Liebeck high lift airfoil
LA5055 Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.0125 | 0.0306 |
| 0.025 | 0.0426 |
| 0.0375 | 0.0528 |
| 0.05 | 0.0611 |
| 0.075 | 0.0769 |
| 0.1 | 0.088 |
| 0.15 | 0.1065 |
| 0.2 | 0.1185 |
| 0.25 | 0.1287 |
| 0.3 | 0.1343 |
| 0.35 | 0.1389 |
| 0.4 | 0.137 |
| 0.45 | 0.1315 |
| 0.5 | 0.1194 |
| 0.55 | 0.1037 |
| 0.6 | 0.087 |
| 0.65 | 0.0704 |
| 0.7 | 0.0583 |
| 0.75 | 0.0454 |
| 0.8 | 0.0324 |
| 0.85 | 0.0222 |
| 0.9 | 0.0148 |
| 0.95 | 0.0065 |
| 1 | 0 |
| 0.95 | -0.0005 |
| 0.9 | -0.0009 |
| 0.85 | -0.0019 |
| 0.8 | -0.0037 |
| 0.75 | -0.0056 |
| 0.7 | -0.0074 |
| 0.65 | -0.0083 |
| 0.6 | -0.0102 |
| 0.55 | -0.012 |
| 0.5 | -0.0139 |
| 0.45 | -0.0148 |
| 0.4 | -0.0185 |
| 0.35 | -0.0204 |
| 0.3 | -0.0231 |
| 0.25 | -0.025 |
| 0.2 | -0.0278 |
| 0.15 | -0.0287 |
| 0.1 | -0.0306 |
| 0.075 | -0.0315 |
| 0.05 | -0.0324 |
| 0.0375 | -0.0324 |
| 0.025 | -0.0315 |
| 0.0125 | -0.0259 |
| 0 | 0 |
LA5055 Airfoil CAD files