Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e58-il-100000-n5 Airfoil,e58-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,68.4181 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e58-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -6.750,-0.3067,0.10775,0.10318,-0.0343,0.9799,0.0295 -6.500,-0.3028,0.10526,0.10072,-0.0343,0.9769,0.0300 -6.250,-0.2998,0.10287,0.09836,-0.0345,0.9734,0.0305 -6.000,-0.2893,0.09993,0.09543,-0.0368,0.9704,0.0310 -5.750,-0.2805,0.09710,0.09262,-0.0386,0.9671,0.0315 -5.500,-0.2719,0.09415,0.08970,-0.0404,0.9629,0.0325 -5.250,-0.2564,0.09082,0.08637,-0.0441,0.9594,0.0331 -5.000,-0.2388,0.08733,0.08287,-0.0485,0.9561,0.0339 -4.750,-0.2247,0.08402,0.07958,-0.0518,0.9510,0.0347 -4.500,-0.1985,0.07993,0.07544,-0.0585,0.9472,0.0355 -4.250,-0.1337,0.07396,0.06933,-0.0790,0.9443,0.0380 -3.250,0.0335,0.05169,0.04659,-0.1138,0.9336,0.0267 -3.000,0.1204,0.04331,0.03775,-0.1332,0.9351,0.0266 -2.750,0.2066,0.03633,0.03007,-0.1505,0.9377,0.0308 -2.500,0.2908,0.03080,0.02336,-0.1647,0.9416,0.0345 -2.250,0.3432,0.02837,0.02015,-0.1706,0.9419,0.0407 -2.000,0.3789,0.02742,0.01887,-0.1727,0.9395,0.0477 -1.750,0.4162,0.02642,0.01758,-0.1749,0.9377,0.0538 -1.500,0.4511,0.02592,0.01693,-0.1766,0.9355,0.0603 -1.250,0.4867,0.02558,0.01648,-0.1784,0.9335,0.0690 -1.000,0.5235,0.02534,0.01610,-0.1803,0.9318,0.0750 -0.750,0.5558,0.02520,0.01597,-0.1815,0.9288,0.0896 -0.500,0.5830,0.02521,0.01606,-0.1816,0.9241,0.1407 -0.250,0.6151,0.02526,0.01610,-0.1827,0.9208,0.1874 0.000,0.6497,0.02529,0.01612,-0.1842,0.9183,0.2206 0.250,0.6765,0.02532,0.01623,-0.1843,0.9127,0.2561 0.500,0.7098,0.02511,0.01631,-0.1858,0.9079,0.3447 0.750,0.7393,0.02395,0.01633,-0.1856,0.9047,0.8435 1.000,0.7631,0.02389,0.01619,-0.1847,0.8957,1.0000 1.250,0.8007,0.02377,0.01595,-0.1864,0.8911,1.0000 1.500,0.8272,0.02378,0.01590,-0.1861,0.8822,1.0000 1.750,0.8649,0.02356,0.01563,-0.1877,0.8774,1.0000 2.000,0.8897,0.02359,0.01567,-0.1870,0.8678,1.0000 2.250,0.9291,0.02320,0.01528,-0.1888,0.8632,1.0000 2.500,0.9532,0.02317,0.01529,-0.1879,0.8523,1.0000 2.750,0.9800,0.02303,0.01524,-0.1874,0.8418,1.0000 3.000,1.0102,0.02272,0.01499,-0.1874,0.8321,1.0000 3.250,1.0436,0.02222,0.01459,-0.1878,0.8231,1.0000 3.500,1.0678,0.02208,0.01460,-0.1867,0.8101,1.0000 3.750,1.0918,0.02198,0.01462,-0.1856,0.7966,1.0000 4.250,1.1415,0.02173,0.01466,-0.1835,0.7635,1.0000 4.500,1.1682,0.02156,0.01468,-0.1828,0.7446,1.0000 4.750,1.2045,0.02075,0.01401,-0.1831,0.7152,1.0000 5.000,1.2683,0.01898,0.01219,-0.1877,0.6572,1.0000 5.250,1.3191,0.01928,0.01151,-0.1905,0.4837,1.0000 5.500,1.3295,0.02079,0.01237,-0.1871,0.3846,1.0000 5.750,1.3343,0.02270,0.01348,-0.1833,0.2665,1.0000 6.000,1.3428,0.02468,0.01474,-0.1803,0.1624,1.0000 6.250,1.3495,0.02716,0.01643,-0.1772,0.0548,1.0000 6.500,1.3628,0.02884,0.01797,-0.1746,0.0278,1.0000 6.750,1.3774,0.03030,0.01951,-0.1723,0.0220,1.0000 7.000,1.3905,0.03188,0.02136,-0.1697,0.0196,1.0000 7.250,1.4001,0.03378,0.02349,-0.1666,0.0182,1.0000 7.500,1.4092,0.03565,0.02559,-0.1635,0.0172,1.0000 7.750,1.4198,0.03744,0.02762,-0.1607,0.0160,1.0000 8.000,1.4306,0.03945,0.02984,-0.1580,0.0148,1.0000 8.250,1.4437,0.04173,0.03232,-0.1556,0.0143,1.0000 8.500,1.4622,0.04428,0.03509,-0.1539,0.0138,1.0000 8.750,1.4862,0.04726,0.03835,-0.1530,0.0133,1.0000 9.000,1.5108,0.05060,0.04204,-0.1523,0.0130,1.0000 9.250,1.5258,0.05385,0.04567,-0.1504,0.0123,1.0000 9.500,1.5316,0.05696,0.04912,-0.1476,0.0115,1.0000 9.750,1.5348,0.06047,0.05300,-0.1445,0.0112,1.0000 10.000,1.5329,0.06413,0.05711,-0.1411,0.0109,1.0000 10.250,1.5269,0.06809,0.06144,-0.1376,0.0107,1.0000 10.500,1.5177,0.07222,0.06595,-0.1339,0.0107,1.0000 10.750,1.5060,0.07648,0.07058,-0.1306,0.0107,1.0000 11.000,1.4928,0.08086,0.07532,-0.1277,0.0108,1.0000 11.250,1.4766,0.08574,0.08054,-0.1253,0.0108,1.0000 11.500,1.4591,0.09089,0.08600,-0.1237,0.0108,1.0000 11.750,1.4409,0.09645,0.09187,-0.1230,0.0109,1.0000 12.000,1.4222,0.10238,0.09809,-0.1233,0.0110,1.0000 12.250,1.4027,0.10893,0.10491,-0.1250,0.0111,1.0000 12.500,1.3833,0.11608,0.11229,-0.1279,0.0111,1.0000