Airfoil analysis convergence problem -- CFD Online Discussion Forums

August 27, 2014, 10:47	Airfoil analysis convergence problem	#1
mayursindhav New Member mayur Join Date: Jul 2014 Posts: 2 Rep Power: 0	Hello friend I am simulating airfoil NACA0012 tlat 18 degree of attack but it is not converge. Graph is straight. I am try by reduce courent number(my solution is density based), refine mesh, Help to come out from this

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