Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe482-il-50000-n5 Airfoil,goe482-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,17.3424 Max Cl/Cd alpha,1.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe482-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.750,0.0595,0.13429,0.12747,-0.0960,0.9112,0.1148 -11.500,0.0659,0.13317,0.12632,-0.1010,0.9063,0.1191 -11.250,0.0585,0.13355,0.12672,-0.1032,0.8964,0.1199 -11.000,0.0981,0.12514,0.11824,-0.1045,0.8925,0.1233 -10.750,0.1162,0.12190,0.11496,-0.1065,0.8866,0.1289 -10.500,0.1185,0.12088,0.11393,-0.1086,0.8781,0.1338 -10.250,0.1146,0.12105,0.11408,-0.1126,0.8714,0.1353 -10.000,0.1352,0.11570,0.10872,-0.1124,0.8635,0.1372 -9.750,0.1625,0.11120,0.10413,-0.1138,0.8583,0.1423 -9.500,0.1701,0.10935,0.10226,-0.1146,0.8502,0.1473 -9.250,0.1661,0.10916,0.10207,-0.1166,0.8416,0.1512 -9.000,0.1547,0.10959,0.10252,-0.1173,0.8314,0.1522 -8.750,0.1828,0.10389,0.09677,-0.1179,0.8259,0.1544 -8.500,0.2108,0.09981,0.09259,-0.1192,0.8213,0.1595 -8.250,0.2112,0.09875,0.09155,-0.1180,0.8107,0.1636 -8.000,0.2101,0.09801,0.09078,-0.1198,0.8038,0.1686 -7.750,0.1905,0.09886,0.09171,-0.1179,0.7912,0.1697 -7.500,0.1794,0.09856,0.09144,-0.1174,0.7822,0.1702 -7.250,0.1895,0.09546,0.08835,-0.1163,0.7738,0.1710 -7.000,0.2296,0.09038,0.08314,-0.1172,0.7701,0.1754 -6.750,0.2287,0.08941,0.08220,-0.1150,0.7604,0.1788 -6.500,0.2294,0.08812,0.08091,-0.1142,0.7529,0.1828 -6.250,0.2074,0.08875,0.08164,-0.1105,0.7417,0.1859 -5.750,0.1645,0.08229,0.07513,-0.1162,0.7219,0.1202 -5.500,0.1849,0.07980,0.07256,-0.1148,0.7176,0.1177 -5.250,0.1748,0.07920,0.07201,-0.1116,0.7074,0.1163 -5.000,0.1834,0.07673,0.06950,-0.1132,0.7014,0.1151 -4.750,0.1800,0.07532,0.06808,-0.1128,0.6930,0.1144 -4.500,0.1851,0.07311,0.06584,-0.1144,0.6855,0.1138 -4.250,0.2126,0.06888,0.06145,-0.1208,0.6821,0.1121 -4.000,0.1997,0.06791,0.06050,-0.1199,0.6705,0.1106 -3.750,0.2642,0.05760,0.04944,-0.1417,0.6673,0.1061 -3.500,0.3025,0.05509,0.04675,-0.1453,0.6647,0.1077 -3.250,0.2959,0.05525,0.04689,-0.1431,0.6533,0.1083 -3.000,0.3418,0.05223,0.04352,-0.1492,0.6502,0.1100 -2.750,0.3979,0.04862,0.03937,-0.1568,0.6480,0.1108 -2.500,0.3951,0.04909,0.03971,-0.1549,0.6371,0.1110 -2.250,0.4405,0.04690,0.03708,-0.1592,0.6338,0.1124 -2.000,0.4894,0.04493,0.03462,-0.1633,0.6315,0.1162 -1.750,0.4842,0.04618,0.03576,-0.1605,0.6209,0.1173 -1.500,0.5231,0.04494,0.03409,-0.1627,0.6173,0.1203 -1.250,0.5637,0.04368,0.03265,-0.1644,0.6148,0.1229 -1.000,0.5554,0.04550,0.03449,-0.1612,0.6042,0.1237 -0.750,0.5875,0.04490,0.03371,-0.1618,0.6004,0.1271 -0.500,0.6279,0.04391,0.03242,-0.1632,0.5980,0.1336 -0.250,0.6201,0.04621,0.03469,-0.1604,0.5874,0.1357 0.000,0.6503,0.04587,0.03433,-0.1608,0.5835,0.1418 0.250,0.6892,0.04502,0.03323,-0.1618,0.5811,0.1501 0.500,0.7276,0.04427,0.03239,-0.1629,0.5786,0.1619 1.000,0.7483,0.04685,0.03497,-0.1606,0.5640,0.1891 1.250,0.7922,0.04568,0.03402,-0.1624,0.5623,0.2430 1.750,0.8009,0.04959,0.03833,-0.1594,0.5466,0.3560 2.000,0.8383,0.04875,0.03767,-0.1597,0.5448,0.4618 2.500,0.8370,0.05352,0.04287,-0.1559,0.5287,0.5730 2.750,0.8687,0.05250,0.04206,-0.1550,0.5271,0.6728 3.750,0.8567,0.06402,0.05371,-0.1490,0.4944,1.0000 4.250,0.8555,0.07085,0.06039,-0.1478,0.4792,1.0000 4.500,0.8817,0.07141,0.06074,-0.1477,0.4765,1.0000 4.750,0.9120,0.07145,0.06059,-0.1476,0.4746,1.0000 5.250,0.9029,0.07927,0.06837,-0.1465,0.4591,1.0000 5.500,0.9303,0.07969,0.06863,-0.1463,0.4573,1.0000 5.750,0.8953,0.08730,0.07638,-0.1459,0.4455,1.0000 6.000,0.9164,0.08839,0.07736,-0.1457,0.4425,1.0000 6.250,0.9428,0.08885,0.07770,-0.1454,0.4405,1.0000 6.500,0.9114,0.09628,0.08526,-0.1454,0.4302,1.0000 6.750,0.9266,0.09820,0.08711,-0.1453,0.4270,1.0000 7.000,0.9488,0.09921,0.08804,-0.1451,0.4246,1.0000 7.500,0.9396,0.10773,0.09662,-0.1453,0.4123,1.0000 7.750,0.9564,0.10947,0.09831,-0.1452,0.4096,1.0000 8.000,0.9776,0.11068,0.09947,-0.1450,0.4076,1.0000 8.250,0.9571,0.11705,0.10593,-0.1457,0.4001,1.0000 8.500,0.9661,0.11965,0.10854,-0.1458,0.3958,1.0000 8.750,0.9837,0.12122,0.11007,-0.1457,0.3930,1.0000 9.000,1.0046,0.12246,0.11128,-0.1455,0.3911,1.0000 9.250,0.9852,0.12872,0.11765,-0.1466,0.3841,1.0000 9.500,0.9939,0.13133,0.12028,-0.1468,0.3797,1.0000