Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e58-il-1000000 Airfoil,e58-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,235.693 Max Cl/Cd alpha,1.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e58-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.0921,0.08863,0.08680,-0.1013,0.9675,0.0085 -8.250,-0.0828,0.08597,0.08414,-0.1028,0.9651,0.0088 -8.000,-0.0684,0.08293,0.08111,-0.1062,0.9632,0.0105 -7.750,-0.0531,0.07998,0.07816,-0.1102,0.9618,0.0107 -7.500,-0.0372,0.07670,0.07488,-0.1138,0.9607,0.0107 -7.250,-0.0202,0.07329,0.07147,-0.1178,0.9597,0.0108 -7.000,0.0010,0.06962,0.06779,-0.1229,0.9589,0.0108 -6.250,0.0310,0.05898,0.05717,-0.1317,0.9481,0.0113 -6.000,0.0602,0.05546,0.05364,-0.1384,0.9474,0.0115 -5.750,0.0931,0.05188,0.05004,-0.1460,0.9468,0.0119 -5.500,0.1288,0.04821,0.04634,-0.1543,0.9462,0.0130 -5.250,0.1734,0.04298,0.04105,-0.1664,0.9454,0.0140 -5.000,0.3062,0.01222,0.00830,-0.2157,0.9428,0.0117 -4.750,0.3291,0.01232,0.00842,-0.2148,0.9402,0.0126 -4.500,0.3604,0.01194,0.00794,-0.2157,0.9390,0.0139 -4.250,0.3956,0.01124,0.00710,-0.2174,0.9380,0.0153 -4.000,0.4338,0.00998,0.00564,-0.2200,0.9372,0.0171 -3.750,0.4675,0.00966,0.00531,-0.2213,0.9360,0.0189 -3.500,0.4999,0.00949,0.00511,-0.2222,0.9350,0.0214 -3.250,0.5334,0.00930,0.00488,-0.2234,0.9339,0.0230 -3.000,0.5703,0.00825,0.00371,-0.2256,0.9328,0.0264 -2.750,0.5983,0.00801,0.00346,-0.2257,0.9305,0.0290 -2.500,0.6250,0.00777,0.00319,-0.2255,0.9274,0.0308 -2.250,0.6550,0.00748,0.00287,-0.2259,0.9250,0.0326 -2.000,0.6860,0.00728,0.00265,-0.2266,0.9230,0.0341 -1.750,0.7186,0.00695,0.00226,-0.2276,0.9211,0.0359 -1.500,0.7507,0.00674,0.00200,-0.2285,0.9191,0.0375 -1.250,0.7757,0.00664,0.00189,-0.2278,0.9152,0.0390 -1.000,0.8040,0.00651,0.00175,-0.2278,0.9119,0.0427 -0.750,0.8353,0.00619,0.00165,-0.2287,0.9089,0.1249 -0.500,0.8665,0.00605,0.00156,-0.2293,0.9058,0.1535 -0.250,0.8911,0.00600,0.00155,-0.2286,0.9004,0.1666 0.000,0.9192,0.00590,0.00150,-0.2286,0.8959,0.1811 0.250,0.9492,0.00579,0.00145,-0.2291,0.8918,0.2078 0.500,0.9758,0.00565,0.00151,-0.2289,0.8864,0.2869 0.750,1.0063,0.00535,0.00157,-0.2297,0.8809,0.4641 1.000,1.0349,0.00496,0.00170,-0.2300,0.8697,0.7210 1.250,1.0555,0.00462,0.00174,-0.2281,0.8557,0.9172 1.500,1.0799,0.00459,0.00171,-0.2272,0.8409,1.0000 1.750,1.1054,0.00469,0.00172,-0.2265,0.8162,1.0000 2.000,1.1245,0.00509,0.00180,-0.2244,0.7529,1.0000 2.250,1.1322,0.00606,0.00221,-0.2199,0.6477,1.0000 2.500,1.1458,0.00687,0.00261,-0.2169,0.5701,1.0000 2.750,1.1581,0.00788,0.00308,-0.2139,0.4608,1.0000 3.000,1.1759,0.00864,0.00348,-0.2120,0.3911,1.0000 3.250,1.1955,0.00933,0.00382,-0.2105,0.3206,1.0000 3.500,1.2146,0.01011,0.00424,-0.2089,0.2553,1.0000 3.750,1.2350,0.01079,0.00462,-0.2076,0.1941,1.0000 4.000,1.2563,0.01140,0.00503,-0.2065,0.1564,1.0000 4.250,1.2791,0.01184,0.00536,-0.2056,0.1309,1.0000 4.500,1.2973,0.01285,0.00598,-0.2039,0.0598,1.0000 4.750,1.3169,0.01375,0.00660,-0.2024,0.0174,1.0000 5.000,1.3395,0.01428,0.00716,-0.2013,0.0128,1.0000 5.250,1.3624,0.01474,0.00769,-0.2003,0.0118,1.0000 5.500,1.3850,0.01521,0.00822,-0.1992,0.0109,1.0000 5.750,1.4072,0.01574,0.00879,-0.1981,0.0097,1.0000 6.000,1.4284,0.01638,0.00948,-0.1969,0.0087,1.0000 6.250,1.4464,0.01749,0.01071,-0.1949,0.0078,1.0000 6.500,1.4619,0.01882,0.01217,-0.1925,0.0074,1.0000 6.750,1.4816,0.01943,0.01286,-0.1909,0.0072,1.0000 7.000,1.5006,0.02009,0.01358,-0.1892,0.0068,1.0000 7.250,1.5179,0.02095,0.01451,-0.1872,0.0064,1.0000 7.500,1.5340,0.02198,0.01562,-0.1850,0.0060,1.0000 7.750,1.5500,0.02310,0.01683,-0.1828,0.0057,1.0000 8.000,1.5665,0.02410,0.01790,-0.1808,0.0054,1.0000 8.250,1.5826,0.02505,0.01891,-0.1789,0.0051,1.0000 8.500,1.5974,0.02637,0.02032,-0.1767,0.0049,1.0000 8.750,1.6121,0.02857,0.02264,-0.1746,0.0046,1.0000 9.000,1.6328,0.03181,0.02610,-0.1736,0.0045,1.0000 9.250,1.6579,0.03685,0.03151,-0.1736,0.0044,1.0000 9.500,1.6620,0.03751,0.03234,-0.1694,0.0043,1.0000 9.750,1.6684,0.03825,0.03321,-0.1658,0.0042,1.0000 10.000,1.6745,0.04048,0.03566,-0.1624,0.0041,1.0000 10.250,1.6783,0.04266,0.03806,-0.1586,0.0039,1.0000 10.500,1.6780,0.04557,0.04123,-0.1546,0.0038,1.0000 10.750,1.6736,0.04883,0.04475,-0.1501,0.0037,1.0000 11.000,1.6636,0.05271,0.04894,-0.1453,0.0036,1.0000 11.250,1.6502,0.05692,0.05344,-0.1406,0.0035,1.0000 11.500,1.6279,0.06240,0.05923,-0.1359,0.0036,1.0000 11.750,1.6066,0.06772,0.06483,-0.1320,0.0036,1.0000 12.000,1.5791,0.07425,0.07165,-0.1288,0.0036,1.0000 12.250,1.5541,0.08063,0.07826,-0.1271,0.0036,1.0000 12.500,1.5298,0.08730,0.08513,-0.1268,0.0037,1.0000