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Search: Posts Made By: nuimlabib
Forum: Main CFD Forum October 1, 2009, 01:14
Replies: 1
Views: 1,830
Posted By nuimlabib
not convergence in high angle of attack in low reynold number

why at the angle of attack iof airfoil s increased in the range of 10 degrees, iteration does not converge, but at a low angle of attack 0 to 8 degrees, to achieve convergence, I use the segregated...
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