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Abramson, Andrew E. [Other] ; Adams, Gaynor J. [Other] ; Bergrun, Norman R. [Other] ; Berman, Julian H. [Other] ; Bisson, Edmond E. [Other] ; Boksenbom, Aaron S. [Other] ; Brown, B. Porter [Other] ; Brown, W. Byron [Other] ; Bryson, Arthur Earl [Other] ; Budinger, Ray E. [Other] ; Campbell, John P. [Other] ; Carpenter, Paul J. [Other] ; Chapman, Dean R. [Other] ; Chilton, Robert G. [Other] ; Costello, George R. [Other] ; Creager, Marcus O. [Other] ; Cummings, Robert L. [Other] ; DeYoung, John [Other] ; Dhawan, S. [Other] ; Roshko, A. [Other] ; Sehy, Albert A. [Other] ; Ginsburg, Ambrose [Other] ; Ferri, Antonio [Other] ; Holms, Arthur G. [Other] ; [...] ; United States, Congress, Senate [Author] ; United States, President (1945-1953 : Truman) [Other] ; United States, National Advisory Committee for Aeronautics [Other]

Thirty-eighth annual report of the National Advisory Committee for Aeronautics 1952. Including technical reports Nos. 1059 to 1110

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  • Media type: E-Book
  • Title: Thirty-eighth annual report of the National Advisory Committee for Aeronautics 1952. Including technical reports Nos. 1059 to 1110
  • Contributor: Abramson, Andrew E. [Other] ; Adams, Gaynor J. [Other] ; Bergrun, Norman R. [Other] ; Berman, Julian H. [Other] ; Bisson, Edmond E. [Other] ; Boksenbom, Aaron S. [Other] ; Brown, B. Porter [Other] ; Brown, W. Byron [Other] ; Bryson, Arthur Earl [Other] ; Budinger, Ray E. [Other] ; Campbell, John P. [Other] ; Carpenter, Paul J. [Other] ; Chapman, Dean R. [Other] ; Chilton, Robert G. [Other] ; Costello, George R. [Other] ; Creager, Marcus O. [Other] ; Cummings, Robert L. [Other] ; DeYoung, John [Other] ; Dhawan, S. [Other] ; Roshko, A. [Other] ; Sehy, Albert A. [Other] ; Ginsburg, Ambrose [Other] ; Ferri, Antonio [Other] ; Holms, Arthur G. [Other] ; Goldstein, Arthur W. [Other] ; Mager, Artur [Other] ; Milwitzky, Benjamin [Other] ; Kaplan, Carl [Other] ; Watkins, Charles E. [Other] ; Mathews, Charles W. [Other] ; Wagoner, Cleo B. [Other] ; Talmadge, Donald B. [Other] ; Hewes, Donald E. [Other] ; Dugan, Duane W. [Other] ; Macks, E. Fred [Other] ; Fuller, Franklyn B. [Other] ; Griffith, George E. [Other] ; Kinney, George R. [Other] ; Westrick, Gertrude C. [Other] ; Goodwin, Glen [Other] ; Dugger, Gordon L. [Other] ; Liepmann, H.W. [Other] ; Runyan, Harry L. [Other] ; Truman, Harry S. [Other] ; Lomax, Harvard [Other] ; Hubbard, Harvey H. [Other] ; Pearson, Henry A. [Other] ; Goodman, I.A. [Other] ; Fischel, Jack [Other] ; Stalder, Jackson R. [Other] ; Lichtenstein, Jacob H. [Other] ; Whitten, James B. [Other] ; Sivell, James C. [Other] ; Donegan, James J. [Other] ; Duberg, John E. [Other] ; Mahoney, John J. [Other] ; Sloop, John L. [Other] ; Livingood, John N.B. [Other] ; Hagerman, John R. [Other] ; Hamrick, Joseph T. [Other] ; Merten, Kenneth F. [Other] ; Lassiter, Leslie W. [Other] ; Sluder, Loma [Other] ; Nucci, Louis M. [Other] ; Habel, Louis W. [Other] ; Miller, Mason F. [Other] ; Heaslet, Max A. [Other] ; Swikert, Max A. [Other] ; Van Dyke, Milton D. [Other] ; Gossard, Myron L. [Other] ; Hunter, Paul A. [Other] ; Wise, Paul H. [Other] ; Klebanoff, Philip S. [Other] ; Hood, Richard [Other] ; Kester, Robert H. [Other] ; Halfman, Robert L. [Other] ; Johnson, Robert L. [Other] ; Miller, Robert W. [Other] ; Naeseth, Rodger L. [Other] ; Vincenti, Walter G. [Other] ; Osborn, Walter M. [Other] ; O'Hare, William M. [Other] ; Wimbrow, William R. [Other] ; Diehl, Z.W. [Other] ; Nemeth, Zolton N. [Other] ; Wilder, Thomas W. [Other] ; Sinnette, John T. [Other] ; McKinney, Marion O. [Other] ; Michael, William H. [Other]
  • Corporation: United States, Congress, Senate [Author] ; United States, President (1945-1953 : Truman) [Other] ; United States, National Advisory Committee for Aeronautics [Other]
  • Published: Washington, DC, 1953
    Online-Ausg., Chester, Vt: NewsBank, inc, 2008
  • Published in: United States congressional serial set ; serial set no. 11676
    Senate document / 83rd Congress, 1st session. Senate ; no. 1
  • Extent: Online-Ressource (1199 p); illustrations, tables
  • Language: English
  • Reproduction series: U.S. Congressional Serial Set, 1817-1980
  • Type of reproduction: Online-Ausg.
  • Place of reproduction: Chester, Vt: NewsBank, inc, 2008
  • Origination:
  • Footnote: 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
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