|September 8, 2015, 13:04||
Join Date: Aug 2015
Posts: 3Rep Power: 2
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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