> Details

Biermann, Arnold E. [Other]; Briggs, L.J [Other]; Brombacher, W.G [Other]; Burgess, C.P [Other]; Cordero, F. [Other]; DeFrance, S.J [Other]; Diehl, Walter S. [Other]; Dryden, Hugh Latimer [Other]; Gelalles, A.G [Other]; Gove, W.D [Other]; Higgins, George J. [Other]; Hoover, Herbert [Other]; Jacobs, Eastman N. [Other]; Joachim, William F. [Other]; Knight, Montgomery [Other]; Kuethe, Arnold Martin [Other]; Lesley, E.P [Other]; Louden, F.A [Other]; March, H.W [Other]; Rothrock, A.M [Other]; Zahm, Albert Francis [Other]; Wenzinger, Carl Joseph [Other]; Wood, Donald H. [Other]; Reid, Elliott G. [Other]; [...] ; United States Congress Senate, United States President (1929-1933 : Hoover), United States National Advisory Committee for Aeronautics

Aeronautics. Fifteenth annual report of the National Advisory Committee for Aeronautics, 1929. Including technical reports Nos. 309 to 336

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  • Media type: E-Book
  • Title: Aeronautics. Fifteenth annual report of the National Advisory Committee for Aeronautics, 1929. Including technical reports Nos. 309 to 336
  • Contributor: Biermann, Arnold E. [Other]; Briggs, L.J. [Other]; Brombacher, W.G. [Other]; Burgess, C.P. [Other]; Cordero, F. [Other]; DeFrance, S.J. [Other]; Diehl, Walter S. [Other]; Dryden, Hugh Latimer [Other]; Gelalles, A.G. [Other]; Gove, W.D. [Other]; Higgins, George J. [Other]; Hoover, Herbert [Other]; Jacobs, Eastman N. [Other]; Joachim, William F. [Other]; Knight, Montgomery [Other]; Kuethe, Arnold Martin [Other]; Lesley, E.P. [Other]; Louden, F.A. [Other]; March, H.W. [Other]; Rothrock, A.M. [Other]; Zahm, Albert Francis [Other]; Wenzinger, Carl Joseph [Other]; Wood, Donald H. [Other]; Reid, Elliott G. [Other]; Thompson, F.L. [Other]; Weick, Fred E. [Other]; Trayer, George William [Other]; Schey, Oscar W. [Other]; Smith, R.H. [Other]
  • Corporation: United States, President (1929-1933 : Hoover) ; United States, National Advisory Committee for Aeronautics
  • imprint: Washington, DC, 1930
    Online-Ausg.: Chester, Vt: NewsBank, inc, 2007
  • Published in: United States congressional serial set ; serial set no. 9221
    Senate document / 71st Congress, 2nd session. Senate ; no. 60
  • Extent: Online-Ressource (787 p); illustrations, tables
  • Language: English
  • Reproductino series: U.S. Congressional Serial Set, 1817-1980
  • Type of reproduction: Online-Ausg.
  • Place of reproduction: Chester, Vt: NewsBank, inc, 2007
  • Origination:
  • Footnote: Table of contents, p. VI
    Table of technical reports, p. VII
    Technical Report No. 309. Joint report on standardization tests on N.P.L. R.A.F. 15 Airfoil Model, by Walter S. Diehl, p. 91
    Technical Report No. 310. Pressure element of constant logarithmic stiffness for temperature compensated altimeter, by W.G. Brombacher and F. Cordero, p. 111
    Technical Report No. 311. Aerodynamic theory and test of strut forms, by R.H. Smith, p. 125
    Technical Report No. 312. The prediction of airfoil characteristics, by George J. Higgins, p. 149
    Technical Report No. 313. Drag and cooling with various forms of cowling for a "Whirlwind" radial air-cooled engine-I, by Fred E. Weick, p. 163
    Technical Report No. 314. Drag and cooling with various forms of cowling for a "Whirlwind" radial air-cooled engine-II, by Fred E. Weick, p. 189
    Technical Report No. 315. Aerodynamic characteristics of airfoils-VI, by National Advisory Committee for Aeronautics, p. 211
    Technical Report No. 316. Tables for pressure of air coming to rest from various speeds, by A.F. Zahm and F.A. Louden, p. 247
    Technical Report No. 317. Wind tunnel tests on a series of wing models through a large angle of attack range. Part I -- Force tests, by Montgomery Knight and Carl J. Wenzinger, p. 255
    Technical Report No. 318. Speed and deceleration trials of U.S.S. Los Angeles, by S.J. DeFrance and C.P. Burgess, p. 305
    Technical Report No. 319. Aerodynamic characteristics of twenty-four air-foils at high speed, by L.J. Briggs and H.L. Dryden, p. 325
    Technical Report No. 320. The measurement of fluctuations of air speed by hot-wire anemometer, by H.L. Dryden and A.M. Kuethe, p. 357
    Technical Report No. 321. Fuel vapor pressures and the relation of vapor pressure to the preparation of fuel for combustion in fuel injection engines, by William F. Joachim and A.M. Rothrock, p. 383
    Technical Report No. 322. Investigation of air flow in open-throat wind tunnels, by Eastman N. Jacobs, p. 397
    Technical Report No. 323. Flow and force equations for a body revolving in fluid, by A.F. Zahm, p. 409
    Technical Report No. 324. Flight tests on U.S.S. Los Angeles. Part I. -- Full scale pressure distribution investigation, by S.J. DeFrance, p. 449
    Technical Report No. 325. Flight tests on U.S.S. Los Angeles. Part II. -- Stress and strength determination, by C.P. Burgess, p. 483
    Technical Report No. 326. Tests of five metal model propellers with various pitch distributions in a free wind stream and in combination with a model VE-7 fuselage, by E.P. Lesley and Elliott G. Reid, p. 499
    Technical Report No. 327. The effect of supercharger capacity on engine and airplane performance, by O.W. Schey and W.D. Gove, p. 517
    Technical Report No. 328. Water pressure distribution on a twin-float seaplane, by F.L. Thompson, p. 537
    Technical Report No. 329. The torsional strength of wings, by C.P. Burgess, p. 555
    Technical Report No. 330. Experimental and analytical determination of the motion of hydraulically operated valve stems in oil engine injection systems, by A.G. Gelalles and A.M. Rothrock, p. 569
    Technical Report No. 331. Collection of wind-tunnel data on commonly used wing sections, by F.A. Louden, p. 589
    Technical Report No. 332. The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine, by Oscar W. Schey and Arnold E. Biermann, p. 635
    Technical Report No. 333. Full-scale turning characteristics of the U.S.S. Los Angeles, by F.L. Thompson, p. 657
    Technical Report No. 334. The torsion of members having sections common in aircraft construction, by George W. Trayer and H.W. March, p. 671
    Technical Report No. 335. Aerodynamic theory and test of strut forms II, by R.H. Smith, p. 721
    Technical Report No. 336. Tests of large airfoils in the propeller research tunnel, including two with corrugated surfaces, by Donald H. Wood, p. 761
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