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Old   February 6, 2009, 07:01
Default HI EVERYBODY I am facing
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I am facing difficult to solve NACA 0012 airfoil case which is imported from fluent...can u please send me the procedure of solving this case in openFoam 1.4.1..
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Old   February 6, 2009, 07:43
Default Naveen, You keep posting th
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Niels Gjoel Jacobsen
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ngj will become famous soon enoughngj will become famous soon enough

You keep posting the same question over and over again besides the fact that you have been given an entire test setup.
The test case can be found at and if you are having problems running it, it is because you haven't tried the tutorials.
You have by far exceeded the tolerance limit of this forum, and I suggest that you consider your general havaviour.
The present behaviour just clutter the forum, and makes it nearly impossible for serious users to find relevant information on the naca-profiles. All they find are unanswered threads composted by you.

Please note that I do not use the Friend-feature, so do not be offended, if I do not accept a request.
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