Question: How can I divide this airfoil into 20 same panels in python? NACA 2412 0.05 0.00 0.00 005 010 0.15 0.20 0.25 0.30 0.35 0.40
NACA 2412 0.05 0.00 0.00 005 010 0.15 0.20 0.25 0.30 0.35 0.40 045 0.50 055 060 065 0.70 075 0.80 0.85 090 095 100
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