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    Title :

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



    Conference:

    42nd, Structures, structural dynamics, and materials conference ; 2001 ; Seattle, WA



    Publication date :

    2001-01-01


    Size :

    11 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






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