Format:
Online-Ressource (532 p)
,
illustrations, tables
Edition:
Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980
Series Statement:
United States congressional serial set serial set no. 10576
Note:
A theoretical study of lateral stability with an automatic pilot, by Frederick H. Imlay, N.A.C.A. [No. 693], p. 273
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Aerodynamic characteristics of horizontal tail surfaces, by Abe Silverstein and S. Katzoff, N.A.C.A. [No. 688], p. 175
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Appendix, p. 80
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Correlation of cooling data from an air-cooled cylinder and several multicylinder engines, by Benjamin Pinkel and Herman H. Ellenbrock, Jr., N.A.C.A. [No. 683], p. 59
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Design charts relating to the stalling of tapered wings, by H.A. Soule and R.F. Anderson, N.A.C.A. [No. 703], p. 513
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Determination of ground effect from tests of a gilder in towed flight, by J.W. Wetmore and L.I. Turner, Jr., N.A.C.A. [No. 695], p. 295
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Effect of exit-slot position and opening on the available cooling pressure for N.A.C.A. nose-slot cowlings, by George W. Stickle, Irven Naiman, and John L. Crigler, N.A.C.A. [No. 687], p. 163
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Effect of fuel-air ratio, inlet temperature and exhaust pressure on detonation, by E.S. Taylor, W.A. Leary, and J.R. Diver, Massachusetts Institute of Technology [No. 699], p. 423
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Effective gust structure of low altitudes as determined from the reactions of an airplane, by Philip Donely, N.A.C.A. [No. 692], p. 263
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Flame speeds and energy considerations for explosions in a spherical bomb, by Ernest F. Fiock, Charles F. Marvin, Jr., Frank R. Caldwell, and Carl H. Roeder, N.A.C.A. [No. 682], p. 39
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Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. V. Effect of airplane relative density, by Oscar Seidman and A.I. Neihouse, N.A.C.A. [No. 691], p. 243
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Investigations on the incompletely developed plane diagonal-tension field, by Paul Kuhn, N.A.C.A. [No. 697], p. 387
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Longitudinal stability and control with special reference to slipstream effects, by S. Katzoff, N.A.C.A. [No. 690], p. 213
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Mechanical properties of flush-riveted joints, by W.C. Brueggeman and Frederick C. Roop, National Bureau of Standards [No. 701], p. 467
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Mechanism of flutter: A theoretical and experimental investigation of the flutter problem, by Theodore Theodorsen and I.E. Garrick, N.A.C.A. [No. 685], p. 101
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Piston temperatures in an air-cooled engine for various operating conditions, by Eugene J. Manganiello, N.A.C.A. [No. 698], p. 413
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Preliminary investigation of the flying qualities of airplanes, by H.A. Soule, N.A.C.A. [No. 700], p. 449
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Preliminary wind-tunnel investigation of an N.A.C.A. 23012 airfoil with various arrangements of Venetian-blind flaps, by Carl J. Wenzinger and Thomas A. Harris, N.A.C.A. [No. 689], p. 197
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Stability of castering wheels for aircraft landing gears, by Arthur Kantrowitz, N.A.C.A. [No. 686[, p. 147
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Static thrust and power characteristics of six full-scale propellers, by Edwin P. Hartman and David Biermann, N.A.C.A. [No. 684], p. 85
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Tensile elastic properties of typical stainless steels and nonferrous metals as affected by plastic deformation and by heat treatment, by D.J. McAdam, Jr., and R.W. Mebs, National Bureau of Standards [No. 696], p. 309
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The application of basic data on planing surfaces to the design of flying-boat hulls, by Walter S. Diehl, Bureau of Aeronautics, Navy Department [No. 694], p. 287
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The calculated effect of various hydrodynamic and aerodynamic factors on the take off of a large flying boat, by R.E. Olson and J.M. Allison, N.A.C.A. [No. 702], p. 497
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The unsteady lift of a wing of finite aspect ratio, by Robert T. Jones, N.AC.A. [No. 681), p. 31
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