Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe801-il-50000 Airfoil,goe801-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,17.9231 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe801-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.2549,0.12519,0.11818,-0.0344,1.0000,0.1223 -9.500,-0.2640,0.12537,0.11848,-0.0347,1.0000,0.1250 -9.250,-0.2809,0.12672,0.11999,-0.0344,1.0000,0.1259 -9.000,-0.2658,0.12040,0.11371,-0.0330,1.0000,0.1286 -8.750,-0.2583,0.11689,0.11024,-0.0312,1.0000,0.1327 -8.500,-0.2621,0.11533,0.10876,-0.0296,1.0000,0.1362 -8.250,-0.2724,0.11464,0.10819,-0.0278,1.0000,0.1392 -8.000,-0.2905,0.11502,0.10870,-0.0255,1.0000,0.1411 -7.750,-0.3138,0.11591,0.10974,-0.0227,1.0000,0.1419 -7.500,-0.3363,0.11681,0.11079,-0.0213,1.0000,0.1425 -7.250,-0.3295,0.11191,0.10595,-0.0187,1.0000,0.1447 -7.000,-0.3218,0.10822,0.10229,-0.0159,1.0000,0.1491 -6.750,-0.3294,0.10678,0.10094,-0.0140,1.0000,0.1526 -6.500,-0.3405,0.10592,0.10017,-0.0133,1.0000,0.1562 -6.250,-0.3554,0.10638,0.10072,-0.0158,1.0000,0.1589 -6.000,-0.3580,0.10361,0.09804,-0.0154,1.0000,0.1608 -5.750,-0.3533,0.09984,0.09431,-0.0108,1.0000,0.1654 -5.500,-0.3551,0.09806,0.09259,-0.0105,1.0000,0.1714 -5.250,-0.3563,0.09779,0.09234,-0.0178,1.0000,0.1768 -5.000,-0.3554,0.09361,0.08825,-0.0114,1.0000,0.1811 -4.750,-0.3520,0.09180,0.08646,-0.0124,1.0000,0.1898 -4.250,-0.3432,0.08686,0.08160,-0.0128,1.0000,0.2030 -4.000,-0.3328,0.08458,0.07931,-0.0166,1.0000,0.2121 -3.750,-0.3160,0.08316,0.07782,-0.0220,1.0000,0.2262 -3.500,-0.3161,0.07974,0.07451,-0.0173,1.0000,0.2312 -3.250,-0.3021,0.07753,0.07228,-0.0200,1.0000,0.2453 -3.000,-0.2885,0.07536,0.07010,-0.0219,1.0000,0.2609 -2.750,-0.2595,0.07231,0.06705,-0.0247,0.9934,0.2831 -2.500,-0.2167,0.06929,0.06396,-0.0316,0.9822,0.3260 -1.750,-0.1592,0.06133,0.05623,-0.0267,0.9495,0.4954 -1.500,-0.1427,0.05890,0.05389,-0.0226,0.9397,0.5693 -1.250,-0.1337,0.05662,0.05169,-0.0183,0.9279,0.6229 -1.000,-0.1202,0.05425,0.04939,-0.0146,0.9166,0.6677 -0.750,-0.0885,0.05181,0.04694,-0.0160,0.9056,0.7074 -0.500,0.2159,0.05067,0.04347,-0.0968,0.8814,0.3384 -0.250,0.2963,0.04898,0.04053,-0.1065,0.8690,0.2073 0.000,0.3617,0.04732,0.03809,-0.1123,0.8590,0.1758 0.250,0.3937,0.04640,0.03703,-0.1135,0.8454,0.1694 0.500,0.4290,0.04588,0.03619,-0.1148,0.8322,0.1657 0.750,0.4664,0.04543,0.03544,-0.1163,0.8197,0.1639 1.000,0.5203,0.04446,0.03406,-0.1194,0.8104,0.1617 1.250,0.5470,0.04451,0.03391,-0.1191,0.7965,0.1625 1.500,0.5737,0.04464,0.03393,-0.1188,0.7833,0.1652 1.750,0.6033,0.04475,0.03395,-0.1189,0.7709,0.1725 2.000,0.6548,0.04379,0.03296,-0.1212,0.7625,0.1923 2.250,0.6748,0.04434,0.03362,-0.1204,0.7488,0.2115 2.500,0.6992,0.04450,0.03431,-0.1205,0.7361,0.3005 2.750,0.7212,0.04387,0.03444,-0.1185,0.7252,1.0000 3.000,0.7605,0.04397,0.03413,-0.1192,0.7158,1.0000 3.250,0.7717,0.04562,0.03564,-0.1177,0.7024,1.0000 3.500,0.7863,0.04715,0.03704,-0.1166,0.6902,1.0000 3.750,0.8345,0.04656,0.03627,-0.1179,0.6832,1.0000 4.000,0.8347,0.04912,0.03880,-0.1159,0.6699,1.0000 4.250,0.8404,0.05143,0.04108,-0.1144,0.6580,1.0000 4.500,0.8885,0.05070,0.04024,-0.1154,0.6514,1.0000 4.750,0.8776,0.05439,0.04395,-0.1132,0.6386,1.0000 5.000,0.8809,0.05711,0.04665,-0.1119,0.6281,1.0000 5.250,0.9201,0.05697,0.04649,-0.1121,0.6203,1.0000 5.500,0.9043,0.06130,0.05084,-0.1103,0.6087,1.0000 5.750,0.9240,0.06272,0.05226,-0.1096,0.5991,1.0000 6.000,0.9496,0.06349,0.05304,-0.1089,0.5889,1.0000 6.250,0.9418,0.06713,0.05669,-0.1073,0.5767,1.0000 6.500,0.9570,0.06875,0.05833,-0.1063,0.5654,1.0000 6.750,1.0141,0.06627,0.05591,-0.1057,0.5554,1.0000 7.500,1.0130,0.07562,0.06538,-0.1018,0.5186,1.0000 7.750,1.0551,0.07426,0.06412,-0.1004,0.5075,1.0000 8.000,1.0367,0.07940,0.06930,-0.0993,0.4937,1.0000 8.250,1.0296,0.08344,0.07340,-0.0984,0.4807,1.0000 8.500,1.0377,0.08586,0.07588,-0.0972,0.4680,1.0000 8.750,1.0757,0.08474,0.07487,-0.0954,0.4562,1.0000 9.000,1.0882,0.08657,0.07679,-0.0942,0.4437,1.0000 9.250,1.0600,0.09355,0.08379,-0.0942,0.4303,1.0000 9.500,1.0477,0.09872,0.08901,-0.0940,0.4184,1.0000 11.500,1.0671,0.12915,0.11999,-0.0930,0.3476,1.0000 11.750,1.0388,0.13776,0.12862,-0.0960,0.3464,1.0000 12.000,1.0201,0.14468,0.13558,-0.0985,0.3449,1.0000