The applicability of small turbofan engines to general aviation aircraft is discussed. The engine and engine/airplane performance, weight, size, and cost interrelationships are examined. The effects of specific engine noise constraints are evaluated. The factors inhibiting the use of turbofan engines in general aviation aircraft are identified.


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    Titel :

    Study of small turbofan engines applicable to general-aviation aircraft


    Beteiligte:
    Merrill, G. L. (Autor:in) / Burnett, G. A. (Autor:in) / Alsworth, C. C. (Autor:in)

    Erscheinungsdatum :

    1973-09-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Study of Small Turbofan Engines Applicable to General-Aviation Aircraft

    G. L. Merrill / G. A. Burnett / C. C. Alsworth | NTIS | 1973


    Small Turbofan Engines: Their impact on General Aviation Aircraft

    I'Anson, L. R. / Schneider, W. F. | SAE Technical Papers | 1981


    Study of Small Civil Turbofan Engines Applicable to Military Trainer Airplanes

    R. W. Heldenbrand / G. L. Merrill / G. A. Burnett | NTIS | 1975


    Study of small civil turbofan engines applicable to military trainer airplanes

    Heldenbrand, R. W. / Merrill, G. L. / Burnett, G. A. | NTRS | 1975