Action of engine nacelle upon wing in supersonic flow is examined; engine installation is shown to influence wave drag due to thickness and drag due to lift; available theoretical procedures make it possible to estimate forces on wing due to combined action of several nacelles; results obtained are compared with supersonic wind-tunnel-test data; effects of relative location of nacelles and of nacelle shape and size on lift, drag, and pitch characteristics of wind-tunnel models are presented; experimental results show that camber and twist of wing should be designed by taking into account effects of flowfield from nacelles.


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    Titel :

    Aerodynamics of powerplant installation on supersonic aircraft


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Sigalla, A. (Autor:in) / Hallstaff, T.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :