Euler method characteristics, an F-14 fuselage geometry model and shock wave pattern predicted by Euler analysis, prediction of F-14 inlet pressure recovery levels, a fuselage induced inlet flow field comparison, avionic integration, and hypersonic vehicle inlet integration are among the topics covered. Information is given in viewgraph form.


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    Title :

    Computational Simulations for Fighter and Hypersonic Vehicle Inlet-Forebody Interactions


    Contributors:
    C. W. Boppe (author)

    Publication date :

    1991


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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