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FLUENT TRANSITION WRONG?

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March 1, 2008, 21:57	FLUENT TRANSITION WRONG?	#1
Rif Guest Posts: n/a	I cannot seem to get the coefficient of drag for the NACA 0012 airfoil in my FLUENT 6.2 simulations. The drag coefficient differ alot from experimental data. My Y plus region was set to 1 . even then the drag is still high. Any help? I'm using a C grid mesh.

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