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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    Titel :

    Computational Simulations for Fighter and Hypersonic Vehicle Inlet-Forebody Interactions


    Beteiligte:
    C. W. Boppe (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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