Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe802a-il-500000-n5 Airfoil,goe802a-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,91.0352 Max Cl/Cd alpha,6.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-goe802a-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.2082,0.10191,0.09955,-0.0473,0.9392,0.0161 -9.500,-0.2025,0.09903,0.09663,-0.0482,0.9258,0.0161 -9.250,-0.1964,0.09623,0.09380,-0.0491,0.9138,0.0160 -9.000,-0.1893,0.09346,0.09102,-0.0502,0.9047,0.0158 -8.750,-0.1824,0.09050,0.08802,-0.0517,0.8953,0.0159 -8.250,-0.1671,0.08476,0.08224,-0.0553,0.8781,0.0167 -8.000,-0.1566,0.08276,0.08020,-0.0567,0.8707,0.0174 -7.750,-0.1410,0.07961,0.07703,-0.0613,0.8627,0.0195 -7.500,-0.1251,0.07603,0.07341,-0.0659,0.8552,0.0196 -7.250,-0.1068,0.07233,0.06965,-0.0710,0.8484,0.0196 -7.000,-0.0860,0.06852,0.06578,-0.0764,0.8410,0.0197 -6.750,-0.0622,0.06448,0.06165,-0.0824,0.8342,0.0198 -6.500,-0.0465,0.06150,0.05865,-0.0838,0.8280,0.0200 -6.250,-0.0281,0.05931,0.05643,-0.0854,0.8212,0.0204 -6.000,-0.0063,0.05697,0.05402,-0.0880,0.8145,0.0211 -5.750,0.0187,0.05419,0.05118,-0.0914,0.8075,0.0224 -5.500,0.0530,0.05046,0.04729,-0.0970,0.8002,0.0236 -5.250,0.0832,0.04716,0.04382,-0.1009,0.7935,0.0237 -5.000,0.1130,0.04402,0.04052,-0.1040,0.7858,0.0238 -4.750,0.1407,0.04084,0.03715,-0.1064,0.7777,0.0239 -4.500,0.1617,0.03843,0.03471,-0.1074,0.7687,0.0242 -4.250,0.1856,0.03653,0.03269,-0.1085,0.7569,0.0245 -4.000,0.2114,0.03473,0.03078,-0.1096,0.7442,0.0249 -3.750,0.2381,0.03298,0.02888,-0.1107,0.7322,0.0257 -3.500,0.2709,0.03137,0.02699,-0.1117,0.7209,0.0282 -3.250,0.3000,0.02966,0.02503,-0.1125,0.7099,0.0284 -3.000,0.3280,0.02813,0.02326,-0.1131,0.6976,0.0285 -2.750,0.3553,0.02658,0.02151,-0.1136,0.6840,0.0285 -2.250,0.4095,0.02354,0.01807,-0.1144,0.6584,0.0285 -2.000,0.4347,0.02179,0.01625,-0.1152,0.6445,0.0275 -1.750,0.4624,0.02060,0.01484,-0.1155,0.6302,0.0271 -1.500,0.4900,0.01956,0.01358,-0.1157,0.6158,0.0271 -1.250,0.5175,0.01864,0.01243,-0.1158,0.6017,0.0270 -1.000,0.5453,0.01779,0.01138,-0.1159,0.5888,0.0275 -0.750,0.5729,0.01697,0.01035,-0.1160,0.5772,0.0278 -0.500,0.6001,0.01623,0.00943,-0.1161,0.5655,0.0274 -0.250,0.6277,0.01547,0.00851,-0.1162,0.5546,0.0273 0.000,0.6548,0.01474,0.00756,-0.1162,0.5434,0.0274 0.250,0.6821,0.01368,0.00628,-0.1162,0.5325,0.0279 0.500,0.7080,0.01259,0.00495,-0.1162,0.5226,0.0285 0.750,0.7344,0.01208,0.00435,-0.1163,0.5129,0.0291 1.000,0.7612,0.01205,0.00428,-0.1163,0.5038,0.0301 1.250,0.7880,0.01187,0.00408,-0.1164,0.4947,0.0310 1.500,0.8141,0.01170,0.00385,-0.1163,0.4857,0.0315 1.750,0.8410,0.01158,0.00373,-0.1163,0.4769,0.0321 2.250,0.8940,0.01157,0.00366,-0.1162,0.4574,0.0337 2.500,0.9203,0.01168,0.00373,-0.1161,0.4469,0.0349 2.750,0.9469,0.01177,0.00383,-0.1160,0.4351,0.0367 3.000,0.9728,0.01190,0.00393,-0.1159,0.4214,0.0393 3.250,0.9986,0.01218,0.00419,-0.1156,0.4066,0.0450 3.500,1.0243,0.01240,0.00439,-0.1154,0.3935,0.0560 3.750,1.0500,0.01259,0.00452,-0.1152,0.3833,0.0646 4.250,1.1011,0.01300,0.00487,-0.1148,0.3625,0.0732 4.500,1.1263,0.01322,0.00506,-0.1145,0.3537,0.0783 5.000,1.1765,0.01356,0.00537,-0.1140,0.3352,0.0862 5.250,1.2011,0.01371,0.00552,-0.1137,0.3237,0.0863 5.500,1.2249,0.01393,0.00569,-0.1133,0.3124,0.0864 5.750,1.2495,0.01409,0.00587,-0.1130,0.3029,0.0865 6.000,1.2732,0.01432,0.00608,-0.1126,0.2946,0.0865 6.500,1.3214,0.01462,0.00644,-0.1119,0.2781,0.0867 6.750,1.3455,0.01478,0.00664,-0.1115,0.2696,0.0869 7.000,1.3681,0.01505,0.00690,-0.1109,0.2589,0.0872 7.250,1.3909,0.01530,0.00717,-0.1104,0.2467,0.0874 7.500,1.4111,0.01575,0.00753,-0.1094,0.2261,0.0877 7.750,1.4281,0.01642,0.00804,-0.1080,0.1956,0.0878 8.000,1.4437,0.01716,0.00863,-0.1064,0.1708,0.0879 8.500,1.4795,0.01818,0.00961,-0.1038,0.1469,0.0882 8.750,1.4955,0.01872,0.01013,-0.1022,0.1368,0.0883 9.000,1.5100,0.01917,0.01060,-0.1002,0.1293,0.0886 9.250,1.5238,0.01977,0.01119,-0.0983,0.1209,0.0888 9.500,1.5392,0.02035,0.01180,-0.0967,0.1124,0.0891 9.750,1.5524,0.02110,0.01252,-0.0948,0.1023,0.0892 10.000,1.5628,0.02204,0.01339,-0.0927,0.0874,0.0893 10.250,1.5710,0.02315,0.01442,-0.0905,0.0721,0.0894 10.500,1.5807,0.02419,0.01543,-0.0885,0.0633,0.0896 10.750,1.5914,0.02519,0.01645,-0.0867,0.0583,0.0902 11.000,1.6010,0.02629,0.01757,-0.0849,0.0532,0.0906 11.250,1.6119,0.02733,0.01866,-0.0834,0.0488,0.0907 11.750,1.6182,0.03073,0.02199,-0.0792,0.0234,0.0910 12.000,1.6155,0.03304,0.02428,-0.0769,0.0170,0.0913 12.250,1.6204,0.03479,0.02612,-0.0753,0.0151,0.0916 12.500,1.6260,0.03652,0.02794,-0.0740,0.0142,0.0921 12.750,1.6302,0.03843,0.02996,-0.0727,0.0134,0.0924 13.000,1.6330,0.04055,0.03217,-0.0715,0.0128,0.0926 13.250,1.6346,0.04286,0.03458,-0.0703,0.0121,0.0931 13.500,1.6360,0.04524,0.03707,-0.0694,0.0116,0.0938 13.750,1.6387,0.04757,0.03951,-0.0686,0.0113,0.0946 14.000,1.6405,0.05009,0.04214,-0.0680,0.0109,0.0955 14.250,1.6409,0.05284,0.04500,-0.0674,0.0106,0.0963 14.500,1.6403,0.05580,0.04808,-0.0671,0.0102,0.0967 14.750,1.6388,0.05899,0.05137,-0.0669,0.0099,0.0972 15.000,1.6358,0.06243,0.05492,-0.0668,0.0097,0.0980 15.250,1.6314,0.06613,0.05875,-0.0669,0.0094,0.0989 15.500,1.6256,0.07013,0.06287,-0.0671,0.0092,0.0993 15.750,1.6181,0.07445,0.06731,-0.0676,0.0090,0.1001 16.000,1.6089,0.07907,0.07206,-0.0682,0.0089,0.1012 16.250,1.5971,0.08418,0.07731,-0.0690,0.0087,0.1018 16.500,1.5880,0.08898,0.08222,-0.0699,0.0086,0.1028 16.750,1.5800,0.09367,0.08703,-0.0709,0.0085,0.1042 17.000,1.5713,0.09851,0.09198,-0.0720,0.0084,0.1057 17.250,1.5620,0.10353,0.09713,-0.0733,0.0083,0.1078 17.500,1.5520,0.10873,0.10244,-0.0748,0.0082,0.1103 17.750,1.5419,0.11402,0.10784,-0.0764,0.0081,0.1121