naca0010 Airfoil

NACA 0010 airfoil

naca0010 Airfoil (x,y) Coordinates

1 0.00105
0.95 0.00672
0.9 0.01207
0.8 0.02187
0.7 0.03053
0.6 0.03803
0.5 0.04412
0.4 0.04837
0.3 0.05002
0.25 0.04952
0.2 0.04782
0.15 0.04455
0.1 0.03902
0.075 0.035
0.05 0.02962
0.025 0.02178
0.0125 0.01578
0 0
0.0125 -0.01578
0.025 -0.02178
0.05 -0.02962
0.075 -0.035
0.1 -0.03902
0.15 -0.04455
0.2 -0.04782
0.25 -0.04952
0.3 -0.05002
0.4 -0.04837
0.5 -0.04412
0.6 -0.03803
0.7 -0.03053
0.8 -0.02187
0.9 -0.01207
0.95 -0.00672
1 -0.00105

naca0010 Airfoil CAD files

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