n64215 Airfoil

 NACA 64(2)-215 airfoil

n64215 Airfoil (x,y) Coordinates

0 0
0.00399 0.01254
0.00637 0.01522
0.01122 0.01945
0.02353 0.0271
0.04836 0.03816
0.07331 0.04661
0.09831 0.05356
0.1484 0.06456
0.19857 0.07274
0.24878 0.07879
0.29901 0.0829
0.34926 0.08512
0.39952 0.08544
0.44977 0.08319
0.5 0.07913
0.5502 0.07361
0.60036 0.06691
0.65048 0.05925
0.70055 0.05085
0.75058 0.04191
0.80055 0.03267
0.85046 0.02349
0.90033 0.01466
0.95016 0.00662
1 0
0.94984 -0.0003
0.89967 -0.00432
0.84954 -0.01003
0.79945 -0.01675
0.74942 -0.02401
0.69945 -0.03141
0.64952 -0.03865
0.59964 -0.04549
0.5498 -0.05171
0.5 -0.05707
0.45023 -0.06129
0.40048 -0.06402
0.35074 -0.06452
0.30099 -0.06346
0.25122 -0.06089
0.20143 -0.05682
0.1516 -0.0511
0.10169 -0.04322
0.07669 -0.03813
0.05164 -0.03184
0.02647 -0.02338
0.01378 -0.01731
0.00863 -0.01382
0.00601 -0.01154
0 0

n64215 Airfoil CAD files

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