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 abstract in SAE -- J v 69 n 11 Nov 1961 p 80-1)


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    Titel :

    Performance of hypersonic Ramjet using detonative combustion


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Arens, M. (Autor:in)

    Kongress:

    SAE Meeting ; 1961



    Erscheinungsdatum :

    1961


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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