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    Title :

    Helicopter flight performance improvement by dynamic blade twist



    Published in:

    Publication date :

    2016




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik




    Helicopter Vibration Reduction in Forward Flight using Blade Integral Twist Control

    Cesnik, C. / Shin, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002




    Improvement of Noise Reduction and Performance for a Helicopter Model Rotor Blade by Active Twist Actuation

    Bailly, J. / Delrieux, Y. | British Library Conference Proceedings | 2009