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    Title :

    Combustion shock tunnel and interface compression to produce stagnation temperatures of 20,000 K and Mach numbers of 35


    Contributors:
    MINUCCI, M. (author) / NAGAMATSU, H. (author) / MYRABO, L.N. (author)

    Conference:

    30th Aerospace Sciences Meeting and Exhibit ; 1992 ; Reno , NV , U.S.A.



    Publication date :

    1992-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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