An evaluation is made on the application of small turbofan engines to general aviation aircraft. The influence of engine cycle parameters, such as bypass ratio and fan pressure ratio and other design features as related to mission and aircraft requirements, are presented.


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    Titel :

    Small Turbofan Engines: Their impact on General Aviation Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    I'Anson, L. R. (Autor:in) / Schneider, W. F. (Autor:in)

    Kongress:

    Business Aircraft Meeting and Exposition ; 1981



    Erscheinungsdatum :

    1981-04-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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