Two conceptual designs of the oblique detonation wave ramjet are presented. The performance is evaluated for stoichiometric hydrogen-air equivalence ratios of phi = 1/3, 2/3 and 1 for a range of flight Mach numbers from 6 to 10.


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    Title :

    Oblique Detonation Wave Ramjet


    Contributors:

    Publication date :

    1980


    Size :

    87 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English