Dillner 20-32-C low Reynolds number airfoil
2032c Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.0125 | 0.0193 |
| 0.025 | 0.0317 |
| 0.05 | 0.0513 |
| 0.075 | 0.0664 |
| 0.1 | 0.078 |
| 0.15 | 0.0934 |
| 0.2 | 0.1013 |
| 0.25 | 0.1044 |
| 0.3 | 0.1048 |
| 0.4 | 0.1002 |
| 0.5 | 0.0905 |
| 0.6 | 0.0771 |
| 0.7 | 0.061 |
| 0.8 | 0.0428 |
| 0.9 | 0.0229 |
| 0.95 | 0.0124 |
| 1 | 0.0016 |
| 1 | -0.0016 |
| 0.95 | 0.0044 |
| 0.9 | 0.01 |
| 0.8 | 0.0202 |
| 0.7 | 0.0286 |
| 0.6 | 0.035 |
| 0.5 | 0.0386 |
| 0.4 | 0.0385 |
| 0.3 | 0.0333 |
| 0.25 | 0.0282 |
| 0.2 | 0.0217 |
| 0.15 | 0.0145 |
| 0.1 | 0.0068 |
| 0.075 | 0.0028 |
| 0.05 | -0.001 |
| 0.025 | -0.0042 |
| 0.0125 | -0.005 |
| 0 | 0 |
2032c Airfoil CAD files