Boeing KC-135 winglet airfoil
kc135winglet Airfoil (x,y) Co-ordinates
| 1 | -0.002 |
| 0.975 | 0.0038 |
| 0.95 | 0.0089 |
| 0.925 | 0.0138 |
| 0.9 | 0.0184 |
| 0.875 | 0.0228 |
| 0.85 | 0.027 |
| 0.825 | 0.0311 |
| 0.8 | 0.0349 |
| 0.775 | 0.0384 |
| 0.75 | 0.0419 |
| 0.725 | 0.0451 |
| 0.7 | 0.0481 |
| 0.675 | 0.0508 |
| 0.65 | 0.0533 |
| 0.625 | 0.0554 |
| 0.6 | 0.0572 |
| 0.575 | 0.0587 |
| 0.55 | 0.0599 |
| 0.5 | 0.0618 |
| 0.45 | 0.0627 |
| 0.4 | 0.0628 |
| 0.35 | 0.0621 |
| 0.3 | 0.0605 |
| 0.25 | 0.0581 |
| 0.2 | 0.0547 |
| 0.175 | 0.0525 |
| 0.15 | 0.0499 |
| 0.125 | 0.0469 |
| 0.1 | 0.0433 |
| 0.075 | 0.0389 |
| 0.05 | 0.0333 |
| 0.0375 | 0.0296 |
| 0.025 | 0.0249 |
| 0.0125 | 0.0179 |
| 0.005 | 0.0119 |
| 0.002 | 0.0077 |
| 1 | -0.0067 |
| 0.975 | -0.0013 |
| 0.95 | 0.0021 |
| 0.925 | 0.0045 |
| 0.9 | 0.0059 |
| 0.875 | 0.0064 |
| 0.85 | 0.0065 |
| 0.825 | 0.006 |
| 0.8 | 0.0049 |
| 0.775 | 0.0036 |
| 0.75 | 0.002 |
| 0.725 | 0.0004 |
| 0.7 | -0.0015 |
| 0.675 | -0.0033 |
| 0.65 | -0.0052 |
| 0.625 | -0.0071 |
| 0.6 | -0.009 |
| 0.575 | -0.0106 |
| 0.55 | -0.0122 |
| 0.5 | -0.0144 |
| 0.45 | -0.0158 |
| 0.4 | -0.0168 |
| 0.35 | -0.0174 |
| 0.3 | -0.0176 |
| 0.25 | -0.0175 |
| 0.2 | -0.0167 |
| 0.175 | -0.0161 |
| 0.15 | -0.0154 |
| 0.125 | -0.0144 |
| 0.1 | -0.0132 |
| 0.075 | -0.0118 |
| 0.05 | -0.01 |
| 0.0375 | -0.009 |
| 0.025 | -0.0077 |
| 0.0125 | -0.006 |
| 0.005 | -0.0041 |
| 0.002 | -0.0032 |
| 0 | 0 |
kc135winglet Airfoil CAD files