Problems associated with operation at hypersonic speeds can be alleviated by operating engine combustion chamber at supersonic mean inlet velocities; governing equations for engine performance with normal detonation wave in chamber are derived; flight regime for which combustion through normal detonation is possible is investigated; performance of ideal detonative ramjet using acetylene fuel is presented for flight Mach numbers of 6 to 10; ramjet engine configuration for performance with normal detonation.


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    Titel :

    Hypersonic ramjet using normal detonation wave


    Weitere Titelangaben:

    Research Council Israel -- Bul


    Beteiligte:
    Arens, M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




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