Meshing in pointwise ( NACA 0012)
I have a final project for my CFD course,and I want help regarding meshing NACA 0012 Airfoil in pointwise,i know how to use the software, I just need help regarding creating the perfect grid,so I can resolve the perfect Cd value.
1)I can use upto 50,000 points
2)I can use structured mesh.
3)Distance of domain from airfoil I can use is 50 chords.
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