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    Title :

    Analysis of helicopter vibratory hub loads alleviation by cyclic trailing-edge blade flap actuation



    Published in:

    Publication date :

    2009



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Unknown



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.50 / 55.60
    Local classification TIB:    275/7040



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