Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    An aeroelastic optimization design approach for structural configuration of flying wings



    Published in:

    Publication date :

    2013



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Chinese



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik




    A constructal aeroelastic design approach for cross-section configuration of flying wing aircraft

    Ebrahimi Fakhari, Hadi / Moshtaghzadeh, Mojtaba / Mardanpour, Pezhman et al. | AIAA | 2024


    Structural Optimization Studies of Wings with Aeroelastic Constraints Using ASTROS

    Striz, A. G. | British Library Conference Proceedings | 1995


    MULTIFIDELITY AEROELASTIC OPTIMIZATION APPLIED TO HAR WINGS

    Le-Lamer, Y. / Quaglia, G. / Benard, E. et al. | TIBKAT | 2021

    Free access