Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe683-il-50000-n5 Airfoil,goe683-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,21.0687 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe683-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.000,-0.3578,0.11318,0.10501,-0.0535,1.0000,0.1121 -12.750,-0.3800,0.10582,0.09769,-0.0565,1.0000,0.1129 -12.500,-0.3962,0.09976,0.09170,-0.0587,1.0000,0.1144 -12.250,-0.3914,0.09776,0.08975,-0.0583,1.0000,0.1161 -12.000,-0.4093,0.09173,0.08378,-0.0603,1.0000,0.1176 -11.750,-0.5867,0.06578,0.05754,-0.0725,1.0000,0.1163 -11.500,-0.6385,0.06107,0.05272,-0.0696,1.0000,0.1164 -11.250,-0.6774,0.05849,0.05008,-0.0646,1.0000,0.1166 -11.000,-0.7173,0.05697,0.04851,-0.0578,1.0000,0.1167 -10.750,-0.7496,0.05578,0.04725,-0.0515,0.9982,0.1171 -10.500,-0.7394,0.05326,0.04452,-0.0524,0.9832,0.1194 -10.250,-0.7349,0.05073,0.04167,-0.0519,0.9681,0.1217 -10.000,-0.7329,0.04821,0.03871,-0.0506,0.9532,0.1245 -9.750,-0.7078,0.04682,0.03730,-0.0516,0.9418,0.1275 -9.500,-0.6785,0.04528,0.03565,-0.0533,0.9327,0.1313 -9.250,-0.6622,0.04355,0.03362,-0.0528,0.9201,0.1352 -9.000,-0.6354,0.04191,0.03179,-0.0538,0.9109,0.1396 -8.750,-0.6056,0.04076,0.03060,-0.0550,0.9010,0.1445 -8.500,-0.5791,0.03921,0.02872,-0.0557,0.8915,0.1507 -8.250,-0.5484,0.03818,0.02772,-0.0568,0.8817,0.1565 -8.000,-0.5222,0.03710,0.02646,-0.0571,0.8717,0.1642 -7.750,-0.4931,0.03611,0.02545,-0.0577,0.8617,0.1720 -7.500,-0.4698,0.03523,0.02438,-0.0573,0.8511,0.1819 -7.250,-0.4424,0.03447,0.02367,-0.0574,0.8412,0.1922 -7.000,-0.4227,0.03384,0.02295,-0.0562,0.8301,0.2035 -6.750,-0.3983,0.03317,0.02211,-0.0557,0.8206,0.2175 -6.500,-0.3818,0.03284,0.02186,-0.0538,0.8092,0.2284 -6.250,-0.3563,0.03228,0.02122,-0.0533,0.8002,0.2422 -6.000,-0.3419,0.03203,0.02083,-0.0510,0.7889,0.2546 -5.750,-0.3149,0.03156,0.02035,-0.0508,0.7805,0.2685 -5.500,-0.2969,0.03133,0.02009,-0.0492,0.7699,0.2804 -5.250,-0.2723,0.03094,0.01962,-0.0485,0.7613,0.2963 -5.000,-0.2564,0.03079,0.01944,-0.0464,0.7513,0.3120 -4.750,-0.2323,0.03046,0.01914,-0.0457,0.7427,0.3295 -4.500,-0.2082,0.03017,0.01887,-0.0450,0.7340,0.3471 -4.250,-0.1847,0.02989,0.01864,-0.0443,0.7246,0.3649 -4.000,-0.1506,0.02938,0.01813,-0.0452,0.7180,0.3855 -3.750,-0.1317,0.02931,0.01813,-0.0438,0.7074,0.4025 -3.500,-0.0973,0.02881,0.01765,-0.0447,0.7007,0.4258 -3.250,-0.0788,0.02874,0.01768,-0.0432,0.6909,0.4492 -3.000,-0.0506,0.02839,0.01743,-0.0430,0.6834,0.4804 -2.750,-0.0237,0.02811,0.01728,-0.0427,0.6760,0.5177 -2.500,0.0019,0.02801,0.01742,-0.0421,0.6670,0.5609 -2.250,0.0575,0.02757,0.01720,-0.0463,0.6609,0.6253 -2.000,0.1109,0.02794,0.01778,-0.0504,0.6513,0.6860 -1.750,0.1793,0.02845,0.01830,-0.0562,0.6436,0.7370 -1.500,0.2294,0.02911,0.01887,-0.0590,0.6362,0.7740 -1.250,0.2626,0.02987,0.01957,-0.0592,0.6273,0.8063 -1.000,0.3039,0.03029,0.01980,-0.0606,0.6212,0.8354 -0.750,0.3327,0.03110,0.02055,-0.0606,0.6126,0.8622 -0.500,0.3705,0.03159,0.02091,-0.0621,0.6051,0.8858 -0.250,0.4111,0.03181,0.02092,-0.0639,0.5999,0.9081 0.000,0.4422,0.03261,0.02172,-0.0652,0.5903,0.9277 0.250,0.4899,0.03275,0.02172,-0.0689,0.5837,0.9451 0.500,0.5393,0.03290,0.02174,-0.0732,0.5771,0.9634 0.750,0.5864,0.03311,0.02192,-0.0778,0.5685,0.9813 1.000,0.6436,0.03257,0.02123,-0.0837,0.5627,0.9952 1.250,0.6664,0.03281,0.02143,-0.0840,0.5560,1.0000 1.500,0.6734,0.03332,0.02194,-0.0813,0.5492,1.0000 1.750,0.6897,0.03345,0.02196,-0.0797,0.5443,1.0000 2.000,0.7034,0.03376,0.02219,-0.0777,0.5393,1.0000 2.250,0.7033,0.03475,0.02325,-0.0740,0.5320,1.0000 2.500,0.7171,0.03509,0.02353,-0.0720,0.5269,1.0000 2.750,0.7393,0.03509,0.02341,-0.0710,0.5231,1.0000 3.000,0.7316,0.03653,0.02493,-0.0664,0.5157,1.0000 3.250,0.7382,0.03729,0.02569,-0.0635,0.5101,1.0000 3.500,0.7577,0.03747,0.02579,-0.0621,0.5061,1.0000 3.750,0.7663,0.03820,0.02650,-0.0595,0.5012,1.0000 4.000,0.7474,0.04020,0.02859,-0.0535,0.4937,1.0000 4.250,0.7607,0.04070,0.02906,-0.0514,0.4893,1.0000 4.500,0.7871,0.04064,0.02891,-0.0509,0.4861,1.0000 4.750,0.7352,0.04421,0.03261,-0.0413,0.4773,1.0000 5.000,0.7304,0.04549,0.03388,-0.0371,0.4718,1.0000 5.250,0.7562,0.04550,0.03383,-0.0365,0.4687,1.0000 5.500,0.7911,0.04517,0.03343,-0.0369,0.4663,1.0000 6.000,0.6884,0.05279,0.04114,-0.0206,0.4494,1.0000 7.500,0.6144,0.07147,0.05985,-0.0067,0.4092,1.0000 8.000,0.5906,0.07850,0.06691,-0.0038,0.3959,1.0000 8.250,0.6085,0.07930,0.06771,-0.0029,0.3937,1.0000 8.750,0.5786,0.08732,0.07578,-0.0009,0.3804,1.0000 9.000,0.5939,0.08841,0.07687,0.0000,0.3774,1.0000 9.250,0.6132,0.08914,0.07761,0.0009,0.3752,1.0000 9.500,0.5814,0.09517,0.08369,0.0013,0.3680,1.0000 9.750,0.5840,0.09758,0.08613,0.0020,0.3632,1.0000 10.000,0.5981,0.09884,0.08742,0.0027,0.3599,1.0000 10.250,0.6188,0.09948,0.08808,0.0036,0.3575,1.0000 10.500,0.5928,0.10494,0.09359,0.0036,0.3503,1.0000 10.750,0.5998,0.10681,0.09549,0.0043,0.3449,1.0000