Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e475-il-50000-n5 Airfoil,e475-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,24.0981 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e475-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.6402,0.09754,0.08844,-0.0246,1.0000,0.1762 -11.750,-0.6276,0.09611,0.08697,-0.0239,1.0000,0.1795 -11.500,-0.7778,0.07009,0.06104,-0.0393,1.0000,0.1896 -11.250,-0.7188,0.07492,0.06583,-0.0347,1.0000,0.1917 -11.000,-0.7036,0.07417,0.06506,-0.0335,1.0000,0.1951 -10.750,-0.8195,0.05969,0.05051,-0.0373,1.0000,0.1996 -10.500,-0.8841,0.05437,0.04504,-0.0317,1.0000,0.2018 -10.250,-0.9326,0.05011,0.04043,-0.0255,1.0000,0.2049 -10.000,-0.9075,0.04986,0.04027,-0.0246,1.0000,0.2085 -9.750,-0.9016,0.04861,0.03896,-0.0221,1.0000,0.2123 -9.500,-0.9092,0.04653,0.03668,-0.0184,1.0000,0.2165 -9.250,-0.9270,0.04387,0.03362,-0.0135,1.0000,0.2210 -9.000,-0.9046,0.04339,0.03322,-0.0124,1.0000,0.2247 -8.750,-0.8933,0.04237,0.03213,-0.0102,1.0000,0.2291 -8.500,-0.8909,0.04076,0.03028,-0.0071,1.0000,0.2339 -8.250,-0.8860,0.03924,0.02853,-0.0042,1.0000,0.2386 -8.000,-0.8674,0.03856,0.02789,-0.0026,1.0000,0.2428 -7.750,-0.8554,0.03753,0.02672,-0.0004,1.0000,0.2477 -7.500,-0.8492,0.03609,0.02495,0.0025,1.0000,0.2533 -7.250,-0.8306,0.03533,0.02423,0.0040,1.0000,0.2574 -7.000,-0.8138,0.03455,0.02341,0.0057,1.0000,0.2623 -6.750,-0.8012,0.03351,0.02215,0.0079,1.0000,0.2683 -6.500,-0.7846,0.03265,0.02121,0.0096,1.0000,0.2731 -6.250,-0.7658,0.03196,0.02052,0.0111,1.0000,0.2780 -6.000,-0.7496,0.03115,0.01955,0.0129,1.0000,0.2840 -5.750,-0.7322,0.03039,0.01870,0.0145,1.0000,0.2897 -5.500,-0.7126,0.02979,0.01812,0.0159,1.0000,0.2950 -5.250,-0.6946,0.02910,0.01731,0.0174,1.0000,0.3013 -5.000,-0.6754,0.02847,0.01664,0.0188,1.0000,0.3073 -4.750,-0.6556,0.02795,0.01613,0.0201,1.0000,0.3134 -4.500,-0.6368,0.02737,0.01542,0.0215,1.0000,0.3207 -4.250,-0.6159,0.02688,0.01501,0.0227,1.0000,0.3266 -4.000,-0.5959,0.02642,0.01453,0.0239,1.0000,0.3339 -3.750,-0.5756,0.02597,0.01408,0.0251,1.0000,0.3414 -3.500,-0.5550,0.02559,0.01375,0.0262,1.0000,0.3492 -3.250,-0.5344,0.02523,0.01336,0.0273,1.0000,0.3576 -3.000,-0.5134,0.02491,0.01313,0.0283,1.0000,0.3660 -2.750,-0.4928,0.02463,0.01288,0.0293,1.0000,0.3756 -2.500,-0.4722,0.02438,0.01270,0.0303,1.0000,0.3859 -2.250,-0.4390,0.02420,0.01263,0.0288,0.9946,0.3984 -2.000,-0.3827,0.02405,0.01261,0.0230,0.9779,0.4172 -1.750,-0.3302,0.02377,0.01249,0.0181,0.9596,0.4386 -1.500,-0.2797,0.02337,0.01231,0.0139,0.9407,0.4629 -1.250,-0.2352,0.02289,0.01208,0.0110,0.9197,0.4915 -1.000,-0.1980,0.02234,0.01181,0.0098,0.8946,0.5236 -0.750,-0.1637,0.02177,0.01156,0.0093,0.8667,0.5632 -0.500,-0.1279,0.02117,0.01134,0.0089,0.8357,0.6132 -0.250,-0.0785,0.02067,0.01127,0.0067,0.8001,0.6782 0.000,0.0000,0.02049,0.01133,0.0000,0.7502,0.7502 0.250,0.0785,0.02067,0.01126,-0.0067,0.6781,0.8000 0.500,0.1279,0.02117,0.01134,-0.0090,0.6130,0.8356 0.750,0.1637,0.02177,0.01155,-0.0093,0.5630,0.8667 1.000,0.1981,0.02234,0.01181,-0.0098,0.5235,0.8947 1.250,0.2352,0.02289,0.01208,-0.0110,0.4915,0.9197 1.500,0.2795,0.02337,0.01231,-0.0138,0.4630,0.9406 1.750,0.3301,0.02376,0.01249,-0.0181,0.4387,0.9596 2.000,0.3827,0.02405,0.01261,-0.0230,0.4172,0.9780 2.250,0.4390,0.02420,0.01263,-0.0288,0.3985,0.9946 2.500,0.4721,0.02438,0.01270,-0.0303,0.3859,1.0000 2.750,0.4927,0.02463,0.01287,-0.0293,0.3757,1.0000 3.000,0.5133,0.02491,0.01313,-0.0283,0.3660,1.0000 3.250,0.5343,0.02523,0.01336,-0.0273,0.3576,1.0000 3.500,0.5549,0.02559,0.01375,-0.0262,0.3491,1.0000 3.750,0.5755,0.02597,0.01407,-0.0251,0.3414,1.0000 4.000,0.5958,0.02642,0.01453,-0.0239,0.3340,1.0000 4.250,0.6158,0.02688,0.01500,-0.0226,0.3266,1.0000 4.500,0.6367,0.02737,0.01542,-0.0215,0.3207,1.0000 4.750,0.6555,0.02794,0.01613,-0.0201,0.3134,1.0000 5.000,0.6753,0.02847,0.01663,-0.0188,0.3072,1.0000 5.250,0.6946,0.02909,0.01731,-0.0174,0.3014,1.0000 5.500,0.7125,0.02979,0.01812,-0.0158,0.2951,1.0000 5.750,0.7321,0.03038,0.01869,-0.0145,0.2897,1.0000 6.000,0.7496,0.03115,0.01956,-0.0129,0.2841,1.0000 6.250,0.7657,0.03196,0.02052,-0.0111,0.2780,1.0000 6.500,0.7845,0.03265,0.02121,-0.0096,0.2731,1.0000 6.750,0.8011,0.03351,0.02214,-0.0079,0.2682,1.0000 7.000,0.8137,0.03455,0.02341,-0.0057,0.2624,1.0000 7.250,0.8305,0.03532,0.02422,-0.0039,0.2574,1.0000 7.500,0.8492,0.03609,0.02495,-0.0025,0.2533,1.0000 7.750,0.8554,0.03752,0.02671,0.0004,0.2478,1.0000 8.000,0.8674,0.03856,0.02790,0.0026,0.2428,1.0000 8.250,0.8858,0.03925,0.02854,0.0042,0.2386,1.0000 8.500,0.8909,0.04075,0.03027,0.0071,0.2339,1.0000 8.750,0.8934,0.04236,0.03212,0.0102,0.2291,1.0000 9.000,0.9046,0.04338,0.03322,0.0124,0.2248,1.0000 9.500,0.9092,0.04652,0.03667,0.0184,0.2165,1.0000 9.750,0.9017,0.04860,0.03895,0.0221,0.2123,1.0000 10.000,0.9082,0.04981,0.04022,0.0245,0.2084,1.0000 10.250,0.9325,0.05011,0.04043,0.0255,0.2048,1.0000 10.500,0.8846,0.05435,0.04501,0.0317,0.2018,1.0000 10.750,0.8202,0.05968,0.05050,0.0372,0.1995,1.0000 11.000,0.7081,0.07358,0.06447,0.0338,0.1951,1.0000 11.250,0.7212,0.07465,0.06556,0.0348,0.1918,1.0000 11.500,0.7877,0.06904,0.05998,0.0397,0.1895,1.0000 11.750,0.6283,0.09614,0.08701,0.0238,0.1796,1.0000 12.000,0.6421,0.09736,0.08826,0.0246,0.1762,1.0000