Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Flutter Analysis of Mission-Adaptive Wing with Variable Camber Continuous Trailing Edge Flap (AIAA 2014-0839)



    Conference:

    Conference; 55th, AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials ; 2014 ; National Harbor, MD



    Publication date :

    2014-01-01


    Size :

    39 pages


    Remarks:

    Includes bibliographical references and author index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Aeroelastic Modeling and Drag Optimization of Aircraft Wing with Variable Camber Continuous Trailing Edge Flap (AIAA 2014-2443)

    Lebofsky, S. / Ting, E. / Nguyen, N. et al. | British Library Conference Proceedings | 2014


    Development of Variable Camber Continuous Trailing Edge Flap for Performance Adaptive Aeroelastic Wing

    Nguyen, Nhan / Lebofsky, Sonia / Ting, Eric et al. | British Library Conference Proceedings | 2015



    Development of Variable Camber Continuous Trailing Edge Flap for Performance Adaptive Aeroelastic Wing

    Chaparro, Daniel / Ting, Eric / Urnes, James et al. | SAE Technical Papers | 2015


    Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW (AIAA 2014-2444)

    Kaul, U. / Nguyen, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014