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    Title :

    Flow Steadiness Over a Double Wedge at Mach 7 Including Effect of Trailing Edge Expansion


    Contributors:

    Conference:

    22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference



    Publication date :

    2018-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    FLOW STEADINESS OVER A DOUBLE WEDGE AT MACH 7 INCLUDING EFFECT OF TRAILING EDGE EXPANSION (AIAA 2018-5388)

    Khraibut, Amna / Gai, Sudhir | British Library Conference Proceedings | 2018




    Separated trailing-edge flow at a transonic Mach number

    VISWANATH, P. R. / BROWN, J. L. | AIAA | 1983


    Separated trailing-edge flow at a transonic Mach number

    Viswanath, P. R. / Brown, J. L. | NTRS | 1983