Format:
Online-Ressource (645 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. 9802
Note:
A comparison between the theoretical and measured longitudinal stability characteristics of an airplane, by Hartley A. Soule and John B. Wheatley [No. 442], p. 53
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A flight investigation of the spinning of the NY-1 airplane with varied mass distribution and other modifications, and an analysis based on wind-tunnel tests, by Nathan F. Schudder [No. 441], p. 37
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Aircraft power-plant instruments, by Harcourt Sontag and W.G. Brombacher [No. 466], p. 447
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Airfoil section characteristics as affected by protuberances, by Eastman N. Jacobs [No. 446], p. 109
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Appendix, p. 65
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Determination of the theoretical pressure distribution for twenty airfoils, by I.E. Garrick [No. 465], p. 433
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General potential theory of arbitrary wing sections, by T. Theodorsen and I.E. Garrick [No. 452], p. 177
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Improved apparatus for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. and H.L. Dryden [No. 448], p. 131
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Increasing the air charge and scavenging the clearance volume of a compression-ignition engine, by J.S. Spanogle, C.W. Hicks, and H.H. Foster [No. 469], p. 525
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Interference on an airfoil of finite span in an open rectangular wind tunnel, by Theodore Theodoresen [No. 561], p. 355
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List of technical reports, p. VII
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Maneuverability investigation of O3U-1 observation airplane, by F.L. Thompson and H.W. Kirschbaum [No. 457], p. 263
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Negative thrust and torque characteristics of an adjustable-pitch metal propeller, by Edwin P. Hartmen [No 464], p. 421
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Nomenclature for aeronautics, by National Advisory Committee for Aeronautics [No. 474], p. 603
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Penetration and duration of fuel sprays from a pump injection system, by A.M. Rothrock and E.T. March [No. 455], p. 241
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Performance of a fuel-injection spark-ignition engine using a hydrogenated safety fuel, by Oscar W. Schey and Alfred W. Young [No. 471], p. 557
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Photomicrographic studies of fuel sprays, by Dana W. Lee and Robert C. Spencer [No. 454], p. 215
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Pressure-distribution measurements on the hull and fins of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 443], p. 67
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Relative loading on biplane wings, by Walter S. Diehl [No. 458], p. 275
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Static thrust of airplane propellers, by Walter S. Diehl [No. 447], p. 125
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Strength tests of thin-walled duralumin cylinders in compression, by Eugene E. Lundquist [No. 473], p. 585
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Tests of nacelle-propeller combinations in various positions with reference to wings. III. -- Clark Y wing -- Various radial-engine cowlings -- Tractor propeller, by Donald H. Wood [No. 462], p. 359
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The N.A.C.A. full-scale wind tunnel, by Smith J. De France [No. 459], p. 291
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The N.A.C.A. high-speed wind tunnel and tests of six propeller sections, by John Stack [No. 463], p. 399
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The N.A.C.A. tank: A high-speed towing basin for testing models of seaplane floats, by Starr Truscott [No. 470], p. 535
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The aerodynamic forces and moments exerted on a spinning model of the NY-1 airplane as measured by the spinning balance, by M.J. Bamber and C.H. Zimmerman [No. 456], p. 249
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The calculation of take-off run, by Walter S. Diehl [No. 450], p. 163
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The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel, by Eastman N. Jacobs, Kenneth E. Ward, and Robert M. Pinkerton [No. 460], p. 299
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The drag of two streamline bodies as affected by protuberances and appendages, by Ira H. Abbot [No. 451], p. 171
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The estimation of maximum load capacity of seaplanes and flying boats, by Walter S. Diehl [No. 453], p. 211
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The experimental determination of the moments of inertia of airplanes, by Hartley A. Soule and Marvel P. Miller [No. 467], p. 501
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The interference between struts in various combinations, by David Biermann and William H. Herrnstein, Jr. [No. 468], p. 515
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Wind-tunnel research comparing lateral control devices particularly at high angles of attack. VI. -- Skewed ailerons and rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 444], p. 81
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Wind-tunnel tests on combinations of a wing with fixed auxiliary airfoils having various chords and profiles, by Fred E. Weick and Robert Sanders [No. 472], p. 567
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Wing characteristics as affected by protuberances of short span, by Eastman N. Jacobs and Albert Sherman [No. 449], p. 155
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Working charts for the determination of the lift distribution between biplane wings, by Paul Kuhn [No. 445], p. 93
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