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Old   September 8, 2015, 13:04
Default Cp plot
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Hi All,
I study on a NACA0012 airfoil with SA turbulence model. I got static CP but I don't know how to plot Cp on the Airfoil.
plz guide me to plot the result on some chord ratio of airfoil.

any help is appreciated.
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Old   November 8, 2015, 22:13
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which software are u using for solving?
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