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NACA0012 airfoil2d simulation in OPENFOAM lift and drag coefficients calculation.

Open Ancy5758 opened this issue 1 year ago • 0 comments

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?

Ancy5758 avatar Apr 21 '24 08:04 Ancy5758