Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe514-il-50000-n5 Airfoil,goe514-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.062 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe514-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.3053,0.11881,0.11263,-0.0462,0.9848,0.0629 -9.750,-0.3058,0.11375,0.10760,-0.0496,0.9792,0.0632 -9.500,-0.3119,0.10750,0.10138,-0.0544,0.9736,0.0638 -9.250,-0.2996,0.10561,0.09951,-0.0553,0.9675,0.0659 -9.000,-0.2936,0.10225,0.09615,-0.0579,0.9617,0.0682 -8.750,-0.3022,0.09764,0.09158,-0.0605,0.9540,0.0692 -8.500,-0.3159,0.09201,0.08599,-0.0647,0.9466,0.0699 -8.250,-0.3408,0.08762,0.08164,-0.0646,0.9361,0.0700 -8.000,-0.3615,0.08143,0.07541,-0.0663,0.9274,0.0707 -7.750,-0.3884,0.07390,0.06775,-0.0671,0.9172,0.0714 -7.500,-0.4288,0.06352,0.05692,-0.0666,0.9067,0.0727 -7.250,-0.4347,0.05797,0.05095,-0.0658,0.8995,0.0758 -7.000,-0.4211,0.05742,0.05040,-0.0642,0.8921,0.0793 -6.750,-0.4267,0.05209,0.04437,-0.0621,0.8844,0.0846 -6.500,-0.3991,0.05223,0.04463,-0.0623,0.8792,0.0906 -6.250,-0.4015,0.04892,0.04073,-0.0589,0.8700,0.0974 -6.000,-0.3663,0.05006,0.04209,-0.0599,0.8643,0.1051 -5.750,-0.3553,0.04906,0.04090,-0.0575,0.8536,0.1125 -5.500,-0.3245,0.04754,0.03903,-0.0583,0.8472,0.1238 -5.250,-0.3101,0.04709,0.03846,-0.0560,0.8352,0.1316 -5.000,-0.2882,0.04613,0.03729,-0.0550,0.8260,0.1402 -4.750,-0.2665,0.04431,0.03494,-0.0542,0.8177,0.1518 -4.500,-0.2464,0.04437,0.03510,-0.0527,0.8078,0.1578 -4.250,-0.2194,0.04280,0.03308,-0.0525,0.8010,0.1698 -4.000,-0.2019,0.04278,0.03309,-0.0506,0.7905,0.1761 -3.750,-0.1707,0.04160,0.03159,-0.0509,0.7843,0.1884 -3.500,-0.1543,0.04143,0.03136,-0.0488,0.7733,0.1957 -3.250,-0.1193,0.04058,0.03029,-0.0495,0.7674,0.2081 -3.000,-0.1033,0.04012,0.02955,-0.0475,0.7558,0.2189 -2.750,-0.0657,0.03946,0.02880,-0.0484,0.7505,0.2295 -2.500,-0.0501,0.03931,0.02851,-0.0463,0.7380,0.2381 -2.250,-0.0234,0.03881,0.02775,-0.0457,0.7291,0.2491 -2.000,0.0043,0.03840,0.02730,-0.0452,0.7202,0.2586 -1.750,0.0271,0.03813,0.02689,-0.0441,0.7099,0.2700 -1.500,0.0594,0.03747,0.02601,-0.0442,0.7023,0.2830 -1.250,0.0821,0.03718,0.02569,-0.0431,0.6910,0.2908 -1.000,0.1215,0.03625,0.02446,-0.0444,0.6841,0.2989 -0.750,0.1477,0.03595,0.02409,-0.0440,0.6721,0.3041 -0.500,0.1937,0.03499,0.02290,-0.0464,0.6655,0.3140 -0.250,0.2215,0.03486,0.02267,-0.0465,0.6526,0.3209 0.000,0.2746,0.03383,0.02142,-0.0501,0.6465,0.3310 0.250,0.2997,0.03381,0.02132,-0.0497,0.6326,0.3378 0.500,0.3318,0.03354,0.02095,-0.0503,0.6212,0.3471 0.750,0.3746,0.03284,0.02014,-0.0524,0.6126,0.3596 1.000,0.3973,0.03292,0.02014,-0.0516,0.5997,0.3703 1.250,0.4334,0.03246,0.01958,-0.0527,0.5904,0.3835 1.500,0.4606,0.03228,0.01938,-0.0525,0.5795,0.3950 1.750,0.4828,0.03230,0.01937,-0.0516,0.5685,0.4076 2.000,0.5168,0.03181,0.01882,-0.0523,0.5604,0.4253 2.250,0.5310,0.03206,0.01912,-0.0503,0.5496,0.4417 2.500,0.5648,0.03137,0.01849,-0.0510,0.5425,0.4728 3.000,0.7553,0.03157,0.01969,-0.0776,0.5191,1.0000 3.250,0.7775,0.03187,0.01981,-0.0766,0.5115,1.0000 3.500,0.7963,0.03230,0.02010,-0.0752,0.5044,1.0000 3.750,0.8104,0.03286,0.02056,-0.0731,0.4971,1.0000 4.000,0.8451,0.03291,0.02039,-0.0741,0.4915,1.0000 4.250,0.8455,0.03389,0.02138,-0.0700,0.4843,1.0000 4.500,0.8656,0.03436,0.02175,-0.0689,0.4786,1.0000 4.750,0.8994,0.03451,0.02172,-0.0699,0.4738,1.0000 5.000,0.8949,0.03570,0.02298,-0.0652,0.4672,1.0000 5.250,0.9124,0.03630,0.02351,-0.0638,0.4619,1.0000 5.500,0.9469,0.03644,0.02351,-0.0648,0.4576,1.0000 5.750,0.9409,0.03783,0.02497,-0.0602,0.4521,1.0000 6.000,0.9459,0.03895,0.02611,-0.0572,0.4471,1.0000 6.250,0.9685,0.03948,0.02659,-0.0566,0.4429,1.0000 6.500,1.0064,0.03957,0.02655,-0.0582,0.4394,1.0000 6.750,0.9726,0.04217,0.02935,-0.0504,0.4334,1.0000 7.000,0.9735,0.04366,0.03088,-0.0473,0.4285,1.0000 7.250,0.9974,0.04416,0.03135,-0.0469,0.4249,1.0000 7.500,1.0359,0.04414,0.03124,-0.0483,0.4221,1.0000 7.750,0.9505,0.05041,0.03782,-0.0370,0.4144,1.0000 8.000,0.9417,0.05305,0.04053,-0.0340,0.4093,1.0000 8.250,0.9686,0.05326,0.04071,-0.0338,0.4064,1.0000 8.500,1.0118,0.05249,0.03988,-0.0349,0.4044,1.0000 9.000,0.7687,0.08178,0.06972,-0.0244,0.3745,1.0000 9.250,0.7850,0.08279,0.07072,-0.0237,0.3715,1.0000 9.500,0.8085,0.08291,0.07084,-0.0229,0.3697,1.0000 10.000,0.7568,0.09582,0.08388,-0.0227,0.3547,1.0000 10.250,0.7784,0.09626,0.08433,-0.0219,0.3523,1.0000 10.750,0.7432,0.10700,0.09519,-0.0222,0.3394,1.0000 11.000,0.7605,0.10806,0.09627,-0.0217,0.3364,1.0000 11.250,0.7846,0.10823,0.09646,-0.0209,0.3343,1.0000 11.500,0.7446,0.11629,0.10459,-0.0220,0.3246,1.0000 11.750,0.7584,0.11770,0.10604,-0.0216,0.3207,1.0000