NACA 63-015A airfoil
n63015a Airfoil (x,y) Co-ordinates
| 0 | 0 |
| 0.005 | 0.01203 |
| 0.0075 | 0.01448 |
| 0.0125 | 0.01844 |
| 0.025 | 0.02579 |
| 0.05 | 0.03618 |
| 0.075 | 0.04382 |
| 0.1 | 0.04997 |
| 0.15 | 0.05942 |
| 0.2 | 0.06619 |
| 0.25 | 0.07091 |
| 0.3 | 0.07384 |
| 0.35 | 0.07496 |
| 0.4 | 0.07435 |
| 0.45 | 0.07215 |
| 0.5 | 0.06858 |
| 0.55 | 0.06387 |
| 0.6 | 0.0582 |
| 0.65 | 0.05173 |
| 0.7 | 0.04468 |
| 0.75 | 0.03731 |
| 0.8 | 0.02991 |
| 0.85 | 0.02252 |
| 0.9 | 0.01512 |
| 0.95 | 0.00772 |
| 1 | 0.00032 |
| 0.95 | -0.00772 |
| 0.9 | -0.01512 |
| 0.85 | -0.02252 |
| 0.8 | -0.02991 |
| 0.75 | -0.03731 |
| 0.7 | -0.04468 |
| 0.65 | -0.05173 |
| 0.6 | -0.0582 |
| 0.55 | -0.06387 |
| 0.5 | -0.06858 |
| 0.45 | -0.07215 |
| 0.4 | -0.07435 |
| 0.35 | -0.07496 |
| 0.3 | -0.07384 |
| 0.25 | -0.07091 |
| 0.2 | -0.06619 |
| 0.15 | -0.05942 |
| 0.1 | -0.04997 |
| 0.075 | -0.04382 |
| 0.05 | -0.03618 |
| 0.025 | -0.02579 |
| 0.0125 | -0.01844 |
| 0.0075 | -0.01448 |
| 0.005 | -0.01203 |
| 0 | 0 |
n63015a Airfoil CAD files