UID:
(DE-602)gbv_754648338
Format:
Online-Ressource (1238 p)
,
illustrations, maps, 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. 11762
Note:
A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory, by Clarence W. Matthews [No. 1155], p. 1125
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A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by the use of accelerometer and attitude-angle measurements, by John A. Zaloveik, Lindsay J. Lina, and James P. Trant, Jr. [No. 1145], p. 899
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A special investigation to develop a general method for three-dimensional photoelastic stress analysis, by M.M. Frocht and R. Guernsey, Jr. [No. 1148], p. 963
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A study of elastic and plastic stress concentration factors due to notches and fillets in flat plates, by Herbert F. Hardrath and Lachlan Ohman [No. 1117], p. 213
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A study of inviscid flow about airfoils at high supersonic speeds, by A.J. Eggers, Jr., Clarence A. Syvertson, and Samuel Kraus [No. 1123], p. 339
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A thermodynamic study of the turbine-propeller engine, by Benjamin Pinkel and Irving M. Karp [No. 1114], p. 117
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A vector study of linearized supersonic flow applications to nonplanar problems, by John C. Martin [No. 1143], p. 845
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Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes, by John M. Riebe and Rodger L. Naeseth [No. 1144], p. 879
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Aerodynamic forces and loadings on symmetrical circular-arc airfoils with plain leading-edge and plain trailing-edge flaps, by Jones F. Cahill, William J. Underwood, Robert J. Nuber, and Gail A. Cheesman [No. 1146], p. 913
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An analysis of laminar free-convection flow and heat transfer about a flat plate parallel to the direction of the generating body force, by Simon Ostrach [No. 1111], p. 63
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Analysis of landing-gear behavior, by Benjamin Milwitzky and Francis E. Cook [No. 1154], p. 1077
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Analytical derivation and experimental evaluation of short-bearing approximation for full journal bearings, by George B. DuBois and Fred W. Ocvirk [No. 1157], p. 1199
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Appendices, p. 72
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Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90 [degree] of turning, by John D. Stanitz and Leonard J. Sheldrake [No. 1116], p. 193
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Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed, by Herbert C. Nelson and Julian H. Berman [No. 1128], p. 469
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Charts and approximate formulas for the estimation of aeroelastic effects on the lateral control of swept and unswept wings, by Kenneth A. Foss and Franklin W. Diederich [No. 1139], p. 715
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Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings, by Franklin W. Diederich and Kenneth A. Foss [No. 1140], p. 743
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Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow, by Harry L. Runyan and Charles E. Watkins [No. 1150], p. 993
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Deflection and stress analysis of thin solid wings of arbitrary plan form with particular reference to delta wings, by Manuel Stein, J. Edward Anderson, and John M. Hedgepeth [No. 1131], p. 513
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Design of two-dimensional channels with prescribed velocity distributions along the channel walls, by John D. Stanitz [No. 1115], p. 153
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Diffusion of heat from a line source in isotropic turbulence, by Mahinder S. Uberoi and Stanley Corrsin [No. 1142}, p. 815
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Direct measurements of skin friction, by Satish Dhawan [No. 1121], p. 281
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Displacement effect of a three-dimensional boundary layer, by Franklin K. Moore [No. 1124], p. 367
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Dynamics of mechanical feedback-type hydraulic servomotors under inertia loads, by Harold Gold, Edward W. Otto, and Victor L. Ransom [No. 1125], p. 373
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Equations, tables, and charts for compressible flow, by Ames Research staff [No. 1135], p. 611
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Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers, by Ralph W. Stone, Jr. [No. 1136], p. 683
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Experiments to determine neighborhood reactions to light airplanes with and without external noise reduction, by Fred S. Elwell [No. 1156], p. 1155
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Hydrocarbon and nonhydrocarbon derivatives of cyclopropane, by Vernon A. Slabey, Paul H. Wise, and Louis C. Gibbons [No. 1112], p. 81
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Initial results of instrument-flying trials conducted in a single-rotor helicopter, by Almer D. Crim, John P. Reeder, and James B. Whitten [No. 1137], p. 695
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Laminar boundary layer on cone in supersonic flow at large angle of attack, by Franklin K. Moore [No. 1132], p. 533
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List of technical reports, p. III
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Mechanism of start and development of aircraft crash fires, by I. Irving Pinkel, G. Merritt Preston and Gerard J. Pesman [No. 1133], p. 546
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Method and graphs for the evaluation of air-induction systems, by George B. Brajinikoff [No. 1141], p. 793
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Method for calculation of laminar heat transfer in air flow around cylinders of arbitrary cross section (including large temperature differences and transpirational cooling), by E.R.G. Eckert and John N.B. Livingood [No. 1118], p. 223
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On the application of transonic similarity rules to wings of finite span, by John R. Spreiter [No. 1153], p. 1055
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On transonic flow past a wave-shaped wall, by Carl Kaplan [No. 1149], p. 981
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One-dimensional analysis of choked-flow turbines, by Robert E. English and Richard H. Cavicchi [No. 1127], p. 451
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Photographic investigation of combustion in a two-dimensional transparent rocket engine, by Donald R. Bellman, Jack C. Humphrey and Theodore Male [No. 1134], p. 599
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Reciprocity relations in aerodynamics, by Max A. Heaslet and John R. Spreiter [No. 1119], p. 253
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Relative importance of various sources of defect-producing hydrogen introduced into steel during application of vitreous coatings, by Dwight G. Moore, Mary A. Mason, and William N. Harrison [No. 1120], p. 269
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Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw, by John D. Bird, Lewis R. Fisher, and Sadie M. Hubbard [No. 1130], p. 495
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Spectrum of turbulence in a contracting stream, by H.S. Ribner and M. Tucker [No. 1113], p. 99
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Study of inadvertent speed increases in transport operation, by Henry A. Pearson [No. 1138], p. 703
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Survey of portions of the chromium-cobalt-nickel- molybdenum quaternary system at 1200 [degrees] C., by Sheldon Paul Rideout and Paul A. Beck [No. 1122], p. 301
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Table of contents, p. II
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The effect of blade-section thickness ratios on the aerodynamic characteristics of related full-scale propellers at mach numbers up to 0.65, by Julian D. Maynard and Seymour Steinberg [No. 1126], p. 395
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The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives, by Robert O. Schade and James L. Hassell, Jr. [No. 1151], p. 1001
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The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight, by Frank M. Hamaker, Stanford E. Neice, and Thomas J. Wong [No. 1147], p. 951
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Theory and procedure for determining loads and motions in chine-immersed hydrodynamic impacts of prismatic bodies, by Emanuel Schnitzer [No. 1152], p. 1025
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Transverse vibrations of hollow thin-walled cylindrical beams, by Bernard Budiansky and Edwin T. Kruszewski [No. 1129], p. 485
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