naca001065 Airfoil

NACA 0010-66 airfoil 

naca001066 Airfoil (x,y) Coordinates

1 0.001
0.95 0.01656
0.9 0.02833
0.8 0.043
0.7 0.04889
0.6 0.05
0.5 0.04956
0.4 0.04822
0.3 0.04578
0.2 0.04178
0.15 0.03856
0.1 0.034
0.075 0.03089
0.05 0.02656
0.025 0.02011
0.0125 0.01489
0 0
0.0125 -0.01489
0.025 -0.02011
0.05 -0.02656
0.075 -0.03089
0.1 -0.034
0.15 -0.03856
0.2 -0.04178
0.3 -0.04578
0.4 -0.04822
0.5 -0.04956
0.6 -0.05
0.7 -0.04889
0.8 -0.043
0.9 -0.02833
0.95 -0.01656
1 -0.001

naca001066 Airfoil CAD files

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