Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-a63a108c-il-200000-n5 Airfoil,a63a108c-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,41.8219 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-a63a108c-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.7432,0.08327,0.07976,0.0147,1.0000,0.0158 -8.500,-0.7591,0.07357,0.07001,0.0046,1.0000,0.0155 -8.250,-0.7718,0.06426,0.06051,-0.0013,1.0000,0.0152 -8.000,-0.7811,0.05490,0.05079,-0.0046,1.0000,0.0150 -7.750,-0.7841,0.04606,0.04141,-0.0060,1.0000,0.0150 -7.500,-0.7784,0.03891,0.03362,-0.0062,1.0000,0.0152 -7.250,-0.7648,0.03364,0.02769,-0.0059,1.0000,0.0158 -7.000,-0.7470,0.02910,0.02234,-0.0054,1.0000,0.0168 -6.750,-0.7228,0.02792,0.02107,-0.0054,1.0000,0.0174 -6.500,-0.6988,0.02589,0.01871,-0.0052,1.0000,0.0179 -6.250,-0.6739,0.02374,0.01619,-0.0049,1.0000,0.0185 -6.000,-0.6481,0.02182,0.01389,-0.0046,1.0000,0.0192 -5.750,-0.6219,0.02048,0.01239,-0.0044,1.0000,0.0198 -5.500,-0.5952,0.01949,0.01134,-0.0043,1.0000,0.0206 -5.250,-0.5681,0.01855,0.01023,-0.0042,1.0000,0.0222 -5.000,-0.5411,0.01775,0.00941,-0.0042,1.0000,0.0235 -4.750,-0.5139,0.01691,0.00851,-0.0042,1.0000,0.0249 -4.500,-0.4867,0.01606,0.00762,-0.0041,1.0000,0.0262 -4.250,-0.4592,0.01538,0.00694,-0.0041,1.0000,0.0278 -4.000,-0.4315,0.01478,0.00633,-0.0042,1.0000,0.0303 -3.750,-0.4036,0.01422,0.00575,-0.0043,1.0000,0.0334 -3.500,-0.3756,0.01368,0.00521,-0.0044,1.0000,0.0367 -3.250,-0.3474,0.01320,0.00475,-0.0046,1.0000,0.0417 -3.000,-0.3191,0.01274,0.00434,-0.0048,1.0000,0.0485 -2.750,-0.2909,0.01229,0.00395,-0.0050,1.0000,0.0599 -2.500,-0.2628,0.01181,0.00361,-0.0052,1.0000,0.0828 -2.250,-0.2352,0.01124,0.00332,-0.0055,1.0000,0.1374 -2.000,-0.2086,0.01045,0.00305,-0.0058,1.0000,0.2534 -1.750,-0.1841,0.00945,0.00288,-0.0058,1.0000,0.4484 -1.250,-0.1257,0.00857,0.00296,-0.0062,0.9826,0.6908 -1.000,-0.0941,0.00839,0.00299,-0.0066,0.9712,0.7592 -0.750,-0.0653,0.00825,0.00303,-0.0061,0.9575,0.8151 -0.500,-0.0414,0.00816,0.00310,-0.0041,0.9382,0.8756 -0.250,-0.0145,0.00813,0.00311,-0.0027,0.9161,0.9320 0.000,0.0184,0.00813,0.00306,-0.0031,0.8947,0.9660 0.250,0.0528,0.00813,0.00299,-0.0041,0.8753,0.9941 0.500,0.0793,0.00812,0.00290,-0.0035,0.8533,1.0000 0.750,0.1038,0.00814,0.00283,-0.0025,0.8288,1.0000 1.000,0.1281,0.00817,0.00275,-0.0014,0.8023,1.0000 1.250,0.1533,0.00822,0.00269,-0.0005,0.7682,1.0000 1.500,0.1784,0.00832,0.00263,0.0006,0.7241,1.0000 1.750,0.2037,0.00851,0.00257,0.0015,0.6645,1.0000 2.000,0.2292,0.00886,0.00253,0.0022,0.5780,1.0000 2.250,0.2555,0.00939,0.00259,0.0025,0.4728,1.0000 2.500,0.2826,0.00999,0.00272,0.0024,0.3727,1.0000 3.000,0.3381,0.01098,0.00309,0.0020,0.2426,1.0000 3.250,0.3660,0.01139,0.00332,0.0018,0.2014,1.0000 3.500,0.3939,0.01178,0.00355,0.0016,0.1689,1.0000 4.000,0.4498,0.01254,0.00408,0.0013,0.1227,1.0000 4.250,0.4776,0.01294,0.00440,0.0012,0.1061,1.0000 4.500,0.5054,0.01333,0.00474,0.0011,0.0928,1.0000 4.750,0.5331,0.01374,0.00510,0.0010,0.0817,1.0000 5.000,0.5607,0.01417,0.00551,0.0009,0.0728,1.0000 5.250,0.5881,0.01462,0.00594,0.0009,0.0653,1.0000 5.500,0.6155,0.01510,0.00640,0.0008,0.0589,1.0000 5.750,0.6427,0.01560,0.00691,0.0008,0.0536,1.0000 6.000,0.6697,0.01613,0.00746,0.0008,0.0489,1.0000 6.250,0.6965,0.01670,0.00805,0.0008,0.0451,1.0000 6.500,0.7231,0.01729,0.00864,0.0009,0.0418,1.0000 6.750,0.7496,0.01793,0.00935,0.0009,0.0389,1.0000 7.000,0.7757,0.01864,0.01011,0.0010,0.0365,1.0000 7.250,0.8016,0.01931,0.01081,0.0011,0.0343,1.0000 7.500,0.8273,0.02010,0.01172,0.0013,0.0323,1.0000 7.750,0.8526,0.02090,0.01257,0.0014,0.0308,1.0000 8.000,0.8773,0.02189,0.01365,0.0017,0.0295,1.0000 8.250,0.9019,0.02288,0.01479,0.0019,0.0282,1.0000 8.500,0.9262,0.02376,0.01570,0.0021,0.0271,1.0000 8.750,0.9498,0.02495,0.01710,0.0024,0.0258,1.0000 9.000,0.9729,0.02613,0.01846,0.0027,0.0248,1.0000 9.250,0.9955,0.02730,0.01974,0.0030,0.0241,1.0000 9.500,1.0171,0.02862,0.02115,0.0034,0.0236,1.0000 9.750,1.0363,0.03069,0.02363,0.0040,0.0229,1.0000 10.000,1.0540,0.03281,0.02608,0.0045,0.0222,1.0000 10.250,1.0709,0.03475,0.02828,0.0051,0.0216,1.0000 10.500,1.0879,0.03633,0.03003,0.0056,0.0211,1.0000 10.750,1.1044,0.03775,0.03152,0.0061,0.0207,1.0000 11.000,1.1062,0.04175,0.03612,0.0071,0.0201,1.0000 11.250,1.1010,0.04612,0.04099,0.0079,0.0197,1.0000 11.500,1.0860,0.05081,0.04609,0.0087,0.0195,1.0000 11.750,1.0599,0.05628,0.05187,0.0079,0.0195,1.0000 12.000,1.0249,0.06569,0.06160,0.0007,0.0197,1.0000 12.250,0.9329,0.09620,0.09241,-0.0237,0.0207,1.0000