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    Title :

    Optimization of an Axisymmetric Mach 6 Reflected-Shock Tunnel Nozzle at Flight Enthalpy


    Contributors:

    Conference:

    AIAA Scitech 2021 Forum



    Publication date :

    2021-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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

    Hameed, Ahsan / Mustafa, Muhammad A. / Shekhtman, David et al. | TIBKAT | 2021



    Reflected shock wave/boundary layer interaction in high-enthalpy shock tunnel

    Kaneko, Munetsugu / Men'shov, Igor / Nakamura, Yoshiaki | AIAA | 2000


    Driver gas contamination in a high-enthalpy reflected shock tunnel

    STALKER, R. J. / CRANE, K. C. A. | AIAA | 1978


    Mach 4 and Mach 8 axisymmetric nozzles for a shock tunnel

    Jacobs, P. A. / Stalker, R. J. | TIBKAT | 1991