n63215 Airfoil

NACA 63(2)-215 airfoil

n63215 Airfoil (x,y) Coordinates

0 0
0.00399 0.0125
0.00637 0.01528
0.0112 0.0198
0.02348 0.02792
0.04829 0.0396
0.07323 0.04847
0.09823 0.05569
0.14834 0.06682
0.19852 0.07487
0.24875 0.08049
0.299 0.08392
0.34926 0.0853
0.39952 0.08457
0.44977 0.08194
0.5 0.07768
0.55019 0.07203
0.60035 0.06524
0.65047 0.05751
0.70053 0.04906
0.75055 0.04014
0.80051 0.03105
0.85043 0.02213
0.9003 0.01368
0.95014 0.00616
1 0
0.94986 0.00016
0.8997 -0.00334
0.84957 -0.00867
0.79949 -0.01513
0.74945 -0.02224
0.69947 -0.02962
0.64953 -0.03691
0.59965 -0.04382
0.54981 -0.05013
0.5 -0.05562
0.45023 -0.06004
0.40048 -0.06315
0.35074 -0.0647
0.301 -0.06448
0.25125 -0.06259
0.20148 -0.05895
0.15166 -0.05336
0.10177 -0.04535
0.07677 -0.03999
0.05171 -0.03328
0.02652 -0.0242
0.0138 -0.01766
0.00863 -0.01388
0.00601 -0.0115
0 0

n63215 Airfoil CAD files

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