Liebeck high lift airfoil
L1003 Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.0125 | 0.02307 |
| 0.025 | 0.03981 |
| 0.0375 | 0.05093 |
| 0.05 | 0.06296 |
| 0.075 | 0.08333 |
| 0.1 | 0.09722 |
| 0.15 | 0.12222 |
| 0.2 | 0.13704 |
| 0.25 | 0.14815 |
| 0.3 | 0.1537 |
| 0.35 | 0.14815 |
| 0.4 | 0.13518 |
| 0.45 | 0.11852 |
| 0.5 | 0.0963 |
| 0.55 | 0.08056 |
| 0.6 | 0.06667 |
| 0.65 | 0.05185 |
| 0.7 | 0.04074 |
| 0.75 | 0.0287 |
| 0.8 | 0.02037 |
| 0.85 | 0.01204 |
| 0.9 | 0.00556 |
| 0.95 | 0.00185 |
| 1 | 0 |
| 1 | 0 |
| 0.95 | -0.00093 |
| 0.9 | -0.00185 |
| 0.85 | -0.00278 |
| 0.8 | -0.0037 |
| 0.75 | -0.00556 |
| 0.7 | -0.00741 |
| 0.65 | -0.00926 |
| 0.6 | -0.01111 |
| 0.55 | -0.01296 |
| 0.5 | -0.01481 |
| 0.45 | -0.01667 |
| 0.4 | -0.01852 |
| 0.35 | -0.02037 |
| 0.3 | -0.02315 |
| 0.25 | -0.02593 |
| 0.2 | -0.0287 |
| 0.15 | -0.03333 |
| 0.1 | -0.03981 |
| 0.075 | -0.04352 |
| 0.05 | -0.04907 |
| 0.0375 | -0.04907 |
| 0.025 | -0.0463 |
| 0.0125 | -0.03704 |
| 0 | 0 |
L1003 Airfoil CAD files