naca001034 Airfoil

NACA 0010-34 airfoil

naca001034 Airfoil (x,y) Coordinates

1 0.001
0.95 0.00856
0.9 0.01556
0.8 0.02767
0.7 0.03733
0.6 0.04433
0.5 0.04856
0.4 0.05
0.3 0.04833
0.2 0.04244
0.15 0.03744
0.1 0.03044
0.075 0.02611
0.05 0.02078
0.025 0.014
0.0125 0.00944
0 0
0.0125 -0.00944
0.025 -0.014
0.05 -0.02078
0.075 -0.02611
0.1 -0.03044
0.15 -0.03744
0.2 -0.04244
0.3 -0.04833
0.4 -0.05
0.5 -0.04856
0.6 -0.04433
0.7 -0.03733
0.8 -0.02767
0.9 -0.01556
0.95 -0.00856
1 -0.001

naca001034 Airfoil CAD files

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