NACA 0015 airfoil
naca0015 Airfoil (x,y) Coordinates
| 1 | 0.00158 |
| 0.95 | 0.01008 |
| 0.9 | 0.0181 |
| 0.8 | 0.03279 |
| 0.7 | 0.0458 |
| 0.6 | 0.05704 |
| 0.5 | 0.06617 |
| 0.4 | 0.07254 |
| 0.3 | 0.07502 |
| 0.25 | 0.07427 |
| 0.2 | 0.07172 |
| 0.15 | 0.06682 |
| 0.1 | 0.05853 |
| 0.075 | 0.0525 |
| 0.05 | 0.04443 |
| 0.025 | 0.03268 |
| 0.0125 | 0.02367 |
| 0 | 0 |
| 0.0125 | -0.02367 |
| 0.025 | -0.03268 |
| 0.05 | -0.04443 |
| 0.075 | -0.0525 |
| 0.1 | -0.05853 |
| 0.15 | -0.06682 |
| 0.2 | -0.07172 |
| 0.25 | -0.07427 |
| 0.3 | -0.07502 |
| 0.4 | -0.07254 |
| 0.5 | -0.06617 |
| 0.6 | -0.05704 |
| 0.7 | -0.0458 |
| 0.8 | -0.03279 |
| 0.9 | -0.0181 |
| 0.95 | -0.01008 |
| 1 | -0.00158 |
naca0015 Airfoil CAD files