Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Structural Design of an Active Trailing-Edge Flap Blade for Helicopter Vibration Control


    Contributors:

    Conference:

    53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference



    Publication date :

    2012-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Structural Design of an Active Trailing-Edge Flap Blade for Helicopter Vibration Control

    Natarajan, B. / Eun, W. / Lee, J. et al. | British Library Conference Proceedings | 2012


    Flexbeam hinge for helicopter blade active trailing edge flap

    KOPANSKI KRIS / COWLES DEVON / BRUNO DAVID E et al. | European Patent Office | 2016

    Free access

    Vibration Analysis of A Helicopter Blade with A Piezoelectric Actuated Trailing Edge Flap

    Ozgumus, O.O. / Kaya, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012



    HELICOPTER AEROFOIL WITH TRAILING EDGE FLAP

    CAVE ANDREW / STACEY SIMON | European Patent Office | 2017

    Free access