n5h20 Airfoil

NACA 5-H-20 rotorcraft airfoil

n5h20 Airfoil (x,y) Co-ordinates

0 0
0.0125 0.031
0.025 0.043
0.05 0.061
0.075 0.076
0.1 0.087
0.15 0.107
0.2 0.121
0.25 0.131
0.3 0.137
0.4 0.144
0.5 0.135
0.6 0.111
0.7 0.079
0.8 0.041
0.9 0.013
0.95 0.0053
1 0
0.95 -0.0093
0.9 -0.021
0.8 -0.048
0.7 -0.059
0.6 -0.059
0.5 -0.057
0.4 -0.055
0.3 -0.0507
0.25 -0.048
0.2 -0.045
0.15 -0.041
0.1 -0.036
0.075 -0.0325
0.05 -0.029
0.025 -0.024
0.0125 -0.019
0 0

n5h20 Airfoil CAD files

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