Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e479-il-50000-n5 Airfoil,e479-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,23.7823 Max Cl/Cd alpha,7.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-e479-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.7269,0.09398,0.08516,-0.0116,1.0000,0.1802 -12.250,-0.6971,0.09561,0.08674,-0.0095,1.0000,0.1828 -12.000,-0.7935,0.07570,0.06686,-0.0203,1.0000,0.1950 -11.750,-0.7412,0.08082,0.07194,-0.0160,1.0000,0.1971 -11.500,-0.7174,0.08142,0.07251,-0.0145,1.0000,0.2008 -11.250,-0.8421,0.06002,0.05107,-0.0259,1.0000,0.2128 -11.000,-0.8178,0.06025,0.05129,-0.0246,1.0000,0.2178 -10.750,-0.9099,0.04905,0.03986,-0.0269,1.0000,0.2235 -10.500,-0.9060,0.04754,0.03834,-0.0255,1.0000,0.2288 -10.250,-0.8989,0.04641,0.03717,-0.0238,1.0000,0.2348 -10.000,-0.9273,0.04270,0.03317,-0.0209,1.0000,0.2411 -9.750,-0.8974,0.04291,0.03350,-0.0202,1.0000,0.2469 -9.500,-0.8977,0.04107,0.03151,-0.0182,1.0000,0.2542 -9.250,-0.8850,0.04005,0.03044,-0.0168,1.0000,0.2608 -9.000,-0.8714,0.03911,0.02944,-0.0153,1.0000,0.2679 -8.750,-0.8640,0.03769,0.02787,-0.0136,1.0000,0.2755 -8.500,-0.8443,0.03720,0.02740,-0.0124,1.0000,0.2826 -8.250,-0.8370,0.03572,0.02574,-0.0106,1.0000,0.2908 -8.000,-0.8146,0.03540,0.02546,-0.0095,1.0000,0.2977 -7.750,-0.8061,0.03405,0.02392,-0.0077,1.0000,0.3067 -7.500,-0.7829,0.03377,0.02373,-0.0067,1.0000,0.3133 -7.250,-0.7734,0.03252,0.02227,-0.0049,1.0000,0.3227 -7.000,-0.7499,0.03231,0.02216,-0.0038,1.0000,0.3293 -6.750,-0.7377,0.03129,0.02099,-0.0020,1.0000,0.3385 -6.500,-0.7166,0.03094,0.02073,-0.0008,1.0000,0.3452 -6.250,-0.7025,0.03017,0.01987,0.0009,1.0000,0.3543 -6.000,-0.6840,0.02972,0.01947,0.0024,1.0000,0.3613 -5.750,-0.6687,0.02913,0.01885,0.0041,1.0000,0.3698 -5.500,-0.6532,0.02863,0.01837,0.0058,1.0000,0.3774 -5.250,-0.6389,0.02821,0.01796,0.0076,1.0000,0.3852 -5.000,-0.6277,0.02770,0.01743,0.0097,1.0000,0.3930 -4.750,-0.6004,0.02743,0.01719,0.0091,0.9911,0.4018 -4.500,-0.5551,0.02703,0.01674,0.0053,0.9692,0.4126 -4.250,-0.5124,0.02653,0.01611,0.0018,0.9466,0.4249 -4.000,-0.4664,0.02629,0.01596,-0.0014,0.9258,0.4344 -3.750,-0.4234,0.02586,0.01546,-0.0043,0.9044,0.4456 -3.500,-0.3837,0.02552,0.01507,-0.0063,0.8814,0.4567 -3.250,-0.3469,0.02524,0.01477,-0.0076,0.8577,0.4663 -3.000,-0.3139,0.02489,0.01430,-0.0084,0.8346,0.4779 -2.750,-0.2826,0.02473,0.01412,-0.0084,0.8116,0.4869 -2.500,-0.2556,0.02449,0.01379,-0.0080,0.7886,0.4974 -2.250,-0.2286,0.02434,0.01358,-0.0073,0.7671,0.5077 -2.000,-0.2024,0.02418,0.01336,-0.0065,0.7468,0.5176 -1.750,-0.1775,0.02402,0.01307,-0.0057,0.7275,0.5293 -1.500,-0.1515,0.02395,0.01300,-0.0048,0.7091,0.5391 -1.250,-0.1265,0.02383,0.01280,-0.0040,0.6912,0.5506 -1.000,-0.1014,0.02375,0.01268,-0.0032,0.6740,0.5625 -0.750,-0.0758,0.02371,0.01264,-0.0024,0.6576,0.5738 -0.500,-0.0506,0.02365,0.01255,-0.0016,0.6418,0.5865 -0.250,-0.0256,0.02362,0.01247,-0.0009,0.6269,0.6005 0.000,0.0000,0.02363,0.01250,0.0000,0.6131,0.6132 0.250,0.0255,0.02362,0.01247,0.0009,0.6004,0.6269 0.500,0.0506,0.02365,0.01255,0.0016,0.5865,0.6418 0.750,0.0758,0.02371,0.01264,0.0024,0.5738,0.6576 1.000,0.1014,0.02375,0.01268,0.0032,0.5625,0.6740 1.250,0.1265,0.02383,0.01280,0.0040,0.5506,0.6912 1.500,0.1515,0.02395,0.01300,0.0048,0.5391,0.7091 1.750,0.1776,0.02402,0.01307,0.0057,0.5294,0.7275 2.000,0.2024,0.02418,0.01336,0.0065,0.5176,0.7468 2.250,0.2286,0.02434,0.01358,0.0073,0.5076,0.7671 2.500,0.2556,0.02449,0.01379,0.0080,0.4975,0.7886 2.750,0.2826,0.02473,0.01412,0.0084,0.4869,0.8116 3.000,0.3139,0.02489,0.01430,0.0084,0.4779,0.8347 3.250,0.3469,0.02524,0.01477,0.0076,0.4663,0.8577 3.500,0.3837,0.02552,0.01507,0.0063,0.4567,0.8815 3.750,0.4234,0.02586,0.01546,0.0043,0.4456,0.9043 4.000,0.4664,0.02628,0.01595,0.0014,0.4343,0.9258 4.250,0.5124,0.02653,0.01611,-0.0018,0.4248,0.9467 4.500,0.5551,0.02702,0.01674,-0.0053,0.4126,0.9693 4.750,0.6004,0.02743,0.01719,-0.0091,0.4018,0.9912 5.000,0.6276,0.02770,0.01743,-0.0097,0.3930,1.0000 5.250,0.6388,0.02821,0.01796,-0.0076,0.3852,1.0000 5.500,0.6531,0.02864,0.01838,-0.0058,0.3774,1.0000 5.750,0.6687,0.02913,0.01884,-0.0041,0.3698,1.0000 6.000,0.6839,0.02972,0.01947,-0.0024,0.3614,1.0000 6.250,0.7025,0.03017,0.01987,-0.0009,0.3543,1.0000 6.500,0.7166,0.03094,0.02073,0.0008,0.3453,1.0000 6.750,0.7377,0.03129,0.02098,0.0020,0.3385,1.0000 7.000,0.7499,0.03230,0.02216,0.0038,0.3293,1.0000 7.250,0.7734,0.03252,0.02227,0.0049,0.3227,1.0000 7.500,0.7829,0.03377,0.02372,0.0067,0.3133,1.0000 7.750,0.8061,0.03406,0.02392,0.0077,0.3067,1.0000 8.000,0.8147,0.03540,0.02546,0.0095,0.2977,1.0000 8.250,0.8371,0.03572,0.02573,0.0106,0.2908,1.0000 8.500,0.8444,0.03719,0.02739,0.0124,0.2826,1.0000 8.750,0.8640,0.03769,0.02788,0.0136,0.2755,1.0000 9.000,0.8716,0.03911,0.02943,0.0153,0.2679,1.0000 9.250,0.8853,0.04004,0.03043,0.0167,0.2608,1.0000 9.500,0.8979,0.04107,0.03151,0.0182,0.2542,1.0000 9.750,0.8977,0.04291,0.03351,0.0201,0.2469,1.0000 10.000,0.9277,0.04269,0.03315,0.0208,0.2411,1.0000 10.250,0.8994,0.04640,0.03716,0.0237,0.2347,1.0000 10.500,0.9061,0.04759,0.03839,0.0254,0.2289,1.0000 10.750,0.9103,0.04906,0.03987,0.0269,0.2235,1.0000 11.000,0.8197,0.06011,0.05114,0.0245,0.2178,1.0000 11.250,0.8469,0.05952,0.05057,0.0261,0.2127,1.0000 11.500,0.7198,0.08116,0.07224,0.0145,0.2008,1.0000 11.750,0.7440,0.08051,0.07163,0.0161,0.1971,1.0000 12.000,0.7966,0.07535,0.06651,0.0204,0.1950,1.0000 12.250,0.6991,0.09545,0.08658,0.0094,0.1828,1.0000 12.500,0.7288,0.09386,0.08504,0.0115,0.1802,1.0000