Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe599-il-100000 Airfoil,goe599-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,48.5119 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe599-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5330,0.09315,0.08813,-0.0244,1.0000,0.1428 -8.750,-0.5368,0.08953,0.08456,-0.0258,1.0000,0.1484 -8.500,-0.5948,0.08374,0.07894,-0.0363,1.0000,0.1518 -8.250,-0.5549,0.08149,0.07668,-0.0283,1.0000,0.1565 -8.000,-0.6100,0.07640,0.07157,-0.0372,1.0000,0.1660 -7.750,-0.6448,0.05400,0.04817,-0.0437,1.0000,0.0805 -7.500,-0.6262,0.05451,0.04909,-0.0421,1.0000,0.0994 -7.250,-0.6428,0.04317,0.03602,-0.0399,1.0000,0.0694 -7.000,-0.6300,0.03888,0.03149,-0.0386,1.0000,0.0682 -6.750,-0.6159,0.03531,0.02753,-0.0370,1.0000,0.0676 -6.500,-0.5993,0.03229,0.02403,-0.0354,1.0000,0.0678 -6.250,-0.5811,0.02977,0.02103,-0.0339,1.0000,0.0701 -6.000,-0.5610,0.02779,0.01897,-0.0329,1.0000,0.0735 -5.750,-0.5391,0.02597,0.01689,-0.0317,1.0000,0.0762 -5.500,-0.5165,0.02460,0.01517,-0.0304,1.0000,0.0809 -5.250,-0.4944,0.02305,0.01366,-0.0296,1.0000,0.0870 -5.000,-0.4710,0.02193,0.01235,-0.0285,1.0000,0.0937 -4.750,-0.4486,0.02067,0.01116,-0.0277,1.0000,0.1043 -4.500,-0.4258,0.01939,0.00995,-0.0268,1.0000,0.1171 -4.250,-0.4036,0.01805,0.00882,-0.0260,1.0000,0.1435 -4.000,-0.3806,0.01636,0.00791,-0.0256,1.0000,0.2514 -3.750,-0.3582,0.01545,0.00762,-0.0251,1.0000,0.3771 -3.500,-0.3359,0.01501,0.00750,-0.0243,1.0000,0.4659 -3.250,-0.3144,0.01476,0.00755,-0.0230,1.0000,0.5518 -3.000,-0.2938,0.01456,0.00762,-0.0214,1.0000,0.6298 -2.750,-0.2743,0.01441,0.00766,-0.0193,1.0000,0.6978 -2.500,-0.2555,0.01431,0.00772,-0.0169,1.0000,0.7580 -2.250,-0.2384,0.01427,0.00781,-0.0140,1.0000,0.8205 -2.000,-0.2195,0.01430,0.00794,-0.0113,1.0000,0.8927 -1.750,-0.1692,0.01445,0.00797,-0.0158,1.0000,0.9812 -1.500,-0.1450,0.01445,0.00777,-0.0168,1.0000,1.0000 -1.250,-0.1258,0.01458,0.00771,-0.0165,1.0000,1.0000 -1.000,-0.1052,0.01478,0.00776,-0.0162,1.0000,1.0000 -0.750,-0.0840,0.01503,0.00786,-0.0160,1.0000,1.0000 -0.500,-0.0625,0.01532,0.00804,-0.0158,1.0000,1.0000 -0.250,-0.0410,0.01566,0.00827,-0.0157,1.0000,1.0000 0.000,0.0024,0.01612,0.00863,-0.0197,0.9941,1.0000 0.250,0.0537,0.01655,0.00898,-0.0251,0.9842,1.0000 0.500,0.1008,0.01687,0.00925,-0.0296,0.9734,1.0000 0.750,0.1452,0.01714,0.00950,-0.0335,0.9626,1.0000 1.000,0.1906,0.01738,0.00974,-0.0374,0.9528,1.0000 1.250,0.2368,0.01755,0.00993,-0.0414,0.9431,1.0000 1.500,0.2760,0.01766,0.01007,-0.0439,0.9311,1.0000 1.750,0.3163,0.01772,0.01020,-0.0465,0.9194,1.0000 2.000,0.3602,0.01765,0.01022,-0.0496,0.9075,1.0000 2.250,0.4124,0.01716,0.00984,-0.0535,0.8925,1.0000 2.500,0.4637,0.01633,0.00915,-0.0565,0.8754,1.0000 2.750,0.5102,0.01549,0.00843,-0.0584,0.8577,1.0000 3.000,0.5450,0.01492,0.00794,-0.0581,0.8347,1.0000 3.250,0.5786,0.01437,0.00747,-0.0575,0.8073,1.0000 3.500,0.6063,0.01411,0.00724,-0.0561,0.7767,1.0000 3.750,0.6314,0.01392,0.00704,-0.0542,0.7387,1.0000 4.000,0.6540,0.01387,0.00700,-0.0521,0.6945,1.0000 4.250,0.6748,0.01391,0.00692,-0.0495,0.6309,1.0000 4.500,0.6897,0.01445,0.00682,-0.0457,0.4972,1.0000 4.750,0.6889,0.01690,0.00744,-0.0405,0.2034,1.0000 5.000,0.7028,0.01859,0.00859,-0.0383,0.1563,1.0000 5.250,0.7216,0.01969,0.00963,-0.0366,0.1423,1.0000 5.500,0.7422,0.02071,0.01065,-0.0352,0.1334,1.0000 5.750,0.7633,0.02195,0.01174,-0.0341,0.1251,1.0000 6.000,0.7880,0.02294,0.01281,-0.0333,0.1187,1.0000 6.250,0.8141,0.02439,0.01414,-0.0330,0.1129,1.0000 6.500,0.8401,0.02564,0.01554,-0.0324,0.1063,1.0000 6.750,0.8665,0.02727,0.01710,-0.0323,0.0994,1.0000 7.000,0.8918,0.02888,0.01899,-0.0315,0.0929,1.0000 7.250,0.9175,0.03133,0.02136,-0.0316,0.0855,1.0000 7.500,0.9391,0.03324,0.02381,-0.0299,0.0811,1.0000 7.750,0.9610,0.03527,0.02598,-0.0290,0.0751,1.0000 8.000,0.9803,0.03955,0.03048,-0.0281,0.0721,1.0000 8.250,0.9946,0.04237,0.03391,-0.0256,0.0709,1.0000 8.500,1.0049,0.04544,0.03759,-0.0228,0.0690,1.0000 8.750,1.0125,0.04915,0.04180,-0.0202,0.0682,1.0000 9.000,1.0183,0.05375,0.04681,-0.0178,0.0697,1.0000 9.250,1.0065,0.06041,0.05432,-0.0134,0.0805,1.0000