Meshing in pointwise ( NACA 0012) -- CFD Online Discussion Forums

April 10, 2013, 20:08	Meshing in pointwise ( NACA 0012)	#1
uzairm New Member Uzair Mansuri Join Date: Apr 2013 Posts: 2 Rep Power: 0	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.

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