NACA 64(1)-212 airfoil
n64212 Airfoil (x,y) Coordinates
| 0 | 0 |
| 0.00418 | 0.01025 |
| 0.00659 | 0.01245 |
| 0.01147 | 0.01593 |
| 0.02382 | 0.02218 |
| 0.04868 | 0.03123 |
| 0.07364 | 0.03815 |
| 0.09865 | 0.04386 |
| 0.14872 | 0.05291 |
| 0.19886 | 0.05968 |
| 0.24903 | 0.0647 |
| 0.29921 | 0.06815 |
| 0.34941 | 0.07008 |
| 0.39961 | 0.07052 |
| 0.44982 | 0.06893 |
| 0.5 | 0.06583 |
| 0.55016 | 0.06151 |
| 0.60029 | 0.05619 |
| 0.65039 | 0.05004 |
| 0.70045 | 0.04322 |
| 0.75047 | 0.0359 |
| 0.80045 | 0.02825 |
| 0.85038 | 0.02054 |
| 0.90027 | 0.01303 |
| 0.95013 | 0.00604 |
| 1 | 0 |
| 0.94987 | 0.00028 |
| 0.89973 | -0.00269 |
| 0.84962 | -0.00708 |
| 0.79955 | -0.01233 |
| 0.74953 | -0.018 |
| 0.69955 | -0.02378 |
| 0.64961 | -0.02944 |
| 0.59971 | -0.03477 |
| 0.54984 | -0.03961 |
| 0.5 | -0.04377 |
| 0.45018 | -0.04703 |
| 0.40039 | -0.0491 |
| 0.35059 | -0.04948 |
| 0.30079 | -0.04871 |
| 0.25097 | -0.0468 |
| 0.20114 | -0.04376 |
| 0.15128 | -0.03945 |
| 0.10135 | -0.03352 |
| 0.07636 | -0.02967 |
| 0.05132 | -0.02491 |
| 0.02618 | -0.01846 |
| 0.01353 | -0.01379 |
| 0.00841 | -0.01105 |
| 0.00582 | -0.00925 |
| 0 | 0 |
n64212 Airfoil CAD files