Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe499-il-200000-n5 Airfoil,goe499-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,99.068 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-goe499-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.2095,0.09106,0.08749,-0.0669,0.9700,0.0187 -8.000,-0.1948,0.08714,0.08357,-0.0714,0.9667,0.0198 -7.750,-0.1859,0.08321,0.07966,-0.0754,0.9604,0.0209 -7.500,-0.1740,0.07893,0.07537,-0.0802,0.9551,0.0213 -7.250,-0.1587,0.07404,0.07048,-0.0864,0.9495,0.0219 -7.000,-0.1434,0.06882,0.06527,-0.0931,0.9432,0.0228 -6.750,-0.1226,0.06714,0.06355,-0.0952,0.9408,0.0243 -6.500,-0.0975,0.06498,0.06133,-0.0992,0.9388,0.0272 -6.250,-0.0828,0.06117,0.05750,-0.1038,0.9310,0.0282 -6.000,-0.0533,0.05577,0.05203,-0.1134,0.9269,0.0297 -5.750,-0.0183,0.04884,0.04500,-0.1260,0.9215,0.0323 -5.500,0.0336,0.03665,0.03246,-0.1463,0.9160,0.0332 -5.250,0.0828,0.02770,0.02285,-0.1611,0.9135,0.0362 -5.000,0.1224,0.02381,0.01838,-0.1670,0.9118,0.0371 -4.750,0.1539,0.02159,0.01573,-0.1694,0.9085,0.0379 -4.500,0.1831,0.02000,0.01376,-0.1707,0.9049,0.0383 -4.250,0.2137,0.01892,0.01240,-0.1719,0.9020,0.0397 -4.000,0.2460,0.01785,0.01105,-0.1732,0.8994,0.0407 -3.750,0.2798,0.01669,0.00959,-0.1746,0.8970,0.0403 -3.500,0.3055,0.01595,0.00865,-0.1744,0.8912,0.0400 -3.250,0.3356,0.01520,0.00773,-0.1748,0.8869,0.0398 -3.000,0.3674,0.01451,0.00691,-0.1756,0.8838,0.0397 -2.750,0.3942,0.01405,0.00635,-0.1754,0.8786,0.0397 -2.500,0.4228,0.01362,0.00584,-0.1756,0.8740,0.0399 -2.250,0.4535,0.01319,0.00533,-0.1761,0.8705,0.0402 -2.000,0.4809,0.01291,0.00499,-0.1760,0.8653,0.0408 -1.750,0.5092,0.01265,0.00465,-0.1760,0.8602,0.0418 -1.500,0.5397,0.01236,0.00427,-0.1764,0.8561,0.0432 -1.250,0.5659,0.01221,0.00407,-0.1760,0.8496,0.0453 -1.000,0.5948,0.01200,0.00382,-0.1761,0.8448,0.0501 -0.750,0.6244,0.01168,0.00366,-0.1764,0.8411,0.0832 -0.500,0.6505,0.01153,0.00369,-0.1762,0.8353,0.1393 -0.250,0.6788,0.01137,0.00373,-0.1763,0.8308,0.2022 0.000,0.7071,0.01126,0.00374,-0.1764,0.8264,0.2466 0.250,0.7332,0.01123,0.00380,-0.1761,0.8202,0.2760 0.500,0.7617,0.01110,0.00379,-0.1761,0.8152,0.3132 0.750,0.7878,0.01090,0.00395,-0.1759,0.8085,0.4129 1.000,0.8148,0.01073,0.00404,-0.1756,0.8022,0.5211 1.250,0.8410,0.01060,0.00413,-0.1752,0.7956,0.6014 1.500,0.8646,0.00995,0.00406,-0.1739,0.7877,1.0000 1.750,0.8910,0.01001,0.00410,-0.1734,0.7777,1.0000 2.000,0.9179,0.01005,0.00414,-0.1730,0.7672,1.0000 2.250,0.9448,0.01010,0.00416,-0.1726,0.7558,1.0000 2.500,0.9710,0.01017,0.00424,-0.1721,0.7433,1.0000 2.750,0.9968,0.01024,0.00432,-0.1715,0.7272,1.0000 3.000,1.0204,0.01030,0.00423,-0.1701,0.6797,1.0000 3.250,1.0400,0.01073,0.00416,-0.1679,0.5958,1.0000 3.500,1.0587,0.01134,0.00443,-0.1659,0.5417,1.0000 3.750,1.0724,0.01231,0.00492,-0.1632,0.4687,1.0000 4.000,1.0884,0.01316,0.00544,-0.1610,0.4054,1.0000 4.250,1.0929,0.01503,0.00630,-0.1573,0.2298,1.0000 4.500,1.0947,0.01763,0.00779,-0.1534,0.0325,1.0000 4.750,1.1145,0.01837,0.00854,-0.1519,0.0231,1.0000 5.000,1.1342,0.01912,0.00942,-0.1504,0.0201,1.0000 5.250,1.1542,0.01979,0.01022,-0.1489,0.0186,1.0000 5.500,1.1731,0.02053,0.01111,-0.1473,0.0165,1.0000 5.750,1.1899,0.02144,0.01214,-0.1454,0.0155,1.0000 6.000,1.2045,0.02250,0.01330,-0.1431,0.0146,1.0000 6.250,1.2167,0.02365,0.01455,-0.1404,0.0140,1.0000 6.500,1.2274,0.02492,0.01588,-0.1376,0.0133,1.0000 6.750,1.2367,0.02650,0.01751,-0.1347,0.0122,1.0000 7.000,1.2485,0.02915,0.02024,-0.1323,0.0111,1.0000 7.250,1.2689,0.03053,0.02172,-0.1310,0.0108,1.0000 7.500,1.2926,0.03219,0.02349,-0.1303,0.0105,1.0000 7.750,1.3199,0.03418,0.02562,-0.1301,0.0102,1.0000 8.000,1.3480,0.03647,0.02812,-0.1301,0.0100,1.0000 8.250,1.3730,0.03896,0.03085,-0.1295,0.0098,1.0000 8.500,1.3926,0.04105,0.03320,-0.1281,0.0093,1.0000 8.750,1.4086,0.04292,0.03529,-0.1264,0.0087,1.0000 9.000,1.4223,0.04492,0.03755,-0.1245,0.0082,1.0000 9.250,1.4343,0.04751,0.04041,-0.1224,0.0079,1.0000 9.500,1.4424,0.05041,0.04361,-0.1198,0.0078,1.0000 9.750,1.4452,0.05343,0.04695,-0.1165,0.0078,1.0000 10.000,1.4433,0.05654,0.05037,-0.1128,0.0078,1.0000 10.250,1.4372,0.05980,0.05393,-0.1089,0.0078,1.0000 10.500,1.4273,0.06341,0.05787,-0.1050,0.0079,1.0000 10.750,1.4145,0.06731,0.06208,-0.1014,0.0080,1.0000 11.000,1.3995,0.07153,0.06659,-0.0984,0.0081,1.0000 11.250,1.3826,0.07605,0.07138,-0.0959,0.0082,1.0000 11.500,1.3640,0.08095,0.07655,-0.0943,0.0083,1.0000 11.750,1.3449,0.08616,0.08200,-0.0935,0.0084,1.0000 12.000,1.3249,0.09184,0.08791,-0.0936,0.0085,1.0000 12.250,1.3040,0.09805,0.09432,-0.0947,0.0086,1.0000 12.500,1.2836,0.10470,0.10117,-0.0970,0.0087,1.0000