How can I write code for plotting modified airfoil surface?
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I have a project about modified 2D NACA2415 airfoil. I will modify upper surface and then analyze it on ANSYS. But, firstly ı need the points of modified naca airfoil. What can ı do for coding of new naca airfoil?
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Parsa
2022-5-21
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Hi Merve
Please take a look at the link below.
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