Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Optimum active twist input scenario for performance improvement and vibration reduction of a helicopter rotor


    Contributors:

    Published in:

    Publication date :

    2017




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik



    Helicopter vibration reduction using active twist control of composite rotor blades

    Pawar, Prashant M. / Jung, Sung-Nam / Yu, Yung-Hoon | Tema Archive | 2008


    Helicopter Vibration Reduction Using Active Twist Control of Composite Rotor Blades

    Pawar, P. / Jung, S. / Yu, Y. et al. | British Library Conference Proceedings | 2008




    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