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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    Title :

    Separation of flow due to compressibility shock


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:
    Weise, A. (author)


    Publication date :

    1947


    Size :

    6 pages


    Remarks:

    3 Supp Sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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