WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT NASA)
0.99964  0.00021
0.99033  0.00285
0.97613  0.00629
0.94994  0.01257
0.90009  0.02433
0.84997  0.03585
0.80012  0.04737
0.74442  0.06026
0.70137  0.07028
0.65056  0.08197
0.60095  0.09328
0.55178  0.10427
0.50043  0.11506
0.45244  0.12335
0.40185  0.12902
0.35283  0.13066
0.30311  0.12819
0.25320  0.12165
0.20035  0.11042
0.15106  0.09548
0.10199  0.07608
0.07574  0.06328
0.06090  0.05510
0.05013  0.04861
0.03467  0.03841
0.02475  0.03106
0.01781  0.02521
0.01353  0.02120
0.00585  0.01259
0.00499  0.01134
0.00388  0.00966
0.00277  0.00786
0.00166  0.00563
0.00083  0.00347
0.00000  0.00000
0.00083 -0.00516
0.00166 -0.00691
0.00277 -0.00856
0.00388 -0.00992
0.00527 -0.01136
0.00641 -0.01231
0.01352 -0.01676
0.03588 -0.02573
0.05113 -0.03040
0.07643 -0.03651
0.10169 -0.04131
0.15067 -0.04833
0.20055 -0.05321
0.25032 -0.05617
0.30166 -0.05779
0.35047 -0.05782
0.40069 -0.05597
0.45007 -0.05253
0.49998 -0.04772
0.55056 -0.04134
0.59970 -0.03396
0.64952 -0.02630
0.70012 -0.01892
0.74995 -0.01234
0.79808 -0.00732
0.84898 -0.00364
0.89907 -0.00133
0.94758 -0.00080
0.97026 -0.00095
0.97832 -0.00104
1.00000 -0.00059