Numerical method for obtaining solution to inverse problem of flow behind given detached shock to any desired accuracy; cases of zero and small incidence; particular attention devoted to analysis of sonic and subsonic region of flow field.


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    Title :

    Theoretical investigation of flow field about blunt-nosed bodies in supersonic flight


    Additional title:

    J Aero/Space Sciences


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :