Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e63-il-200000-n5 Airfoil,e63-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,110.041 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-e63-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.3714,0.11498,0.11161,-0.0175,1.0000,0.0125 -7.500,-0.3722,0.11289,0.10956,-0.0166,1.0000,0.0126 -7.250,-0.3744,0.11098,0.10769,-0.0154,1.0000,0.0126 -7.000,-0.3641,0.10791,0.10464,-0.0177,0.9978,0.0126 -6.750,-0.3484,0.10439,0.10106,-0.0215,0.9950,0.0126 -6.500,-0.3313,0.10064,0.09731,-0.0255,0.9918,0.0126 -6.250,-0.3123,0.09680,0.09348,-0.0299,0.9883,0.0126 -6.000,-0.2900,0.09268,0.08935,-0.0352,0.9851,0.0126 -5.750,-0.2670,0.08864,0.08530,-0.0406,0.9822,0.0127 -5.500,-0.2474,0.08485,0.08151,-0.0449,0.9777,0.0127 -5.250,-0.2215,0.08067,0.07732,-0.0509,0.9744,0.0127 -5.000,-0.1978,0.07460,0.07127,-0.0575,0.9721,0.0131 -4.750,-0.1810,0.07037,0.06705,-0.0607,0.9671,0.0135 -4.500,-0.1577,0.06642,0.06308,-0.0646,0.9638,0.0139 -4.250,-0.1254,0.06225,0.05889,-0.0711,0.9615,0.0144 -4.000,-0.0901,0.05807,0.05466,-0.0784,0.9588,0.0149 -3.750,-0.0542,0.05390,0.05043,-0.0856,0.9544,0.0152 -3.500,-0.0058,0.04907,0.04551,-0.0956,0.9522,0.0153 -3.250,0.0675,0.04220,0.03840,-0.1114,0.9518,0.0137 -3.000,0.1139,0.03842,0.03445,-0.1184,0.9507,0.0115 -2.750,0.1741,0.03311,0.02881,-0.1291,0.9507,0.0104 -2.500,0.2365,0.02805,0.02334,-0.1387,0.9514,0.0096 -2.250,0.2961,0.02363,0.01836,-0.1466,0.9526,0.0092 -2.000,0.3502,0.02020,0.01427,-0.1524,0.9541,0.0094 -1.750,0.3943,0.01825,0.01176,-0.1556,0.9536,0.0113 -1.500,0.4347,0.01673,0.00987,-0.1584,0.9525,0.0152 -1.250,0.4738,0.01557,0.00850,-0.1606,0.9510,0.0160 -1.000,0.5130,0.01473,0.00754,-0.1630,0.9493,0.0179 -0.750,0.5500,0.01419,0.00683,-0.1648,0.9468,0.0233 -0.500,0.5833,0.01358,0.00640,-0.1661,0.9419,0.0961 -0.250,0.6218,0.01277,0.00639,-0.1690,0.9390,0.3824 0.000,0.6574,0.01194,0.00637,-0.1706,0.9364,0.7202 0.250,0.6763,0.01139,0.00605,-0.1681,0.9276,1.0000 0.500,0.7124,0.01121,0.00577,-0.1696,0.9233,1.0000 0.750,0.7416,0.01112,0.00562,-0.1697,0.9146,1.0000 1.000,0.7774,0.01089,0.00531,-0.1711,0.9095,1.0000 1.250,0.8061,0.01080,0.00519,-0.1711,0.8992,1.0000 1.500,0.8379,0.01065,0.00502,-0.1717,0.8886,1.0000 1.750,0.8723,0.01044,0.00481,-0.1727,0.8773,1.0000 2.000,0.9092,0.01021,0.00463,-0.1743,0.8641,1.0000 2.250,0.9524,0.00992,0.00433,-0.1772,0.8461,1.0000 2.500,1.0035,0.00966,0.00404,-0.1819,0.8187,1.0000 2.750,1.0510,0.00960,0.00386,-0.1857,0.7762,1.0000 3.000,1.0861,0.00987,0.00390,-0.1869,0.7182,1.0000 3.250,1.1113,0.01039,0.00426,-0.1860,0.6522,1.0000 3.500,1.1313,0.01107,0.00461,-0.1841,0.5827,1.0000 3.750,1.1490,0.01186,0.00505,-0.1819,0.5094,1.0000 4.000,1.1664,0.01271,0.00556,-0.1798,0.4343,1.0000 4.250,1.1846,0.01358,0.00611,-0.1780,0.3635,1.0000 4.500,1.2033,0.01450,0.00672,-0.1764,0.2948,1.0000 4.750,1.2225,0.01547,0.00739,-0.1749,0.2271,1.0000 5.000,1.2423,0.01645,0.00821,-0.1736,0.1662,1.0000 5.250,1.2615,0.01758,0.00903,-0.1722,0.1069,1.0000 5.500,1.2809,0.01874,0.00995,-0.1709,0.0604,1.0000 5.750,1.2977,0.02036,0.01115,-0.1691,0.0151,1.0000 6.000,1.3163,0.02187,0.01274,-0.1672,0.0067,1.0000 6.250,1.3359,0.02316,0.01430,-0.1654,0.0055,1.0000 6.500,1.3540,0.02469,0.01609,-0.1634,0.0050,1.0000 6.750,1.3711,0.02649,0.01812,-0.1612,0.0046,1.0000 7.000,1.3883,0.02859,0.02045,-0.1590,0.0044,1.0000 7.250,1.4067,0.03102,0.02315,-0.1570,0.0042,1.0000 7.500,1.4260,0.03385,0.02632,-0.1552,0.0042,1.0000 7.750,1.4443,0.03713,0.03001,-0.1531,0.0041,1.0000 8.000,1.4595,0.04087,0.03425,-0.1506,0.0041,1.0000 8.250,1.4698,0.04508,0.03901,-0.1475,0.0042,1.0000 8.500,1.4745,0.04963,0.04410,-0.1438,0.0043,1.0000 8.750,1.4740,0.05432,0.04929,-0.1397,0.0044,1.0000 9.000,1.4667,0.05933,0.05477,-0.1350,0.0044,1.0000 9.250,1.4536,0.06380,0.05976,-0.1300,0.0045,1.0000 9.500,1.4361,0.06799,0.06425,-0.1250,0.0045,1.0000 9.750,1.4171,0.07243,0.06882,-0.1209,0.0046,1.0000 10.000,1.3974,0.07723,0.07386,-0.1179,0.0046,1.0000 10.250,1.3770,0.08247,0.07934,-0.1163,0.0046,1.0000 10.500,1.3548,0.08859,0.08568,-0.1164,0.0047,1.0000 10.750,1.3334,0.09537,0.09265,-0.1183,0.0047,1.0000