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    Title :

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



    Conference:

    16th, AIAA International Space Planes and Hypersonic Systems and Technologies Conference ; 2009 ; Bremen, Germany



    Publication date :

    2009-01-01


    Size :

    7 pages


    Remarks:

    Includes bibliographic references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Detonation tube technique for simulating rocket plumes in space environment

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




    Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels

    Z. L. Jiang / W. Zhao / C. Wang et al. | AIAA | 2002