n11h9 Airfoil

NACA 11-H-9 rotorcraft airfoil

n11h9 Airfoil (x,y) Co-ordinates

0 0
0.0034 0.0127
0.0078 0.0174
0.02 0.0266
0.0447 0.04
0.0699 0.0502
0.0952 0.0585
0.1461 0.0711
0.1973 0.0799
0.2484 0.0857
0.2996 0.0889
0.4022 0.0883
0.5039 0.0772
0.6039 0.0597
0.7029 0.0391
0.8015 0.0184
0.9001999 0.0017
0.9499 0.0027
1 0
0.9501 -0.0071
0.8998001 -0.0105
0.7985 -0.0127
0.697 -0.0117
0.5961 -0.0089
0.4961 -0.0051
0.3978 -0.0014
0.3004 0.0014
0.2516 0.0023
0.2027 0.0028
0.1538 0.0025
0.1048 0.0013
0.0801 -0.0004
0.0552 -0.0009
0.03 -0.0024
0.0171 -0.0031
0.0116 -0.0031
0 0

n11h9 Airfoil CAD files

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