Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e479-il-50000 Airfoil,e479-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,15.9336 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-e479-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4152,0.11252,0.10364,0.0180,1.0000,0.4580 -9.500,-0.3962,0.10855,0.09964,0.0174,1.0000,0.4655 -9.250,-0.4143,0.10805,0.09917,0.0183,1.0000,0.4770 -9.000,-0.3756,0.10317,0.09424,0.0172,1.0000,0.4883 -8.750,-0.3726,0.10067,0.09175,0.0174,1.0000,0.4985 -8.500,-0.3781,0.09943,0.09053,0.0182,1.0000,0.5116 -8.250,-0.3459,0.09513,0.08618,0.0171,1.0000,0.5211 -8.000,-0.3439,0.09296,0.08403,0.0176,1.0000,0.5332 -7.750,-0.4399,0.08183,0.07292,0.0090,1.0000,0.4264 -7.500,-0.4434,0.07755,0.06863,0.0078,1.0000,0.4224 -7.250,-0.4579,0.07320,0.06432,0.0070,1.0000,0.4231 -7.000,-0.4295,0.07187,0.06297,0.0078,1.0000,0.4334 -6.750,-0.4412,0.06798,0.05911,0.0075,1.0000,0.4357 -6.500,-0.4706,0.06321,0.05443,0.0076,1.0000,0.4388 -6.250,-0.5530,0.05466,0.04601,0.0083,1.0000,0.4418 -6.000,-0.4850,0.05711,0.04844,0.0099,1.0000,0.4523 -5.750,-0.5587,0.04932,0.04071,0.0114,1.0000,0.4586 -5.500,-0.5159,0.05018,0.04163,0.0130,1.0000,0.4676 -5.250,-0.5646,0.04478,0.03623,0.0157,1.0000,0.4763 -5.000,-0.5359,0.04496,0.03650,0.0176,1.0000,0.4842 -4.750,-0.5667,0.04164,0.03315,0.0212,1.0000,0.4933 -4.500,-0.5597,0.04115,0.03276,0.0243,1.0000,0.5004 -4.250,-0.5741,0.03948,0.03105,0.0277,1.0000,0.5087 -4.000,-0.5797,0.03830,0.02987,0.0305,1.0000,0.5163 -3.750,-0.5808,0.03748,0.02905,0.0329,1.0000,0.5250 -3.500,-0.5811,0.03648,0.02801,0.0348,1.0000,0.5337 -3.250,-0.5551,0.03556,0.02695,0.0318,0.9906,0.5471 -3.000,-0.4874,0.03568,0.02710,0.0242,0.9678,0.5627 -2.750,-0.4278,0.03554,0.02697,0.0182,0.9446,0.5769 -2.500,-0.3668,0.03522,0.02663,0.0120,0.9232,0.5923 -2.250,-0.3012,0.03475,0.02614,0.0054,0.9035,0.6082 -2.000,-0.2457,0.03422,0.02558,0.0006,0.8836,0.6237 -1.750,-0.2088,0.03360,0.02491,-0.0014,0.8620,0.6382 -1.500,-0.1691,0.03327,0.02455,-0.0030,0.8418,0.6525 -1.250,-0.1292,0.03312,0.02442,-0.0039,0.8223,0.6651 -1.000,-0.0991,0.03282,0.02410,-0.0038,0.8035,0.6787 -0.750,-0.0752,0.03253,0.02377,-0.0031,0.7857,0.6931 -0.500,-0.0539,0.03230,0.02350,-0.0020,0.7686,0.7081 -0.250,-0.0251,0.03237,0.02360,-0.0011,0.7518,0.7215 0.000,0.0000,0.03239,0.02362,0.0000,0.7361,0.7362 0.250,0.0251,0.03237,0.02360,0.0011,0.7216,0.7517 0.500,0.0539,0.03230,0.02350,0.0020,0.7081,0.7686 0.750,0.0752,0.03253,0.02377,0.0031,0.6931,0.7856 1.000,0.0991,0.03282,0.02410,0.0038,0.6786,0.8035 1.250,0.1293,0.03312,0.02442,0.0039,0.6650,0.8224 1.500,0.1692,0.03327,0.02455,0.0030,0.6526,0.8418 1.750,0.2087,0.03361,0.02491,0.0014,0.6383,0.8620 2.000,0.2456,0.03422,0.02557,-0.0006,0.6237,0.8837 2.250,0.3010,0.03475,0.02614,-0.0054,0.6083,0.9035 2.500,0.3668,0.03522,0.02663,-0.0120,0.5923,0.9232 2.750,0.4278,0.03553,0.02696,-0.0182,0.5768,0.9446 3.000,0.4875,0.03568,0.02709,-0.0242,0.5626,0.9679 3.250,0.5551,0.03554,0.02693,-0.0318,0.5471,0.9906 3.500,0.5811,0.03647,0.02800,-0.0348,0.5337,1.0000 3.750,0.5807,0.03747,0.02904,-0.0329,0.5251,1.0000 4.000,0.5794,0.03831,0.02988,-0.0305,0.5163,1.0000 4.250,0.5741,0.03947,0.03104,-0.0276,0.5087,1.0000 4.500,0.5592,0.04118,0.03278,-0.0243,0.5005,1.0000 4.750,0.5666,0.04164,0.03315,-0.0212,0.4933,1.0000 5.000,0.5358,0.04497,0.03651,-0.0176,0.4842,1.0000 5.250,0.5648,0.04476,0.03620,-0.0157,0.4763,1.0000 5.500,0.5157,0.05020,0.04164,-0.0130,0.4676,1.0000 5.750,0.5591,0.04930,0.04069,-0.0114,0.4586,1.0000 6.000,0.4856,0.05707,0.04840,-0.0100,0.4522,1.0000 6.250,0.5539,0.05460,0.04594,-0.0083,0.4418,1.0000 6.500,0.4711,0.06319,0.05441,-0.0077,0.4388,1.0000 6.750,0.4418,0.06795,0.05909,-0.0076,0.4357,1.0000 7.000,0.4300,0.07187,0.06297,-0.0079,0.4334,1.0000 7.250,0.4582,0.07320,0.06431,-0.0071,0.4230,1.0000 7.500,0.4441,0.07753,0.06861,-0.0078,0.4224,1.0000 7.750,0.4414,0.08178,0.07286,-0.0091,0.4263,1.0000 8.000,0.4534,0.08534,0.07645,-0.0097,0.4250,1.0000 8.250,0.3468,0.09512,0.08617,-0.0172,0.5210,1.0000 8.500,0.3780,0.09937,0.09045,-0.0183,0.5115,1.0000 8.750,0.3731,0.10064,0.09171,-0.0175,0.4987,1.0000 9.000,0.3765,0.10317,0.09424,-0.0174,0.4883,1.0000 9.250,0.4150,0.10802,0.09914,-0.0184,0.4770,1.0000 9.500,0.3971,0.10855,0.09964,-0.0176,0.4655,1.0000 9.750,0.4164,0.11254,0.10365,-0.0182,0.4580,1.0000