Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e222-il-50000-n5 Airfoil,e222-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,38.8341 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e222-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4605,0.08991,0.08279,-0.0434,1.0000,0.0482 -9.000,-0.4633,0.08595,0.07891,-0.0442,1.0000,0.0479 -8.750,-0.4689,0.08176,0.07480,-0.0453,1.0000,0.0475 -8.500,-0.4797,0.07702,0.07015,-0.0471,1.0000,0.0471 -8.250,-0.4926,0.07248,0.06569,-0.0491,1.0000,0.0466 -8.000,-0.5052,0.06784,0.06105,-0.0508,1.0000,0.0462 -7.750,-0.5152,0.06343,0.05658,-0.0518,1.0000,0.0458 -7.500,-0.5225,0.05906,0.05207,-0.0524,1.0000,0.0455 -7.250,-0.5256,0.05476,0.04755,-0.0528,1.0000,0.0452 -7.000,-0.5243,0.05057,0.04305,-0.0529,1.0000,0.0451 -6.750,-0.5182,0.04660,0.03868,-0.0528,1.0000,0.0451 -6.500,-0.5077,0.04297,0.03461,-0.0526,1.0000,0.0453 -6.250,-0.4936,0.03969,0.03086,-0.0522,1.0000,0.0457 -6.000,-0.4766,0.03682,0.02750,-0.0516,1.0000,0.0464 -5.750,-0.4575,0.03442,0.02460,-0.0509,1.0000,0.0478 -5.500,-0.4385,0.03241,0.02239,-0.0502,1.0000,0.0502 -5.250,-0.4189,0.03092,0.02077,-0.0495,1.0000,0.0536 -5.000,-0.3980,0.02940,0.01896,-0.0485,1.0000,0.0567 -4.750,-0.3766,0.02797,0.01725,-0.0473,1.0000,0.0595 -4.500,-0.3558,0.02665,0.01583,-0.0462,1.0000,0.0633 -4.250,-0.3346,0.02555,0.01464,-0.0454,1.0000,0.0694 -4.000,-0.3125,0.02446,0.01351,-0.0448,1.0000,0.0822 -3.750,-0.2896,0.02325,0.01243,-0.0445,1.0000,0.1150 -3.500,-0.2660,0.02200,0.01174,-0.0451,1.0000,0.2071 -3.250,-0.2434,0.02123,0.01144,-0.0451,1.0000,0.3123 -3.000,-0.2220,0.02079,0.01127,-0.0444,1.0000,0.3934 -2.750,-0.2015,0.02052,0.01117,-0.0433,1.0000,0.4639 -2.500,-0.1821,0.02035,0.01113,-0.0419,1.0000,0.5264 -2.250,-0.1494,0.02033,0.01120,-0.0427,0.9922,0.5984 -2.000,-0.1175,0.02038,0.01132,-0.0431,0.9838,0.6664 -1.750,-0.0893,0.02039,0.01138,-0.0427,0.9743,0.7292 -1.500,-0.0623,0.02038,0.01138,-0.0419,0.9647,0.7914 -1.250,-0.0317,0.02036,0.01134,-0.0417,0.9558,0.8611 -1.000,0.0162,0.02023,0.01110,-0.0455,0.9472,0.9522 -0.750,0.0597,0.02024,0.01082,-0.0495,0.9365,1.0000 -0.500,0.0990,0.02041,0.01073,-0.0525,0.9271,1.0000 -0.250,0.1378,0.02057,0.01068,-0.0553,0.9171,1.0000 0.000,0.1723,0.02071,0.01064,-0.0571,0.9057,1.0000 0.250,0.2080,0.02086,0.01064,-0.0590,0.8948,1.0000 0.500,0.2469,0.02097,0.01063,-0.0613,0.8850,1.0000 0.750,0.2839,0.02106,0.01062,-0.0632,0.8743,1.0000 1.000,0.3176,0.02117,0.01066,-0.0645,0.8622,1.0000 1.250,0.3523,0.02125,0.01070,-0.0658,0.8505,1.0000 1.500,0.3877,0.02131,0.01072,-0.0672,0.8389,1.0000 1.750,0.4240,0.02131,0.01071,-0.0685,0.8276,1.0000 2.000,0.4599,0.02129,0.01072,-0.0697,0.8158,1.0000 2.250,0.4919,0.02133,0.01077,-0.0702,0.8020,1.0000 2.500,0.5239,0.02136,0.01082,-0.0706,0.7880,1.0000 2.750,0.5560,0.02137,0.01089,-0.0710,0.7735,1.0000 3.000,0.5880,0.02136,0.01094,-0.0713,0.7585,1.0000 3.250,0.6185,0.02140,0.01102,-0.0713,0.7423,1.0000 3.500,0.6465,0.02149,0.01119,-0.0709,0.7244,1.0000 3.750,0.6758,0.02155,0.01135,-0.0706,0.7063,1.0000 4.000,0.7062,0.02157,0.01143,-0.0704,0.6879,1.0000 4.250,0.7339,0.02169,0.01161,-0.0698,0.6676,1.0000 4.500,0.7612,0.02181,0.01181,-0.0691,0.6462,1.0000 4.750,0.7881,0.02197,0.01208,-0.0684,0.6238,1.0000 5.000,0.8148,0.02215,0.01231,-0.0676,0.6003,1.0000 5.250,0.8389,0.02242,0.01265,-0.0664,0.5747,1.0000 5.500,0.8629,0.02272,0.01300,-0.0653,0.5479,1.0000 5.750,0.8861,0.02306,0.01343,-0.0640,0.5198,1.0000 6.000,0.9082,0.02346,0.01386,-0.0626,0.4903,1.0000 6.250,0.9293,0.02393,0.01435,-0.0611,0.4595,1.0000 6.500,0.9492,0.02448,0.01489,-0.0595,0.4277,1.0000 6.750,0.9677,0.02512,0.01552,-0.0578,0.3947,1.0000 7.000,0.9849,0.02586,0.01631,-0.0560,0.3610,1.0000 7.250,1.0010,0.02670,0.01711,-0.0541,0.3276,1.0000 7.500,1.0160,0.02765,0.01803,-0.0522,0.2948,1.0000 7.750,1.0297,0.02873,0.01908,-0.0502,0.2620,1.0000 8.000,1.0425,0.02993,0.02024,-0.0483,0.2315,1.0000 8.250,1.0542,0.03125,0.02153,-0.0463,0.2032,1.0000 8.500,1.0648,0.03271,0.02300,-0.0443,0.1772,1.0000 8.750,1.0738,0.03431,0.02453,-0.0422,0.1545,1.0000 9.000,1.0814,0.03599,0.02625,-0.0399,0.1329,1.0000 9.250,1.0860,0.03787,0.02804,-0.0376,0.1143,1.0000 9.500,1.0895,0.03982,0.03005,-0.0354,0.0952,1.0000 9.750,1.0902,0.04191,0.03212,-0.0333,0.0794,1.0000 10.000,1.0922,0.04423,0.03447,-0.0315,0.0672,1.0000 10.250,1.0955,0.04675,0.03711,-0.0298,0.0583,1.0000 10.500,1.0966,0.04939,0.03972,-0.0284,0.0529,1.0000 10.750,1.1037,0.05204,0.04268,-0.0271,0.0472,1.0000 11.000,1.1050,0.05477,0.04548,-0.0261,0.0435,1.0000 11.250,1.1090,0.05777,0.04870,-0.0252,0.0408,1.0000 11.500,1.1139,0.06111,0.05241,-0.0243,0.0386,1.0000 11.750,1.1150,0.06475,0.05635,-0.0237,0.0372,1.0000 12.000,1.1124,0.06869,0.06058,-0.0235,0.0362,1.0000 12.250,1.1062,0.07307,0.06523,-0.0239,0.0355,1.0000 12.500,1.0969,0.07792,0.07034,-0.0249,0.0350,1.0000 12.750,1.0844,0.08342,0.07610,-0.0267,0.0347,1.0000 13.000,1.0684,0.08975,0.08268,-0.0294,0.0347,1.0000 13.250,1.0484,0.09727,0.09045,-0.0335,0.0349,1.0000 13.500,1.0243,0.10638,0.09979,-0.0390,0.0354,1.0000 13.750,0.9967,0.11744,0.11106,-0.0461,0.0362,1.0000