Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e63-il-500000-n5 Airfoil,e63-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,159.982 Max Cl/Cd alpha,1 Url,http://airfoiltools.com/polar/csv?polar=xf-e63-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.000,-0.2521,0.09042,0.08811,-0.0460,0.9843,0.0066 -6.750,-0.2488,0.08807,0.08578,-0.0460,0.9793,0.0066 -6.500,-0.2360,0.08508,0.08281,-0.0487,0.9761,0.0068 -6.250,-0.2148,0.08135,0.07908,-0.0536,0.9742,0.0071 -6.000,-0.2003,0.07811,0.07584,-0.0567,0.9701,0.0074 -5.750,-0.1822,0.07475,0.07249,-0.0607,0.9661,0.0075 -5.500,-0.1560,0.07095,0.06868,-0.0668,0.9637,0.0081 -5.250,-0.1259,0.06697,0.06469,-0.0739,0.9621,0.0083 -5.000,-0.1072,0.06383,0.06155,-0.0776,0.9561,0.0087 -4.750,-0.0728,0.05986,0.05755,-0.0855,0.9533,0.0090 -4.500,-0.0309,0.05559,0.05324,-0.0951,0.9516,0.0093 -4.250,0.0117,0.05122,0.04880,-0.1040,0.9505,0.0094 -3.750,0.0902,0.04300,0.04044,-0.1188,0.9438,0.0096 -3.500,0.1391,0.03839,0.03573,-0.1278,0.9422,0.0096 -3.250,0.1911,0.03373,0.03092,-0.1367,0.9412,0.0097 -3.000,0.2438,0.02919,0.02618,-0.1449,0.9407,0.0097 -2.500,0.3619,0.01835,0.01450,-0.1635,0.9415,0.0062 -2.250,0.4181,0.01401,0.00945,-0.1695,0.9425,0.0048 -2.000,0.4592,0.01224,0.00727,-0.1723,0.9417,0.0046 -1.750,0.4973,0.01096,0.00570,-0.1744,0.9407,0.0049 -1.500,0.5339,0.01011,0.00471,-0.1763,0.9392,0.0056 -1.250,0.5698,0.00957,0.00411,-0.1780,0.9373,0.0077 -1.000,0.5976,0.00921,0.00371,-0.1779,0.9309,0.0091 -0.750,0.6318,0.00873,0.00315,-0.1791,0.9270,0.0094 -0.500,0.6680,0.00833,0.00265,-0.1808,0.9235,0.0102 -0.250,0.7010,0.00778,0.00246,-0.1821,0.9159,0.1582 0.000,0.7417,0.00712,0.00238,-0.1853,0.9114,0.4129 0.250,0.7795,0.00666,0.00233,-0.1876,0.9018,0.5986 0.500,0.8184,0.00597,0.00220,-0.1899,0.8899,0.8571 0.750,0.8624,0.00566,0.00190,-0.1933,0.8725,1.0000 1.000,0.9071,0.00567,0.00174,-0.1970,0.8411,1.0000 1.250,0.9402,0.00589,0.00173,-0.1979,0.7989,1.0000 1.500,0.9658,0.00621,0.00181,-0.1973,0.7540,1.0000 1.750,0.9882,0.00662,0.00199,-0.1960,0.7045,1.0000 2.000,1.0091,0.00709,0.00218,-0.1944,0.6504,1.0000 2.250,1.0297,0.00761,0.00241,-0.1928,0.5929,1.0000 2.500,1.0500,0.00820,0.00267,-0.1912,0.5281,1.0000 2.750,1.0663,0.00929,0.00310,-0.1890,0.4027,1.0000 3.000,1.0850,0.01039,0.00356,-0.1875,0.2842,1.0000 3.250,1.1062,0.01124,0.00403,-0.1865,0.2014,1.0000 3.500,1.1286,0.01196,0.00444,-0.1856,0.1400,1.0000 3.750,1.1513,0.01264,0.00486,-0.1847,0.0904,1.0000 4.000,1.1741,0.01331,0.00533,-0.1839,0.0498,1.0000 4.250,1.1963,0.01412,0.00592,-0.1829,0.0145,1.0000 4.500,1.2206,0.01454,0.00636,-0.1822,0.0121,1.0000 4.750,1.2451,0.01495,0.00688,-0.1815,0.0110,1.0000 5.000,1.2692,0.01541,0.00742,-0.1807,0.0100,1.0000 5.250,1.2928,0.01598,0.00809,-0.1798,0.0091,1.0000 5.500,1.3147,0.01685,0.00913,-0.1786,0.0079,1.0000 5.750,1.3359,0.01779,0.01020,-0.1772,0.0075,1.0000 6.000,1.3575,0.01862,0.01115,-0.1759,0.0074,1.0000 6.250,1.3781,0.01961,0.01226,-0.1745,0.0073,1.0000 6.500,1.3980,0.02077,0.01356,-0.1729,0.0072,1.0000 6.750,1.4174,0.02210,0.01505,-0.1712,0.0071,1.0000 7.000,1.4365,0.02369,0.01689,-0.1695,0.0071,1.0000 7.250,1.4564,0.02528,0.01866,-0.1680,0.0070,1.0000 7.500,1.4771,0.02650,0.02004,-0.1667,0.0066,1.0000 7.750,1.4974,0.02769,0.02140,-0.1654,0.0061,1.0000 8.000,1.5174,0.02867,0.02252,-0.1641,0.0054,1.0000 8.250,1.5374,0.02906,0.02300,-0.1631,0.0045,1.0000 8.500,1.5564,0.02969,0.02372,-0.1618,0.0040,1.0000 8.750,1.5734,0.03063,0.02476,-0.1604,0.0035,1.0000 9.000,1.5839,0.03353,0.02798,-0.1576,0.0030,1.0000 9.250,1.6028,0.03418,0.02881,-0.1562,0.0025,1.0000 9.500,1.6132,0.03688,0.03190,-0.1533,0.0020,1.0000 9.750,1.6225,0.03907,0.03438,-0.1505,0.0016,1.0000 10.000,1.6295,0.04097,0.03650,-0.1475,0.0014,1.0000 10.250,1.6342,0.04235,0.03805,-0.1441,0.0013,1.0000 10.500,1.6329,0.04471,0.04065,-0.1399,0.0013,1.0000 10.750,1.6228,0.04842,0.04471,-0.1349,0.0013,1.0000 11.000,1.6101,0.05230,0.04893,-0.1302,0.0012,1.0000 11.250,1.6035,0.05515,0.05198,-0.1269,0.0012,1.0000 11.500,1.5814,0.06041,0.05756,-0.1229,0.0011,1.0000 11.750,1.5592,0.06615,0.06362,-0.1202,0.0012,1.0000 12.000,1.5363,0.07225,0.06998,-0.1191,0.0011,1.0000 12.250,1.5093,0.07989,0.07789,-0.1196,0.0012,1.0000 12.500,1.4893,0.08700,0.08519,-0.1220,0.0011,1.0000 12.750,1.4645,0.09645,0.09485,-0.1266,0.0012,1.0000 13.000,1.4342,0.10936,0.10798,-0.1348,0.0012,1.0000