naca0006 Airfoil

NACA 0006 airfoil

naca0006 Airfoil (x,y) Coordinates

1 0.00063
0.95 0.00403
0.9 0.00724
0.8 0.01312
0.7 0.01832
0.6 0.02282
0.5 0.02647
0.4 0.02902
0.3 0.03001
0.25 0.02971
0.2 0.02869
0.15 0.02673
0.1 0.02341
0.075 0.021
0.05 0.01777
0.025 0.01307
0.0125 0.00947
0 0
0.0125 -0.00947
0.025 -0.01307
0.05 -0.01777
0.075 -0.021
0.1 -0.02341
0.15 -0.02673
0.2 -0.02869
0.25 -0.02971
0.3 -0.03001
0.4 -0.02902
0.5 -0.02647
0.6 -0.02282
0.7 -0.01832
0.8 -0.01312
0.9 -0.00724
0.95 -0.00403
1 -0.00063

naca0006 Airfoil CAD files

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