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Search without synonyms: title: National Advisory Committee for Aeronautics -- Reports

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    National Advisory Committee for Aeronautics | TIBKAT

    National Advisory Committee for Aeronautics, NACA - University Conference on Aerodynamics

    Engineering Index Backfile | 1948
    , and orienting reference material for further study; supersonics, stability and control, and wing characteristics considered. Eng Soc Lib, NY. ...
    Publisher: Durand Reprinting Committee, California Institute of Technology

    Aerodynamic characteristics of airfoils / by National Advisory Committee for Aeronautics ; 3

    TIBKAT | 1923

    The variable density wind tunnel of the national advisory committee for aeronautics

    Munk, M.M. / Miller, E.W. | Engineering Index Backfile | 1926
    Publisher: National Advisory Committee for Aeronautics

    Aerodynamic characteristics of airfoils / by National Advisory Committee for Aeronautics ; 4: Continuation of reports Nos. 93, 124, and 182

    TIBKAT | 1926

    The variable density wind tunnel of the National Advisory Committee for Aeronautics : [part 1 und 2]

    Munk, Max M. / Miller, Elton W. | TIBKAT | 1925

    Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics

    Munk, Max M. | TIBKAT | 1925

    Nomenclature for aeronautics

    Engineering Index Backfile | 1920
    Nomenclature and list of symbols approved by Executive Committee of National Advisory Committee for Aeronautics. ...
    Publisher: National Advisory Committee for Aeronautics
    Keywords: Aeronautics

    Applications of modern hydrodynamics to aeronautics

    Prandtl, L. | Engineering Index Backfile | 1921
    Publisher: National Advisory Committee for Aeronautics
    Keywords: Aeronautics

    Bibliography of aeronautics 1923, Paul Brockett

    Engineering Index Backfile | 1926
    Publisher: National Advisory Committee for Aeronautics
    Keywords: Aeronautics

    Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds

    National Advisory Committee for Aeronautics | TIBKAT | 1958

    Airfoil section characteristics as affected by variations of Reynolds Number

    Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937
    Publisher: National Advisory Committee for Aeronautics

      Airfoil section characteristics as affected by variations of Reynolds Number

      Jacobs, E.N. / Sherman, A. | Engineering Index Backfile
      characteristics with changes in Reynolds Number are inferred and methods of allowing for these variations in practice determined. ...
      Publisher: National Advisory Committee for Aeronautics

      Airfoil section characteristics as affected by variations of Reynolds Number

      Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937
      Publisher: National Advisory Committee for Aeronautics

    Report on ice formation on aircraft -- By French committee for study of ice formation

    Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    A comparison of typical national gas turbine establishment and NACA axial-flow compressor blade sections in cascade at low speed

    Felix, A. Richard / Emery, Hames C. | TIBKAT | 1957
    Publisher: National Advisory Committee for Aeronautics , Washington, DC

    Internal-flow systems for aircraft

    Rogallo, F.M. | Engineering Index Backfile | 1941
    Results of investigation to determine efficient arrangements for internal flow system when such system operates by itself or in combination ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Charts for helicopter-performance estimation

    Talkin, H.W. | Engineering Index Backfile | 1945
    Charts for helicopter-performance estimation. (Advance Confidential Report L5E04 Aug 1945) ...
    Publisher: National Advisory Committee for Aeronautics

    Full-scale wind-tunnel and flight tests of Fairchild 22 airplane equipped with zap flap and zap Ailerons

    Dearborn, C.H. / Soulee´ / H.A. | Engineering Index Backfile
    Publisher: National Advisory Committee for Aeronautics

    Experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling

    Manganiello, E.J. / Bogatsky, D. | Engineering Index Backfile | 1945
    determined for range of length, aspect ratio, diffusing exit, and shape of exhaust nozzle; ejectors of rectangular cross section were tested because ...
    Publisher: National Advisory Committee for Aeronautics

    Method for computing leading-edge loads

    Rhode, R.V. / Pearson, H.A. | Engineering Index Backfile | 1931
    Development of formula for determination of proper design load for portion of wing forward of front spar; comparison of results from ...
    Publisher: National Advisory Committee for Aeronautics

    On similarity rules for transonic flows

    Kaplan, C. | Engineering Index Backfile | 1949
    Method used by H.S.TSIEN to derive similarity rules for hypersonic flows is utilized to derive T.vonKARMAN'S similarity rules for transonic ...
    Publisher: National Advisory Committee for Aeronautics

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