Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e1210-il-50000-n5 Airfoil,e1210-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,25.7752 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-e1210-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.2051,0.10974,0.10304,-0.0369,1.0000,0.0870 -9.500,-0.2105,0.10653,0.09994,-0.0379,1.0000,0.0877 -9.250,-0.2111,0.10392,0.09748,-0.0379,1.0000,0.0891 -9.000,-0.2085,0.10203,0.09573,-0.0370,1.0000,0.0909 -8.750,-0.2166,0.09993,0.09382,-0.0363,0.9997,0.0914 -8.500,-0.1992,0.09500,0.08890,-0.0425,0.9670,0.0932 -8.250,-0.1881,0.08943,0.08331,-0.0500,0.9392,0.0956 -8.000,-0.1831,0.08268,0.07651,-0.0591,0.9145,0.0969 -7.750,-0.1471,0.08011,0.07387,-0.0625,0.8941,0.1010 -7.500,-0.1371,0.07496,0.06863,-0.0690,0.8714,0.1034 -7.250,-0.1389,0.06828,0.06181,-0.0776,0.8501,0.1054 -7.000,-0.1426,0.06146,0.05477,-0.0850,0.8310,0.1077 -6.750,-0.1233,0.05970,0.05290,-0.0855,0.8128,0.1107 -6.500,-0.1196,0.05504,0.04798,-0.0891,0.7967,0.1139 -6.250,-0.1250,0.04769,0.03991,-0.0947,0.7836,0.1180 -6.000,-0.1022,0.04739,0.03966,-0.0934,0.7672,0.1209 -5.750,-0.0860,0.04514,0.03713,-0.0939,0.7530,0.1249 -5.500,-0.0722,0.04099,0.03220,-0.0959,0.7416,0.1302 -5.250,-0.0504,0.04040,0.03166,-0.0949,0.7269,0.1335 -5.000,-0.0286,0.03896,0.02996,-0.0947,0.7149,0.1379 -4.750,-0.0078,0.03663,0.02697,-0.0952,0.7030,0.1438 -4.500,0.0153,0.03593,0.02627,-0.0945,0.6906,0.1476 -4.250,0.0402,0.03493,0.02504,-0.0941,0.6799,0.1529 -4.000,0.0638,0.03357,0.02318,-0.0941,0.6680,0.1589 -3.750,0.0900,0.03291,0.02248,-0.0936,0.6581,0.1636 -3.500,0.1139,0.03224,0.02165,-0.0931,0.6461,0.1694 -3.250,0.1416,0.03133,0.02034,-0.0929,0.6372,0.1761 -3.000,0.1653,0.03092,0.01995,-0.0923,0.6256,0.1814 -2.750,0.1930,0.03031,0.01907,-0.0919,0.6169,0.1888 -2.500,0.2176,0.02989,0.01853,-0.0914,0.6061,0.1954 -2.250,0.2446,0.02947,0.01802,-0.0909,0.5975,0.2027 -2.000,0.2702,0.02920,0.01752,-0.0904,0.5875,0.2115 -1.750,0.2967,0.02884,0.01718,-0.0899,0.5787,0.2192 -1.500,0.3226,0.02866,0.01683,-0.0893,0.5701,0.2296 -1.250,0.3479,0.02846,0.01664,-0.0886,0.5610,0.2390 -1.000,0.3762,0.02824,0.01622,-0.0883,0.5538,0.2522 -0.750,0.3998,0.02823,0.01630,-0.0876,0.5441,0.2647 -0.500,0.4272,0.02803,0.01603,-0.0871,0.5371,0.2813 -0.250,0.4513,0.02805,0.01612,-0.0864,0.5287,0.3005 0.000,0.4764,0.02797,0.01611,-0.0858,0.5208,0.3263 0.250,0.5039,0.02771,0.01589,-0.0853,0.5150,0.3636 0.500,0.5241,0.02784,0.01637,-0.0843,0.5061,0.4155 0.750,0.5467,0.02752,0.01645,-0.0830,0.4996,0.5115 1.000,0.5646,0.02699,0.01656,-0.0800,0.4941,0.6929 1.250,0.6011,0.02706,0.01690,-0.0812,0.4849,1.0000 1.500,0.6279,0.02738,0.01690,-0.0808,0.4790,1.0000 1.750,0.6513,0.02793,0.01725,-0.0802,0.4726,1.0000 2.000,0.6727,0.02859,0.01779,-0.0794,0.4653,1.0000 2.250,0.6992,0.02893,0.01789,-0.0789,0.4598,1.0000 2.500,0.7219,0.02954,0.01836,-0.0782,0.4538,1.0000 2.750,0.7411,0.03037,0.01914,-0.0773,0.4468,1.0000 3.000,0.7667,0.03078,0.01938,-0.0767,0.4416,1.0000 3.250,0.7925,0.03123,0.01964,-0.0763,0.4369,1.0000 3.500,0.8062,0.03242,0.02089,-0.0749,0.4295,1.0000 3.750,0.8293,0.03301,0.02137,-0.0742,0.4242,1.0000 4.000,0.8578,0.03328,0.02145,-0.0740,0.4203,1.0000 4.250,0.8684,0.03472,0.02297,-0.0724,0.4137,1.0000 4.500,0.8852,0.03572,0.02396,-0.0713,0.4079,1.0000 4.750,0.9110,0.03614,0.02426,-0.0708,0.4037,1.0000 5.000,0.9354,0.03673,0.02473,-0.0703,0.3997,1.0000 5.250,0.9336,0.03897,0.02716,-0.0680,0.3928,1.0000 5.500,0.9508,0.03994,0.02810,-0.0670,0.3880,1.0000 5.750,0.9791,0.04021,0.02825,-0.0667,0.3845,1.0000 6.000,0.9834,0.04210,0.03019,-0.0648,0.3794,1.0000 6.250,0.9674,0.04528,0.03355,-0.0620,0.3728,1.0000 6.500,0.9842,0.04627,0.03451,-0.0610,0.3688,1.0000 6.750,1.0169,0.04624,0.03437,-0.0609,0.3660,1.0000 7.000,0.9019,0.05765,0.04616,-0.0564,0.3534,1.0000 7.250,0.9201,0.05864,0.04712,-0.0557,0.3502,1.0000 7.500,0.9512,0.05835,0.04674,-0.0549,0.3482,1.0000 8.000,0.8790,0.07363,0.06224,-0.0575,0.3308,1.0000 9.000,0.8087,0.09794,0.08676,-0.0636,0.3045,1.0000 9.250,0.8145,0.10101,0.08984,-0.0640,0.3010,1.0000 9.500,0.8300,0.10275,0.09156,-0.0638,0.2985,1.0000 9.750,0.8508,0.10374,0.09252,-0.0632,0.2966,1.0000 10.000,0.8149,0.11254,0.10143,-0.0666,0.2888,1.0000 10.250,0.8196,0.11582,0.10473,-0.0673,0.2854,1.0000