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February 5, 2009, 03:17 |
Hi Foam Guyes
This is Venk
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#1 |
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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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