se asurl yy ae) S883 88 JO SSOUMSY TL | o | rtnedelSafSalS rng’ as sayouy 05 reg jo y3deq | ~ ane AN a S soyouy r asuely = mettre AN JO FIPEM 165 HOMOGENEOUS BEAMS LI'T| 241° | S'S] 82° | 90'L| ers] o2° | 66°|9°ST| FO | Or € g g 06° |99°1| 82'S] 90'T| ET's] S80°S| IT'T |SO'F16°ST| #OVRF | BO g r 66° | $9°T| 89°S| 90°T| €0°Z| 68°F| 6O'T | ZE°F| 6 FT ag 5 ee g b GO'T | SIL] 19°3| 89° | Fe" |FO'T| 2go° |é6e'zlo's | # 07% 073 z P OL’ | 18° | ZL | Ss'T| Fo°L| ee'F| OT | ¥6'Z| O'OT 04 074 P #¢ 89° 109° |06° |FZ°T| IS'L| 20°F] 2e't | P2°2| 2°6 074 04 ¥ g 99° |00° {06° | 70° |0O° |S0°T| T2° | IL°s| e's 04 04 §Z g vo" (or (49° | 29° | 99° | eB" | 2° | Te's\| rz Hy 04 z j 09° | cr’ |ec° | 16° |F8° |o2z°T| g6° | OT'Z|Z'2Z $2 ' 04 g z 09° |8e° | 2° | OF |9T° | 1Z° | eb | Tet] o'F 0}4 074 T Zz g¢° |zz° |sz° | te [60° |80° | og |98° joe | 403% 7 T 4 82° |10° |g0° |6%° | 90° |#0° | 62° | PR Lat | 4200 ¥ ¥ 0p Ht | My tI soa] ‘IVvNOang €8° | 9O°T| IT'S| T2°T|Se't| Po°F| SIL | 6t'e| 6'Or| 0 F a 07 P PF eZ° | 18° |2p'T| so tlez‘t!or'e| 66° |2°2/e'6 Hoe aot §¢ #8 r9° |08° |0%°T| 88° |or't| 22°2| €6° | 96°2| T‘OT 0}4 0}- g g *9° | 19° |26° |06° |98° |28°T|] 88° | Te°z| 62 tak tok g g zo" | 09" |SL° | 06° | FL" | 89°T| 98° |66T/8'9 | #9 % € & co’ |os° | or |o2° | or' | 28° | e2° | eO'TI O'S 07 &t 04 §Z 42 ee ee" 128° 1:90° 10r 190° | 2o* | OF 210'°9 ie 04 1S 1% we tS" 1 YE" 98" «1:6e" 11S". | SO AIST SF 0} 0} $3 +3 HOMOGENEOUS BEAMS PROPERTIES AND PRINCIPAL DIMENSIONS OF 166 STANDARD T RAILS Axis 1-1 10019 sn pow H FBO. ED RO NAAN Hater cueg coh UWOlT}PIS TAA CD SH HID OI OS AND HED elt) eIj10uy jo e AQHA OOROHDNEOOCORMHONM yUSO WW HAND HOWDANHTROMOOHOMD rt NNN 0D 09 09 SHO fe | | LON ttt RBA cia tor aaonans oon oo ad AARON NANA AANA soyouy 1 Up ctortoctoctostoetoorefactsche chores rte ee soyou oul Erte iveskoniuspocciano tories tes tacts ea enskortaeniainte 4 SAAN AANA tH soyouy reebok ritingtonpotante ts ofS cofn Pp rlemtortectet ctertende toate eter soyou ‘RUT Hisuportetieicals ri or orte chert — lS cate q TEA ONNN CD 01 OD OD OD HH HH HD 1919 1919 sayouy erenbs RA Sia a tata stato sooe9.c0 09 00% valy AAA NOD 09 oH HID IGOOM MN WDAD spuno 1” 19010 puned OHORRS SS ISBSSELSESESS pre x sod 44310 OM DDHADOW me HOMOGENEOUS BEAMS 167 Sometimes, the sections are not symmetrical and the neutral axis itself must be found. As an example, consider the beam shown in Fig. 6 (a). It is composed of anI beam and a channel riveted together. Sucha beam is often used to carry the track of a traveling crane. The first problem is to locate the neutral axis cd, Fig. 6 (6). Assume any axis, as ab, about which to take ordinary moments of the areas. The moment of each area about ab is equal in each case to the product of the area and the dis- tance from its center of gravity to ab. The areas and loca- tion of the centers of gravity of the beam and column sections can be obtained from the tables. Adding these moments, the work is as follows: Moment of I beam=20.59X9 .......=185.31 Moment of channel= 11.76 X (18+.78) = 220.85 Total.. .406.16 16 The total area “ee the eon is 20. 59 ve 11. 76= 32.35 sq. in. Therefore, the distance from the line ab to the neutral Amar 3935 °° It now remains, by the method given, to find the moments of inertia of the channel and the I beam about the axis cd and to add them together. This can be done with the help of the tables, as follows: The moment of inertia of the channel about cd is 9.39+11.76X (5.44+.78)?= 464.36. Likewise, the moment of inertia of the I beam about the axis cd is 921.2+20.59 x (12.56 —9)2=1,182.15; therefore, the total moment of inertia is 464.36 + 1,182.15 = 1,646.51 in*. axis cd is FORMULAS FOR DESIGN BENDING-MOMENT FORMULAS In any homogeneous beam the maximum stress at any section of the beam developed by the loads may be found by the following formula: Bast c in which M is the bending moment at that point, in inch- 168 HOMOGENEOUS BEAMS pounds; J, the moment of inertia of the section referred to the inch; c, the distance, in inches, from the neutral axis to - the most remote fiber; and s, the maximum stress, in pounds per square inch. This stress, of course, occurs in the most remote fiber. This is the general equation for beams. It expresses the bending moment about any section, caused by the loads and reactions, in terms of the maximum unit stress at the section and the dimensions of the beam at that section IT J (nat is, ) . Thestresss may be either tension or compres- Cc sion, but it is always the maximum stress in the section. It is evident that if a beam is going to break, the break will occur at that section about which the external bending moment is maximum. If this section holds, every other part of the beam will be strong enough. Therefore, it is the section of a beam about which the external bending moment is maximum that is always investigated. I The quantity a is equal to the section modulus; therefore, the formula is often written M=sS, in which S is the section modulus. In the preceding tables the moments of inertia, etc. are given with the inch as a base, and s is usually measured in pounds per square inch. Therefore, in the preceding for- | mulas M must be given in inch-pounds and not in foot- pounds. EXAMPLE,— What is the maximum stress in a simple beam 12 ft. long and uniformly loaded with 1,000 Ib. per ft. of length? The beam is rectangular in section, 10 in. broad and 14 in. deep. SoLuTiIon.—The total load on the beam is 1,000 12 =12,000 lb. The maximum bending moment, in foot- Wl pounds, is 7%. In this case, W=12,000 Ib. and /=12 ft. Therefore, the maximum moment, which shall be called M, HOMOGENEOUS BEAMS 169 12, 12 equals =X = 18,000 ft.-lb. To change this to inch- pounds, multiply by 12. Thus, 12X 18,000 = 216,000 in.-Ib. bd2 10X14x14 The section modulus of the beam is — 6 —— = 326.67. Substituting these values in the formula, 216,000 =s x 326.67, and s= 216,000 + 326.67 = 661.22 lb. per sq. in. Ans. MODULUS OF RUPTURE Assume that the load on a beam is increased until it breaks. From the loading that causes failure, M can be found, while S can be found from the shape of the beam sec- _ tion. Substituting these values in the formula M=Ss, a value for s will be obtained. This value of s, which corre- sponds to the moment that causes the beam to break, is called the modulus of rupture, or ultimate unit bending stress, of the material. Since the formula M=Ss is strictly cor- rect only for values of s below the elastic limit, the modulus of rupture will not agree exactly with either the ultimate unit tensile or the ultimate unit compressive strength of the material. The modulus of rupture is a valuable constant, however, because by substituting it in the formula M=Ss the breaking moment of a beam can be ascertained. In designing a beam, of course the beam is not intended to develop the ultimate unit bending stress, but only a fraction of it, depending on the factor of safety used. For timber, a factor of 6 is usually employed; for wrought iron, one of 4 is sufficient; while for cast iron, from 6 to 10 is employed. For structural steel, the factor of safety gen- erally used is about 4. With structural steel, however, instead of dividing the modulus of rupture by the factor of safety it is customary to use certain approved unit working bending stresses. For light roof construction, this value is often taken as high as 18,000 to 20,000 lb. per sq. in In ordinary building construction, 16,000 lb. is usually employed and in bridge work, 12,500 lb. per sq. in. is often used. ExAMPLE.—Design a rectangular white-oak beam to carry a safe load of 2,000 1b. located at the center, the span being 11 ft. 5 in. i aie ey 170 HOMOGENEOUS BEAMS SoLuTion.—The maximum external bending moment is WI 2,000 X 187 4 4 for white oak is 7,000, and a factor of safety of 6 will be used. ‘Therefore, s=7,000+6=1,167 lb. per sq. in. Substituting these values in the formula, 68,500=SX1,167, and =68,500 in.-lb, The modulus of rupture bd? S=68,500+1,167=58.71. S= ae therefore, either the breadth or the depth of the beam may be assumed and the other dimensions found. It will also be noted that in the value of S the breadth is involved only as a first power, while the depth is squared. Therefore, to design an econom- ical beam, the better plan is to make the beam narrow and as deep as possible. Of course, there are practical considera- tions that govern this matter, such as obtaining commercial sizes of material and the like. In the problem at hand, let is be assumed that the beam bd? bX 10? will be 10 in.deep. Then, d=10 in., S=58.71 er ae ~ 6X 58.71 and pa = 8.523 in. The next larger size of com- mercial timber is 4 in. x 10 in., and is therefore the size to be used. The modulus of rupture of metals and timbers will be found in the two tables on pages 126 and 128. WEIGHT OF BEAMS Every beam, whether it is made of wood, steel, or stone, has a certain weight, and the question is whether it should be considered or not. Neglecting the weight of the beam itself in beam design does not make so much difference on ’ a short span with heavy loads as it does on a long span with comparatively light loads. Just when the weight of the beam itself should be considered and just when it should not, is a matter of experience, and no set rule can be laid down. Usually, however, if the weight of the beam is less than 5% of the load it is intended to carry, its weight may be neglected. HOMOGENEOUS BEAMS 171 Since, in some cases, it has been decided that the weight of the beam itself must be taken into account, the methods of attaining these results will be considered. As the weight of the beam cannot be obtained until its size is known, and as the size of the beam cannot be found until the total bend- ing moment is known, this problem can be solved only by trial. The following example will serve to illustrate the method to be pursued: ExaMPLe.—Calculate the size of I beam required to carry, besides its own load, a uniformly distributed load of 960 lb. per ft. over a span of 20 ft. ‘SoLuTION.—The total load on the beam, exclusive of its own weight, is 960 X 20=19,200 1b. The maximum bend- WI 19,200 x 20 X 12 8 wl ae M =Ss=-— = 576,000. Giving s a value of 16,000 and ing moment is = 576,000 in.-lb. neglecting the weight of the beam, 16,000 x S=576,000, or S =576.000+ 16,000=36. On consulting the table on page 148, it will be seen that the value of S here found corre- sponds to that of a 12-in. 31.5-lb. 1 beam. This beam would satisfy the requirements if the weight of the beam itself were left out of consideration, but as it is necessary to provide for this additional load, the next larger size may be chosen and a trial calculation made to see whether it will support the com- bined load. This beam is a 12-in. one, weighing 35 Ib. per ft.; hence, the weight of the beam is 35 X 20=700 1b. From the Wl preceding formula 3 the maximum bending moment due 700 X 20x 12 to the weight of the beam alone is —_— = 21,000 in.-ib. The sum of this moment and that of the external load is 576,000 + 21,000 =597,000 in.-lb.=M. M=Ss, or 597,000 = 16,000 x S; therefore, S=597,000+ 16,000 =37.31. As the value given for S in the table is greater than this, the beam selected is of ample strength. As was stated, it is usually considered safe to neglect the weight of the beam itself in calculations of beam design. 172 HOMOGENEOUS BEAMS FORMULAS FOR DEFLECTION OF BEAMS Case Method of Loading eae : are Sey we pS 3 EI ‘ we 8 El III Malas 15 EI Gente at See aie, soos iy akan arabe 1 WR A 4 @D 8 El Eel wey2t—x) V3xQl—2) Vv yi b y 27 IEI -— — ——1— — = a We (3p — 422) VI V] a8 4 7 48 El = 2 “ 5WB vil 384 El 3WB Vill 320 EI . : HOMOGENEOUS BEAMS 173 TaBLE—(Continued) Case Method of Loading sense | KK Y Wwe ms ae =p 60 EI Y x rw 3,600 EI XI _3 WP 322 EI 5 WB II 5WR 4 926 EI Yy aap gh ee ee oe We ere - ® 192 El XIV Wwe 384 EI For overhang: —— sa (3 xl—4 x)? vied opr = — ae = = isne ri For part between sup- | | | 3 ports: eer 174 HOMOGENEOUS BEAMS As the amount of load a beam must carry, particularly the live load, is very uncertain at best, the addition of a slight weight due to the weight of the beam itself is seldom con- sidered to be a factor of great importance. When beams carry floors, it is customary to find the weight of the floor per square foot and then multiply this value by the distance between beams and by the span to get the total load on the beam, Many engineers assume that the weight of the beams themselves add a certain weight per square foot to the weight of the floor. This added weight is assumed to be 8 lb. for wooden beams and 6 1b. for steel beams. Thus, if all the materials composing a floor, exclusive of beams, were calculated to weigh 12 lb. per sq. ft., a weight of 20 lb. per sq. ft. would be taken to constitute the total load of a floor supported by wooden beams, while 18 lb. per sq. ft. would be taken for the total load of one supported by steel beams. This method, while not absolutely accurate, is one way of estimating the weight of the beams in a floor. In concrete beams and stone beams, however, the weight of the beam ttself must almost always be considered. ‘DEFLECTION Deflection is the name applied to the distortion or bend- ing produced in a beam when subjected to bending stresses. The measure of the deflection at any point on a beam is the vertical displacement of the point from its original position. Stiffness is a measure of the ability of a body to resist bending; this property is very different from the strength of the material or its power to resist rupture. The stiffness of a beam does not depend so much on the elasticity of the material of which it is composed as on its length of span. This property of stiffness is as important in building construction as mere strength, and the two should be considered together; thus, the floor joists of a building may be strong enough to resist breaking, but they may also be so long as to lack stiffness, in which case the floor will be springy and will vibrate from persons walking on it. If there is a plastered ceiling on the under side of the joists of such a floor, the deflection of the joists may cause the HOMOGENEOUS BEAMS 175. plaster to crack and fall into the room below. The allow- able deflection of a plastered ceiling is usually placed at xéo of the span, or wy in. for each foot of span. Where stiffness is lacking in the rafters of a roof, they will be liable to sag, thereby causing unsightly hollows in the surface, in which moisture and snow may lodge. The amount of deflection that exists in beams loaded and supported in different ways may be calculated by the for- mulas given in the accompanying table. In using these for- mulas, all the loads should be expressed in pounds and the - lengths in inches. The modulus of elasticity is denoted by E, and the moment of inertia of the section by J. ExampLe.—A 10-in. 35-lb. steel I beam supported at the ends must sustain a uniformly distributed load of 10,000 lb. The span of the beam is 20 ft., and its moment of inertia is 146.4. There is to be a plastered ceiling on its under side, the allowable deflection of which is #% in. for each foot of span. Will the deflection of the beam be excessive? SoLuTION.—The formula of the deflection of a beam of this 5 character, from the table, is adic The modulus of elas- 384 EI ticity of structural steel is 29,000,000. Substituting the values of the example in the formula, the deflection equals 5 X 10,000 < 2403 384 X 29,000,000 x 146.4 © Since the allowable deflection is ss of the span, the total allowable deflection is s45X 240=% in. This is greater than the calculated deflection, and the beam therefore satisfies the required conditions. The values for N and N’, the coefficients of deflection for uniform and center loads, respectively, given in the tables containing the properties of sections of I beams, channels, 42, or about zs in. 5 WB and Z bars, were obtained from the formulas N = ———— 384 EI We ., . : and N’=———,, in which W equals 1,000 Ib.; J, 12 in.; E, 48 EI 29,000,000; and J, the moment of inertia about the axis 1-1. Therefore, these coefficients represent the deflection, in 176 HOMOGENEOUS BEAMS inches, of a beam 1 ft. long having a load of 1,000 lb. Mul- tiplying the proper coefficient by the cube of the span, in feet, and by the number of 1,000-lb. units in the given load, will give the deflection of a beam for any load and span. EXAMPLE.—What is the deflection of a 20-in, 65-Ib. I beam that carries a center load of 28,000 lb. and has a span of 20 ft.? SoLuTION.—The amount of deflection is obtained by mul- tiplying the coefficient of deflection for beams with center - loads (column 138 in the table of properties of I beams) by the cube of the span, in feet, and the number of 1,000-lb. by units in the load. Hence, the deflection equals 00000106 x 203 x 28992 — .237 in. SUDDENLY APPLIED LOADS In the formulas and investigations so far discussed, it has been assumed that the loads on the beams were laid gently in place. This, however, is not always the case, for the load may be suddenly or almost instantaneously applied, or it may even be dropped on the beam. Of course, in design- ing such beams, a large factor of safety may be employed, but if the load is dropped or very suddenly applied, this method is at best a matter of guesswork and experience. The investigation of sudden loads divides itself naturally into two classes. The first includes loads that are not raised above a beam and whose weight is suddenly applied to the beam. The second class of loads includes those that fall vertically on a beam, as when heavy boxes or crates are dropped on the beams of a floor. As the problems of the first class are the simplest to solve, they will be taken up first. When a load is placed suddenly on a beam, the stress produced is twice as great as if the same load had been at rest; that is, a beam to sustain a sud- denly applied load should have twice the transverse strength required to sustain the same load at rest. Often, a problem occurs concerning suddenly applied loads in which the beam has a quiet load, which is the dead load, and a suddenly applied load, which is the live load. Sucha problem should be solved as follows: HOMOGENEOUS BEAMS 177 ExAMPLE.—Design an I beam to carry a uniformly dis- tributed load of 140 lb. per ft. on a span of 12 ft., and also a centrally concentrated, suddenly applied load of 3,700 1b. SoLUTION.—The bending moment due to the uniformly WI (14012) x12 distributed load is “tie 3 =2,520 ft.-lb., ‘or 2,520 X 12 =30,240 in.-lb. The concentrated load, if gently 3,700 X 12 applied, would cause a bending moment of ri =11,100 ft.-lb., or 11,100 X 12=133,200 in.-lb. Since, how- ever, the load is suddenly applied, it will produce stresses equivalent to twice this bending moment, or 133,200 2 = 266,400 in.-lb. The total moment that the beam must be designed to withstand is therefore 266,400+30,240 = 296,640=Ss. Since s=16,000, then, S=296,640~+ 16,000 =18.54. Referring to the table on page 148, it will be found that a 9-in., 21.5-lb. I beam is required. The other class of loads referred to are those which drop on a beam from a distance above it. It is customary in considering the effect of a falling concentrated load to deter- mine the statical or quiet load concentrated at the center that would produce the same stress, and then to design the peam for this statical load. The formula used to accom- plish this is aE wiew(1+ Pts): in which W, is the static load, in pounds, concentrated at the center, that would produce the same stress in the beam as the falling load; W, the falling load, in pounds, that strikes the beam in the center of the span; h, the distance, in inches, that the load falls; d, the deflection of beam, in inches, pro- duced by load W statically applied; and a, the constant. The value of d is found as previously explained, while a is found by the formula 1 ta 14.499 V2 +. Ww in which W2 is the combined weight, in pounds, of beam and dead load that it supports; and W is the falling load. 178 HOMOGENEOUS BEAMS From the construction of the formulas, it will be noted that the size of a beam required to sustain a certain falling load cannot be found direct. The size of beam must be assumed; then the formulas are used to ascertain whether the beam will meet the requirements. ExamPLe.—A 12-in., 40-lb. I beam carries, besides its own weight, a uniform load of 260 lb. per ft. The span is 10 ft. Ifaload of 400 lb. drops on the beam from a distance of 18 in., will it develop a unit stress beyond the safe unit stress of 12,500 1b.? SoLuTION.—The total static load per foot on the beam is 260+ weight of beam per foot =260+40=300 lb. per ft. The total static load on the beam, therefore, is 300 X span =300 X10=3,000 lb. The deflection due to the falling load of 400 lb., according to column 18, of the table on page 000 is .00000505 x 103 xk .4=.00202 in. The constant a thus equals 1 ae 1 9140 1+.489 Like slates WwW 400° Therefore, 2 ah 2X .2142« 18 wiaw(1+ i) a. = 25,117 Ib. The maximum bending moment due to this load is 25,117 X 10 ; ————— = 62,792.5 ft.-lb., or 62,792.5 X 12 = 753,510 in.-lb. The maximum bending moment due to the static or dead _ 8,000 < 10 ; load is ue gore =3,750 ft.-lb., or 3,750 XK 12 =45,000 in.-lb. The total bending moment of both the static and sudden load is therefore 753,510+45,000=798,510 in.-lb.=Ss. From the table on page 148, S=41. Therefore, 798,510 =41s, and s=798,510+41=19,476 lb. per sq. in. This is greater than 12,500, which was assumed as the allowable unit stress. Even if 16,000 lb. were taken as the allowable unit stress, the actual stress would still be too large and a beam of larger size would have to be assumed. WOOD AND CAST-IRON COLUMNS 1757. WOOD AND CAST-IRON COLUMNS WOODEN POSTS MATERIALS The kinds of timber usually employed for columns are the long-leaf and short-leaf yellow pines, red pine, white and red oak, spruce, hemlock, cypress, fir, and redwood. The timber generally preferred is the yellow pine, the long-leaf variety being stronger and more durable than the short- leaf. The disadvantage of this wood is that the resinous sap makes it very inflammable. The compressive strength of timber varies greatly, accord- ing to the amount of moisture it contains, a decrease in moisture resulting in increased strength. The percentage of moisture in wood is usually reckoned from the dry weight. Thus, if a certain piece of timber that weighed 165 lb. when green weighs 100 lb. when kiln dried, it would be said that in this instance the wood when green contained 65% of moisture. The drying of green wood does not effect an increase in strength until the moisture is decreased to a value amounting to about 20 to 30% of the weight of the dry material; that is, the strength of a piece of green wood when being dried remains constant until the moisture remaining in the piece is reduced to from about 20 to 30% of the weight of the dry wood, and from this stage the strength starts to increase. Experiments made by Tieman, the results of which are given in the Proceedings of the American Society for Testing Materials, show, for instance, the following variations in strength of long-leaf pine: If the strength of the green wood is taken as 1, then the strength of air-dried wood con- taining 12% moisture is 2.4, and that of kiln-dried wood containing 34% moisture is 2.9. Thus, it is important when consulting tables of strength of timber to know the percentage of moisture contained in 180 WOOD AND CAST-IRON COLUMNS the samples tested. Generally, this percentage amounts to about 18% in ordinary commercial stock. The table on page 128 gives the ultimate compressive strengths of the more common kinds of timber, together with their moduli of elasticity. SHORT POSTS A post, or column, may in its elementary form be con- sidered as a cubical or rectangular block, as shown in Fig. 1. If the post does not exceed in length from six to ten times the smallest dimension of its cross-sectional area, it~ is designated asa short post, or column. The load that a short post may safely carry may be estimated by multiply- ing its sectional area, in square inches, by the safe unit compression of the material parallel to the grain. The ultimate unit values for compression are given in the table on page 128. A factor of safety of. 5 is generally used, but in some instances it may Fic. 1 be good practice to use 6. The proper factor of safety to choose is usually governed by the conditions to be met. ExamPpLe.—A short post of Georgia yellow pine is 12 in. square and 6 ft. long. What safe load will it support while standing on end? The factor of safety is 5. SoLuTIon.—The ultimate strength of Georgia yellow pine is 5,000 lb.; hence, the safe unit compressive stress is 5,000+5 =1,0001b. The area of the post is 12 in. x 12 in.=144 sq. in. Therefore, the safe load is 144 x 1,000 = 144,000 Ib. Posts under compression develop more strength if the end surfaces are true and level. The tendency then is to resist WOOD AND CAST-IRON COLUMNS 181 compression equally, and not to crush at one place before the remainder of the section can be brought under compres- sion, as would be the case if the bearing surfaces were uneven and rough. LONG POSTS If the length of a post is over ten times its dinrabter or the width of its narrowest side, it is termed a long post. A post of this length, if not secured against yielding sidewise, is liable to bend before breaking, as shown in Fig. 2 (a). In this case, the compressive stress is not. | uniformly distributed over the cross- sectional area of the post, but will de- crease from a maximum value at the concave side of the post to a minimum value at the convex side. Or, if the bending proceed far enough, the com- pressive stress at the convex side may ‘change into one of tension. In some cases, the post will split, as shown in Fig. 2 (b), the two halves bending inde- pendently. The formula generally used for long square or rectangular wooden columns with flat ends, deducted from elaborate tests made on full-sized specimens at the (b) Watertown Arsenal, is: ’ Fic. 2 Si *s~T00d in which u is the ultimate strength of post per square inch of sectional area; s, the ultimate compressive strength of mate- rial, in pounds per square inch; /, the length of post, in inches; and d, the dimensions of least side of post, in inches. EXaMPLE.—A white-pine post with flat ends is 10 in. square and 20 ft. long. Using a factor of safety of 6, what safe load will the post support? SoLuTIon.—The ultimate compressive strength of white pine parallel to the grain is 3,500 lb. per sq. in. Inserting the several values in the formula, 182 WOOD AND CAST-IRON COLUMNS 3,500 X 240 u= 3,500 — poaian la = 2,660 lb. 100 x 10 Since the factor of safety is 6, the safe bearing value per square inch of sectional area is 2,660+6=4434 lb. The area of the post being 100 sq. in., the safe load is 100 x 4434 = 44,333 Ib. The column formulas in general use do not give a direct method of calculating the dimensions of a post that will safely support a given load. The usual method of obtain- ing this information is to assume values for the dimen- sions of the post; substitute these values in the formula, and then solve for u, the ultimate average compression per square inch of sectional area of post. If the assumed dimen- sions give a value of u that is satisfactory for the given con- ditions, they are accepted as ‘correct. If, however, the resulting value of u is smaller than desirable, it shows that the sectional area is too small. Larger dimensions must - then be chosen and the solution repeated until a satisfactory result is obtained. If, on the contrary, the value of u is much greater than the required ultimate strength per square inch of the post sec- tion, a smaller cross-sectional area is chosen and the corre- sponding value of wis found. After a few trials, a size that gives a satisfactory stress for the given conditions is found. ExaMpLeE.—Design to the nearest inch a white-oak post that is to be 15 ft. long and that is to carry a load of 40,000 Ib. with a factor of safety of 5. The post is to be square in cross-section. SoLUTION.—Since a factor of safety of 5 is to be used, the required post must crush under a load of 5X 40,000 = 200,000 lb. The ultimate compressive strength of white oak, from the table on page 128, is 5,000 lb. As a trial, first try a 7” X7” post. Substituting the correct values in the preceding formula, z 5,000 x 15 x 12 . u= 5,000 — = 3,714 lb. per sq. in. 100 X 7 The ultimate strength of the post is therefore 3,714 X7X7=181,986 lb. But the required’ ultimate strength is i 2 WOOD AND CAST-IRON COLUMNS 183 200,000 lb. Therefore, a 7”X7” post is not strong enough. Next, try a 10”X10” post. Thus, 5,000 X 15 x 12 100 x 10 The ultimate strength of this post is therefore 4,100 x 10 xX 10=410,000 lb. Since this value is greater than 200,000, the post is safe; but perhaps a smaller post would also fill the requirements. Therefore, try an 8” X8” post. Thus, 5,000 X 15 X 12 ; u=5,000 — = 3,875 lb. per sq. in. 100 x8 The ultimate strength of this post is therefore 3,875 X8X8 = 248,000 lb. Since this result is greater than the required ultimate strength, the post is strong enough. Moreover, it has been found that a 7”X7” post is not strong enough. Therefore, unless the timber be cut to fractions of an inch, the 8” X 8” post is the smallest post that will fulfil the require- ments. If the formula just given is transposed so as to read u=5, = 4,100 lb. per sq. in. l oe u=s | 1————], the factor | 1———— } may be calculated 100 d 100 d for various values of / and d and arranged in the form of a table, as shown on pages 184-186, that will prove of great assistance when using the formula. In this table, the first column contains various lengths of posts, in inches, and in the top horizontal row are values of the least thickness of a post, in inches. In order to find the factor for a given post, first find the nearest length in the first column; then proceed from this value to the right until a point is reached that is below the least dimension in width. The value found at this point is the factor desired. ExampLe.—A 12” X14” Georgia-pine post is 18 ft. long. What safe load will it carry? SoLutTion.—According to the table, the ultimate strength per square inch for Georgia pine is 5,000 lb. The length of the post, in inches, is 18 X 12=216, and the area of the post is 12X14=168 sq. in. According to the table, the factor l is 821. Inserting this value in the f la; st ——— is nserting this value in the formula, u s( 100 :) 9T oT lat &T él 006° | 068" | 8Z8" | E98" | EFS G68" | €88" | 698" | 08 006° | 688" | $28" | 298 ¥68" | I88" | 798 006' | 288" | TZ8 68" | 6248 006° | 988 £68" 006° II Ot 6 8 Z £9" OrT 0g9° gor 299° OOT €89° G6 OOL 06 LIL g8 €eL° | 009° 08 OsZ’ | $c9" GL 292° | 0S9" OL €8Z° | $Z9° g9 008° | O02 09 LTS" | GGL gg 8" | OSZ" Og oss’ | G22" cP 498° | 008° | 009° | OF €88° | Ges" | OS9" | oe 006° | OG8" | OOL | OF ¢L8° | OGL’ | GZ 006° | 008" | 0z OSs" | ST 006° | OT € a T SeyoUuT Ut ‘ssoUyoIyyT, Jsevo’T SNAWN1IOO NAGOOM UVINONVLOUN AOA SINVISNOD 289° | e¢9' | 769° | 0S9" 002’ | Lg9° 902° | £99" SIZ | TL9° 6IL' | 629° ZL | 989° T@Z' | 869° sez | O02" PPL | LOL’ OSL: | FIL 9S2° | TZ" 292 | 6ZL" 692° | 9&2" CLL | SPL" I8Z' | OGZ° L8L° | LGL" P6L | FOL’ oos’ | T22° 908° | 622° erg | 982" 618° | $62" zs" | 008" Tes° | 208" ges’ | PIS" ers" | 1Z8" gs’ | 6z8" 9¢8° | 988° 009° L19 #t | et | at | ir | or | 6 8 Z 9 c J ee I SoyouyT Ul ‘ssoUNo,T, Jsve’] eS (panuyuo))—SNWNTOO NAGOOM UVINONVLOAY AOA SLNVISNOO WOOD AND CAST-IRON COLUMNS 187 =5,000 X .821=4,105. The ultimate strength of the post is therefore 168 X 4,105 =689,640 lb. - With 5 as a factor of safety, the safe strength of the post is 689,640+5 = 137,928 lb. : CAST-IRON COLUMNS COLUMN FORMULAS Cast-tron columns are most frequently used in buildings of moderate height, but in some cases they have been used in buildings of sixteen, and even more, stories. The uncer- tain strength of cast iron has compelled the adoption of a low unit stress per square inch, or, in other words, a high factor of safety. The safe loads that cast-iron columns will carry can be obtained by the use of the table on pages 188-189. The first column of this table gives the external diameters of various columns, and the second column, the several thick- nesses that the column of a given diameter is likely to possess. ExampLe.—A hollow, cylindrical column is 18 ft. long, and has an external diameter of 14 in. and an internal one of 114 in. (a) What safe load will it support? (6) What load will it support if the internal diameter is 11 in.? , 14—11.5 SoLuTION.—(a) The thickness of the metal is — 3 =1.25 in. Proceeding in the table from 14 in the first column to the value 1} in the second column, and then con- tinuing to the right until the column headed 18 is reached, the value 386 is found. This shows that the column will support a safe load of 386,000 lb. (6) In a column having an internal diameter of 11 in., the thickness of the metal is =u in. Proceeding to the right from the value 14 in the second column of the table, the value 454 is found in the column headed 18; hence, the safe load for this column is 454,000 Ib. It is thus evident that a difference in the thickness of the WOOD AND CAST-IRON COLUMNS 188 ¥6'62T 8¢ TP Zee | 193 | 18% | TOE | ZZE | SVE | SIE | OSE | FEE val 99 6IT 62° 8E €2z | OFZ | 8Ga | L22 | 26a | STE | Eee | OSE | E9E | iT 90° 60I 06° FE €0Z | 612 | 986 | SSG | OLZ | L8S | FOE | G6TE | TEE bal 61°86 or ' Is €8T | Z6L | SIZ | 86% | Shs | 69% | FL ) LBS | 86zG T 16°98 €8° 1% ZOL | SZT | S8T | GOS | 9IS | OFS | VHS | FSS | 89S 4 Il 8° ZOT 9€ FE 002 | Z12 | S82 | FSS | ELS | 164 | 8OE | ESE il €0° 86 20" 1S ZSL | S6L | SIZ! SEZ | 6S | 99S | T8S | GbS™ -al 8E°88 8Z° 8% POT | BLT | FEL | 602 | GZS | OFS | ESS | 99G [ 8é°8Z 80°SG OFT | SSL | ZZT | GST | 66L | ETS | SGs | 9EZ ¥ €1'°89 08° 1G LIL | S&L | 6FL | TOT | SLZT | SST | S6T | 90% ; OL 16°98 $8° 2% ZOL | LLL | P6L | T1lS | 836 | HHS | 8G I eo 82 S1'°Sm OFT | O9T | GZT | OBL | 90S’ | 02GB 4 EES 1 18°69 PE SS OST | SL | 9ST | 69T | EST | 96T | LOG £ Gl’ 09 tr 61 EI | ZL | SET | TST | O9T | OLT | O8T E 6 GL°89 66°14 SZL | Sb | LST | ZZT | 98ST | 006 T GG‘ 19 69 6T FIT | 9ZT | GEL | SST | 99T | SAT ¢ 8e°s¢ 80° LT 66 OTT | ZOE | SEL | ST | SST H 8 €9°S¢ F891 86 OTL | SZL | 9ET | 6FT £0'9F SL FT 98 96 SOT | 6IT | O€1 4 y. 0° FF 60° FI zs_«| eG | «LOL | GIT | hE G9 SE LES ZL 68 $6 cOL t 9 te FS ® > : ons a ge zz | oc | St | or | ot | ot | Or | 8 9 BE wZo Bese | 5 os we |rae a 5 os 8d 88 qa0,J ur ‘uUINJOD Jo 44BuUe'] 0% & 8 o “ oo 8 n Lou) i (= Malns fo soj90.q “Spus 10144) SNIN'109 NOUI-LSVO TVOIMGNITAO ‘MOTION WOd ‘SANNOd 40 SANVSNOHL NI ‘SaVOT FAVS 139 WOOD AND CAST-IRON COLUMNS 20 A ona tot tod t= enlao ca aniad <-* eaten ~domnalb enteseaian muclancsta foo wlan cate fo0 rte i i ce oe ee ee ee ee ee ee oe oe ee ee nn | 8T 9T tI €T él syog youy-f Joy posog sejoy] san’q jo ssouyory yy, ees SHOT youy-f 10} palog ssjoy{ 190 s3n’q jo ColHOo he ssouyoy | aM TO CAST-IRON COLUMNS Ble|plelFiclalxk 4 4 i } DIMENSIONS, IN INCHES, OF STANDARD CONNECTIONS b WOOD AND CAST-IRON COLUMNS 191 metal of 1.5—1.25=.25 in. gives an increase in strength of 454,000 — 386,000 = 68,000 Ib. The table may also be used for calculating the strength of columns when a factor of safety other than 8 is to be used. Let W be safe load given in the table: W; the safe load corresponding to another factor of safety; and 7, the new factor of safety. Then, W:Wi=7:8, 8SW and W,=— f _ Wit 8 ExamPLe.—A hollow, cast-iron column of 13-in. external diameter and 1}-in. metal is 18 ft. long. Assuming that the factor of safety is 6, find the safe load. SoLUTION.—From the table W=343,000; hence, accord- ing to the formula, 8 X 343,000 W.= ara or = 457,000 1b., nearly. Many concerns have their own standard designs for column connections and brackets. These are usually embodied in tables that give the required dimensions. The accompany- ing table gives the standard dimensions of brackets on cast-iron columns for I-beam connections, both for double and for single beams. The top surface of the shelf should have a pitch away from the column of 4 in. to the foot to allow for the deflection of the beam. The top surface of the shelf should have a pitch away from the column of } in. to the foot to allow for the deflection of the beam. As the holes in the column are cored, it will usually be necessary to have the beams drilled in the field in order to insure alinement. In this table the values given in the columns marked A, B, C, etc. are the various dimensions for brackets, these dimensions being represented by corresponding letters in the figures accompanying the table. Thus, for a 12-in. I-beam connection, the distance from the bottom of the beam flange 192 SAND AND CEMENT to the center of the outside bolt ot the vertical lug should be 3 in.; the pitch of the bolts, 3 in.; the projection of the bracket beyond the column, 44 in.; the depth of the ver- tical leg of the bracket, 7? in.; etc. SAND AND CEMENT aS CEMENTING MATERIALS Any substance that becomes plastic under certain treat- ment and subsequently reverts to a tenacious and inelastic condition may, in a broad sense, be termed a cement, How- ever, nearly all the cementing materials employed in build- ing construction are obtained by the heating, or calcination, as it is called, of minerals composed wholly or in part of lime. The different composition of these minerals, as well as the properties of the calcined products, enables the various resulting substances to be classified as. limes, hydraulic cements, plasters, and miscellaneous cements. Although all these materials have cementing properties, the term cement is commonly used to apply only to the group made up of hydraulic cements, hydraulic meaning that these substances possess the ability to set, or become hard, under water. Limes and hydraulic cements (commonly called simply cements) are composed essentially of oxide of calcium, or lime, generally called quicklime, with which may be com- bined certain argillaceous, or clayey, elements, notably silica and alumina, it being to these elements that the hydraulic properties of certain of these materials are due. The quantity of silica and alumina present in these substances enables them to be classified as common limes, hydraulic limes, and cements. The ratio of the quantity of sflica and alumina present in these materials to the quantity of lime is called the hydraulic index. In common limes, this index is less than y%; in hydraulic limes, it lies between 7% and 4%; and in cements, it exceeds y%. These limes merge into each other so grad- ually, however, that it is often difficult to distinguish the dividing line between them. SAND AND CEMENT 193 LIMES The commercial varieties of lime may be classified as common, hydrated, and hydraulic. The common limes, also called quicklimes, may be subdivided into rich, or fat, lime, and meager, or poor, lime. Common Limes.—The grade of common lime known as fat, or rich, lime is almost pure oxide of calcium, CaO, and contains only about 5% .of impurities. It has a specific gravity of about 2.3 and a great affinity for water, of which it absorbs about one-quarter of its weight. This absorp- tion is accompanied by a great rise in temperature, by the lime bursting, and by the giving off of vapor. The lime finally crumbles into a powder. This powder occupies from two and one-half to three and one-half times as much volume as the original lime, the exact amount depending on its initial purity. When the lime is in this plastic state, it is said to be slaked. It is then unctuous and soft to the touch, and from this peculiarity it derives the name of fat or rich. Meager, or poor, lime consists of from 60 to 90% of pure lime, the remainder being impurities, such as sand or other foreign matter. These impurities have no chemical action on the lime, but simply act as adulterants. Compared with fat lime, poor lime slakes more slowly and evolves less heat. The resulting paste is also thinner and not so smooth, greatly resembling fat slaked lime mixed with sand. Poor lime is not so good for building purposes as fat lime, nor has it such extensive use. Hydrated Lime.—The class of lime called hydrated lime (calcium hydrate) is merely thoroughly slaked fat lime dried in the form of a fine powder, Ca(OH)»s. It is used exten- sively in conjunction with cement for making mortar, and also in the sand-lime brick industry. Hydraulic Limes.—Limes that contain enough quick- lime to slake when water is added, and enough clay or sand to form a chemical combination when wet, thus giving them the property of setting under water, are called hydraulic limes. Limes of this class are made by burning limestones con- taining from 5 to 30% of clay or sand. They are often 194 SAND AND CEMENT considered as divided into three classes, namely, feebly hydraulic, ordinarily hydraulic, and eminently hydraulic, in proportion to the quantity of argillaceous materials present. The slaking qualities vary from slaking in a few minutes with considerable heat after water is added, in the feebly hydraulic, to slaking only after many hours, with practically no evolution of heat and without cracking or powdering, in the eminently hydraulic. The time of setting under water also varies from setting as hard as soap in 2 years, with the feebly hydraulic, to becoming as hard as stone in 3 or 4 days, with the eminently hydraulic. If carbonate of magnesia is present in the lime, it reduces the energy of the slaking, but increases the rapidity of the setting and the ultimate strength when set. CEMENTS Cement may be divided into four general classes: Port- land, natural, puzzolan (also called pozzuolana), and mixed. The relative importance of each cement is indicated by the order in which it is named. Portland cement may be defined as the product resulting from the process of grinding an intimate mixture of cal- careous (containing lime) and argillaceous (containing clay) materials, calcining (heating) the mixture until it starts to fuse, or melt, and grinding the resulting clinker to a fine powder. It must contain not less than 1.7 times as much lime by weight as it does of those materials which give the lime its hydraulic properties, and must contain no materials added after calcination, except small quantities of certain substances used to regulate the activity or the time of setting. Natural cement is the product resulting from the burning and subsequent pulverization of an argillaceous limestone or other suitable rock in its natural condition, the heat of burning being insufficient to cause the material to start to melt. Puzzolan cement is a material resulting from grinding together, without subsequent calcination, an intimate mixture of slaked lime and a puzzolanic substance, such as SAND AND CEMENT 195 blast-furnace slag or volcanic scoria. The only variety of puzzolan cement employed at all extensively in American practice is slag cement. This cement is made by grinding together a mixture of blast-furnace slag and slaked lime. The slag used for this purpose is granulated, or quenched, in water as soon as it leaves the furnace, which operation drives off most of the dangerous sulphides and renders the slag puzzolanic. Mixed cements cover a wide range of products obtained by mixing, or blending, the foregoing cements with each other or with other inert substances. Sand cements, im- proved cements, and many second-grade cements belong to this class. Mixed cements. however, are of comparatively little importance. Properties of Cements——The hydraulic cements differ from the limes in that they do not slake after calcination, and that they set, or harden, under water. They can be formed into a paste with water without any sensible increase in volume and with little, if any, disengagement of heat. They do not shrink appreciably in hardening, so that the sand and broken stone with which they are mixed are employed merely through motives of economy and not, as with limes, of necessity. The color uf the different grades of cement is variable, but in certain cases it is distinctive. Portland cement is a -dark-bluish or greenish gray; if it is a light yellow, it may indicate underburning. Natural cement ranges in color from a light straw, through the grays, to a chocolate brown. Slag cement is gray with usually a tinge of lilac. In general, however, the color of cement is no criterion of its quality Cement is packed either in wooden barrels or in cloth or paper bags, the latter being the form of package most com- monly employed. A barrel of Portland or of slag cement contains the equivalent of 4 bags, while but 3 bags of natural cement equals a barrel. The average weights of the various cements are given in the table on page 196. In proportioning mortar or concrete by volume, the com- mon assumption is that a bag of Portland cement occupies OG, CU, iit: 596 SAND AND CEMENT AVERAGE WEIGHTS OF HYDRAULIC CEMENTS Net Net Weight per Cubic Foot Kind of | Weight | Weight Pounds Cement of Bag of Barrel Pounds Pounds Packed Ines Portland ... 94 376 100-120 70-90 Natural. ... 94 . 282 75-95 45-65 SOG fos tk 823 330 80-100 55-75 Portland cement may be distinguished by its dark color, heavy weight, slow rate of setting, and greater strength. Natural cement is characterized by lighter color, lighter © weight, quicker set, and lower strength. Slag cement is somewhat similar to Portland, but may be distinguished from it by its lilac-bluish color, by its lighter weight, and by the greater fineness to which it is ground. Portland cement is adaptable to any class of mortar or concrete construction, and is unquestionably the best mate- rial for all such purposes. Natural and slag cements, how- ever are cheaper, and, under certain conditions, may be sub- stituted for the more expensive Portland cement. All heavy construction, especially if exposed, all reinforced- concrete work, sidewalks, concrete blocks, foundations of buildings, piers, walls abutments, etc. should be made with Portland cement. In second-class work, as in rubble masonry, brick sewers, unimportant work in damp or wet situations, or in heavy work in which the working loads will not be applied until long after completion, natural cement may be employed to advantage. Slag cement is best adapted to heavy foundation work that is immersed in water or at least continually damp. This kind of cement should never be exposed directly to dry air, nor should it be subjected either to attrition or impact. SAND AND CEMENT 197 SAND AND ITS MIXTURES SAND Sand is an aggregation of loose grains of crystalline struc- ture, derived from the disintegration of rocks. It is called stlicious, argillaceous, or calcareous, according to the char- acter of the rock from which it is derived. Sand is obtained from the seashore, from the banks and beds of rivers, and from land deposits. The first class, called sea sand, contains alkaline salts that attract and retain moisture and cause efflorescence in brick masonry. This efflorescence is not at first apparent but becomes more marked as time goes on. It can be removed temporarily at least by washing the stone- work in very dilute hydrochloric acid. The second, termed river sand, is generally composed of rounded particles, and may or may not contain clay or other impurities. The third, called pit sand, is usually composed of grains that are more angular; it often contains clay and organic matter. When washed and screened, it is a good sand for general purposes. Sand is used in making mortar because it prevents excess- ive shrinkage and reduces the quantity of lime or cement required. Lime adheres better to the particles of sand than it does to its own particles; hence, it is considered that sand adds strength to lime mortar. On cement mortar, on the contrary, sand has a weakening effect. Properties of Sand.—The weight of sand is determined by merely filling a cubic-foot measure with dried sand and obtaining its weight. Dry sand weighs from 80 to 120 lb. per cu. ft.; moist sand, however, occupies more space and weighs less per cubic foot. The weight of sand is more or less dependent on its specific gravity and on the size and shape of the sand grains, but, other things being equal, the heaviest sand makes the best mortar. The specific gravity of sand ranges from 2.55 to 2.80. For all practical purposes the specific gravity may be assumed to be 2.65 with little danger of error. By percentage of voids is meant the amount of air space in the sand. Structurally, it is one of the most important 198 SAND AND CEMENT properties of sand. The greater these voids, the more cement paste will be required to fill them in order to give a dense mortar. The percentage of voids may be determined by observing the quantity of water that can be introduced into a vessel filled with sand, but it is best computed as follows: - 100 X weight per cubic foot percentage of voids=100— sin wna daan HX =— 62.5 X specific gravity EXAMPLE.—What is the percentage of voids in a sand having a specific gravity of 2.65 and weighing 105 lb. per cu. ft.? : SoLuTION.—Substituting in the formula, the percentage of voids is 100 X 105 62.5 X 2.65 The percentage of voids depends principally on the size and shape of the sand grains and the gradation of its fine- ness, and hence will vary from 25 to 50%. Sand contain- | ing over 45% of voids should not be used to make mortars. The shape of the grains of sand is of chief importance in the influence that the sand exerts on the percentage of voids. Obviously, a sand with rounded grains will compact into a more dense mass than one whose grains are angular or flat like particles of mica. Therefore the more nearly the grains approach the spherical in shape, the more dense and strong will be the mortar. This fact is contrary to the common opinion on the subject. The fineness of sand is determined by passing a dried sample through a series of sieves having 10, 20, 30, 40, 50, 74, 100, and 200 meshes, respectively, to the linear inch: The result of this test, expressed in the amount of sand passing each sieve, is known as the granulometric composition of the sand. Material that does not pass a 4-in. screen is not considered to be sand, and should be separated by screening. Sand that is practically all retained on a No. 30 sieve is called coarse, while 80 or 90% of sand known as fine will pass through this sieve. Fine sand produces a weaker mortar than coarse sand, but a mixture of fine and coarse sand will surpass either one. =100—63.4=36.6 SAND AND CEMENT 199 The purity, or cleanness, of sand may be roughly ascer- tained by rubbing it between the fingers and observing how much dirt remains. To determine the percentage of the impurities more accurately, a small dried and weighed sam- ple is placed in a vessel and stirred up with water. The sand is allowed to settle, the dirty water poured off, and the process repeated until the water pours off clear. The sand is then dried and weighed. The loss in weight gives the quantity of impurities contained in the sand.. The presence of dirt, organic loam, mica, etc. is decidedly injurious and tends to weaxen the resulting mortar. Clay or fine min- eral matter in small proportions may actually result in increased strength, but excessive quantities of these mate- rials may be a possible source of weakness. The best mod- ern practice limits the quantity of ampurities found by this washing cest to 5%. It is advisable, prior to the selection of a sand, to deter- mine what its strength will be when made into mortar. Preparation of Sand.—Sand is prepared for use by (1) screening. to remove the pebbles and coarser grains the fineness of the meshes of the screen depending on the kind of work in which the sand is to be used; (2) washing, to remove salt, clay, and other foreign matter; and (3) drying if necessary. When dry sand is required, it is obtained by evaporating the moisture either in a machine, called a sand dryer, or in large, shallow, iron pans supported on stones, with a wood fire placed underneath. LIME AND CEMENT MORTARS Mortars are composed of lime or cement and sand mixed to the proper consistency with water. The proportions of the ingredients depend on the character of the work in which the mortar is to be used. In proportioning mortar, the quantities of the separate ingredients are usually designated by a ratio, such as 1-1, 1-2, 1-8, etc. Thus, 1-2 signifies that 1 part of lime or cement is used to 2 parts of sand; etc. For great accuracy these measurements should be made by weight, but they are usually made by volume, which is almost the same thing. 200 . SAND AND CEMENT Lime Mortars.—In lime mortar, besides effecting an econ- omy, the presence of sand is necessary to prevent the shrink- age that would otherwise occur during the hardening of the paste. When a mortar is made of lime and sand, enough lime should be present to just cover completely each grain of sand. An excess of lime over this quantity will cause the mortar to shrink excessively on drying, while a deficiency of lime will produce a weak and crumbly mortar. The cor- rect quantity of lime depends on the character of the ingre- dients, the method of treatment, and, to some extent on the judgment of the builder. The mixtures employed vary from 1-24 to 1-5. Building laws in many municipalities require the use of a 1-3 mixture, and for most materials this proportion will be found satisfactory, although for rich, fat limes a 1-34 or a 1-4 mixture is sometimes preferable. In mixing lime mortar,a bed of sand is made in a mortar box, and the lime distributed as evenly as possible over it, first measuring both the lime and the sand in order that the proportions specified may be obtained. The lime is then slaked by pouring on water, after which it should be covered with a layer of sand, or, preferably, a tarpaulin, to retain the vapor given off while the lime is undergoing the chemical reaction of slaking. Additional sand is then used, if necessary, until the mortar attains the proper pro- portions. Care should be taken to add just the proper quantity of water to slake the lime completely to a paste. If too much water is used, the mortar will never attain its proper strength, while if too little is used at first, and more is added during the process of slaking, the lime will have a tendency to chill, thereby injuring its setting and hardening properties. Rather than make up small batches, it is considered better practice to make lime mortar in large quantities and to keep it standing in bulk so that it can be used as needed. Lime mortar is employed chiefly for brickwork of the second class and its use is continually decreasing as that of cement increases. It is absolutely unsuitable for any important construction, because it possesses neither strength SAND AND CEMENT 201 nor the property of resisting water. It cannot be used in damp or wet situations, nor should it ever be laid in cold weather, as it is very susceptible to the action of frost, being much injured thereby. Moreover, since it hardens by the action of dry air, only the exterior of lime mortar ever becomes fully hardened, so that anything like a concrete with lime as a matrix is impossible. However, for second- class brickwork, such as is commonly used in the walls of smaller buildings, lime mortars are economical and suf- ficiently good. The strength of lime mortars is extremely variable, depend- ing on the ingredients themselves and on their treatment, environment, etc. Moreover, it is unsafe to figure a lime- mortar joint as possessing much strength, since only a part of the joint is hardened and capable of developing any strength at all. The tensile strength of thoroughly hard- ened 1-3 lime mortars averages from 40 to 70 lb. per sa. in., and the compressive strength from 150 to 300 lb. Cement Mortars.—The sand for all mortars should be clean, of suitable size and granulometric composition. For structures designed to withstand heavy unit stresses, or for those intended to resist either the penetration of moisture or the actual pressure of water, the selection of the sand should be most carefully made. Generally, it is not advi- sable to use asand containing over 5% of loam by the wash- ing test, nor one that soils the fingers when it is rubbed between them. Very fine sand, such as is found on the sea- shore, should not be employed in mortar unless it is intended simply for pointing or for grouting. A simple method of determining the best sand for cement mortar is to prepare mixtures of the cement, sand, and water, using the same quantities in each case, and fhen to place each mixture in a measure; that mixture giving the least volume of mortar may be considered to contain the most desirable sand for use. Limestone screenings, brick dust, crushed cinders, etc., are.sometimes substituted for sand in making mortars, and, if care is taken in their selection, they may prove economical and entirely suitable for certain purposes. 202 | SAND AND CEMENT The theory of the composition of a correctly proportioned mortar is that the cement paste will just a little more than fill all the voids between the particles of sand, thus giving an absolutely dense mortar at the least expense. The cor- rect proportion of cement to sand, therefore, is more or less variable, depending on the granulometric composition of the sand. Since, however, Portland-cement paste that has set weighs nearly as much as sand, and since the average sand contains about 30 to 40% of voids, it is evident that 1-3 mixtures most nearly approach the best and most economical proportion. Mortars, however, are made in proportions varying from 1-1 to 1-8. The richer mixtures are used for facing, point- ing, waterproofing, granolithic mixtures, etc., the 1-2 mix- ture being usually made for such purposes. The leaner mixtures are used for rough work, filling, backing, etc., but should never be employed where either much strength or much density is desired. Natural-cement mortars are commonly made 1 part of sand less than Portland-cement mortars intended for the same purpose; that is, where a 1-3 Portland-cement mortar would be used, a 1-2 natural mortar would be required, although natural-cement mortars should be decreased by about 2 parts of sand to equal the strength of Portland. In other words, a 1-4 Portland mortar closely equals the strength of a 1-2 natural mortar. Puzzolan cements are usually proportioned the same as Portlands. Cements are commonly proportioned by volume, the unit volume of the cement barrel being assumed. Ifa1-3 mortar is desired, a box having a capacity of 10.8 cu. ft. is filled with sand and mixed with 4 bags or 1 bbl. of cement. A box 3 ft. 3x4 in. square and 1 ft. deep will have a capacity of very nearly 10.8 cu. ft. and, besides, makes a convenient size of box for actual work. For general purposes, the mortar should be of a plastic consistency—firm enough to stand at a considerable angle yet soft enough to work easily. Wet mortars are easiest to work and are the strongest. However, they are subject to greater shrinkage, are slower setting, and are more easily SAND AND CEMENT 203 attacked by frost. Dry mortars, on the other hand, are often friable and porous. In the following table are given the quantities of materials required to produce 1 cu. yd. of compacted mortar. The proportions are by volume, a cement barrel being assumed to contain 3.6 cu. ft. MATERIALS REQUIRED PER CUBIC YARD OF MORTAR i a i ee ; : Portland Cement} Loose Sand Kind of Mixture Barrels Cubic Yards } 1-1... 4.95 .65 - 4-2.. 3.28 88 er i—3. 2.42 1.01 1-4... 1.99 1.06 : 1-5. . 1.62 1.11 1-6.. 1.34 1.15 1-7... 1.18 1 i) Wf 1-8.. 1.05 1.18 XAMPLE.—How much cement and sand will be required to obtain 8.5 cu. yd. of 1-3 Portland-cement mortar? SoL_uTion.—According to the table, 1 cu. yd. of a 1-3 Port- land-cement mortar requires 2.42 bbl. of cement; therefore, 8.5 cu. yd. will require 8.5 2.42=20.57 bbl. of cement. Also, since 1 cu. yd. of a mixture of this kind requires 1.01 cu. yd. of sand, the quantity of sand required will be 8.51.01 =8.59 cu. yd. Mortar that is to be mixed by hand is prepared on a plat- form or in a mortar box. The sand is first measured by [ means of a bottomless box with handles on the sides. After filling the box, the sand is struck off level, the box lifted up, and the sand spread in a low, flat pile. The required num- ber of bags of cement are then emptied on the sand and spread evenly over it. The pile is then mixed with shovels, working through it not less than four times. After this operation, the dry mixture is formed into a ring, or crater, and the water intended to be used is poured into the center. The material from the sides of the basin is then shoveled 204 SAND AND CEMENT into the center until the water is entirely absorbed, after which the pile is worked again with shovels and hoes until the mixture is uniform and in a plastic condition. Another method of mixing, where a mortar box is used, is to gather the mixed dry materials at one end of the box and pour in the water at the other end drawing the mixture into the water with a hoe, a little at a time, and hoeing until a plastic consistency is obtained. Properties and Uses of Cement Mortars.—The strength of a mortar is measured by its resistance to tensile, compressive, TENSILE STRENGTH OF CEMENT MORTARS Tensile Strength, in Pounds per Square Inch Proportions Portland Cement | Natural Cement Cement Sand ae Parts 7 da. 28 da.|3 mo.| 7 da. |28 da.|3 mo. 1 1 450 | 600 | 610 | 160 | 245 | 280 it 2 280 | 380 | 395 | 115 | 175 | 215 1 3 170 | 245 | 280 85 | 130 | 165 1 4 125 | 180 | 220 60 | 100 | 135 1 5 80 | 140 | 175 40 75 | 110 1 6 50 | 115 | 145 25 1 Z 30 95 | 120 15 50 75 1 8 20 70 | 100 10 45 65 cross-breaking, and shearing stresses, and also by determi- nations of its adhesion to inert surfaces, its resistance to impact, abrasion, etc. There is no definitely fixed ratio between the strength of mortar subjected to these different stresses, but there is nevertheless a close relation between them, so that, practically, it may be assumed that if a mor- tar shows either abnormally high or low values in any one test, the same relation will develop when tested under other stresses. In practice, therefore, the strength of mortar is SAND AND CEMENT 205 commonly determined through its resistance to tensile stresses, and its resistance to other forms of stress is com- puted from these results. The tensile strength of mortar has been shown to vary with the character of its ingredients, with its consistency, its age, and with many other factors. In the accompany- ing table is given a fair average of the tensile strength that may be expected from mortars of Portland and natural cements that are made in the field and with a sand of fair quality but not especially prepared. The strength of Portland-cement mortar increases up to about 3 mo.; after that period, it remains practically con- stant for an indefinite time. Natural-cement mortar, on the other hand, continues to increase in strength for 2 or 3 yr., its ultimate strength being about 25% in excess of that attained in 3 mo. The strength of slag-cement mortar averages about three-quarters of that of Portland-cement mortar. The compressive strength of cement mortars is usually given in textbooks as being from eight to ten times the tensile strength. This value is rather high for the average mortar, a ratio of from 6 to 8 being one more nearly realized in prac- tice. The ratio increases with the age and richness of the mortar, and varies considerably with the quality of the sand. Portland-cement mortars of 1-3 mixture that are 3 mo. old develop, on an average, a compressive strength of about 1,800 lb. per sq. in., while 1-2 natural-cement mortars average about 1,600 lb. The strength of mortars in cross-breaking and shear may be taken at about one and one-half to two times the tensile strength, with a fair amount of accuracy. The adhesion of mortars to inert materials varies both with the character of the mortar and with the roughness and porosity of the surfaces with which they are in contact. The adhesion of 1-2 Portland-cement mortar, 28 da. old to sandstone averages about 100 lb. per sq. in.; to limestone, 75 lb.; to brick, 60 lb.; to glass, 50 lb.; and to iron or steel, 75 to 125 Ib. Natural-cement mortars have nearly the same adhesive strength as those made of Portland cement. 206 . SAND AND CEMENT In bricklaying and in other places in which mortar is employed it is frequently desired to use a material that is more plastic or smoother than pure cement mortar. This quality is usually obtained by adding from 10 to 25% of lime to the mortar. This addition of lime not only renders the mortar more plastic, and hence easier to work, but also increases both its adhesive strength and its density, which assists in making the mortar waterproof. Hydrated lime is to be preferred for use in cement mortar, because its complete slaking is assured. Hydrated lime may also be readily handled and measured on the work. Occasionally, small quantities of cement are added to lime mortars so as to make them set quicker and to increase their strength. Such mixtures, however, are not especially economical nor are they convenient in practice. Retempering of Mortar.—Mortar composed of cement, sand, and water soon begins to set and finally becomes hard. When it is desired to use this material, more water has to be added and the mixture worked until it again becomes plastic. This process is called retempering. Laboratory tests generally show that retempering slightly increases the strength of mortar, but the reworking is more thorough as a rule in the laboratory than would be the case in actual work. Any part of the hardened mortar that is not retem- pered is a source of weakness when incorporated in the building. The adhesive strength of cement, moreover, is greatly diminished. by this process For these reasons, it is generally inadvisable to permit the use of retempered mortars; but if they are allowed, great care should be taken to see that the second working is thorough and complete. Laying Mortar in Freezing Weather.—Frost or even cold has a tendency to retard greatly the set of cement mortars. When the temperature, moreover, is so low that the water with which the mortar is mixed freezes before it combines with the cement, it may, if care is not exercised, result in complete destruction of the work. A single freezing is not particularly harmful. because when thawing occurs, the arrested chemical action continues. A succession of alter- nate freezings.and thawings, however, is extremely injurious, . SAND AND CEMENT 207 Nevertheless, Portland-cement mortars may be laid even under the worst conditions if certain precautions are ob- served, but mortars of natural cement should never be used in extremely cold weather, as they are generally completely ruined by freezing. The bad results that arise during mild frosts may be suc- cessfully guarded against by heating the sand and water and by using a quick-setting cement mixed rich and as dry as possible. In extremely cold weather, salt must be added to the water, so as to convert it into a brine that requires a temperature lower than 32° F. to freeze it. The common rule for adding salt is to use a quantity equal to 1% of the weight of the water for each degree of temperature that is expected below 33° F. Thus, at 32° F., a 1% solution would be used, while at 25°, an 8% solution would be required. Solutions greater than 12% should not be employed, and if a temperature below 20° F. is expected, heat must be used in addition to the salt. The finished work should also be protected with canvas or straw. Manure should not be used for this purpose, because the acids it contains tend to rot the cement. Unless the conditions are such as to make it imperative, it is not advisable to lay mortars during freezing weather. Shrinkage of Mortars.—Cement mixtures exposed to the air shrink during the process of hardening, while those immersed in water tend to expand. The shrinkage of ordinary cement mortars is slight, and when they are used as a bonding material it need not be considered. When used as a monolith, as in sidewalks, shrinkage is guarded against by keeping the mortar wet during setting. This can be done by covering with moist straw or by sprinkling the mixture with water. Grouting.— By grouting is meant the process of filling spaces in masonry with a thin, semifluid mixture known as grout. This mixture consists of cement, 1 or 2 parts of sand, and an excess of water. Grout can be used for filling the voids in walls of rubble masonry for backing arches and tunnels, and for filling the joints between paving brick. In fact, it can be used in all places where mortar cannot be laid in the ordinary 208 TESTS ON CEMENT manner. When hardened, grout is weak, friable, and porous. Coloring of Mortars.—Colors are often used in mortars to effect contrasts, or to subdue the glaring tone of cement in sidewalks or in similar situations. Red lead weakens mortar and should not be used. The color of hardened mortar is quite different in appearance from one that is still wet, so that where it is important to secure the cor- rect tints, preliminary trials should be made until the pro- portions desired have been determined. The various materials employed to produce different colors in mortar, together with the quantity required per barrel of cement, are as follows: For gray, 2 lb. of lampblack; for black, 45 lb. of manganese dioxide; for blue, 19 lb. of ultra- marine; for red 22 lb. of iron oxide; for bright red, 22 lb. of Pompeian or English red; and for violet, 22 lb. of violet oxide of iron. TESTS ON CEMENT FIELD INSPECTION In order to determine correctly the structural value of a shipment of cement, an examination in the field is very necessary. A number of packages of cement should be weighed at intervals, and the average weight should never be permitted to fall below 94 lb. per bag, since mortar and concrete are usually proportioned on the assumption of this weight. Each package should also be plainly marked with the brand and name of the manufacturer; those not branded should be discarded, and, if possible, a mixture of different brands should be avoided. A possible indication of inferiority is the presence of lumps throughout the bulk of the material. On standing, cement gradually absorbs moisture from the air. At first this mois- ture is present in merely a minute and harmless state, but eventually it combines chemically with the cement; that is, in the same manner as when cement and water are actually mixed together in practice. In the first condition, lumps usually appear, but they are so soft that they may be readily TESTS ON CEMENT 209 crushed with the fingers, and of course would be entirely broken up when mixed into mortar. When, however, the cement contains lumps that are hard and pebble-like and that can be crushed only with considerable effort, it indicates that chemical action has begun. Cement containing any appreciable amount of these hardened lumps is generally of decidedly inferior quality, and it should never be permitted to enter any important part of a structure. Storing cement too long will tend to weaken it. Cement from 2 to 6 mo. old is usually the safest and will produce the best results. The color of Portland cement, ranging from bluish to yellowish gray, affords no indication of quality except in cases where different shipments or different parts of the same shipment show a variation in color, thus pointing to a lack of uniformity. SAMPLING In securing a sample for testing, the essential point is to get one that will fairly represent the entire shipment whose qualities are to be determined. The common practice is to take a small portion of material from every tenth barrel, or, what is the same thing, from every fortieth bag. When tests are to be made, however, on a shipment of only a few barrels, more packages than one in ten should be opened; and when the shipment is large, say over 150 bbl., it should be sub- divided and each portion tested separately. The bags selected should be taken at random and from different layers and not all from one part of the pile. The cement, moreover, should be taken not only from the top of the packages, but from the center and sides as well. When the cement is contained in barrels, a sampling auger is used to extract the sample, a hole being bored in the staves midway between the heads. After the samples of cement have been taken from the packages they are thoroughly mixed in a can or basin, and this mixed sample is used for the various tests. To make a complete series of tests, the sample should contain from 6 to 8 lb. The cement, after sampling and before testing, ae TESTS ON CEMENT must be well protected, as exposure to heat, cold, dampness, or any other abnormal condition may seriously affect the results. PURPOSE AND CLASSIFICATION OF TESTS In order that a mortar or a concrete made with cement shall give good results in actual construction it must possess two important properties, namely, strength and durability. The primary purpose of cement testing, therefore, is to deter- mine whether any particular shipment of cement possesses sufficient strength and durability to admit of its use in construction. A determination of the quality of cement necessitates the employment of several tests, which may be classified as primary tests and secondary tests. The former tests, which include tests for soundness and tensile strength, are made to give directly a measure of the essential qualities of strength and durability. Unfortunately, neither of these tests is capable of being made with precision. Therefore, the second- ary tests, which include tests to determine the time of setting, the fineness, the specific gravity, and the chemical analysis, are made to obtain additional information in regard to the character of the material. However, with the possible exception of the test of time of setting, the secondary tests have but little importance and only indicate by their results indirectly the properties of the material. PRIMARY TESTS TESTS FOR SOUNDNESS Soundness may be defined as the property of cement that tends to withstand any forces that may operate to destroy or disintegrate it. This property of soundness, or, as it is sometimes called, constancy of volume, is the most important requisite of a good cement. The most common cause of unsoundness in Portland cement is an excess of free or uncombined lime, which crystallizes with great increase of volume, and thus breaks up and destroys the bond of the cement. This excess of lime ra eee yy re Pree Ora ae a -- Ce Ne a eal TESTS ON CEMENT 211 may be due to incorrect proportioning or to insufficient grind- ing of the raw materials, to underburning, or to lack of sufficient storing before use, called seasoning. A certain amount of seasoning is usually necessary, because almost every cement, no matter how well proportioned or burned it may be, will contain a small amount of this excess of lime, which, on standing, will absorb moisture from the air, slake, and become inert. Excess of magnesia or the alkalies may also cause unsound- ness, but the ordinary cement rarely contains a sufficient amount of these ingredients to be harmful. Sulphate of lime is occasionally responsible for unsoundness, but this ingredient usually acts in the opposite direction, tending to make sound a cement that otherwise might disintegrate. The property of soundness is determined in one or more of three ways: by measurements of expansion, by normal tests, and by accelerated tests. Measurements of expansion are made by forming specimens of cement, usually in the shape of prisms, and measuring the change in volume by means of a micrometer screw. At the present time, however, it is believed that expansion is not a sure index of unsoundness, so that this test is seldom employed. Normal tests consist in making specimens of cement mixed with water, preserving them in air or in water under normal conditions, and observing their behavior, The common practice is to make from a paste of neat, or pure, cement on glass plates about 4 in. square, two circular pats, about 3 in. in diameter, 4 in. thick at the center, and tapering to a thin edge. These pats are kept in moist air for 24 hr.; then one of them is placed in fresh water of ordinary tempera- ture and the other is preserved in air. The condition of the pats is observed 7 da. and 28 da. from the date of making, and thereafter at such times as may be desired. The most characteristic forms of failure are illustrated in Figs. 1 and 2. Fig. 1 (a) shows a pat in good condition. Fig. 1 (d) illustrates shrinkage cracks that are due, not to inferior cement, but to the fact that the pat has been ailowed 212 TESTS ON CEMENT to dry out too quickly after being made. Pats must be kept in a moist atmosphere while hardening, or these cracks, indicative merely of careless manipulation will develop. Fig. 1 (c) shows cracks that are due to the expansion of the cement. This condition is common in the air pats, and is not indicative of injurious properties. Pats kept in water. however, should not show these cracks. (d) | (e) (f) IG Fig. 1 (d) shows cracking of the glass plate to which the pat is attached. This cracking is caused by expansion or con- traction of the cement, combined with strong adhesion to the glass. It rarely indicates injurious properties. Fig. 1 (e) illustrates blotching of the pats, the cause of which should always be investigated by chemical analysis or otherwise, which may or may not warrant the rejection of the material. Slag cements or cements adulterated with slag invariably show this blotching. —_— -_ Ye): TESTS ON CEMENT 213 Fig. 1 (f) shows the radial cracks that mark the first stages of disintegration. Such cracks should never occur with good material. They are signs of real failure, and cement showing them should never be used. Fig. 2 shows three pats that, for different reasons, have left the glass plate on which they were made. The disk shown in (a) left the plate because of J lack of adhesion; the one in (b), through contraction; and the one in (c), through expansion. The _ condition illustrated in (a) is “ never dangerous in either air or water; that in (c) is only danger- Fic. 2 ous when existing in a marked degree; and that in (b) hardly ever occurs in water, but in air it often indicates dangercus properties. Air pats that develop the curvature shown in (b) generally disintegrate later. A curvature of about % in. in a 3-in. pat can be considered to be about the limit of safety. The normal pat tests are the only absolutely fair and accurate methods of testing cements for soundness, but the serious objection to them lies in the fact that frequently several months or even years elapse before failure in the cement so tested becomes apparent. To overcome this difficulty the accelerated tests have been devised. These tests are intended to produce in a few hours results that require months in the normal tests. Many forms of accelerated tests have been devised. At present, however, the only tests employed commercially are the boiling test and the steam test. The boiling test is made by forming specimens of neat- cement paste into pats, such as are employed for the normal tests, or preferably into balls about 14 in. in diameter. The specimens are allowed to remain in moist air for 24 hr. and are then tested. The form of apparatus used for the boiling test is shown in Fig. 3. It consists of a copper tank that is heated by a 214 TESTS ON CEMENT Bunsen burner and is filled with water. The water in the tank is kept ata uniform height by means of a constant-level bottle. A wire screen placed an inch from the bottom of the tank prevents the specimens from coming into contact with the heated bottom. The test pieces, which are 24 hr. old, are placed in the apparatus, which is filled with water of a normal temperature, and heat is applied at a rate such that the water will come to boiling in about 4 hr. Quiet boiling is continued for 3 hr., after which the specimens are removed and examined, Care must be taken that the water employed Fic. 3 x is clean and fresh, because impure water may seriously affect the results.. The same water, also, should never be used for more than one test. A good cement will not be affected by this treatment, and the ball will remain firm and hard. Inferior cement will fail by checking, cracking, or entirely disintegrating. The steam test is made in the same way as the boiling test, except that instead of immersing the specimens in water, they are kept in the steam above the water. The apparatus employed is the same as that used for the boiling test. The ee a ea TESTS ON CEMENT 215 wire screen, however, is raised so that it is an inch above the surface of the water; also, there must be provided a cover that is close enough to retain the steam without creating pressure. The steam test is less severe than the boiling test and is somewhat less accurate. Results of Tests for Soundness.—The peeult of the normal tests, if properly made and interpreted, may be considered reliable guides to the soundness of the material, and cement failing in these tests should always berejected. The acceler- ated tests, on the other hand, furnish merely indications, and are by no means infallible. A cement passing the boiling test can generally be assumed sound and safe for use, but, if failure occurs, it simply means that other tests should be performed with greater care and watchfulness. It often is advisable to hold for a few weeks cement that fails in boiling, so that the expansive elements may have an opportunity to hydrate and become inert; but if the material fulfils all the conditions except the boiling test, and is sound in the normal tests up to 28 da., it is generally safe for use. All things being equal, however, a cement that will pass the boiling test is to be preferred. TESTS FOR TENSILE STRENGTH The tensile-strength test is for the purpose of ascertaining a measure of the ability cf the material to withstand the loads that the structure must carry. This test is made by form- ing specimens, called briquets, of cement and cement mortar, and determining the force necessary to rupture them in ten- sion at the expiration of fixed intervals of time. Cement constructions are rarely called on to withstand tensile stresses, but if the tensile strength is known, the resistance to other forms of stress may be computed with a fair degree of accur- acy. The tensile-strength test is the most convenient for laboratory determinations, on account of the small size of the specimens and the comparatively low stress required to cause rupture. Cement is tested both neat or pure and in a mortar com- monly composed of 1 part of cement and 3 parts of sand. The period at which the briquets are broken have been fixed 216 TESTS ON CEMENT by usage at 7 da. and 28 da. after making, although tests covering much longer periods of time are necessary in research or in investigative work. Normal Consistency.—The strength of cement and cement mortars varies considerably with the amount of water employed in making the briquets. Dry mixtures ordinarily give the higher results for short-time tests, and wet mixtures show stronger with a greater lapse of time. For testing purposes, therefore, it is essential that all cements be mixed, not with the same amount of water, but with the amount that will bring all the cements to the same physical condition, or to what is called normal consistency. Different cements require different percentages of water because of their vary- ing chemical composition, degree of burning, age, fineness, etc. The normal consistency of neat-cement pastes may be determined by the method that follows. This method is to form of the paste a ball about 2 in. in diameter and to drop this ball on a table from a height of about 2 ft. If the cement is of the correct consistency, the ball will not crack nor will it flatten to less than half its original thickness. The percentage of water required will vary from 16 to 25, depending on the characteristics of the material, the average cement taking about 20%. Consistency of Sand Mortars.—The consistency of sand mortars, however, cannot be obtained by the foregoing method, because the mixture is tooincoherent. For mortars, therefore, it is necessary to employ a formula by means of which the sand consistency can be computed when that of the neat paste is known. Several such formulas have been devised, of which the following is adaptable to the greatest variety of conditions. Let x be the per cent. of water required for the sand mix- ture; NV, the per cent. of water required to bring the neat cement to normal consistency; u, the parts of sand to one of cement; and S, a constant depending on the character of the sand. Then, _38N+Sn+1 4(n+1) For crushed-quartz sand, the constant S is 30, for Ottawa sand, it becomes 25; and for the bar and bank sands used in TESTS ON CEMENT 217 construction, it varies from 25 to 35, and must be determined for each particular sand. EXAMPLE.—How much water is required in a mixture of 1 part of cement and 3 parts of crushed-quartz sand? The neat cement requires 19% of water to give normal consis- tency. F SoLutTion.—Here, N=19, S=30, andu=3. Substituting these values in the formula, _3X19+30X3+41 4X (3+1) Sand for Mortar Tests.—The size, gradation, and shape of the particles of sand with which cement mortars are made have great influence on the resulting strength. There are two varieties of standard sand for cement testing, one an artificial sand of crushed quartz, the particles of which are angular in shape, and the other a natural sand from Ottawa, Illinois, the particles of which are almost spherical. Both sands are sifted to a size that will pass a sieve of 20 meshes to the inch and be retained on a sieve of 30 meshes, the dia- meters of the sieve wires be- ing .0112 and .0165 in., re- me is an ae spectively. The Ottawa sand will develop strengths in 1-3 mortars about 20 to 30% greater than those obtained with crushed quartz, and itis theoretically the better sand for testing, but, at present, crushed quartz is more exten- sively employed. On most Fic. 4 important works, tests for purposes of comparison are also made of the actual sand-entering the construction. Form of Briquet.—The form of tensile briquet, adopted as standard in the United States, is shown in Fig. 4. Its cross-section is exactly 1 sq. in. =9.3% wy — wt fpr Lit } St 218 TESTS ON CEMENT Molds.—_Cement briquets are made in molds that come either single or in gangs of three, four, or five. The gang molds are preferable, as they tend to produce greater uni- formity in the results. Molds should be made of brass or of some other non-corrodible material; those made of cast iron soon rust and become unfit for use. Method of Making Briquets.—First, 1,000 g. of cement is carefully weighed and placed on the mixing table in the form of a crater, and into the center of this is poured the amount of water that has previously been determined to give the correct normal consistency. Cement from the sides of the crater is then turned into the center, by means of a trowel, until all the water is absorbed, after which the mass is vigorously worked with the hands, as dough is kneaded, for 14 min. When sand mixtures are being tested, 250 g. of cement and 750 g. of sand are first weighed and thor- oughly mixed dry until the color of the pile is uniform; then the water is added and the operation is completed by vigor- ous kneading. After kneading, the material is immediately placed into the molds, which should first have been wiped with oil to pre- vent the cement from sticking to them. The entire mold is filled with material at once—not compacted in layers—and pressed in firmly with the fingers without any ramming or pounding. An excess of material is then placed on the mold and a trowel drawn over it under moderate pressure, at each stroke cutting off more and more of the excess material, until the surface of the briquets is smooth and even. The mold is then turned over, and more material placed in it and smoothed, as before. The mixing and molding should be performed on a surface of slate, glass, or some other smooth, non-absorbent material. During the mixing the operator should wear rubber gloves, so as to protect his hands from the action of the lime in the cement. - Storage of Briquets.—For 24 hr. after making, the briquets are stored in a damp closet so that the cement can harden in a moist atmosphere. The damp closet is simply a tight box of soapstone with doors of wood lined with zinc, or some similar arrangement, with a receptacle for water at the TESTS ON CEMENT 219 bottom and racks for holding the briquets. The briquets remain in the molds while in the damp closet, but at the expiration of 24 hr. they are removed, marked, and placed in clean water near 70° F. until broken. Testing Machines.—There are many styles of testing machines on the market. In Fig. 5 is shown what is called a shot machine, made by the Fairbanks Company. It is HIG oO constructed on the cast-iron frame a, and is operated as fol- lows: The cup/ is hung on the end of the beam d, the poise r placed at the zero mark, and the beam balanced by turning the weight 7. The hopper 0 is then filled with fine shot, and the briquet to be tested is placed in the clips kh. The hand- wheel p is now tightened sufficiently to cause the graduated beam d to rise to the stop k, and the automatic valve 7 220 TESTS ON CEMENT opened so as to allow the shot to run into the cup f. The flow of the shot can be regulated by means of a small valve located where the spout joins the reservoir. When the briquet breaks, the beam d drops and by means of the lever ¢ automatically closes the valve 7. After the specimen has broken, the cup with its contents is removed, and the counter- poise g is hung in its place. The cup f is then hung on the hook under the large ball ¢, and the shot weighed. The weighing is done by using the poise 7 on the graduated beam d and the weights on the counterpoise g. The result will show the number of pounds required to break the specimen. A mold for a single briquet is shown at c. Rate of Loading Testing Machine.—The load should be applied in all tests at the uniform rate of 600 lb. per min. The briquets should be broken as soon as they are removed from the storage tanks and while they are still wet, because drying out tends to lower their strength. The average of from three to five briquets should be taken as the result of a test. Results of Tensile-Strength Tests.—The tensile strength of cement tested in the preceding manner should increase with age up to about 3 mo, and should then remain practically stationary for longer periods. The average results of tests of Portland cement made in the Philadelphia laboratories, covering a period of several years and based on over 200,000 briquets, are given in the accompanying table. Specifications for strength commonly stipulate minimum values for the 7- and 28-da. tests, the customary require- ments for Portland cement being 500 lb. at 7 da. and 600 lb. at 28 da., when tested neat, and 170 lb. at 7 da. and 240 lb. at 28 da., when tested in a mortar consisting of 1 part of cement and 3 parts of crushed-quartz sand. When Ottawa sand is used, the requirements for mortar should be raised to 200 and 280 lb., respectively. Retrogression in strength of the neat briquets between 7 and 28 da. is not necessarily indicative of undesirable properties, but if the mortar briquets show retrogression, the cement should be condemned. Abnormally high strength in the 7-da. test of neat cement, say over 900 lb., may generally be taken as an indication of TESTS ON CEMENT 221 TENSILE STRENGTH OF CEMENT BRIQUETS (Pounds per Square Inch) — 3) a & ee He | ud | we | ae “B / eo fel rea 75 Slate. 60 SARA Girls, a elas Brean sore ONG DiS TA Ne IBS. Gm a be 55 Cased oe PE pede wee Nickels Oe eink See ee 50 PROPORTIONING OF INGREDIENTS Effect on Strength and Imperviousness.—The strength of concrete depends on the strength of the cement and the thoroughness with which the cement binds togethe. the various pieces of aggregate. The more completely the voids are filled, the more completely will the aggregate be held together. Therefore, the more solid and condensed the con- crete is, the less voids it will have, and the stronger it will be. The same is true with regard to making concrete water- proof: the more dense the concrete is, the more nearly water- proof it is. A mixture of 1 part of cement, 14 parts of sand, and 3 parts of stone, which would be considered extravagantly rich for ve —~ PLAIN CONCRETE 235 a dry place, is probably as dense a concrete, and as good for waterproofing qualities, as can be made. When a concrete is made of cement, sand, and stone, and the stone is of such a size that it will pass through a 3-in. ring, but will not pass through a 24-in. ring, the concrete is weaker and requires more cement than one made with graded stone from 3-in. down. When the stone is graded in size, the stones of smaller size fill the voids between the larger stones and thus reduce the quantity of cement and sand required. Proportioning by Weight.—A method of proportioning the materials, that is simple and fairly accurate, is as fol- lows: A batch of concrete is mixed in known proportions. The same quantity of water is used that it is proposed to use on the work, and the mixture is rammed and tamped in the receptacle in a uniform manner. The receptacle should pre- ferably be of metal; a tin washtub, or a short section of 12-in. pipe, capped at one end, will answer. When the receptacle is full, it is weighed, and if the weight of the recep- tacle itself has previously been found, the weight of the con- crete may be obtained. Various other mixtures of concrete are tried in the same manner, and since the denser the mixture the stronger it will be, the heaviest concrete is the strongest for the particular work. Each batch of concrete must be weighed and taken out of the receptacle before it has time to set; otherwise, some difficulty might be experienced in getting.it loose. ; Usual Proportions of Materials.—The strongest concrete does not always have to be used, as it may be required to withstand only slight stresses and be simply used for its weight. The strongest concrete would then be unnecessarily expensive. Therefore, the foregoing method for proportion- ing concrete is seldom employed. The engineer usually specifies a mixture from his own experience without testing the aggregates in any way, except to see that the stone is under the specified maximum size and that the sand is in large grains and free from dirt and loam. A common pro- portion for unimportant work is 1-3-6. This proportion may be used for foundations below ground, in engine bases, 236 PLAIN CONCRETE in the foundations for asphalt pavements, and for similar purposes. A richer mixture, 1-2-4 is used in piers, in dams, in important reinforced-concrete work, and in other places where great strength is desired. _ Water for Concrete.—The wetter the concrete is, the easier it will be put in place, but mixtures that are too wet are not so strong as medium mixtures. The amount of water that will make the best mixture is such that after the con- crete has been put in place and rammed it will quake like jelly when struck with a spade, and water will come to the surface. If the concrete is wetter than this, the water will have a slight chemical effect on the cement, and, moreover, the sand and cement will tend to separate from the broken stone. In cinder concrete, owing to the porosity of the cinders, it is necessary to use a little more water, so that the cement will be liquid enough to fill the little cavities in each cinder. This precaution is indispensable when the concrete is to be used with steel, as otherwise the steel will be rapidly corroded by the action of air reaching it through the pores in the cinder. Dry Concrete.—With the advent of the concrete block, a great deal is heard about dry concrete. This name is given to concrete in which as little water as possible is mixed. In the concrete-block manufacturing business, the mold in which each block is made is required as soon as possible, so that it can be used over again and thus increase the capacity of the machine to which it belongs. For this reason, the concrete-block manufacturers use, often, dry concrete, and attempt to supply the remainder of the water required for the complete crystallization, or setting, of the cement by curing the blocks; that is, by sprinkling them with water for a week or so. The results of recent tests seem to indicate that dry concrete will show higher com- pression values for a limited time after it is made, but that the rate of increase of strength is not so great as with wet concrete. After 1 yr. or 6 mo., the strength of the wet con- | crete will be found to have attained, and perhaps surpassed, that of the dry mixture. PLAIN CONCRETE 237 A serious objection to dry concrete is that it cannot be rammed to so dense a mass as wet concrete. Therefore, if a waterproof concrete is desired, it should be mixed wet. PROPERTIES OF CONCRETE GENERAL CHARACTERISTICS Corrosion of Steel in Concrete.—It has been conclusively proved by experience and test that steel or iron completely embedded in the usual mixture of concrete will not corrode seriously. Portland cement contains free alkali, and steel or iron will not rust in the presence of an alkali. Corrosion will occur only where the concrete has been carelessly placed and where voids in the concrete have exposed the metal. Wet concrete offers more protection to iron or steel than a dry mixture, because the metal is better coated with the cement mixture. Cinder concrete, when of a rich mixture— at least one sufficiently rich in cement to coat every particle of the cinder—will protect ironwork or steelwork as well as stone concrete; but, if it is not properly mixed and particles of the uncoated coal or cinder come in contact with the steel, rapid corrosion is likely to take place. Effect of Fire on Concrete.—Concrete is essentially a fire- proof material. All the ingredients of which it is composed are of a highly refractdry nature, the aggregates being the elements of the mixture that are most quickly affected by intense heat. This is especially true of granite and lime- stone aggregates, the former being likely to crack or burst when heated, and the latter liable to calcine. After cement has set, the chemical union of its particles is liable to destruc- tion by fire, because intense heat robs the cement of the water of crystallization, or dehydrates the cement, thus softening the material and making it crumbly. If concrete in a mass is subjected to intense heat, this action of dehydra- tion extends into the concrete for a depth of only } to 4 1ncu, and is not likely to penetrate farther. Considére, a French concrete expert, has found by experi- ment that a 1-3 mortar will shrink from about .05 to .15% 238 PLAIN CONCRETE in setting in air, and that the shrinkage will be two to three times as great with neat cement. The shrinkage in concrete will be much less than with neat cement or cement mortar. The shrinkage of concrete is lessened by embedding in it steel rods or bars, as these, by their tensile resistance, prevent the shrinkage of the material in setting. By the experi- ments of Considére, it is found that with 1-3 mortar rein- forced with steel the shrinkage in setting is about one-fifth _ that of the same mortar without the steel reinforcement. Effect of Thermal ‘Changes in Concrete.—Nearly ail materials expand slightly as they become heated. Con- crete and steel also follow this law. The contraction or the expansion of concrete due to changes in temperature is about the same as that of steel. The average coefficient of expan- sion of a 1-2-4 concrete for each Fahrenheit degree in change of temperature is .0000055. Experiments made on 1-3-6 concrete give a coefficient of expansion of 0000065, which is practically the same as the coefficient of steel. Effect of Vibration on Concrete.—The effect of constant vibration on concrete structures has not been definitely determined. Many buildings and bridges constructed of concrete reinforced with steel rods and bars have withstood heavy and constant vibration, either continuous or inter- mittent, for an extended period of years with no apparent deterioration in strength. Fresh concrete is always, how- ever, subject to deterioration by vibration, and the strength of concrete subjected to jar or shock when setting is materially reduced, because the process of crystallization between the particles, and the consequent cohesion of the mass, seems to be partly destroyed. WORKING STRESSES AND STRENGTH VALUES OF CONCRETE The ultimate strength of concrete varies so with the pro- portion of the mixture, manner of working, character of ingredients, and age of material, that it is necessary to assume low unit working stresses for it. The usual working stress for plain concrete under com- pression is from 250 to 300 lb. per sq. in., although, in-masses, eo PLAIN CONCRETE 239 as in footings, a 1-24—5 concrete would safely sustain as much as 500 lb. per sq. in. When reinforced concrete is subjected to compression from loads causing bending, it is customary to figure the safe allowable unit compressive stress in the compression portion of a reinforced-concrete beam. at from 500 to 600 or even 750 lb. per sq. in. In tension, concrete has little value; in fact, it cannot be relied on to resist this stress. Generally, the tensile strength of plain concrete is about one-tenth of its compressive strength. The modulus of rupture, or the unit value for figuring the transverse strength of plain concrete, is much lower than the modulus of rupture of any of the good building stones. The safe unit bending stress for plain concrete, based on a factor of safety of 4, from values of the modulus of rupture obtained from recent tests made on concrete 30 da. old, is about 110 lb. This value is for concrete composed of 1 part of cement, 2 parts of sand, and 4 parts of broken stone. With a poorer mixture, as a 1—2—5 concrete, a safe bending stress of about 95 lb. should be used, while with a 1-3-5 mixture, the safe bending stress is barely 70 lb., and this value shows a corresponding decrease as the mixture becomes leaner. The safe unit shearing stress of plain concrete is, in practice, taken at a very low figure when compared with recent tests giving the ultimate shearing resistance of this material. This low figure is probably due to the fact that few tests have been made to determine the value of plain concrete in shear; or perhaps it is due to the unreliability of concrete, as found in practice, to resist this stress. The conservative safe unit shearing stress of plain concrete is taken at 50 Ib., although the value may be increased for rich mixtures and careful workmanship to 75 lb. The safe grip, or bond, as it is called, of concrete on steel rods or bars with plain surfaces embedded in it, is taken, for purposes of calculation, at 50 lb. per sq. in. of the surface of the metal in contact with the concrete. All the values just mentioned are based on concrete at least 1 mo. old. There is great diversity of opinion regard- 240 PLAIN CONCRETE ing the safe unit values of plain concrete, and there is no uniformity in the building laws of the several cities regard- ing the strength of this material. This is shown by the following table, which gives the working values of concrete allowed by the building laws of several cities: UNIT WORKING VALUES OF CONCRETE ALLOWED BY VARIOUS CITIES Direct - Compres- | Shear | Unit Cotapress- sion Pounds i Name of City Pounds Se Unde wes ding rT uare Pounds per ae Inch Square Inch New York....... ; 350 50 500 Philadelphia...... 250 50 600 Cleveland. . \ 400 50 500 San Francisco . 450 75 500 PAUSED «a: 35- 040.030 350 50 500 TOPOUtO\. cxcee acess 340 50 500 An average ultimate unit compressive strength of 2,000 Ib. . would be conservative for a 1-2-4 concrete, from 1 to 3 mo, old, and 1,600 lb. for a 1-3-6 concrete of the same age. Mixtures varying in richness between these limits would have proportional values. The tensile strength of concrete is more affected by the quality of the mixture than is its compressive stress. There- fore, a conservative ultimate-tensile-strength value of a 1-2-4 mixture would be about 200 lb., while for a 1-3-6 mixture, it would be about 125 Ib. The shearing strength of concrete is usually much less than the compressive strength. For a 1—2—4 mixture an average ultimate shearing strength of 1,480 lb. per sq. in. has been determined by tests, while a 1-3-5 mixture has given 1,180 lb., and a 1-3-6 mixture has given a value in shear of 1,150 Ib. per sq. in. The average modulus of rupture for plain concrete that was from 33 to 35 da. old has been found to be 439 lb. per sq. in. 241 PLAIN CONCRETE S8T | S9T | SZT | G24 |00S‘T |00E‘T |000'T |009 OST | O&T | OOT | 09 ot | O'9 I 00Z | SLT | OFT | T8 |009'T |OZF‘T |OZT'T |OS9 OO9T | GFT | SIT | G9 ir | 99g I GTZ | P6T | 8ST | ¥6 OZL'T oge'T 092'T O¢Z CLT | GOT | 9ZT | SZ ot | o's T O&@ | II | SLT | 9OT |OFP8 T 069'T OOF T }O¢s v8SI | GOT | OFT | $8 6 oy I PPS | 8ZG | OGT | EST |OS6 1 |OZ8 T OSE T |086 | G6T | S8T | SST | 86 8 OF I 09Z | GFZ | 80Z | SET |080'Z |096'T 099 TOOT T} 806 | 961 | 99T | OTT | 2 ae I GLZ | €9% | GZS | 9ST |00Z'Z |OOT‘Z 008 1 |0GZ T} OGG | OIG | O8T | Sat | 9 0'€ I ¥6Z | I8Z | HHS | GLT |OSE'S |0SZ'S |0S6'T |OEF'T | GES | GZS | GBI | SFI | ¢ G°s I €1é | OOF | 69Z | 00Z |00S'Z |O0F'S |OST'S |009'T | OSZ | OFZ | OIZ | OMT | F 0% I ‘Ou g/ ‘Our eon T| ‘ep Zz |ow gow g}'ow | ‘ep 2 |‘our g/‘ow ¢g)‘ou [| ‘ep 2 |jeu04Gg} pueg) yUsUIED | you] slenbg sod spunog | youy orenbg Jed spunog | youy elenbg Jed spunog s]UsIpelsuy reayg uorsseidur07 uolsuay, jo uoljsodolg ANOLS GHHSNUD AGNV ‘ANVS ‘INANGO GNVILYOd WOUd ACVW ALAAMONOD AO HLONAULS ALVWILTN ANVAAAV 242 PLAIN CONCRETE for a 1-2—4 mixture, 380 lb. per sq. in. for a 1-2-5 mixture, and 285 lb. per sq. in. for a 1-3-5 mixture, while a 1-3-6 mixture gave a result of 226 lb. per sq. in. The values given in the accompanying table are recom- mended as ultimate values by W. Purves Taylor, engineer in charge of the municipal testing laboratory of Philadelphia. The figures represent values obtained from six hundred experiments made on concrete properly mixed with good Portland cement. It will be noticed that the values given for shear are considerably lower than those just given. The results obtained depend to a large extent on the method of testing. Some engineers prefer the lower values. MIXING AND WORKING OF CONCRETE CONCRETE MIXTURES Methods of Measuring Ingredients.—After deciding what proportions of ingredients will be used for the concrete, the engineer must be able to calculate the exact quantity of each material that he must order. An ordinary box car holds from 400 to 600 bags of cement. The purchaser is charged for the bags by the manufacturer, unless they are of paper, but he gets a rebate for those which are returned. Cement is usually measured by the barrel just as it comes from the manufacturer, or as 4 bags to the barrel, while broken stone and sand are measured loose ina barrel. Port- land cement, after it is taken out of its original package and stirred up, fills a larger volume than when packed. It is therefore necessary to state just how the cement is to be measured; and, as said before, the custom is to measure it by the barrel, compact. A cement barrel contains about 3.8 cu. ft. Fuller’s Rule for Quantities——A practical rule has been devised by W. B. Fuller whereby, after the proportions of ingredients have been fixed, the quantity of material for a certain work may be obtained. It is called Fuller’s rule for quantities, and may be expressed in mathematical symbols as follows: PLAIN CONCRETE 243 Let c be the number of parts of cement; s, the number of parts of sand; g, the number of parts of gravel or broken stone; C, the number of barrels of Portland cement required — for 1 cu. yd. of concrete; S, the number of cubic yards of sand required for 1 cu. yd. of concrete; and G, the number of cubic yards of stone or gravel’required for 1 cu. yd. of concrete. Then If the broken stone is of uniformly large size, with no smaller stone in it, the voids will be greater than if the stone were graded. Therefore, 5% must be added to each value found by the preceding formulas. ExAmMPLe.—lIf a 1-2-4 mixture is considered, what will be: (a) the number of barrels of cement, (b) the number of cubic yards of sand, and (c) the number of cubic yards of stone required for 1 cu. yd. of concrete. So_tuTion.—(a) Here c=1, s=2, and g=4. Substituting these values in the first formula, a ee. 1+2+4 (b) Substituting the values of C and s in the second formula, 3.8 S=— X1.57X2=.44 27 (c) Substituting the values of C and g in the third formula, 3.8 G=—X 1.57 X4=.88 27 Table of Quantities.—The table on pages 244 and 245, giving the quantities of ingredients for concrete of various pro- portions, was prepared by Edwin Thacher. It will be noted in this table that the difference in the character and size of the stone or gravel used has been taken into account. These values will be found to agree fairly well with values found by Fuller’s rule. PLAIN CONCRETE 244 OL | OG’ | ZE°T| 18° | 8G° | TS'T| 62 99° | 8h] 22° | $G° | SP T/G'S | G'S T 68° | 98° | ZT‘T}| €O'T| 6E* | €8'T| 86° 6€° | 62°T| 46° | 6€° | Za°T!O0'S | O07 T 98° | 88° | 92°T| 86° er" | SFT! 96° cb’ | 8°T| £6" | Ch | 9E'T1 SF | 07% ui 18° | Ih’ | PET] &6° Lv’ | €o°T| 06 cy’ | 8b'L| 68 tr | OF TOF | OG I LL’ | bh | Hh T| 88° og’ | 99°T| $8 6h" | 19'T| €8° | 8h | 24G°T/ S's | O@ I eZ’ | 2b’ | 9° T| 18" bo" | 82°T| 62 eg¢° | 82°T} 242° | ao” | OLT/O'S | 0% I 16° | T8° | P81] 9O'T| SS | TS°T| OO'T| Ee" | 9F'T| 86 Se" |r tS h | St I 88° | €8° | 9F'T| OO'T] 8E° | POT) 86° Le° | 19°T] 96 98° |} ZO°T|O'F | Git T €8° | 98° | 249°T| 96 Tr’ | 62°1T| £6 OF’ | FLT] 16 6€° | o2° T/S°S | Git T 82° | 68° | IZ°T} 68° cy’ | 96'°T| 28 &b° | 06°T| 8 oh’ 1S8'T/0°E | ST T el or | 8° T} 28" 6h" | 91°S| 08 8b° |60°S| 8LZ° | Zh’ |} 90'S1S°t | GT T 16 9%° | IZ°1I| SO'L| 66° | 88°T| OO'T| 62° | 88°T| 86 86° | F8 T/o's | OT T 98° | 66° | 68°T| 86 €€° | 91°S| 96 os | O1'S| ¥6 Tg" |90°3|O0'€ | OT i 08 oe" | OL S| 26 1° | Ih Z| 68 9¢° | E'S} OL ce" |62°S|S°% | O'T T pL’ | GE" | OF'S| £8" Ir | o2°S| O08" Ob" | €9°S| 82 6€° | 46°72; 086 | OT + 22/2 w|.. 8128/8 SPlanle@ nl _ Sle ale@nl_#! eo | » i eee Elec ele klEelebleeleeiaelacize/2)2| 3 asi|ae|Fsiaelee| Blas i[ee| Biss [sei' Bl) & | & | B qnQ peuser9g nO nO Japuy pue auoyg [[eug poueelog isnq pouseslog sng youl F ‘parry | ysow yM— | —sepuy pue | —sepuy pue syuarporBu] soyouy $Z ‘eu0Zg | SeyoUT FZ ‘“oUoIg | YoU] T “98U0}S jo uorjsodoig eyoINUOD pewuUeYy JO PleX IQnD | 10} postnboy sjustpoisuy SNOILYOdOUd SNOTAVA dO ALAUONOD AOA SINAIGAAONI AO SALLIINVNO 245 PLAIN CONCRETE BUIISSSRLTG Sse ane be oe oe Oh oe oe oe oe ee Be oe | reir be ee ee oe ee | rt be oe oe ee ee oe oe | PAPO WOP AOD OOHRINMOORRDOOKRHRDDARDO re CANAAN 69 019 CF CFD 01D 01D CVD CVD EXD OD YD CVD 01D OVD SH SH SH SH eH eH eH 11D ce ee Be ee Be oe Boe Re he ho he] 246 PLAIN CONCRETE _ WORKING OF CONCRETE Mixing of Concrete-——Concrete may be mixed either by hand or by machine. For small work, the concrete is mixed by hand in small batches, such as would be made up from 1 of 2 bags of cement. In mixing, hand work should be performed on a flat, water-tight platform. The sand, after it has been measured, is spread over the platform in an even layer. Upon the sand is placed the cement, and these two materials are turned over with shovels at least three times, or until the uniform color of the mixture indicates that they are thoroughly incorporated. The stones, or aggregates, having previously been well wetted, are then placed on the top of the mixture of sand and cement and these materials are also turned at least three times, water being added after the first turning. The water should always be added in small quantities. Ifa hose is used for this purpose, it should be fitted with a sprinkling nozzle, as otherwise much of the cement is liable to be washed out of the mixture. The concrete, when ready for placing, should be of uniform con- sistency, either mealy for a dry mix or mushy for a wet mix. In large work, the mixing should be done by machine. Retempering of Concrete.—If the cement of the concrete has attained its initial set before being placed—that is, if the concrete has commenced to harden—remixing with water, or retempering of concrete, as it is called, should not be allowed; and if concrete treated in this manner has been deposited in the forms, it should be taken out and removed from the site of the operation, because concrete cannot be retempered properly, except in small quantities for labor- atory tests. Concreting at High Temperatures.—If the weather is extremely warm, the stone and sand are liable to become heated toa high temperature. Then, in mixing the materials, the water necessary for the crystallization of the cement is rapidly absorbed by the stone and the sand, or else rapidly evaporated by contact with them. Again, the extreme heat will hasten the setting of the cement, and this tends to cause the concrete to cake in the mixing machine, pro- ducing lumpy and inferior concrete. In order to overcome Ey eo iy ee rege © PLAIN CONCRETE 247 such difficulties, the stone should be thoroughly wetted with a hose, and the sand and stone should be kept under cover, away from the direct rays of the sun. Likewise, the mixing platform or machine should be roofed over. It is well, also, to wet down the finished concrete work with a hose several times a day in extremely hot weather, and less frequently in moderate temperatures. . Concreting in Freezing Weather.—Although it is practi- cable to mix and place concrete at a temperature as low as 27° F., it is not advisable to lay concrete work when the temperature is below 32°; neither should it be mixed and placed even at this temperature, if there is a possibility that the temperature will fall. If concrete is frozen, its setting is retarded and it is liable to become worthless, never properly setting and obtaining the requisite hardness and strength. There is, however, no certainty of the action of frost on concrete, as frozen concrete will frequently thaw out and set, with apparently little loss of strength. To prevent the freezing of concrete when the temperature has fallen below 32° F., salt is sometimes used in the mixture. The addition of 1} lb. of salt to the water used with 1 bag of cement will not decrease the strength of the concrete; or, a 10% solution of salt can be used in the water employed in mixing the concrete. The addition of salt, however, is never advisable if a surface finish is required, as it is liable to cause efflorescence, or a white deposit, on the surface causing the work to become very unsightly. Aggregates that are coated with ice or that have been exposed to severe weather for a long time should be heated or thawed out before being used. Concrete that is exposed to freezing after it was set should always be protected by placing over it a layer of boards and straw, or salt hay, or cement bags; or, where the work is in the nature of a rein- forced-concrete floor system, by heating the interior of the structure by means of salamanders or fires. Joining of Old Concrete With New.— New and old concrete can be joined only with difficulty, and the strength of such a connection is always uncertain. The joining of old and new concrete work is best done by thoroughly chipping, or 248 STEEL REINFORCEMENT cutting away, the old surface, saturating it with water, and working into it thin coats of a 1-1 Portland-cement mortar, and, then, while the coating is still fresh, placing egataat it the new concrete. There are some high-grade, imported cements that, in the form of cement mortar, more readily adhere to old concrete work than the usual Portland cements. These cements are frequently used for patching and piecing out work already in place. ELEMENTS OF STEEL REINFORCEMENT THEORY OF STEEL REINFORCEMENT Principles of Construction.—When a beam is subjected to transverse stress, the portion of the beam section above the neutral axis is in compression, while in that portion below the neutral axis, tensile stresses are created. Ordi- narily, concrete is about ten times as strong in compression as itisin tension. Thus, it can readily be seen that a beam of plain concrete without steel reinforcement would fail primarily from lack of tensile resistance, without realizing its full compressive strength. In order, therefore, to make concrete an eco- nomical material to use in construction, its deficiency in Fic. 1 tensile resistance must be made up by embedding steel rods, bars, or some other form of metallic reinforcement in that portion of the beam section subjected to tensile stress. In order to explain more fully this primary principle of reinforced concrete, reference is made to the reinforced, rectangular concrete beam shown in Fig.1. The neutral line of the section is shown at 4 7; in the side view (a), while the neutral axis is represented by y y in the end view (b). When the concrete beam is under transverse stress, there is neither STEEL REINFORCEMENT 249 tensile nor compressive stress at the neutral axis. Therefore. the point in the beam marked a, which is on the neutral axis, is subjected to zero stress. Imagine that the concrete is cut away below the neutral plane, leaving the steel reinforcing rods, or bars, exposed as atb. Itis evident that the strength of the beam is not much affected by the cutting away of the concrete in this manner, as the necessary tension below the neutral axis is supplied by the reinforcing rods of steel, while the necessary compression Fic. 2 above it is furnished by the concrete, asatc,c. The amount of compression in each square inch of concrete above the neutral axis varies from zero at the axis to maximum at the extreme upper surface of the beam. The concrete below the neutral axis yy is usually so filled with very fine cracks that all the tension must be carried by the steel alone. In ordinary reinforced-concrete column _ construction, merely vertical rods are employed. They are tied, however, at intervals with wire or other ties. 250 STEEL REINFORCEMENT The principle of hooped columns is best explained as follows: It is well known that a column of sand will not resist com- pression, because it will spread, and it is likewise certain that a cylinder of; say, very thin metal will sustain only a small load. However, if the cylinder is filled with sand, the combination, in which the tensile strength of the cylinder is realized with the compressive resistance of the sand, will result in a strong column, or post, capable of resisting con- siderable compression. This principle is applied to the rein- forcement of concrete columns by binding, or tying, together the concrete with cylindrical hoops, or helical, or spiral, windings of steel. Parts of Steel Reinforcement Defined. —In Fig. 2 (a) is shown a perspective view of a complete bay of a reinforced- concrete floor system, and in (b), a diagrammatic representa- tion of a typical system of reinforcement for a concrete girder and column. In (a), the heavy members A running between columns are commonly known as girders, and the lighter members B running between girders, as beams. In both (a) and (bd), the rods, or bars, a are the main reinforcing bars, or rods, of the girders. The beams, of course, have similar main reinforcing bars. Of these main reinforcing bars, several are bent up, as at b, to form trussed bars. The web reinforcement of the girders is shown at c, and consists of U-shaped pieces of iron or steel, called stirrups. The rods that reinforce the slab of the reinforced-concrete floor system, called slab rods, are shown at d, This slab reinforcement may consist of straight rods, expanded metal, woven-wire lath, or any other metallic reinforcement. The rods of the columns, shown at e, are called longitudinal column rods, and the hooped separators, or ties, shown at f, column ties. Any rod, or bar, used to resist shearing stresses is desig- nated asa shear bar. A rod, or bar, used to resist the shrink- age of the concrete in setting, or to provide against cracks due to thermal changes, is called a shrinkage rod. Shrinkage rods are shown at g in view (a). long as the steel holds, the beam will not fail. If the main reinforcing rods do not extend to the bearings, failure by vertical shear may occur near the abutments, along the line x x. Ordinarily, however, failures of this kind sel- dom happen, because the main rods usually extend across all _— | alte x —— Fic. 3 such lines of vertical shear, and add greatly to the shearing resistance of the beam. If the slab concrete is not placed at the same time that. the concrete of the beam section is poured, failure by shearing usually occurs at the junction of the beam with the slab, as shown atcc. The shearing resistance at this junction may be increased, however, by extending stirrups d into the slab. If the crack cc opens, it usually joins with a crack like ee at each end of the beam, as suggested in the preceding paragraph. The lines of failure indicated at e e are those which usually occur from diagonal tension stresses that cross these lines of failure at right angles. A beam is held against failure in this manner by placing stirrups in the concrete either vertically or obliquely. The bending up of the main reinforcing rods. 252 STEEL REINFORCEMENT to form the trussed bar, as shown at ff, will also assist in resisting such stresses, and, besides, will provide against negative bending moment where tension instead of compres- sion is created at gg. The line of fracture shown at ee is typical of nearly all reinforced-concrete failures. METALLIC REINFORCEMENT CHARACTERISTICS OF METALS USED FOR REINFORCEMENT Mild, or Soft, Steel——The commercial mild, or soft, steel, which is an excellent material for reinforcing rods, especially in concrete structures subjected to sudden strain or shock, should have a unit ultimate tensile strength of from 52,000 to 62,000 Ib. and an elastic limit of not less than one-half this amount. It should have an elongation of at least 25% in 8 in., and should be capable of being bent cold through 180° and hammered flat on itself without evidence of fracture on the outside circumference of the bend. Medium Steel.—The grade of steel known as medium more fully meets all the requirements of reinforced-concrete con- struction than any other grade. Commercial medium steel should have an ultimate unit tensile stress of 60,000 to 70,000 lb., and an elastic limit of not less than one-half this amount. Upon testing, the elongation should be found to be at least 22% in a length of 8 in., and it should withstand bending through 180° around a diameter equal to the diameter or the thickness of the pieces tested. Such a test piece should not show fracture on the outside circum- ference of the bent portion. High-Carbon Steel.—The name high-carbon steel is applied to steels rolled particularly for the reinforcement of concrete. Such steels contain a higher percentage of carbon than either medium or soft steel. The product as a rule is brittle, and possesses a unit ultimate tensile strength of from 80,000 to 100,000 lb., with an elastic limit of about one-half of its ultimate strength. The amount of elongation in 8 in. is sometimes as low as 5%, and seldom exceeds 15 to 18%. Ordinarily, it will not bend much beyond a right angle with- STEEL REINFORCEMENT 253 out showing fracture. On account of the brittleness and general unreliability of high-carbon steel, the material should be carefully tested and’/inspected before being used in rein- forced-concrete construction. AREAS AND WEIGHTS OF SQUARE AND ROUND BARS Square Round ‘1 e Size Inches Weight Weight Area per Foot Area per Foot Inches Poswax Inches Puasa ts 39 .013 0031 010 4 0156 053 0123 042 0352 120 0276 094 0625 E213 0491 167 0977 S532 0767 261 6 .478 1104 .376 1914 .651 503 511 a 2500 .850 1963 . 668 .3164 1.076 2485 .845 .3906 1.328 . 3068 1.043 4727 1.607 nous 1.262 5625 1.913 .4418 1.502 6602 2.245 -5185 1.763 .7656 2.603 .6013 2.044 .8789 2.989 . 6903 2.347 1 tA 3.400 . 7854 2.670 14 1.1289 3.838 .88 3.014 1g 1.2656 4.303 .9940 3.379 1 1.4102 4.795 1.1075 3.766 1 1.5625 5.312 1.2272 4.173 Bt ey 7 5.857 1.3530 4.600 1 1.8906 6.428 1.4849 5.049 1l& 2.0664 |~> 7.026 1.6230 5.518 14 2.2500 7.650 1.7671 6.008 175 2.4414 8.301 1.9175 6.520 it 2.6406 8.978 2.0739 T2051 1 2.8477 9.682 2.2365 7.604 it 3.0625 10.413 2.4053 8.178 1 3.2852 11.170 2.5802 8.773 it, 3.5156 11.953 2.7612 9.388 y 3.7539 12.763 2.9483 10.024 2 4.0000 13 3.1416 10.681 254 STEEL REINFORCEMENT There are to be had on the market twisted bars of square and hexagonal section. Such bars are from 8 to 25% stronger than the bars in their original form. The per- centage of increase of strength is greatest with the bars of small section and least with those of large section. Rerolled Bars.—Bars made from old steel rails can be obtained for reinforcing concrete. In making such bars, the flange, web, and bulb of the rails are cut apart, and rerolled into square and round sections. The square sections may be had twisted, the twisting being performed while the material is hot. , Much of this material has a high elastic limit and tensile strength, but it is inclined to be brittle and variable in strength and ductility. Besides, any lapping or folding of the original material when passed through the rolls is liable to develop laminations throughout the bar, tending to diminish its strength. TYPES OF STEEL REINFORCEMENT Plain Bar Iron.—The cheapest form of metallic reinforce- ment for concrete is the plain, round, rolled bar. Bars of this kind can be obtained in any part of the United States. The pound price of round, rolled bars is lower than that of any other form of rolled steel, so they offer the cheapest and most available material. For slabs, 3- to 4-in. round bars are used, while for beam, ({ girder, and column reinforce- ment, from §- to 1}-in. bars are ordinarily employed. (e) @ The principal objection to Fic. 1 the use of plain, round bars in reinforced-concrete work is that they are not gripped, or held, well by the concrete. Plain square and flat bars are sometimes used for the reinforcement of concrete, though, generally, both of these sections, when so used, are deformed by twisting. STEEL REINFORCEMENT 255 EN ENEN NEN a (é) Fic. 2 In the nomenclature of reinforced concrete, round, rolled sections are designated as rods; square sections as bars; and rectangular sec- tions, as flats, or flat bars. In the table on page 253 are given the areas and weights of square and round bars from ys- to 2-in. sizes. Bars of Special Con- struction.—Some early forms of bars used in reinforcement of con- crete are shown in Fig. 1. That shown in (a) is known as the Hyatt bar. An early form of the Thacher bar is shown in (b). In (c) is shown the Staff bar. It consists of a flat bar, through which a coun- tersunk punch has been partly driven, thus forcing the metal out on the opposite side so as to form projections. The De Mann bar is shown in (d). Two forms of the untt bar are shown in (e) and (f); that in (e) is known as the Siam- ese bar and that at (f) as the quad bar. 256 STEEL REINFORCEMENT Square-Twisted Bars.—The square-twisted bar consists of a square bar thatis twisted by giving it a certain number of turns around its axis, either while it is hot or while it is cold. This bar is often known as the Ransome bar. By twisting the bar to the screw shape, as shown in Fig. 2 (a), a form is obtained that has great resistance to pulling from a mass of concrete. If the square bars are twisted cold, their elastic limit and ultimate strength are increased from 8 to 25%. PHYSICAL PROPERTIES OF THE RANSOME BAR < sa - oe ‘ Hfe ais 2g y fee) oo le.) ee le. ble..| Be agea) ae io) £3 (S33) eee) 85a alse] wa (82/98 |Sbs| sae] SS Sg08).. 8» 183| ee Teese 408) gee 95/95 e 182) 28 |e ¢|/ e286 Sq 0 N18 8 eg | 28) eH a) SOU) ese Pl “s |8 | ae le sls ag 5] > §|A = 8 erie z Ay e¥ } 5 0625 213| 62,350 | 86,700 | 3,897 5,419 3 1406 478) 61,8 86, 12,176 2 2500 8 60,120 | 86,850 | 15,030 21 vis 2 3906 |1.328) 57,890 | 85,820 | 22,612 33,520 1 5625 |1.913) 56,720 | 85,240 | 31,905 47,948 $|1 7656 |2.603) 56,150 | 84,730 | 42, ,86 1 a 1.0000 |3.400)} 55,760 | 84,275 | 55,760 84,275 14/4 1.5625 |5.312) 55,450 | 83,150 | 86,641 129° 921 The physical properties of the Ransome bar are given in the accompanying table. Spiral Bar.—In Fig. 2 (b) is shown a type of twisted bar called the spiral bar. It is made by rolling steel and then twisting it. The twisted bars have elastic limits of from 65,000 to 80,000 lb. The section of the bar is practically round, with four attached half-round beads. These beads assume the spiral form on twisting the bar, and the same advantage with regard to the bond is secured as with square- STEEL REINFORCEMENT 257 twisted bars. An added advantage is assumed to exist in the elimination of all the sharp corners that occur in the square bar. Kahn Cup Bar.—One of the latest types of reinforcing bars to be commercially used is the Kahn cup bar illustrated in Fig. 2 (c). The ribs are connected by cross-ribs, forming cups, or depressions, of such a shape as to allow the concrete to flow into them readily. In this way, a positive mechanical bond in the concrete is provided. The properties of the Kahn cup bar are given in the accompanying table. PROPERTIES OF THE KAHN CUP BAR Ultimate Nominal Sectional Weicht Elastic Tensile Size Area per Foot Limit of | Strength of Bar Square Pounds Each Bar | of Each Inches Inches Pounds Bar Pounds 2 1406 .502 5,000 9,800 .893 9, 17,500 3906 1.394 14,000 27,300 5625 2.008 21,000 : 7656 2.733 28,000 1 1 3.570 37,000 70,000 1k 1.2656 4.518 47.000 ; 1} 1.5625 5.578 ; 109,400 Square-Twisted Lug Bars.—The twisted lug bar shown in Fig. 2 (d) is a development of the square-twisted bar. The square bar in this case is rolled with rounded corners, and with projections, or lugs, a at intervals, thus providing additional mechanical bond in the concrete. The rounded corners of this bar eliminate the sharp angles of the ordinary square-twisted bar. These bars have a high elastic limit. Their safe working strength is based on a safe unit stress of 20,000 lb. The properties of twisted lug bars are given in the accompanying table. Corrugated Bar.—In Fig. 2 (e) and (f) are shown two styles of deformed bar of the corrugated type known as the Johnson 258 STEEL REINFORCEMENT PROPERTIES OF TWISTED LUG BARS Size of Net Sectional Weight per Safe Working Bar a _ Foot Each Bar Inches | Square Inches Pounds Pounds } 0625 . 222 1,250 1406 .492 2,810 . 2500 .870 i . 3906 1.350 7,810 . 5625 1.940 11,250 . 7656 2.640 15,310 if 1.0000 © 3.450 14 1.2656 4.350 25,310 1}; 1.5625 5.370 3 bar, named after its inventor, A. L. Johnson. The old style of bar is shown in (e), and the new style in (f). High-carbon steel having an elastic limit of from 65,000 to 70,000 Ib. per sq. in. is used in making the Johnson bar. This type of bar was one of the first deformed bars to be manufactured. The following table gives the size, net section, and —_— of Johnson bars : SIZE, NET SECTION, AND WEIGHT OF CORRUGATED, OR JOHNSON, BARS Size of Bars Weight per Foot Net Section Inches Pounds Square Inches 4 .78 .19 1.56 .38 2.25 .55 1 2.90 .70 14 4.56 1.10 Universal Bar.—In Fig. 2 (g) is shown a type of flat deformed bar, called the Universal bar, that has been used to some extent for reinforcement. The net section and weight of the various sizes of the Universal bar are given in the following table. STEEL REINFORCEMENT 259 NET SECTIONS AND WEIGHTS OF UNIVERSAL BARS N Size of Bar Weight per Foot Net Section Ct Inches Pounds Square Inch 1 x1 13 .19 2 xX 12% 1.35 -41 3 X12 1.97 54 4 X2 2.26 .65 5 X 24 2.85 .80 Thacher Bar.—The deformed bar illustrated in Fig. 2 (h), called the Thacher bar, was devised in order to obtain a bar so deformed that the net section throughout the bar would be uniform. By having the section uniform, the bar is of the same strength at every point. In forming this bar, an SIZE, WEIGHT, AND ULTIMATE TENSILE STRENGTH OF THACHER BARS (Medium Steel) Average Diameter Weight Area of Net Ultimate of Bar per Foot ' Section Tensile Strength Inches Pounds Inches for Each Bar Pounds .16 .047 3,000 .34 210 6,400 -61 .18 11,500 .95 .28 17,900 1.39 .41 ,200 k 1.87 .55 35,200 1 2.41 A A 45,400 1} 3.06 .90 57,600 14 3.74 1.10 70,400 12 4.49 1.32 84,500 14 5.30 1.56 99,800 1% 6.15 1.81 115,800 13 7.07 2.08 133,100 1¢ 7.99 2.35 150,400 2 9.01 2.65 169,600 260 STEEL REINFORCEMENT effort is made to eliminate all sharp corners. The Thacher bar is rolled from medium steel and has an elastic limit of about 35,000 lb. The accompanying table gives the size, weight, and ultimate tensile strength of the Thacher bar. SIZE, AREA, AND WEIGHT OF DIAMOND BARS Pi eta coe Area of Section Weight per Foot Tackas Square Inches Pounds L .062 22 f .14 -48 .19 -65 + .25 85 .39 1.33 .56 1.91 .76 2.60 1 1.00 8.40 14 1.56 5.31 Diamond Bar.—One of the most recent forms of deformed bars is the Diamond bar, which is shown in Fig. 2 (7). This bar is rolled with a cross-section of constant area. The nominal size, area, and weight of Diamond bars are given in the accompanying table. NK Ze Kahn Trussed Bar.—Fig. 3 shows two styles of a deformed bar known as the Kahn trussed bar. In the old style of bar, shown in (a), the prongs are opposite each other; in the new style, shown in (db), they are staggered. The shapes of the bar STEEL REINFORCEMENT 261 in section are shown in Fig. 4. The fins are partly sheared across and also in a direction parallel with the axis of the bar, and are bent up, as shown in Fig. 3 so as to form a grip with the concrete and to provide the stirrups, or web members, necessary to resist diagonal stresses. The Kahn bars are made in the several sizes indicated in Fig. 4. The respective sectional areas of the bars are also “> M$ $14 Bar-Weight=1.4 tb. per foot-Area=0.41 SGM. 2436 Bar-Meight =/02 1b. per foot-Aréd=3.00 SG.li- 3228 Bar-Meight=27 lb per foor —hreda0.79 SF M7. 1x3 Bar-Weight «48 /b. per foot -Aréa=141 5g.la ae rads Bar-Weight =68 1b. per foot-Ared=200 59.1. Fic. 4 given in this figure. These bars are rolled of mild steel, as this metal will best stand the shearing stresses to which the bar is subjected in manufacture. The elastic limit of the metal in the bars ranges from 33,000 to 35,000 Ib. per sq. in. Trus-Con Bar.—Another deformed bar, known as the trus-con bar, is illustrated in Fig. 5. This bar is round in 262 STEEL REINFORCEMENT section and has notched shoulders for holding washers. eee Fic. 5 The washers are punched so that they will slip over the projections, and, then by turning, they are locked with the bar. The trus-con bar is made in ' §. 8-1, 14-, and 1}-in. sizes. Monolith Steel Bars.—In Fig. 6 is shown the monolith steel bar. This type of bar has no sharp cor- ners, and is not reduced in area or strength by deformations. It also has large surface area. The bar is grooved on the sides so Fic. 6 that round iron stirrups, as shown ata, may be inserted. These stirrups are held in place in the bar by swedging the flanges of the bar together. The monolith steel bars are made in sections equivalent to 3-, 8-, 1-, and 14-in. square bars, and are rolled for stirrups of 3%s-, #s-, 3-, and 4-in. diameter. Columbian Bar.—A rolled shape known as the Columbian bar is extensively used in the construction of the Columbian fire- proof floor systems and reinforced-con- crete structures. The typical forms of this type of bar are shown in Fig. 7. (a) Mild steel is used for rolling the Colum- bian bar. This kind of steel has an ul- timate strength of from 60,000 to 70,000 Ib. per sq. in. and an elastic limit of one- half the ultimate strength. The smallest bar, shown in (a), is known as the 1-in. bar, while the type of bar shown in (db), is made in 2-, 24-, 34-, and 44-in. sizes. The 5-in. bar carries a double rib at the bottom. (bo) Fic. 7 STEEL REINFORCEMENT 263 U Bars.—In Fig. 8 is shown a section of U bar that can be used to advantage in reinforced-concrete construction either as a tension or as a compression member, being particularly efficient for the latter pur- pose. These bars are rolled from high elastic- limit steel, and are in some instances made from rerolled steel rails. They are }, ¥%, %, and 4 in. in thickness, weigh. from 3 to 9 lb. per ft., and can be ob- tained in lengths up to 60 ft. Structural Shapes Used as Steel Reinforcement.—The usual rolled-steel structural shapes have been used extensively for reinforced-concrete construction. They have an advantage in that they can be readily obtained. Structural shapes as metallic reinforcement for concrete work are being super- seded by either plain or deformed rolled bars. One advan- tage of the use of structural shapes is that a rigid framework can be built up, after the manner of skeleton construction, though of much lighter section, and the concrete then filled in around it. Expanded Metal. Among the earlier forms of metallic (a) : reinforcement for concrete is the dis- torted steel plate known as expanded metal, a familiar il- lustration of which is shown in Fig. 9 (a). This form of reinforcement is manufactured by partly shearing a sheet of steel in parallel rows, as shown in Fig. 9 (b), and then pulling the ma- terial sidewise, thus forming a diamond mesh. In this way, the area of a sheet is increased about eight times, with acor- tesponding decrease in weight per unit area and without any waste of material. The steel from which expanded metal is Fic. 9 STEEL REINFORCEMENT 264 f 9 a af ai OOL‘Z% 92° T 898° 4 9 al et ai 002 FT 8" 5 ¥ ag & 8 sg or 000 1% 98° T OOF” Z ag € 8 *e ai OOF 6T L40°1 com OT ap € 8 7¢ as 009 FT 18° £S" or 1? € 8 ae ai 0026 gg" GOT” OT hs g 8 . 4 él ogs'9 Lg" 601" a ™e € 8 - él Orgs 0Z° 6S0° 9T 7 16 9 7 8 008' 2 4a Ost" 91 13 9 = 8 066 ¢ 66° 280° 9T me a! € *p a 00€ TT 9° 88ST" a p 4 a *p 8 006 ST 98° £93" a ae sa oe 8 002'Z1 69° £02" 8T spunog yout 1294S yout 400 he psa soeyout | yout 00 | yp axenic arenbg 7005 azeredag| 4 oN qSeW TeeW | S}e0yg jo Jad 47PEM ome Jo, | mabe | udu | sporny | yaduoy | “Grdteg. | SPURCd 12a tase [prepueag PEM O1sely TYqSIOM [euorjoeg EO WS TIVLAW GHAGNVdXa AO SAZIS STEEL REINFORCEMENT 265 manufactured has a unit tensile strength of about 65,000 Ib. and an average elastic limit of about 30,000 lb. It is 7 “) Fic. 10 principally used in reinforced-concrete construction as slab reinforcement. The sizes of expanded metal are given in the accompanying table. Kahn Expanded Metal.—Another concrete-slab reinforce- ment, called Kahn expanded metal, is shown in Fig. 10. This PROPERTIES OF KAHN EXPANDED METAL eae f > od ~ o. '§ e) ® 2 4 § Once a (e) pA S| o & tu oes on = £[ So 8 loess) BS 8 | Gegg | oy aS a g |A2 Gigs | Og ¢ 260 § “wo |fo 8 © 3 o Oe ss eon BD rs) Ss 3 om & q ee fe) lal ° af |.Ms 5 2/\s “lo8e8| S8eR Gyr | eS | O50, # jeefs gem | oe 2 |Fg soz | | “Shr alee 2/ 2 |,.48 | 8,640 | 33,600 17, 3), 2.43 Sree (|- 82 5,760 22,400 25 | 1.48 4) 4 | 124 | 4'320 | 16800 | 33 | 1.08 5 5 |-..19 3,420 13,300 | 41 | .87 6} 6 | .16 | 2880 | 11,200 | 49 72 7 7 .14 2,520 9,800 | 57 62 S| 8 .12 | 2,160 65 55 form of reinforcement is manufactured by shearing a rolled - section along lines parallel with its length, and then pulling 266 STEEL REINFORCEMENT the metal so sheared in a direction at right angles to the lines of shear. In this type of expanded metal, the main bars of the section represent the material available for the rein- forcement of the slab, while the light cross-bars act as spacing bars and also as shrinkage rods when embedded in concrete. The advantage claimed for the Kahn expanded metal is that it transmits the load directly to the supports without any tendency to elongate or distort. The properties of this reinforcing metal are given in the accompanying table. Herring-Bone Metal Lath.—In Fig. 11 is shown a type of expanded metal known as herring-bone metal lath. This. STEEL REINFORCEMENT 267 metal is particularly interesting, because, when bent into the form shown in Fig. 12, it provides a self-centering material that is useful for light roof construction. When bent in this manner, the herring- bone expanded metal is known to the manufac- turers as trussit. The lon- gitudinal ribs, as at a, give it at least sufficient trans- verse resistance to allow the placing of a thin roof slab of concrete on it without other centering or > support. Sheet-Metal Reinforce- ment.—The type of metal reinforcement known as Ferroinclave is used for making floor slabs and for stair and roof construction. This reinforce- ment consists of sheet metal that is bent into grooves, as indicated in Fig. 13 (a), annealed sheet steel generally of No, 24 U. S. gauge, being used in its manufacture. The corrugations are made dovetailed in section so that the end of one sheet can slip into another, as shown. The sheets are 20§ in. in width and 10 ft. in length. Fig. 13 (b) shows ’ how this type of metallic reinforcement is used in con- structing a slab for a light roof. Lock-Woven and _ Tie-Locked Wire Fabric.—In Fig. 14 (a) is illustrated the form of wire net- ting known as lock-woven witre fabric. The cross-wires of this (») fabric are joined by means of a staple of light wire, which is bent so as to embrace the cross- ing wires at their intersection. Another type of junction for cross-wires is shown in Fig. 14 (b), which illustrates the principal features of the tie-locked fabric. Here, the cross-wires are secured, or Fic. 13 (a) Fic. 14 268 STEEL REINFORCEMENT locked, in position by means of a small disk, or washer, and 4 La Fic. 15 i by kinking the wires. Electrically Welded Fabric.—The Clinton wire cloth is a fabric that is secured at the intersections by a per- fect electric weld, and it has at intervals a double wire that twines in and out, as shown at a, Fig. 15. Triangular- and Square-Mesh Wire Reinforcement. — The two types of wire re- inforcement shown in Fig. 16 are extensively manufactured for reinforced-concrete construction. The reinforcement shown in (a) is known as the triangular-mesh reinforcement, and that shown in (bd), as the square-mesh reinforcement. The latter consists of heavy longitudinal wires and cross-wires, or spacing wires. \\ — — =I) Fic. 16 The cross-wires are carried through and (8) twisted around the longitudinal wires so as to form the rectangular spaces. STEEL REINFORCEMENT 269 SYSTEMS OF STEEL REINFORCEMENT LOOSE-ROD SYSTEMS A complete floor system constructed of loose rods is shown in Fig. 1. The beam reinforcement consists of three rein- forcing rods. Two of these rods run straight through the entire length of the beam, as at a, while the third one is bent upwards at the ends, as at b. This bent member provides tensile resistance at the top of the beams and thus takes care of the negative bending moment, which occurs in all beams fixed at the end. The bend in such rods is usually made at an angle of about 30° with the horizontal. The rods should be straight at the center of the span for at least one-third the distance between the supports. A tie-rod c that is 4 or 5 ft. in length, and sometimes bent down at the ends, should be placed over the top of the beam juncture. The girder reinforcement consists of five rods, two of them being bent up, as shown at e, to provide against negative bending moment. In the best work, two short rods? are located transversely through the column. These rods tie the adjoining girders together and provide additional rigidity at the junction of the girders with the column. The slab rods, shown at h, are generally spaced at about 6 inches from center to center. They should bond with the stirrups, or web reinforcement, of the beams, and may be threaded through, interlocked, or wired to them. It is customary to provide shrinkage rods that extend at right angles to the regular slab reinforcement, in order to prevent shrinkage cracks in the concrete. For this purpose, }-in. round or square rods 7 are generally used, and these are spaced about 2 ft. from center to center. In order to bond the concrete over the main girders securely, it is also good practice to provide over these important members rods d of about the same size asthe slabrods. These rods should fun through holes punched in the top of the stirrup, as 270 STEEL REINFORCEMENT pe ; iN" | mill Fic. 1 STEEL REINFORCEMENT 271 illustrated at g, and should extend at right angles to the axis of the girder. Sometimes, similar rods are used in the slab over beams, as shown Sea at k, —=— _ The longitudinal reinforce- ment of the concrete columns consists of four round rods /, It is customary to project them above the concrete of each story about a foot and to splice them by lapping and wiring or by using pipe sockets m, as illustrated. Frequently, it is not possible to lay out beforehand the electric-light or power wiring, but if this installation is to be adopted l}-in. pipes to serve as a REE] passageway should be embed- “ ded near the center of the span of all beams and girders, close to the under side of the slab aa construction, as at m. Kahn System.— The i alite -—— system of reinforced-concrete construction is based on the said use of the Kahn trussed bar. -—— A typical monolithic construc- tion based on the use of the Kahn system is shown in aR Fig. 2. The ani ©: of the beams " and girders are ee es ae ** shown at a,and Sed Peps ee dads Se re 2 Fic. 2 _ they consist of 272 STEEL REINFORCEMENT Kahn bars with the prongs bent upwards so as to form stirrups. The bars are usually placed in the forms on a 2-in, bed of con- crete, and after being centered, or registered in their proper posi- tions, they are secured by wiring or by block- ing. In order that the girders and beam connections over col- sie Ket i. perpen ah aetna oooh Ceniiheaes Idee eS ee EE EPCRA 3, vib a ae ke : = | umns may have con- ies tinuity, an inverted 4 Kahn bar b is used b over such junctions. Kahn bars are spaced in each corner of the column, as shown in Fig. 3, with the prongs bent at right angles. The bars are usually tied to- gether with heavy wire or light rods, wound around them as shown part way up the col- umns in Fig, 2. The Kahn bar is fre- quently used with con- crete and hollow terra- cotta tile to form floor systems designed for light loads. This type of construction is illus- trated in Fig. 4. In view (a) is shown a ie ii (@) Fic. 4 5 rs) asa pee ved wane Hh : : paves ves pep eee Reo he ERS S Hs BA fetes. + Sakeer S- SSeS ear casas ow 7 STEEL REINFORCEMENT 273 cross-section of the construction through the beams or secondary members, of the floor system. Usually, the tiles are from 12 to 16 in. in width and from 6 to 12 in. in depth, the hollow part having the cross-section indicated at a. The tiles are spaced about 53 in. apart, and in the space between them is laid concrete that is reinforced with Kahn bars. The concrete is carried over the top of the tile to a depth of about 2 in. The Kahn bar shown at b in (6b) is provided with the usual prongs, or stirrups, which are bent upwards toward the abutments. The tiles c are serrated, or corrugated, along the sides, so as to provide some shearing strength in addition to the adhesion of the concrete. During the construction of this floor system, the Fic. 5 tiles should be held temporarily in position either by placing blocking between them or by nailing them to the forms. It is not customary in this type of construction to use shrinkage rods in the slab that is laid over the top of the tile. Since the tiles are quickly laid on the centering and, con- sequently, minimize the quantity of concrete required for the construction of the floor, and, also, since the concrete placed in conjunction with the tiles sets more rapidly than when placed alone, this particular type of construction can be carried on with considerable rapidity. Such a floor con- struction as this, embodying tile having a hollow air space, acts as a good deadener of sound and also tends to preven: hcat from passing from one floor to another. 274 STEEL REINFORCEMENT Merrick System.—In Fig. 5 is shown the Merrick floor system of reinforced-concrete construction. The space between girders is occupied by narrow concrete beams a, as shown in the transverse section (a). Between these beams are placed boxes made of one of the many styles of metal fabric on the market. These boxes run the entire length of the clear span of the floorbeams, as shown in the longitudinal section (b), and serve to make the floor lighter. They are indicated in both views by the heavy dotted lines b. Above and below the metal-fabric boxes is a layer of con- crete. This layer is usually made about 2 in. thick, so as to give a flat ceiling and a flat floor surface. Gabriel System.—The Gabriel system of reinforced-concrete construction consists of steel reinforcing bars to which are attached round-iron stirrups. These stirrups are formed by wrapping a wire a several times around the reinforcing bar Fic. 6 and extending it up into the slab, as illustrated in Fig. 6, which shows this particular type of construction complete and in its several details. The wiring of the columns is continuous, and extends from the bottom to the top, as indicated in the figure, particularly in the sectional view (0). Several of the reinforcing rods of both the girders and the beams bend upwards, as shown at c and d, respectively. They also lap over the center of the column to form an additional bond in the concrete, as shown at e. In this sys- tem of construction a lap bar is sometimes provided at the top of the junction, as shown. The slab is shown reinforced with woven wire and shrinkage rods of round iron. STEEL REINFORCEMENT 275 With the Gabriel system of floor construction, hollow tile is also used, as illustrated in Fig. 7. The system shown in view (a) is suitable only for very light construction. The hollow tiles a are sandwiched between reinforced-concrete joists, as at b, and the reinforcement of the floor consists of a main reinforcing bar c, around which a round-iron stirrup is wrapped so as to extend continuously. A similar con- struction is shown in view (b). Here, however, a slab of Fie. 7 concrete is extended over the top of the tile, thus giving additional compressive strength at the top of the concrete beams and permitting this construction to be used for heavier loads. Mushroom System of Reinforcement.—A system of rein- forced-concrete construction that differs from all others in that no beams nor girders are used throughout is illustrated in Fig. 8. This system of construction, termed the mushroom 276 STEEL REINFORCEMENT Fic. 8 RANI iT Wit \\ \\\ a\\\\\W ji | NIN \\W \ \ i { Wy: \\ call ) if i NO WEI iM VA S\ Vit 4; A y STEEL REINFORCEMENT . 277 system, consists of reinforced columns that have a spréad cap of heavy reinforcing bars radiating from the column, as illustrated at a, Fig. 8. These rods are held radially by circular reinforcing bars b, to which they are securely wired. By means of this heavy reinforcement, the column is greatly strengthened at the top, and by spreading in this way, it supports a large portion of the floor slab, after the manner of radiating cantilevers. The flat slab that covers the column supports is reinforced in several directions with light reinforcing rods. , FABRICATED SYSTEMS Unit System.—The girder frame in the unt system is now made of plain bars, and the stirrups in the latest develop- ment are in the form of an inverted U, the construction of the frame being as shown in Fig. 9. The frame shown in view (a) is fabricated, or fastened together, by a shrinking process; that is, each stirrup and tie-rod is hot-shrunk to the main members. This girder frame is designed to withstand the hard usage of shipment and unloading. The type of frame shown in view (b) is designed for use in districts located so far away from the shops of the manufacturer as to make the freight rates for shipping complete frames prohibitory. In the frames shown in Fig. 9 there are four main rein- forcing rods a, although the frame may be made up with any 278 STEEL REINFORCEMENT number of rods necessary to secure the desired sectional area. The two rods at the top are bent upwards, as shown at 3, and the ends ¢ are turned over so as to add to their grip in the concrete. The stirrups in both frames are shown at d, 2-in. round bar iron being used for the stirrups of the frame shown in view (a), and light strap, about 4 in. <1 in., for the stirrups of the construction shown in view (b). In the latter frame, the section at the right of the figure shows the reinforcing bars held in the clamping device, which con- ‘+sists of the casting e, the clip f, and the stirrup g. These parts are secured by means of a bolt h. Pin-Connected Girder Frame.—Another type of rod rein- forcement built up in the form of a girder frame is illustrated in Fig. 10. This reinforcement is known as the pin-con- nected girder frame, and it is arranged so that the frames forming the reinforcement of the beams and girders may be connected by pins and links at intersections and over column supports. " Cummings System of Reinforced Concrete.—The system of steel reinforcement shown in Fig. 11, known as the Cum- mings loop-truss girder, consists of a series of main reinforcing bars a, to which are attached a set of smaller bars b that turn up at the ends and form a loop welded at the ends. These STEEL REINFORCEMENT 279 loops are secured to the main reinforcing rods by means of metal clips c. Fic. 11 Shear-Frame System of Steel Reinforcement.—The shear- frame system is employed to resist the negative, or reversed, bending moments that occur at the points of support of monolithic beams and girders. This type of reinforcement consists of a built-up frame constructed as shown in Fig. 12. The shear frame consists of straight top rods a and bent bottom rods b. These two sets of rods are securely clamped together by means of flat bar-iron plates, or clips, c, which also act as stirrups. Additional stirrups are provided at g, Fic. 12 and where the top and bottom rods join they are firmly fastened together by means of special clamps f. 280 STEEL REINFORCEMENT This type of reinforcement provides a positive tie, or junction, between beams and at the intersection of beams, girders, and columns, insuring against failure at these points by providing resistance to shear and to failure by horizontal Fic. 13 or oblique tension cracks. The frame may be used with any type of reinforcement, and is placed at the junction of. beams with girders, as shown in Fig. 13, and at the inter- section of the girder and column supports. MISCELLANEOUS SYSTEMS Brayton System.—The system of reinforced concrete known as the Brayton is illustrated in Fig. 14. The main reinforcing member is a standard, rolled-steel, I-beam section, and the entire reinforcement, including the steel- work, is put together in a manner similar to the usual-steel- frame construction. The structural-steel beams that form the reinforcement carry the dead load of the centering and the weight of the concrete. Thus, shores need not be used in the erection. The I-beam a forming the main reinforcing member of the concrete beam is shown in view (a). As shown at b, the stirrups extend beyond the top flange of the I beam in the form of loops, and are either riveted through the web or fastened by clipping them to the lower flange, as indicated in (b). The I beam is supported on a column built up of angles and provided with brackets d. The slab rods are STEEL REINFORCEMENT. 281 fastened to the stirrups by means of clips and wiring, as shown in detail in view (c). ear Fic. 14 Visintini System.—Another system of concrete construction is the Visintint system. A general view of a girder con- structed according to this system is shown in Fig. 15. The girders can be made of any width and breadth required to withstand the stresses. In France, the columns of buildings are also built by this system, but in the United States solid columns have been preferred. The beams are made along Fioe.. 15 the lines of latticed steel girders. In light work, the vertical webs a, which are in compression, are not always reinforced, 282 CONCRETE DESIGN but the slanting webs b, which are in tension, always have steel in them. The upper and lower chords contain each a set of three reinforcing rods, as shown at d and e, respect- ively. The beams may be made in any convenient location — and put in place on the job afterwards. When solid rein- forced-concrete columns are used with this system, these columns are cast in place and are provided with brackets to hold the principal girders. These girders are then hoisted on to these brackets. Part of the end of the girder is made solid, as shown at c, in order to resist the stresses in shear and direct compression due to the reaction of the support. DESIGN OF CONCRETE STRUCTURAL MEMBERS “PLAIN CONCRETE CONCRETE BEAMS Method of Design.—Stone and plain-concrete beams are designed by exactly the same method as any other kind of beam, except that the weight of the beam itself can hardly ever be neglected. The formula employed is as follows: in which M is the bending moment; s, the wnit stress pro- duced; J, the moment of inertia; c, the distance from the neutral axis to the most remote fiber; and S, the section modulus. : b d2 In a beam of rectangular section, aie Se in which b is the breadth of the beam and d is its depth of the beam. The modulus of rupture for various kinds of stones and other materials is given in the accompanying table. With the values in this table, a factor of safety of from 10 to 20 is usually employed when problems dealing with the CONCRETE DESIGN 283 MODULI OF RUPTURE OF VARIOUS MINERALS Modulus ° Fh Material Rupture Slate. . AS a POR fe a He Re Glass. . ; — Bluestone flagging. . Marble, white, Italian. . Marble, white, Vermont.. Marble, gray, ‘Vermont. . Granite, Quincy, Massachusetts. Granite, New York.. Granite, Connecticut. . Sandstone, Massachusetts. . Sandstone, Middletown, Connecticut. . Sandstone, Ohio.. Freestone, Little Falls, New York... Freestone, Belleville, New Jersey. . Freestone, Dorchester, Massachusetts. Freestone, Hubeginy.. : Freestone, Caen, Normandy. . Limestone, average value. . Brick, common, or Philadelphia pressed. Brick, best hard. . So ecegen sas Rubble masonry in cement. Sena ict se abe 200 ae) - - - - bent ben Fr rk fen rt ret DN CD Oo - — sungubasszessuesuss safe load instead of the ultimate breaking load are being solved. The weight of the stone itself must almost always be taken into account. ExAMPLE.—Design a Quincy granite lintel 6 in. wide on a 5-ft. span to carry a uniform load, which includes its own weight, of 300 lb. per ft., with a factor of safety of 10. SoLuTIon.—In this example, W =300X5=1,500 lb. and 1=5X12=60 in. Therefore, Ae OO raga in.-lb. 8 8 According to the table, the modulus of rupture for Quincy granite is 1,800, and if a factor of safety of 10 is used, the value of s is 1,800+10=180 lb. per sq. in. Therefore, : 68¢ Tag Les , dureq F-Z-1 |° °9}eI0U0d euOjsOWIY’T © 99¢ Ig SSP uInI pay, $-Z-I |° eJe1NU0d BuO SOUT L0G LSP GoP JM $-Z-I |° eJetOU0S suUOYsOUUVT 96F C6PF OF dweq P-Z-1 | °° 939INUOD JOABIL) 06S LLY ISP tun pe $-Z-I |° °°" * eyeTOUOd JeARILy Ger O8S 16§ JOM #-Z-I |' °° °° eJerNUOD JEAvINy 8T9 16g 667 dweq $-Z-1 ** gqarouoo oyluRINy 99¢ 9E¢ CLP umtpeyL $-Z-L |' °° * eyeroUOD 9yIUeILD) 6E¢ TO¢ GLE JOM $-Z-I |' °° * oyarouOD o4lUeIT 0SZ GGG 86T dureq G-Z-T |° °° °* ayerouUOD Japulg LLG T&S S61 unt psy] G-2=] ** 9gar0u00 7opu OFS OFS CLI pbs thot = G-Z-T |° °° *° a}e10U0d Jepul 048 | 798 | css | 989 | 068 Cate % ne aoe) I Soe eesoreqsORy O80'T | 800'T | 9Z0'T | 888 88¢ { AIp JO yy StoM } ¢-I + ws ite n> ot ODE s %F' TT ‘7072 ‘ ‘ : ‘ [elioyzeur Ap jo mig go's | e96't | F249'T | ZIS'T | 192 |{qusiom srg save S quouleo JvoNy IAT | 4M9OZ| AMET) AMP | AMT! “VPT . AdU94SISuUO? a [eHozey, sesy snore, ye oinjdny jo snfnpoy; GLAAXONOD dO AANIdnAaA AO TINGOW 284 CONCRETE DESIGN 285 Substituting these quantities in the formula M=S s, then 11,250 =d2X180. Thus, d?=62.5 and d=7.906, say 8, in. The modulus of rupture of concrete is usually less than that of stone. The table on page 284 gives values found by the United States Geological Survey. Three degrees of wetness are recognized in mixing the concrete, namely, wet, medium, and damp. Wet concrete is such that sufficient water is added to make it semiliquid; damp concrete is decidedly granular, with little tendency to lump; while medium concrete is of a consistency between the other two mixtures. The values given in the table are mostly for 1-2-4 mixtures. A 1-3-6 mixture gives values at least 15% lower than the 1-2-4 mixture. The factor of safety employed is sometimes 4, but usually 6 or higher, as the strength of concrete is uncertain. EXAMPLE.—Design a concrete beam 12 in. wide on a 12-ft. ‘span to carry 800 lb. at its center. The safe working stress is to be 100 lb. per sq. in. Wl 800Xx12x12 SoLuTION.—The moment is equal to Sa = apa = 28,800 in.-lb. Assume the beam itself weighs 260 Ib. per ft. Then the moment due to the dead load is 260 X12 X12 X12 = 56,160 in.-lb. The total moment is 8 56,160 + 28,800 =84,960 in.-lb. Substituting the correct 12x a? values in the formula M=Ss, then 84,960= a X 100. Therefore, d?= 424.8 and d=20.6, say, 21 in. CONCRETE COLUMNS Plain-concrete and stone columns may be divided into two classes, namely, those which are centrally loaded, and those which are eccentrically loaded. The height of the column should never be more than twelve times the least dimen- sion of the cross-section and even less for stone and brick. Column Centrally Loaded.—For a centrally loaded column the allowable compressive stress per square inch is multiplied by the area of the cross-section of the column to find the { 286 CONCRETE DESIGN allowable load. Thus, if it is decided to allow an intensity of stress of 300 lb. per sq. in., and the column is of square section 10 in. on a side, the allowable load will be 10 x 10 x 300 =30,000 lb. The breaking load’'on columns between two and twelve times as high as the least dimension of their cross-section seems to be independent of their height. A column between these two limits, however, cannot with- stand as high an intensity of stress as a cube, for it is more ULTIMATE UNIT CRUSHING STRENGTH OF STONE CON- CRETE WITH PORTLAND-CEMENT MORTAR Proportion of Compression ~ Ingredients Pounds per Square Inch Cement Sand Stone | 7 da. | 1 mo. | 3 mo. | 6 mo. 1 2.0 4 1,600 | 2,150 | 2,400 | 2,500 1 2.5 5 1,480 | 1,950 | 2,250 | 2,350 1 3.0 6 1,250 | 1,800 | 2,100 | 2,200 1 3.5 7 1,100 | 1,660 | 1,960 | 2,080 1 4.0 8 980 | 1,520 ,820 | 1,950 1 4.5 9 850 | 1,400 | 1,690 | 1,840 1 5:0 10 750 | 1,260 | 1,550 | 1,720 1 5.5 11 650 | 1,120 | 1,420 | 1,600 1 6.0 12 600 | 1,000 ,300 | 1,500 NOTE.—For gravel concrete, use 75% of the figures given in the table. likely to break by shearing. For this reason, when employ- ing values taken from the tables on pages 286 and 287, for column calculations, a larger factor of safety should be used than with other work. This factor is usually taken as at least 6, and 10 or higher for masonry. EXAMPLE.—What is the allowable working load ona concrete column that is 10 ft. high and 12 in. in diameter and made of 1-2-4 stone concrete 6 mo. old with a factor of safety of 6. SoLutTion.—The cross-sectional area of the column is .7854 X 12?=113.1 sq. in. From the table the ultimate CONCRETE DESIGN ULTIMATE UNIT CRUSHING STRENGTH OF VARIOUS STONES AND STONE MASONRY PIERS 287 © +25 0 wea > >: Peta Bon wn Material RECe Material Esve pgs Eg 8 3 8 ug 5 ah Granite, Colo.......| 15,000 | Limestone, Mar- Granite, Cotin:-3..% 14,000 quette, Mich....... 8,000 Granite, NOS <2 ps'k' 16,000 | Limestone, Consho- Granite, Me......... 15,000 hocken, Pa... 15,000 Granite, Minn. .....| 25,000 | Marble, Montgomery Granite: IN eyo 22s: 16,000 CORIPAS< (See ees 11,000 Granite, N. H. .....| 12,000 | Marble, Lee (dolo- Bluestone.......... 15,000 mite), Mass........ 22,800 Sandstone, Middle- Marble, Pleasantville town, Conn....... 7,000 (dolomite), Y..| 22,000 Sandstone, Long- Marble, ltalian. . .| 12,000 meadow, Mass... .| 10,000 | Marble, Vt.. 0,000 Sandstone, Hudson Slate. . oi ec dee ,000 River, N. Y.. 12,000 | Piers, ‘ashlar, Blue- Sandstone, Little stone. ; 2,100 Falls (brown), Granite, ashlar piers. 2,100 i Micense sce ce 2} 40.000: | Piers; ashlar, lime- Sandstone, Ohio... . ,000 stone. 1,500 Sandstone, Hum- Piers, ashlar, common melstown (brown), sandstone........ 1,050 Be bees Se eas 12,000 | Piers rubble, cement Limestone, Kings- mortar. é 900 nm, N. 12,000 | Piers, rubble, lime Limestone, Garrison mo sos intake 480 Station, 'N. Y.. 18,000 Limestone, Bedford (oolitic), Ind. ....| 8,000 crushing strength of 1-2-4 concrete 6 mo. old is 2,500 Ib. per sq. in. _ 2,500 of stress is a7 2 carry is 113.1X 2000 = 47,125 Ib. Using a factor of safety of 6, the safe intensity Then the safe total load the column can 288 CONCRETE DESIGN ULTIMATE CRUSHING STRENGTH OF BRICK MASONRY PIERS (Average Age of Brickwork, 6 Months) Oo ud 9 4 2 E Material Composition of Mortar | & he e HES Bao 2 Oo AeA Wire-cut brick......... A 1 cement} 5 sand 3,000 Dry-pressed brick....... 1 cement, 5 sand 3,400 Dry-pressed brick....... 1 cement, 1 lime, 3 sand | 2,300 Repressed brick. 1 cement, 5 sand 1,700 sass ot gpa sand-struck rick. . 1 cement, 5 sand 1,900 Li ie, " sand-struck rick. . 1 cement, 7 sand 853 Hard, sand-struck brick. 1 cement, 1 sand 2,100 Hard, sand-struck brick.| 1 cement, 1 lime, 3 sand | 1,500 Hard, sand-struck brick. 1 cement, 5 sand 1,200 Sand-lime brick......... 1 cement, 3 sand 1,100 Sand-lime brick......... 1 lime, 3 sand 450 Sand-lime brick......... Neat cement 1,400 Terra-cotta work.... 1 cement, 3 sand 2,000 Eccentrically Loaded Column.—The stress on an eccen- trically loaded column is computed by the following formulas: For circular columns, Oe ds ser he oe For rectangular columns, P GP, TA? id In these formulas, s is the stress, in pounds per square inch, developed in the column; P, the total load on the column, in pounds; A, the area of column section, in square inches; é, the eccentricity of eccentric part of load, in inches; P,, the eccentric part of load in pounds; d, the diameter of column, or dimensions measured in the plane of the eccen- tricity, in inches. CONCRETE DESIGN | 289 If the total load is eccentric, the formulas just given reduce to the following: For circular columns P. (, ,8¢ s=— a A d For rectangular columns, P.(, , 6 A gem ae A d According to these formulas, it is necessary first, in design- ing a column that will stand a given load, to select by inspection the section of column that seems to be about correct, and then to solve the equation fors. This value of s must be less than the allowable working stress it is pro- posed to use. If it is larger, a larger area of column must be selected, and the problem worked out again; if it is very much smaller, possibly too large a section for economy has been selected, and in this case a smaller section should be assumed and the equation again solved for s. It should be borne in mind that the height of the column must not be greater than twelve times the least dimension of the cross- section. The eccentricity should not be so great as to cause tension in the column. EXAMPLE.—Design a cylindrical column of 1-2-4 stone concrete, 18 ft. high, to carry with a factor of 6, a central load of 100,000 lb. and an eccentric load of 100,000 Ib., the eccentricity being 4 in. SoLUTION.—Since the column is 18 ft. high, it should be at least 18 in. in diameter. The ultimate crushing strength may be taken as 2,500 lb. persq. in. in6mo. The safe working stress would therefore be 2,500 +6=417 lb. per sq. in. A column 28 in. in diameter will be tried first. The area of the cross-section is .7854 X 282, or 615.75 sq. in. To apply the first formula, A = 615.75, P=200,000, P,=100 000, e=4, and d=28. Substituting in the formula, ne 8 X 4X 100,000 615.75 615.75 X 28 =325+186=511 Ib. per sq. in. 290 CONCRETE DESIGN This stress is larger than the allowable stress, which shows that the column section selected is too small. If a section 31 in. in diameter is assumed, then, A=.7854 X 31°=754.77 sq. in. Substituting in the formula, _ 200,000 _8x4x 100,000 754.77 = 754.77 X 31 Since this is less than 417 lb., a column of this diameter is safe. In a fire, a column is apt to be injured by the heat to a distance below the surface of 14 in. Therefore, in design- ing columns by the preceding methods, 14 in. should be added all around the column proper. Ss = 402 lb. per sq. in. REINFORCED CONCRETE BEAMS The design of reinforced concrete is not an exact science. The majority of the recommendations and formulas herein given are taken from the excellent report of the ‘Joint Committee.”’ The Joint Committee is a committee of mem- bers of the American Society of Civil Engineers, the American Society for Testing Materials, the American Engi- neering and Maintenance of Way Association, and the Association of American Portland Cement Manufacturers formed ‘“‘for the purpose of investigating current practice and providing definite information concerning the properties of concrete and reinforced concrete.” Only Portland cement is suitable for reinforced concrete. The aggregate is divided into two classes, namely, fine and coarse. Fine aggregate consists of sand, crushed stone, or gravel screenings, and which, when dry, passes through a screen having holes } in. in diameter. Coarse aggregate consists of crushed stone or gravel which is retained on a screen having holes 4 in. in diameter, but which passes through a screen having holes 1 in. in diameter or smaller. In both fine and coarse aggregates, a gradation of size of the particles is generally desirable. CONCRETE DESIGN 291 Cinder concrete is not suitable for reinforced-concrete structures. For reinforced-concrete work, a mixture based on the pro- portion of 1-6 is generally used; that is, 1 part of cement to a total of 6 parts of fine and coarse aggregates, measured separately. The fine and coarse aggregates are often in the proportion of 1-2, which makes a concrete that is commonly called a 1-2-4 mixture. Forcolumns, richer mixtures are often required, and leaner mixtures can often be used in mass work. Moving live loads and suddenly applied loads require special consideration. These loads can often be taken care of by increasing the amount of live load used in the cal- culation. The weight of the beam or the floor slab itself should always be considered when estimating the dead load. The span length of beams should be taken as the length from center to center of supports aad not of the clear span, but it need not be considered longer than the clear span plus the depth of the beam. Brackets are not considered as reducing the clear span. In the formulas about to be given, rather than employ ultimate stresses and divide the result by the factor of safety, working, or safe, stresses should be used. Rectangular Beams.—The following notation will be used in the design of beams and columns: F,=tensile stress in steel, in pounds per square inch; F,.=compressive stress in concrete, in pounds per square inch; E;=modulus of elasticity of steel; * E-=modulus of elasticity of concrete; n=E,+E,; M=moment of resistance of beam, in inch-pounds; A=area of steel, in square inches; b=breadth of beam, in inches; d=depth of beam, in inches, from top to center of steel reinforcement; k=coefficient; j =coefficient; A p=ratio of area of steel to bd= bd’ 292 CONCRETE DESIGN First assume values for F;, F,, and . These values are usually controlled by building ordinances. The following values are recommended as safe working values by the Joint Committee and are used throughout the text to serve as examples in working out problems used as illustrations: F,=16,000; F-=650; »=15 for concrete capable of devei- oping an average compressive stress of 2,000 pounds in 28 days when tested in cylinders of specified shape. After values of F;, F,, and m are decided on, substitute them in the following formula and solve for . This formula gives the value of » that makes F s and F, reach their full values under the same load. 1 p=4tX Baa) F, \nF, Substituting the values mentioned above 1 = = .00769 tities: 16,000 / 16,000 650 \15x650 The value of & is now found by the formula k= V2pn+ (pn)?— pn Substituting the values for p and m gives k= V2 x .00769 X 15 + (.00769 X 15)2— .00769 & 15 = .379 From this value, j is found by the following formula: j=1-3k Substituting the value of & just found, j=1—-4X.379 =.874, or enorodiradtely. %. For any value of F;, F;, and n employed, the preceding formulas must be solved to obtain p, k, and 7 before the problem proper can be attacked. For example, the values of k and j may be taken as # and i, respectively. because these values are close to the values found from the values of F;, F;., and n, assumed. The resisting moment M may then be found by transposing in either of the following formulas: M M 2M leech Sint eae ad ans F Side cocaine Aja pid! ° jee = PPP ORS > ee wer » ae, 4 ar Tr) (ere tats % a Me CONCRETE DESIGN 293 The first of these will be found to be the more convenient to use in most cases, and it may be transposed to the fol- lowing: _ M=F,Ajd. As an example, design a girder on a 20-ft. span to carry a load of 700 lb. per ft. This load includes the weight of the girder. The total load is 20x 700=14,000 lb. The bend- ‘ . WI 14,000 x 20 ing moment is 3 = diay ae = = 420,000 in.-lb. Assume the effective depth of the girder— that is, the distance from the top to the center of the steel reinforcement, or d—to be 18 in. Substituting the correct values in the equation M=F;Ajd, 420,000 =16,000 x AX} X18, and A =1.667 sq. in. Since A=pbd, and since p is limited to .00769, 1.667 = .00769 Xb X18 and b=12.04, say 123, in. All that now remains is to decide how much concrete to put below the steel. This does not affect directly the =35,000 ft.-lb., or 35,000 X 12 strength of the beam. Its principal uses are to hold the steel in place and protect it from fire and rust. The Joint Com- mittee recommends a thickness of 2 in. for girders, 14 in. for beams, and 1 in. for slabs. Therefore, the girder just designed would be 123 in. broad and 20 in. in total depth, and it would have 1.667 sq. in. of steel 18 in. from the top. ExaMPLE.—Design a floor slab ona 10-ft. span tocarry a load of 250 lb. persq. ft. This load includes its own weight. SoLuTion.—Consider a section of the slab 12 in. wide. The total load is 250 10=2,500 lb. The maximum mo- Wi 2,500 10 ment is car Ce as ft.-lb., or 37,500 in.-lb. A= .00769 bd, but b=12 in., as a strip that wide is consid- ered. Therefore, A =.00769X12d=.09d. Substituting the values for M, A, Fs and j in the equation for the moment, 37,500 = 16,000 X .09 dx 4 X d; d?=29.76, and d=5.5. There- fore, A=.09X5.5=.495, say 4, sq. in. The slab must therefore be 64 in. thick and have 4 sq. in. of steel every foot, which must be placed 54 in. from the top. Of course, all the steel must not be put in one rod, but in several rods spaced at equal distances so that it will average 4 sq. in. per ft. 294 CONCRETE DESIGN These solutions give the most economical design; that is, when the allowable unit stress in the steel and the allowable unit stress in the concrete are realized under the proposed load. This condition is determined by the value used for p. However, other values of p are sometimes used, and in such cases the procedure is as follows: Assume a value of ». Find the value of k by the for- mula k= V2 pn+(pn)2—pn. Then find the value of j by the formula j=1—%3k. Next assume values for F, and F,. Find M from the conditions of the problem. Assume values for either } or d, and find the other by means of the formula F;=M-~+pjbd?, Also find the same dimension by © the formula F,=2 M+jkbd?, and use the largest value found by either of these equations. Sometimes the problem is thus: b, d, and M are given. . Assume F,, then find A by the formula M=F,Ajd, using ¢ for 7. Solve p=A-~+bhd for p, which should, by changing }b, if required, be kept less than the value of p that gives the most economical design mentioned above. Then to check, find k andj as on page 292 from the value of » obtained and find F, and F, accurately by the formulas at the foot of page 292. These values must not be excessive. To investigate a beam already built, proceed as follows: Measure the value of b, d, and A. Calculate the value of p as well as the moment of the loads on the beam, or that are to be put on the beam, including the weight of the beam itself. Assume a value for , and find the value of k by the formula k= V2 pn+(pn)?—pn. Find the value of j by the formula 7=1—4k. Find the stress in the steel by the for- mula F,=M-+ Ajd, and then the stress in the concrete by the formula F.=2M-+jkbd?, Neither of these values should exceed the safe allowable limit. Continuous Beams.—If W is the total uniform load on a beam and / is its length, then, for a simple beam, the moment is W/+8. In building construction, many beams and floor slabs are continuous, and in this case the external moment at the center of the span is decreased and there is produced a negative moment over each support. Sufficient steel CONCRETE DESIGN 295 should be placed over each support at the top of the beam to withstand this moment. This steel should extend far enough on each side of the support to reach the point where the bending moment changes sign. In many cases one- quarter of the span each way will be sufficient. This steel is often made up partly of rods bent up from the bottom of the beam and partly from extra rods inserted at the top. For both beams and slabs for interior spans of continuous beams the Joint Committee recommends that the bending Wl moment be taken as eT, both at the center of the span and over the support. In beams for end spans and the adjoining Wl support, the bending moment should be taken at to After the bending moment is found, the beam is designed in the manner already stated. Some engineers claim this reduction in bending moment Wl is unwarranted and use a? for all cases. No matter which method is followed, the beam should be reinforced over the support. Caution must be exercised in designing continuous T beams. At the support, the compression in the concrete is apt to be excessive, as it comes on the stem of the T. The Joint Committee allows a higher stress in the concrete here and recommends a value approaching 750 lb. It is often necessary to leave some steel at the bottom of T beams near the supports to assist in withstanding this compression. Beams Reinforced at Top and Bottom.—For beams rein- forced at the top and bottom, the preceding notation, with the following additional characters, is employed: A’=area of compressive steel at top of beam, in square inches; , p’ =ratio of area of compressive steel to bd ret F’ =compressive stress in steel, in pounds per square inch; d’ =distance from top of beam to top steel, in inches. 296 CONCRETE DESIGN To design such a beam, assume values for p, p’, da’, d, and ”, Then find k by the formula k= \? n (o+0°7) +n2(p+p'P—n(p+p’) After k is found, assume a value for ), and find F, by the formula 6 p'n d' a’\ | l3k~e+——— (e—-—) (2 pa] same 2% (5) (14) | Also, find F by the formula 1-—k eee, and F,’ by the formula @ tale d F,’=nF- ; The values of F,, Fs, and F,’ should all be within safe limits. FF’ will usually be low, which shows that the steel is not used economically. On account of this defect, double reinforced beams are seldom used except in plkebe where a ies Fic. 1 the size of the beam is limited by the conditions of the problem. As an example, design a girder, as shown in Fig. 1, to carry besides its own weight 450 Ib. per ft. The section of CONCRETE DESIGN 297 the girder is limited to that shown. The steel in the bottom should be kept up 2 in. to protect it from fire, so that the effective depth, or d, is only 18 in. In the first place, the 12. 20 beam itself weighs 150 LP Kya t= 250 lb. per ft. The total load to be carried is therefore 450 + 250 =700 Ib. per ft., or 700 X 30=21,000 Ib. in all. The span is here taken, for convenience, as the clear distance betwéen supports and not the distance from center to center of support, which wi is more correct. The maximum bending moment is — _ 21,000 X 30 8 First find A by the formula given for rectangular beams, =78,750 ft.-lb., or 78,750 X 12 =945,000 in.-Ib. M F,=—. Assume that j=} and that F;=16,000. Then, 945,000 AX$+18’ If the beam were reinforced at the bottom only, the allowable steel would be about .0075 x bd=.0075X12x18 =1.62 sq. in. The excess of steel is then 3.75—1.62=2.13 sq.in. It is for this reason that reinforcement must be put at the top of the beam; if it were not put there, the stress in the concrete at that place would be too great. The amount of steel required at the top is usually about two and one-quarter times the excess at the bottom, or, in the problem at hand, 2} 2.13=4.79, say 43, sq. in. Assume that this steel is placed 2 in. from the top. This completes the approximate design of the beam; that is, its size and the amount and location of the steel at the top and bottom have been assumed. It now remains to see whether or not the values assumed will be safe. First k must be found by the formula given, which is a’ k= NE n (0+) +n?(p+ p’)?—n(p+p’) 3.75 The values of p, p’, d, and d’ are: p=——-——-=.01736, 12x18 16,000 = or A=3.75 sq. in. 298 CONCRETE DESIGN 4.75 | Aga aappemtek 02199, d=18, and d’=2. Assuming that n=15 and substituting these values in the foriaula, 2 et i k= bees 15 (o1726-+.02199 =) + 15?(.01736 + .02199)? — 15(.01736 + .02199) = .380. 6 M 6 pn d’ d’ bd2| 3 k—k2+——— (k-—) (1-— [sear Z*(2-$) (1-3) | Substituting the values-in this equation, 6 X 945,000 ; 6 X .02199 « 15 —— —(,380 — 1- erent? Ts) ( | =651 lb. per sq. in., which, according to the stresses used in these examples, is about safe. The stress in the steel in tension is found by the formula, 1—k - | ae ral Substituting the correct values, Now, F,.= F,= 12 x 18? E X .3880 — .3802+ 1—.380 F,=15X 651 X 330 _ = 15,930 lb. per sa. in., which is also safe. The stress in the steel in. compression is found by the formula d’ k-— d F,'=nF-; k Substituting the correct values, F,/=15X 651 X 380— v's =6,913 Ib. 380 per sq. 1n. This value is low, but it cannot be helped. It is this fact that makes the double reinforced beam uneconomical. T Beams.—The Joint Committee makes the following * suggestions in regard to T beams: ‘In beam and slab construction, an effective bond should be provided at the junction of the beam and slab. When CONCRETE DESIGN 299 the principal slab reinforcement is parallel to the beam, transverse reinforcement should be used extending over the beam and well into the slab. ““Where adequate bond between slab and web of beam is provided, the slab may be considered as an integral part of the beam, but its effective width shall be determined by the following rules: “1. It shall not exceed one-fourth of the span length of the beam. “2. Its overhang width on either side of the web shall not exceed four times the thickness of the slab. “3. In the design of T beams acting as continuous beams, due consideration should be given to the compressive stresses at the support.” The notation used for T-beam formulas is the same as before, with the following exceptions: ‘b=width of flange, in inches; b’=width of stem or beam proper, in inches; t=thickness of slab, in inches. ; First assume values for F,;, F, and. Also, assume values for d, b’, andt. The value to be taken for 6 is determined partly by the rules just given. Assume an approximate value of A from the formula M=A(d—4t)F,. Solve the following 2 ndA + bt2 — 2nA+2 bt If kd is less than t, design the same as a rectangular beam; that is, again find k by the formula formula for kd: k= V2 pn+ (pn)? — pn where ae not El : bd b’d Then find 7 by the formula j=i— sk. and M by the formula M=F,Ajd, F jkbd? which must not exceed If kd is greater than t, proceed as follows: Find jd by 3kd-—2i ¢t the formula j@d=d—— 300 CONCRETE DESIGN Find F, by the formula a M * Ajd and find F, by the formula F Mka °” bt(kd —4t)jd These values of F, and F, must be less than the allowable values. These formulas neglect the compression in the stem. For approximate results, the formulas for rectangular beams may be used. ‘ As an example, design a beam to carry 5,184 Ib. per ft. on a span of 10 ft. The load given includes the weight of the beam, and the floor slab is 5 in, thick. The bending 5,184 X 10 X 10 : =64,800 ft.-lb., or 64,800X12 =777,600 in.-lb. Assume that F;=16,000 lb., F,.=650 Ib., and =15, and that d=16 in, and b!=16 in; b is governed by the preceding rules. It must not exceed one-fourth the span, or 30 in., and its overhang must be less than four times the thickness of the slab, which would limit its width to 16+2X4xX5=56in. Thereforebis takenat 30in. Solving for A in the formula, M=A (d—it)F,, 777,600=A (16-24) 16,000. Therefore, A=3.6 sq. in.; ee x OS ee 2X 15X3.6+2X30X5 3X6,073-2X5 5 . = 6073, and jd<16— Y wiht, oe re A id 2x6.073-5 3 ie __ 777,600 POS a5 141 =15,319 lb. per sq. in., which is safe, and _ 777,600 X 6.073 “30 X 5(6.073 — 24)14.1 which is also safe. Shear and Bond.—One method of failure of beams that is common is shown in Fig. 2. Such cracks are caused by shear or diagonal tension. They are preveuted by bend- ing up some of the main reinforcing rods to make truss rods and by the use of Y-shaped stirrups. The size and the moment is =625 lb. per sq. in., ie q CONCRETE DESIGN 301 method of placing these stirrups are still matters of discus- sion that depend much on the experience of the designer. One important thing to be re- membered is that they arecom- paratively short and that /7 there is danger of their pulling Fic. 2 out of the concrete. For these reasons they are frequently securely fastened to the slab reinforcement or bent over at the ends. Sometimes deformed bars are used, as they give a more secure grip on the concrete. When inclined stirrups are used, they should be fastened to the main reinforcing bars in sucha way that they will not slip. An approximate formula for shear in a rectangular beam reinforced at the bottom is = where v=unit shearing stress in pounds per square inch at any point, V =total vertical shear at that point in pounds, and the other terms have the same meaning as before. The Joint Committee recommends for a grade of concrete mentioned above a unit safe shear of 40 pounds. If V is greater than this, stirrups must be used. The same formula may be used for T beams with b’ insérted instead of band jd referring to T beams. Even with web reinforcement, v should never exceed 120 pounds. No absolute rules can be given for the size and placement of stirrups. In many instances ? in. square or ¥’ X 1” flats are used, but not in all cases. The spacing of stirrups is greater at the center of the span than at the supports. The Joint Committee recommends a maximum limit of spacing of three-fourths the depth of the beam. The spacing at the supports is often one-fifth or one-sixth of the depth of the beam. Great care is required in the design of stirrups of T beams to insure that the slab and the beam proper are securely tied together. An approximate formula for ordinary rectangular beams Vs with verticalstirrupsis P= 42° where P =stress in one stirrup, 5 7 s=spacing of stirrups, V=proportion ot shear supposed to be carried by reinforcement, usually %, and j and d have the values already given. 302 CONCRETE DESIGN The Joint Committee recommends that the bonding stress between plain reinforcing bars and concrete be assumed to be 80 lb. and in the case of drawn wire, to be 40 lb. for the same grade of concrete as specified in discussing beams. The ditference in stress in the tensile steel at two sections must be taken up by the bond to the concrete between these two sections and should be investigated. } COLUMNS Concentrically Loaded Columns.—There are two general methods of reinforcing concrete columns with steel. One Fic. 3 method is known as straight reinforcement and the other as hooped reinforcement. These two styles of reinforcement are illustrated in Fig.3. In (a) is shown straight reinforcement. This consists of steel rods that stand vertically in the con- crete. Sometimes, the rods are placed directly in the middle of the column, but as a rule they are arranged around the outside of the column about 2 in. from the surface. These steel rods are tied together by wire ties, asshown ata. The “we 4 PI CONCRETE DESIGN 303 distance between two ties should not exceed the width, or diameter of the column. If the ties are spaced too far apart, the column is apt to fail by the reinforcement bulging. In Fig. 3 (b) is shown a column reinforced with hooped reinforcement. This type of reinforcement consists of either a steel spiral or a separate steel hoop that is about 2 in. from the surface of the column, as shown at b. Some columns have both styles of reinforcement just mentioned. In the design, as given here, A; is the effective area of the concrete. The effect of fire is to injure the concrete for a depth of about 14 in. from the surface. Therefore, in investigating a column already built, first deduct 14 in. all the way around the column from the total area of the con- crete so as to get the effective area of the concrete. For the same reason, after a column is designed, add a coat 14 in. on all sides for fire protection. The reinforcement to protect it from fire should be embedded at least 2 in. in the concrete. In a hooped column, the effective area should not only be limited to 14 in. from the surface, but should further be limited to the concrete within the hooping. Outside of the hooping, of course, at least 2 in. of concrete must be placed. In height, columns should be less than fifteen times their least dimension. Straight Reinforcement.—Let A, represent the effective area of cross-section of concrete, in square imches; As, the area of cross-section of steel in square inches; E,, the modulus of elasticity of concrete; E,, the modulus of elasticity of steel; F,, the safe compressive stress per unit area of concrete; F,, the safe compressive stress per unit area of steel; m, the E ratio = and W, the total load on column. ec The design formulas are as follows: W =F(A,+nAs) F,=nF, Any values of F, and m as may be required may be used. The Joint Committee uses 450 lb. for F,; and 15 for m for - grade of concrete as specified in discussing beams. These values are used here for the sake of example. 304 CONCRETE DESIGN If a column is 12 in. square and has 3 sq. in. of steel, determine the safe load that it will carry. Deducting 13 in. from each surface, the column will be 81 sq.in. But3 sq. in. of this area is steel. Therefore, the effective area of the column is 81—3=78 sq. in. By the formula, W=450 (78+15 X 3) =55,350 Ib. The stress in the steel is there- fore 450 X 15 =6,750 Ib. per sq. in., which is safe. The use of steel in a column has two advantages. In the first place, the formulas do not take into account the length of the column; the longer a column is, the more it is apt to bend or bulge, and the steel helps materially to resist this tendency. Then again, the introduction of steel permits the column to be made much smaller in size, and this is often of great advantage. Having shown how to investigate a column, the method of designing one to carry a certain load will now be con- sidered. Thus, assume that it is desired to design a column to carry a load of 40 T. The percentage of reinforcement does not have to be a definite amount as is the case with beams, but may be any amount. Suppose that it is desired not to have the column too large; therefore, assume that the reinforcement will occupy 4% as much area as the concrete. Let A,=area of concrete. Then, A,=4% of A-=aA;. Substituting the correct values in the formula it will be found that 80,000 = 450(A,+NA,) =450(A,+15 X 3A.) =720 Ag. A,=111 sq. insand A,=y5A,=4.4+ sq. in. Therefore, the total area=A,+A,=116 sq. in. If the column is square, it will be 10.77 in. on a side; say 11 in., to allow for chamfered corners. When 14 in. of fireproofing is put on, the column will be 14 in. square and will contain a little over 4.4 sq. in. of steel. Empirical Rules for Straight Reinforcement.—One or two more or less empirical formulas are used in designing concrete columns with straight reinforcement. These formulas mostly originate from the building laws of various cities. The building laws of one large city, for instance, furnish good examples of such formulas. They stipulate that the safe allowable load shall be 500 Ib. per sq. in. of column section, counting both concrete and steel the same. If CONCRETE DESIGN 305 sufficient steel is inserted, this rule will of course be as safe as the formula already given. In a large building, the loads on the columns in the lower floors become very great, and as it is usually not desirable to increase the outside size of the column, the percentage of reinforcement is increased. A favorite style of reinforce- ment employed under such conditions is shown in Fig. 4: It consists of four angles riveted back to back in the center of the column to form a steel core. The area of this steel core can be increased if desired by using packing plates between the angles. The laws of this city then assume that the steel core takes all the vertical load and that the concrete prevents it from bending sidewise. The rule for designing such a column is, therefore, to allow a safe stress of 16,000 lb. per sa. in. on the steel and nothing on the concrete. Thus, suppose 160 T. is to be safely car- tied. Thisequals 160 x 2,000 =320,000 lb. The area required for the steel core, then, will be 320,000+16,000=20 sq. in. If four angles are to be used, each one will have to have an area of 20+4=5 sq. in. Angles 4 in. X4 in. x4 in. would be large enough. It is recommended that vertical rods be inserted in the concrete around the steel core to help stiffen it. The rule just given is of an empirical nature and is here presented to show the practice sometimes followed. Hooped Reinforcement.—Hooping of concrete columns increases the ultimate strength of the concrete contained inside the hooping, but has little effect below the elastic limit. Therefore, with hooping, a greater unit stress may be used, although the steel in the hooping itself does not carry the load applied. The amount of hooping should not be less than 1% of the volume of the concrete inclosed. The clear spacing between the bands should not exceed one- fourth the diameter of the inclosed column. Adequate means must be provided to hold the hooping in place while the concrete is being placed. The Joint Committee allows a unit working stress of 540 lb. on hooped concrete columns, 306 CONCRETE DESIGN and on hooped columns that contain in addition’ more than 1% and less than 4% of longitudinal reinforcement they allow a unit working stress of 650 lb. This is for the grade of concrete above specified. Some engineers consider these stresses rather high; nevertheless, in all cases the stress selected should be governed by the laws of the locality and ’ the experience of the designer. Eccentrically Loaded Columns.—It is difficult to find a column that is entirely concentrically loaded. If, in a build- ing, the live load is transferred from one girder to another, the girders being carried by the same column, their deflection will put a twist in the column itself. Also, the outside columns of buildings are often eccentrically loaded.. In the lower floors of buildings the eccentric load due to unequal distribution of load, in panels, may usually be neglected because of the large concentric load on the column, but in the top floors of a building the matter may at least deserve attention. If the load is eccentric, the following method will usually give safe results: First, assume a section and find the stress in the concrete and steel due to bending as in a beam with double reinforce- ment. Next,-find the stress in the concrete and steel due to direct compression and add the two algebraically. The sums obtained should not exceed the allowable stress for columns. Sometimes it is found advisable to put more steel in the tension side than is used in the other side. As this method is approximate, low unit stresses should be used. ARCHES In reinforced-concrete arches, the arch ring is nearly always thinner at the crown than near the haunches. The arch in reinforced -concrete work is often either true parabolic or the curve is made up of a series of circular arcs approach- ing the shape of a parabola. The reinforcement for arches is ‘usually placed in two layers—one near the intrados and the other near the extrados—and these two layers of reinforcement are usually laced together with lighter rods In constructing bridges of reinforced concrete, it is consid- ered advisable to lay all the concrete at once, but if this is CONCRETE DESIGN 307 impossible, the bridge may be constructed in parallel sections running lengthwise of the arch. By following this method of construction, the arch is not materially weakened, for each ring may be considered as a complete unit of the arch. The manufacturers of Kahn bars have suggested an approxi- mate method of reinforced-concrete arch design. This method is based on an article by F. F:! Weld, C. E., published in the Engineering Record. It consists in using an empirical formula obtained from a study of many existing arches and original designs analyzed by more elaborate methods. The first step in the design is to determine the rise of the arch. This should be at least one-tenth of the span. _The curve that the arch takes, especially where uniform loads are expected, is often a parabola. This parabolic curve is usually followed by the center line of the arch ring, and not by the curve of the intrados. This curve may be drawn by plotting a sufficient number of points determined by the following formula: PB, es e ak ( = | in which Y is the rise of parabola, in feet, at any point under consideration; H, the rise, in feet, at the center of the arch; X, the horizontal distance, in feet, from vertical center line of arch to point under consideration; and S, the span of the arch, in feet. As an example, lay out the parabolic curve for the center line of an arch where the span is 88 ft. First, the rise must be determined; this is at least one- tenth of the span, which is 8.8, or practically 9, ft. Having the rise and the span, proceed to lay out the curve shown in Fig. 10 as follows: First lay off to a convenient scale the line ab equal to the span. At the center of ab, orc, erecta perpendicular, and on it measure cd equal to the rise H. Then, the points a, d, and b lie on the required curve. To obtain other points, proceed as follows: Divide the span into any number of convenient parts, say in this case, eight, because eight is an even number, which makes one division point at c. Then, each division is 11 ft. long. Now, the first division immediately to the right of c is e. 308 CONCRETE DESIGN From: ¢ erect a perpendicular. Then, returning to the formula, it is desired to find the vertical distance to the Fic. 10 parabolic curve. This distance is denoted by Y. The fol- — lowing values are known: H=9, X=11, and S=88. Sub- stituting these. values in the formula, 2X47\-* Y=9x]1- 7") | = 8.4375 ft. Lay off ef equal to 8.4375 ft. Then f is a point on the curve. Suppose it is desired to locate the curve at the first division point from a, namely, g. Through g draw a perpendicular. Here, H=9, X =33, and S=88. Therefore, 2 Y=9xX E 7) | =3.9375 ft. 88 From g, there is plotted upwards to scale 3.9375 ft. to h, which is a point on the curve. Other points may be obtained in the same manner and the parabolic curve drawn through them. * ; Instead of using the formula to determine the location of points along the parabola, as just shown, it is customary Svan to be divided into 10 eguatl Parks . H ‘ t ' | { ' ' ‘ ' ' o++----7 S\ z : C4) i 4 Fic. 11 to divide an arch into ten equal horizontal parts and then use the values given in Fig. 11. These values are derived from the formula on page 307, and enable a parabola to be plotted with ease when the span is divided into ten equal parts. The rise at each one of these parts is given in terms CONCRETE DESIGN _ 309 of the total rise. As will be observed, these values are independent of the span. As an example, consider an arch having a span of 70 ft. and arise of 8 ft. In this case, H=8 and the height of the curve at 70+10=7 ft. from each end is .36X8=2.88 ft. At 14 ft. from each end, the height of the curve above the spring line is .64< 8=5.12 ft., and so on, until the necessary number of points on the curve are located. The curve may then be drawn, passing through these points. Having determined the rise to be given to the arch, the next step is to find the thickness of the arch ring at the crown. This may be found by the formula proposed by F. F. Weld, C. E., which is 2 follows: Dense 4 10 200 400’ in which D is the crown thickness, in inches; S, the span of the arch, in feet; L, the live load per square foot; and F, the dead load at crown per square foot, exclusive of the weight of the arch itself. Thus, for example, take an arch whose span is 64 ft., whose live load is 100 Ib. per sq. ft., and whose dead load is 200 Ib. per sq. ft., and determine its thickness at the crown. In this case, S=64, L=100, and F=200. Then, 64 100 200 D bere 15.4 in. If there is no live load, the formula may still be used. Thus, find the thickness of an arch at the crown when the span is 40 ft. and the dead load at the crown is 150 lb. per sq. ft. Here, S=40, L=0, and F=150. Therefore, 40 150 . D=~ = —=10. in. +55 et 0.6996, say 11, in The arch ring is made thinner at the crown than else- where. The custom is to increase gradually the thickness of the arch ring from the crown to the abutments. The thick- ness of the arch ring directly above points on the spring line, one-quarter of the span from the abutments, is made from one and one-fourth to one and one-half times the thickness at the crown. From these points to the abutments the arch- 310 CONCRETE DESIGN ring thickness usually increases more rapidly, and while no definite proportions can be laid down, it is usually at least twice as thick at the skewbacks as at the crown. One of the points yet to be considered is the amount of steel reinforcement to be used. As was said, this rein- forcement usually is placed in two layers, one layer near the intrados and the other near the extrados. If the arch carried only a dead load and the conditions were absolutely uniform, only one layer of reinforcement would be neces- sary; but, in actual practice, as even the changes of temper- ature cause large variations in stress, two layers of rein- forcement are used unless a very careful analysis of stresses has been made to prove that they are not needed. The. amount of steel in each layer is kept uniform throughout its length. The cross-sectional area ot steel in each layer is equal to 745 of 1% of the area of the arch-ring section at the crown. Thus, suppose that the thickness of an arch at the crown is 24 in. For a width of 1 ft., the area of the arch-ring section is 24*12=288 sq. in. The area of the steel in the top or bottom layer per foot of arch width is therefore 288 X 1.152 sq. in. The area of a $-in. round bar is .6013 sq. in. Therefore, one $-in. round bar placed near the extrados and one }-in. round bar placed near the intrados, every 6 in. in width along the bridge, will be found sufficient. The distance from the center of the bars to the surface of the intrados and extrados, that is, the depth to which the bars are to be embedded in the concrete, is another question that must be decided. The nearer the reinforce- ment is to the surface, the more efficient it will be. On the other hand, the reinforcement must be embedded deep enough, so that it will not tear loose and so that it will be protected from fire and rust. As a general rule, the distance from the center of the steel reinforcement to the surface of the arch ring should be from 2 to 8 in. The two layers of reinforcement are laced together by light steel rods that are run from one layer to the other. No uniform method is followed in designing these shear members, as they are called, and the amount of material used also varies greatly. FOUNDATIONS | 311 As an example of a complete problem, the following case is suggested: Design a reinforced-concrete arch for a 65-ft. span. This arch is to carry a live load of 200 lb. per sq. ft. and a dead load of 300 lb. per sq. ft. at the crown. First, the rise of the arch must be determined. This may be taken as one-tenth the span, or 6.5 ft. The curve of the arch may now be laid out. If the curve to be followed is a parabola, the method of constructing it is given on page 307. This curve may be used either as the center line or as the intrados of the arch, preferably the former. The thickness of the arch ring at the crown may now be determined by the formula on page 309. In this case, S=65, L=200, and F=300. Therefore, — 65 200 300 D rer rr 16.3123 in. Calling this thickness 18 in., the thickness of the arch ring at the quarter points may be taken as 14 X 18=27 in., and its thickness at the haunches may be taken as 2K 18 =36 in. The amount of steel reinforcement required for each layer must now be determined. For each foot of width of the arch, this will be 18X12 yo0 X 74 =.864 sq. in. A 3-in. round rod has an area of .4418 sq. in.; therefore, one }-in. rod every 6 in. near the extrados, and one 1}-in. rod every 6 in. near the intrados will be sufficient. These rods should be embedded 2 or 3 in. in the concrete. The two layers of reinforcement should be either securely tied together or bonded into the concrete with shear or diagonal members. FOUNDATIONS BEARING VALUE OF FOUNDATION SOILS There is some difference of opinion regarding the safe _ bearing value of foundation soils, due probably to the diffi- culty of arriving at any experimental results that will have a general application. Conservative engineering practice, however, dictates that the greatest unit pressure on the PM ate a 5 i =} - FOUNDATIONS i4- : it 4 be aad 4 TT, : 4? a 0! 2p! ; sok he 2 275 ee | : ogee ates o o9 95 29% 994% 054 5 bod SC BFS py? 9 52 29% H¥,5 an hee ai Aah ob eked pate oe | ‘Con. Col 4-1" Rods. re > > co 5 a J ha) By “5 + ie eh ~~ eS. 14 Anchor Bolts. See vo a 4 a4 4% ay elo Je + 0 ett +7 xs ie. 4 | +4++4-+4 20% Basement Floor L 312 Ways ee ea - 10°06" Square— — "Bars $"C.10C Both Fic. 1 rp pS eit coe FOUNDATIONS 313 different foundation soils shall not exceed the values given in the accompanying table The observance of the revised building laws of the several cities is considered good engineering practice, for they are usually the results of careful investigations and records of long experience. The following, taken from the New York Building Laws, is interesting and gives bearing values that are well within the safe limits: SAFE BEARING VALUES OF DIFFERENT FOUNDATION SOILS Tons per Material Square Foot Granite rock ies go Pea a 30 Limestone, compact 25 Sandstone, compact pede. 20 Shale fecciandon: 6: or soft friable rock. . 8 to 10 Gravel and sand, compact. . ‘| 6 to 10 Gravel, dry and coarse, packed ‘and confined . 6 Gravel and sand, mixed with dry clay. 4to6 Clay, absolutely ‘dry and in thick 4 Clay, moderately dry and in thick bedan. : 3 Clay, soft (similar to Chicago clay).. .| 1 tol} Sand, compact, well-cemented, and confined . | 4 Sand. clean and dry, in natural beds and confined 2 Earth, solid, dry, and in natural beds 202s 4 Where no test of the sustaining power of the soil is made, different soils, excluding mud, at the bottom of the footings shall be deemed to sustain safely the following loads to the superficial foot: Soft clay, 1 T. per sq. ft. Ordinary clay and sand together, in layers, wet and springy, 2 T. per sq. ft. Loam. clay, or fine sand, firm and dry, 3 T. per sq. ft. Very firm, coarse sand, stiff gravel, or hard clay, 4 T. per sq. ft., or as otherwise determined by the Commissioner of Buildings having jurisdiction. 314 FOUNDATIONS Where a test is made of the sustaining power of the soil, — the Commissioner of Buildings shall be notified so that he ° may be present in person or by representative. The record of the test shall be filed in the Department of Buildings. SPREAD FOOTINGS DESIGN AND CONSTRUCTION - The term spread footings is applied to either wall or column footings that have a considerable projection beyond the upper tier of the footing, wall, or column base, as the case may be. The usual type of spread footing for the support of a column is illustrated in Fig. 1. This footing was designed to be used with a structural-steel column core, and is one that would ordinarily be used for a ten- or twelve-story building that is to be erected on unstable soil. : Placing Reinforcement in Column Footings.—The rein- forcing rods, or bars, are placed from 2 to 4 in. from the bottom of the footing, and are arranged so as to cross each other at right angles. No attempt is made to interlace the bars or rods. It is good practice, however, to wire them, together, for by so doing, any danger of misplacing the bars is avoided. Several tiers of bars, or rods, are used in heavy footings, although spread footings that support light loads ‘are sometimes reinforced with expanded metal or woven- wire fabric. In designing column footings in reinforced concrete, some steel reinforcement is often placed in the upper part of the footing directly under the base of the column. This rein- forcement acts as a mattress to distribute the concentrated - load from the column and also as a bond to tie the concrete together. Two other methods of arranging the reinforcing rods in concrete column footings are shown in Fig. 2. In (a), the rods and bars are crossed at right angles; every other bar is made short so as to save metal. FOUNDATIONS 315 In the method of placing the steel reinforcement shown in Figs. 1 and 2 (a), it will be observed that the corners of the footings are subjected to great moment. order to strengthen the corners of the footing, the reinforcing rods are frequently ar- ranged as shown in Fig. 2 (0). The steel reinforce- ment of column _ foot- ings is never painted, even if the footings are to be placed in damp situations. Coating the bars will partly destroy the bond that it is neces- sary to maintain be- tween the concrete and steel; besides, the concrete is sufficient protection for the steel ‘against any serious corrosion. In all in- stances, however, the steel bars should be cut off enough to allow the ends to be entirely protected. Spread Footings for Optside Columns.—In- stead of a continuous footing, ztsolated spread footings are frequently used in outside, or wall, columns. Therefore, in m = BL Ue aeay poser 44 + - | 11 Ht Reinforcing Rods and Bars I t va 1% +4 ba oe ae Et es + rt—-t- 1 Reinforcing 4 Mods and Bars * AA ARIE Si 17% A, AS Ee ee TALS xt HATS pay WG-4 RK ~ (b) Fic. 2 Such footings are illustrated in Fig.3. The position that the footings occupy on the building plan is shown, the wall footing being at a and the corner footing at b. 316 FOUNDATIONS FORMULAS FOR THE DESIGN OF FOOTINGS The theoretical design of a spread reinforced-concrete footing consists first in determining the total load on the column to be supported by the footing, and then finding the required area of the bottom reinforced-concrete footing or layer of concrete by dividing the load by the assumed allowable bearing value of the soil. The next thing to find is the area of the base of the column where it bears on the upper tier, or layer, of concrete, because the size of this por- tion of the footing is fixed by the size of the column base. Aftcr the areas of the bottom and top tiers, or layers, of con- { ! rt = al b-50 RSRP ITA, FS ag RSF ee Fic. 3 crete have been ascertained, the projection of the bottom tier beyond the upper is known, and the bending-moment stress on the lower tier of concrete can be calculated. Sufficient steel rods may then be introduced, and the footing made of a depth that will resist this bending moment. The usual formulas for bending moments and the resist- ance of reinforced-concrete rectangular sections may be applied in determining the strength of reinforced-concrete spread footings. However, in office practice, it is desirable to use direct formulas for finding the area of steel reinforcement required and for determining the unit compression created in the upper portion of the concrete footing. FOUNDATIONS 317 The formula for finding the area of steel reinforcement _ required is expressed as follows: Wx 27,0002’ in which A is the sectional area of steel reinforcement, in _ square inches, required for each linear foot of spread footings along one side; W, the total load, in pounds, on a portion of projection of footing 1 ft. in width; x, the projection of footing, in inches; and ¢, the distance, in inches, from center of action of steel reinforcement to top surface of concrete footing. oe =] i +=20° ==. —fosition f Canter Y oY Re Reinforcerrent ue | | | | Pressure on So $000 pe goers a ge saa Ad Se Fic. 4 —_——_— The following formula is used to determine the compres- sion created on the concrete due to bending stress: Ce. 4.5922 The value C is the compression, in pounds per square inch of section, and the other values are the same as in the first formula. In order to explain the application of the preceding formulas, assume that the reinforced-concrete footing of a column is required to sustain 900,000 lb., and that, as the soil will safely support 4,000 lb. per sq. ft. of bearing area, the footing will be 900,000+ 4,000 =225 sq. ft. To obtain this area, the footing will have to be 15 ft. square, and the 318 FOUNDATIONS design shown in Fig. 4 may be assumed in applying the formula. In this figure, the projection of the footing, or the dis- tance x, is 60 in., and the dimension #, or the distance from the center of action of the steel reinforcement to the top of the footing, is 20'in. The pressure on a projection of the footing 1 ft. in width is‘equal to the unit pressure on the soil, or, 4,000 X 5 =20,000 lb., which is the value of W in the formula. These values may be substituted in the formula for determining the amount of the steel reinforcement, so that __ 20,000 x 60 27,000 X 20 This area of steel is to be included in each linear foot of the footing course; therefore, the reinforcement may consist of 1-in. square twisted bars spaced practically every 6 in. both ways, or other bars at a spacing to give this sectional area may be used. The amount of the steel reinforcement having thus been determined, it remains to find out whether or not the con- crete in the footing course is overstressed, and the second formula may be applied as follows: ; 20,000 x 60 C= 653 Ib. 4.59 X 20 X 20 This result, which is the maximum compression, in pounds per square inch, on the concrete section, is somewhat high. If good concrete is used, the footing as reinforced and designed may be considered safe, though, in fact, the thick- ness of the concrete footing might be increased several inches. = 2.2 sq. in. CANTILEVER FOUNDATIONS In reinforced-concrete construction, as well as in other types of construction, it is frequently necessary to place a new building close against the walls of an adjoining building. In many instances the wall of the adjoining property rests entirely on its own lot and is not a party wall built half on each side of the party line; also, the adjoining building may be of inferior construction or may be occupied by tenants OO EE 2 Ee ee ee eee ames a FOUNDATIONS 319 engaged in manufacture. Under such conditions it is unde- sirable to tear out the wall and build a party wall. With buildings of ordinary height and load, provided the basement floor of the new building does not extend below that of the old, few difficulties are encountered in the design of the foundations for the new structure; but if the new building is to be many stories in height and requires exten- sive foundations along the wall lines, the problem of the design of the reinforced-concrete foundations becomes more complicated, because it is desirable to proportion the footings so that the center of action of the loads will coincide with the center of action from the pressure of the soil beneath. In order to accomplish this desired result in a steel structure, a cantilever-girder system of foundation construction would be employed, and a similar system can be constructed in reinforced concrete. In Fig. 1 is shown the detail drawings of a reinforced- concrete cantilever-foundation construction for a six-story building, the floors of which are designed for light manu- facturing purposes. In view (a) is shown a diagrammatic cross-section of the building, which illustrates the conditions of loading and the spans of the cantilever and other girders. The live load to be supported by the floor construction and the cantilever girder is 220 lb. per sq. ft., and the soil beneath the footings is capable of supporting safely 6,000 lb. per sq. ft. The details of the construction and the reinforcement are shown in view (b). The footing is reinforced against failure from transverse stress by bars a, placed near the bottom of the footing, and further by a mattress of rods or bars placed directly beneath the bearing of the foundation wall column, as at b. The column, or wall pier, ¢ is rein- forced with vertical reinforcing bars, which are tied at close intervals with wire or loop ties d. Particular attention is called to the manner in which the outside rods of the founda- tion pier or column run straight through and up into the column above, being continued as the inside rods of the upper tiers. The outside rods of the first-floor wall column are bent so as to pass obliquely through the cantilever bracket of the foundation pier or column and the flare at the FOUNDATIONS 320 70 TO deg mats: ee Br aie va lafats twanshauir eas Wee ewe ms FasL “SK | 1 ye aU thir Pies Seee ew ND sel jo : 321 FOUNDA TIONS 4 —_-— + -— — — 40 — 4 : | Pass Fa=s ae 7 9-7 EY code | enter eke 1049,9 @ seg ele x | | u ft she yt09 8281082,018 8109 M1 bs F SS ed . = ay JO MAY 207 ye ye eee ee saemepgase: me Fe beinae ecane bap Nake i" 1 Ay, te e109 4 bs hp ole " . ; 4 ee al we “Pe tS evayuar, 21) seu: seer, f +. ‘a | k "De. rab Lh 4 a = 1 Hes s 1 ait —— 200 acts t-r anh Lt if | att itt a! 2D Oe oe = So Te ihe . pate no Soa Soe ee tS Baer sug my bs f/-06 3 surg 1 tS, 1-6 om SPECIFICATIONS 367 \ The amount of carpenter work on the forms is variable, depending on the experience of the carpenters and the intricacy of the work. USually, a carpenter can erect 20 lin. ft. of column form in a day, or 40 sq. ft. of floor and girder form. These figures are for smooth, finished work, and not for rough work. SPECIFICATIONS CONDENSED SPECIFICATIONS FOR REINFORCED- CONCRETE WORK The following specification is the briefest form that can be used in specifying reinforced-concrete construction. It briefly states the requirements of the architect regarding the submission of the construction for approval, the char- acter of the concrete and the steel reinforcement, and the floor load upon which the calculation for the design of the floor system is based. REINFORCED-CONCRETE CONSTRUCTION General.—The reinforced-concrete construction shall be of an approved and successful type, and the contractor shall submit for the architect’s approval framing plans, and details of construction, together with schedules showing the amount of steel reinforcement in all the beams, girders, and columns, The contractor is to assume all responsibility for the safety ‘and protection of the work during construction, and shall deliver the same in a complete and finished condition in compliance with the specifications and the accompanying plans. Concrete.—The concrete for beams, girders, and slabs shall be proportioned of 1 part Portland cement, 24 parts sand, 5 parts broken stone or gravel. The concrete for columns shall be a 1-2-4 mixture. Cement.—The cement shall conform to the requirements of the standard specifications for cement adopted by the American Society for Testing Materials, on November 14, 1904. 368 SPECIFICATIONS Aggregates.—The sand shall be clean, and not contain over 3% of loam. Broken stone and gravel shall be hard and close-grained, and free from dust and dirt; they shall be of such size as to pass through a ring 1 in. in diameter. Reinforcing Steel.—The steel for the reinforcement shall be manufactured by the open-hearth process. This steel should have an ultimate tensile strength of from 60,000 to 70,000 Ib. per sq. in. and an elastic limit of at least half that amount, with an elongation of at least 20%. A bar shall bend cold through an angle of 180° and close down on itself without showing signs of fracture. High-carbon steel or ¥ steel with an elastic limit greater than 45,000 Ib. per sq. in. shall not be used. The beam and girder reinforcement shall consist of square- twisted or approved type of deformed bar, while the slab reinforcement may be of square-twisted bars, deformed bars, or of an approved form of expanded metal or woven or electrically welded wire fabric. The column rods may be of plain round or square-twisted bars. The girders and beams must have the rods so bent and arranged as to provide amply for the bending moments throughout their length and also to take care of the negative bending moments near the bearings and supports. Sufficient stirrups must be provided tals een near the bearings or throughout the length of the beams and ~ girders to resist the horizontal, oblique shearing, and tensile stresses. Floor and Test Loads.—The floors and columns throughout shall be designed to sustain a live floor load of 150 Ib. per ~ sq. ft. The finished floor systems shall be tested in two © places, to be designated. The test load shall be equal to © one and one-half times the amount of the live floor load. The test loads shall be so placed as to fully load the girders © and beams of one bay. MEMORANDA MEMORANDA ~~ MEMORANDA MEMORANDA MEMORANDA MEMORANDA MEMORANDA MEMORANDA Promotion Advancement in Salary -@ Business Suceess = Secured Through the Concrete Engineering, Complete Architectural, Architec- tural Drawing and Designing, Building Contractors’, and Structural Engineering COURSES OF INSTRUCTION OF THE International Correspondence Schools International Textbook * Company, Proprietors SCRANTON, PA., U.S.A. & ~) oo . SEE FOLLOWING PAGES Superintendent of Construction of Million-Dollar Concrete Building There is now being built in San Bernardino, Cal., a great precooling plant for citrus fruits that will cost one million dollars. The superintendent of construction in charge of this plant, which is built of reinforced con- crete, is Wm. L. Snook, 1643 W. Thitty-Fifth Street, Los Angeles, Cal., an I. C. S. trained man, Mr. Snook states: “For the last 3 years I have been superintendent of con- struction of reinforced-concrete buildings. At the present time I am superintending the construction of the largest ice and precooling plant of its kind in the country.”’ Many Opportunities for Concrete Engineers WANTED — COMPETENT, EXPERIENCED reinforced concrete engineer and designer; only firct-class man need apply; good salary and steady position with large responsible firm, Ad- dress immediately Builders’ Material Supply Co /> : Kansas City, Mo. WANTED—A ca Who can gonerete. torms. fons i : [) . Apply ITT CO.; ‘Macedon, Address, with references, » Apected, No. 3871, care Engi- emonsl Se Field Engineer in United States Service When I enrolled I was doing odd jobs wherever I could get work to do. Through study of my Course I have filled important positions in the United States Reclamation Service, Inspector in the General Land Office, and other United States Government posi- tions, ranging in salary from $75 to $200 a month. I am now Field Engineer with the United States Reclamation Service in charge of the location and construction for the irrigation of about 25,000 acres of land on the Payette-Boise Project. I am enrolled for the Concrete Engineering Course. The Schools have done wonders for me and I highly recommend them to any one who wishes to learn and advance and be worth more to their employers. W. W. PEFLEy, 215 N. 14th St., Boise; Idaho PASSED CIVIL SERVICE EXAMINATION H. W Tuorne, 1379 E. Fifty-Third St., Los Angeles, Cal., enrolled for the Architectural Course while employed as a carpenter, earning $3.50 a day. After studying, he gradually advanced to a high class of work and was able to do his own calculating. Later he took the civil service examination for deputy building inspector and received the highest average ever given in Los Angeles. He was able to answer the technical questions in the examination by means of the knowledge acquired from his Course. HIGH-SCHOOL STUDENT BECOMES DRAFTSMAN Oscar GEORGE KNEcHT, 1245 E. 5th St., Kansas City, Mo., enrolled for the Architectural Drawing Course in December, 1905, when 21 years of age, while attending high school and working as a baker’s helper in the afternoons and evenings. He was then earning $6 a week. After completing a small art of the Course he secured a position with an architect y showing some of his ei np and was steadily advanced until he received $15 a week. e was then offered a position as architectural draftsman with Clark-Williams Company, contractors and builders, at a salary of $20 a week, which ition he now holds. Ina letter dated December 6, 1907, r. Knecht says: ‘‘My opinion of your method of instruc- tion is that it is a very good one. I prefer it to a college course because, if I were under a personal instructor I would have him sg solve every difficult problem and would not be studying them out for myself.” BECAME DESIGNER AND BUILDER L. W. Eppy, 1801 Sunnyside Ave., Fruitvale, Cal., had been out of the United States Navy _but a short time, and was working as ac nter’s helper at $2 a day, when he enrolled in the I. C. S$. Building Contractors’ Course. Mr. Eddy is now a designer and builder, earning $6 a day. He says this was through the help of the Course, especially in concrete and stair-building work. INCOME INCREASED $500 A YEAR Cuar_Les E. WERKING, Hagerstown, Ind., a foreman car- nter, enrolled for the I. C. S. Complete Architectural ourse. He says, “I never entered into anything I enjoyed more and gained so much.’’ Mr. Werking is now an archi- tect, with income increased from $750 a year to $1,250 a year. FROM $6 A WEEK TO $25 A WEEE Harry Crossy, Hyde Park, Cincinnati, Ohio, was earn- ing but $6 a week when he enrolled for the Complete Archi- tectural Course. It was hard for him to persevere because of his circumstances. But he has studied until now he is an architectural draftsman earning $25 a week. 5 Now Earns $300 a Month M. P. Kellogg, of San Diego, Cal., enrolled for and studied in the I. C. S. Complete Archi- tectural Course. For 16 years he had been a carpenter and contractor. After studying his Course he began the practice of architec- ture. Mr. Kellogg has won several prizes, over many competitors, for the excellence of his designs. In a letter to us regarding his progress Mr. Kellogg says: ‘‘My success is due to the instruction received from the Inter- national Correspondence Schools. I am well satisfied with your system of teaching; in fact, I think it as good as personal instruction. I consider my Scholarship the best investment I ever made—it has been worth several times the cost to me. My Bound Volumes have been especially helpful. I shall be glad to answer any letters regarding the Schools and my Course with them. - My business now nets me about $300 a month.” MACHINIST TO STRUCTURAL DESIGNER Epmunp B. La Sate, Batavia., Ill, was employed as a machinist when he enrolled in the Structural Engineering Course of the I. C.S. He was ambitious, of course, to become a structural draftsman and designer, but the numerous books he bought were found to be a waste of money. After studying the Course, Mr. La Salle obtained work as a draftsman. Recently, he has accepted a position in Chicago as structural designer, at a salary of $130 a month. He designs standpipes and steel tanks; also towers for water-supply stations. HIS COURSE BROUGHT RAPID INCREASE ErNEstT N. WoopBECK, 133 Crawford Ave., Detroit, Mich., was learning the business of carpenter for reinforced concrete work when he enrolled with the I. C. S. for a Concrete Engi- neering Course. His studies made it possible for him to become layerout of work from building plans. He had only a seventh grade education when he enrolled, but in eighteen months he increased his salary nearly 40 per cent. NOW OWNS A PROSPEROUS BUSINESS Won. F. GLeason, 709 Crawford Ave., Augusta, Ga., was earning $2.50 a day as a carpenter when he enrolled for the Complete Architectural Course with the I.C.S. This enabled him to become superintendent of construction for a concrete building block and tile company. He has since established @ prosperous business of his own as a member of the Skinner & Gleason Contracting Company, builders, making a specialty ’ of concrete construction and brick work. His income is at least $2,000 a year. TEMPORARY EMPLOYMENT MADE PERMANENT Harry L. ACKERLEY, 3 Richard St., West Lynn, Mass., says: ‘‘I first enrolled for a Course in Architecture. After taking the preliminary studies I applied for a position as draftsman and was given ‘temporary’ employment. I remained with the concern four years. I then enrolled for an Electrical Engineering Course, which has been invaluable to me. I am now employed by the General Electric Com- pany and my salary has been increased 350 per cent.” SALARY INCREASED 400 PER CENT. Mitton S. GRAWL, 1803 Erie Ave., Philadelphia, Pa., at the time of enrolling in the Architectural Drawing Course, was working in a meat store. The Course started him on the road to success. Today he is chief draftsman for a steel company in Philadelphia, with 400 per cent. increase in income over his salary as clerk. 7 Won Prizes in Five Contests The fact that my house plans have won prizes in five different contests argues well for the Course I took with the International Correspondence Schools. My early education was derived from the public schools. At the age of 15 I built a rowboat so well that I was advised to take up carpentering. I did so, serving my term with Henry Lorenz, of Matamoras, Pa., and working with the builders around Port Jervis. Then I decided to go into the building con- tracting business for myself, and knowing that a knowledge of architecture and drafting was necessary, I enrolled with the I. C. S., studying evenings, rainy days, and odd times until I earned my Diploma. I now do con- siderable planning and drafting, and I am satisfied that I will soon be able to give up all other work. The Course was a great help to mein many ways. I say that no mechanic has any chance to advance these days unless he takes up a good course of study along the line of his trade, such as the International Correspondence Schools give. C. A. WAGNER, Port Jervis, N. Y. } NOW OWNS A CONCRETE FACTORY Not being able to afford a college education, Cuas. F. CuLP, New Rockford, N. Dak., enrolled with the I. C. S. for the Complete Architectural Course, paying for it with the first money he earned after becoming of age. At the time, his wages as a carpenter were only $1.25 a day. He is now a presperces contractor and builder, being also the owner of a actory for the making of cement products. He attributes his success very largely to his work with the I. C. S. CARPENTER TO $10-A-DAY DRAFTSMAN ELMER B. Cutts, Hinckley, Ill., was working for his father as enter, earning 174 cents an hour at hard labor, when he took up a course of study in the I. C. S. The knowledge gained from the Course as placed him in the position of chief draftsman for the Robert Cutts Construction Company. He prepares plans for various dwellings, hotels, churches, and public buildings, earning $10 a day. NOW SUPERINTENDENT FRANK FREE, Greenfield, Ohio, was a common éarpenter employed some eight months a year at $2.70 a day, when he enrolled for the Complete Architectural Course, and after- ward for the Concrete Engineering Course. He is now super- intendent of construction for Samuel Hannaford & Sons, Cincinnati, Ohio, engaged on reinforced concrete and other construction. His aslary is $1,500 a year. NOW AN ARCHITECT Epwarp THAL, 702 Ohio Building, Toledo, Ohio, was earn- ing $18 a week as a paper hanger and painter when he enrolled with the Schools for the Complete Architectural Course. He is now an architect and engineer, making a specialty of rein- forced concrete, with an income several hundred per cent. larger than when he enrolled. NOW IS STRUCTURAL DRAFTSMAN C. B. GitBertT, care Philadelphia Engineering Compeanss Philadelphia, Pa., prior to becoming a student in the I. C. S. Structural Engineering Course was general utility man in a shoe factory, with little or no chance to rise. Before he had completed his I. C. S. Course he secured a position as structural draftsman with the Niles-Bement-Pond Company. His prospects are bright and his income is greater. CARPENTER TO CONTRACTOR FRANK J. BERDEL, 333 Columbus Ave., Canton, Ohio, writes: ‘‘I enrolled for the Building Contractors’ Course three years ago while employed as a carpenter, receiving $2.50 a day for 10 hours’ work. After studying evenings for one year I started contracting. Though but 25 years old my income is $12 a day.” 9 Now Reinforcement Contractor I am a pretty busy man these days, but I must send you a little message of appreciation concerning your Concrete Engineering Course. Two years ago I was a machinist’s helper in a railroad shop, earning 23 cents an hour. But I was ambitious and when your repre- sentative approached me I soon saw that I would make the mistake of my life if I did not sign up for a Course. I found your Concrete Engineering Course a veritable gold mine. I immediately secured work on a reinforced concrete building. Before this was completed I was tendered the position of steel foreman on a large reinforced concrete building in Portland, at just double my former salary. I am now a reinforcement contractor, bending, fabricating and placing steel reinforcement in all classes of reinforced concrete construc- tion. I have now four large contracts under way. Iam thankful for the fact that a repre- sentative of the I. C. S. yanked me out of my hole and pointed out a way for me to stay out. C. G. WiILForD, Jr., 147 Front St., Portland, Ore. 10 BETTERED HIS POSITION AND SALARY Cuas. A. CARPENTER, 16 West 3d St., Fulton, N. Y., was _a steam fitter, earning $65 a month, when he enrolled with the Schools, at the age of 5. for a Mechanical Drawing Course and afterward for the Mechanical Engineering Course. He is master mechanic of reinforced concrete work for the Walter Bradley Concrete Company. His Courses have enabled hi to design several new machines, one of which saves the com- pany 25 per cent. of the cost of production. His salary has anhargi about 50 per cent. since he began to study his first ourse. FROM BRICKLAYER TO GENERAL CONTRACTOR W. C. Davis, Michigan Building, Wichita, Kans., was working as a bricklayer, with no prospect of advancement, when he enrolled with the Schools for the Complete Archi- tectural Course. After successfully superintending the con- struction of a large warehouse he became a member of the H. I. Ellis Construction Company, employing from 50 to 100 men. He says that his Course enables him to superintend the field work of the company, especially in the line of masonry and concrete. His income has increased at least 300 per cent. PASSED A SUCCESSFUL EXAMINATION Otis M. TOWNSEND Eighth St., Ocean City, N. J., was an 72 ada boy when he enrolled with the Schools’ for the mplete Architectural Course. He is now an architect and ogee employing 40 carpenters and keeping a draftsman in his office. 27 Aig ean enabled him to pass the state exam- ination On and receive a certificate as an architect. SALARY INCREASED 400 PER CENT. When C. M. Maynarp, 810 Belleville Ave., New Bedford, Mass., enrolled for the Building Contractors’ Course he was a carpenter, earning $1.75 a day. He gives the I. C. S. the credit for establishing him as a contractor and builder and increasing his income about 400 per cent. FROM POVERTY TO PROSPERITY H. L. Tuomas, Englewood, Colo., enrolled in the I. C. S. while out of work, without money, and with a family of six to support. Just one year after starting the I. C. S. Course he secured a position as draftsman, at $55 a month. Soon he got a better position at $75 a month, laying out work, and making plans and designs, all of which he could do without instruction other than that received from the Course. At present Mr. Thomas is with the Denver Union Water Company, as structural engineer. i Fireman Becomes Architect Michael O’Connor, Kansas City, Mo., a fire- man, became ambitious to learn architecture. He enrolled for the I. C. S. Complete Archi- tectural Course and studied during his spare time. Soon he drew plans for a $5,000 dwelling and they were accepted. Then he tried again with equal success. Now the self-taught architect is on the way to fortune. His city is proud of him. In an article about his career the Kansas City Star says: “The Kansas City fireman that has equipped himself for the profession of archi- tect by studious application between alarms furnishes an example of applied ambition that has become rather rare in these days of larger privileges. In olden times, when oppor- tunities for learning were few, there were more instances of such fruitful self-help. In fact, many of the great men of American history, several Presidents among them, gained their learning by great sacrifice. The Kansas City fireman has used only time that many men similarly placed have wasted. He has fitted himself for one of the noblest of professions. He has furnished a ‘modern instance’ worthy of emulation.” 12 BRICKLAYER BECOMES FOREMAN, AT $7 A DAY A. Rousseau, Hardin, Mont., was an ordinary bricklayer, earning $2.50 a day, when he enrolled for the Building Con- tractors’ Course. The studies enabled him to draw complete plans for his work and for outside work. He is now foreman, earning $7 a day. HILTON & SADLER, ARCHITECTS L. L. H1LTon and F. E. SADLER, Architects, Janesville, Wis., were carpenters when they enrolled in the I. C. S. Complete Architectural Course. Now they, as a firm, occupy a position of honor in Janesville. They have designed and superintended the building of many schools, churches, factories, and other large buildings in their own and in surrounding cities. CARPENTER BECOMES FOREMAN J. F. HARRINGTON, Missoula, Mont., before enrolling in the I. C. S., was a journeyman carpenter, earning $4.50 a day. The Course of study taught him to understand building plans = Se he has secured the position of foreman and earns a day. TEN TIMES HIS FORMER SALARY When the National Convention of Carpenters met in Scran- ton some years ago, JOHN G. GARBART, 16 Verner Avenue, Ingram, Pa., visited the I. C. S. Instruction Department. What he saw convinced him that he needed a Course and he enrolled in our School of Architecture. He was then earning $1.50 a day. His Course has enabled him to purchase the business of his former employer and he now earns ten times what he did when he enrolled. ANOTHER CARPENTER BECOMES A BUILDING CONTRACTOR CHARLES F. STENGEL, Jefferson, Wis., was a carpenter when he started to study in the I.C.S. Asa result of partly finish- ing the Complete Architectural Course he is in business with a friend, doing two-thirds of the building work in his vicinity. His business is mre larger every year and he says he owes his success to the I. C. S. NOW EARNS $5,000 A YEAR ~ Ep. J. WEAVER, Youngstown, Ohio, considers that the work he did with the I.C. S. in his two Courses, Architectural Draw- ing and Complete Architectural, are the foundation of his success in his chosen profession. When he enrolled he was a machine hand in a planing mill, earning $2 a day. He is now a practicing architect, and has earned $5,000 a year for several years past. 13 Salary Increased 300 Per Cent. When I began my Course in the Inter- national Correspondence Schools I was em- ployed as wheelwright at the Rodenhausen Wagon Works, Philadelphia, at a salary of $8 a week. JI am nowin business for myself as carpenter and builder. Since enrolling with your institution I have been so benefited that my salary has increased over 300 per cent. Your method of instruction is clear, com- prehensive, and direct in its meaning. It is my opinion that there is no better way for a workman to receive an education, without losing time from his work, than to enroll with the International Correspondence Schools. I had attended no school since 1897, until I enrolled with the I. C. S., December 19, 1900. My first Course was Mechanical Draw- ing. In May, 1904, I began working on the Complete Architectural Course, from which I have derived great benefits for the position I now hold. Please note that I fully realize and appre- ciate the interest you have taken in my Course. Trusting that other workmen will enroll in an I. C. S. Course and be benefited as I have been, I am, Henry A. Hosert, 2620 E. Cumberland St., Philadelphia, Pa. 14 Erected the Largest Rein- forced Concrete Build- ing in the World Erik Holman, Room 657, Pacific Building, San Francisco, Cal., had worked as a carpenter and contractor on a small scale for some years before he enrolled with the I. C. S. for the Complete Architectural Course. Having suc- cessfully superintended the erection of the first large reinforced concrete building in Los Angeles, he was called upon to erect the Pacific Building, corner of Market and Fourth Sts., San Francisco, Cal., costing $1,500,000, said to be the largest reinforced concrete office building in the world. He is now a consulting engineer, with an average income of $300 a month. 15 From the New Jersey State Board of Architects The New Jersey State Board of Architects in its second annual report, 1904, in recom- mendations under the heading of ‘‘ Books for Study,’’ makes the following statement indors- ing the International Correspondence Schools’ Courses of study: “The Board having received numerous inquiries concerning the extent of the prep- aration necessary to fif one to engage in an examination for a certificate to practice archi- tecture in the State, it has been thought best that the following information be issued. “The Boa d recommends, where it is pos- sible, that the student complete a full course in architecture at some well-known university or other institution of learning. A diploma of graduation supplemented by a proper amount of experience is sufficient evidence to the Board that the applicant for a certificate is worthy of one and that the formal exami- nation may be waived. “The Board realizes that to many this is impossible and to such it can recommend the Courses of study conducted through the mails by the International Correspondence Schools, Scranton, Pa. Any one who has taken one of these Courses will be well prepared to pass the Board’s examination.” 16