n0011sc Airfoil

 NASA/Langley 11% symmetrical supercritical airfoil

n0011sc Airfoil (x,y) Co-ordinates

0 0
0.002 0.009225
0.0065243 0.015751
0.0125 0.020323
0.025 0.026208
0.0375 0.030242
0.05 0.033373
0.075 0.038117
0.1 0.041643
0.125 0.0444
0.15 0.046615
0.175 0.048421
0.2 0.049905
0.25 0.052125
0.3 0.053588
0.35 0.054467
0.4 0.054783
0.45 0.054571
0.5 0.053758
0.55 0.052376
0.6 0.05041
0.625 0.049198
0.65 0.047824
0.675 0.046281
0.7 0.044556
0.725 0.042635
0.75 0.040499
0.775 0.038127
0.8 0.035492
0.825 0.032564
0.85 0.029306
0.875 0.025676
0.9 0.021625
0.925 0.017099
0.95 0.012034
0.975 0.006361
1 0
0.975 -0.006361
0.95 -0.012034
0.925 -0.017099
0.9 -0.021625
0.875 -0.025676
0.85 -0.029306
0.825 -0.032564
0.8 -0.035492
0.775 -0.038127
0.75 -0.040499
0.725 -0.042635
0.7 -0.044556
0.675 -0.046281
0.65 -0.047824
0.625 -0.049198
0.6 -0.05041
0.55 -0.052376
0.5 -0.053758
0.45 -0.054571
0.4 -0.054783
0.35 -0.054467
0.3 -0.053588
0.25 -0.052125
0.2 -0.049905
0.175 -0.048421
0.15 -0.046615
0.125 -0.0444
0.1 -0.041643
0.075 -0.038117
0.05 -0.033373
0.0375 -0.030242
0.025 -0.026208
0.0125 -0.020323
0.0065243 -0.015751
0.002 -0.009225
0 0

n0011sc Airfoil CAD files

DOWNLOAD FROM HERE

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