Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e226-il-50000-n5 Airfoil,e226-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,32.1977 Max Cl/Cd alpha,5.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-e226-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.5882,0.09754,0.09039,-0.0176,1.0000,0.0431 -10.250,-0.5951,0.09103,0.08394,-0.0213,1.0000,0.0426 -10.000,-0.6057,0.08369,0.07664,-0.0260,1.0000,0.0418 -9.750,-0.6229,0.07597,0.06893,-0.0319,1.0000,0.0409 -9.500,-0.6457,0.06931,0.06222,-0.0367,1.0000,0.0401 -9.250,-0.6674,0.06442,0.05722,-0.0380,1.0000,0.0394 -9.000,-0.6824,0.05988,0.05247,-0.0384,1.0000,0.0392 -8.750,-0.6897,0.05587,0.04819,-0.0381,1.0000,0.0395 -8.500,-0.6918,0.05215,0.04415,-0.0373,1.0000,0.0402 -8.250,-0.6894,0.04865,0.04029,-0.0363,1.0000,0.0410 -8.000,-0.6829,0.04532,0.03655,-0.0352,1.0000,0.0418 -7.750,-0.6729,0.04217,0.03295,-0.0338,1.0000,0.0428 -7.500,-0.6592,0.03929,0.02964,-0.0325,1.0000,0.0436 -7.250,-0.6425,0.03669,0.02660,-0.0311,1.0000,0.0446 -7.000,-0.6242,0.03439,0.02401,-0.0297,1.0000,0.0460 -6.750,-0.6062,0.03249,0.02203,-0.0284,1.0000,0.0480 -6.500,-0.5880,0.03087,0.02028,-0.0270,1.0000,0.0515 -6.250,-0.5690,0.02935,0.01851,-0.0253,1.0000,0.0570 -6.000,-0.5524,0.02790,0.01709,-0.0238,1.0000,0.0634 -5.750,-0.5355,0.02641,0.01554,-0.0220,1.0000,0.0723 -5.500,-0.5193,0.02491,0.01405,-0.0203,1.0000,0.0922 -5.250,-0.5036,0.02341,0.01290,-0.0189,1.0000,0.1375 -5.000,-0.4884,0.02216,0.01212,-0.0176,1.0000,0.2118 -4.750,-0.4717,0.02124,0.01143,-0.0160,1.0000,0.2735 -4.500,-0.4543,0.02053,0.01088,-0.0145,1.0000,0.3306 -4.250,-0.4370,0.01995,0.01039,-0.0127,1.0000,0.3843 -4.000,-0.4199,0.01945,0.01001,-0.0107,1.0000,0.4342 -3.750,-0.4026,0.01904,0.00970,-0.0086,1.0000,0.4834 -3.500,-0.3852,0.01869,0.00944,-0.0065,1.0000,0.5322 -3.250,-0.3679,0.01840,0.00920,-0.0043,1.0000,0.5800 -3.000,-0.3506,0.01817,0.00906,-0.0020,1.0000,0.6270 -2.750,-0.3334,0.01800,0.00895,0.0005,1.0000,0.6732 -2.500,-0.3160,0.01789,0.00889,0.0029,1.0000,0.7196 -2.250,-0.2976,0.01783,0.00885,0.0053,1.0000,0.7666 -2.000,-0.2759,0.01784,0.00886,0.0070,1.0000,0.8152 -1.750,-0.2463,0.01791,0.00888,0.0070,1.0000,0.8659 -1.500,-0.2019,0.01805,0.00887,0.0039,1.0000,0.9149 -1.250,-0.1384,0.01823,0.00884,-0.0033,0.9955,0.9559 -1.000,-0.0697,0.01833,0.00872,-0.0120,0.9897,0.9881 -0.750,-0.0193,0.01841,0.00862,-0.0176,0.9785,1.0000 -0.500,0.0221,0.01849,0.00856,-0.0214,0.9640,1.0000 -0.250,0.0635,0.01858,0.00853,-0.0250,0.9497,1.0000 0.000,0.1053,0.01865,0.00852,-0.0284,0.9357,1.0000 0.250,0.1475,0.01870,0.00851,-0.0317,0.9216,1.0000 0.500,0.1867,0.01873,0.00850,-0.0342,0.9065,1.0000 0.750,0.2231,0.01875,0.00851,-0.0360,0.8906,1.0000 1.000,0.2573,0.01877,0.00853,-0.0373,0.8740,1.0000 1.250,0.2896,0.01879,0.00855,-0.0380,0.8570,1.0000 1.500,0.3205,0.01880,0.00858,-0.0383,0.8397,1.0000 1.750,0.3480,0.01884,0.00864,-0.0380,0.8212,1.0000 2.000,0.3728,0.01892,0.00874,-0.0371,0.8013,1.0000 2.250,0.3985,0.01897,0.00881,-0.0362,0.7820,1.0000 2.500,0.4246,0.01900,0.00889,-0.0352,0.7631,1.0000 2.750,0.4466,0.01914,0.00905,-0.0337,0.7412,1.0000 3.000,0.4709,0.01921,0.00915,-0.0324,0.7203,1.0000 3.250,0.4937,0.01934,0.00932,-0.0310,0.6977,1.0000 3.500,0.5176,0.01945,0.00948,-0.0296,0.6750,1.0000 3.750,0.5402,0.01962,0.00969,-0.0281,0.6501,1.0000 4.000,0.5634,0.01978,0.00988,-0.0266,0.6250,1.0000 4.250,0.5865,0.01997,0.01011,-0.0251,0.5988,1.0000 4.500,0.6086,0.02022,0.01039,-0.0235,0.5704,1.0000 4.750,0.6306,0.02050,0.01069,-0.0220,0.5407,1.0000 5.000,0.6523,0.02082,0.01102,-0.0204,0.5099,1.0000 5.250,0.6732,0.02121,0.01144,-0.0188,0.4767,1.0000 5.500,0.6936,0.02165,0.01189,-0.0172,0.4420,1.0000 5.750,0.7135,0.02216,0.01236,-0.0156,0.4069,1.0000 6.000,0.7327,0.02276,0.01295,-0.0140,0.3698,1.0000 6.250,0.7511,0.02346,0.01361,-0.0124,0.3328,1.0000 6.500,0.7688,0.02426,0.01438,-0.0108,0.2946,1.0000 6.750,0.7854,0.02519,0.01521,-0.0092,0.2580,1.0000 7.000,0.8016,0.02625,0.01622,-0.0077,0.2212,1.0000 7.250,0.8165,0.02747,0.01734,-0.0061,0.1880,1.0000 7.500,0.8307,0.02887,0.01864,-0.0045,0.1567,1.0000 7.750,0.8434,0.03042,0.02016,-0.0029,0.1257,1.0000 8.000,0.8540,0.03203,0.02165,-0.0014,0.0965,1.0000 8.250,0.8641,0.03385,0.02334,0.0002,0.0769,1.0000 8.500,0.8754,0.03576,0.02527,0.0018,0.0648,1.0000 8.750,0.8877,0.03772,0.02734,0.0034,0.0565,1.0000 9.000,0.9024,0.03993,0.02974,0.0049,0.0514,1.0000 9.250,0.9163,0.04204,0.03206,0.0063,0.0473,1.0000 9.500,0.9274,0.04423,0.03424,0.0075,0.0441,1.0000 9.750,0.9394,0.04684,0.03729,0.0089,0.0415,1.0000 10.000,0.9475,0.04962,0.04041,0.0103,0.0395,1.0000 10.250,0.9516,0.05250,0.04358,0.0118,0.0386,1.0000 10.500,0.9511,0.05555,0.04690,0.0134,0.0378,1.0000 10.750,0.9466,0.05885,0.05044,0.0146,0.0372,1.0000 11.000,0.9386,0.06246,0.05431,0.0152,0.0369,1.0000 11.250,0.9264,0.06662,0.05871,0.0150,0.0368,1.0000 11.500,0.9104,0.07146,0.06378,0.0136,0.0367,1.0000 11.750,0.8893,0.07753,0.07008,0.0107,0.0370,1.0000 12.000,0.8634,0.08526,0.07802,0.0058,0.0375,1.0000 12.250,0.8298,0.09605,0.08899,-0.0018,0.0386,1.0000