low spped wing computation -- CFD Online Discussion Forums

November 21, 2002, 05:20	low spped wing computation	#1
echo Guest Posts: n/a	I am using Fluent6.0 to computate lift/drag ratio of straight wing with aspect ration 12.The airfoil is NFL1050,the computational result of lift/drag ratio is too small,only about 20. The solver is segeregated solver,I have refined grid around the front edge. I have computated 2D airfoil,the result is fine. Who can tell me How I can get good result of wing?

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