The results from DLR, Airbus, and ONERA from the Second AIAA Computational Fluid Dynamics Drag Prediction Workshop are presented. The lift, drag, and pitching moments are calculated for the DLR-F6 configuration at transonic flow conditions by solving the Reynolds-averaged Navier-Stokes equations on structured as well as on unstructured, hybrid grids.
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Brodersen et al. (2005) studied this question.
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