Aeronautics. Twentieth annual report of the National Advisory Committee for Aeronautics, 1934, including technical reports Nos. 475 to 507

Medientyp: E-Book

Titel: Aeronautics. Twentieth annual report of the National Advisory Committee for Aeronautics, 1934, including technical reports Nos. 475 to 507

Körperschaft: United States, National Advisory Committee for Aeronautics

Erschienen: Washington, DC, 1935
Online-Ausg., Chester, Vt: NewsBank, inc, 2007

Umfang: Online-Ressource (657 p); illustrations, tables

Sprache: Englisch

Reproduktionsreihe: U.S. Congressional Serial Set, 1817-1980

Art der Reproduktion: Online-Ausg.

Hersteller der Reproduktion: Chester, Vt: NewsBank, inc, 2007

Entstehung:

Anmerkungen: A description and test results of a spark-ignition and a compression-ignition 2-stroke cycle engine, by J.A. Spanogle and E.G. Whitney [No. 495], p. 395
A flight investigation of the effect of mass distribution and control setting on the spinning of the XN2Y-1 airplane, by N.F. Scudder [No. 484], p. 185
A flight investigation of the lateral control characteristics of short wide ailerons and various spoilers with different amounts of wing dihedral, by Fred E. Weick, Hartley A. Soule, and Melvin N. Gough [No. 494], p. 381
Air conditions close to the ground and the effect on airplane landings, by F.L. Thompson, W.C. Peck, and A.P. Beard [No. 489], p. 271
An aerodynamic analysis of the autogiro rotor with a comparison between calculated and experimental results, by John B. Wheatley [No. 487], p. 235
Computation of the two-dimensional flow in a laminar boundary layer, by Hugh L. Dryden [No. 497], p. 435
Effect of moderate air flow on the distribution of fuel sprays after injection cut-off, by A.M. Rothrock and R.C. Spencer [No. 483], p. 163
Effect of viscosity on fuel leakage between lapped plungers and sleeves and on the discharge from a pump-injection system, by A.M. Rothrock and E.T. Marsh [No. 477], p. 63
Experimental verification of the theory of wind-tunnel boundary interference, by Theodore Theodorsen and Abe Silverstein [No. 478], p. 79
General theory of aerodynamic instability and the mechanism of flutter, by Theodore Theodorsen [No. 496], p. 413
Heat transfer from finned metal cylinders in an air stream, by Arnold E. Biermann and Benjamin Pinkel [No. 488], p. 251
Improved airplane windshields to provide vision in stormy weather, by William C. Clay [No. 498], p. 445
Infrared radiation from explosions in a spark-ignition engine, by Charles F. Marvin, Jr., Frank R. Caldwell, and Sydney Steele [No. 486], p. 223
List of technical reports, p. VII
On the theory of laminar boundary layers involving separation, by Th. von Karman and C.B. Milliken [No. 504], p. 541
Relation of hydrogen and methane to carbon monoxide in exhaust gases from internal combustion engines, by Harold C. Gerrish and Arthur M. Tessmann [No. 476], p. 53
Relative loading on biplane wings of unequal chords, by Walter S. Diehl [No. 501], p. 503
Scale effect on Clark V airfoil characteristics from N.A.C.A. full-scale wind-tunnel tests, by Abe Silverstein [No. 502], p. 509
Stability of thin-walled tubes under torsion, by L.H. Donnell [No. 479], p. 95
Tests of nacelle-propeller combinations in various positions in reference to wings. IV. -- Thick wing -- various radial engine cowlings -- tandem propellers, by James G. McHugh [No. 505], p. 561
Tests of 16 related airfoils at high speeds, by John Stack and Albert B. von Doenhoff [No. 492], p. 339
Tests of nacelle-propeller combinations in various positions in reference to wings. V. -- Clark Y biplane cellule -- N.A.C.A. cowled nacelle -- tractor propeller, by E. Floyd Valentine [No. 506], p. 603
Tests of nacelle-propeller combinations in various positions with reference to wings. VI. -- Wings and nacelles with pusher propeller, by Donald H. Wood and Carlton Bioletti [No. 507], p. 619
The aerodynamic effects of wing cut-outs, by Albert Sherman [No. 480], p. 117
The drag of airplane wheels, wheel fairings, and landing gears-I, by William H. Herrnstein, Jr. and David Biermann [No. 485], p. 193
The effect of spray strips on the take-off performance of a model of a flying boat hull, by Starr Truscott [No. 503], p. 523
The influence of tip shape on the wing-load distribution as determined by flight tests, by Richard V. Rhode [No. 500], p. 479
The physical effects of detonation in a closed cylindrical chamber, by C.S. Draper [No. 493], p. 361
The weathering of aluminum alloy sheet materials used in aircraft, by Willard Mutchler [No. 490], p. 285
Vibration response of airplane structures, by T. Theodorsen and A.G. Gelalles [No. 491], p. 319
Wind tunnel research comparing lateral control devices, particularly at high angles of attack. XII. -- Upper surface ailerons on wings with split flaps, by Fred E. Weick and Carl J. Wenzinger [No. 499], p. 463
Wing pressure distribution and rotor-blade motion of an autogiro as determined in flight, by John B. Wheatley [No. 475], p. 43
Wing-fuselage interference, tail buffeting, and air flow about the tail of a low-wing monoplane, by James A. White and Manley J. Hood [No. 482], p. 143
Working charts for the determination of propeller thrust at various air speeds, by Edwin P. Hartman [No. 481], p. 123
© 2007 by NewsBank, Inc. All rights reserved

Nur in Feld suchen:

Zuletzt gesuchte Begriffe: