naca001035 Airfoil

NACA 0010-35 airfoil

naca001035 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 0.04878
0.3 0.04478
0.2 0.03789
0.15 0.03289
0.1 0.02667
0.075 0.02289
0.05 0.01844
0.025 0.01267
0.0125 0.00878
0 0
0.0125 -0.00878
0.025 -0.01267
0.05 -0.01844
0.075 -0.02289
0.1 -0.02667
0.15 -0.03289
0.2 -0.03789
0.3 -0.04478
0.4 -0.04878
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

naca001035 Airfoil CAD files

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