Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e473-il-50000 Airfoil,e473-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,15.7903 Max Cl/Cd alpha,2.5 Url,http://airfoiltools.com/polar/csv?polar=xf-e473-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.4221,0.11729,0.10818,0.0153,1.0000,0.4395 -9.750,-0.4024,0.11319,0.10406,0.0149,1.0000,0.4464 -9.500,-0.4208,0.11302,0.10394,0.0161,1.0000,0.4592 -9.250,-0.3810,0.10797,0.09882,0.0153,1.0000,0.4691 -9.000,-0.3834,0.10595,0.09683,0.0159,1.0000,0.4797 -8.750,-0.3761,0.10401,0.09489,0.0165,1.0000,0.4928 -8.500,-0.3540,0.10035,0.09122,0.0162,1.0000,0.5023 -8.250,-0.3546,0.09852,0.08942,0.0171,1.0000,0.5154 -8.000,-0.3609,0.09776,0.08869,0.0188,1.0000,0.5303 -7.750,-0.3233,0.09311,0.08402,0.0174,1.0000,0.5388 -7.500,-0.3190,0.09111,0.08204,0.0183,1.0000,0.5524 -7.250,-0.3182,0.08960,0.08057,0.0198,1.0000,0.5680 -7.000,-0.3102,0.08795,0.07894,0.0209,1.0000,0.5839 -6.750,-0.2772,0.08398,0.07497,0.0195,1.0000,0.5929 -6.500,-0.2680,0.08191,0.07294,0.0204,1.0000,0.6077 -6.250,-0.4693,0.06871,0.05987,0.0134,1.0000,0.4410 -6.000,-0.4673,0.06533,0.05652,0.0139,1.0000,0.4394 -5.750,-0.4786,0.06149,0.05273,0.0149,1.0000,0.4365 -5.500,-0.5071,0.05664,0.04792,0.0160,1.0000,0.4336 -5.250,-0.5333,0.05211,0.04338,0.0176,1.0000,0.4345 -5.000,-0.5545,0.04796,0.03916,0.0195,1.0000,0.4370 -4.750,-0.5719,0.04406,0.03509,0.0214,1.0000,0.4402 -4.500,-0.5589,0.04247,0.03355,0.0231,1.0000,0.4445 -4.250,-0.5471,0.04104,0.03215,0.0249,1.0000,0.4500 -4.000,-0.5466,0.03885,0.02984,0.0268,1.0000,0.4556 -3.750,-0.5424,0.03697,0.02788,0.0287,1.0000,0.4606 -3.500,-0.5291,0.03600,0.02699,0.0306,1.0000,0.4657 -3.250,-0.5229,0.03473,0.02568,0.0325,1.0000,0.4713 -3.000,-0.5216,0.03336,0.02417,0.0346,1.0000,0.4773 -2.750,-0.5140,0.03292,0.02389,0.0367,1.0000,0.4822 -2.500,-0.5132,0.03253,0.02353,0.0385,0.9995,0.4873 -2.250,-0.4108,0.03178,0.02278,0.0231,0.9543,0.5020 -2.000,-0.3206,0.03051,0.02150,0.0115,0.9078,0.5172 -1.750,-0.2388,0.02908,0.02003,0.0025,0.8610,0.5325 -1.500,-0.1762,0.02806,0.01889,-0.0023,0.8118,0.5472 -1.250,-0.1329,0.02752,0.01821,-0.0035,0.7664,0.5589 -1.000,-0.1039,0.02716,0.01764,-0.0030,0.7292,0.5706 -0.750,-0.0803,0.02697,0.01727,-0.0019,0.6975,0.5841 -0.500,-0.0520,0.02689,0.01715,-0.0013,0.6717,0.5975 -0.250,-0.0261,0.02682,0.01706,-0.0006,0.6486,0.6122 0.000,0.0000,0.02679,0.01701,0.0000,0.6291,0.6290 0.250,0.0261,0.02683,0.01706,0.0006,0.6122,0.6486 0.500,0.0520,0.02689,0.01715,0.0013,0.5975,0.6715 0.750,0.0804,0.02697,0.01727,0.0019,0.5842,0.6975 1.000,0.1039,0.02716,0.01764,0.0030,0.5706,0.7292 1.250,0.1328,0.02752,0.01821,0.0036,0.5589,0.7664 1.500,0.1760,0.02805,0.01888,0.0023,0.5471,0.8116 1.750,0.2387,0.02908,0.02003,-0.0025,0.5325,0.8610 2.000,0.3205,0.03051,0.02151,-0.0115,0.5173,0.9078 2.250,0.4108,0.03179,0.02278,-0.0231,0.5020,0.9543 2.500,0.5135,0.03252,0.02352,-0.0386,0.4872,0.9997 2.750,0.5140,0.03291,0.02387,-0.0367,0.4821,1.0000 3.000,0.5215,0.03336,0.02417,-0.0346,0.4773,1.0000 3.250,0.5228,0.03472,0.02567,-0.0325,0.4714,1.0000 3.500,0.5290,0.03599,0.02698,-0.0306,0.4656,1.0000 3.750,0.5423,0.03697,0.02787,-0.0287,0.4607,1.0000 4.000,0.5466,0.03884,0.02984,-0.0268,0.4555,1.0000 4.250,0.5471,0.04104,0.03215,-0.0249,0.4500,1.0000 4.500,0.5587,0.04247,0.03356,-0.0231,0.4446,1.0000 4.750,0.5721,0.04405,0.03507,-0.0214,0.4402,1.0000 5.000,0.5545,0.04795,0.03915,-0.0195,0.4370,1.0000 5.250,0.5335,0.05209,0.04336,-0.0176,0.4344,1.0000 5.500,0.5072,0.05663,0.04791,-0.0160,0.4337,1.0000 5.750,0.4787,0.06149,0.05273,-0.0149,0.4365,1.0000 6.000,0.4670,0.06534,0.05653,-0.0139,0.4393,1.0000 6.250,0.4691,0.06869,0.05985,-0.0135,0.4410,1.0000 7.500,0.3195,0.09107,0.08199,-0.0184,0.5525,1.0000 7.750,0.3241,0.09310,0.08400,-0.0175,0.5387,1.0000 8.000,0.3639,0.09792,0.08885,-0.0190,0.5304,1.0000 8.250,0.3550,0.09848,0.08938,-0.0172,0.5155,1.0000 8.500,0.3546,0.10033,0.09120,-0.0163,0.5025,1.0000 8.750,0.3785,0.10412,0.09500,-0.0167,0.4931,1.0000 9.000,0.3841,0.10593,0.09680,-0.0160,0.4797,1.0000 9.250,0.3820,0.10796,0.09881,-0.0154,0.4693,1.0000 9.500,0.4212,0.11297,0.10388,-0.0162,0.4593,1.0000 9.750,0.4031,0.11318,0.10404,-0.0150,0.4465,1.0000 10.000,0.4244,0.11741,0.10829,-0.0154,0.4397,1.0000