naca001264 Airfoil

NACA 0012-64 airfoil

naca001264 Airfoil (x,y) Coordinates

1 0.0012
0.95 0.01027
0.9 0.01867
0.8 0.0332
0.7 0.0448
0.6 0.0532
0.5 0.05827
0.4 0.06
0.3 0.05827
0.2 0.05293
0.15 0.04867
0.1 0.0424
0.075 0.03813
0.05 0.03267
0.025 0.02453
0.0125 0.01813
0 0
0.0125 -0.01813
0.025 -0.02453
0.05 -0.03267
0.075 -0.03813
0.1 -0.0424
0.15 -0.04867
0.2 -0.05293
0.3 -0.05827
0.4 -0.06
0.5 -0.05827
0.6 -0.0532
0.7 -0.0448
0.8 -0.0332
0.9 -0.01867
0.95 -0.01027
1 -0.0012

naca001264 Airfoil CAD files

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