Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe458-il-200000-n5 Airfoil,goe458-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,86.9425 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe458-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.2910,0.11101,0.10764,-0.0356,1.0000,0.0149 -8.750,-0.2944,0.10906,0.10576,-0.0348,1.0000,0.0149 -8.500,-0.2987,0.10729,0.10404,-0.0334,1.0000,0.0149 -8.250,-0.2811,0.10296,0.09972,-0.0386,0.9958,0.0150 -8.000,-0.2649,0.09888,0.09564,-0.0431,0.9908,0.0150 -7.750,-0.2484,0.09482,0.09158,-0.0477,0.9860,0.0150 -7.500,-0.2336,0.09091,0.08768,-0.0517,0.9796,0.0150 -7.250,-0.2190,0.08712,0.08390,-0.0558,0.9726,0.0151 -7.000,-0.1998,0.08289,0.07967,-0.0612,0.9670,0.0151 -6.750,-0.1822,0.07879,0.07557,-0.0660,0.9593,0.0151 -6.500,-0.1578,0.07413,0.07090,-0.0726,0.9548,0.0151 -6.250,-0.1378,0.06998,0.06673,-0.0778,0.9468,0.0150 -6.000,-0.1117,0.06539,0.06210,-0.0843,0.9419,0.0150 -5.750,-0.0933,0.06130,0.05796,-0.0880,0.9340,0.0146 -5.500,-0.0687,0.05694,0.05356,-0.0934,0.9286,0.0129 -5.250,-0.0431,0.05247,0.04901,-0.0992,0.9200,0.0119 -5.000,-0.0092,0.04721,0.04363,-0.1067,0.9142,0.0112 -4.750,0.0198,0.04241,0.03869,-0.1121,0.9055,0.0105 -4.500,0.0545,0.03676,0.03281,-0.1181,0.8991,0.0100 -4.250,0.0871,0.03056,0.02627,-0.1225,0.8913,0.0097 -4.000,0.1190,0.02509,0.02022,-0.1254,0.8850,0.0094 -3.750,0.1477,0.02159,0.01611,-0.1263,0.8777,0.0097 -3.500,0.1768,0.01906,0.01299,-0.1267,0.8712,0.0108 -3.250,0.2060,0.01829,0.01172,-0.1266,0.8640,0.0148 -3.000,0.2328,0.01640,0.00951,-0.1267,0.8568,0.0180 -2.750,0.2615,0.01507,0.00784,-0.1264,0.8497,0.0180 -2.500,0.2885,0.01406,0.00657,-0.1260,0.8417,0.0183 -2.250,0.3168,0.01322,0.00558,-0.1258,0.8348,0.0195 -2.000,0.3432,0.01266,0.00488,-0.1254,0.8257,0.0215 -1.750,0.3705,0.01212,0.00419,-0.1252,0.8174,0.0257 -1.500,0.3981,0.01184,0.00377,-0.1250,0.8089,0.0304 -1.250,0.4249,0.01164,0.00343,-0.1246,0.7995,0.0308 -1.000,0.4522,0.01148,0.00315,-0.1244,0.7905,0.0315 -0.750,0.4795,0.01134,0.00282,-0.1241,0.7811,0.0343 -0.500,0.5055,0.01100,0.00270,-0.1238,0.7707,0.1170 -0.250,0.5323,0.01097,0.00260,-0.1235,0.7607,0.1298 0.000,0.5592,0.01095,0.00252,-0.1232,0.7509,0.1462 0.250,0.5855,0.01083,0.00251,-0.1230,0.7404,0.1928 0.500,0.6117,0.01080,0.00251,-0.1227,0.7295,0.2195 0.750,0.6380,0.01076,0.00253,-0.1224,0.7193,0.2581 1.000,0.6641,0.01068,0.00256,-0.1221,0.7091,0.3170 1.250,0.6886,0.01030,0.00264,-0.1216,0.6976,0.4991 1.500,0.7238,0.00949,0.00265,-0.1230,0.6838,1.0000 1.750,0.7492,0.00963,0.00270,-0.1224,0.6696,1.0000 2.000,0.7746,0.00979,0.00280,-0.1219,0.6563,1.0000 2.250,0.7999,0.00995,0.00289,-0.1214,0.6438,1.0000 2.500,0.8252,0.01012,0.00299,-0.1209,0.6312,1.0000 2.750,0.8501,0.01030,0.00312,-0.1203,0.6177,1.0000 3.000,0.8748,0.01049,0.00326,-0.1197,0.6037,1.0000 3.250,0.8999,0.01068,0.00344,-0.1192,0.5921,1.0000 3.500,0.9253,0.01086,0.00374,-0.1187,0.5831,1.0000 3.750,0.9504,0.01106,0.00395,-0.1182,0.5735,1.0000 4.000,0.9754,0.01124,0.00420,-0.1177,0.5625,1.0000 4.250,0.9981,0.01148,0.00444,-0.1167,0.5395,1.0000 4.500,1.0131,0.01199,0.00462,-0.1141,0.4655,1.0000 4.750,1.0136,0.01368,0.00527,-0.1094,0.2882,1.0000 5.000,1.0098,0.01626,0.00660,-0.1048,0.0928,1.0000 5.250,1.0184,0.01793,0.00790,-0.1016,0.0107,1.0000 5.500,1.0372,0.01865,0.00870,-0.1001,0.0062,1.0000 5.750,1.0559,0.01938,0.00961,-0.0985,0.0056,1.0000 6.000,1.0733,0.02022,0.01063,-0.0966,0.0052,1.0000 6.250,1.0885,0.02118,0.01178,-0.0945,0.0050,1.0000 6.500,1.1007,0.02229,0.01304,-0.0919,0.0049,1.0000 6.750,1.1091,0.02351,0.01437,-0.0888,0.0048,1.0000 7.000,1.1156,0.02486,0.01602,-0.0854,0.0048,1.0000 7.250,1.1236,0.02628,0.01752,-0.0823,0.0048,1.0000 7.500,1.1336,0.02783,0.01915,-0.0796,0.0048,1.0000 7.750,1.1474,0.02946,0.02086,-0.0776,0.0049,1.0000 8.000,1.1668,0.03135,0.02283,-0.0762,0.0049,1.0000 8.250,1.1923,0.03348,0.02509,-0.0757,0.0051,1.0000 8.500,1.2212,0.03594,0.02774,-0.0758,0.0053,1.0000 8.750,1.2477,0.03861,0.03065,-0.0757,0.0055,1.0000 9.000,1.2685,0.04139,0.03368,-0.0747,0.0057,1.0000 9.250,1.2841,0.04430,0.03685,-0.0732,0.0060,1.0000 9.500,1.2960,0.04750,0.04030,-0.0714,0.0062,1.0000 16.250,1.0625,0.19873,0.19557,-0.1077,0.0161,1.0000 16.500,1.0659,0.20504,0.20187,-0.1111,0.0160,1.0000