NACA 1410 airfoil
naca1410 Airfoil (x,y) Coordinates
| 1 | 0.00105 |
| 0.95021 | 0.00832 |
| 0.90034 | 0.01513 |
| 0.80049 | 0.02741 |
| 0.70051 | 0.03804 |
| 0.60042 | 0.04692 |
| 0.50025 | 0.05385 |
| 0.4 | 0.05836 |
| 0.29937 | 0.0594 |
| 0.24907 | 0.05809 |
| 0.1988 | 0.05531 |
| 0.14861 | 0.05062 |
| 0.09854 | 0.04338 |
| 0.07358 | 0.03837 |
| 0.0487 | 0.03194 |
| 0.02398 | 0.02297 |
| 0.01174 | 0.01639 |
| 0 | 0 |
| 0.01326 | -0.01515 |
| 0.02602 | -0.02055 |
| 0.0513 | -0.02726 |
| 0.07642 | -0.03157 |
| 0.10146 | -0.03462 |
| 0.15139 | -0.03844 |
| 0.2012 | -0.04031 |
| 0.25093 | -0.04091 |
| 0.30063 | -0.04064 |
| 0.4 | -0.03936 |
| 0.49975 | -0.03439 |
| 0.59958 | -0.02914 |
| 0.69949 | -0.02304 |
| 0.79951 | -0.01629 |
| 0.89966 | -0.00901 |
| 0.94979 | -0.00512 |
| 1 | -0.00105 |
naca1410 Airfoil CAD files