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    Title :

    OPTIMIZATION OF AN AXISYMMETRIC MACH 6 REFLECTED-SHOCK TUNNEL NOZZLE AT FLIGHT ENTHALPY


    Contributors:

    Conference:

    AIAA SciTech Forum and Exposition ; 2021 ; Online


    Published in:

    Publication date :

    2021



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik



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