naca001064 Airfoil

NACA 0010-64 airfoil

naca001064 Airfoil (x,y) Coordinates

1 0.001
0.95 0.00856
0.9 0.01556
0.8 0.02767
0.7 0.03733
0.6 0.04433
0.5 0.04856
0.4 0.05
0.3 0.04856
0.2 0.04411
0.15 0.04056
0.1 0.03533
0.075 0.03178
0.05 0.02722
0.025 0.02044
0.0125 0.01511
0 0
0.0125 -0.01511
0.025 -0.02044
0.05 -0.02722
0.075 -0.03178
0.1 -0.03533
0.15 -0.04056
0.2 -0.04411
0.3 -0.04856
0.4 -0.05
0.5 -0.04856
0.6 -0.04433
0.7 -0.03733
0.8 -0.02767
0.9 -0.01556
0.95 -0.00856
1 -0.001

naca001064 Airfoil CAD files

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