NACA 64(1)-012A airfoil
n64012a Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.005 | 0.00961 |
| 0.0075 | 0.01158 |
| 0.0125 | 0.01464 |
| 0.025 | 0.02018 |
| 0.05 | 0.02788 |
| 0.075 | 0.03364 |
| 0.1 | 0.03839 |
| 0.15 | 0.0458 |
| 0.2 | 0.05132 |
| 0.25 | 0.05534 |
| 0.3 | 0.05809 |
| 0.35 | 0.05965 |
| 0.4 | 0.05993 |
| 0.45 | 0.05863 |
| 0.5 | 0.05605 |
| 0.55 | 0.05244 |
| 0.6 | 0.04801 |
| 0.65 | 0.04289 |
| 0.7 | 0.03721 |
| 0.75 | 0.03118 |
| 0.8 | 0.025 |
| 0.85 | 0.01882 |
| 0.9 | 0.01263 |
| 0.95 | 0.00644 |
| 1 | 0.00025 |
| 0.95 | -0.00644 |
| 0.9 | -0.01263 |
| 0.85 | -0.01882 |
| 0.8 | -0.025 |
| 0.75 | -0.03118 |
| 0.7 | -0.03721 |
| 0.65 | -0.04289 |
| 0.6 | -0.04801 |
| 0.55 | -0.05244 |
| 0.5 | -0.05605 |
| 0.45 | -0.05863 |
| 0.4 | -0.05993 |
| 0.35 | -0.05965 |
| 0.3 | -0.05809 |
| 0.25 | -0.05534 |
| 0.2 | -0.05132 |
| 0.15 | -0.0458 |
| 0.1 | -0.03839 |
| 0.075 | -0.03364 |
| 0.05 | -0.02788 |
| 0.025 | -0.02018 |
| 0.0125 | -0.01464 |
| 0.0075 | -0.01158 |
| 0.005 | -0.00961 |
| 0 | 0 |
n64012a Airfoil CAD files