Format:
Online-Ressource (750 p)
,
illustrations, tables
Edition:
Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
Series Statement:
United States congressional serial set serial set no. 10174
Note:
A study of two-control operation of an airplane, by Robert T. Jones [No. 579], p. 73
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A theory of primary failure of straight centrally loaded columns, by Eugene E. Lundquist and Claude M. Fligg [No. 582], p. 141
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Air propellers in yaw, by E.P. Lesley, George F. Worley, and Stanley Moy [No. 597], p. 459
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Airfoil section characteristics as affected by variations of the Reynolds number, by Eastman N. Jacobs and Albert Sherman [No. 586], p. 227
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Alternating-current equipment for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. [No. 598], p. 475
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An analysis of lateral stability in power-off flight with charts for use in design, by Charles H. Zimmerman [No. 589], p. 297
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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
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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
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Appendix, p. 159
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Blower cooling of finned cylinders, by Oscar W. Schey and Herman H. Ellerbrock, Jr. [No. 587], p. 269
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Characteristics of six propellers including the high-speed range, by Theodore Theodorsen, George W. Stickle, and M.J. Brevoort [No. 594], p. 401
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Cooling of airplane engine at low air speeds, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 593], p. 391
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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
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Electrical thermometers for aircraft, by John B. Peterson and S.H.J. Womack [No. 606], p. 633
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Experimental investigation of wind-tunnel interference on the down wash behind an airfoil, by Abe Silverstein and S. Katzoff [No. 609], p. 689
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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
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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
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Fuel spray and flame formation in a compression-ignition engine employing airflow, by A.M. Rothrock and C.D. Waldron [No. 588], p. 281
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Full-scale tests of N.A.C.A. cowlings, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 592], p. 361
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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
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Heat transfer to fuel sprays injected into heated gases, by Robert F. Selden and Robert C. Spencer [No. 580], p. 91
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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
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Prechamber compression-ignition engine performance, by Charles S. Moore and John H. Collins, Jr. [No. 577], p. 49
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Pressure distribution measurements of an 0-2H airplane in flight, by H.A. Pearson [No. 590], p. 319
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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
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Resume and analysis of N.A.C.A. lateral control research, by Fred E. Weick and Robert T. Jones [No. 605], p. 605
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Span load distribution for tapered wings with partial-span flaps, by H.A. Pearson [No. 585], p. 209
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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
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Strength of welded aircraft joints, by W.C. Brueggeman [No. 584], p. 177
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Stress analysis of beams with shear deformation of the flanges, by Paul Kuhn [No. 608], p. 669
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Table of contents, p. III
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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
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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
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Torsion tests of tubes, by Ambrose H. Stang, Walter Ramberg, and Goldie Back [No. 601], p. 515
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Wind-tunnel and flight tests of slot-lip ailerons, by Joseph A. Shortal [No. 563], p. 537
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Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps, by Carl J. Wenzinger [No. 611], p. 733
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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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