Performance of ramjet having detonation wave combustion process; flight speeds from Mach 2.5 to 10 are examined and thermodynamic property changes presented; engine cycle performance characteristics are computed including air specific impulse, specific fuel consumption and thermal efficiency; subsonic burning ramjet is shown to have superior performance compared to detonation wave engine; differences and some design features.


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    Titel :

    Detonation wave hypersonic ramjet


    Weitere Titelangaben:

    ARS -- J


    Beteiligte:
    Sargent, W.H. (Autor:in) / Gross, R.A. (Autor:in)

    Erschienen in:

    ARS Journal ; 30 , n 6


    Erscheinungsdatum :

    1960


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Hypersonic ramjet using normal detonation wave

    Arens, M. | Engineering Index Backfile | 1960




    Oblique detonation wave ramjet

    Morrison, R. B. | NTRS | 1980