Twenty-third annual report of the National Advisory Committee for Aeronautics, 1937. Including technical reports Nos. 577 to 611

Medientyp: E-Book

Titel: Twenty-third annual report of the National Advisory Committee for Aeronautics, 1937. Including technical reports Nos. 577 to 611

Körperschaft: United States, National Advisory Committee for Aeronautics

Erschienen: Washington, DC, 1937
Online-Ausg., Chester, Vt: NewsBank, inc, 2007

Umfang: Online-Ressource (750 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 study of two-control operation of an airplane, by Robert T. Jones [No. 579], p. 73
A theory of primary failure of straight centrally loaded columns, by Eugene E. Lundquist and Claude M. Fligg [No. 582], p. 141
Air propellers in yaw, by E.P. Lesley, George F. Worley, and Stanley Moy [No. 597], p. 459
Airfoil section characteristics as affected by variations of the Reynolds number, by Eastman N. Jacobs and Albert Sherman [No. 586], p. 227
Alternating-current equipment for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. [No. 598], p. 475
An analysis of lateral stability in power-off flight with charts for use in design, by Charles H. Zimmerman [No. 589], p. 297
An analysis of the factors that determine the periodic twist of an autogiro rotor blade, with a comparison of predicted and measured results, by John B. Wheatley [No. 600], p. 503
An analytical and experimental study of the effect of periodic blade twist on the thrust torque, and flapping motion of an autogiro rotor, by John B. Wheatley [No. 591], p. 353
Appendix, p. 159
Blower cooling of finned cylinders, by Oscar W. Schey and Herman H. Ellerbrock, Jr. [No. 587], p. 269
Characteristics of six propellers including the high-speed range, by Theodore Theodorsen, George W. Stickle, and M.J. Brevoort [No. 594], p. 401
Cooling of airplane engine at low air speeds, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 593], p. 391
Cooling test of a single-row radial engine with several N.A.C.A. cowlings, by M.J. Brevoort, George W. Stickle, and Herman H. Ellerbrock, Jr. [No. 596], p. 449
Electrical thermometers for aircraft, by John B. Peterson and S.H.J. Womack [No. 606], p. 633
Experimental investigation of wind-tunnel interference on the down wash behind an airfoil, by Abe Silverstein and S. Katzoff [No. 609], p. 689
Flight measurements of the dynamic longitudinal stability of several airplanes and a correlation of the measurements with pilots' observations of handling characteristics, by Hartley A. Soule [No. 578], p. 69
Flight tests of the drag and torque of the propeller in terminal-velocity dives, by Richard V. Rhode and Henry A. Pearson [No. 599], p. 493
Fuel spray and flame formation in a compression-ignition engine employing airflow, by A.M. Rothrock and C.D. Waldron [No. 588], p. 281
Full-scale tests of N.A.C.A. cowlings, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 592], p. 361
Full-scale tests of a new type N.A.C.A. nose-slot cowling, by Theodore Theodorsen, M.J. Brevoort, George W. Stickle, and M.N. Gough [No. 595], p. 439
Heat transfer to fuel sprays injected into heated gases, by Robert F. Selden and Robert C. Spencer [No. 580], p. 91
Measurements of intensity and scale of wind-tunnel turbulence and their relation to the critical Reynolds number of spheres, by Hugh L. Dryden, G.B. Schubauer, W.C. Mock, Jr., and H.K. Skramstad [No. 581], p. 109
Prechamber compression-ignition engine performance, by Charles S. Moore and John H. Collins, Jr. [No. 577], p. 49
Pressure distribution measurements of an 0-2H airplane in flight, by H.A. Pearson [No. 590], p. 319
Pressure-distribution measurements at large angles of pitch on fins of different span-chord ratio on a 1/40 scale model of the U.S. airship "Akron," by James G. McHugh [No. 604], p. 585
Resume and analysis of N.A.C.A. lateral control research, by Fred E. Weick and Robert T. Jones [No. 605], p. 605
Span load distribution for tapered wings with partial-span flaps, by H.A. Pearson [No. 585], p. 209
Spinning characteristics of the XN2Y-1 airplane obtained from the spinning balance and compared with results from the spinning tunnel and from flight tests, by M.J. Bamber and R.O. House [No. 607], p. 649
Strength of welded aircraft joints, by W.C. Brueggeman [No. 584], p. 177
Stress analysis of beams with shear deformation of the flanges, by Paul Kuhn [No. 608], p. 669
Table of contents, p. III
Tests of related forward-camber airfoils in the variable-density wind tunnel, by Eastman N. Jacobs, Robert M. Pinkerton, and Harry Greenberg [No. 610], p. 697
The rolling friction of several airplane wheels and tires and the effect of rolling friction on take-off, by J.W. Wetmore [No. 583], p. 169
Torsion tests of tubes, by Ambrose H. Stang, Walter Ramberg, and Goldie Back [No. 601], p. 515
Wind-tunnel and flight tests of slot-lip ailerons, by Joseph A. Shortal [No. 563], p. 537
Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps, by Carl J. Wenzinger [No. 611], p. 733
Wind-tunnel investigation of wings with ordinary ailerons and full-span external airfoil flaps, by Robert C. Platt and Joseph A. Shortal [No. 603], p. 563
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