Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Aeroelastic Analysis of Wind Tunnel Test Data of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap (VCCTEF) (AIAA 2015-1405)


    Contributors:

    Conference:

    AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials (Conference)



    Publication date :

    2015-01-01


    Size :

    28 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Wind Tunnel Investigation of a Flexible Wing High-Lift Configuration with a Variable Camber Continuous Trailing Edge Flap Design (AIAA 2015-2417)

    Nguyen, Nhan T. / Precup, Nathan / Livne, Eli et al. | British Library Conference Proceedings | 2015


    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



    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