naca000834 Airfoil

naca000834 Airfoil

naca000834 Airfoil (x,y) Coordinates

1 0.0008
0.95 0.00684
0.9 0.01244
0.8 0.02213
0.7 0.02987
0.6 0.03547
0.5 0.03884
0.4 0.04
0.3 0.03867
0.2 0.03396
0.15 0.02996
0.1 0.02436
0.075 0.02089
0.05 0.01662
0.025 0.0112
0.0125 0.00756
0 0
0.0125 -0.00756
0.025 -0.0112
0.05 -0.01662
0.075 -0.02089
0.1 -0.02436
0.15 -0.02996
0.2 -0.03396
0.3 -0.03867
0.4 -0.04
0.5 -0.03884
0.6 -0.03547
0.7 -0.02987
0.8 -0.02213
0.9 -0.01244
0.95 -0.00684
1 -0.0008

naca000834 Airfoil CAD files

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