Kooperativer Bibliotheksverbund

UID:

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 , A study of second-order supersonic flow theory, by Milton D. Van Dyke [No. 1081], p. 489 , A theoretical analysis of the effects of fuel motion on airplane dynamics, by Albert A. Sehy [No. 1080], p. 467 , 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 , 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 , 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 , 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 , An iterative transformation procedure for numerical solution of flutter and similar characteristic-value problems, by Myron L. Gossard [No. 1073], p. 303 , Analysis of temperature distribution in liquid-cooled turbine blades, by John N.B. Livingood and W. Byron Brown [No. 1066], p. 169 , Analysis of the effects of wing interference on the tail contributions to the rolling derivatives, by William H. Michael, Jr. [No. 1086], p. 569 , Automatic control systems satisfying certain general criterions on transient behavior, by Aaron S. Boksenbom and Richard Hood [No. 1068], p. 207 , Axisymmetric supersonic flow in rotating impellers, by Arthur W. Goldstein [No. 1083], p. 523 , Chordwise and compressibility corrections to slender-wing theory, by Harvard Lomax and Loma Sluder [No. 1105], p. 1049 , 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 , 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 , 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 , 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 , 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 , 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 , Effects of compressibility on the performance of two full-scale helicopter rotors, by Paul J. Carpenter [No. 1078], p. 449 , 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 , Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow, by Robert L. Halfman [No. 1108], p. 1101 , 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 , 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 , 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 , 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 , Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system, by Artur Mager [No. 1067], p. 191 , Generalized theory for seaplane impact, by Benjamin Milwitzky [No. 1103], p. 951 , Heat transfer to bodies in a high-speed rarified gas stream, by Jackson R. Stalder, Glen Goodwin and Marcus O. Creager [No. 1093] , 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 , 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 , Inelastic column behavior, by John E. Duberg and Thomas W. Wilder, III [No. 1072], p. 286 , 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 , 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 , List of technical reports, p. III , Lubrication and cooling studies of cylindrical-roller bearings at high speeds, by E. Fred Macks and Zolton N. Nemeth [No. 1064], p. 143 , 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 , 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 , 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 , On a solution of the nonlinear differential equation for transonic flow past a wave-shaped wall, by Carl Kaplan [No. 1069], p. 221 , On reflection of shock waves from boundary layers, by H.W. Liepmann, A. Roshko and S. Dhawan [No. 1100], p. 889 , Preliminary investigation of a new type of supersonic inlet, by Antonio Ferri and Louis M. Nucci [No. 1104], p. 1029 , 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 , 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 , Sound from a two-blade propeller at supersonic tip speeds, by Harvey H, Hubbard and Leslie W. Lassiter [No. 1079], p. 457 , Stresses in a two-bay noncircular cylinder under transverse loads, by George E. Griffith [No. 1097], p. 811 , 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 , Table of contents, p. II , The Langley annular transonic tunnel, by Louis W. Habel, James H. Henderson, and Mason F. Miller [No. 1106], p. 1069 , The linearized charateristics method and its application to practical nonlinear supersonic problems, by Antonio Ferri [No. 1102], p. 933 , 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 , Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan forum at subsonic speeds, by John DeYoung [No. 1071], p. 245 , Transonic flow past a wedge profile with detached bow wave, by Walter G. Vincenti and Cleo B. Wagoner [No. 1095], p. 759 , 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 , p. 715 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (1503 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. 12180

Note: A comparative analysis of the performance of long-range hypervelocity vehicles, by Alfred J. Eggers, Jr., H. Julian Allen, and Stanford E. Neice, NACA [No. 1382], p. 1141 , A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts, by C.C. Shufflebarger, Chester B. Payne, and George L. Cahen, NACA [No. 1365], p. 669 , A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary layer transition, by Albert F. Von Doenhoff and Elmer A. Horton, NACA [No. 1349], p. 239 , A method for simulating the atmospheric entry of long-range ballistic missiles, by A.J. Eggers, Jr., NACA [No. 1378], p. 1009 , A method of computing the transient temperature of thick walls form arbitrary variation of adiabatic-wall temperature and heat-transfer coefficient, by P.R. Hill, NACA [No. 1372], p. 877 , A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures, by Elbridge Z. Stowell, NACA [No. 1343], p. 125 , A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver, by Leonard Sternfield, NACA [No. 1344], p. 131 , A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at hight supersonic speeds, by H. Julian Allen and A.J. Eggers, Jr. NACA [No. 1381], p. 1125 , A summary of preliminary investigations into the characteristics of combustion screech in ducted burners, by Lewis Laboratory Staff, NACA [No. 1384], p. 1195 , A theoretical and experimental study of planing surfaces including effects of cross section and plan form, by Charles L. Shuford, Jr., NACA [No. 1355], p. 373 , A variational theorem for creep with applications to plates and columns, by J. Lyell Sanders, Jr., Harvey G. McComb, Jr., and Floyd R. Schlechte, NACA [No. 1342], p. 117 , A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96, by Albert J. Evans and George Liner, NACA [No. 1375], p. 933 , An analysis of pressure studies and experimental and theoretical downwash and sidewash behind five pointed-tip wings at supersonic speeds, by William B. Boatright, NACA [No. 1380], p. 1067 , An experimental investigation of sting-support effects on drag and a comparison with jet effects at transonic speeds, by Maurice S. Cahn, NACA [No. 1353], p. 327 , Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses, by Richard R. Heldenfels and Louis F. Vosteen, NACA [No. 1361], p. 593 , Area-suction boundary-layer control as applied to the trailing-edge flaps of a 35 [degree] swept-wing airplane, by Woodrow L. Cook, Seth B. Anderson, and George E. Cooper, NACA [No. 1370], p. 823 , Blowing-type boundary-layer control as applied to the trailing-edge flaps of a 25 [degree] swept-wing airplane, by Mark W. Kelly, Seth B. Anderson, and Robert C. Innis, NACA [No. 1369], p. 799 , Boron and zirconium from crucible refractories in a complex heat-resistant alloy, by R.F. Decker, John P. Rowe, and J.W. Freeman, University of Michigan, [No. 1392], p. 1457 , Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine, by Leslie W. Lassiter and Robert W. Hess, NACA [No. 1367], p. 703 , Characteristics of the Langley 8-foot transonic tunnel with slotted test section, by Ray H. Wright, Virgil S. Ritchie, and Albin O. Pearson, NACA [No. 1389], p. 1297 , Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number, by Eli Reshotku and Ivan E. Beckwith, NACA [No. 1379], p. 1016 , Differential equations of motion for combined flapwise vending, chordwise bending, and torsion of twisted non-uniform rotor blades, by John C. Houbolt and George W. Brooks, NACA [No. 1346], p. 179 , Ditching investigations of dynamic models and effects of design parameters on ditching characteristics, by Lloyd J. Fisher and Edward L. Hoffman, NACA [No. 1347], p. 197 , Drag minimization for wings and bodies in supersonic flow, by Max A. Heaslet and Franklyn B. Fuller, NACA [No. 1385], p. 1213 , Effect of chord size on weight and cooling characteristics of air-cooled turbine blades, by Jack B. Esgar, Eugene F. Schum, and Arthur N. Curren, NACA [No. 1354], p. 359 , Effect of fuel variables on carbon formation in turbojet-engine combustors, by Edmund R. Jonash, Jerrold D. Wear, and William P. Cook, NACA [No. 1352], p. 309 , Elliptic cones alone and with wings at supersonic speeds, by Leland H. Jorgensen, NACA [No. 1376], p. 975 , Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw, by Lewis R. Fisher, NACA [No. 1357], p. 461 , Full-scale investigation of several jet-engine noise-reduction nozzles, by Willard D. Coles and Edmund E. Callaghan, NACA [No. 1387], p. 1249 , Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality, by B. Porter Brown, NACA [No. 1348], p. 225 , Growth of disturbances in a flame-generated shear region, by Perry L. Blackshear, Jr., NACA [No. 1360], p. 546 , Incompressible flutter characteristics of representative aircraft wings, by C.H. Wilts, California Institute of Technology, [No. 1390], p. 1385 , Investigation of a nonlinear control system, by I. Flugge-Lotz, C.F. Taylor, and H.E. Lindberg, Stanford University, [No. 1391], p. 1423 , Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, by Dean R. Chapman, Donald M. Kuehn, and Howard K. Larson, NACA [No. 1356], p. 419 , Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2, by Leland H. Jorgensen and Edward W. Perkins, NACA [No. 1371], p. 857 , Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 7.4, by Edward W. Perkins, Leland H. Jorgensen, and Simon C. Sommer, NACA [No. 1386], p. 1231 , List of technical reports, p. III , Measurement of static pressure on aircraft, by William Gracey, NACA [No. 1364], p. 643 , Measurements of free-space oscillating pressures near propellers at flight Mach numbers to 0.72, by Max C. Kurbjun and Arthur W. Vogeley, NACA [No. 1377], p. 999 , Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions, by F.B. Gustafson and Robert J. Topscott, NACA [No. 1350], p. 255 , NACA Research on slurry fuels, by M.L. Pinns, W.T. Olson, H.C. Barnett, and R. Breitwieser, NACA [No. 1388], p. 1273 , On flow of electrically conducting fluids over a flat plate in presence of a transverse magnetic field, by Vernon J. Rossow, NACA [No. 1358], p. 489 , Origin and prevention of crash fires in turbojet aircraft, by I. Irving Pinkel, Solomon Weiss, G. Merritt Preston, and Gerard J. Pesman, NACA [No. 1363], p. 623 , Survey of hydrogen combustion properties, by Isadore L. Drell and Frank E. Belles, NACA [No. 1383], p. 1161 , Systemic two-dimensional cascade tests of NACA 65-Series compressor blades at low speeds, by James C. Emery, L. Joseph Herrig, John R. Erwin, and A. Richard Felix, NACA [No. 1368], p. 713 , Table of contents, p. II , The mechanism of thermal-gradient mass transfer in the sodium hydroxide - nickel system, by Charles E. May, NACA [No. 1366], p. 683 , The response of an airplane to random atmospheric disturbances, by Franklin W. Diederich, NACA [No. 1345], p. 142 , The similarity rules for second-order subsonic and supersonic flow, by Milton D. Van Dyke, NACA [No. 1374], p. 925 , Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus- and liner cross-sectional areas, by Charles C. Graves and Jack S. Grobman, NACA [No. 1373], p. 899 , Theoretical combustion performance of several high-energy fuels for ramjet engines, by Leonard K. Tower, Roland Breitwieser, and Benson E. Gammon, NACA [No. 1362], p. 605 , Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades, by Robert P. Coleman and Arnold M. Feingold, NACA [No. 1351], p. 267 , Thin airfoil theory based on approximate solution of the transonic flow equation, by John R. Spreiter and Alberta Y. Alksne, NACA [No. 1359], p. 509 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)