naca0008 Airfoil

NACA 0008 airfoil

naca0008 Airfoil (x,y) Coordinates

1 0.00084
0.95 0.00537
0.9 0.00965
0.8 0.01749
0.7 0.02443
0.6 0.03043
0.5 0.03529
0.4 0.03869
0.3 0.04001
0.25 0.03961
0.2 0.03825
0.15 0.03564
0.1 0.03121
0.075 0.028
0.05 0.02369
0.025 0.01743
0.0125 0.01263
0 0
0.0125 -0.01263
0.025 -0.01743
0.05 -0.02369
0.075 -0.028
0.1 -0.03121
0.15 -0.03564
0.2 -0.03825
0.25 -0.03961
0.3 -0.04001
0.4 -0.03869
0.5 -0.03529
0.6 -0.03043
0.7 -0.02443
0.8 -0.01749
0.9 -0.00965
0.95 -0.00537
1 -0.00084

naca0008 Airfoil CAD files

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