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    Title :

    Comparative flow path analysis and design assessment of an axisymmetric hydrogen fueled scramjet flight test engine at a Mach number of 6.5


    Contributors:
    McClinton, C. (author) / Roudakov, A. (author) / Semenov, V. (author) / Kopehenov, V. (author)

    Conference:

    Space Plane and Hypersonic Systems and Technology Conference ; 1996 ; Norfolk , VA , U.S.A.



    Publication date :

    1996-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English