NACA 64-108 airfoil
n64108 Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.00472 | 0.00682 |
| 0.00719 | 0.00828 |
| 0.01215 | 0.01058 |
| 0.0246 | 0.01457 |
| 0.04956 | 0.02032 |
| 0.07455 | 0.02471 |
| 0.09955 | 0.02832 |
| 0.14958 | 0.03405 |
| 0.19962 | 0.03835 |
| 0.24968 | 0.04152 |
| 0.29974 | 0.0437 |
| 0.3498 | 0.04494 |
| 0.39987 | 0.04528 |
| 0.44994 | 0.04431 |
| 0.5 | 0.04236 |
| 0.55005 | 0.03959 |
| 0.6001 | 0.03617 |
| 0.65013 | 0.03219 |
| 0.70015 | 0.02777 |
| 0.75016 | 0.02302 |
| 0.80015 | 0.01802 |
| 0.85013 | 0.01297 |
| 0.9001 | 0.00808 |
| 0.95005 | 0.00364 |
| 1 | 0 |
| 0.94995 | -0.00048 |
| 0.8999 | -0.00292 |
| 0.84987 | -0.00625 |
| 0.79985 | -0.01006 |
| 0.74984 | -0.01406 |
| 0.69985 | -0.01805 |
| 0.64987 | -0.02189 |
| 0.5999 | -0.02545 |
| 0.54995 | -0.02863 |
| 0.5 | -0.03132 |
| 0.45006 | -0.03335 |
| 0.40013 | -0.03456 |
| 0.3502 | -0.03464 |
| 0.30026 | -0.03398 |
| 0.25032 | -0.03256 |
| 0.20038 | -0.03039 |
| 0.15042 | -0.02733 |
| 0.10045 | -0.02316 |
| 0.07545 | -0.02047 |
| 0.05044 | -0.01716 |
| 0.0254 | -0.01271 |
| 0.01285 | -0.0095 |
| 0.00781 | -0.00758 |
| 0.00528 | -0.00632 |
| 0 | 0 |
n64108 Airfoil CAD files