> Details

Allen, H. Julian [Other]; Anderson, Raymond F. [Other]; Anderson, Walter B. [Other]; Bailey, F.J [Other]; Becker, John V. [Other]; Biermann, David [Other]; Delano, James B. [Other]; Diehl, Walter S. [Other]; Garrick, I.E [Other]; Gerrish, Harold C. [Other]; Gracey, W. [Other]; Greenberg, Harry [Other]; Hartman, Edwin P. [Other]; Hootman, James A. [Other]; Jacobs, Eastman N. [Other]; Jones, Robert Thomas [Other]; Kaplan, Carl [Other]; Katzoff, S. [Other]; Kuhn, Paul [Other]; Rothrock, A.M [Other]; Silverstein, Abe [Other]; Pinkel, Benjamin [Other]; Wenzinger, Carl J. [Other]; Voss, Fred [Other]; [...] ; United States Congress Senate, United States National Advisory Committee for Aeronautics

Twenty-fourth annual report of the National Advisory Committee for Aeronautics, 1938. Including technical reports Nos. 612 to 644

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  • Media type: E-Book
  • Title: Twenty-fourth annual report of the National Advisory Committee for Aeronautics, 1938. Including technical reports Nos. 612 to 644
  • Contributor: Allen, H. Julian [Other]; Anderson, Raymond F. [Other]; Anderson, Walter B. [Other]; Bailey, F.J. [Other]; Becker, John V. [Other]; Biermann, David [Other]; Delano, James B. [Other]; Diehl, Walter S. [Other]; Garrick, I.E. [Other]; Gerrish, Harold C. [Other]; Gracey, W. [Other]; Greenberg, Harry [Other]; Hartman, Edwin P. [Other]; Hootman, James A. [Other]; Jacobs, Eastman N. [Other]; Jones, Robert Thomas [Other]; Kaplan, Carl [Other]; Katzoff, S. [Other]; Kuhn, Paul [Other]; Rothrock, A.M. [Other]; Silverstein, Abe [Other]; Pinkel, Benjamin [Other]; Wenzinger, Carl J. [Other]; Voss, Fred [Other]; Soule, Hartley Akin [Other]; Pearson, Henry A. [Other]; Wetmore, Joseph W. [Other]; Rhode, Richard V. [Other]; Spencer, Robert C. [Other]; Selden, Robert F. [Other]; Pinkerton, Robert M. [Other]; Lindsey, W.F. [Other]; Osgood, William R. [Other]
  • Corporation: United States, National Advisory Committee for Aeronautics
  • Published: Washington, DC, 1939
    Online-Ausg., Chester, Vt: NewsBank, inc, 2007
  • Published in: United States congressional serial set ; serial set no. 10318
    Senate document / 76th Congress, 1st session. Senate ; no. 3
  • Extent: Online-Ressource (643 p); illustrations, tables
  • Language: English
  • Reproduction series: U.S. Congressional Serial Set, 1817-1980
  • Type of reproduction: Online-Ausg.
  • Place of reproduction: Chester, Vt: NewsBank, inc, 2007
  • Origination:
  • Footnote: 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
    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
    A photographic study of combustion and knock in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 622], p. 213
    A study of the torque equilibrium of an auto-giro rotor, by F.J. Bailey, Jr. [No. 623], p. 235
    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
    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
    Appendix, p. 130
    Approximate stress analysis of multistringer beams with shear deformation of the flanges, by Paul Kuhn [No. 636], p. 469
    Auto-ignition and combustion of diesel fuel in a constant-volume bomb, by Robert F. Selden [No. 617], p. 147
    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
    Column strength of tubes elastically restrained against rotation at the ends, by William R. Osgood [No. 615], p. 101
    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
    Compressible flow about symmetrical Jonkowski profiles, by Carl Kaplan [No. 621], p. 197
    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
    Drag of cylinders of simple shapes, by W.F. Lindsey [No. 619], p. 169
    Heat-transfer processes in air-cooled engine cylinders, by Benjamin Pinkel [No. 612], p. 49
    Interrelation of exhaust-gas constituents, by Harold C. Gerrish and Fred Voss [No. 616], p. 139
    List of technical reports, p. III
    On sonic reciprocal relations in the theory of nonstationary flows, by I.E. Garrick [No. 629], p. 347
    Pressure distribution over airfoils with Fowler flaps, by Carl J. Wenzinger and Walter B. Anderson [No. 620], p. 177
    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
    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
    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
    The aerodynamic characteristics of four full-scale propellers having different plan forms, by Edwin P. Hartman and David Biermann [No. 643], p. 617
    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
    The crinkling strength and the bending strength of round aircraft tubing, by William R. Osgood [No. 632], p. 387
    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
    The experimental and calculated characteristics of 22 tapered wings, by Raymond F. Anderson [No. 627], p. 273
    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
    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
    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
    The transition phase in the take-off of an airplane, by J.W. Wetmore [No. 626], p. 261
    The variation with Reynolds number of pressure distribution over an airfoil section, by Robert M. Pinkerton [No. 613], p. 65
    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
    Two dimensional subsonic compressible flow past elliptical cylinders, by Carl Kaplan [No. 624], p. 245
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