Format:
Online-Ressource (643 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. 10318
Note:
A discussion of certain problems connected with the design of hulls of flying boats and the use of general test data, by Walter S. Diehl [No. 625], p. 253
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A flight comparison of conventional ailerons on a rectangular wind and of conventional and floating wing-tip ailerons on a tapered wing, by H.A. Soule and W. Gracey [No. 630], p. 351
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A photographic study of combustion and knock in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 622], p. 213
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A study of the torque equilibrium of an auto-giro rotor, by F.J. Bailey, Jr. [No. 623], p. 235
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Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel, by Robert M. Pinkerton and Harry Greenberg [No. 628], p. 297
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Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings, by Eastman N. Jacobs and R.V. Rhode [No. 631], p. 357
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Appendix, p. 130
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Approximate stress analysis of multistringer beams with shear deformation of the flanges, by Paul Kuhn [No. 636], p. 469
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Auto-ignition and combustion of diesel fuel in a constant-volume bomb, by Robert F. Selden [No. 617], p. 147
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Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing-edge flaps, by H. Julian Allen [No. 634], p. 435
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Column strength of tubes elastically restrained against rotation at the ends, by William R. Osgood [No. 615], p. 101
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Comparative flight and full-scale wind-tunnel measurements of the maximum life of an airplane, by Abe Silverstein, S. Katzoff, and James A. Hootman [No. 618], p. 161
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Compressible flow about symmetrical Jonkowski profiles, by Carl Kaplan [No. 621], p. 197
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Determination of the boundary-layer transition on three symmetrical airfoils in the N.A.C.A. full-scale wind tunnel, by Abe Silverstein, and John V. Becker [No. 637], p. 491
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Drag of cylinders of simple shapes, by W.F. Lindsey [No. 619], p. 169
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Heat-transfer processes in air-cooled engine cylinders, by Benjamin Pinkel [No. 612], p. 49
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Interrelation of exhaust-gas constituents, by Harold C. Gerrish and Fred Voss [No. 616], p. 139
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List of technical reports, p. III
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On sonic reciprocal relations in the theory of nonstationary flows, by I.E. Garrick [No. 629], p. 347
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Pressure distribution over airfoils with Fowler flaps, by Carl J. Wenzinger and Walter B. Anderson [No. 620], p. 177
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Pressure distribution over an N.A.C.A. 23012 airfoil with an N.A.C.A. 23012 external-airfoil flap, by Carl J. Wenzinger [No. 614], p. 85
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Pressure distribution over an N.A.C.A. 23012 airfoil with a slotted and a plain flap, by Carl J. Wenzinger and James B. Delano [No. 633], p. 403
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Tests of five full-scale propellers in the presence of a radical and a liquid-cooled engine nacelle, including test of two spinners, by David Biermann and Edwin P. Hartman [No. 642], p. 587
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The aerodynamic characteristics of four full-scale propellers having different plan forms, by Edwin P. Hartman and David Biermann [No. 643], p. 617
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The aerodynamic characteristics of full-scale propellers having 2, 3, and 4 blades of Clark Y and R.A.F 6 airfoil sections, by Edwin P. Hartman and David Biermann [No. 640], p. 547
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The crinkling strength and the bending strength of round aircraft tubing, by William R. Osgood [No. 632], p. 387
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The effect of compressibility on eight full-scale propellers operating in the take-off and climbing range, by David Biermann and Edwin P. Hartman [No. 639], p. 517
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The experimental and calculated characteristics of 22 tapered wings, by Raymond F. Anderson [No. 627], p. 273
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The influence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts, by Robert T. Jones [No. 638], p. 507
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The negative thrust and torque of several full-scale propellers and their application to various flight problems, by Edwin P. Hartman and David Biermann [No. 641], p. 571
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The torsional and bending deflection of full-scale aluminum-alloy propeller blades under normal operating conditions, by Edwin P. Hartman and David Biermann [No. 644], p. 627
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The transition phase in the take-off of an airplane, by J.W. Wetmore [No. 626], p. 261
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The variation with Reynolds number of pressure distribution over an airfoil section, by Robert M. Pinkerton [No. 613], p. 65
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Theoretical stability and control characteristics of wings with various amounts of taper and twist, by Henry A. Pearson and Robert T. Jones [No. 635], p. 451
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Two dimensional subsonic compressible flow past elliptical cylinders, by Carl Kaplan [No. 624], p. 245
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