Determination of relative performance for two cases where each system employs isentropic spike external compression inlet and internal compression inlet; results indicate that specific impulse of supersonic ramjet will be superior to that of subsonic ramjet at Mach numbers above approximately 7 for configurations having isentropic spike external compression inlets and above 10 for those having internal compression inlets.


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    Titel :

    Relative thermodynamic efficiency of supersonic combustion and subsonic combustion hypersonic ramjets


    Weitere Titelangaben:

    ARS -- J


    Beteiligte:

    Erschienen in:

    ARS Journal ; 30 , n 11


    Erscheinungsdatum :

    1960


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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