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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    Titel :

    Conceptual Design of Single Turbofan Engine Powered Light Aircraft


    Beteiligte:
    F. S. Snyder (Autor:in) / C. G. Voorhees (Autor:in) / A. M. Heinrich (Autor:in) / D. N. Baisden (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    174 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Conceptual design of single turbofan engine powered light aircraft

    Snyder, F. S. / Voorhees, C. G. / Heinrich, A. M. et al. | NTRS | 1977


    RECENT CONCEPTUAL DESIGN STUDIES OF SINGLE TURBOFAN ENGINE AIRCRAFT

    Schairer, Edward T. | SAE Technical Papers | 1977




    Turbofan engine and aircraft comprising turbofan engine

    GARDES PASCAL / MENOU FABIEN / GOUGEON PASCAL et al. | Europäisches Patentamt | 2021

    Freier Zugriff