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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    Title :

    Hypersonic ramjet using normal detonation wave


    Additional title:

    Research Council Israel -- Bul


    Contributors:
    Arens, M. (author)

    Published in:

    Publication date :

    1960


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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