Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe359-il-1000000 Airfoil,goe359-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,130.602 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe359-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.2755,0.09981,0.09829,-0.0256,1.0000,0.0103 -8.250,-0.2721,0.09718,0.09568,-0.0258,1.0000,0.0109 -8.000,-0.2701,0.09448,0.09300,-0.0264,0.9999,0.0115 -7.750,-0.2498,0.09004,0.08857,-0.0335,0.9951,0.0116 -7.500,-0.2327,0.08601,0.08454,-0.0388,0.9828,0.0117 -7.250,-0.2061,0.08107,0.07958,-0.0468,0.9563,0.0117 -7.000,-0.1758,0.07418,0.07257,-0.0570,0.9158,0.0119 -6.750,-0.1616,0.07155,0.06976,-0.0586,0.8793,0.0121 -6.500,-0.1457,0.06900,0.06710,-0.0611,0.8574,0.0124 -6.250,-0.1273,0.06623,0.06424,-0.0645,0.8403,0.0128 -6.000,-0.1064,0.06314,0.06108,-0.0686,0.8259,0.0138 -5.750,-0.0690,0.05771,0.05553,-0.0793,0.8128,0.0155 -5.500,-0.0420,0.05343,0.05115,-0.0846,0.8007,0.0155 -5.250,-0.0139,0.04899,0.04660,-0.0897,0.7891,0.0156 -5.000,0.0164,0.02823,0.02584,-0.0865,0.7466,0.0164 -4.750,0.0390,0.02604,0.02358,-0.0886,0.7346,0.0172 -4.500,0.0755,0.02235,0.01970,-0.0942,0.7246,0.0202 -4.250,0.1045,0.01832,0.01550,-0.0978,0.7144,0.0203 -4.000,0.1284,0.01378,0.01076,-0.1010,0.7047,0.0195 -3.750,0.1639,0.02391,0.02036,-0.1098,0.7195,0.0215 -3.500,0.1875,0.02458,0.02102,-0.1097,0.7056,0.0226 -3.250,0.2188,0.02394,0.02018,-0.1095,0.6919,0.0266 -2.750,0.2752,0.01578,0.01096,-0.1111,0.6672,0.0279 -2.500,0.3014,0.01479,0.00987,-0.1112,0.6534,0.0290 -2.250,0.3282,0.01430,0.00929,-0.1112,0.6404,0.0303 -2.000,0.3556,0.01381,0.00865,-0.1112,0.6286,0.0327 -1.750,0.3840,0.01513,0.00990,-0.1107,0.6163,0.0359 -1.500,0.4117,0.01428,0.00881,-0.1105,0.6047,0.0360 -1.250,0.4393,0.01347,0.00780,-0.1104,0.5933,0.0361 -1.000,0.4667,0.01063,0.00467,-0.1105,0.5832,0.0331 -0.750,0.4944,0.01018,0.00410,-0.1103,0.5725,0.0335 -0.500,0.5220,0.00970,0.00350,-0.1101,0.5614,0.0335 -0.250,0.5494,0.00943,0.00314,-0.1099,0.5498,0.0341 0.000,0.5769,0.00922,0.00286,-0.1098,0.5385,0.0346 0.250,0.6043,0.00903,0.00262,-0.1096,0.5278,0.0349 0.500,0.6315,0.00888,0.00241,-0.1094,0.5139,0.0351 0.750,0.6585,0.00878,0.00223,-0.1092,0.4973,0.0353 1.000,0.6855,0.00878,0.00216,-0.1090,0.4816,0.0358 1.250,0.7127,0.00876,0.00208,-0.1089,0.4693,0.0361 1.500,0.7400,0.00857,0.00184,-0.1088,0.4595,0.0369 1.750,0.7674,0.00848,0.00169,-0.1086,0.4506,0.0395 2.000,0.7949,0.00847,0.00167,-0.1085,0.4427,0.0419 2.250,0.8221,0.00852,0.00168,-0.1084,0.4345,0.0439 2.500,0.8497,0.00855,0.00169,-0.1083,0.4268,0.0461 2.750,0.8769,0.00861,0.00172,-0.1082,0.4187,0.0544 3.000,0.9009,0.00701,0.00205,-0.1080,0.4101,1.0000 3.250,0.9280,0.00714,0.00213,-0.1079,0.4004,1.0000 3.500,0.9547,0.00731,0.00222,-0.1077,0.3874,1.0000 3.750,0.9804,0.00757,0.00233,-0.1073,0.3604,1.0000 4.000,1.0053,0.00793,0.00249,-0.1069,0.3223,1.0000 4.250,1.0281,0.00852,0.00279,-0.1062,0.2681,1.0000 4.500,1.0513,0.00907,0.00311,-0.1055,0.2305,1.0000 4.750,1.0754,0.00951,0.00339,-0.1050,0.2047,1.0000 5.000,1.0997,0.00991,0.00365,-0.1045,0.1798,1.0000 5.250,1.1190,0.01088,0.00422,-0.1033,0.1130,1.0000 5.500,1.1379,0.01188,0.00490,-0.1020,0.0526,1.0000 5.750,1.1619,0.01228,0.00524,-0.1014,0.0399,1.0000 6.000,1.1841,0.01288,0.00571,-0.1006,0.0152,1.0000 6.250,1.2087,0.01321,0.00607,-0.1001,0.0140,1.0000 6.500,1.2327,0.01358,0.00651,-0.0995,0.0128,1.0000 6.750,1.2559,0.01404,0.00703,-0.0987,0.0115,1.0000 7.000,1.2783,0.01456,0.00761,-0.0979,0.0106,1.0000 7.250,1.3012,0.01500,0.00809,-0.0972,0.0101,1.0000 7.500,1.3232,0.01551,0.00866,-0.0963,0.0096,1.0000 7.750,1.3445,0.01608,0.00928,-0.0953,0.0092,1.0000 8.000,1.3649,0.01671,0.00996,-0.0942,0.0087,1.0000 8.250,1.3837,0.01744,0.01076,-0.0929,0.0082,1.0000 8.500,1.3987,0.01847,0.01187,-0.0910,0.0078,1.0000 8.750,1.4040,0.02019,0.01373,-0.0877,0.0073,1.0000 9.000,1.4243,0.02063,0.01420,-0.0867,0.0070,1.0000 9.250,1.4383,0.02148,0.01511,-0.0847,0.0069,1.0000 9.500,1.4475,0.02241,0.01612,-0.0820,0.0067,1.0000 9.750,1.4543,0.02349,0.01726,-0.0790,0.0066,1.0000 10.000,1.4601,0.02468,0.01852,-0.0761,0.0064,1.0000 10.250,1.4645,0.02605,0.01997,-0.0734,0.0063,1.0000 10.500,1.4687,0.02756,0.02157,-0.0710,0.0061,1.0000 10.750,1.4723,0.02926,0.02335,-0.0690,0.0059,1.0000 11.000,1.4754,0.03116,0.02532,-0.0672,0.0058,1.0000 11.250,1.4786,0.03317,0.02739,-0.0657,0.0056,1.0000 11.500,1.4810,0.03534,0.02963,-0.0644,0.0055,1.0000 11.750,1.4829,0.03764,0.03200,-0.0632,0.0054,1.0000 12.000,1.4843,0.04006,0.03448,-0.0621,0.0053,1.0000 12.250,1.4846,0.04262,0.03709,-0.0609,0.0051,1.0000 12.500,1.4855,0.04512,0.03965,-0.0595,0.0051,1.0000 12.750,1.4880,0.04744,0.04200,-0.0577,0.0050,1.0000 13.000,1.5049,0.04882,0.04332,-0.0539,0.0049,1.0000 13.250,1.4997,0.05192,0.04662,-0.0534,0.0047,1.0000 13.500,1.4978,0.05475,0.04959,-0.0533,0.0046,1.0000 13.750,1.4991,0.05743,0.05238,-0.0527,0.0046,1.0000 14.000,1.5025,0.06004,0.05510,-0.0514,0.0046,1.0000 14.250,1.5036,0.06293,0.05810,-0.0505,0.0046,1.0000 14.500,1.5332,0.06326,0.05835,-0.0479,0.0050,1.0000 14.750,1.5246,0.06677,0.06203,-0.0481,0.0051,1.0000 15.750,1.4575,0.08881,0.08510,-0.0520,0.0058,1.0000 16.000,1.4469,0.09384,0.09027,-0.0536,0.0058,1.0000