Pre proccesor procedure for NACA 0012 -- CFD Online Discussion Forums

February 5, 2009, 03:17	Hi Foam Guyes This is Venk	#1
venkateshtl Guest Posts: n/a	Hi Foam Guyes This is Venkatesh from India I created C grid and imported from the fluent for NACA0012 airfoil. Now i need procedure to solve it in openFoam. Eulers equaton with mach .85

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