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    Title :

    Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades


    Contributors:

    Conference:

    19th AIAA Applied Aerodynamics Conference ; 2001 ; Anaheim , CA , U.S.A.



    Publication date :

    2001-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    AIAA-2001-1433 Trailing Edge Flap Control Methodology for Vibration Reduction of Helicopter with Dissimilar Blades

    Roget, B. / Chopra, I. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2001


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