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    Titel :

    NUMERICAL PREDICTION OF STAGNATION-POINT SHOCK-DETACHMENT DISTANCE FOR HYPERSONIC LOW DENSITY FLOW OVER BLUNT NOSE SHAPES



    Kongress:

    24th, International congresss of aeronautical sciences ; 2004 ; Yokohama, Japan



    Erscheinungsdatum :

    01.01.2004


    Format / Umfang :

    ICAS 2004-3.7.R.1


    Anmerkungen:

    Also known as ICAS 2004.; HELD ON CD-ROM



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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