N-12 airfoil
n12 Airfoil (x,y) Co-ordinates
| 1 | 0 |
| 0.95 | 0.0086 |
| 0.9 | 0.0138 |
| 0.8 | 0.0242 |
| 0.7 | 0.034 |
| 0.6 | 0.0418 |
| 0.5 | 0.048 |
| 0.4 | 0.052 |
| 0.3 | 0.0528 |
| 0.2 | 0.0508 |
| 0.15 | 0.0472 |
| 0.1 | 0.0392 |
| 0.075 | 0.0352 |
| 0.05 | 0.0292 |
| 0.025 | 0.021 |
| 0.0125 | 0.0154 |
| 0 | 0 |
| 0.0125 | -0.0152 |
| 0.025 | -0.02 |
| 0.05 | -0.028 |
| 0.075 | -0.0348 |
| 0.1 | -0.0386 |
| 0.15 | -0.044 |
| 0.2 | -0.048 |
| 0.3 | -0.0518 |
| 0.4 | -0.05 |
| 0.5 | -0.047 |
| 0.6 | -0.0418 |
| 0.7 | -0.034 |
| 0.8 | -0.0246 |
| 0.9 | -0.0134 |
| 0.95 | -0.008 |
| 1 | 0 |
n12 Airfoil CAD files