NACA 6-H-20 rotorcraft airfoil
n6h20 Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.0125 | 0.033 |
| 0.025 | 0.047 |
| 0.05 | 0.067 |
| 0.075 | 0.083 |
| 0.1 | 0.096 |
| 0.15 | 0.1196 |
| 0.2 | 0.135 |
| 0.25 | 0.147 |
| 0.3 | 0.155 |
| 0.4 | 0.161 |
| 0.5 | 0.151 |
| 0.6 | 0.121 |
| 0.7 | 0.08 |
| 0.8 | 0.041 |
| 0.9 | 0.012 |
| 0.95 | 0.0053 |
| 1 | 0 |
| 0.95 | -0.011 |
| 0.9 | -0.023 |
| 0.8 | -0.051 |
| 0.7 | -0.057 |
| 0.6 | -0.051 |
| 0.5 | -0.043 |
| 0.4 | -0.0385 |
| 0.3 | -0.0356 |
| 0.25 | -0.0334 |
| 0.2 | -0.032 |
| 0.15 | -0.0305 |
| 0.1 | -0.0275 |
| 0.075 | -0.0254 |
| 0.05 | -0.023 |
| 0.025 | -0.019 |
| 0.0125 | -0.015 |
| 0 | 0 |
n6h20 Airfoil CAD files