Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A Design Scheme Aimed at Minimizing Actuator and Structural Loads of a Span Morphing Aircraft


    Contributors:

    Conference:

    47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference



    Publication date :

    2006-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





    AIAA-2006-2137 A Design Scheme Aimed at Minimizing Actuator and Structural Loads of a Span Morphing Aircraft

    Boothe, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006


    AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING

    Lee, J. / Kim, S. / Jung, S. et al. | British Library Conference Proceedings | 2021


    Aeroelastic Analysis of a Span Morphing Wing with Moving Loads

    Singha, Debashis / Murugan, Senthil | TIBKAT | 2022


    Aeroelastic analysis of a span morphing wing with moving loads

    Singha, Debashis / Murugan, Senthil | AIAA | 2022