NACA 0024 airfoil
naca0024 Airfoil (x,y) Coordinates
| 1 | 0.00252 |
| 0.95 | 0.01613 |
| 0.9 | 0.02896 |
| 0.8 | 0.05247 |
| 0.7 | 0.07328 |
| 0.6 | 0.09127 |
| 0.5 | 0.10588 |
| 0.4 | 0.11607 |
| 0.3 | 0.12004 |
| 0.25 | 0.11883 |
| 0.2 | 0.11475 |
| 0.15 | 0.10691 |
| 0.1 | 0.09365 |
| 0.075 | 0.084 |
| 0.05 | 0.07109 |
| 0.025 | 0.05229 |
| 0.0125 | 0.03788 |
| 0 | 0 |
| 0.0125 | -0.03788 |
| 0.025 | -0.05229 |
| 0.05 | -0.07109 |
| 0.075 | -0.084 |
| 0.1 | -0.09365 |
| 0.15 | -0.10691 |
| 0.2 | -0.11475 |
| 0.25 | -0.11883 |
| 0.3 | -0.12004 |
| 0.4 | -0.11607 |
| 0.5 | -0.10588 |
| 0.6 | -0.09127 |
| 0.7 | -0.07328 |
| 0.8 | -0.05247 |
| 0.9 | -0.02896 |
| 0.95 | -0.01613 |
| 1 | -0.00252 |
naca0024 Airfoil CAD files