NACA 64-008A airfoil
n64008a Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.005 | 0.00646 |
| 0.0075 | 0.00778 |
| 0.0125 | 0.00983 |
| 0.025 | 0.01353 |
| 0.05 | 0.01863 |
| 0.075 | 0.02245 |
| 0.1 | 0.02559 |
| 0.15 | 0.03047 |
| 0.2 | 0.03414 |
| 0.25 | 0.03681 |
| 0.3 | 0.03866 |
| 0.35 | 0.03972 |
| 0.4 | 0.03998 |
| 0.45 | 0.03921 |
| 0.5 | 0.03757 |
| 0.55 | 0.03524 |
| 0.6 | 0.03234 |
| 0.65 | 0.02897 |
| 0.7 | 0.02521 |
| 0.75 | 0.02117 |
| 0.8 | 0.01698 |
| 0.85 | 0.01278 |
| 0.9 | 0.00858 |
| 0.95 | 0.00438 |
| 1 | 0.00018 |
| 0.95 | -0.00438 |
| 0.9 | -0.00858 |
| 0.85 | -0.01278 |
| 0.8 | -0.01698 |
| 0.75 | -0.02117 |
| 0.7 | -0.02521 |
| 0.65 | -0.02897 |
| 0.6 | -0.03234 |
| 0.55 | -0.03524 |
| 0.5 | -0.03757 |
| 0.45 | -0.03921 |
| 0.4 | -0.03998 |
| 0.35 | -0.03972 |
| 0.3 | -0.03866 |
| 0.25 | -0.03681 |
| 0.2 | -0.03414 |
| 0.15 | -0.03047 |
| 0.1 | -0.02559 |
| 0.075 | -0.02245 |
| 0.05 | -0.01863 |
| 0.025 | -0.01353 |
| 0.0125 | -0.00983 |
| 0.0075 | -0.00778 |
| 0.005 | -0.00646 |
| 0 | 0 |
n64008a Airfoil CAD files