Up to present turbojet engines employed have been essentially subsonic engines suitably strengthened; future may bring use of engines specifically designed for appropriate range of Mach number; some implications of this change of outlook reviewed in so far as they affect prediction of engine performance.


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    Titel :

    Some aspects of turbojet performance calculation at high flight Mach numbers


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Palmer, J.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1956


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    Turbojet-engine mechanical design for high mach number flight

    Schnitzer, H.C. | Engineering Index Backfile | 1958


    Flight characteristics at high mach numbers

    Outman, V. / Graff, G.S. | Engineering Index Backfile | 1950


    FLIGHT CHARACTERISTICS AT HIGH MACH NUMBERS

    GRAFF, G. S. / OUTMAN, V. | SAE Technical Papers | 1950


    Flight characteristics at high mach numbers

    Outman, V. / Graff, G.S. | Engineering Index Backfile | 1951