naca0018 Airfoil

NACA 0018 airfoil

naca0018 Airfoil (x,y) Coordinates

1 0.00189
0.95 0.0121
0.9 0.02172
0.8 0.03935
0.7 0.05496
0.6 0.06845
0.5 0.07941
0.4 0.08705
0.3 0.09003
0.25 0.08912
0.2 0.08606
0.15 0.08018
0.1 0.07024
0.075 0.063
0.05 0.05332
0.025 0.03922
0.0125 0.02841
0 0
0.0125 -0.02841
0.025 -0.03922
0.05 -0.05332
0.075 -0.063
0.1 -0.07024
0.15 -0.08018
0.2 -0.08606
0.25 -0.08912
0.3 -0.09003
0.4 -0.08705
0.5 -0.07941
0.6 -0.06845
0.7 -0.05496
0.8 -0.03935
0.9 -0.02172
0.95 -0.0121
1 -0.00189

naca0018 Airfoil CAD files

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