NACA 5-H-10 rotorcraft airfoil
n5h10 Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.0125 | 0.015 |
| 0.025 | 0.021 |
| 0.05 | 0.031 |
| 0.075 | 0.038 |
| 0.1 | 0.0437 |
| 0.15 | 0.053 |
| 0.2 | 0.061 |
| 0.25 | 0.066 |
| 0.3 | 0.069 |
| 0.4 | 0.072 |
| 0.5 | 0.067 |
| 0.6 | 0.055 |
| 0.7 | 0.039 |
| 0.8 | 0.02 |
| 0.9 | 0.0067 |
| 0.96 | 0.0027 |
| 1 | 0 |
| 0.96 | -0.0047 |
| 0.9 | -0.011 |
| 0.8 | -0.024 |
| 0.7 | -0.029 |
| 0.6 | -0.029 |
| 0.5 | -0.028 |
| 0.4 | -0.027 |
| 0.3 | -0.025 |
| 0.25 | -0.024 |
| 0.2 | -0.023 |
| 0.15 | -0.021 |
| 0.1 | -0.0185 |
| 0.075 | -0.0168 |
| 0.05 | -0.015 |
| 0.025 | -0.012 |
| 0.0125 | -0.0093 |
| 0 | 0 |
n5h10 Airfoil CAD files