Paper derives equations governing performance of ramjet using detonative combustion, and evaluates performance; engine layout permits normal detonation wave stabilized in diverging combustion chamber passage, or oblique wave stabilized on wedge; lower speed limit of detonative ramjet and cycle calculation; difficulties encountered by ramjets designed for hypersonic speeds may be alleviated if ramjet is designed to burn incoming air at supersonic velocities in stabilized detonation wave. (See also SAE -- Paper 419A for meeting Oct 9-13 1961 8 p)


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    Titel :

    Performance of hypersonic ramjet using detonative combustion


    Weitere Titelangaben:

    SAE -- J


    Beteiligte:
    Arens, M. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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