NACA0012 airfoil2d simulation in OPENFOAM lift and drag coefficients calculation.
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Ancy5758 commented
Hello
Try to find out the lift and drag coefficients of NACA0012 airfoil in OpenFOAM using airFoil2D tutorial, with my own mesh. The lift and drag coefficients are not matching with the experimental data. Suggest some papers to refer or some solution to rectify the issue?