• Media type: E-Book
  • Title: Thirty-sixth annual report of the National Advisory Committee for Aeronautics, 1950. Including technical reports Nos. 951 to 1002
  • Contributor: Amer, Kenneth B. [Other]; Bird, John D. [Other]; Boksenbom, Aaron S. [Other]; Brevoort, Maurice J. [Other]; Brown, Byron W. [Other]; Brown, Clinton E. [Other]; Bursnall, William J. [Other]; Chapin, Edward C. [Other]; Chapman, Dean R. [Other]; Chubb, R.S. [Other]; Coles, Willard D. [Other]; Corrsin, Stanley [Other]; Costello, George R. [Other]; Crate, Harold [Other]; Curfman, Howard J. [Other]; Delano, John B. [Other]; Diederich, Franklin W. [Other]; Diesendruck, Leo [Other]; Donely, Philip [Other]; White, A.E. [Other]; Eggers, A.J. [Other]; Goodman, Alex [Other]; Gessow, Alfred [Other]; Kantrowitz, Arthur [Other]; Regier, Arthur A. [Other]; Goldstein, Arthur W. [Other]; Mager, Artur [Other]; Eisenstadt, Bertram J. [Other]; Lundin, Bruce T. [Other]; Frick, C.W. [Other]; Watkins, Charles E. [Other]; Mathews, Charles W. [Other]; Wu, Chung-Hua [Other]; Gardner, Clifford S. [Other]; Frey, D.N. [Other]; Mulholland, Donald R. [Other]; Wilcox, E. Clinton [Other]; Klunker, E.B. [Other]; Stowell, Elbridge Z. [Other]; Hall, Eldon W. [Other]; Reissner, Eric [Other]; Ellis, Gaylord O. [Other]; Heimerl, George J. [Other]; Wood, George P. [Other]; Ivey, H. Reese [Other]; Mirels, Harold [Other]; Johnson, Harold L. [Other]; Press, Harry [Other]; Runyan, Harry L. [Other]; Lomax, Harvard [Other]; Hubbard, Harvey H. [Other]; Ribner, Herbert S. [Other]; Thompson, Jim Rogers [Other]; Zalcovcik, John A. [Other]; Evvard, John C. [Other]; Sanders, John C. [Other]; Stanitz, John D. [Other]; Herriot, John G. [Other]; Livingood, John N.B. [Other]; Spreiter, John R. [Other]; Freeman, John W. [Other]; Margolis, Kenneth [Other]; Feldman, Lewis [Other]; Fisher, Lewis R. [Other]; Wolfenstein, Lincoln [Other]; Sluder, Loma [Other]; Uberoi, Mahinder S. [Other]; Stein, Manuel [Other]; Lessen, Martin [Other]; Heaslet, Max A. [Other]; Laverne, Melvin E. [Other]; Seide, Paul [Other]; Gooderum, Paul B. [Other]; Hood, Richard [Other]; Gardiner, Robert A. [Other]; Nelson, Robert L. [Other]; Haefeli, Rudolph C. [Other]; Katzoff, S. [Other]; Manson, S.S. [Other]; Rollin, Vern Gordon [Other]; Tucker, Warren A. [Other]; Roberts, William M. [Other]; Malvestuto, Frank S. [Other]; Sanders, J. Lyell [Other]; Loftin, Laurence K. [Other]
  • Corporation: United States, National Advisory Committee for Aeronautics
  • Published: Washington, DC, 1951
    Online-Ausg.: Chester, Vt: NewsBank, inc, 2008
  • Published in: United States congressional serial set ; serial set no. 11554
    House document / 82nd Congress, 1st session. House ; no. 48
  • Extent: Online-Ressource (987 p); illustrations, tables
  • Language: English
  • Reproductino series: U.S. Congressional Serial Set, 1817-1980
  • Type of reproduction: Online-Ausg.
  • Place of reproduction: Chester, Vt: NewsBank, inc, 2008
  • Origination:
  • Footnote: 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
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