Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx63137-il-200000-n5 Airfoil,fx63137-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,85.1715 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-fx63137-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.2513,0.06200,0.05840,-0.1032,0.9344,0.0184 -9.500,-0.3218,0.03337,0.02864,-0.1426,0.9066,0.0181 -9.250,-0.2866,0.03087,0.02595,-0.1500,0.9007,0.0189 -9.000,-0.2465,0.02887,0.02372,-0.1566,0.8968,0.0202 -8.750,-0.2162,0.02648,0.02091,-0.1614,0.8885,0.0220 -8.500,-0.1777,0.02628,0.02072,-0.1646,0.8835,0.0233 -8.250,-0.1405,0.02431,0.01829,-0.1692,0.8779,0.0251 -8.000,-0.1092,0.02340,0.01725,-0.1712,0.8702,0.0258 -7.750,-0.0731,0.02246,0.01614,-0.1740,0.8647,0.0265 -7.500,-0.0423,0.02153,0.01502,-0.1757,0.8580,0.0272 -7.250,-0.0102,0.02058,0.01385,-0.1774,0.8516,0.0281 -7.000,0.0248,0.01964,0.01261,-0.1795,0.8466,0.0293 -6.750,0.0531,0.01915,0.01208,-0.1802,0.8399,0.0301 -6.500,0.0845,0.01861,0.01142,-0.1814,0.8342,0.0310 -6.250,0.1176,0.01806,0.01071,-0.1828,0.8290,0.0324 -6.000,0.1454,0.01757,0.01006,-0.1831,0.8214,0.0337 -5.750,0.1766,0.01705,0.00950,-0.1842,0.8150,0.0349 -5.500,0.2063,0.01658,0.00896,-0.1848,0.8087,0.0359 -5.250,0.2360,0.01612,0.00843,-0.1855,0.8025,0.0369 -5.000,0.2680,0.01567,0.00789,-0.1865,0.7975,0.0380 -4.750,0.2983,0.01529,0.00741,-0.1873,0.7919,0.0390 -4.500,0.3298,0.01481,0.00692,-0.1884,0.7858,0.0402 -4.250,0.3631,0.01443,0.00647,-0.1898,0.7804,0.0420 -4.000,0.3941,0.01412,0.00609,-0.1907,0.7743,0.0446 -3.750,0.4258,0.01382,0.00577,-0.1917,0.7682,0.0485 -3.500,0.4585,0.01359,0.00549,-0.1929,0.7631,0.0553 -3.250,0.4885,0.01341,0.00529,-0.1934,0.7568,0.0662 -3.000,0.5205,0.01315,0.00508,-0.1945,0.7508,0.0850 -2.750,0.5532,0.01294,0.00488,-0.1957,0.7455,0.1166 -2.500,0.5853,0.01260,0.00476,-0.1970,0.7386,0.1879 -2.250,0.6201,0.01219,0.00469,-0.1990,0.7325,0.3088 -2.000,0.6513,0.01208,0.00474,-0.1998,0.7265,0.3810 -1.750,0.6804,0.01209,0.00482,-0.2000,0.7198,0.4231 -1.500,0.7099,0.01215,0.00488,-0.2002,0.7142,0.4569 -1.250,0.7381,0.01224,0.00499,-0.2002,0.7078,0.4826 -1.000,0.7663,0.01232,0.00506,-0.2001,0.7007,0.5017 -0.750,0.7947,0.01240,0.00510,-0.2000,0.6943,0.5156 -0.500,0.8222,0.01249,0.00517,-0.1998,0.6864,0.5300 -0.250,0.8506,0.01258,0.00520,-0.1998,0.6795,0.5451 0.000,0.8777,0.01268,0.00530,-0.1995,0.6713,0.5581 0.250,0.9055,0.01277,0.00534,-0.1993,0.6642,0.5673 0.500,0.9328,0.01286,0.00541,-0.1992,0.6557,0.5758 0.750,0.9600,0.01294,0.00547,-0.1989,0.6472,0.5823 1.000,0.9865,0.01303,0.00556,-0.1986,0.6373,0.5897 1.250,1.0136,0.01313,0.00561,-0.1983,0.6279,0.5969 1.500,1.0400,0.01323,0.00571,-0.1979,0.6180,0.6037 1.750,1.0670,0.01336,0.00579,-0.1977,0.6088,0.6117 2.000,1.0933,0.01349,0.00592,-0.1973,0.5995,0.6182 2.250,1.1197,0.01363,0.00605,-0.1970,0.5900,0.6263 2.500,1.1457,0.01379,0.00620,-0.1966,0.5797,0.6333 2.750,1.1710,0.01394,0.00635,-0.1961,0.5667,0.6401 3.000,1.1959,0.01414,0.00648,-0.1955,0.5522,0.6474 3.250,1.2196,0.01436,0.00667,-0.1946,0.5365,0.6536 3.500,1.2432,0.01461,0.00687,-0.1938,0.5194,0.6612 3.750,1.2665,0.01487,0.00710,-0.1929,0.5019,0.6686 4.000,1.2894,0.01517,0.00735,-0.1920,0.4860,0.6772 4.250,1.3122,0.01548,0.00763,-0.1911,0.4719,0.6857 4.500,1.3351,0.01579,0.00793,-0.1902,0.4586,0.6952 4.750,1.3576,0.01610,0.00826,-0.1893,0.4443,0.7046 5.250,1.4008,0.01681,0.00896,-0.1871,0.4183,0.7259 5.500,1.4216,0.01720,0.00936,-0.1859,0.4063,0.7369 5.750,1.4416,0.01761,0.00977,-0.1846,0.3935,0.7493 6.000,1.4608,0.01801,0.01020,-0.1831,0.3785,0.7625 6.250,1.4779,0.01847,0.01067,-0.1812,0.3630,0.7775 6.500,1.4917,0.01901,0.01119,-0.1788,0.3494,0.7947 6.750,1.5049,0.01953,0.01172,-0.1763,0.3343,0.8149 7.000,1.5169,0.02000,0.01225,-0.1735,0.3166,0.8422 7.500,1.5272,0.02128,0.01350,-0.1658,0.2844,1.0000 7.750,1.5403,0.02213,0.01430,-0.1638,0.2662,1.0000 8.000,1.5518,0.02307,0.01520,-0.1617,0.2462,1.0000 8.250,1.5607,0.02420,0.01625,-0.1592,0.2322,1.0000 8.500,1.5709,0.02530,0.01733,-0.1571,0.2207,1.0000 8.750,1.5825,0.02636,0.01841,-0.1552,0.2055,1.0000 9.000,1.5902,0.02771,0.01972,-0.1530,0.1887,1.0000 9.250,1.5964,0.02923,0.02118,-0.1508,0.1767,1.0000 9.500,1.6032,0.03078,0.02272,-0.1487,0.1660,1.0000 9.750,1.6131,0.03214,0.02413,-0.1471,0.1492,1.0000 10.000,1.6167,0.03407,0.02600,-0.1450,0.1360,1.0000 10.250,1.6203,0.03609,0.02798,-0.1432,0.1275,1.0000 10.500,1.6286,0.03775,0.02973,-0.1417,0.1176,1.0000 10.750,1.6345,0.03969,0.03170,-0.1402,0.1056,1.0000 11.000,1.6370,0.04201,0.03401,-0.1387,0.0977,1.0000 11.250,1.6391,0.04446,0.03645,-0.1373,0.0926,1.0000 11.500,1.6431,0.04677,0.03883,-0.1360,0.0880,1.0000 11.750,1.6464,0.04924,0.04138,-0.1349,0.0835,1.0000 12.000,1.6467,0.05211,0.04430,-0.1339,0.0797,1.0000 12.250,1.6538,0.05428,0.04660,-0.1331,0.0759,1.0000 12.500,1.6585,0.05680,0.04920,-0.1324,0.0716,1.0000 12.750,1.6608,0.05965,0.05211,-0.1318,0.0683,1.0000 13.000,1.6638,0.06250,0.05504,-0.1312,0.0659,1.0000 13.250,1.6653,0.06559,0.05818,-0.1309,0.0634,1.0000 13.500,1.6653,0.06897,0.06162,-0.1306,0.0613,1.0000 13.750,1.6649,0.07251,0.06522,-0.1305,0.0592,1.0000 14.000,1.6668,0.07578,0.06862,-0.1304,0.0578,1.0000 14.250,1.6678,0.07924,0.07220,-0.1305,0.0563,1.0000 14.500,1.6676,0.08293,0.07599,-0.1307,0.0548,1.0000 14.750,1.6660,0.08690,0.08007,-0.1311,0.0534,1.0000 15.000,1.6628,0.09119,0.08444,-0.1317,0.0519,1.0000