Partial differential equations for three- dimensional inviscid flow solved for flow field over blunt body shapes at various angles of attack, for application to Apollo spacecraft


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    Title :

    Inverse solution of blunt-body flowfields at large angle of attack.


    Contributors:


    Publication date :

    1967-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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    ADLER, B. K. / DRESSER, H. S. / WAITER, S. A. | AIAA | 1967


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