• Media type: E-Book
  • Title: Aeronautics. Ninth annual report of the National Advisory Committee for Aeronautics, 1923. Administrative report without technical reports
  • Contributor: Ames, Joseph S. [Other]; Bacon, David L. [Other]; Brown, W.G. [Other]; Buckingham, Edgar [Other]; Carroll, T. [Other]; Coolidge, Calvin [Other]; Diehl, Walter S. [Other]; Hersey, Mayo D. [Other]; Hoot, H.I. [Other]; Lesley, E.P. [Other]; Munk, Max M. [Other]; Newlin, John A. [Other]; Norton, Frederick Harwood [Other]; Pickering, S.F. [Other]; Reid, Elliott G. [Other]; Silsbee, Francis B. [Other]; Trayer, George William [Other]; Weaver, E.R. [Other]; Wilson, Edwin Bidwell [Other]; Zahm, Albert Francis [Other]; Woods, Baldwin Munger [Other]
  • Corporation: United States, President (1923-1929 : Coolidge) ; United States, National Advisory Committee for Aeronautics
  • imprint: Washington, DC, 1924
    Online-Ausg.: Chester, Vt: NewsBank, inc, 2007
  • Published in: United States congressional serial set ; serial set no. 8255
    Senate document / 68th Congress, 1st session. Senate ; no. 2
  • Extent: Online-Ressource (560 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 constant pressure bomb, by F.W. Stevens [No. 176], p. 303
    A study of longitudinal dynamic stability in flight, by F.H. Norton [No. 170], p. 229
    Aerodynamic characteristics of airfoils -- III, by National Advisory Committee for Aeronautics [No. 182], p. 395
    Aeronautics: Ninth annual report of the National Advisory Committee for Aeronautics, 1923, including technical reports Nos. 159 to 185, follows p. 56
    An airship slide rule, by E.R. Weaver and S.F. Pickering [No. 160], p. 91
    Analysis of W.F. Durand's and E.P. Lesley's propeller tests, by Max M. Munk [No. 175], p. 289
    Appendix to Administrative report: Relation between aeronautic research and aircraft design, by Joseph S. Ames, p. 57
    Complete study of longitudinal oscillation of a VE-7 airplane, by F.H. Norton and W.G. Brown [No. 162], p. 127
    Deflection of beams with special reference to shear deformations by J.A. Newlin and G.W. Trayer [No. 180] p. 355
    Diaphragms for aeronautic instruments, by M.D. Hersey [No. 165], p. 155
    Dynamic stability as affected by the longitudinal moment of inertia, by Edwin B. Wilson [No. 172], p. 251
    Engine performance and the determination of absolute ceiling, by Walter S. Diehl [No. 171], p. 239
    Form factors of beams subjected to transverse loading only, by J.A. Newlin and G.W. Trayer [No. 181] p. 375
    Indices, p. 399
    Jet propulsion for airplanes, by Edgar Buckingham [No. 159], p. 73
    List of technical reports, p. VIII
    Measurement of the damping in roll on the JN4h in flight, by F.H. Norton [No. 167], p. 199
    Pages listed in the Contents Note reflect printed page numbers within successive, separately paginated parts of the publication
    Publication contains discontinuous pagination
    Relative efficiency of direct and geared drive propellers, by Walter S. Diehl [No. 178], p. 335
    Reliable formulae for estimating airplane performance and the effects of changes in weight, wing area, or power, by Walter S. Diehl [No. 173], p. 259
    Table of contents, p. VII
    Table of contents, p. VII
    Technical reports dated 1924
    The aerodynamic forces on airships hulls, by Max M. Munk [No. 184], p. 451
    The aerodynamic plane table, by A.F. Zahm [No, 166], p. 187
    The analysis of free flight propeller tests and its application to design, by Max M. Munk [No. 183], p. 439
    The distribution of lift over wing tips and ailerons, by David L. Bacon [No. 161], p. 103
    The effect of airfoil thickness and plan form on lateral control, by H.I. Hoot [No. 169], p. 217
    The effect of electrode temperature on the sparking voltage of short spark gaps, by F.B. Silsbee [No. 179], p. 345
    The effect of slipstream obstructions on air propellers, by E.P. Lesley and B.M. Woods [No. 177], p. 311
    The general efficiency curve for air propellers, by Walter S. Diehl [No. 168], p. 205
    The inertia coefficients of an airship in a frictionless fluid, by H. Bateman [No. 164], p. 139
    The resistance of spheres in wind tunnels and in air, by D.L. Bacon and E.G. Reid [No. 185], p. 469
    The smaller angular oscillations of airplanes in steady flight, by F.H. Norton [No. 174], p. 281
    The vertical, longitudinal and lateral accelerations experienced by an S.E. 5A airplane while maneuvering, by F.H. Norton and T. Carroll [No. 163], p. 133
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