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Abbott, Ira H.A [Other]; Anderson, Raymond F. [Other]; Bioletti, Carlton [Other]; Brevoort, Maurice J. [Other]; Cohn, Mildred [Other]; Dawson, John R. [Other]; Dryden, Hugh Latimer [Other]; Fiock, Ernest F. [Other]; Foster, Hampton H. [Other]; Garrick, I.E [Other]; Gulick, B.G [Other]; Harris, Thomas A. [Other]; Herrnstein, William H. [Other]; Jones, Robert Thomas [Other]; Lee, Dana W. [Other]; Marvin, Charles Frederick [Other]; Parkinson, John B. [Other]; Peterson, John B. [Other]; Pinkerton, Robert M. [Other]; Rothrock, A.M [Other]; Silverstein, Abe [Other]; Sherman, Albert [Other]; Wharton, Armistead [Other]; Waldron, C.D [Other]; [...] ; United States Congress Senate, United States National Advisory Committee for Aeronautics

Twenty-second annual report of the National Advisory Committee for Aeronautics, 1936. Including technical reports Nos. 542 to 576

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  • Media type: E-Book
  • Title: Twenty-second annual report of the National Advisory Committee for Aeronautics, 1936. Including technical reports Nos. 542 to 576
  • Contributor: Abbott, Ira H.A. [Other]; Anderson, Raymond F. [Other]; Bioletti, Carlton [Other]; Brevoort, Maurice J. [Other]; Cohn, Mildred [Other]; Dawson, John R. [Other]; Dryden, Hugh Latimer [Other]; Fiock, Ernest F. [Other]; Foster, Hampton H. [Other]; Garrick, I.E. [Other]; Gulick, B.G. [Other]; Harris, Thomas A. [Other]; Herrnstein, William H. [Other]; Jones, Robert Thomas [Other]; Lee, Dana W. [Other]; Marvin, Charles Frederick [Other]; Parkinson, John B. [Other]; Peterson, John B. [Other]; Pinkerton, Robert M. [Other]; Rothrock, A.M. [Other]; Silverstein, Abe [Other]; Sherman, Albert [Other]; Wharton, Armistead [Other]; Waldron, C.D. [Other]; Roeder, Carl H. [Other]; Wenzinger, Carl Joseph [Other]; Zimmerman, Charles Horton [Other]; Smith, Clyde W. [Other]; Weick, Fred E. [Other]; Schubauer, Galen Brandt [Other]; White, James A. [Other]; Wheatley, John B. [Other]; Shortal, Joseph Adams [Other]; Scudder, Nathan F. [Other]; Schey, Oscar W. [Other]; Windler, Ray [Other]; Platt, Robert C. [Other]; Spencer, Robert C. [Other]; Robinson, Russell Gideon [Other]; Rollin, Vern Gordon [Other]
  • Corporation: United States, National Advisory Committee for Aeronautics
  • Published: Washington, DC, 1937
    Online-Ausg., Chester, Vt: NewsBank, inc, 2007
  • Published in: United States congressional serial set ; serial set no. 10106
    Senate document / 75th Congress, 1st session. Senate ; no. 3
  • Extent: Online-Ressource (583 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 simplified application of the method of operators to the calculation of disturbed motions of an airplane, by Robert T. Jones [No. 560], p. 313
    Aerodynamic characteristics of N.A.C.A. 23012 and 23021 airfoils with 20-percent-chord external-airfoil flaps of N.A.C.A. 23012 section, by Robert C. Platt and Ira H. Abbott [No. 573], p. 523
    Air flow around finned cylinders, by M.J. Brevoort and Vern G. Rollin [No. 555], p. 237
    Air flow in the boundary layer near a plate, by Hugh L. Dryden [No. 562], p. 339
    Aircraft accidents method of analysis, report prepared by committee on aircraft accidents [No. 576], p. 564
    Aircraft compass characteristics, by John B. Peterson and Clyde W. Smith [No. 551], p. 187
    Calculated and measured pressure distributions over the midspan section of the N.A.C.A. 4412 airfoil, by Robert M. Pinkerton [No. 563], p. 365
    Combustion in a bomb with a fuel-injection system, by Mildred Cohn and Robert C. Spencer [No. 544], p. 107
    Cooling characteristics of a 2-row radial engine, by Oscar W. Schey and Vern G. Rollin [No. 550], p. 177
    Determination of the characteristics of tapered wings, by Raymond F. Anderson [No. 572], p. 503
    Effect of nozzle design on fuel spray and flame formation in a high-speed compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 561], p. 327
    Effect of tip shape and dihedral on lateral-stability characteristics, by Joseph A. Shortal [No. 548], p. 149
    Effects of air-fuel ratio on fuel spray and flame formation in a compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 545], p. 119
    Further studies of flame movement and pressure development in an engine cylinder, by Charles F. Marvin, Jr., Armistead Wharton, and Carl H. Roeder [No. 556], p. 251
    Ground-handling forces on a 1/40-scale model of the U.S. airship "Akron," by Abe Silverstein and B.G. Gulick [No. 566], p. 405
    Interference of wing and fuselage from tests of 28 combinations in the N.A.C.A. variable-density tunnel, by Albert Sherman [No. 575], p. 555
    List of technical reports, p. III
    Measurements of fuel distribution within sprays for fuel-injection engines, by Dana W. Lee [No. 565], p. 389
    Potential flow about arbitrary biplane wing sections, by I.E. Garrick [No. 542], p. 47
    Preliminary tests in the N.A.C.A. free-spinning wind tunnel, by C.H. Zimmerman [No. 557], p. 265
    Pressure distribution over a rectangular airfoil with a partial-span split flap, by Carl J. Wenzinger and Thomas A. Harris [No. 571], p. 491
    Pressure distribution over an airfoil section with a flap and tab, by Carl J. Wenzinger [No. 574], p. 543
    Propulsion of a flapping and oscillating airfoil, by I.E. Garrick [No. 567], p. 419
    Some effects of argon and helium upon explosions of carbon monoxide and oxygen, by Ernest F. Fiock and Carl H. Roeder [No. 553], p. 213
    Tank tests of N.A.C.A. model 40 series of hulls for small flying boats and amphibians, by John B. Parkinson and John R. Dawson [No. 543], p. 77
    Tests of a wing-nacelle-propeller combination at several pitch settings up to 42℗ʻ, by Ray Windler [No. 564], p. 381
    The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data, by Fred E. Weick and Robert T. Jones [No. 570], p. 465
    The effect of turbulence on the drag of flat plates, by G.B. Schubauer and H.L. Dryden [No. 546], p. 129
    The forces and moments acting on parts of the XN2Y-1 airplane during spins, by N.F. Scudder [No. 559], p. 305
    The quiescent-chamber type compression-ignition engine, by H.H. Foster [No. 568], p. 429
    Turbulence factors of N.A.C.A. wind tunnels as determined by sphere tests, by Robert C. Platt [No. 558], p. 283
    Wind-tunnel interference with particular reference to off-center positions of the wing and to the downwash at the tail, by Abe Silverstein and James A. White [No. 547], p. 135
    Wind-tunnel investigation of ordinary and split flaps on airfoils of different profile, by Carl J. Wenzinger [No. 554], p. 223
    Wind-tunnel investigation of the aerodynamic balancing of upper-surface ailerons and split flaps, by Carl J. Wenzinger [No. 549], p. 159
    Wind-tunnel tests of 10-foot-diameter auto-giro rotors, by John B. Wheatley and Carlton Bioletti [No. 552], p. 199
    Wing-nacelle-propeller interference for wings of various spans force and pressure-distribution tests, by Russel G. Robinson and William H. Herrnstein, Jr. [No. 569], p. 449
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