Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e61-il-1000000-n5 Airfoil,e61-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,176.6 Max Cl/Cd alpha,2 Url,http://airfoiltools.com/polar/csv?polar=xf-e61-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.1650,0.11801,0.11618,-0.0775,0.9815,0.0046 -10.250,-0.1583,0.11527,0.11344,-0.0781,0.9789,0.0046 -10.000,-0.1479,0.11214,0.11031,-0.0801,0.9774,0.0047 -9.750,-0.1367,0.10907,0.10723,-0.0821,0.9763,0.0047 -9.500,-0.1248,0.10590,0.10406,-0.0844,0.9752,0.0047 -8.500,-0.0002,0.07559,0.07387,-0.0974,0.9623,0.0041 -8.250,0.0097,0.07180,0.07008,-0.0995,0.9612,0.0034 -8.000,0.0205,0.06799,0.06628,-0.1018,0.9603,0.0031 -7.500,-0.0364,0.08135,0.07955,-0.1003,0.9615,0.0030 -7.000,0.0352,0.05568,0.05401,-0.1027,0.9411,0.0027 -6.750,0.0419,0.05278,0.05111,-0.1036,0.9367,0.0028 -6.500,0.0452,0.05020,0.04854,-0.1036,0.9299,0.0029 -6.250,0.0585,0.04662,0.04496,-0.1067,0.9250,0.0029 -6.000,0.0799,0.04289,0.04122,-0.1118,0.9225,0.0036 -5.750,0.0973,0.03901,0.03732,-0.1164,0.9158,0.0039 -5.500,0.1257,0.03400,0.03228,-0.1248,0.9116,0.0042 -5.250,0.1648,0.02726,0.02548,-0.1381,0.9075,0.0050 -4.750,0.2017,0.03936,0.03743,-0.1568,0.9113,0.0052 -4.500,0.2529,0.03538,0.03337,-0.1675,0.9093,0.0055 -4.250,0.3006,0.03141,0.02928,-0.1767,0.9043,0.0062 -4.000,0.3717,0.02432,0.02193,-0.1922,0.9019,0.0074 -3.750,0.4520,0.01528,0.01227,-0.2079,0.9017,0.0085 -3.500,0.5027,0.01283,0.00940,-0.2140,0.8991,0.0090 -3.250,0.5535,0.01024,0.00634,-0.2205,0.8964,0.0106 -3.000,0.5883,0.00966,0.00562,-0.2224,0.8893,0.0113 -2.750,0.6253,0.00900,0.00477,-0.2247,0.8824,0.0119 -2.500,0.6579,0.00844,0.00404,-0.2259,0.8733,0.0124 -2.250,0.6896,0.00805,0.00352,-0.2269,0.8639,0.0131 -2.000,0.7212,0.00753,0.00286,-0.2278,0.8537,0.0128 -1.750,0.7513,0.00717,0.00235,-0.2283,0.8419,0.0125 -1.500,0.7802,0.00692,0.00198,-0.2286,0.8290,0.0122 -1.250,0.8083,0.00676,0.00170,-0.2287,0.8156,0.0120 -0.750,0.8629,0.00661,0.00134,-0.2284,0.7896,0.0119 -0.500,0.8895,0.00660,0.00123,-0.2282,0.7766,0.0121 -0.250,0.9157,0.00662,0.00116,-0.2278,0.7633,0.0127 0.000,0.9417,0.00667,0.00113,-0.2274,0.7500,0.0148 0.250,0.9672,0.00675,0.00115,-0.2269,0.7366,0.0162 0.500,0.9926,0.00684,0.00117,-0.2264,0.7225,0.0207 0.750,1.0189,0.00683,0.00128,-0.2261,0.7075,0.0932 1.000,1.0469,0.00670,0.00145,-0.2265,0.6922,0.2753 1.250,1.0743,0.00661,0.00164,-0.2267,0.6759,0.4455 1.500,1.1015,0.00654,0.00186,-0.2269,0.6562,0.6342 2.000,1.1426,0.00647,0.00219,-0.2237,0.6091,1.0000 2.250,1.1659,0.00676,0.00234,-0.2228,0.5802,1.0000 2.500,1.1885,0.00711,0.00253,-0.2218,0.5450,1.0000 2.750,1.2102,0.00756,0.00276,-0.2206,0.5021,1.0000 3.000,1.2316,0.00807,0.00303,-0.2194,0.4544,1.0000 3.250,1.2532,0.00858,0.00335,-0.2182,0.4094,1.0000 3.500,1.2730,0.00926,0.00371,-0.2168,0.3496,1.0000 3.750,1.2886,0.01036,0.00427,-0.2147,0.2515,1.0000 4.000,1.3074,0.01116,0.00474,-0.2131,0.1885,1.0000 4.250,1.3260,0.01199,0.00523,-0.2115,0.1292,1.0000 4.500,1.3443,0.01285,0.00578,-0.2098,0.0743,1.0000 4.750,1.3614,0.01385,0.00646,-0.2079,0.0201,1.0000 5.000,1.3825,0.01442,0.00697,-0.2067,0.0047,1.0000 5.250,1.4054,0.01477,0.00735,-0.2058,0.0035,1.0000 5.500,1.4278,0.01514,0.00776,-0.2048,0.0031,1.0000 5.750,1.4497,0.01557,0.00823,-0.2037,0.0026,1.0000 6.000,1.4707,0.01608,0.00880,-0.2024,0.0021,1.0000 6.250,1.4887,0.01687,0.00973,-0.2004,0.0017,1.0000 6.500,1.5078,0.01744,0.01035,-0.1987,0.0016,1.0000 6.750,1.5257,0.01808,0.01106,-0.1968,0.0016,1.0000 7.000,1.5425,0.01880,0.01190,-0.1947,0.0015,1.0000 7.250,1.5581,0.01964,0.01283,-0.1924,0.0015,1.0000 7.500,1.5726,0.02058,0.01387,-0.1899,0.0015,1.0000 7.750,1.5858,0.02163,0.01503,-0.1872,0.0014,1.0000 8.000,1.5977,0.02279,0.01630,-0.1843,0.0014,1.0000 8.250,1.6087,0.02409,0.01772,-0.1814,0.0014,1.0000 8.500,1.6189,0.02551,0.01927,-0.1783,0.0014,1.0000 8.750,1.6284,0.02707,0.02097,-0.1752,0.0014,1.0000 9.000,1.6393,0.02855,0.02257,-0.1725,0.0014,1.0000 9.250,1.6503,0.02998,0.02413,-0.1699,0.0013,1.0000 9.500,1.6616,0.03136,0.02565,-0.1674,0.0012,1.0000 9.750,1.6717,0.03293,0.02734,-0.1648,0.0012,1.0000 10.000,1.6810,0.03458,0.02913,-0.1622,0.0011,1.0000 10.250,1.6880,0.03669,0.03142,-0.1593,0.0011,1.0000 10.500,1.6947,0.03870,0.03358,-0.1566,0.0010,1.0000 10.750,1.6987,0.04117,0.03625,-0.1536,0.0010,1.0000 11.000,1.7008,0.04388,0.03916,-0.1506,0.0010,1.0000 11.250,1.7017,0.04660,0.04208,-0.1476,0.0010,1.0000 11.500,1.7016,0.04934,0.04500,-0.1449,0.0010,1.0000 11.750,1.6980,0.05262,0.04849,-0.1420,0.0010,1.0000 12.000,1.6923,0.05619,0.05227,-0.1394,0.0009,1.0000 12.250,1.6882,0.05945,0.05569,-0.1372,0.0009,1.0000 12.500,1.6746,0.06441,0.06091,-0.1349,0.0009,1.0000 12.750,1.6653,0.06868,0.06536,-0.1334,0.0009,1.0000 13.000,1.6580,0.07271,0.06957,-0.1325,0.0008,1.0000 13.250,1.6367,0.07956,0.07669,-0.1318,0.0009,1.0000 13.500,1.6202,0.08585,0.08319,-0.1322,0.0009,1.0000 13.750,1.6215,0.08893,0.08631,-0.1328,0.0008,1.0000 14.000,1.5931,0.09832,0.09599,-0.1349,0.0008,1.0000 14.250,1.5709,0.10704,0.10493,-0.1381,0.0009,1.0000