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    Titel :

    Computational and Experimental Investigation of A 2-D Scramjet Inlet at Mach Numbers From 10 to 25



    Kongress:

    5th International conference, Aerospace planes and hypersonics technologies ; 1993 ; Munich; Germany



    Erscheinungsdatum :

    1993-01-01


    Format / Umfang :

    AIAA-93-5043


    Anmerkungen:

    Separate paper nos AIAA-93-5000 to AIAA-93-5169 with gaps


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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