NREL's S817 Airfoil
       33.       36.

  0.000097  0.001209
  0.000360  0.002472
  0.004428  0.010189
  0.013037  0.018535
  0.026561  0.027298
  0.044732  0.036303
  0.067447  0.045401
  0.094395  0.054524
  0.125168  0.063482
  0.159422  0.072091
  0.196730  0.080162
  0.236695  0.087518
  0.278854  0.093990
  0.322764  0.099414
  0.367930  0.103634
  0.413876  0.106495
  0.460088  0.107831
  0.506064  0.107442
  0.551323  0.104955
  0.595770  0.099994
  0.639510  0.092179
  0.683540  0.082026
  0.727479  0.070903
  0.770556  0.059582
  0.811952  0.048605
  0.850827  0.038354
  0.886342  0.029037
  0.917813  0.020567
  0.945064  0.013016
  0.967742  0.006897
  0.985115  0.002693
  0.996181  0.000538
  1.000000  0.000000

  0.000097  0.001209
  0.000009 -0.000344
  0.000088 -0.001044
  0.000269 -0.001673
  0.000601 -0.002252
  0.001068 -0.002831
  0.001348 -0.003124
  0.002331 -0.003985
  0.009208 -0.007511
  0.023293 -0.011505
  0.043224 -0.015059
  0.069056 -0.018360
  0.100341 -0.021950
  0.136148 -0.025898
  0.175927 -0.030099
  0.218923 -0.034424
  0.264584 -0.038702
  0.312212 -0.042753
  0.361251 -0.046380
  0.411034 -0.049379
  0.461007 -0.051521
  0.510533 -0.052546
  0.559060 -0.052087
  0.606201 -0.049264
  0.652988 -0.043963
  0.699386 -0.036994
  0.745363 -0.029123
  0.790264 -0.021329
  0.833208 -0.014263
  0.873235 -0.008386
  0.909350 -0.003976
  0.940561 -0.001118
  0.965947  0.000302
  0.984691  0.000585
  0.996152  0.000262
  1.000000  0.000000