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Stoevesandt, B. (author), Shishkin, A. (author), Peinke, J. (author), Wagner, C. (author)
Since the accuracy of the widely used Reynolds Averaged Navier Stokes (RANS) approach is limited simulating turbulent flow separation on airfoils, we applied a spectral/hp element method to predict the turbulent flow separation at an airfoil for an angle of attack of 12°. The spectral/hp approach allows to solve the incompressible Navier-Stokes...
conference paper 2006