Method predicts whole 2 and 3-dimensional hypersonic flow field, including shock wave curvatures and resulting vorticity; validity of method is checked by comparing predictions of theory with experiment for surface pressures and bow shock waves of bodies of revolution.


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    Title :

    Generalized shock-expansion method and its application to bodies traveling at high supersonic air speeds


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Journal of the Aeronautical Sciences ; 22 , n 4 ; p 231-238 + 248


    Publication date :

    1955


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :