A 13.49-percent-thick, slotted, natural-laminar-flow airfoil, the S207, for a transport aircraft has been designed and analyzed theoretically. The two primary objectives of high maximum lift, insensitive to roughness, and low profile drag have been achieved. The drag-divergence Mach number is predicted to be greater than 0.70.


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    Title :

    Design of a Slotted, Natural-Laminar-Flow Airfoil for a Transport Aircraft


    Contributors:

    Publication date :

    2019-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :