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    Title :

    Numerical and Experimental Investigation on Detonation Tube for Simulating the Rocket Exhaust Gas at High Enthalpy Shock Tunnel


    Contributors:

    Conference:

    16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference



    Publication date :

    2009-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Numerical Analysis on Detonation Tube for Simulating the Rocket Exhaust Gas at High Enthalpy Shock Tunnel

    Shigematsu, K. / Matsuo, A. / Itoh, K. et al. | British Library Conference Proceedings | 2009


    Detonation tube technique for simulating rocket plumes in space environment

    Leng, J. / Oman, R.A. / Hopkins, H.B. | Engineering Index Backfile | 1968


    Numerical and experimental studies of rocket exhaust flow in rocket launch tube

    SUNG, HONG-GYE / KIM, YOON-GON / KIM, JONG et al. | AIAA | 1992