naca1410 Airfoil

 NACA 1410 airfoil

naca1410 Airfoil (x,y) Coordinates

1 0.00105
0.95021 0.00832
0.90034 0.01513
0.80049 0.02741
0.70051 0.03804
0.60042 0.04692
0.50025 0.05385
0.4 0.05836
0.29937 0.0594
0.24907 0.05809
0.1988 0.05531
0.14861 0.05062
0.09854 0.04338
0.07358 0.03837
0.0487 0.03194
0.02398 0.02297
0.01174 0.01639
0 0
0.01326 -0.01515
0.02602 -0.02055
0.0513 -0.02726
0.07642 -0.03157
0.10146 -0.03462
0.15139 -0.03844
0.2012 -0.04031
0.25093 -0.04091
0.30063 -0.04064
0.4 -0.03936
0.49975 -0.03439
0.59958 -0.02914
0.69949 -0.02304
0.79951 -0.01629
0.89966 -0.00901
0.94979 -0.00512
1 -0.00105

naca1410 Airfoil CAD files

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