n63212 Airfoil

NACA 63(1)-212 airfoil

n63212 Airfoil (x,y) Coordinates

0 0
0.00417 0.01032
0.00657 0.0126
0.01145 0.01622
0.02378 0.02284
0.04863 0.03238
0.07358 0.03963
0.09859 0.04554
0.14868 0.0547
0.19882 0.06137
0.249 0.06606
0.2992 0.06901
0.34941 0.0703
0.39962 0.06991
0.44982 0.06799
0.5 0.06473
0.55016 0.0603
0.60029 0.05491
0.65038 0.0487
0.70043 0.04182
0.75045 0.03451
0.80042 0.02698
0.85035 0.01947
0.90025 0.01224
0.95012 0.00566
1 0
0.94988 0.00066
0.89975 -0.0019
0.84965 -0.00601
0.79958 -0.01106
0.74955 -0.01661
0.69957 -0.02238
0.64962 -0.0281
0.59971 -0.03349
0.54848 -0.0384
0.5 -0.04267
0.45018 -0.04609
0.40038 -0.04849
0.35059 -0.0497
0.3008 -0.04957
0.251 -0.04816
0.20118 -0.04545
0.15132 -0.04124
0.10141 -0.0352
0.07642 -0.03115
0.05137 -0.02606
0.02622 -0.01912
0.01355 -0.01408
0.00843 -0.0112
0.00538 -0.00932
0 0

n63212 Airfoil CAD files

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