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
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An analysis of supersonic aerodynamic heating with continuous fluid injection, by E.B. Klunker and H. Reese Ivey [No. 990], p. 701
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An introduction to the physical aspects of helicopter stability, by Alfred Gessow and Kenneth B. Amer [No. 993], p. 739
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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
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Appendices, p. 100
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Application of radial-equilibrium condition to axial-flow compressor and turbine design, by Chung-Hua Wu and Lincoln Wolfenstein [No. 955], p. 165
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Attainable circulation about airfoils in cascade, by Arthur W. Goldstein and Artur Mager [No. 953], p. 117
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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
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Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1000], p. 909
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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
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Critical stress of ring-stiffened cylinders in torsion, by Manuel Stein, J. Lyell Sanders, Jr., and Harold Crate [No. 989], p. 693
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Determination of plate compressive strengths at elevated temperatures, by George J. Heimerl and William M. Roberts [No. 960], p. 251
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Direct method of design and stress analysis of rotating disks with temperature gradient, by S.S. Manson [No. 952], p. 103
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Elastic and plastic buckling of simply supported solid-core sandwich plates in compression, by Paul Seide and Elbridge Z. Stowell [No. 967], p. 357
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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
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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
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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
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Free-space oscillating pressures near the tips of rotating propellers, by Harvey H. Hubbard and Arthur A. Regier [No. 996], p. 785
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Frequency response of linear systems from transient data, by Melvin E. Laverne and Aaron S. Boksenbom [No. 977], p. 547
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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
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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
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General algebraic method applied to control analysis of complex engine types, by Aaron S. Boksenbom and Richard Hood [No. 980], p. 581
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Icing-protection requirements for reciprocating-engine induction systems, by Willard D. Coles, Vern G. Rollin, and Donald R. Mulholland [No. 982], p. 611
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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
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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
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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
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Laminar mixing of a compressible fluid, by Dean R. Chapman [No. 958], p. 231
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Line-vortex theory for calculation of supersonic downwash, by Harold Mirels and Rudolph C. Haefeli [No. 983], p. 635
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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
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Linearized compressible-flow theory for sonic flight speeds, by Max A. Heaslet, Harvard Lomax, and John R. Spreiter [No. 956], p. 195
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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
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Method of designing cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello [No. 978], p. 559
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On stability of free laminar boundary layer between parallel streams, by Martin Lessen [No. 979], p. 571
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On the theory of oscillating airfoils of finite span in subsonic compressible flow, by Eric Reissner [No. 1002], p. 969
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One-dimensional flows of an imperfect diatomic gas, by A.J. Eggers [No. 959], p. 239
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Small bending and stretching of sandwich-type shells, by Eric Reissner [No. 975], p. 483
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Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip, by John D. Bird [No. 969], p. 379
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Summary of information relating to gust loads on airplanes, by Philip Donely [No. 997], p. 807
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Table of contents, p. II
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The aerodynamic forces on slender plane and cruciform-wing and body combinations, by John R. Spreiter [No. 962], p. 271
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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
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The application of the statistical theory of extreme values to gust-load problems, by Harry Press [No. 991], p. 711
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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
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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
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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
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The longitudinal stability of elastic swept wings at supersonic speed, by C.W. Frick and R.S. Chubb [No. 965], p. 327
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The reversibility theorem for thin airfoils in subsonic and supersonic flow, by Clinton E. Brown [No. 986], p. 669
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The supersonic axial-flow compressor, by Arthur Kantrowitz [No. 974], p. 473
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Theoretical analysis of various thrust-augmentation cycles for turbojet engines, by Bruce T. Lundin [No. 981], p. 593
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Theoretical comparison of several methods of thrust augmentation for turbojet engines, by Eldon W. Hall and E. Clinton Wilcox [No. 992], p. 727
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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
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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
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Two-dimensional compressible flow in centrifugal compressors with straight blades, by John D. Stanitz and Gaylord O. Ellis [No. 954], p. 141
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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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