n6h20 Airfoil

NACA 6-H-20 rotorcraft airfoil

n6h20 Airfoil (x,y) Coordinates

0 0
0.0125 0.033
0.025 0.047
0.05 0.067
0.075 0.083
0.1 0.096
0.15 0.1196
0.2 0.135
0.25 0.147
0.3 0.155
0.4 0.161
0.5 0.151
0.6 0.121
0.7 0.08
0.8 0.041
0.9 0.012
0.95 0.0053
1 0
0.95 -0.011
0.9 -0.023
0.8 -0.051
0.7 -0.057
0.6 -0.051
0.5 -0.043
0.4 -0.0385
0.3 -0.0356
0.25 -0.0334
0.2 -0.032
0.15 -0.0305
0.1 -0.0275
0.075 -0.0254
0.05 -0.023
0.025 -0.019
0.0125 -0.015
0 0

n6h20 Airfoil CAD files

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