Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag19-il-50000-n5 Airfoil,ag19-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,37.1008 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-ag19-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.5328,0.11368,0.10686,0.0138,1.0000,0.0876 -8.250,-0.5343,0.11143,0.10470,0.0098,1.0000,0.0909 -8.000,-0.5370,0.10933,0.10271,0.0045,1.0000,0.0918 -7.750,-0.5277,0.10440,0.09784,0.0044,1.0000,0.0928 -7.500,-0.5165,0.09990,0.09335,0.0053,1.0000,0.0945 -7.250,-0.5077,0.09607,0.08956,0.0038,1.0000,0.0961 -7.000,-0.4986,0.09224,0.08577,0.0011,1.0000,0.0975 -6.750,-0.4883,0.08823,0.08179,-0.0025,1.0000,0.0978 -6.500,-0.4679,0.08010,0.07354,-0.0120,1.0000,0.0494 -6.250,-0.4542,0.07554,0.06899,-0.0152,1.0000,0.0463 -5.750,-0.4053,0.06231,0.05540,-0.0323,1.0000,0.0389 -5.500,-0.3836,0.05724,0.05015,-0.0363,1.0000,0.0390 -5.250,-0.3597,0.05213,0.04480,-0.0405,1.0000,0.0395 -5.000,-0.3436,0.04926,0.04201,-0.0407,1.0000,0.0424 -4.750,-0.3160,0.04434,0.03664,-0.0444,1.0000,0.0422 -4.500,-0.2861,0.03937,0.03113,-0.0475,1.0000,0.0413 -4.250,-0.2566,0.03519,0.02635,-0.0494,1.0000,0.0411 -4.000,-0.2281,0.03180,0.02246,-0.0505,1.0000,0.0417 -3.750,-0.1998,0.02894,0.01913,-0.0509,1.0000,0.0431 -3.500,-0.1717,0.02664,0.01640,-0.0511,1.0000,0.0471 -3.250,-0.1434,0.02457,0.01383,-0.0509,1.0000,0.0535 -3.000,-0.1167,0.02277,0.01184,-0.0504,1.0000,0.0589 -2.750,-0.0901,0.02119,0.01000,-0.0496,1.0000,0.0677 -2.500,-0.0634,0.01997,0.00864,-0.0492,1.0000,0.0864 -2.250,-0.0356,0.01874,0.00737,-0.0490,1.0000,0.1199 -2.000,-0.0077,0.01733,0.00639,-0.0492,1.0000,0.2041 -1.750,0.0175,0.01584,0.00589,-0.0491,1.0000,0.4175 -1.500,0.0330,0.01385,0.00544,-0.0450,1.0000,0.9564 -1.250,0.0591,0.01385,0.00493,-0.0446,1.0000,1.0000 -1.000,0.0850,0.01390,0.00461,-0.0444,1.0000,1.0000 -0.750,0.1106,0.01396,0.00439,-0.0441,1.0000,1.0000 -0.500,0.1360,0.01405,0.00425,-0.0438,1.0000,1.0000 -0.250,0.1610,0.01417,0.00417,-0.0435,1.0000,1.0000 0.000,0.1858,0.01431,0.00414,-0.0433,1.0000,1.0000 0.250,0.2103,0.01448,0.00420,-0.0430,1.0000,1.0000 0.500,0.2346,0.01470,0.00433,-0.0428,1.0000,1.0000 0.750,0.2586,0.01495,0.00453,-0.0427,1.0000,1.0000 1.000,0.2924,0.01525,0.00480,-0.0446,0.9908,1.0000 1.250,0.3430,0.01550,0.00504,-0.0494,0.9663,1.0000 1.500,0.3911,0.01566,0.00525,-0.0534,0.9398,1.0000 1.750,0.4336,0.01578,0.00543,-0.0558,0.9092,1.0000 2.000,0.4725,0.01588,0.00562,-0.0573,0.8756,1.0000 2.250,0.5062,0.01599,0.00577,-0.0575,0.8377,1.0000 2.500,0.5361,0.01613,0.00591,-0.0568,0.7967,1.0000 2.750,0.5629,0.01631,0.00605,-0.0554,0.7527,1.0000 3.000,0.5876,0.01656,0.00624,-0.0536,0.7052,1.0000 3.250,0.6114,0.01688,0.00653,-0.0518,0.6545,1.0000 3.500,0.6347,0.01728,0.00679,-0.0500,0.6006,1.0000 3.750,0.6577,0.01776,0.00711,-0.0484,0.5457,1.0000 4.000,0.6808,0.01835,0.00752,-0.0469,0.4915,1.0000 4.250,0.7040,0.01901,0.00802,-0.0458,0.4398,1.0000 4.500,0.7273,0.01976,0.00871,-0.0447,0.3926,1.0000 4.750,0.7513,0.02056,0.00942,-0.0440,0.3484,1.0000 5.000,0.7754,0.02142,0.01021,-0.0434,0.3079,1.0000 5.250,0.7994,0.02236,0.01108,-0.0428,0.2717,1.0000 5.500,0.8236,0.02333,0.01209,-0.0423,0.2373,1.0000 5.750,0.8472,0.02439,0.01324,-0.0417,0.2071,1.0000 6.000,0.8707,0.02555,0.01444,-0.0410,0.1803,1.0000 6.250,0.8940,0.02682,0.01580,-0.0404,0.1565,1.0000 6.500,0.9166,0.02818,0.01719,-0.0397,0.1358,1.0000 6.750,0.9394,0.02972,0.01894,-0.0389,0.1170,1.0000 7.000,0.9613,0.03141,0.02077,-0.0382,0.1010,1.0000 7.250,0.9822,0.03318,0.02267,-0.0374,0.0865,1.0000 7.500,1.0036,0.03560,0.02554,-0.0364,0.0758,1.0000 7.750,1.0226,0.03775,0.02799,-0.0357,0.0641,1.0000 8.000,1.0409,0.04077,0.03124,-0.0347,0.0581,1.0000 8.250,1.0570,0.04424,0.03533,-0.0337,0.0519,1.0000 8.500,1.0700,0.04711,0.03843,-0.0331,0.0461,1.0000 8.750,1.0777,0.05195,0.04400,-0.0322,0.0431,1.0000 9.000,1.0805,0.05700,0.04960,-0.0316,0.0415,1.0000 9.250,1.0778,0.06220,0.05525,-0.0315,0.0405,1.0000 9.500,1.0692,0.06759,0.06101,-0.0318,0.0399,1.0000 9.750,1.0522,0.07348,0.06719,-0.0332,0.0402,1.0000 10.000,1.0285,0.08016,0.07405,-0.0366,0.0410,1.0000 10.250,1.0046,0.08887,0.08284,-0.0436,0.0422,1.0000