Aerodynamic design and development of wing and high-lift system for DC-9 family of short-to-medium-range jet transports are reviewed, starting with overall design goals of short takeoff and landing field lengths, maximum practical cruise speed, and low direct operating costs; aerodynamic design of wing and high-lift system is discussed in detail with primary emphasis placed on DC-9 Series 20, 30, and 40; wing incorporates full-span leading edge slats for extremely high maximum lift capability and specially designed airfoils for low cruise drag.


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    Titel :

    Aerodynamic design of DC-9 wing and high-lift system


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Schaufele, R.D. (Autor:in) / Ebeling, A.W. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Design



    Erscheinungsdatum :

    1967


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic Design of the DC-9 Wing and High-Lift System

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