NACA 0006 airfoil
naca0006 Airfoil (x,y) Coordinates
| 1 | 0.00063 |
| 0.95 | 0.00403 |
| 0.9 | 0.00724 |
| 0.8 | 0.01312 |
| 0.7 | 0.01832 |
| 0.6 | 0.02282 |
| 0.5 | 0.02647 |
| 0.4 | 0.02902 |
| 0.3 | 0.03001 |
| 0.25 | 0.02971 |
| 0.2 | 0.02869 |
| 0.15 | 0.02673 |
| 0.1 | 0.02341 |
| 0.075 | 0.021 |
| 0.05 | 0.01777 |
| 0.025 | 0.01307 |
| 0.0125 | 0.00947 |
| 0 | 0 |
| 0.0125 | -0.00947 |
| 0.025 | -0.01307 |
| 0.05 | -0.01777 |
| 0.075 | -0.021 |
| 0.1 | -0.02341 |
| 0.15 | -0.02673 |
| 0.2 | -0.02869 |
| 0.25 | -0.02971 |
| 0.3 | -0.03001 |
| 0.4 | -0.02902 |
| 0.5 | -0.02647 |
| 0.6 | -0.02282 |
| 0.7 | -0.01832 |
| 0.8 | -0.01312 |
| 0.9 | -0.00724 |
| 0.95 | -0.00403 |
| 1 | -0.00063 |
naca0006 Airfoil CAD files