Meshing in pointwise ( NACA 0012)
Hey,
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. |
All times are GMT -4. The time now is 08:24. |