n63415 Airfoil

NACA 63(2)-415 airfoil

n63415 Airfoil (x,y) Coordinates

0 0
0.003 0.01287
0.00525 0.01585
0.00991 0.02074
0.02198 0.02964
0.0466 0.04264
0.07147 0.05261
0.09647 0.06077
0.14669 0.07348
0.19705 0.08279
0.2475 0.08941
0.298 0.09362
0.34852 0.09559
0.39905 0.09527
0.44955 0.09289
0.5 0.08871
0.55039 0.08298
0.6007 0.07595
0.65093 0.0678
0.70106 0.05877
0.75109 0.04907
0.80102 0.039
0.85085 0.02885
0.90059 0.01884
0.95028 0.00931
1 0
0.94972 0.00333
0.89941 0.00184
0.84915 -0.00193
0.79989 -0.00716
0.74891 -0.01327
0.69894 -0.01989
0.64907 -0.0266
0.5993 -0.03311
0.54961 -0.03918
0.5 -0.04459
0.45045 -0.04909
0.40095 -0.05243
0.35148 -0.05439
0.302 -0.05474
0.2525 -0.05361
0.20295 -0.05095
0.15331 -0.04656
0.10353 -0.04009
0.07853 -0.03565
0.0534 -0.03
0.02802 -0.0222
0.01509 -0.01646
0.00975 -0.01305
0.007 -0.01087
0 0

n63415 Airfoil CAD files

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