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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    Title :

    Small Turbofan Engines: Their impact on General Aviation Aircraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Business Aircraft Meeting and Exposition ; 1981



    Publication date :

    1981-04-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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