Aeronautics. Eighth annual report of the National Advisory Committee for Aeronautics, 1922. Including technical reports Nos. 133 to 158

Media type: E-Book

Title: Aeronautics. Eighth annual report of the National Advisory Committee for Aeronautics, 1922. Including technical reports Nos. 133 to 158

Contributor: Bacon, D.L. [Other]; Bateman, H. [Other]; Bear, R.M. [Other]; Brown, W. Byron [Other]; Brown, W.G. [Other]; Carroll, T. [Other]; Chu, Lynn [Other]; Durand, William Frederick [Other]; Eaton, H.N. [Other]; Gregg, Willis Ray [Other]; Harding, Warren Gamaliel [Other]; Harper, D.R. [Other]; Hill, G.C. [Other]; Hoff, Wilhelm [Other]; Lesley, E.P. [Other]; MacNair, W.A. [Other]; Munk, Max M. [Other]; Norton, Frederick Harwood [Other]; Reid, H.J.E. [Other]; Zahm, Albert Francis [Other]; Smith, R.H. [Other]; Sparrow, S.W. [Other]

Corporation: United States, President (1921-1923 : Harding) ; United States, Forest Products Laboratory ; United States, Dept. of Agriculture, Forest Service ; United States, National Advisory Committee for Aeronautics

imprint: Washington, DC, 1923
Online-Ausg.: Chester, Vt: NewsBank, inc, 2007

Extent: Online-Ressource (717 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 study of airplane maneuvers with special reference to angular velocities, by H.J.E. Reid [No. 155], p. 561
A study of taking off and landing an airplane, by T. Carroll [No. 154], p. 553
Analysis of stresses in German airplanes, by Wilhelm Hoff [No. 143], p. 263
Controllability and maneuverability of airplanes, by F.H. Norton and W.G. Brown [No. 153], p. 535
Damping coefficients due to tail surfaces in aircraft, by Lynn Chu [No. 136], p. 111
Experimental research on air propellers, V, by W.F. Durand and E.P. Lesley [No. 141], p. 167
General biplane theory, by Max M. Munk [No. 151], p. 473
General theory of thin wing sections, by Max M. Munk [No. 142], p. 243
Influence of model surface and air flow texture on resistance of aerodynamic bodies, by A.F. Zahm [No. 139], p. 151
Internal stresses in laminated construction, by Forest Products Laboratory [No. 145], p. 325
Lift and drag effects of wing-tip rake, by A.F. Zahm, R.M. Bear, and G.C. Hill [No. 140], p. 157
List of technical reports, p. VIII
Mathematical equations for heat conduction in the fins of air-cooled engines, by D.R. Harper and W.B. Brown [No. 158], p. 677
Nomenclature for aeronautics, by National Advisory Committee for Aeronautics [No. 157], p. 617
Performance of B.M.W. 185-horsepower airplane engine, by S.W. Sparrow [No. 135], p. 101
Performance of Maybach 300-horsepower airplane engine, by S.W. Sparrow [No. 134], p. 89
Point drag and total drag of Navy struts no. 1 modified, by A.F. Zahm, R.H. Smith, and G.C. Hill [No. 137], p. 125
Pressure distribution over the rudder and fin of an airplane in flight, by F.H. Norton and W.G. Brown [No. 149], p. 439
Pressure distribution over thick airfoils -- model tests, by F.H. Norton and D.L. Bacon [No. 150], p. 449
Standard atmosphere, by W.R. Gregg [No. 147], p. 397
Table of contents, p. VII
The aerodynamic properties of thick airfoils, II, by F.H. Norton and D.L. Bacon [No. 152], p. 519
The altitude effect on air speed indicators, II, by H.N. Eaton and W.A. MacNair [No. 156], p. 571
The decay of a simple eddy, by H. Bateman [No. 144], p. 317
The drag of 'C' class airship hull with varying length of cylindric midships, by A. F. Zahm, R.H. Smith, and G.C. Hill [No. 138], p. 141
The pressure distribution over the horizontal tail surfaces of an airplane, III, by F.H. Norton and W. G. Brown [No. 148], p. 411
The six-component wind balance, by A.F. Zahm [No. 146], p. 383
The tail plane, by Max M. Monk [No. 133], p. 53
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