naca1410 Airfoil
NACA 1410 airfoil naca1410 Airfoil (x,y) Coordinates 1 0.00105 0.95021 0.00832 0.90034 0.01513 0.80049 0.02741 0.70051 0.03804 0.60042 0.04692 0.50025 0.05385 0.4 0.05836 0.29937 0.0594 0.24907 0.05809 0.1988 0.05531 0.14861…
naca001264a08cli0.2 Airfoil
NACA 0012-64 a=0.8 c(li)=0.2 airfoil naca001264a08cli0.2 Airfoil (x,y) Coordinates 1 0.0012 0.9505 0.01271 0.90091 0.02355 0.8012 0.04253 0.70077 0.05663 0.60038 0.06662 0.49993 0.07157 0.39946 0.07279 0.299 0.06974 0.19858 0.06221 0.14839…
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