n63210 Airfoil

NACA 63-210 airfoil

n63210 Airfoil (x,y) Coordinates

0 0
0.0043 0.00876
0.00669 0.01107
0.01162 0.01379
0.02398 0.01939
0.04886 0.02753
0.07382 0.03372
0.09882 0.03877
0.1489 0.04665
0.19902 0.0524
0.24917 0.05647
0.29933 0.0591
0.34951 0.0603
0.39968 0.06009
0.44985 0.05861
0.5 0.05599
0.55013 0.05235
0.60024 0.04786
0.65032 0.04264
0.70036 0.03684
0.75038 0.03061
0.80036 0.02414
0.8503 0.01761
0.90021 0.01212
0.9501 0.0053
1 0
0.9499 0.0012
0.89979 -0.00087
0.8497 -0.00415
0.79964 -0.00822
0.74962 -0.01271
0.69964 -0.0174
0.64968 -0.02204
0.58976 -0.02644
0.54987 -0.03045
0.5 -0.03393
0.45015 -0.03671
0.40032 -0.03867
0.35049 -0.0397
0.30067 -0.03966
0.25083 -0.03857
0.20098 -0.03648
0.1511 -0.03319
0.10118 -0.02843
0.07618 -0.02524
0.05114 -0.02121
0.02602 -0.01567
0.01338 -0.01165
0.00831 -0.00967
0.0057 -0.00776
0 0

n63210 Airfoil CAD files

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