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