TY - GEN

AU - United States Congress House

AU - United States National Advisory Committee for Aeronautics

AU - Amer, Kenneth B.

AU - Bird, John D.

AU - Boksenbom, Aaron S.

AU - Brevoort, Maurice J.

AU - Brown, Byron W.

AU - Brown, Clinton E.

AU - Bursnall, William J.

AU - Chapin, Edward C.

AU - Chapman, Dean R.

AU - Chubb, R.S

AU - Coles, Willard D.

AU - Corrsin, Stanley

AU - Costello, George R.

AU - Crate, Harold

AU - Curfman, Howard J.

AU - Delano, John B.

AU - Diederich, Franklin W.

AU - Diesendruck, Leo

AU - Donely, Philip

AU - White, A.E

AU - Eggers, A.J

AU - Goodman, Alex

AU - Gessow, Alfred

AU - Kantrowitz, Arthur

AU - Regier, Arthur A.

AU - Goldstein, Arthur W.

AU - Mager, Artur

AU - Eisenstadt, Bertram J.

AU - Lundin, Bruce T.

AU - Frick, C.W

AU - Watkins, Charles E.

AU - Mathews, Charles W.

AU - Wu, Chung-Hua

AU - Gardner, Clifford S.

AU - Frey, D.N

AU - Mulholland, Donald R.

AU - Wilcox, E. Clinton

AU - Klunker, E.B

AU - Stowell, Elbridge Z.

AU - Hall, Eldon W.

AU - Reissner, Eric

AU - Ellis, Gaylord O.

AU - Heimerl, George J.

AU - Wood, George P.

AU - Ivey, H. Reese

AU - Mirels, Harold

AU - Johnson, Harold L.

AU - Press, Harry

AU - Runyan, Harry L.

AU - Lomax, Harvard

AU - Hubbard, Harvey H.

AU - Ribner, Herbert S.

AU - Thompson, Jim Rogers

AU - Zalcovcik, John A.

AU - Evvard, John C.

AU - Sanders, John C.

AU - Stanitz, John D.

AU - Herriot, John G.

AU - Livingood, John N.B

AU - Spreiter, John R.

AU - Freeman, John W.

AU - Margolis, Kenneth

AU - Feldman, Lewis

AU - Fisher, Lewis R.

AU - Wolfenstein, Lincoln

AU - Sluder, Loma

AU - Uberoi, Mahinder S.

AU - Stein, Manuel

AU - Lessen, Martin

AU - Heaslet, Max A.

AU - Laverne, Melvin E.

AU - Seide, Paul

AU - Gooderum, Paul B.

AU - Hood, Richard

AU - Gardiner, Robert A.

AU - Nelson, Robert L.

AU - Haefeli, Rudolph C.

AU - Katzoff, S.

AU - Manson, S.S

AU - Rollin, Vern Gordon

AU - Tucker, Warren A.

AU - Roberts, William M.

AU - Malvestuto, Frank S.

AU - Sanders, J. Lyell

AU - Loftin, Laurence K.

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

PY - 1951

N2 - 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

N2 - An analysis of supersonic aerodynamic heating with continuous fluid injection, by E.B. Klunker and H. Reese Ivey [No. 990], p. 701

N2 - An introduction to the physical aspects of helicopter stability, by Alfred Gessow and Kenneth B. Amer [No. 993], p. 739

N2 - 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

N2 - Appendices, p. 100

N2 - Application of radial-equilibrium condition to axial-flow compressor and turbine design, by Chung-Hua Wu and Lincoln Wolfenstein [No. 955], p. 165

N2 - Attainable circulation about airfoils in cascade, by Arthur W. Goldstein and Artur Mager [No. 953], p. 117

N2 - 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

N2 - Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1000], p. 909

N2 - 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

N2 - Critical stress of ring-stiffened cylinders in torsion, by Manuel Stein, J. Lyell Sanders, Jr., and Harold Crate [No. 989], p. 693

N2 - Determination of plate compressive strengths at elevated temperatures, by George J. Heimerl and William M. Roberts [No. 960], p. 251

N2 - Direct method of design and stress analysis of rotating disks with temperature gradient, by S.S. Manson [No. 952], p. 103

N2 - Elastic and plastic buckling of simply supported solid-core sandwich plates in compression, by Paul Seide and Elbridge Z. Stowell [No. 967], p. 357

N2 - 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

N2 - 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

N2 - 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

N2 - Free-space oscillating pressures near the tips of rotating propellers, by Harvey H. Hubbard and Arthur A. Regier [No. 996], p. 785

N2 - Frequency response of linear systems from transient data, by Melvin E. Laverne and Aaron S. Boksenbom [No. 977], p. 547

N2 - 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

N2 - 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

N2 - General algebraic method applied to control analysis of complex engine types, by Aaron S. Boksenbom and Richard Hood [No. 980], p. 581

N2 - Icing-protection requirements for reciprocating-engine induction systems, by Willard D. Coles, Vern G. Rollin, and Donald R. Mulholland [No. 982], p. 611

N2 - 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

N2 - 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

N2 - 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

N2 - Laminar mixing of a compressible fluid, by Dean R. Chapman [No. 958], p. 231

N2 - Line-vortex theory for calculation of supersonic downwash, by Harold Mirels and Rudolph C. Haefeli [No. 983], p. 635

N2 - 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

N2 - Linearized compressible-flow theory for sonic flight speeds, by Max A. Heaslet, Harvard Lomax, and John R. Spreiter [No. 956], p. 195

N2 - 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

N2 - Method of designing cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello [No. 978], p. 559

N2 - On stability of free laminar boundary layer between parallel streams, by Martin Lessen [No. 979], p. 571

N2 - On the theory of oscillating airfoils of finite span in subsonic compressible flow, by Eric Reissner [No. 1002], p. 969

N2 - One-dimensional flows of an imperfect diatomic gas, by A.J. Eggers [No. 959], p. 239

N2 - Small bending and stretching of sandwich-type shells, by Eric Reissner [No. 975], p. 483

N2 - Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip, by John D. Bird [No. 969], p. 379

N2 - Summary of information relating to gust loads on airplanes, by Philip Donely [No. 997], p. 807

N2 - Table of contents, p. II

N2 - The aerodynamic forces on slender plane and cruciform-wing and body combinations, by John R. Spreiter [No. 962], p. 271

N2 - 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

N2 - The application of the statistical theory of extreme values to gust-load problems, by Harry Press [No. 991], p. 711

N2 - 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

N2 - 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

N2 - 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

N2 - The longitudinal stability of elastic swept wings at supersonic speed, by C.W. Frick and R.S. Chubb [No. 965], p. 327

N2 - The reversibility theorem for thin airfoils in subsonic and supersonic flow, by Clinton E. Brown [No. 986], p. 669

N2 - The supersonic axial-flow compressor, by Arthur Kantrowitz [No. 974], p. 473

N2 - Theoretical analysis of various thrust-augmentation cycles for turbojet engines, by Bruce T. Lundin [No. 981], p. 593

N2 - Theoretical comparison of several methods of thrust augmentation for turbojet engines, by Eldon W. Hall and E. Clinton Wilcox [No. 992], p. 727

N2 - 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

N2 - 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

N2 - Two-dimensional compressible flow in centrifugal compressors with straight blades, by John D. Stanitz and Gaylord O. Ellis [No. 954], p. 141

N2 - Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds, by John C. Evvard [No. 951], p. 71

BT - United States congressional serial set ; serial set no. 11554

BT - House document / 82nd Congress, 1st session. House ; no. 48

CY - Washington, DC

UR - http://slubdd.de/katalog?TN_libero_mab2

ER -