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Solving NACA AIRFOIL

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Old   February 6, 2009, 06:01
Default HI EVERYBODY I am facing
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NAVEEN.K.M
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HI EVERYBODY


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, 06:43
Default Naveen, You keep posting th
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ngj
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Niels Gjoel Jacobsen
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Naveen,

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
http://powerlab.fsb.hr/ped/kturbo/Op...P/naca0012.tgz 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.

/Niels
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