Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe767-il-50000-n5 Airfoil,goe767-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,23.9355 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-goe767-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.6192,0.09237,0.08433,-0.0031,1.0000,0.0877 -10.000,-0.6460,0.08224,0.07423,-0.0105,1.0000,0.0880 -9.750,-0.6903,0.07150,0.06344,-0.0185,1.0000,0.0877 -9.500,-0.7282,0.06455,0.05631,-0.0204,1.0000,0.0879 -9.250,-0.7565,0.05809,0.04949,-0.0210,1.0000,0.0887 -9.000,-0.7579,0.05454,0.04574,-0.0205,1.0000,0.0903 -8.750,-0.7446,0.05283,0.04402,-0.0196,1.0000,0.0925 -8.500,-0.7395,0.04978,0.04074,-0.0188,1.0000,0.0948 -8.250,-0.7368,0.04599,0.03652,-0.0178,1.0000,0.0976 -8.000,-0.7295,0.04255,0.03263,-0.0166,1.0000,0.1008 -7.750,-0.7103,0.04131,0.03141,-0.0157,1.0000,0.1041 -7.500,-0.6951,0.03920,0.02902,-0.0146,1.0000,0.1090 -7.250,-0.6785,0.03714,0.02671,-0.0135,1.0000,0.1140 -7.000,-0.6584,0.03593,0.02547,-0.0125,1.0000,0.1194 -6.750,-0.6401,0.03410,0.02329,-0.0114,1.0000,0.1263 -6.500,-0.6185,0.03321,0.02248,-0.0105,1.0000,0.1326 -6.250,-0.5983,0.03188,0.02090,-0.0094,1.0000,0.1408 -6.000,-0.5763,0.03107,0.02016,-0.0085,1.0000,0.1485 -5.750,-0.5548,0.03002,0.01895,-0.0075,1.0000,0.1571 -5.500,-0.5323,0.02915,0.01808,-0.0065,1.0000,0.1653 -5.250,-0.5096,0.02813,0.01697,-0.0056,1.0000,0.1731 -5.000,-0.4862,0.02723,0.01608,-0.0047,1.0000,0.1802 -4.750,-0.4624,0.02632,0.01501,-0.0038,1.0000,0.1877 -4.500,-0.4384,0.02545,0.01427,-0.0030,1.0000,0.1941 -4.250,-0.4142,0.02468,0.01343,-0.0021,1.0000,0.2019 -4.000,-0.3900,0.02390,0.01276,-0.0013,1.0000,0.2091 -3.750,-0.3658,0.02322,0.01214,-0.0004,1.0000,0.2170 -3.500,-0.3417,0.02258,0.01158,0.0004,1.0000,0.2259 -3.250,-0.3182,0.02200,0.01113,0.0012,1.0000,0.2362 -3.000,-0.2927,0.02143,0.01074,0.0014,0.9951,0.2475 -2.750,-0.2366,0.02073,0.01022,-0.0041,0.9297,0.2718 -2.500,-0.1832,0.02004,0.00971,-0.0085,0.8462,0.3072 -2.250,-0.1448,0.01948,0.00926,-0.0096,0.7637,0.3592 -2.000,-0.1203,0.01904,0.00898,-0.0080,0.7060,0.4327 -1.750,-0.1002,0.01869,0.00890,-0.0054,0.6651,0.5320 -1.500,-0.0783,0.01853,0.00901,-0.0026,0.6324,0.6450 -1.250,-0.0498,0.01861,0.00917,-0.0009,0.6037,0.7438 -1.000,-0.0111,0.01886,0.00937,-0.0010,0.5762,0.8254 -0.750,0.0355,0.01923,0.00954,-0.0030,0.5506,0.8882 -0.500,0.0876,0.01961,0.00964,-0.0064,0.5271,0.9385 -0.250,0.1573,0.01987,0.00961,-0.0137,0.5020,0.9831 0.000,0.2009,0.01997,0.00947,-0.0170,0.4836,1.0000 0.250,0.2215,0.02011,0.00946,-0.0159,0.4703,1.0000 0.500,0.2429,0.02029,0.00953,-0.0149,0.4573,1.0000 0.750,0.2644,0.02051,0.00960,-0.0138,0.4463,1.0000 1.000,0.2860,0.02076,0.00975,-0.0128,0.4345,1.0000 1.250,0.3083,0.02105,0.00994,-0.0118,0.4235,1.0000 1.500,0.3309,0.02136,0.01012,-0.0108,0.4138,1.0000 1.750,0.3537,0.02173,0.01045,-0.0099,0.4041,1.0000 2.000,0.3764,0.02210,0.01072,-0.0089,0.3953,1.0000 2.250,0.3992,0.02253,0.01111,-0.0080,0.3864,1.0000 2.500,0.4220,0.02295,0.01147,-0.0070,0.3779,1.0000 2.750,0.4449,0.02342,0.01187,-0.0061,0.3703,1.0000 3.000,0.4676,0.02394,0.01240,-0.0052,0.3618,1.0000 3.250,0.4907,0.02436,0.01268,-0.0041,0.3551,1.0000 3.500,0.5129,0.02497,0.01340,-0.0032,0.3456,1.0000 3.750,0.5357,0.02539,0.01372,-0.0021,0.3383,1.0000 4.000,0.5577,0.02600,0.01440,-0.0012,0.3290,1.0000 4.250,0.5804,0.02642,0.01475,-0.0001,0.3211,1.0000 4.500,0.6023,0.02704,0.01544,0.0008,0.3124,1.0000 4.750,0.6248,0.02754,0.01591,0.0018,0.3043,1.0000 5.000,0.6470,0.02817,0.01656,0.0028,0.2967,1.0000 5.250,0.6687,0.02884,0.01731,0.0037,0.2884,1.0000 5.500,0.6917,0.02933,0.01771,0.0047,0.2819,1.0000 5.750,0.7119,0.03029,0.01887,0.0056,0.2731,1.0000 6.000,0.7353,0.03072,0.01920,0.0066,0.2670,1.0000 6.250,0.7541,0.03188,0.02060,0.0075,0.2584,1.0000 6.500,0.7764,0.03250,0.02119,0.0084,0.2519,1.0000 6.750,0.7956,0.03361,0.02243,0.0093,0.2447,1.0000 7.000,0.8152,0.03460,0.02353,0.0103,0.2375,1.0000 7.250,0.8388,0.03505,0.02385,0.0112,0.2325,1.0000 7.500,0.8511,0.03711,0.02628,0.0121,0.2247,1.0000 7.750,0.8717,0.03792,0.02712,0.0130,0.2192,1.0000 8.000,0.8890,0.03923,0.02851,0.0140,0.2138,1.0000 8.250,0.8982,0.04147,0.03104,0.0149,0.2072,1.0000 8.500,0.9177,0.04240,0.03197,0.0158,0.2027,1.0000 8.750,0.9315,0.04404,0.03372,0.0167,0.1982,1.0000 9.000,0.9253,0.04779,0.03786,0.0175,0.1925,1.0000 9.250,0.9366,0.04940,0.03954,0.0184,0.1881,1.0000 9.500,0.9655,0.04923,0.03925,0.0195,0.1848,1.0000 9.750,0.8960,0.05902,0.04956,0.0185,0.1807,1.0000 10.000,0.7742,0.07994,0.07056,0.0053,0.1745,1.0000 10.250,0.7942,0.08003,0.07066,0.0068,0.1718,1.0000 10.750,0.7286,0.09933,0.08994,-0.0042,0.1621,1.0000 11.000,0.7394,0.10133,0.09196,-0.0041,0.1588,1.0000