Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-dae11-il-50000 Airfoil,dae11-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,6.38902 Max Cl/Cd alpha,7 Url,http://www.airfoiltools.com/polar/csv?polar=xf-dae11-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.3113,0.14249,0.13712,-0.0320,0.9845,0.1373 -8.500,-0.3320,0.14335,0.13807,-0.0308,0.9850,0.1387 -8.250,-0.3553,0.14422,0.13903,-0.0288,0.9862,0.1392 -8.000,-0.3200,0.13641,0.13117,-0.0293,0.9831,0.1451 -7.750,-0.3256,0.13500,0.12980,-0.0276,0.9837,0.1489 -7.500,-0.3480,0.13477,0.12966,-0.0229,0.9876,0.1507 -7.250,-0.3724,0.13472,0.12970,-0.0180,0.9934,0.1520 -7.000,-0.4022,0.13473,0.12983,-0.0116,1.0000,0.1526 -6.750,-0.4224,0.13467,0.12983,-0.0106,1.0000,0.1545 -6.500,-0.4469,0.13488,0.13012,-0.0091,1.0000,0.1553 -6.250,-0.4695,0.13505,0.13036,-0.0112,1.0000,0.1560 -6.000,-0.4341,0.12745,0.12275,-0.0058,1.0000,0.1647 -5.750,-0.4488,0.12631,0.12165,-0.0045,1.0000,0.1687 -5.500,-0.4674,0.12586,0.12126,-0.0070,1.0000,0.1718 -5.250,-0.4698,0.12257,0.11802,-0.0067,1.0000,0.1744 -5.000,-0.4631,0.11932,0.11478,-0.0029,1.0000,0.1803 -4.750,-0.4693,0.11761,0.11308,-0.0055,1.0000,0.1874 -4.500,-0.4707,0.11462,0.11012,-0.0077,1.0000,0.1914 -4.250,-0.4668,0.11168,0.10721,-0.0041,1.0000,0.1972 -4.000,-0.4629,0.10931,0.10481,-0.0121,1.0000,0.2074 -3.750,-0.4610,0.10613,0.10168,-0.0066,1.0000,0.2122 -3.500,-0.4516,0.10336,0.09887,-0.0125,1.0000,0.2249 -3.250,-0.4402,0.10112,0.09658,-0.0155,1.0000,0.2398 -3.000,-0.4392,0.09761,0.09315,-0.0109,1.0000,0.2450 -2.750,-0.4277,0.09488,0.09039,-0.0134,1.0000,0.2604 -2.500,-0.4168,0.09222,0.08771,-0.0145,1.0000,0.2773 -2.250,-0.4073,0.08968,0.08518,-0.0142,1.0000,0.2951 -2.000,-0.3993,0.08734,0.08286,-0.0129,1.0000,0.3151 -1.750,-0.3878,0.08510,0.08062,-0.0133,1.0000,0.3456 -1.000,-0.3717,0.07887,0.07451,-0.0046,1.0000,0.4480 0.000,-0.1668,0.06816,0.06281,-0.0497,0.9939,0.3968 0.250,-0.1965,0.06799,0.06312,-0.0325,0.9873,0.5151 0.500,-0.2468,0.06682,0.06238,-0.0083,0.9822,0.6359 0.750,0.0785,0.06028,0.05079,-0.0896,0.9744,0.1487 1.000,0.1134,0.06073,0.05078,-0.0916,0.9656,0.1528 1.250,0.1532,0.06191,0.05173,-0.0945,0.9586,0.1656 1.500,0.1846,0.06250,0.05209,-0.0960,0.9469,0.1809 1.750,0.2161,0.06343,0.05293,-0.0976,0.9378,0.2107 2.000,0.2582,0.06415,0.05435,-0.1008,0.9307,0.3388 2.250,0.2803,0.06323,0.05457,-0.0997,0.9183,1.0000 2.500,0.3053,0.06514,0.05604,-0.1007,0.9065,1.0000 2.750,0.3425,0.06832,0.05880,-0.1036,0.8974,1.0000 3.000,0.3612,0.06955,0.05981,-0.1037,0.8835,1.0000 3.250,0.3784,0.07095,0.06101,-0.1035,0.8706,1.0000 3.500,0.3975,0.07275,0.06263,-0.1038,0.8597,1.0000 3.750,0.4331,0.07599,0.06564,-0.1064,0.8510,1.0000 4.000,0.4444,0.07694,0.06648,-0.1055,0.8379,1.0000 4.250,0.4585,0.07854,0.06798,-0.1051,0.8269,1.0000 4.500,0.4951,0.08212,0.07139,-0.1079,0.8194,1.0000 4.750,0.5017,0.08285,0.07207,-0.1065,0.8066,1.0000 5.000,0.5141,0.08459,0.07374,-0.1060,0.7965,1.0000 5.250,0.5474,0.08790,0.07694,-0.1082,0.7882,1.0000 5.500,0.5513,0.08880,0.07783,-0.1067,0.7764,1.0000 5.750,0.5717,0.09152,0.08049,-0.1075,0.7692,1.0000 6.000,0.5904,0.09352,0.08246,-0.1078,0.7578,1.0000 6.250,0.5970,0.09520,0.08413,-0.1070,0.7482,1.0000 6.500,0.6295,0.09867,0.08755,-0.1090,0.7402,1.0000 6.750,0.6286,0.09968,0.08859,-0.1074,0.7293,1.0000 7.000,0.6635,0.10385,0.09272,-0.1097,0.7230,1.0000 7.250,0.6610,0.10448,0.09340,-0.1080,0.7110,1.0000 7.500,0.6751,0.10725,0.09617,-0.1084,0.7042,1.0000 7.750,0.6930,0.10957,0.09851,-0.1088,0.6935,1.0000 8.000,0.6969,0.11164,0.10063,-0.1082,0.6850,1.0000 8.250,0.7255,0.11503,0.10405,-0.1097,0.6763,1.0000 8.500,0.7225,0.11653,0.10559,-0.1086,0.6665,1.0000 8.750,0.7589,0.12100,0.11010,-0.1108,0.6596,1.0000 9.000,0.7493,0.12173,0.11088,-0.1093,0.6488,1.0000 9.250,0.7673,0.12515,0.11437,-0.1101,0.6423,1.0000 9.500,0.7780,0.12728,0.11657,-0.1102,0.6314,1.0000 9.750,0.7818,0.12976,0.11911,-0.1101,0.6234,1.0000 10.000,0.8107,0.13354,0.12296,-0.1115,0.6143,1.0000 10.250,0.8046,0.13506,0.12455,-0.1109,0.6046,1.0000 10.500,0.8251,0.13879,0.12837,-0.1119,0.5976,1.0000