The potential performance of oblique detonation wave ramjets is analyzed in terms of multishock diffusion, oblique detonation waves, and heat release. Results are presented in terms of thrust coefficients and specific impulses for a range of flight Mach numbers of 6 to 16.


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    Title :

    Evaluation of the oblique detonation wave ramjet


    Contributors:

    Publication date :

    1978-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Oblique detonation wave ramjet

    Morrison, R. B. | NTRS | 1980


    Oblique Detonation Wave Ramjet

    R. B. Morrison | NTIS | 1980