n5h10 Airfoil

NACA 5-H-10 rotorcraft airfoil

n5h10 Airfoil (x,y) Co-ordinates

0 0
0.0125 0.015
0.025 0.021
0.05 0.031
0.075 0.038
0.1 0.0437
0.15 0.053
0.2 0.061
0.25 0.066
0.3 0.069
0.4 0.072
0.5 0.067
0.6 0.055
0.7 0.039
0.8 0.02
0.9 0.0067
0.96 0.0027
1 0
0.96 -0.0047
0.9 -0.011
0.8 -0.024
0.7 -0.029
0.6 -0.029
0.5 -0.028
0.4 -0.027
0.3 -0.025
0.25 -0.024
0.2 -0.023
0.15 -0.021
0.1 -0.0185
0.075 -0.0168
0.05 -0.015
0.025 -0.012
0.0125 -0.0093
0 0

n5h10 Airfoil CAD files

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