The conceptual design of a four place single turbofan engine powered light aircraft was accomplished utilizing contemporary light aircraft conventional design techniques as a means of evaluating the NASA-Ames General Aviation Synthesis Program (GASP) as a preliminary design tool. In certain areas, disagreement or exclusion were found to exist between the results of the conventional design and GASP processes. Detail discussion of these points along with the associated contemporary design methodology are presented.


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    Title :

    Conceptual Design of Single Turbofan Engine Powered Light Aircraft


    Contributors:

    Publication date :

    1977


    Size :

    174 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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