NACA 0012-34 airfoil
naca001234 Airfoil (x,y) Coordinates
| 1 | 0.0012 |
| 0.95 | 0.01027 |
| 0.9 | 0.01867 |
| 0.8 | 0.0332 |
| 0.7 | 0.0448 |
| 0.6 | 0.0532 |
| 0.5 | 0.05827 |
| 0.4 | 0.06 |
| 0.3 | 0.058 |
| 0.2 | 0.05093 |
| 0.15 | 0.04493 |
| 0.1 | 0.03653 |
| 0.075 | 0.03133 |
| 0.05 | 0.02493 |
| 0.025 | 0.0168 |
| 0.0125 | 0.01133 |
| 0 | 0 |
| 0.0125 | -0.01133 |
| 0.025 | -0.0168 |
| 0.05 | -0.02493 |
| 0.075 | -0.03133 |
| 0.1 | -0.03653 |
| 0.15 | -0.04493 |
| 0.2 | -0.05093 |
| 0.3 | -0.058 |
| 0.4 | -0.06 |
| 0.5 | -0.05827 |
| 0.6 | -0.0532 |
| 0.7 | -0.0448 |
| 0.8 | -0.0332 |
| 0.9 | -0.01867 |
| 0.95 | -0.01027 |
| 1 | -0.0012 |
naca001234 Airfoil CAD files