NACA 64(2)-015A airfoil
n64015a Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.005 | 0.01193 |
| 0.0075 | 0.01436 |
| 0.0125 | 0.01815 |
| 0.025 | 0.02508 |
| 0.05 | 0.03477 |
| 0.075 | 0.04202 |
| 0.1 | 0.04799 |
| 0.15 | 0.05732 |
| 0.2 | 0.06423 |
| 0.25 | 0.06926 |
| 0.3 | 0.0727 |
| 0.35 | 0.07463 |
| 0.4 | 0.07487 |
| 0.45 | 0.07313 |
| 0.5 | 0.06978 |
| 0.55 | 0.06517 |
| 0.6 | 0.05956 |
| 0.65 | 0.05311 |
| 0.7 | 0.046 |
| 0.75 | 0.03847 |
| 0.8 | 0.03084 |
| 0.85 | 0.02321 |
| 0.9 | 0.01558 |
| 0.95 | 0.00795 |
| 1 | 0.00032 |
| 0.95 | -0.00795 |
| 0.9 | -0.01558 |
| 0.85 | -0.02321 |
| 0.8 | -0.03084 |
| 0.75 | -0.03847 |
| 0.7 | -0.046 |
| 0.65 | -0.05311 |
| 0.6 | -0.05956 |
| 0.55 | -0.06517 |
| 0.5 | -0.06978 |
| 0.45 | -0.07313 |
| 0.4 | -0.07487 |
| 0.35 | -0.07463 |
| 0.3 | -0.0727 |
| 0.25 | -0.06926 |
| 0.2 | -0.06423 |
| 0.15 | -0.05732 |
| 0.1 | -0.04799 |
| 0.075 | -0.04202 |
| 0.05 | -0.03477 |
| 0.025 | -0.02508 |
| 0.0125 | -0.01815 |
| 0.0075 | -0.01436 |
| 0.005 | -0.01193 |
| 0 | 0 |
n64015a Airfoil CAD files