Based on premise that supersonic burning is possible, performance of ramjet cycles is calculated over range of flight Mach numbers from 4 to 7; effects of parameters such an inlet design, combustor area, divergence, wall friction, and nozzle performance; estimates of engine weight and cooling loads included.


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    Titel :

    Analysis of ramjet engines using supersonic combustion


    Weitere Titelangaben:

    NACA -- Tech Note


    Beteiligte:
    Weber, R.J. (Autor:in) / Mackay, J.S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1958


    Format / Umfang :

    49 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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    Weber, Richard J. / MacKay, John S. | TIBKAT | 1958


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    Weber, Richard J / Mackay, John S | NTRS | 1958



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