NACA 2-H-15 rotorcraft airfoil
n2h15 Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.0125 | 0.01921 |
| 0.025 | 0.02781 |
| 0.05 | 0.04133 |
| 0.075 | 0.05244 |
| 0.1 | 0.06195 |
| 0.15 | 0.07798 |
| 0.2 | 0.0913 |
| 0.25 | 0.10172 |
| 0.3 | 0.10985 |
| 0.4 | 0.1186 |
| 0.5 | 0.11635 |
| 0.6 | 0.1 |
| 0.7 | 0.06815 |
| 0.8 | 0.0305 |
| 0.9 | 0.00695 |
| 0.95 | 0.00157 |
| 1 | 0 |
| 0.95 | -0.02443 |
| 0.9 | -0.02545 |
| 0.8 | -0.0276 |
| 0.7 | -0.03185 |
| 0.6 | -0.032 |
| 0.5 | -0.03045 |
| 0.4 | -0.0286 |
| 0.3 | -0.02705 |
| 0.25 | -0.02638 |
| 0.2 | -0.026 |
| 0.15 | -0.02543 |
| 0.1 | -0.02475 |
| 0.075 | -0.02406 |
| 0.05 | -0.02338 |
| 0.025 | -0.02219 |
| 0.0125 | -0.01989 |
| 0 | 0 |
n2h15 Airfoil CAD files