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Airfoil Pressure coefficients don't match!

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Old   August 17, 2009, 06:57
Default Airfoil Pressure coefficients don't match!
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Kappe
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Hi,
I meshed a NACA0012, C-grid about 20K node points. Used K-Epsilon viscous model. Compared it with Abbott values. Doesn't match satisfactorily.
Please suggest where i would've gone wrong.
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Old   August 18, 2009, 05:58
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I have also checked the y+ values which are between 30-60
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