System consists of movable auxiliary aerodynamic sensors mounted on fuselage and connected to trailing-edge flaps by rigid mechanical linkages. System achieves alleviation by reducing lift-curve slope of airplane to such a small value that gust-induced angles of attack will result in small changes in lift.


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    Title :

    Gust alleviation system to improve ride comfort of light airplanes


    Contributors:

    Publication date :

    1975-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






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