Thirty-sixth annual report of the National Advisory Committee for Aeronautics, 1950. Including technical reports Nos. 951 to 1002

Medientyp: E-Book

Titel: Thirty-sixth annual report of the National Advisory Committee for Aeronautics, 1950. Including technical reports Nos. 951 to 1002

Körperschaft: United States, National Advisory Committee for Aeronautics

Erschienen: Washington, DC, 1951
Online-Ausg., Chester, Vt: NewsBank, inc, 2008

Umfang: Online-Ressource (987 p); illustrations, tables

Sprache: Englisch

Reproduktionsreihe: U.S. Congressional Serial Set, 1817-1980

Art der Reproduktion: Online-Ausg.

Hersteller der Reproduktion: Chester, Vt: NewsBank, inc, 2008

Entstehung:

Anmerkungen: 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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