A patented dual purpose circulation control airfoil is designed for operation at high speeds in the vicinity of transonic speed and for low speed applications such as landing speeds. A blunt trailing edge possesses a varying radius of curvature to comprise a high speed and low speed coanda surface.


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    Title :

    Dual Purpose Circulation Control Airfoil


    Contributors:

    Publication date :

    1972


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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