NACA 8-H-12 rotorcraft airfoil
n8h12 Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.0036 | 0.0152 |
| 0.008 | 0.0201 |
| 0.0198 | 0.0294 |
| 0.0442 | 0.0431 |
| 0.0691 | 0.0538 |
| 0.0943 | 0.0626 |
| 0.145 | 0.0763 |
| 0.1961 | 0.086 |
| 0.2475 | 0.0924 |
| 0.2997 | 0.0953 |
| 0.4029 | 0.0903 |
| 0.5039 | 0.0767 |
| 0.6036 | 0.0585 |
| 0.7025 | 0.0384 |
| 0.8011 | 0.0189 |
| 0.9001999 | 0.0034 |
| 0.9499 | 0.0012 |
| 1 | 0 |
| 0.95 | -0.0063 |
| 0.8998001 | -0.0105 |
| 0.7988 | -0.0164 |
| 0.5964 | -0.0229 |
| 0.4961 | -0.0244 |
| 0.3971 | -0.0249 |
| 0.3003 | -0.0245 |
| 0.2525 | -0.0242 |
| 0.2039 | -0.0235 |
| 0.155 | -0.0224 |
| 0.1057 | -0.0206 |
| 0.0809 | -0.0192 |
| 0.0558 | -0.0174 |
| 0.0302 | -0.0141 |
| 0.0169 | -0.0112 |
| 0.0114 | -0.0095 |
| 0 | 0 |
n8h12 Airfoil CAD files