naca000834 Airfoil
naca000834 Airfoil (x,y) Coordinates
| 1 | 0.0008 |
| 0.95 | 0.00684 |
| 0.9 | 0.01244 |
| 0.8 | 0.02213 |
| 0.7 | 0.02987 |
| 0.6 | 0.03547 |
| 0.5 | 0.03884 |
| 0.4 | 0.04 |
| 0.3 | 0.03867 |
| 0.2 | 0.03396 |
| 0.15 | 0.02996 |
| 0.1 | 0.02436 |
| 0.075 | 0.02089 |
| 0.05 | 0.01662 |
| 0.025 | 0.0112 |
| 0.0125 | 0.00756 |
| 0 | 0 |
| 0.0125 | -0.00756 |
| 0.025 | -0.0112 |
| 0.05 | -0.01662 |
| 0.075 | -0.02089 |
| 0.1 | -0.02436 |
| 0.15 | -0.02996 |
| 0.2 | -0.03396 |
| 0.3 | -0.03867 |
| 0.4 | -0.04 |
| 0.5 | -0.03884 |
| 0.6 | -0.03547 |
| 0.7 | -0.02987 |
| 0.8 | -0.02213 |
| 0.9 | -0.01244 |
| 0.95 | -0.00684 |
| 1 | -0.0008 |
naca000834 Airfoil CAD files