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