Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Aerofoil profile and sweep optimisation for a blended wing-body aircraft using a discrete adjoint method


    Contributors:

    Published in:

    Publication date :

    2006



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Unknown



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.60 / 55.50
    Local classification TIB:    275/7040





    Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps AIAA Paper

    Qin, N. / Wong, S. / Le Moigne, A. et al. | British Library Conference Proceedings | 2007


    Blended wing body aircraft

    CHITTICK IAN / RAKOWITZ MARK / REIST THOMAS | European Patent Office | 2023

    Free access

    BLENDED WING BODY AIRCRAFT

    BANERJEE SIDDHARTHO / GALIN ALEXANDRE / CHITTICK IAN | European Patent Office | 2023

    Free access