Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe416a-il-500000 Airfoil,goe416a-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,71.0034 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-goe416a-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.500,-0.4675,0.13663,0.13446,-0.0010,1.0000,0.0131 -13.250,-0.4766,0.13206,0.12990,-0.0017,1.0000,0.0136 -9.250,-0.7442,0.05164,0.04832,-0.0387,1.0000,0.0137 -9.000,-0.7354,0.04815,0.04478,-0.0390,1.0000,0.0140 -8.750,-0.7263,0.04514,0.04167,-0.0393,1.0000,0.0143 -8.500,-0.7156,0.04234,0.03872,-0.0394,1.0000,0.0147 -8.250,-0.7026,0.03969,0.03589,-0.0392,1.0000,0.0153 -8.000,-0.6876,0.03717,0.03315,-0.0389,1.0000,0.0161 -7.750,-0.6700,0.03509,0.03081,-0.0382,1.0000,0.0172 -7.500,-0.6460,0.03611,0.03153,-0.0371,1.0000,0.0187 -7.250,-0.6373,0.03060,0.02552,-0.0361,1.0000,0.0196 -7.000,-0.6194,0.02764,0.02257,-0.0357,1.0000,0.0208 -6.750,-0.6004,0.02597,0.02084,-0.0348,1.0000,0.0219 -6.500,-0.5814,0.02458,0.01932,-0.0335,1.0000,0.0233 -6.250,-0.5622,0.02371,0.01828,-0.0320,1.0000,0.0251 -6.000,-0.5425,0.02554,0.01991,-0.0300,1.0000,0.0269 -5.250,-0.4477,0.01665,0.01054,-0.0316,0.9950,0.0196 -5.000,-0.4127,0.01534,0.00925,-0.0330,0.9919,0.0183 -4.750,-0.3769,0.01434,0.00821,-0.0347,0.9882,0.0186 -4.500,-0.3410,0.01303,0.00687,-0.0367,0.9850,0.0195 -4.250,-0.3056,0.01203,0.00582,-0.0386,0.9803,0.0196 -4.000,-0.2718,0.01107,0.00476,-0.0401,0.9736,0.0204 -3.750,-0.2378,0.01044,0.00406,-0.0415,0.9672,0.0218 -3.500,-0.2068,0.01002,0.00357,-0.0422,0.9580,0.0240 -3.250,-0.1775,0.00973,0.00320,-0.0424,0.9473,0.0266 -3.000,-0.1495,0.00946,0.00283,-0.0421,0.9352,0.0323 -2.750,-0.1272,0.00727,0.00209,-0.0424,0.9220,0.4184 -2.500,-0.1008,0.00737,0.00227,-0.0418,0.9078,0.4803 -2.250,-0.0741,0.00745,0.00230,-0.0412,0.8925,0.4955 -2.000,-0.0471,0.00757,0.00230,-0.0407,0.8758,0.5065 -1.750,-0.0203,0.00768,0.00238,-0.0402,0.8579,0.5196 -1.500,0.0067,0.00773,0.00239,-0.0398,0.8395,0.5278 -1.250,0.0344,0.00784,0.00239,-0.0395,0.8192,0.5360 -1.000,0.0618,0.00782,0.00231,-0.0393,0.7969,0.5396 -0.750,0.0895,0.00786,0.00227,-0.0391,0.7733,0.5435 -0.500,0.1174,0.00793,0.00222,-0.0390,0.7506,0.5472 -0.250,0.1456,0.00800,0.00217,-0.0390,0.7280,0.5500 0.000,0.1735,0.00801,0.00210,-0.0389,0.7055,0.5522 0.250,0.2014,0.00807,0.00208,-0.0389,0.6832,0.5546 0.500,0.2295,0.00814,0.00208,-0.0389,0.6641,0.5571 0.750,0.2578,0.00820,0.00208,-0.0390,0.6459,0.5596 1.000,0.2861,0.00828,0.00209,-0.0391,0.6284,0.5622 1.250,0.3145,0.00837,0.00211,-0.0392,0.6111,0.5648 1.500,0.3425,0.00841,0.00213,-0.0392,0.5934,0.5674 1.750,0.3708,0.00846,0.00217,-0.0393,0.5760,0.5699 2.000,0.3991,0.00853,0.00222,-0.0394,0.5566,0.5727 2.250,0.4272,0.00863,0.00226,-0.0395,0.5353,0.5757 2.500,0.4555,0.00874,0.00231,-0.0396,0.5133,0.5788 2.750,0.4832,0.00883,0.00237,-0.0396,0.4920,0.5820 3.000,0.5111,0.00894,0.00248,-0.0397,0.4722,0.5851 3.250,0.5390,0.00908,0.00259,-0.0397,0.4548,0.5886 3.500,0.5670,0.00922,0.00271,-0.0398,0.4402,0.5923 3.750,0.5947,0.00934,0.00284,-0.0399,0.4247,0.5960 4.000,0.6220,0.00952,0.00300,-0.0399,0.4006,0.6003 4.250,0.6494,0.00972,0.00315,-0.0399,0.3744,0.6052 4.500,0.6769,0.00989,0.00330,-0.0399,0.3451,0.6100 4.750,0.7037,0.01014,0.00348,-0.0399,0.3060,0.6153 5.000,0.7300,0.01050,0.00372,-0.0398,0.2691,0.6214 5.250,0.7562,0.01084,0.00402,-0.0397,0.2455,0.6279 5.500,0.7825,0.01118,0.00433,-0.0396,0.2248,0.6361 5.750,0.8087,0.01149,0.00465,-0.0395,0.2039,0.6459 6.000,0.8350,0.01176,0.00494,-0.0395,0.1792,0.6588 6.250,0.8598,0.01225,0.00529,-0.0393,0.1277,0.6771 6.500,0.8833,0.01284,0.00583,-0.0389,0.0937,0.7078 6.750,0.9046,0.01312,0.00638,-0.0378,0.0674,0.8118 7.000,0.9267,0.01347,0.00689,-0.0368,0.0498,1.0000 7.250,0.9509,0.01416,0.00754,-0.0364,0.0368,1.0000 7.500,0.9742,0.01496,0.00833,-0.0358,0.0268,1.0000 7.750,0.9977,0.01569,0.00907,-0.0353,0.0218,1.0000 8.000,1.0201,0.01655,0.01001,-0.0346,0.0190,1.0000 8.250,1.0436,0.01718,0.01070,-0.0341,0.0170,1.0000 8.500,1.0639,0.01822,0.01179,-0.0332,0.0153,1.0000 8.750,1.0809,0.01964,0.01334,-0.0318,0.0143,1.0000 9.000,1.1014,0.02055,0.01436,-0.0309,0.0136,1.0000 9.250,1.1203,0.02162,0.01553,-0.0298,0.0129,1.0000 9.500,1.1385,0.02272,0.01672,-0.0287,0.0123,1.0000 9.750,1.1565,0.02375,0.01783,-0.0276,0.0116,1.0000 10.000,1.1714,0.02510,0.01924,-0.0263,0.0109,1.0000 10.250,1.1753,0.02811,0.02247,-0.0237,0.0103,1.0000 10.500,1.1893,0.02949,0.02401,-0.0222,0.0100,1.0000 10.750,1.2013,0.03099,0.02568,-0.0206,0.0098,1.0000 11.000,1.2087,0.03266,0.02752,-0.0184,0.0096,1.0000 11.250,1.2127,0.03456,0.02961,-0.0160,0.0094,1.0000 11.500,1.2142,0.03672,0.03196,-0.0139,0.0092,1.0000 11.750,1.2133,0.03917,0.03461,-0.0120,0.0091,1.0000 12.000,1.2100,0.04195,0.03760,-0.0106,0.0090,1.0000 12.250,1.2045,0.04512,0.04098,-0.0098,0.0088,1.0000 12.500,1.1959,0.04890,0.04497,-0.0097,0.0088,1.0000 12.750,1.1851,0.05322,0.04951,-0.0104,0.0087,1.0000 13.000,1.1717,0.05826,0.05477,-0.0120,0.0087,1.0000 13.250,1.1560,0.06402,0.06075,-0.0145,0.0087,1.0000 13.500,1.1381,0.07051,0.06744,-0.0179,0.0088,1.0000 13.750,1.1176,0.07789,0.07502,-0.0220,0.0088,1.0000 14.000,1.0957,0.08596,0.08327,-0.0268,0.0089,1.0000 14.250,1.0723,0.09485,0.09233,-0.0322,0.0090,1.0000 14.500,1.0479,0.10451,0.10214,-0.0381,0.0091,1.0000 14.750,1.0221,0.11533,0.11311,-0.0447,0.0093,1.0000 15.000,0.9935,0.12761,0.12551,-0.0519,0.0095,1.0000 15.250,0.9572,0.14282,0.14083,-0.0604,0.0098,1.0000