The Second AIAA CFD High-Lift Prediction Workshop was held in San Diego, California in June 2013. The goals of the workshop continued in the tradition of the first high-lift workshop: to assess the numerical prediction capability of current-generation computational fluid dynamics technology for swept, medium-/high-aspect-ratio wings in landing/takeoff (high-lift) configurations. This workshop analyzed the flow over the DLR-F11 model in landing configuration at two different Reynolds numbers. Twenty-six participants submitted a total of 48 data sets of computational fluid dynamics results. A variety of grid systems (both structured and unstructured) were used. Trends due to grid density and Reynolds number were analyzed, and effects of support brackets were also included. This paper analyzes the combined results from all workshop participants. Comparisons with experimental data are made. A statistical summary of the computational fluid dynamics results is also included. Presented as Paper 2014-0747 at the 52nd AIAA Aerospace Sciences Meeting, National Harbor, MD, 13-17 January 2014


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    Title :

    Overview and Summary of the Second AIAA High-Lift Prediction Workshop



    Published in:

    Publication date :

    2015




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.50
    Local classification TIB:    770/7040



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