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    Title :

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



    Conference:

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



    Publication date :

    1993-01-01


    Size :

    AIAA-93-5043


    Remarks:

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


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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