NACA 0010-65 airfoil
naca001065 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 | 0.04889 |
| 0.3 | 0.04578 |
| 0.2 | 0.04089 |
| 0.15 | 0.03756 |
| 0.1 | 0.033 |
| 0.075 | 0.02989 |
| 0.05 | 0.02589 |
| 0.025 | 0.01967 |
| 0.0125 | 0.01467 |
| 0 | 0 |
| 0.0125 | -0.01467 |
| 0.025 | -0.01967 |
| 0.05 | -0.02589 |
| 0.075 | -0.02989 |
| 0.1 | -0.033 |
| 0.15 | -0.03756 |
| 0.2 | -0.04089 |
| 0.3 | -0.04578 |
| 0.4 | -0.04889 |
| 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 |
naca001065 Airfoil CAD files