NACA 64-110 airfoil
n64110 Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.00465 | 0.00844 |
| 0.00712 | 0.01023 |
| 0.01207 | 0.01303 |
| 0.0245 | 0.01793 |
| 0.04945 | 0.025 |
| 0.07443 | 0.03037 |
| 0.09944 | 0.03479 |
| 0.14947 | 0.04178 |
| 0.19953 | 0.047 |
| 0.24959 | 0.05087 |
| 0.29967 | 0.0535 |
| 0.34975 | 0.05495 |
| 0.39984 | 0.05524 |
| 0.44992 | 0.05391 |
| 0.5 | 0.05138 |
| 0.55007 | 0.04786 |
| 0.60012 | 0.04356 |
| 0.65016 | 0.0386 |
| 0.70019 | 0.03313 |
| 0.7502 | 0.02729 |
| 0.80019 | 0.0212 |
| 0.85016 | 0.01512 |
| 0.90012 | 0.00929 |
| 0.95006 | 0.00406 |
| 1 | 0 |
| 0.94994 | -0.0009 |
| 0.89988 | -0.00413 |
| 0.84984 | -0.0084 |
| 0.79981 | -0.01324 |
| 0.7498 | -0.01833 |
| 0.69981 | -0.02341 |
| 0.64984 | -0.0283 |
| 0.59988 | -0.03284 |
| 0.54993 | -0.0369 |
| 0.5 | -0.04034 |
| 0.45008 | -0.04295 |
| 0.40016 | -0.04452 |
| 0.35025 | -0.04465 |
| 0.30033 | -0.04378 |
| 0.25041 | -0.04191 |
| 0.20047 | -0.03904 |
| 0.15053 | -0.03506 |
| 0.10056 | -0.02963 |
| 0.07557 | -0.02613 |
| 0.05055 | -0.02184 |
| 0.0255 | -0.01607 |
| 0.01293 | -0.01195 |
| 0.00788 | -0.00953 |
| 0.00535 | -0.00794 |
| 0 | 0 |
n64110 Airfoil CAD files