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Bear, R.M [Other]; Crowley, J.W [Other]; Diehl, Walter S. [Other]; Gove, W.D [Other]; Green, M.W [Other]; Heald, R.H [Other]; Hicks, Chester W. [Other]; Keulegan, Garbis Hovannes [Other]; Knight, Montgomery [Other]; Loeser, Oscar E. [Other]; Louden, F.A [Other]; Mixson, R.E [Other]; Rhode, Richard V. [Other]; Schey, Oscar W. [Other]; Smith, R.H [Other]; Stevens, F.W [Other]; Strother, D.H [Other]; Ware, Marsden [Other]; Weick, Fred E. [Other]; Zahm, Albert Francis [Other]; Wood, Donald H. [Other]; Wilson, Ernest E. [Other] ; United States Congress Senate, United States National Advisory Committee for Aeronautics

Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308

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  • Media type: E-Book
  • Title: Aeronautics. Fourteenth annual report of the National Advisory Committee for Aeronautics, 1928, including Technical Reports Nos. 283 to 308
  • Contributor: Bear, R.M. [Other]; Crowley, J.W. [Other]; Diehl, Walter S. [Other]; Gove, W.D. [Other]; Green, M.W. [Other]; Heald, R.H. [Other]; Hicks, Chester W. [Other]; Keulegan, Garbis Hovannes [Other]; Knight, Montgomery [Other]; Loeser, Oscar E. [Other]; Louden, F.A. [Other]; Mixson, R.E. [Other]; Rhode, Richard V. [Other]; Schey, Oscar W. [Other]; Smith, R.H. [Other]; Stevens, F.W. [Other]; Strother, D.H. [Other]; Ware, Marsden [Other]; Weick, Fred E. [Other]; Zahm, Albert Francis [Other]; Wood, Donald H. [Other]; Wilson, Ernest E. [Other]
  • Corporation: United States, National Advisory Committee for Aeronautics
  • imprint: Washington, DC, 1929
    Online-Ausg.: Chester, Vt: NewsBank, inc, 2007
  • Published in: United States congressional serial set ; serial set no. 9003
    Senate document / 70th Congress, 2nd session. Senate ; no. 178
  • Extent: Online-Ressource (582 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: A preliminary investigation of supercharging an air-cooled engine in flight, by Marsden Ware and Oscar W. Schey [No. 283], p. 81
    A study of wing flutter, by A.F. Zahm and R.M. Bear [No. 285], p. 107
    Aerodynamic characteristics of airfoils-V, by National Advisory Committee for Aeronautics [No. 286], p. 135
    Aircraft accidents, by Special Subcommittee of the National Advisory Committee for Aeronautics [No. 308], p. 557
    An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 303], p. 477
    An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 304], p. 487
    An investigation of the use of discharge valves and intake control for improving the performance of N.A.C.A. Roots Type Supercharger, by Oscar W. Schey and Ernest E. Wilson [No. 302], p. 477
    Characteristics of five propellers in flight, by J.W. Crowley, Jr., and R.E. Mixson [No. 292], p. 265
    Drag of C-class airship hulls of various fineness ratios, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 291], p. 249
    Effect of variation of chord and span of ailerons on rolling and yawing moments in level flight, by R.H. Heald and D.H. Strother [No. 298], p. 383
    Forces on elliptic cylinders in uniform air stream, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 289], p. 215
    Full scale tests on a thin metal propeller at various tip speeds, by Fred E. Weick [No. 301], p. 463
    Full-scale wind-tunnel tests of a series of metal propellers on a VE-7 airplane, by Fred E. Weick [No. 306], p. 519
    Investigation of damping liquids for aircraft instruments, by G.H. Keulegan [No. 299], p. 403
    Pressure distribution over a rectangular monoplane wing model up to 90' angle of attack, by Montgomery Knight and Ocsar Loeser, Jr. [No. 288], p. 195
    Pressure distribution tests on PW-9 models from -18' through 90' angle of attack, by Oscar E. Loeser, Jr. [No. 296], p. 333
    Reduction of observed airplane performance to standard conditions, by Walter S. Diehl [No. 297], p. 355
    Table of contents, p. VI
    The comparative performance of roots type aircraft engine superchargers as affected by change in impeller speed and displacement, by Marsden Ware and Ernest E. Wilson [No. 284], p. 93
    The gaseous explosive reaction: A study of the kinetics of composite fuels, by F.W. Stevens [No. 305], p. 501
    The measurement of maximum cylinder pressures, by Chester W. Hicks [No. 294], p. 309
    The pressure distribution over the horizontal and vertical tail surfaces of the F6C-4 pursuit airplane in violent maneuvers, by R.V. Rhode [No. 307], p. 537
    The twenty-foot propeller research tunnel of the National Advisory Committee for Aeronautics, by Fred E. Weick and Donald H. Wood [No. 300], p. 427
    The variation in engine power with altitude determined from measurements in flight with a hub dynamometer, by W.D. Gove [No. 295], p. 321
    Theories of flow similitude, by A.F. Zahm [No. 287], p. 185
    Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane, by Walter S. Diehl [No. 293], p. 289
    Water-pressure distribution on a seaplane float, by F.L. Thompson [No. 290], p. 233
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