%0 Generic

%T Twenty-first annual report of the National Advisory Committee for Aeronautics, 1935. Including technical reports Nos. 508 to 541

%A United States Congress Senate

%A United States President (1933-1945 : Roosevelt)

%A United States National Advisory Committee for Aeronautics

%A Bamber, Millard J.

%A Biermann, David

%A Bioletti, Carlton

%A Brevoort, Maurice J.

%A Brombacher, W.G

%A Burke, Walter F.

%A Clay, William C.

%A Cohn, Mildred

%A Deming, A.F

%A Fiock, Ernest F.

%A Foster, Hampton H.

%A Gerrish, Harold C.

%A Gough, Melvin Neilson

%A Harris, Thomas A.

%A Herrnstein, William H.

%A Hood, Manley J.

%A Jacobs, Eastman N.

%A Joyner, Upshur T.

%A Kaplan, Carl

%A Rothrock, A.M

%A Waldron, C.D

%A Roeder, Carl H.

%A Zimmerman, Charles Horton

%A Lee, Dana W.

%A Marsh, E.T

%A Stowell, E.Z

%A Lundquist, Eugene E.

%A Roosevelt, Franklin Delano

%A Weick, Fred E.

%A Schubauer, Galen Brandt

%A King, H. Kendall

%A Soule, Hartley Akin

%A Wheatley, John B.

%A Ward, Kenneth E.

%A Scudder, Nathan F.

%A Seidman, Oscar

%A Schey, Oscar W.

%A Kuhn, Paul

%A Noyes, Richard W.

%A Platt, Robert C.

%A Pinkerton, Robert M.

%A Wallace, Rudolf

%A Rollin, Vern Gordon

%A McAvoy, William H.

%D 1936

%X A comparison of fuel sprays from several types of injection nozzles, by Dana W. Lee [No. 520], p. 251

%X A flight investigation of the spinning of the F4B-2 biplane with various loads and tail surfaces, by N.F. Scudder and Oscar Seidman [No. 529], p. 413

%X A turbulence indicator utilizing the diffusion of heat, by G.B. Schubauer [No. 524], p. 337

%X Aerodynamic characteristics of a wing with fowler flaps, including flap loads downwash, and calculated effect of take-off, by Robert C. Platt [No. 534], p. 477

%X Aerodynamic characteristics of wings with cambered external-airfoil flaps, including lateral control with a full-span flap, by Robert C. Platt [No. 541], p. 609

%X Air flow in a separating laminar boundary layer, by G.B. Schubauer [No. 527], p. 369

%X Altitude-pressure tables based on the United States Standard Atmosphere, by W.G. Brombacher [No. 538], p. 531

%X An analysis of longitudinal stability in power-off flight with charts for use in design, by Charles H. Zimmerman [No. 521], p. 289

%X Analysis of 2-spar cantilever wings with special reference to torsion and load transference, by Paul Kuhn [No. 508], p. 45

%X Appendices, p. 64

%X Appendix, p. 201

%X Appendix, p. 249

%X Appendix, p. 318

%X Appendix, p. 487

%X Appendix, p. 76

%X Characteristics of the N.A.C.A. 23012 airfoil from tests in the full-scale and variable-density tunnels, by Eastman N. Jacobs and William C. Clay [No. 530], p. 435

%X Distribution and regularity of injection from a multicylinder fuel-injection pump, by A.M. Rothrock and E.T. Marsh [No. 533], p. 465

%X Experimental investigation of the Robinson-type cup anemometer, by M.J. Brevoort and U.T. Joyner [No. 513], p. 143

%X Flight investigation of lateral control devices for use with full-span flaps, by H.A. Soule and W.H. McAvoy [No. 517], p. 209

%X Full-scale wind-tunnel tests of a PCA-2 autogiro rotor, by John B. Wheatley and Manley J. Hood [No. 515], p. 179

%X General equations for the stress analysis of rings, by Eugene E. Lundquist and Walter F. Burke [No. 509], p. 69

%X Hydrogen as an auxiliary fuel in compression-ignition engines, by Harold C. Gerrish and Hampton H. Foster [No. 535], p. 495

%X Interference of wing and fuselage from tests of 209 combinations in the N.A.C.A. variable-density tunnel, by Eastman N. Jacobs and Kenneth E. Ward [No. 540], p. 571

%X Investigation of full-scale split trailing-edge wing flaps with various chords and hinge locations, by Rudolf Wallace [No. 539], p. 545

%X List of technical reports, p. III

%X Noise from two-blade propellers, by E.Z. Stowell and A.F. Deming [No. 526], p. 359

%X Potential flow about elongated bodies of revolution, by Carl Kaplan [516], p. 189

%X Reduction of hinge moments of airplane control surfaces by tabs, by Thomas A. Harris [No. 528], p. 381

%X Some effects of injection advance angle, engine-jacket temperature, and speed on combustion in a compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 525], p. 343

%X Some factors affecting combustion in an internal-combustion engine, by A.M. Rothrock and Mildred Cohn [No. 512], p. 125

%X Spinning characteristics of wings. I. -- Rectangular Clark Y monoplane wing, by M.J. Bamber and C.H. Zimmerman [No. 519], p. 231

%X Tests in a variable-density wind tunnel of related airfoils having the maximum camber unusually far forward, by Eastman N. Jacobs and Robert M. Pinkerton [No. 537], p. 521

%X The drag of airplane wheels, wheel fairings and landing gears. II. -- Nonretractable and partly retractable landing gears, by David Biermann and William H. Herrnstein, Jr. [No. 518], p. 219

%X The drag of airplane wheels, wheel fairings, and landing gears -- III, by William H. Herrnstein, Jr. and David Biermann [No. 522], p. 321

%X The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders, by Oscar W. Schey and Vern G. Rollin [No. 511], p. 111

%X The effect of water vapor on flame velocity in equivalent CO-O2 mixtures, by Ernest F. Fiock and H. Kendall King [No. 531], p. 445

%X The influence of wing setting on the wing lead and rotor speed of a PCA-2 autogiro as determined in flight, by John B. Wheatley [No. 323], p. 333

%X The measurements of the field of view from airplane cockpits, by Melvin N. Gough [No. 514], p. 167

%X The soap-bubble method of studying the combustion of mixtures of CO and O2, by Ernest F. Fiock and Carl H. Roeder [No. 532], p. 451

%X Wind-tunnel research comparing lateral control devices particularly at high angles of attack. XIII. -- Auxiliary airfoils used as external ailerons, by Fred E. Weick and Richard W. Noyes [No. 510], p. 79

%X Wind-tunnel tests of a 10-foot-diameter gyroplane rotor, by John B. Wheatley and Carlton Bioletti [No. 536], p. 511

%C Washington, DC

%U http://slubdd.de/katalog?TN_libero_mab2