Abstract
Incompressible flow separating from the upper surface of an airfoil at an 18° angle of attack and a Reynolds number of Re = 105, based on the freestream velocity and chord length c, is studied by the means of large-eddy simulation (LES). The numerical method is based on second-order central spatial discretization on a Cartesian grid using an immersed boundary technique. The results are compared with an LES using body-fitted nonorthogonal grids and with experimental data.
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Communicated by R.D. Moser.
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Eisenbach, S., Friedrich, R. Large-eddy simulation of flow separation on an airfoil at a high angle of attack and Re = 105 using Cartesian grids. Theor. Comput. Fluid Dyn. 22, 213–225 (2008). https://doi.org/10.1007/s00162-007-0072-z
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DOI: https://doi.org/10.1007/s00162-007-0072-z