Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Experimental Flowpath Characterization of the T2 Shock Tunnel Mach 7.0 Hybrid Axisymmetric Contour Nozzle



    Conference:

    AIAA SCITECH 2024 Forum



    Publication date :

    2024-01-01



    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


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

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



    Mach 4 and Mach 8 axisymmetric nozzles for a shock tunnel

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