NACA 5-H-15 rotorcraft airfoil
n5h15 Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.0125 | 0.01607 |
| 0.025 | 0.02615 |
| 0.05 | 0.0405 |
| 0.075 | 0.05205 |
| 0.1 | 0.0617 |
| 0.15 | 0.077 |
| 0.2 | 0.0884 |
| 0.25 | 0.0974 |
| 0.3 | 0.1044 |
| 0.4 | 0.1056 |
| 0.5 | 0.0979 |
| 0.6 | 0.0801 |
| 0.7 | 0.0557 |
| 0.8 | 0.0294 |
| 0.9 | 0.0099 |
| 0.95 | 0.0041 |
| 1 | 0 |
| 0.95 | -0.0094 |
| 0.9 | -0.0188 |
| 0.8 | -0.0357 |
| 0.7 | -0.0448 |
| 0.6 | -0.049 |
| 0.5 | -0.0496 |
| 0.4 | -0.0486 |
| 0.3 | -0.0461 |
| 0.25 | -0.0441 |
| 0.2 | -0.0418 |
| 0.15 | -0.0377 |
| 0.1 | -0.0333 |
| 0.075 | -0.03005 |
| 0.05 | -0.0268 |
| 0.025 | -0.02235 |
| 0.0125 | -0.01783 |
| 0 | 0 |
n5h15 Airfoil CAD files