Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically reentrant afterbody flying at large angle of attack


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    Title :

    A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack


    Contributors:

    Publication date :

    1966-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English