Partial differential equation for perturbation velocity potential is examined for free stream Mach numbers close to and equal to one. (20¢)


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    Titel :

    Linearized compressible-flow theory for sonic flight speeds


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Heaslet, M.A. (Autor:in) / Lomax, H. (Autor:in) / Spreiter, J.R. (Autor:in)


    Erscheinungsdatum :

    1950


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Linearized compressible-flow theory for sonic flight speeds

    Heaslet, Max A. / Lomax, Harvard / Spreiter, John R. | TIBKAT | 1949


    Linearized compressible-flow theory for sonic flight speeds

    Heaslet, M.A. / Lomax, H. / Spreiter, J.R. | Engineering Index Backfile | 1949


    Linearized Compressible-flow Theory for Sonic Flight Speeds

    Heaslet, Max A / Lomax, Harvard / Spreiter, John R | NTRS | 1949


    Linearized Compressible Flow

    McBain, G. D. | Wiley | 2012


    Linearized potential theory of propeller induction in compressible flow

    Davidson, R.E. | Engineering Index Backfile | 1953