Profitable short-range and through-stop operations require excellent short runway performance; empty weight, balance, stall characteristics, and systems advantages of wing-mounted engines dictated engine location; wing-nacelle geometry relationship was major consideration in deciding to mount nacelles so close to wing; high-speed cruise at low altitude required minimum wing span and area and maximum sweep; thus inherent takeoff performance limitations of twin-engine airplane required flap system efficiency and increased flap size.


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    Titel :

    Aerodynamic design philosophy of boeing 737


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Olason, M.L. (Autor:in) / Norton, D.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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