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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    Titel :

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


    Beteiligte:


    Erscheinungsdatum :

    2010


    Format / Umfang :

    8 Seiten





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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