Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e230-il-100000 Airfoil,e230-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,32.624 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-e230-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.7082,0.08491,0.08067,0.0062,1.0000,0.0562 -10.500,-0.7321,0.07626,0.07197,0.0015,1.0000,0.0545 -10.250,-0.8606,0.07511,0.07039,-0.0013,1.0000,0.0561 -10.000,-0.8778,0.07035,0.06553,-0.0018,1.0000,0.0549 -9.750,-0.8988,0.06587,0.06089,-0.0008,1.0000,0.0537 -9.500,-0.9190,0.06088,0.05562,0.0009,1.0000,0.0518 -9.250,-0.9543,0.05474,0.04845,0.0050,1.0000,0.0475 -9.000,-0.9463,0.05114,0.04452,0.0066,1.0000,0.0464 -8.750,-0.9402,0.04665,0.03970,0.0081,1.0000,0.0458 -8.500,-0.9312,0.04278,0.03542,0.0099,1.0000,0.0453 -8.250,-0.9194,0.03978,0.03191,0.0118,1.0000,0.0460 -8.000,-0.9046,0.03751,0.02910,0.0137,1.0000,0.0469 -7.750,-0.8853,0.03356,0.02486,0.0146,1.0000,0.0479 -7.500,-0.8622,0.03069,0.02182,0.0153,1.0000,0.0493 -7.250,-0.8378,0.02842,0.01942,0.0160,1.0000,0.0513 -7.000,-0.8130,0.02645,0.01732,0.0167,1.0000,0.0542 -6.750,-0.7883,0.02477,0.01544,0.0177,1.0000,0.0582 -6.500,-0.7687,0.02290,0.01370,0.0190,1.0000,0.0681 -6.250,-0.7521,0.02094,0.01193,0.0209,1.0000,0.0881 -6.000,-0.7402,0.01862,0.01018,0.0234,1.0000,0.1634 -5.750,-0.7231,0.01757,0.00950,0.0248,1.0000,0.2359 -5.500,-0.7060,0.01685,0.00909,0.0265,1.0000,0.3010 -5.250,-0.6872,0.01617,0.00857,0.0281,1.0000,0.3558 -5.000,-0.6678,0.01553,0.00812,0.0297,1.0000,0.4060 -4.750,-0.6480,0.01498,0.00771,0.0313,1.0000,0.4567 -4.500,-0.6279,0.01445,0.00739,0.0331,1.0000,0.5051 -4.250,-0.6076,0.01399,0.00708,0.0349,1.0000,0.5533 -4.000,-0.5872,0.01360,0.00685,0.0367,1.0000,0.6015 -3.750,-0.5668,0.01327,0.00667,0.0387,1.0000,0.6494 -3.500,-0.5454,0.01302,0.00657,0.0406,1.0000,0.6956 -3.250,-0.5225,0.01287,0.00651,0.0423,1.0000,0.7401 -3.000,-0.4971,0.01285,0.00655,0.0437,1.0000,0.7825 -2.750,-0.4633,0.01302,0.00673,0.0436,1.0000,0.8202 -2.500,-0.4251,0.01332,0.00697,0.0427,1.0000,0.8536 -2.250,-0.3759,0.01378,0.00732,0.0397,1.0000,0.8792 -2.000,-0.3277,0.01421,0.00763,0.0367,1.0000,0.9020 -1.750,-0.2660,0.01462,0.00789,0.0309,1.0000,0.9176 -1.500,-0.2080,0.01485,0.00802,0.0254,1.0000,0.9329 -1.250,-0.1521,0.01492,0.00800,0.0199,1.0000,0.9483 -1.000,-0.0968,0.01484,0.00788,0.0142,1.0000,0.9635 -0.750,-0.0408,0.01460,0.00763,0.0081,1.0000,0.9781 -0.500,0.0165,0.01421,0.00726,0.0014,1.0000,0.9920 -0.250,0.0589,0.01385,0.00695,-0.0032,1.0000,1.0000 0.000,0.0525,0.01408,0.00722,0.0001,1.0000,1.0000 0.250,0.1068,0.01400,0.00720,-0.0065,0.9781,1.0000 0.500,0.1678,0.01383,0.00710,-0.0135,0.9505,1.0000 0.750,0.2035,0.01378,0.00704,-0.0150,0.9163,1.0000 1.000,0.2184,0.01380,0.00704,-0.0123,0.8817,1.0000 1.250,0.2303,0.01381,0.00702,-0.0089,0.8514,1.0000 1.500,0.2426,0.01381,0.00699,-0.0054,0.8232,1.0000 1.750,0.2563,0.01379,0.00694,-0.0022,0.7964,1.0000 2.000,0.2716,0.01377,0.00687,0.0008,0.7697,1.0000 2.250,0.2889,0.01376,0.00682,0.0033,0.7414,1.0000 2.500,0.3072,0.01377,0.00678,0.0056,0.7128,1.0000 2.750,0.3265,0.01379,0.00678,0.0077,0.6834,1.0000 3.000,0.3466,0.01383,0.00676,0.0097,0.6528,1.0000 3.250,0.3671,0.01390,0.00676,0.0115,0.6210,1.0000 3.500,0.3884,0.01401,0.00682,0.0131,0.5862,1.0000 3.750,0.4101,0.01416,0.00693,0.0147,0.5495,1.0000 4.000,0.4320,0.01436,0.00705,0.0161,0.5105,1.0000 4.250,0.4540,0.01462,0.00720,0.0174,0.4686,1.0000 4.500,0.4761,0.01494,0.00742,0.0186,0.4226,1.0000 4.750,0.4981,0.01536,0.00773,0.0197,0.3729,1.0000 5.000,0.5197,0.01593,0.00811,0.0207,0.3208,1.0000 5.250,0.5408,0.01663,0.00858,0.0217,0.2632,1.0000 5.500,0.5614,0.01736,0.00906,0.0223,0.1983,1.0000 5.750,0.5807,0.01860,0.00997,0.0232,0.1374,1.0000 6.000,0.5981,0.02060,0.01165,0.0246,0.0878,1.0000 6.250,0.6171,0.02209,0.01302,0.0260,0.0719,1.0000 6.500,0.6372,0.02384,0.01479,0.0275,0.0651,1.0000 6.750,0.6584,0.02544,0.01647,0.0288,0.0607,1.0000 7.000,0.6792,0.02753,0.01857,0.0300,0.0579,1.0000 7.250,0.6994,0.03011,0.02137,0.0313,0.0562,1.0000 7.500,0.7182,0.03208,0.02380,0.0328,0.0541,1.0000 7.750,0.7347,0.03450,0.02663,0.0342,0.0523,1.0000 8.000,0.7479,0.03761,0.03020,0.0358,0.0522,1.0000 8.250,0.7572,0.04120,0.03424,0.0375,0.0528,1.0000 8.500,0.7620,0.04516,0.03862,0.0391,0.0536,1.0000 8.750,0.7637,0.04927,0.04306,0.0406,0.0547,1.0000 9.000,0.7636,0.05361,0.04762,0.0418,0.0558,1.0000 9.250,0.7678,0.05748,0.05172,0.0429,0.0578,1.0000 9.500,0.7037,0.06491,0.05981,0.0431,0.0622,1.0000 9.750,0.6692,0.07082,0.06580,0.0404,0.0636,1.0000 10.000,0.6428,0.07885,0.07383,0.0345,0.0658,1.0000