n6h10 Airfoil

NACA 6-H-10 rotorcraft airfoil

n6h10 Airfoil (x,y) Coordinates

0 -0.00114
0.0125 0.01916
0.025 0.02759
0.05 0.0386
0.075 0.0476
0.1 0.056
0.15 0.06938
0.2 0.0794
0.25 0.08769
0.3 0.092
0.4 0.09517
0.5 0.08537
0.6 0.0653
0.7 0.04114
0.8 0.01971
0.9 0.00571
0.95 0.0011
1 0
0.95 -0.0068
0.9 -0.013
0.8 -0.02356
0.7 -0.02283
0.6 -0.0168
0.5 -0.00979
0.4 -0.005
0.3 -0.00309
0.25 -0.00199
0.2 -0.00161
0.15 -0.00198
0.1 -0.00335
0.075 -0.00428
0.05 -0.0046
0.025 -0.00449
0.0125 -0.00392
0 -0.00114

n6h10 Airfoil CAD files

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