Format:
Online-Ressource (508 p)
,
illustrations, tables
Edition:
Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
Series Statement:
United States congressional serial set serial set no. 8414
Note:
Appendix to Technical Report No. 190, p. 137
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Index to Technical Report No. 206, p. 421
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List of illustrations in Technical Report No. 198, p. 272
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Table of contents for Technical Report No. 198, p. 271
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Table of contents, p. VII
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Technical Report No. 186. The application of propeller test data to design and performance calculations, by Walter S. Diehl, p. 67
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Technical Report No. 187. Flame speed and spark intensity, by D.W. Randolph and F.B. Silsbee, p. 79
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Technical Report No. 188. Stresses in wood members subjected to combined column and beam action, by J.A. Newlin and G.W. Trayer, p. 93
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Technical Report No. 189. Relation of fuel-air ratio to engine performance, by Stanwood W. Sparrow, p. 107
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Technical Report No. 190. Correcting horsepower measurements to a standard temperature, by Stanwood W. Sparrow, p. 123
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Technical Report No. 191. Elements of the wing section theory and of the wing theory, by Max M. Munk, p. 139
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Technical Report No. 192. Charts for graphical estimation of airplace performance, by Walter S. Diehl, p. 165
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Technical Report No. 193. Pressure distribution over the wings of an MB-3 airplane in flight, by F.H. Norton, p. 177
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Technical Report No. 194. Investigation of slipstream velocity, by J.W. Crowley, Jr., p. 197
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Technical Report No. 195. Standardization tests of N.A.C.A. No. 1 wind tunnel, by Elliott G. Reid, p. 205
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Technical Report No. 196. Comparison of model propeller tests with airfoil theory, by William F. Durand and E.P. Lesley, p. 235
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Technical Report No. 197. A new relation between the induced yawing moment and the rolling moment of an airfoil in straight motion, by Max M. Munk, p. 261
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Technical Report No. 198. Astronomical methods in aerial navigation, by K. Hilding Beij, p. 269
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Technical Report No. 199. Interference tests on an N.A.C.A. pitot tube, by Elliott G. Reid, p. 321
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Technical Report No. 200. Some problems on the lift and rolling moment of airplane wings, by James B. Scarborough, p. 329
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Technical Report No. 201. The effects of shielding the tips of airfoils, by Elliott G. Reid, p. 345
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Technical Report No. 202. The sparking voltage of spark plugs, by F.B. Silsbee, p. 355
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Technical Report No. 203. Accelerations in flight, by J.H. Doolittle, p. 371
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Technical Report No. 204. Forces on airships in gusts, by C.P. Burgess, p. 389
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Technical Report No. 205. The effect of changes in compression ratio upon engine performance, by Stanwood W. Sparrow, p. 397
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Technical Report No. 206. Nonmetallic diaphragms for instruments, by H.N. Eaton and C.T. Buckingham, p. 419
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Technical Report No. 207. Aerodynamic characteristics of airfoils at high speeds, by L.J. Briggs, G.F. Hull, and H.L. Dryden, p. 463
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Technical Report No. 208. A determination of turning characteristics of the C-7 airship by means of a camera obscura, by J.W. Crowley, Jr., and R.G. Freeman, p. 481
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Technical Report No. 209. Characteristics of a single float seaplane during take-off, by J.W. Crowley, Jr. and K.M. Ronan, p. 489
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