Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64110-il-100000 Airfoil,n64110-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,41.6393 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-n64110-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.250,-0.5973,0.12572,0.12064,0.0047,1.0000,0.0995 -11.000,-0.5947,0.12194,0.11687,0.0030,1.0000,0.1042 -10.750,-0.6164,0.11782,0.11287,-0.0040,1.0000,0.1079 -10.500,-0.6061,0.11271,0.10777,-0.0035,1.0000,0.1104 -10.250,-0.5907,0.10951,0.10452,-0.0021,1.0000,0.1155 -10.000,-0.6087,0.10497,0.10010,-0.0079,1.0000,0.1213 -9.750,-0.6448,0.09885,0.09412,-0.0181,1.0000,0.1222 -9.500,-0.5931,0.09708,0.09221,-0.0077,1.0000,0.1308 -9.250,-0.6243,0.09121,0.08648,-0.0164,1.0000,0.1355 -9.000,-0.5984,0.08870,0.08394,-0.0116,1.0000,0.1436 -8.750,-0.6199,0.08300,0.07834,-0.0178,1.0000,0.1483 -8.500,-0.6136,0.07956,0.07494,-0.0170,1.0000,0.1570 -8.250,-0.6372,0.07446,0.06988,-0.0215,1.0000,0.1614 -7.750,-0.6451,0.06678,0.06220,-0.0229,1.0000,0.1836 -6.750,-0.6377,0.04256,0.03594,-0.0282,1.0000,0.1057 -6.500,-0.6185,0.03617,0.02862,-0.0262,1.0000,0.0765 -6.250,-0.6001,0.03232,0.02408,-0.0244,1.0000,0.0701 -6.000,-0.5790,0.03025,0.02145,-0.0226,1.0000,0.0682 -5.750,-0.5594,0.02774,0.01889,-0.0217,1.0000,0.0712 -5.500,-0.5386,0.02591,0.01688,-0.0204,1.0000,0.0731 -5.250,-0.5171,0.02413,0.01487,-0.0189,1.0000,0.0740 -5.000,-0.4961,0.02263,0.01324,-0.0174,1.0000,0.0760 -4.750,-0.4761,0.02152,0.01197,-0.0157,1.0000,0.0799 -4.500,-0.4583,0.02008,0.01067,-0.0141,1.0000,0.0860 -4.250,-0.4410,0.01910,0.00970,-0.0122,1.0000,0.0921 -4.000,-0.4257,0.01802,0.00873,-0.0102,1.0000,0.0999 -3.750,-0.4103,0.01713,0.00791,-0.0084,1.0000,0.1165 -3.500,-0.3946,0.01590,0.00694,-0.0068,1.0000,0.1548 -3.250,-0.3946,0.01340,0.00703,-0.0018,1.0000,0.6427 -3.000,-0.3834,0.01376,0.00745,0.0023,1.0000,0.7092 -2.750,-0.3718,0.01410,0.00781,0.0062,1.0000,0.7476 -2.500,-0.3618,0.01445,0.00815,0.0103,1.0000,0.7819 -2.250,-0.3599,0.01493,0.00869,0.0168,1.0000,0.8209 -2.000,-0.3456,0.01576,0.00958,0.0222,0.9909,0.8698 -1.750,-0.3106,0.01628,0.00998,0.0222,0.9829,0.8975 -1.500,-0.2686,0.01639,0.00993,0.0191,0.9745,0.9109 -1.250,-0.2180,0.01656,0.00992,0.0142,0.9682,0.9217 -1.000,-0.1700,0.01663,0.00986,0.0096,0.9606,0.9321 -0.750,-0.1115,0.01677,0.00988,0.0030,0.9559,0.9406 -0.500,-0.0588,0.01681,0.00983,-0.0026,0.9488,0.9484 -0.250,-0.0003,0.01687,0.00982,-0.0093,0.9437,0.9565 0.000,0.0653,0.01685,0.00978,-0.0174,0.9395,0.9610 0.250,0.1225,0.01680,0.00973,-0.0240,0.9332,0.9683 0.500,0.1863,0.01667,0.00962,-0.0316,0.9288,0.9736 0.750,0.2394,0.01656,0.00957,-0.0374,0.9211,0.9815 1.000,0.2984,0.01635,0.00944,-0.0442,0.9152,0.9877 1.250,0.3502,0.01619,0.00938,-0.0497,0.9066,0.9960 1.500,0.3956,0.01602,0.00934,-0.0537,0.8988,1.0000 1.750,0.4151,0.01612,0.00952,-0.0530,0.8854,1.0000 2.000,0.4329,0.01623,0.00970,-0.0517,0.8718,1.0000 2.250,0.4489,0.01638,0.00992,-0.0501,0.8584,1.0000 2.500,0.4639,0.01656,0.01019,-0.0481,0.8453,1.0000 2.750,0.4797,0.01652,0.01025,-0.0455,0.8297,1.0000 3.000,0.4918,0.01597,0.00972,-0.0406,0.8038,1.0000 3.250,0.5021,0.01497,0.00866,-0.0341,0.7696,1.0000 3.500,0.5131,0.01435,0.00798,-0.0289,0.7342,1.0000 3.750,0.5287,0.01403,0.00769,-0.0254,0.7046,1.0000 4.000,0.5455,0.01373,0.00742,-0.0221,0.6676,1.0000 4.250,0.5588,0.01342,0.00693,-0.0177,0.5763,1.0000 4.500,0.5494,0.01650,0.00746,-0.0114,0.1547,1.0000 4.750,0.5646,0.01811,0.00870,-0.0096,0.1123,1.0000 5.000,0.5829,0.01945,0.00990,-0.0081,0.0973,1.0000 5.250,0.6044,0.02069,0.01108,-0.0070,0.0863,1.0000 5.500,0.6281,0.02229,0.01262,-0.0062,0.0792,1.0000 5.750,0.6548,0.02386,0.01424,-0.0056,0.0748,1.0000 6.000,0.6816,0.02576,0.01612,-0.0053,0.0710,1.0000 6.250,0.7077,0.02803,0.01854,-0.0049,0.0675,1.0000 6.500,0.7334,0.03019,0.02105,-0.0041,0.0663,1.0000 6.750,0.7579,0.03291,0.02416,-0.0033,0.0665,1.0000 7.000,0.7803,0.03625,0.02784,-0.0024,0.0677,1.0000 7.250,0.8020,0.04047,0.03230,-0.0019,0.0694,1.0000 7.500,0.8164,0.04344,0.03636,0.0010,0.0764,1.0000 7.750,0.8320,0.04848,0.04162,0.0017,0.0810,1.0000 9.250,0.7557,0.08724,0.08275,-0.0042,0.1638,1.0000 9.500,0.6159,0.09182,0.08750,-0.0100,0.1780,1.0000 9.750,0.6451,0.09430,0.09001,-0.0063,0.1652,1.0000