Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe559-il-500000-n5 Airfoil,goe559-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,64.1855 Max Cl/Cd alpha,1.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe559-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.3342,0.10583,0.10372,-0.0340,1.0000,0.0015 -9.250,-0.3299,0.10259,0.10050,-0.0351,1.0000,0.0017 -9.000,-0.3272,0.09933,0.09727,-0.0360,0.9947,0.0017 -8.750,-0.3101,0.09447,0.09240,-0.0417,0.9681,0.0017 -8.500,-0.2687,0.08710,0.08494,-0.0556,0.9333,0.0017 -8.250,-0.2301,0.08043,0.07806,-0.0690,0.8800,0.0017 -8.000,-0.2277,0.07727,0.07455,-0.0707,0.7892,0.0017 -7.750,-0.2289,0.07473,0.07179,-0.0709,0.7418,0.0017 -7.500,-0.2334,0.07126,0.06825,-0.0732,0.7190,0.0017 -7.250,-0.2364,0.06801,0.06493,-0.0752,0.7041,0.0017 -7.000,-0.2339,0.06457,0.06140,-0.0769,0.6904,0.0017 -6.750,-0.2290,0.06090,0.05762,-0.0786,0.6788,0.0017 -6.500,-0.2230,0.05774,0.05434,-0.0793,0.6668,0.0017 -6.250,-0.2128,0.05425,0.05068,-0.0799,0.6554,0.0018 -6.000,-0.2027,0.05121,0.04749,-0.0799,0.6432,0.0018 -5.750,-0.1907,0.04817,0.04426,-0.0796,0.6302,0.0018 -5.500,-0.1767,0.04514,0.04102,-0.0789,0.6170,0.0018 -5.250,-0.1622,0.04233,0.03799,-0.0782,0.6027,0.0018 -5.000,-0.1531,0.03846,0.03393,-0.0776,0.5900,0.0019 -4.750,-0.1393,0.03550,0.03074,-0.0768,0.5775,0.0020 -4.500,-0.1221,0.03289,0.02788,-0.0758,0.5664,0.0021 -4.250,-0.1028,0.03044,0.02515,-0.0745,0.5567,0.0024 -4.000,-0.0819,0.02826,0.02270,-0.0732,0.5480,0.0025 -3.750,-0.0502,0.02824,0.02231,-0.0711,0.5399,0.0037 -3.500,-0.0353,0.02437,0.01823,-0.0702,0.5333,0.0040 -3.000,0.0104,0.02081,0.01412,-0.0680,0.5207,0.0049 -2.750,0.0356,0.01949,0.01255,-0.0669,0.5146,0.0055 -2.500,0.0637,0.01921,0.01201,-0.0659,0.5088,0.0064 -2.250,0.0896,0.01863,0.01112,-0.0650,0.5032,0.0066 -1.750,0.1390,0.01461,0.00684,-0.0639,0.4939,0.0087 -1.500,0.1655,0.01378,0.00588,-0.0634,0.4893,0.0106 -1.250,0.1928,0.01399,0.00585,-0.0629,0.4850,0.0128 -1.000,0.2160,0.01217,0.00411,-0.0619,0.4816,0.0087 -0.750,0.2416,0.01171,0.00346,-0.0611,0.4777,0.0037 -0.500,0.2646,0.01104,0.00273,-0.0602,0.4739,0.0032 -0.250,0.2889,0.01062,0.00220,-0.0595,0.4703,0.0029 0.000,0.3145,0.01036,0.00181,-0.0592,0.4668,0.0029 0.250,0.3408,0.01023,0.00154,-0.0590,0.4630,0.0033 0.500,0.3782,0.00765,0.00166,-0.0618,0.4593,0.9593 0.750,0.4133,0.00775,0.00165,-0.0638,0.4560,0.9672 1.000,0.4468,0.00782,0.00169,-0.0654,0.4530,0.9736 1.250,0.4784,0.00790,0.00175,-0.0666,0.4499,0.9801 1.500,0.5122,0.00798,0.00185,-0.0683,0.4467,0.9845 1.750,0.5254,0.01048,0.00271,-0.0671,0.0061,0.9928 2.000,0.5586,0.01070,0.00303,-0.0686,0.0030,0.9967 2.250,0.5920,0.01108,0.00357,-0.0702,0.0029,0.9999 2.500,0.6108,0.01159,0.00420,-0.0686,0.0031,1.0000 2.750,0.6290,0.01213,0.00492,-0.0667,0.0038,1.0000 3.000,0.6450,0.01282,0.00573,-0.0644,0.0049,1.0000 3.250,0.6603,0.01353,0.00655,-0.0619,0.0089,1.0000 3.500,0.6750,0.01425,0.00735,-0.0592,0.0129,1.0000 3.750,0.6758,0.01587,0.00896,-0.0545,0.0114,1.0000 4.000,0.6929,0.01646,0.00966,-0.0523,0.0098,1.0000 4.250,0.7096,0.01713,0.01038,-0.0501,0.0081,1.0000 4.500,0.7232,0.01841,0.01163,-0.0475,0.0069,1.0000 5.000,0.7735,0.02273,0.01581,-0.0466,0.0033,1.0000 5.250,0.7967,0.02300,0.01627,-0.0447,0.0030,1.0000 5.500,0.8262,0.02433,0.01770,-0.0441,0.0025,1.0000 5.750,0.8549,0.02625,0.01970,-0.0436,0.0021,1.0000 6.000,0.8805,0.02830,0.02186,-0.0429,0.0019,1.0000 6.250,0.9021,0.03145,0.02512,-0.0421,0.0017,1.0000 6.500,0.9220,0.03522,0.02901,-0.0410,0.0016,1.0000 6.750,0.9409,0.03747,0.03145,-0.0390,0.0016,1.0000 7.000,0.9586,0.03967,0.03387,-0.0368,0.0016,1.0000 7.250,0.9762,0.04133,0.03577,-0.0342,0.0015,1.0000 7.500,0.9936,0.04313,0.03780,-0.0317,0.0015,1.0000 7.750,1.0098,0.04516,0.04003,-0.0292,0.0014,1.0000 8.000,1.0235,0.04758,0.04265,-0.0266,0.0013,1.0000 8.250,1.0332,0.05016,0.04544,-0.0240,0.0012,1.0000 8.500,1.0395,0.05297,0.04846,-0.0212,0.0012,1.0000 8.750,1.0432,0.05588,0.05156,-0.0182,0.0011,1.0000 9.000,1.0447,0.05873,0.05460,-0.0153,0.0011,1.0000 9.250,1.0434,0.06152,0.05757,-0.0124,0.0011,1.0000 9.500,1.0383,0.06434,0.06057,-0.0092,0.0010,1.0000 9.750,1.0303,0.06690,0.06328,-0.0061,0.0010,1.0000 10.000,1.0160,0.06933,0.06584,-0.0022,0.0010,1.0000 10.250,1.0006,0.07191,0.06855,0.0008,0.0010,1.0000 10.500,0.9846,0.07474,0.07150,0.0028,0.0010,1.0000 10.750,0.9674,0.07796,0.07484,0.0038,0.0010,1.0000 11.000,0.9483,0.08172,0.07872,0.0040,0.0010,1.0000 11.250,0.9301,0.08578,0.08289,0.0034,0.0010,1.0000 11.500,0.9135,0.09004,0.08725,0.0020,0.0010,1.0000 11.750,0.8942,0.09514,0.09245,0.0000,0.0010,1.0000 12.000,0.8768,0.10048,0.09788,-0.0026,0.0011,1.0000