NACA 0018 airfoil
naca0018 Airfoil (x,y) Coordinates
| 1 | 0.00189 |
| 0.95 | 0.0121 |
| 0.9 | 0.02172 |
| 0.8 | 0.03935 |
| 0.7 | 0.05496 |
| 0.6 | 0.06845 |
| 0.5 | 0.07941 |
| 0.4 | 0.08705 |
| 0.3 | 0.09003 |
| 0.25 | 0.08912 |
| 0.2 | 0.08606 |
| 0.15 | 0.08018 |
| 0.1 | 0.07024 |
| 0.075 | 0.063 |
| 0.05 | 0.05332 |
| 0.025 | 0.03922 |
| 0.0125 | 0.02841 |
| 0 | 0 |
| 0.0125 | -0.02841 |
| 0.025 | -0.03922 |
| 0.05 | -0.05332 |
| 0.075 | -0.063 |
| 0.1 | -0.07024 |
| 0.15 | -0.08018 |
| 0.2 | -0.08606 |
| 0.25 | -0.08912 |
| 0.3 | -0.09003 |
| 0.4 | -0.08705 |
| 0.5 | -0.07941 |
| 0.6 | -0.06845 |
| 0.7 | -0.05496 |
| 0.8 | -0.03935 |
| 0.9 | -0.02172 |
| 0.95 | -0.0121 |
| 1 | -0.00189 |
naca0018 Airfoil CAD files