Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e817-il-200000-n5 Airfoil,e817-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,71.3484 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e817-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.5363,0.08600,0.08258,-0.0519,0.9986,0.0048 -10.750,-0.5470,0.07674,0.07323,-0.0595,0.9960,0.0047 -10.500,-0.5585,0.06787,0.06422,-0.0679,0.9928,0.0047 -10.250,-0.5710,0.05983,0.05599,-0.0760,0.9879,0.0046 -10.000,-0.5749,0.05363,0.04959,-0.0836,0.9833,0.0046 -9.750,-0.5827,0.04805,0.04376,-0.0897,0.9764,0.0046 -9.500,-0.5862,0.04354,0.03897,-0.0949,0.9698,0.0045 -9.250,-0.5889,0.03998,0.03512,-0.0970,0.9619,0.0045 -9.000,-0.5799,0.03620,0.03093,-0.0995,0.9577,0.0045 -8.750,-0.5675,0.03315,0.02750,-0.1006,0.9539,0.0046 -8.500,-0.5560,0.03079,0.02476,-0.1002,0.9489,0.0046 -8.250,-0.5365,0.02840,0.02205,-0.1009,0.9463,0.0047 -8.000,-0.5133,0.02629,0.01966,-0.1017,0.9445,0.0048 -7.750,-0.4880,0.02447,0.01760,-0.1028,0.9432,0.0049 -7.500,-0.4745,0.02330,0.01626,-0.1011,0.9388,0.0051 -7.250,-0.4552,0.02149,0.01425,-0.1011,0.9356,0.0054 -7.000,-0.4298,0.01990,0.01246,-0.1021,0.9336,0.0066 -6.750,-0.4008,0.01896,0.01136,-0.1033,0.9322,0.0079 -6.500,-0.3709,0.01816,0.01043,-0.1047,0.9311,0.0121 -6.250,-0.3402,0.01696,0.00917,-0.1062,0.9302,0.0257 -6.000,-0.3216,0.01609,0.00851,-0.1055,0.9268,0.0663 -5.750,-0.2985,0.01496,0.00778,-0.1061,0.9241,0.1467 -5.500,-0.2704,0.01425,0.00732,-0.1071,0.9223,0.2365 -5.250,-0.2404,0.01398,0.00707,-0.1081,0.9209,0.2776 -5.000,-0.2098,0.01381,0.00685,-0.1090,0.9197,0.3038 -4.750,-0.1788,0.01366,0.00667,-0.1099,0.9188,0.3266 -4.500,-0.1474,0.01355,0.00652,-0.1110,0.9179,0.3514 -4.250,-0.1156,0.01346,0.00639,-0.1121,0.9171,0.3732 -4.000,-0.0949,0.01348,0.00638,-0.1109,0.9137,0.3846 -3.750,-0.0715,0.01347,0.00630,-0.1102,0.9108,0.3947 -3.500,-0.0437,0.01344,0.00621,-0.1104,0.9091,0.4053 -3.250,-0.0137,0.01339,0.00612,-0.1111,0.9076,0.4166 -3.000,0.0173,0.01332,0.00603,-0.1119,0.9064,0.4275 -2.750,0.0486,0.01326,0.00597,-0.1129,0.9054,0.4388 -2.500,0.0801,0.01321,0.00588,-0.1138,0.9045,0.4504 -2.250,0.1124,0.01315,0.00583,-0.1149,0.9036,0.4620 -2.000,0.1265,0.01335,0.00604,-0.1124,0.8984,0.4721 -1.750,0.1537,0.01337,0.00608,-0.1125,0.8961,0.4841 -1.500,0.1836,0.01336,0.00608,-0.1131,0.8944,0.4959 -1.250,0.2149,0.01333,0.00609,-0.1139,0.8930,0.5083 -1.000,0.2468,0.01329,0.00610,-0.1149,0.8919,0.5210 -0.750,0.2795,0.01325,0.00610,-0.1160,0.8908,0.5336 -0.500,0.2969,0.01344,0.00636,-0.1141,0.8858,0.5449 -0.250,0.3234,0.01349,0.00648,-0.1140,0.8829,0.5574 0.000,0.3539,0.01347,0.00653,-0.1146,0.8809,0.5704 0.250,0.3862,0.01342,0.00656,-0.1156,0.8793,0.5839 0.500,0.4197,0.01335,0.00658,-0.1167,0.8779,0.5976 1.000,0.4676,0.01350,0.00695,-0.1153,0.8690,0.6235 1.250,0.5010,0.01337,0.00694,-0.1163,0.8666,0.6377 1.500,0.5367,0.01319,0.00689,-0.1178,0.8647,0.6522 1.750,0.5568,0.01327,0.00714,-0.1162,0.8576,0.6655 2.000,0.5910,0.01303,0.00703,-0.1172,0.8535,0.6801 2.250,0.6231,0.01279,0.00694,-0.1176,0.8481,0.6946 2.500,0.6542,0.01245,0.00675,-0.1178,0.8396,0.7095 2.750,0.6833,0.01204,0.00648,-0.1173,0.8270,0.7245 3.000,0.7091,0.01158,0.00614,-0.1160,0.8068,0.7396 3.250,0.7315,0.01128,0.00603,-0.1142,0.7810,0.7550 3.500,0.7539,0.01102,0.00587,-0.1124,0.7410,0.7707 3.750,0.7884,0.01105,0.00516,-0.1123,0.5824,0.7861 4.000,0.7928,0.01210,0.00563,-0.1075,0.4604,0.8030 4.250,0.7947,0.01328,0.00624,-0.1027,0.3386,0.8218 4.500,0.7985,0.01449,0.00689,-0.0984,0.2181,0.8430 4.750,0.8072,0.01547,0.00749,-0.0950,0.1313,0.8687 5.000,0.8162,0.01626,0.00803,-0.0916,0.0764,0.9063 5.250,0.8316,0.01694,0.00856,-0.0894,0.0409,1.0000 5.500,0.8508,0.01784,0.00930,-0.0882,0.0188,1.0000 5.750,0.8704,0.01878,0.01029,-0.0868,0.0120,1.0000 6.000,0.8903,0.01968,0.01137,-0.0855,0.0099,1.0000 6.250,0.9084,0.02085,0.01264,-0.0839,0.0086,1.0000 6.500,0.9254,0.02246,0.01437,-0.0821,0.0079,1.0000 6.750,0.9469,0.02439,0.01643,-0.0811,0.0075,1.0000 7.000,0.9737,0.02615,0.01835,-0.0810,0.0073,1.0000 7.250,1.0025,0.02827,0.02069,-0.0812,0.0072,1.0000 7.500,1.0295,0.03068,0.02338,-0.0810,0.0071,1.0000 7.750,1.0530,0.03338,0.02642,-0.0803,0.0070,1.0000 8.000,1.0720,0.03612,0.02954,-0.0788,0.0068,1.0000 8.250,1.0879,0.03834,0.03208,-0.0770,0.0063,1.0000 8.500,1.1011,0.04049,0.03454,-0.0749,0.0056,1.0000 8.750,1.1112,0.04261,0.03694,-0.0726,0.0050,1.0000 9.000,1.1179,0.04476,0.03934,-0.0700,0.0046,1.0000 9.250,1.1173,0.04767,0.04257,-0.0663,0.0045,1.0000 9.500,1.1110,0.05095,0.04617,-0.0622,0.0044,1.0000 9.750,1.1011,0.05432,0.04983,-0.0581,0.0044,1.0000 10.000,1.0878,0.05797,0.05384,-0.0543,0.0043,1.0000 10.250,1.0713,0.06210,0.05823,-0.0511,0.0043,1.0000 10.500,1.0531,0.06650,0.06287,-0.0486,0.0043,1.0000 10.750,1.0309,0.07185,0.06839,-0.0471,0.0044,1.0000 11.000,1.0068,0.07793,0.07470,-0.0470,0.0044,1.0000 11.250,0.9810,0.08508,0.08204,-0.0487,0.0045,1.0000 11.500,0.9549,0.09371,0.09084,-0.0529,0.0047,1.0000