A method for solving the viscous hypersonic flow field around realistic configurations is presented. The numerical procedure for generating the required finite difference grid and the two-factored implicit flow solver are described. Results are presented for the shuttle orbiter and a generic wing-body configuration at hypersonic Mach numbers.


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    Titel :

    Numerical Simulation of the Hypersonic Flow Around Lifting Vehicles


    Beteiligte:
    Y. Rizk (Autor:in) / D. Chaussee (Autor:in) / J. Steger (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Numerical simulation of the hypersonic flow around lifting vehicles

    Rizk, Yehia / Chaussee, Denny / Steger, Joseph | NTRS | 1987


    Numerical simulation of the hypersonic flow around lifting vehicles

    Rizk, Yehia / Chaussee, Denny / Steger, Joseph | NTRS | 1987


    Numerical Simulation of the Hypersonic Flow around Lifting Vehicles

    Y. Rizk / D. Chaussee / J. Steger | NTIS | 1987