Analytically and empirically derived external and internal aerodynamic data have been applied to the high-speed cruise development of a low-drag, minimum thrust loss, strut mounted nacelle. The nacelle considered for this study houses a high bypass ratio subsonic fan engine with a short fan duct and a primary plug nozzle. The analysis technique has been geared to a simple geometric description of the nacelle and exhaust system so that high-speed computers may be used to generate trade data. The trade data permit the selection of exhaust systems which, when combined with the complete nacelle, will provide the highest thrust-minus-drag configuration consistent with the airplane cruise mission.


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    Titel :

    Aerodynamic Considerations for Engine Exhaust Design for Subsonic High Bypass Fan Engines


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Frazier, G. T. (Autor:in)

    Kongress:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1966



    Erscheinungsdatum :

    01.02.1966




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch