Aeronautics. Tenth annual report of the National Advisory Committee for Aeronautics, 1924. Including technical reports Nos. 186 to 209.

Aeronautics. Tenth annual report of the National Advisory Committee for Aeronautics, 1924. Including technical reports Nos. 186 to 209. [electronic resource]

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Bibliographic Details
Online Access:	Online Access
Corporate Authors:	United States. Congress. Senate, United States. National Advisory Committee for Aeronautics
Other Authors:	Beij, K. Hilding, Briggs, Lyman J. (Lyman James), 1874-1963, Buckingham, C.T, Burgess, Charles Paine, 1888-, Crowley, J. W., Diehl, Walter S. (Walter Stuart), 1893-1976, Doolittle, J. H., Dryden, Hugh L. (Hugh Latimer), 1898-1965, Durand, William Frederick, 1859-1958, Eaton, Herbert N. (Herbert Nelson), 1892-, Freeman, R. G., Hull, G. F., Lesley, E. P. (Everett Parker), 1874-1945, Munk, Max M. (Max Michael), 1890-, Newlin, J. A. (John A.), 1872-1943, Norton, F. H. (Frederick Harwood), 1896-1992, Randolph, D. W., Reid, Elliott G., Ronan, K. M., Scarborough, James B. (James Blaine), Silsbee, Francis B. (Francis Briggs), 1889-, Sparrow, Stanwood W., Trayer, George W. (George William), 1888-1976
Format:	Government Document Electronic eBook
Language:	English
Published:	Washington, DC, 1925.
Series:	United States congressional serial set ; serial set no. 8414. Senate document (United States. Congress. Senate) ; 68th Congress, no. 158.
Subjects:	United States. > National Advisory Committee for Aeronautics. Advisory boards. Aeronautics. Airplanes. Airships. Military aircraft. Transportation research. Annual Reports. Monographs.

Description
Item Description:	Table of contents, p. VII. Technical Report No. 186. The application of propeller test data to design and performance calculations, by Walter S. Diehl, p. 67. Technical Report No. 187. Flame speed and spark intensity, by D.W. Randolph and F.B. Silsbee, p. 79. 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. Technical Report No. 189. Relation of fuel-air ratio to engine performance, by Stanwood W. Sparrow, p. 107. Technical Report No. 190. Correcting horsepower measurements to a standard temperature, by Stanwood W. Sparrow, p. 123. Appendix to Technical Report No. 190, p. 137. Technical Report No. 191. Elements of the wing section theory and of the wing theory, by Max M. Munk, p. 139. Technical Report No. 192. Charts for graphical estimation of airplace performance, by Walter S. Diehl, p. 165. Technical Report No. 193. Pressure distribution over the wings of an MB-3 airplane in flight, by F.H. Norton, p. 177. Technical Report No. 194. Investigation of slipstream velocity, by J.W. Crowley, Jr., p. 197. Technical Report No. 195. Standardization tests of N.A.C.A. No. 1 wind tunnel, by Elliott G. Reid, p. 205. Technical Report No. 196. Comparison of model propeller tests with airfoil theory, by William F. Durand and E.P. Lesley, p. 235. 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. Technical Report No. 198. Astronomical methods in aerial navigation, by K. Hilding Beij, p. 269. Table of contents for Technical Report No. 198, p. 271. List of illustrations in Technical Report No. 198, p. 272. Technical Report No. 199. Interference tests on an N.A.C.A. pitot tube, by Elliott G. Reid, p. 321. Technical Report No. 200. Some problems on the lift and rolling moment of airplane wings, by James B. Scarborough, p. 329. Technical Report No. 201. The effects of shielding the tips of airfoils, by Elliott G. Reid, p. 345. Technical Report No. 202. The sparking voltage of spark plugs, by F.B. Silsbee, p. 355. Technical Report No. 203. Accelerations in flight, by J.H. Doolittle, p. 371. Technical Report No. 204. Forces on airships in gusts, by C.P. Burgess, p. 389. Technical Report No. 205. The effect of changes in compression ratio upon engine performance, by Stanwood W. Sparrow, p. 397. Technical Report No. 206. Nonmetallic diaphragms for instruments, by H.N. Eaton and C.T. Buckingham, p. 419. Index to Technical Report No. 206, p. 421. Technical Report No. 207. Aerodynamic characteristics of airfoils at high speeds, by L.J. Briggs, G.F. Hull, and H.L. Dryden, p. 463. 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. Technical Report No. 209. Characteristics of a single float seaplane during take-off, by J.W. Crowley, Jr. and K.M. Ronan, p. 489.
Physical Description:	508 p. : illustrations, tables.