Format:
Online-Ressource (1199 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. 11676
Note:
A biharmonic relaxation method for calculating thermal stress in cooled irregular cylinders, by Arthur G. Holms [No. 1059], p. 71
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A study of second-order supersonic flow theory, by Milton D. Van Dyke [No. 1081], p. 489
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A theoretical analysis of the effects of fuel motion on airplane dynamics, by Albert A. Sehy [No. 1080], p. 467
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Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow, by Charles E. Watkins and Julian H. Berman [No. 1099], p. 863
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Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow, by Dean R. Chapman [No. 1063], p. 129
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An empirically derived basis for calculating the area, rate, and distribution of water-drop impingement on airfoils, by Norman R. Bergrun [No. 1107], p. 1079
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An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer, by Arthur Earl Bryson, Jr. [No. 1094], p. 725
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An iterative transformation procedure for numerical solution of flutter and similar characteristic-value problems, by Myron L. Gossard [No. 1073], p. 303
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Analysis of temperature distribution in liquid-cooled turbine blades, by John N.B. Livingood and W. Byron Brown [No. 1066], p. 169
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Analysis of the effects of wing interference on the tail contributions to the rolling derivatives, by William H. Michael, Jr. [No. 1086], p. 569
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Automatic control systems satisfying certain general criterions on transient behavior, by Aaron S. Boksenbom and Richard Hood [No. 1068], p. 207
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Axisymmetric supersonic flow in rotating impellers, by Arthur W. Goldstein [No. 1083], p. 523
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Chordwise and compressibility corrections to slender-wing theory, by Harvard Lomax and Loma Sluder [No. 1105], p. 1049
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Comparison of high-speed operating characteristics of size 215 cylindrical-roller bearings as determined in turbojet engine and in laboratory test rig, by E. Fred Macks and Zolton N. Nemeth [No. 1084], p. 537
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Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume -- 2-alkylbiphenyl and the two isomeric 2-alkylbicyclohexyl series, by Irving A. Goodman and Paul H. Wise [No. 1065], p. 159
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Detailed computational procedure for design of cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello, Robert L. Cummings, and John T. Sinnette, Jr. [No. 1060], p. 91
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Discussion of boundary-layer characteristics near the wall of an axial-flow compressor, by Artur Mager, John J. Mahoney, and Ray E. Budinger [No. 1085], p. 549
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Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons, by Jack Fischel, Rodger L. Naeseth, John R. Hagerman, and William M. O'Hare [No. 1091], p. 649
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Effect of initial mixture temperature on flame speed of methane-air, propane-air and ethylene-air mixtures, by Gordon L. Dugger [No. 1061], p. 105
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Effects of compressibility on the performance of two full-scale helicopter rotors, by Paul J. Carpenter [No. 1078], p. 449
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Effects on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system, by Charles W. Mathews, Donald B. Talmadge, and James B. Whitten [No. 1076], p. 375
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Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow, by Robert L. Halfman [No. 1108], p. 1101
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Experimental determination of the effect of horizontal tail size, tail length, and vertical location on low-speed static longitudinal stability and damping in pitch of a model having 45 [degree] sweptback wing and tail surfaces, by Jacob H. Lichtenstein [No. 1096], p. 789
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Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities, by Dean R. Chapman, William R. Wimbrow, and Robert H. Kester [No. 1109], p. 1145
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Flight investigation a mechanical feel device in an irreversible elevator control system of a large airplane, by B. Porter Brown, Robert G. Chilton, and James B. Whitten [No. 1101], p. 919
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Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane, by John P. Campbell, Paul A. Hunter, Donald E. Hewes, and James B. Whitten [No. 1092], p. 697
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Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system, by Artur Mager [No. 1067], p. 191
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Generalized theory for seaplane impact, by Benjamin Milwitzky [No. 1103], p. 951
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Heat transfer to bodies in a high-speed rarified gas stream, by Jackson R. Stalder, Glen Goodwin and Marcus O. Creager [No. 1093]
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Hydrodynamic impact of a system with a single elastic mode. I-- Theory and generalized solution with an application to an elastic airframe, by Wilbur L. Mayo [No. 1074], p. 349
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Hydrodynamic impact of a system with a single elastic mode. II - Comparison of experimental force and response with theory, by Robert W. Miller and Kenneth F. Merton [No. 1075], p. 367
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Inelastic column behavior, by John E. Duberg and Thomas W. Wilder, III [No. 1072], p. 286
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Internal-liquid-film-cooling experiments with airstream temperatures to 2000 [degrees] F in 2- and 4- inch diameter horizontal tubes, by George R. Kinney, Andrew E. Abramson and John L. Sloop [No. 1087], p. 581
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Investigation of wear and friction properties under sliding conditions of some materials suitable for cages of rolling-contact bearings, by Robert L. Johnson, Max A. Swikert, and Edmond E. Bisson [No. 1062], p. 117
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List of technical reports, p. III
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Lubrication and cooling studies of cylindrical-roller bearings at high speeds, by E. Fred Macks and Zolton N. Nemeth [No. 1064], p. 143
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Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data, by James J. Donegan and Henry A. Pearson [No. 1070], p. 233
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Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data, by James C. Sivell and Gertrude C. Westrick [No. 1090], p. 623
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Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design, by Joseph T. Hamrick, Ambrose Ginsburg, and Walter M. Osborn [No. 1082], p. 513
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On a solution of the nonlinear differential equation for transonic flow past a wave-shaped wall, by Carl Kaplan [No. 1069], p. 221
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On reflection of shock waves from boundary layers, by H.W. Liepmann, A. Roshko and S. Dhawan [No. 1100], p. 889
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Preliminary investigation of a new type of supersonic inlet, by Antonio Ferri and Louis M. Nucci [No. 1104], p. 1029
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Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment, by Harry L. Runyan [No. 1089], p. 615
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Some features of artificially thickened fully developed turbulent boundary layers with zero pressure gradient, by P.S. Klebanoff and Z.W. Diehl [No. 1110], p. 1165
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Sound from a two-blade propeller at supersonic tip speeds, by Harvey H, Hubbard and Leslie W. Lassiter [No. 1079], p. 457
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Stresses in a two-bay noncircular cylinder under transverse loads, by George E. Griffith [No. 1097], p. 811
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Summary of methods for calculating dynamic lateral stability and response and for estimating lateral stability derivatives, by John P. Campbell and Marion O. McKinney [No. 1098], p. 823
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Table of contents, p. II
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The Langley annular transonic tunnel, by Louis W. Habel, James H. Henderson, and Mason F. Miller [No. 1106], p. 1069
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The linearized charateristics method and its application to practical nonlinear supersonic problems, by Antonio Ferri [No. 1102], p. 933
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Theoretical damping in roll and rolling moment due to differential wing incidence for slender cruciform wings and wing-body combinations, by Gaynor J. Adams and Duane W. Dugan [No. 1088], p. 603
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Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan forum at subsonic speeds, by John DeYoung [No. 1071], p. 245
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Transonic flow past a wedge profile with detached bow wave, by Walter G. Vincenti and Cleo B. Wagoner [No. 1095], p. 759
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Two- and three-dimensional unsteady lift problems in high-speed flight, by Harvard Lomax, Max A. Heaslet, Franklin B. Fuller and Loma Sluder [No. 1077], p. 393
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p. 715
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