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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    Title :

    Study of small turbofan engines applicable to general-aviation aircraft


    Contributors:

    Publication date :

    1973-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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