Inverse solution for equilibrium real gas flowfields over axisymmetric blunt bodies traveling at supersonic speed at large angle of attack is formulated; computer program based on theory is developed which overcomes instabilities and singularities that characterize solution; several particular real air solutions are obtained for axisymmetric shapes; angle-of-attack solution for sphere was used to verify formulation; Apollo flowfield at 22° angle of attack was obtained and found to agree with flight test pressure distribution, and satisfied internal consistency checks.


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    Title :

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


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 5 , n 6 ; p 1079-1085


    Publication date :

    1967


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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

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


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    Yang, X. / Wang, Z. / Wang, C. | British Library Online Contents | 1997