The first simulation of a the flow around a complete wingbody configuration based on direct solution of the incompressible Navier-Stokes equations without user specified turbulence model using an adaptive residual stabilized finite element method (Direct Finite Element Simulation DFS), was performed by the Computational Technology Laboratory at KTH and presented the 2nd AIAA High Lift Prediction Workshop, San Diego, June 22-23, 2013:
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