Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe359-il-200000-n5 Airfoil,goe359-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,82.0458 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe359-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.2748,0.11603,0.11261,-0.0303,1.0000,0.0180 -9.000,-0.2710,0.11324,0.10987,-0.0310,1.0000,0.0180 -8.750,-0.2677,0.11047,0.10715,-0.0315,1.0000,0.0180 -8.500,-0.1712,0.09035,0.08739,-0.0370,0.9932,0.0186 -8.250,-0.1543,0.08615,0.08318,-0.0383,0.9854,0.0199 -8.000,-0.1422,0.08238,0.07941,-0.0408,0.9733,0.0210 -7.750,-0.1311,0.07847,0.07550,-0.0435,0.9561,0.0218 -7.500,-0.1177,0.07429,0.07129,-0.0469,0.9390,0.0227 -7.250,-0.2275,0.09006,0.08699,-0.0347,0.9843,0.0196 -7.000,-0.2086,0.08646,0.08338,-0.0388,0.9662,0.0205 -6.750,-0.1869,0.08244,0.07935,-0.0443,0.9441,0.0211 -6.500,-0.1480,0.07602,0.07284,-0.0598,0.9234,0.0178 -6.250,-0.1250,0.07149,0.06825,-0.0631,0.9104,0.0172 -6.000,-0.0967,0.06693,0.06360,-0.0697,0.8946,0.0170 -5.750,-0.0674,0.06229,0.05885,-0.0769,0.8782,0.0171 -5.500,-0.0399,0.05841,0.05488,-0.0827,0.8626,0.0193 -5.250,-0.0174,0.05622,0.05260,-0.0850,0.8481,0.0213 -5.000,0.0128,0.05162,0.04785,-0.0911,0.8347,0.0206 -4.750,0.0433,0.04748,0.04354,-0.0963,0.8222,0.0207 -4.500,0.0738,0.04382,0.03971,-0.1005,0.8096,0.0217 -4.250,0.1076,0.04004,0.03568,-0.1049,0.7976,0.0244 -4.000,0.1435,0.03528,0.03060,-0.1093,0.7866,0.0253 -3.750,0.1776,0.03064,0.02556,-0.1127,0.7763,0.0282 -3.500,0.1998,0.03033,0.02520,-0.1127,0.7641,0.0309 -3.250,0.2307,0.02719,0.02171,-0.1143,0.7527,0.0321 -3.000,0.2611,0.02446,0.01855,-0.1153,0.7415,0.0345 -2.750,0.2915,0.02193,0.01549,-0.1158,0.7305,0.0365 -2.500,0.3203,0.02019,0.01329,-0.1160,0.7192,0.0372 -2.250,0.3487,0.01917,0.01183,-0.1159,0.7077,0.0390 -2.000,0.3759,0.01764,0.01000,-0.1160,0.6968,0.0400 -1.750,0.4035,0.01676,0.00880,-0.1158,0.6856,0.0398 -1.250,0.4580,0.01526,0.00685,-0.1154,0.6630,0.0406 -1.000,0.4851,0.01470,0.00613,-0.1151,0.6522,0.0414 -0.750,0.5121,0.01427,0.00556,-0.1149,0.6420,0.0423 -0.500,0.5389,0.01393,0.00510,-0.1145,0.6311,0.0431 -0.250,0.5657,0.01366,0.00475,-0.1143,0.6196,0.0447 0.000,0.5923,0.01348,0.00449,-0.1140,0.6078,0.0472 0.250,0.6189,0.01329,0.00422,-0.1136,0.5960,0.0478 0.500,0.6454,0.01314,0.00399,-0.1133,0.5850,0.0478 0.750,0.6722,0.01301,0.00382,-0.1130,0.5740,0.0479 1.000,0.6989,0.01294,0.00370,-0.1128,0.5637,0.0482 1.250,0.7255,0.01291,0.00360,-0.1125,0.5537,0.0486 1.500,0.7522,0.01291,0.00353,-0.1122,0.5435,0.0493 1.750,0.7789,0.01293,0.00350,-0.1119,0.5338,0.0503 2.000,0.8053,0.01296,0.00347,-0.1116,0.5236,0.0526 2.250,0.8316,0.01299,0.00347,-0.1113,0.5129,0.0592 2.500,0.8577,0.01268,0.00367,-0.1112,0.5031,0.2789 3.000,0.9083,0.01172,0.00389,-0.1101,0.4849,1.0000 3.250,0.9341,0.01192,0.00401,-0.1098,0.4739,1.0000 3.500,0.9597,0.01213,0.00416,-0.1094,0.4623,1.0000 3.750,0.9851,0.01235,0.00431,-0.1089,0.4509,1.0000 4.000,1.0107,0.01257,0.00449,-0.1085,0.4402,1.0000 4.250,1.0363,0.01278,0.00468,-0.1082,0.4303,1.0000 4.500,1.0614,0.01302,0.00491,-0.1077,0.4196,1.0000 4.750,1.0863,0.01327,0.00514,-0.1073,0.4082,1.0000 5.000,1.1109,0.01354,0.00538,-0.1067,0.3932,1.0000 5.250,1.1337,0.01388,0.00564,-0.1060,0.3629,1.0000 5.500,1.1540,0.01444,0.00594,-0.1049,0.3110,1.0000 5.750,1.1713,0.01533,0.00645,-0.1034,0.2555,1.0000 6.000,1.1890,0.01626,0.00709,-0.1021,0.2162,1.0000 6.250,1.2089,0.01697,0.00768,-0.1010,0.1866,1.0000 6.500,1.2202,0.01849,0.00864,-0.0990,0.1090,1.0000 6.750,1.2323,0.01992,0.00974,-0.0969,0.0544,1.0000 7.000,1.2515,0.02062,0.01046,-0.0957,0.0429,1.0000 7.250,1.2669,0.02166,0.01143,-0.0940,0.0175,1.0000 7.500,1.2852,0.02239,0.01230,-0.0926,0.0155,1.0000 7.750,1.3027,0.02315,0.01323,-0.0911,0.0143,1.0000 8.000,1.3183,0.02404,0.01429,-0.0893,0.0130,1.0000 8.250,1.3334,0.02489,0.01529,-0.0876,0.0120,1.0000 8.500,1.3454,0.02584,0.01640,-0.0853,0.0115,1.0000 8.750,1.3551,0.02691,0.01762,-0.0829,0.0110,1.0000 9.000,1.3627,0.02814,0.01901,-0.0803,0.0106,1.0000 9.250,1.3682,0.02956,0.02059,-0.0778,0.0103,1.0000 9.500,1.3712,0.03124,0.02246,-0.0753,0.0100,1.0000 9.750,1.3714,0.03326,0.02463,-0.0730,0.0097,1.0000 10.000,1.3676,0.03580,0.02732,-0.0710,0.0093,1.0000 10.250,1.3592,0.03900,0.03064,-0.0692,0.0090,1.0000 10.500,1.3476,0.04275,0.03449,-0.0678,0.0088,1.0000 10.750,1.3543,0.04476,0.03662,-0.0671,0.0084,1.0000 11.000,1.3546,0.04753,0.03951,-0.0664,0.0082,1.0000 11.250,1.3531,0.05054,0.04263,-0.0658,0.0081,1.0000 11.500,1.3516,0.05361,0.04581,-0.0652,0.0080,1.0000 11.750,1.3504,0.05667,0.04896,-0.0646,0.0079,1.0000 12.000,1.3497,0.05967,0.05205,-0.0640,0.0077,1.0000 12.250,1.3499,0.06255,0.05502,-0.0633,0.0076,1.0000 12.500,1.3511,0.06532,0.05786,-0.0625,0.0075,1.0000 12.750,1.3532,0.06798,0.06061,-0.0617,0.0074,1.0000 13.000,1.3563,0.07055,0.06327,-0.0608,0.0073,1.0000 13.250,1.3603,0.07305,0.06591,-0.0599,0.0073,1.0000 13.500,1.3647,0.07554,0.06850,-0.0589,0.0072,1.0000 13.750,1.3685,0.07817,0.07125,-0.0582,0.0071,1.0000 14.000,1.3713,0.08100,0.07419,-0.0577,0.0069,1.0000 14.250,1.3745,0.08378,0.07706,-0.0572,0.0067,1.0000 14.500,1.3839,0.08565,0.07891,-0.0558,0.0063,1.0000 14.750,1.3957,0.08773,0.08101,-0.0535,0.0060,1.0000 15.000,1.3828,0.09268,0.08622,-0.0554,0.0059,1.0000 15.250,1.3746,0.09733,0.09110,-0.0569,0.0059,1.0000