naca001065 Airfoil

NACA 0010-65 airfoil

naca001065 Airfoil (x,y) Coordinates

1 0.001
0.95 0.01178
0.9 0.021
0.8 0.035
0.7 0.04389
0.6 0.04867
0.5 0.05
0.4 0.04889
0.3 0.04578
0.2 0.04089
0.15 0.03756
0.1 0.033
0.075 0.02989
0.05 0.02589
0.025 0.01967
0.0125 0.01467
0 0
0.0125 -0.01467
0.025 -0.01967
0.05 -0.02589
0.075 -0.02989
0.1 -0.033
0.15 -0.03756
0.2 -0.04089
0.3 -0.04578
0.4 -0.04889
0.5 -0.05
0.6 -0.04867
0.7 -0.04389
0.8 -0.035
0.9 -0.021
0.95 -0.01178
1 -0.001

naca001065 Airfoil CAD files

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