NACA 0010-66 airfoilÂ
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