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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    Title :

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


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1967 Design



    Publication date :

    1967


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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

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