NACA 63(2)-215 airfoil
n63215 Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.00399 | 0.0125 |
| 0.00637 | 0.01528 |
| 0.0112 | 0.0198 |
| 0.02348 | 0.02792 |
| 0.04829 | 0.0396 |
| 0.07323 | 0.04847 |
| 0.09823 | 0.05569 |
| 0.14834 | 0.06682 |
| 0.19852 | 0.07487 |
| 0.24875 | 0.08049 |
| 0.299 | 0.08392 |
| 0.34926 | 0.0853 |
| 0.39952 | 0.08457 |
| 0.44977 | 0.08194 |
| 0.5 | 0.07768 |
| 0.55019 | 0.07203 |
| 0.60035 | 0.06524 |
| 0.65047 | 0.05751 |
| 0.70053 | 0.04906 |
| 0.75055 | 0.04014 |
| 0.80051 | 0.03105 |
| 0.85043 | 0.02213 |
| 0.9003 | 0.01368 |
| 0.95014 | 0.00616 |
| 1 | 0 |
| 0.94986 | 0.00016 |
| 0.8997 | -0.00334 |
| 0.84957 | -0.00867 |
| 0.79949 | -0.01513 |
| 0.74945 | -0.02224 |
| 0.69947 | -0.02962 |
| 0.64953 | -0.03691 |
| 0.59965 | -0.04382 |
| 0.54981 | -0.05013 |
| 0.5 | -0.05562 |
| 0.45023 | -0.06004 |
| 0.40048 | -0.06315 |
| 0.35074 | -0.0647 |
| 0.301 | -0.06448 |
| 0.25125 | -0.06259 |
| 0.20148 | -0.05895 |
| 0.15166 | -0.05336 |
| 0.10177 | -0.04535 |
| 0.07677 | -0.03999 |
| 0.05171 | -0.03328 |
| 0.02652 | -0.0242 |
| 0.0138 | -0.01766 |
| 0.00863 | -0.01388 |
| 0.00601 | -0.0115 |
| 0 | 0 |
n63215 Airfoil CAD files