Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe741-il-50000-n5 Airfoil,goe741-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,14.0642 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe741-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.2664,0.12320,0.11618,-0.0133,0.7312,0.1402 -10.000,-0.2742,0.12109,0.11407,-0.0160,0.7266,0.1414 -9.750,-0.2760,0.11825,0.11125,-0.0189,0.7208,0.1418 -9.250,-0.2713,0.10381,0.09667,-0.0264,0.7117,0.0902 -9.000,-0.2571,0.10101,0.09381,-0.0258,0.7066,0.0887 -8.750,-0.2493,0.09757,0.09040,-0.0276,0.7005,0.0870 -8.500,-0.2476,0.09380,0.08665,-0.0298,0.6952,0.0852 -8.000,-0.2815,0.08281,0.07560,-0.0391,0.6882,0.0806 -7.750,-0.2844,0.07942,0.07220,-0.0405,0.6832,0.0804 -7.500,-0.2881,0.07555,0.06826,-0.0422,0.6782,0.0804 -7.250,-0.2904,0.07179,0.06439,-0.0432,0.6738,0.0804 -7.000,-0.2923,0.06799,0.06042,-0.0435,0.6702,0.0804 -6.750,-0.2910,0.06437,0.05660,-0.0437,0.6664,0.0804 -6.500,-0.2862,0.06087,0.05291,-0.0441,0.6611,0.0803 -6.250,-0.2810,0.05750,0.04927,-0.0437,0.6564,0.0802 -6.000,-0.2754,0.05418,0.04558,-0.0426,0.6525,0.0804 -5.750,-0.2682,0.05100,0.04195,-0.0411,0.6492,0.0806 -5.500,-0.2505,0.04947,0.04035,-0.0409,0.6436,0.0817 -5.250,-0.2329,0.04813,0.03888,-0.0404,0.6385,0.0833 -5.000,-0.2169,0.04642,0.03690,-0.0392,0.6344,0.0854 -4.750,-0.2013,0.04436,0.03441,-0.0377,0.6311,0.0875 -4.500,-0.1838,0.04237,0.03193,-0.0367,0.6266,0.0893 -4.250,-0.1634,0.04091,0.03016,-0.0362,0.6211,0.0910 -4.000,-0.1415,0.04002,0.02918,-0.0356,0.6167,0.0933 -3.750,-0.1190,0.03906,0.02800,-0.0347,0.6132,0.0969 -3.500,-0.0950,0.03778,0.02626,-0.0336,0.6104,0.1017 -3.250,-0.0718,0.03755,0.02613,-0.0340,0.6041,0.1055 -3.000,-0.0466,0.03693,0.02532,-0.0339,0.5992,0.1111 -2.750,-0.0206,0.03632,0.02462,-0.0335,0.5955,0.1178 -2.500,0.0078,0.03565,0.02372,-0.0331,0.5925,0.1274 -2.250,0.0334,0.03572,0.02392,-0.0336,0.5876,0.1366 -2.000,0.0599,0.03586,0.02409,-0.0342,0.5819,0.1489 -1.750,0.0885,0.03577,0.02395,-0.0344,0.5778,0.1647 -1.500,0.1177,0.03558,0.02367,-0.0344,0.5746,0.1845 -1.250,0.1477,0.03529,0.02330,-0.0343,0.5720,0.2073 -1.000,0.1672,0.03627,0.02441,-0.0352,0.5647,0.2270 -0.750,0.1910,0.03637,0.02460,-0.0351,0.5600,0.2517 -0.500,0.2167,0.03617,0.02443,-0.0346,0.5566,0.2818 -0.250,0.2422,0.03577,0.02414,-0.0338,0.5539,0.3154 0.000,0.2547,0.03679,0.02537,-0.0335,0.5473,0.3476 0.250,0.2684,0.03709,0.02605,-0.0325,0.5416,0.4033 0.750,0.4831,0.03576,0.02555,-0.0575,0.5349,1.0000 1.000,0.4936,0.03751,0.02726,-0.0571,0.5280,1.0000 1.250,0.5061,0.03878,0.02843,-0.0561,0.5218,1.0000 1.500,0.5257,0.03917,0.02866,-0.0546,0.5181,1.0000 1.750,0.5482,0.03928,0.02860,-0.0531,0.5154,1.0000 2.000,0.5428,0.04216,0.03153,-0.0520,0.5058,1.0000 2.250,0.5567,0.04300,0.03227,-0.0504,0.5006,1.0000 2.500,0.5788,0.04312,0.03224,-0.0489,0.4975,1.0000 2.750,0.6042,0.04296,0.03192,-0.0474,0.4952,1.0000 3.000,0.5771,0.04720,0.03626,-0.0452,0.4820,1.0000 3.250,0.5993,0.04726,0.03621,-0.0436,0.4788,1.0000 3.500,0.6264,0.04694,0.03575,-0.0421,0.4767,1.0000 4.000,0.6126,0.05170,0.04048,-0.0380,0.4598,1.0000 4.250,0.6399,0.05140,0.04006,-0.0365,0.4577,1.0000 4.750,0.6162,0.05614,0.04474,-0.0312,0.4412,1.0000 5.250,0.6011,0.06059,0.04911,-0.0268,0.4256,1.0000 5.500,0.6277,0.06050,0.04895,-0.0256,0.4232,1.0000 6.000,0.6162,0.06540,0.05379,-0.0225,0.4081,1.0000 6.250,0.6384,0.06572,0.05405,-0.0213,0.4055,1.0000 6.500,0.6133,0.07001,0.05835,-0.0202,0.3943,1.0000 6.750,0.6339,0.07046,0.05875,-0.0190,0.3911,1.0000 7.250,0.6278,0.07591,0.06418,-0.0174,0.3779,1.0000 7.500,0.6460,0.07673,0.06497,-0.0165,0.3750,1.0000 8.000,0.6412,0.08241,0.07066,-0.0155,0.3625,1.0000 8.250,0.6588,0.08331,0.07153,-0.0146,0.3594,1.0000 8.500,0.6808,0.08381,0.07201,-0.0137,0.3572,1.0000 8.750,0.6521,0.08979,0.07805,-0.0143,0.3488,1.0000 9.000,0.6636,0.09147,0.07972,-0.0138,0.3451,1.0000 9.250,0.6828,0.09232,0.08056,-0.0130,0.3426,1.0000 9.500,0.6700,0.09664,0.08492,-0.0134,0.3361,1.0000 9.750,0.6722,0.09950,0.08780,-0.0134,0.3318,1.0000 10.000,0.6853,0.10113,0.08945,-0.0129,0.3287,1.0000 10.250,0.7053,0.10196,0.09028,-0.0122,0.3263,1.0000 10.500,0.6876,0.10700,0.09537,-0.0131,0.3195,1.0000 10.750,0.6941,0.10934,0.09774,-0.0130,0.3152,1.0000 11.000,0.7107,0.11057,0.09898,-0.0125,0.3121,1.0000 11.250,0.7151,0.11312,0.10157,-0.0125,0.3076,1.0000 11.500,0.7097,0.11671,0.10521,-0.0131,0.3011,1.0000