NASA/Langley 11% symmetrical supercritical airfoil
n0011sc Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.002 | 0.009225 |
| 0.0065243 | 0.015751 |
| 0.0125 | 0.020323 |
| 0.025 | 0.026208 |
| 0.0375 | 0.030242 |
| 0.05 | 0.033373 |
| 0.075 | 0.038117 |
| 0.1 | 0.041643 |
| 0.125 | 0.0444 |
| 0.15 | 0.046615 |
| 0.175 | 0.048421 |
| 0.2 | 0.049905 |
| 0.25 | 0.052125 |
| 0.3 | 0.053588 |
| 0.35 | 0.054467 |
| 0.4 | 0.054783 |
| 0.45 | 0.054571 |
| 0.5 | 0.053758 |
| 0.55 | 0.052376 |
| 0.6 | 0.05041 |
| 0.625 | 0.049198 |
| 0.65 | 0.047824 |
| 0.675 | 0.046281 |
| 0.7 | 0.044556 |
| 0.725 | 0.042635 |
| 0.75 | 0.040499 |
| 0.775 | 0.038127 |
| 0.8 | 0.035492 |
| 0.825 | 0.032564 |
| 0.85 | 0.029306 |
| 0.875 | 0.025676 |
| 0.9 | 0.021625 |
| 0.925 | 0.017099 |
| 0.95 | 0.012034 |
| 0.975 | 0.006361 |
| 1 | 0 |
| 0.975 | -0.006361 |
| 0.95 | -0.012034 |
| 0.925 | -0.017099 |
| 0.9 | -0.021625 |
| 0.875 | -0.025676 |
| 0.85 | -0.029306 |
| 0.825 | -0.032564 |
| 0.8 | -0.035492 |
| 0.775 | -0.038127 |
| 0.75 | -0.040499 |
| 0.725 | -0.042635 |
| 0.7 | -0.044556 |
| 0.675 | -0.046281 |
| 0.65 | -0.047824 |
| 0.625 | -0.049198 |
| 0.6 | -0.05041 |
| 0.55 | -0.052376 |
| 0.5 | -0.053758 |
| 0.45 | -0.054571 |
| 0.4 | -0.054783 |
| 0.35 | -0.054467 |
| 0.3 | -0.053588 |
| 0.25 | -0.052125 |
| 0.2 | -0.049905 |
| 0.175 | -0.048421 |
| 0.15 | -0.046615 |
| 0.125 | -0.0444 |
| 0.1 | -0.041643 |
| 0.075 | -0.038117 |
| 0.05 | -0.033373 |
| 0.0375 | -0.030242 |
| 0.025 | -0.026208 |
| 0.0125 | -0.020323 |
| 0.0065243 | -0.015751 |
| 0.002 | -0.009225 |
| 0 | 0 |
n0011sc Airfoil CAD files