Format:
Online-Ressource (560 p)
,
illustrations, tables
Edition:
Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
Series Statement:
United States congressional serial set serial set no. 8255
Note:
A constant pressure bomb, by F.W. Stevens [No. 176], p. 303
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A study of longitudinal dynamic stability in flight, by F.H. Norton [No. 170], p. 229
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Aerodynamic characteristics of airfoils -- III, by National Advisory Committee for Aeronautics [No. 182], p. 395
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Aeronautics: Ninth annual report of the National Advisory Committee for Aeronautics, 1923, including technical reports Nos. 159 to 185, follows p. 56
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An airship slide rule, by E.R. Weaver and S.F. Pickering [No. 160], p. 91
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Analysis of W.F. Durand's and E.P. Lesley's propeller tests, by Max M. Munk [No. 175], p. 289
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Appendix to Administrative report: Relation between aeronautic research and aircraft design, by Joseph S. Ames, p. 57
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Complete study of longitudinal oscillation of a VE-7 airplane, by F.H. Norton and W.G. Brown [No. 162], p. 127
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Deflection of beams with special reference to shear deformations by J.A. Newlin and G.W. Trayer [No. 180] p. 355
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Diaphragms for aeronautic instruments, by M.D. Hersey [No. 165], p. 155
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Dynamic stability as affected by the longitudinal moment of inertia, by Edwin B. Wilson [No. 172], p. 251
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Engine performance and the determination of absolute ceiling, by Walter S. Diehl [No. 171], p. 239
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Form factors of beams subjected to transverse loading only, by J.A. Newlin and G.W. Trayer [No. 181] p. 375
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Indices, p. 399
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Jet propulsion for airplanes, by Edgar Buckingham [No. 159], p. 73
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List of technical reports, p. VIII
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Measurement of the damping in roll on the JN4h in flight, by F.H. Norton [No. 167], p. 199
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Pages listed in the Contents Note reflect printed page numbers within successive, separately paginated parts of the publication
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Publication contains discontinuous pagination
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Relative efficiency of direct and geared drive propellers, by Walter S. Diehl [No. 178], p. 335
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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
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Table of contents, p. VII
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Table of contents, p. VII
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Technical reports dated 1924
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The aerodynamic forces on airships hulls, by Max M. Munk [No. 184], p. 451
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The aerodynamic plane table, by A.F. Zahm [No, 166], p. 187
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The analysis of free flight propeller tests and its application to design, by Max M. Munk [No. 183], p. 439
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The distribution of lift over wing tips and ailerons, by David L. Bacon [No. 161], p. 103
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The effect of airfoil thickness and plan form on lateral control, by H.I. Hoot [No. 169], p. 217
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The effect of electrode temperature on the sparking voltage of short spark gaps, by F.B. Silsbee [No. 179], p. 345
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The effect of slipstream obstructions on air propellers, by E.P. Lesley and B.M. Woods [No. 177], p. 311
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The general efficiency curve for air propellers, by Walter S. Diehl [No. 168], p. 205
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The inertia coefficients of an airship in a frictionless fluid, by H. Bateman [No. 164], p. 139
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The resistance of spheres in wind tunnels and in air, by D.L. Bacon and E.G. Reid [No. 185], p. 469
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The smaller angular oscillations of airplanes in steady flight, by F.H. Norton [No. 174], p. 281
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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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