Compressibility shocks accompanying local or total supersonic flows lead to pronounced flow separations which result in unusually high energy losses on airplane wings, vanes, and in diffusers; phenomena investigated experimentally and theoretically. English translation from Technische Berichte v 10 n 2 1943.


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    Titel :

    Separation of flow due to compressibility shock


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Beteiligte:
    Weise, A. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    6 pages


    Anmerkungen:

    3 Supp Sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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