Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe625-il-100000 Airfoil,goe625-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,33.8147 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe625-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.1389,0.13423,0.12933,-0.0615,0.9692,0.1437 -10.750,-0.1346,0.13113,0.12621,-0.0677,0.9657,0.1498 -10.500,-0.1588,0.12849,0.12363,-0.0723,0.9571,0.1518 -10.250,-0.1059,0.12287,0.11795,-0.0732,0.9544,0.1543 -10.000,-0.0755,0.11896,0.11400,-0.0770,0.9514,0.1592 -9.750,-0.1036,0.11769,0.11277,-0.0816,0.9415,0.1657 -9.500,-0.0870,0.11228,0.10735,-0.0855,0.9373,0.1678 -9.250,-0.0380,0.10773,0.10273,-0.0879,0.9354,0.1714 -9.000,0.0327,0.09831,0.09353,-0.1011,0.9026,0.1841 -8.750,0.0934,0.09292,0.08807,-0.1032,0.9007,0.1881 -8.500,0.1144,0.08895,0.08406,-0.1066,0.8977,0.1963 -8.250,0.0224,0.08896,0.08416,-0.1077,0.8808,0.2010 -8.000,0.1131,0.08230,0.07741,-0.1081,0.8808,0.2051 -7.750,0.1291,0.07999,0.07510,-0.1072,0.8715,0.2103 -7.500,0.0487,0.07799,0.07316,-0.1102,0.8594,0.2198 -7.250,0.0044,0.08311,0.07810,-0.1059,0.8722,0.2184 -7.000,0.0047,0.07887,0.07386,-0.1072,0.8635,0.2227 -6.750,0.0621,0.07591,0.07083,-0.1080,0.8614,0.2298 -6.500,-0.0121,0.07316,0.06803,-0.1101,0.8426,0.2411 -6.250,0.0460,0.07006,0.06495,-0.1092,0.8408,0.2451 -6.000,-0.0658,0.05102,0.04456,-0.1177,0.8216,0.1678 -5.750,-0.0652,0.04864,0.04182,-0.1149,0.8075,0.1656 -5.500,-0.0340,0.04498,0.03766,-0.1170,0.8032,0.1663 -5.250,-0.0225,0.04293,0.03538,-0.1150,0.7906,0.1668 -5.000,0.0151,0.04025,0.03268,-0.1169,0.7854,0.1691 -4.750,0.0410,0.03882,0.03118,-0.1166,0.7757,0.1716 -4.500,0.0720,0.03686,0.02897,-0.1171,0.7673,0.1738 -4.250,0.1132,0.03452,0.02626,-0.1191,0.7630,0.1763 -4.000,0.1306,0.03350,0.02501,-0.1173,0.7485,0.1789 -3.750,0.1723,0.03172,0.02274,-0.1191,0.7435,0.1825 -3.500,0.1914,0.03063,0.02154,-0.1176,0.7290,0.1849 -3.250,0.2209,0.02957,0.02041,-0.1176,0.7186,0.1885 -3.000,0.2532,0.02862,0.01931,-0.1180,0.7087,0.1939 -2.750,0.2794,0.02802,0.01847,-0.1174,0.6968,0.1993 -2.500,0.3143,0.02680,0.01712,-0.1183,0.6884,0.2053 -2.250,0.3376,0.02640,0.01668,-0.1173,0.6761,0.2119 -2.000,0.3734,0.02550,0.01556,-0.1183,0.6685,0.2226 -1.750,0.3942,0.02528,0.01542,-0.1171,0.6570,0.2329 -1.500,0.4280,0.02455,0.01460,-0.1179,0.6501,0.2477 -1.250,0.4495,0.02448,0.01453,-0.1168,0.6405,0.2623 -1.000,0.4791,0.02414,0.01416,-0.1170,0.6334,0.2808 -0.750,0.5070,0.02390,0.01399,-0.1170,0.6269,0.2998 -0.500,0.5284,0.02391,0.01413,-0.1160,0.6188,0.3182 -0.250,0.5600,0.02360,0.01384,-0.1165,0.6132,0.3447 0.000,0.5826,0.02360,0.01406,-0.1157,0.6068,0.3775 0.250,0.6035,0.02349,0.01435,-0.1147,0.6004,0.4438 0.500,0.6435,0.02231,0.01472,-0.1144,0.5957,0.9258 0.750,0.7305,0.02268,0.01472,-0.1258,0.5899,1.0000 1.000,0.7403,0.02330,0.01528,-0.1230,0.5841,1.0000 1.250,0.7601,0.02365,0.01548,-0.1218,0.5791,1.0000 1.500,0.7883,0.02385,0.01545,-0.1219,0.5752,1.0000 1.750,0.8061,0.02445,0.01595,-0.1205,0.5711,1.0000 2.000,0.8142,0.02531,0.01683,-0.1176,0.5662,1.0000 2.250,0.8326,0.02588,0.01732,-0.1162,0.5617,1.0000 2.500,0.8598,0.02619,0.01748,-0.1162,0.5578,1.0000 2.750,0.8944,0.02645,0.01752,-0.1174,0.5546,1.0000 3.000,0.8931,0.02776,0.01897,-0.1132,0.5497,1.0000 3.250,0.9044,0.02870,0.01992,-0.1109,0.5449,1.0000 3.500,0.9295,0.02912,0.02025,-0.1106,0.5407,1.0000 3.750,0.9670,0.02916,0.02009,-0.1121,0.5370,1.0000 4.000,0.9710,0.03041,0.02141,-0.1089,0.5318,1.0000 4.250,0.9768,0.03151,0.02257,-0.1059,0.5259,1.0000 4.500,1.0071,0.03168,0.02262,-0.1063,0.5213,1.0000 4.750,1.0507,0.03152,0.02226,-0.1087,0.5177,1.0000 5.000,1.0388,0.03349,0.02440,-0.1033,0.5124,1.0000 5.250,1.0318,0.03528,0.02630,-0.0989,0.5068,1.0000 5.500,1.0621,0.03551,0.02645,-0.0993,0.5027,1.0000 5.750,1.1109,0.03510,0.02587,-0.1023,0.4994,1.0000 6.000,1.0815,0.03800,0.02897,-0.0951,0.4937,1.0000 6.250,0.9812,0.04500,0.03628,-0.0810,0.4841,1.0000 6.500,1.0738,0.04139,0.03245,-0.0875,0.4830,1.0000 6.750,1.1533,0.03959,0.03045,-0.0941,0.4805,1.0000 7.000,0.8964,0.06048,0.05198,-0.0710,0.4588,1.0000 7.250,0.9603,0.05669,0.04808,-0.0721,0.4589,1.0000 7.500,1.0351,0.05251,0.04377,-0.0745,0.4589,1.0000 7.750,1.1402,0.04715,0.03821,-0.0805,0.4591,1.0000 10.000,0.7071,0.12423,0.11622,-0.0669,0.3607,1.0000 10.250,0.6972,0.12975,0.12179,-0.0680,0.3610,1.0000