Format:
Online-Ressource (717 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. 8161
Note:
A study of airplane maneuvers with special reference to angular velocities, by H.J.E. Reid [No. 155], p. 561
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A study of taking off and landing an airplane, by T. Carroll [No. 154], p. 553
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Analysis of stresses in German airplanes, by Wilhelm Hoff [No. 143], p. 263
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Controllability and maneuverability of airplanes, by F.H. Norton and W.G. Brown [No. 153], p. 535
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Damping coefficients due to tail surfaces in aircraft, by Lynn Chu [No. 136], p. 111
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Experimental research on air propellers, V, by W.F. Durand and E.P. Lesley [No. 141], p. 167
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General biplane theory, by Max M. Munk [No. 151], p. 473
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General theory of thin wing sections, by Max M. Munk [No. 142], p. 243
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Influence of model surface and air flow texture on resistance of aerodynamic bodies, by A.F. Zahm [No. 139], p. 151
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Internal stresses in laminated construction, by Forest Products Laboratory [No. 145], p. 325
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Lift and drag effects of wing-tip rake, by A.F. Zahm, R.M. Bear, and G.C. Hill [No. 140], p. 157
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List of technical reports, p. VIII
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Mathematical equations for heat conduction in the fins of air-cooled engines, by D.R. Harper and W.B. Brown [No. 158], p. 677
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Nomenclature for aeronautics, by National Advisory Committee for Aeronautics [No. 157], p. 617
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Performance of B.M.W. 185-horsepower airplane engine, by S.W. Sparrow [No. 135], p. 101
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Performance of Maybach 300-horsepower airplane engine, by S.W. Sparrow [No. 134], p. 89
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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
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Pressure distribution over the rudder and fin of an airplane in flight, by F.H. Norton and W.G. Brown [No. 149], p. 439
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Pressure distribution over thick airfoils -- model tests, by F.H. Norton and D.L. Bacon [No. 150], p. 449
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Standard atmosphere, by W.R. Gregg [No. 147], p. 397
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Table of contents, p. VII
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The aerodynamic properties of thick airfoils, II, by F.H. Norton and D.L. Bacon [No. 152], p. 519
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The altitude effect on air speed indicators, II, by H.N. Eaton and W.A. MacNair [No. 156], p. 571
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The decay of a simple eddy, by H. Bateman [No. 144], p. 317
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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
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The pressure distribution over the horizontal tail surfaces of an airplane, III, by F.H. Norton and W. G. Brown [No. 148], p. 411
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The six-component wind balance, by A.F. Zahm [No. 146], p. 383
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The tail plane, by Max M. Monk [No. 133], p. 53
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