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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    Title :

    Some aspects of turbojet performance calculation at high flight Mach numbers


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1956


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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