NACA 5-H-20 rotorcraft airfoil
n5h20 Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.0125 | 0.031 |
| 0.025 | 0.043 |
| 0.05 | 0.061 |
| 0.075 | 0.076 |
| 0.1 | 0.087 |
| 0.15 | 0.107 |
| 0.2 | 0.121 |
| 0.25 | 0.131 |
| 0.3 | 0.137 |
| 0.4 | 0.144 |
| 0.5 | 0.135 |
| 0.6 | 0.111 |
| 0.7 | 0.079 |
| 0.8 | 0.041 |
| 0.9 | 0.013 |
| 0.95 | 0.0053 |
| 1 | 0 |
| 0.95 | -0.0093 |
| 0.9 | -0.021 |
| 0.8 | -0.048 |
| 0.7 | -0.059 |
| 0.6 | -0.059 |
| 0.5 | -0.057 |
| 0.4 | -0.055 |
| 0.3 | -0.0507 |
| 0.25 | -0.048 |
| 0.2 | -0.045 |
| 0.15 | -0.041 |
| 0.1 | -0.036 |
| 0.075 | -0.0325 |
| 0.05 | -0.029 |
| 0.025 | -0.024 |
| 0.0125 | -0.019 |
| 0 | 0 |
n5h20 Airfoil CAD files