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