This paper presents the numerical simulation (DLR TAU-code) and the analysis of viscous high-lift flow around a complex wing/body configuration (DLR ALVAST) in landing configuration. The investigations aim for a better understanding of the aerodynamics at the wing root and the lift breakdown for such a configuration.


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    Title :

    Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-Lift Configuration


    Contributors:


    Publication date :

    2010


    Size :

    8 Seiten





    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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