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Search: Posts Made By: openfoam
Forum: OpenFOAM Running, Solving & CFD May 22, 2009, 05:00
Replies: 85
Views: 21,745
Posted By openfoam
Cl value not macths with experimental value

Hi,
This venkatesh solved the Airfoil case NACA 0012.
Problem Description:NACA 0012 airfoil with Reynolds number=3e6,Mach number=0.85,2D case and AOA 1.Experimental value of Cl is 0.30 ,but it...
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