naca0015 Airfoil

NACA 0015 airfoil

naca0015 Airfoil (x,y) Coordinates

1 0.00158
0.95 0.01008
0.9 0.0181
0.8 0.03279
0.7 0.0458
0.6 0.05704
0.5 0.06617
0.4 0.07254
0.3 0.07502
0.25 0.07427
0.2 0.07172
0.15 0.06682
0.1 0.05853
0.075 0.0525
0.05 0.04443
0.025 0.03268
0.0125 0.02367
0 0
0.0125 -0.02367
0.025 -0.03268
0.05 -0.04443
0.075 -0.0525
0.1 -0.05853
0.15 -0.06682
0.2 -0.07172
0.25 -0.07427
0.3 -0.07502
0.4 -0.07254
0.5 -0.06617
0.6 -0.05704
0.7 -0.0458
0.8 -0.03279
0.9 -0.0181
0.95 -0.01008
1 -0.00158

naca0015 Airfoil CAD files

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