Paper attempts to define some important and less recognized characteristics of scramjet (supersonic combustion ramjet); parameter considered as predominant is specific impulse when variation of specific impulse as function of flight Mach number is investigated for different cycles; in general, field of application for turbojet engine is between 0 and 5 to 6, and subsonic burning ramjet, between 1.3 to 2 and 6 to 8, whereas scramjet is considered useful above 5 to 6 Mach; cycles and performances in supersonic combustion; engine design requirements of engine components, in particular, inlet, combustion, tangential injection with chemical reaction, analysis of flow field in combustor and nozzle; engine development and testing.


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    Titel :

    Review of scramjet propulsion technology


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Ferri, A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch







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