Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e49-il-50000 Airfoil,e49-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,37.4986 Max Cl/Cd alpha,7.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e49-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.4056,0.13285,0.12668,-0.0153,1.0000,0.0966 -8.250,-0.4173,0.13262,0.12654,-0.0146,1.0000,0.0975 -8.000,-0.4308,0.13256,0.12659,-0.0139,1.0000,0.0979 -7.750,-0.4079,0.12466,0.11860,-0.0121,1.0000,0.1041 -7.500,-0.4132,0.12283,0.11683,-0.0107,1.0000,0.1077 -7.250,-0.4219,0.12191,0.11601,-0.0107,1.0000,0.1106 -7.000,-0.4275,0.12166,0.11585,-0.0147,1.0000,0.1121 -6.750,-0.4193,0.11566,0.10987,-0.0097,1.0000,0.1167 -6.500,-0.4172,0.11306,0.10731,-0.0096,1.0000,0.1216 -6.250,-0.4145,0.11188,0.10619,-0.0152,1.0000,0.1258 -6.000,-0.4104,0.10777,0.10214,-0.0138,1.0000,0.1286 -5.750,-0.4052,0.10448,0.09888,-0.0122,1.0000,0.1350 -5.500,-0.3895,0.10232,0.09673,-0.0215,1.0000,0.1412 -5.250,-0.3891,0.09828,0.09274,-0.0156,1.0000,0.1465 -5.000,-0.3693,0.09541,0.08986,-0.0235,1.0000,0.1559 -4.750,-0.3654,0.09200,0.08649,-0.0200,1.0000,0.1636 -4.500,-0.3497,0.08866,0.08315,-0.0234,1.0000,0.1733 -4.250,-0.3316,0.08535,0.07984,-0.0268,1.0000,0.1866 -4.000,-0.3133,0.08220,0.07667,-0.0296,1.0000,0.2007 -3.750,-0.2827,0.07943,0.07375,-0.0365,1.0000,0.2252 -3.500,-0.2684,0.07604,0.07040,-0.0368,1.0000,0.2414 -3.250,-0.2580,0.07314,0.06754,-0.0351,1.0000,0.2612 -3.000,-0.2356,0.07037,0.06475,-0.0378,1.0000,0.2984 -2.750,-0.2209,0.06796,0.06235,-0.0373,1.0000,0.3367 -2.500,-0.2129,0.06520,0.05966,-0.0342,1.0000,0.3732 -1.250,0.0672,0.05107,0.04418,-0.0853,1.0000,0.3410 -0.750,0.2283,0.04552,0.03599,-0.1087,1.0000,0.1376 -0.500,0.2622,0.04476,0.03476,-0.1103,1.0000,0.1322 -0.250,0.2942,0.04453,0.03389,-0.1111,1.0000,0.1264 0.000,0.3234,0.04438,0.03345,-0.1117,1.0000,0.1257 0.250,0.3497,0.04446,0.03323,-0.1116,1.0000,0.1275 0.500,0.3757,0.04472,0.03334,-0.1117,1.0000,0.1331 0.750,0.4023,0.04519,0.03368,-0.1120,1.0000,0.1471 1.000,0.4311,0.04575,0.03440,-0.1130,1.0000,0.1902 1.250,0.4561,0.04474,0.03496,-0.1128,1.0000,1.0000 1.500,0.4746,0.04591,0.03564,-0.1121,1.0000,1.0000 1.750,0.4922,0.04715,0.03662,-0.1117,1.0000,1.0000 2.000,0.5092,0.04845,0.03772,-0.1114,1.0000,1.0000 2.250,0.5257,0.04981,0.03893,-0.1112,1.0000,1.0000 2.500,0.5417,0.05125,0.04026,-0.1110,1.0000,1.0000 2.750,0.5572,0.05276,0.04170,-0.1108,1.0000,1.0000 3.000,0.5722,0.05435,0.04325,-0.1107,1.0000,1.0000 3.250,0.5866,0.05604,0.04491,-0.1106,1.0000,1.0000 3.500,0.6122,0.05837,0.04724,-0.1129,0.9928,1.0000 3.750,0.6973,0.06105,0.04993,-0.1247,0.9359,1.0000 4.000,0.7455,0.06179,0.05071,-0.1292,0.9066,1.0000 4.250,0.7841,0.06238,0.05138,-0.1320,0.8831,1.0000 4.500,0.8217,0.06287,0.05204,-0.1345,0.8614,1.0000 4.750,0.8661,0.06313,0.05244,-0.1377,0.8417,1.0000 5.000,0.8988,0.06329,0.05277,-0.1391,0.8194,1.0000 5.250,0.9524,0.06273,0.05252,-0.1428,0.8009,1.0000 5.500,0.9864,0.06232,0.05234,-0.1436,0.7771,1.0000 5.750,1.0276,0.06134,0.05165,-0.1448,0.7542,1.0000 6.000,1.0853,0.05889,0.04959,-0.1471,0.7338,1.0000 6.250,1.1264,0.05714,0.04831,-0.1472,0.7091,1.0000 6.500,1.1845,0.05353,0.04523,-0.1482,0.6873,1.0000 6.750,1.2604,0.04753,0.03993,-0.1498,0.6651,1.0000 7.000,1.3564,0.03901,0.03232,-0.1518,0.6174,1.0000 7.250,1.3672,0.03646,0.02954,-0.1437,0.5325,1.0000 7.500,1.3538,0.03732,0.02967,-0.1352,0.4364,1.0000 7.750,1.3417,0.03946,0.03127,-0.1286,0.3507,1.0000 8.000,1.3221,0.04281,0.03389,-0.1220,0.2430,1.0000 8.250,1.3016,0.04765,0.03752,-0.1165,0.1342,1.0000 8.500,1.2998,0.05142,0.04081,-0.1129,0.0973,1.0000 8.750,1.3099,0.05433,0.04354,-0.1104,0.0825,1.0000 9.000,1.3578,0.05646,0.04571,-0.1112,0.0698,1.0000 9.250,1.4605,0.06121,0.05057,-0.1197,0.0583,1.0000 9.500,1.5087,0.06688,0.05694,-0.1220,0.0579,1.0000 9.750,1.5333,0.07275,0.06335,-0.1217,0.0582,1.0000 10.000,1.5347,0.07669,0.06782,-0.1181,0.0589,1.0000 10.250,1.5208,0.07969,0.07136,-0.1126,0.0597,1.0000 10.500,1.4981,0.08317,0.07538,-0.1068,0.0607,1.0000 10.750,1.4737,0.08726,0.07995,-0.1019,0.0616,1.0000 11.000,1.4491,0.09176,0.08486,-0.0979,0.0625,1.0000 11.250,1.4243,0.09660,0.09005,-0.0948,0.0633,1.0000 11.500,1.3990,0.10175,0.09551,-0.0928,0.0640,1.0000 11.750,1.3732,0.10726,0.10129,-0.0919,0.0647,1.0000 12.000,1.3475,0.11322,0.10748,-0.0921,0.0654,1.0000