Kooperativer Bibliotheksverbund

UID:

Format: II, 14 Seiten , Diagramme , 4"

Series Statement: Technical reports / National Advisory Committee for Aeronautics 1060

Language: English

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 (987 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. 11554

Note: A radar method of calibrating airspeed installations on airplanes in maneuvers at high altitudes and at transonic and supersonic speeds, by John A. Zalcovcik [No. 985], p. 661 , An analysis of supersonic aerodynamic heating with continuous fluid injection, by E.B. Klunker and H. Reese Ivey [No. 990], p. 701 , An introduction to the physical aspects of helicopter stability, by Alfred Gessow and Kenneth B. Amer [No. 993], p. 739 , Analysis of spanwise temperature distribution in three types of air-cooled turbine blade, by John N.B. Livingood and W. Byron Brown [No. 994], p. 753 , Appendices, p. 100 , Application of radial-equilibrium condition to axial-flow compressor and turbine design, by Chung-Hua Wu and Lincoln Wolfenstein [No. 955], p. 165 , Attainable circulation about airfoils in cascade, by Arthur W. Goldstein and Artur Mager [No. 953], p. 117 , Blockage corrections for three-dimensional-flow closed-throat wind tunnels, with consideration of the effect of compressibility, by John G. Herriot [No. 995], p. 771 , Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1000], p. 909 , Comparative drag measurements at transonic speeds of rectangular and sweptback NACA 65-109 airfoils mounted on a freely falling body, by Charles W. Mathews and Jim Rogers Thompson [No. 988], p. 685 , Critical stress of ring-stiffened cylinders in torsion, by Manuel Stein, J. Lyell Sanders, Jr., and Harold Crate [No. 989], p. 693 , Determination of plate compressive strengths at elevated temperatures, by George J. Heimerl and William M. Roberts [No. 960], p. 251 , Direct method of design and stress analysis of rotating disks with temperature gradient, by S.S. Manson [No. 952], p. 103 , Elastic and plastic buckling of simply supported solid-core sandwich plates in compression, by Paul Seide and Elbridge Z. Stowell [No. 967], p. 357 , Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis, by John C. Sanders and Edward C. Chapin [No. 987], p. 673 , Flight investigation of the effect of various vertical-tail modifications on the directional stability and control characteristics of a propeller-driven fighter airplane, by Harold L. Johnson [No. 973], p. 453 , Flutter of a uniform wing with an arbitrarily placed mass according to a differential-equation analysis and a comparison with experiment, by Harry L. Runyan and Charles E. Watkins [No. 966], p. 339 , Free-space oscillating pressures near the tips of rotating propellers, by Harvey H. Hubbard and Arthur A. Regier [No. 996], p. 785 , Frequency response of linear systems from transient data, by Melvin E. Laverne and Aaron S. Boksenbom [No. 977], p. 547 , Fundamental effects of aging on creep properties of solution-treated low-carbon N-155 alloy, by D.N. Frey, J.W. Freeman, and A.E. White [No. 1001], p. 939 , Further experiments on the flow and heat transfer in a heated turbulent air jet, by Stanley Corrsin and Mahinder S. Uberoi [No. 998], p. 859 , General algebraic method applied to control analysis of complex engine types, by Aaron S. Boksenbom and Richard Hood [No. 980], p. 581 , Icing-protection requirements for reciprocating-engine induction systems, by Willard D. Coles, Vern G. Rollin, and Donald R. Mulholland [No. 982], p. 611 , Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings, by Alex Goodman and Lewis R. Fisher [No. 968], p. 367 , Investigation of the NACA 4-(3)(08)-03 and NACA 4-(3)(08)-045 two-blade propellers at forward mach numbers to 0.725 to determine the effects of compressibility and solidity on performance, by John B. Delano and Lewis Feldman [No. 999], p. 877 , Investigation with an interferometer of the turbulent mixing of a free supersonic jet, by Paul B. Gooderum, George P. Wood, and Maurice J. Brevoort [No. 963], p. 289 , Laminar mixing of a compressible fluid, by Dean R. Chapman [No. 958], p. 231 , Line-vortex theory for calculation of supersonic downwash, by Harold Mirels and Rudolph C. Haefeli [No. 983], p. 635 , Linear theory of boundary effects in open wind tunnels with finite jet lengths, by S. Katzoff, Clifford S. Gardner, Leo Diesendruck, and Bertram J. Eisenstadt [No. 976], p. 509 , Linearized compressible-flow theory for sonic flight speeds, by Max A. Heaslet, Harvard Lomax, and John R. Spreiter [No. 956], p. 195 , Method for determining the frequency-response characteristics of an element or system from the system transient output response to a known input function, by Howard J. Curfman, Jr. and Robert A. Gardiner [No. 984], p. 651 , Method of designing cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello [No. 978], p. 559 , On stability of free laminar boundary layer between parallel streams, by Martin Lessen [No. 979], p. 571 , On the theory of oscillating airfoils of finite span in subsonic compressible flow, by Eric Reissner [No. 1002], p. 969 , One-dimensional flows of an imperfect diatomic gas, by A.J. Eggers [No. 959], p. 239 , Small bending and stretching of sandwich-type shells, by Eric Reissner [No. 975], p. 483 , Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip, by John D. Bird [No. 969], p. 379 , Summary of information relating to gust loads on airplanes, by Philip Donely [No. 997], p. 807 , Table of contents, p. II , The aerodynamic forces on slender plane and cruciform-wing and body combinations, by John R. Spreiter [No. 962], p. 271 , The application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory, by Max A. Heaslet and Harvard Lomax [No. 961], p. 257 , The application of the statistical theory of extreme values to gust-load problems, by Harry Press [No. 991], p. 711 , The calculation of downwash behind supersonic wings with an application to triangular plan forms, by Harvard Lomax, Loma Sluder, and Max A. Heaslet [No. 957], p. 211 , The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings, by Warren A. Tucker and Robert L. Nelson [No. 972], p. 425 , The effects of variations in Reynolds Number between 3.0 X 10 [to the sixth power] and 2.5 X 10 [to the sixth power] upon the aerodynamic characteristics of a number of NACA 6-Series airfoil sections, by Laurence K. Loftin, Jr. and William J. Bursnall [No. 964], p. 307 , The longitudinal stability of elastic swept wings at supersonic speed, by C.W. Frick and R.S. Chubb [No. 965], p. 327 , The reversibility theorem for thin airfoils in subsonic and supersonic flow, by Clinton E. Brown [No. 986], p. 669 , The supersonic axial-flow compressor, by Arthur Kantrowitz [No. 974], p. 473 , Theoretical analysis of various thrust-augmentation cycles for turbojet engines, by Bruce T. Lundin [No. 981], p. 593 , Theoretical comparison of several methods of thrust augmentation for turbojet engines, by Eldon W. Hall and E. Clinton Wilcox [No. 992], p. 727 , Theoretical lift and damping in roll and supersonic speeds of thin sweptback tapered wings with streamwise tips, subsonic leading edges, and supersonic trailing edges, by Frank S. Malvestuto, Jr., Kenneth Margolis, and Herbert S. Ribner [No. 970], p. 395 , Theoretical stability derivatives of thin sweptback wings tapered to a point with sweptback or sweptforward trailing edges for a limited range of supersonic speeds, by Frank S. Malvestuto, Jr. and Kenneth Margolis [No. 971], p. 411 , Two-dimensional compressible flow in centrifugal compressors with straight blades, by John D. Stanitz and Gaylord O. Ellis [No. 954], p. 141 , Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds, by John C. Evvard [No. 951], p. 71 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)