Solution for 2-dimensional flow of inviscid gas is obtained by numerical methods of analysis, divided into subsonic region analyzed by relaxation method of Southwell and supersonic region treated by method of characteristics; shapes of sonic line and shock wave are obtained by iteration techniques; distribution in flow pattern indicates interaction between subsonic and supersonic regions is negligible; comparisons with theoretical and experimental results.


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    Titel :

    Numerical solution of flow of perfect gas over circular cylinder at infinite mach number


    Weitere Titelangaben:

    NASA -- Memo


    Beteiligte:
    Hamaker, F.M. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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