A 14-percent-thick, slotted, natural-laminar-flow airfoil, the S204, for light business-jet applications has been designed and analyzed theoretically. The two primary objectives of high maximum lift, relatively 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 Business-Jet Applications


    Contributors:

    Publication date :

    2012


    Size :

    68 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English