n64212 Airfoil

 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

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