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Pre proccesor procedure for NACA 0012

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Old   February 5, 2009, 04:17
Default Hi Foam Guyes This is Venk
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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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