Performance of supersonic combustion ramjet is examined in relation to that of subsonic ramjet; at low hypersonic speeds internal performance of two cycles are comparable, but at speeds above Mach 7, supersonic combustion cycle should offer superior performance; beyond Mach 9 lack of reliable intake data makes estimation of possible engine performance conjectural; as acceleration engine supersonic combustion ramjet, flying at relatively low altitudes, offers possibilities unattainable with conventional ramjet; appraisal of available data on mixing and reaction rates is made to assess feasibility of supersonic combustion.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Feasibility of supersonic combustion ramjets for low hypersonic speeds


    Weitere Titelangaben:

    Aerodynamics Power Plant Installation -- 1 -- AGARDograph


    Beteiligte:
    Hawkins, R. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    48 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    Gun-launching supersonic-combustion ramjets

    Valenti, A.M. / Molder, S. / Salter, G.R. | Engineering Index Backfile | 1963


    The potential of supersonic combustion ramjets

    DuPont, A.A. | Tema Archiv | 1995


    The Potential of Supersonic Combustion Ramjets

    DuPont, A. A. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995


    Intakes for hypersonic ramjets

    Molder, S. | Engineering Index Backfile | 1963