naca001234 Airfoil

 NACA 0012-34 airfoil

naca001234 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 0.058
0.2 0.05093
0.15 0.04493
0.1 0.03653
0.075 0.03133
0.05 0.02493
0.025 0.0168
0.0125 0.01133
0 0
0.0125 -0.01133
0.025 -0.0168
0.05 -0.02493
0.075 -0.03133
0.1 -0.03653
0.15 -0.04493
0.2 -0.05093
0.3 -0.058
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

naca001234 Airfoil CAD files

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