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 :

    An inverse solution for the determination of flow fields about axisymmetric blunt bodies at large angle of attack.


    Contributors:

    Publication date :

    1966-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English