Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m26-il-100000-n5 Airfoil,m26-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,41.4164 Max Cl/Cd alpha,7.5 Url,http://airfoiltools.com/polar/csv?polar=xf-m26-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.2726,0.12423,0.11898,0.0010,0.6186,0.0247 -8.500,-0.2658,0.12202,0.11675,-0.0018,0.6157,0.0248 -8.250,-0.2601,0.11989,0.11463,-0.0045,0.6131,0.0248 -8.000,-0.2514,0.11758,0.11229,-0.0075,0.6108,0.0248 -7.500,-0.2312,0.10611,0.10075,-0.0063,0.6068,0.0254 -7.250,-0.2211,0.10199,0.09665,-0.0070,0.6043,0.0258 -7.000,-0.2104,0.09864,0.09330,-0.0086,0.6019,0.0263 -6.750,-0.1989,0.09555,0.09020,-0.0106,0.5996,0.0270 -6.500,-0.1861,0.09262,0.08723,-0.0129,0.5973,0.0281 -6.250,-0.1717,0.08979,0.08435,-0.0155,0.5952,0.0296 -6.000,-0.1548,0.08711,0.08159,-0.0186,0.5933,0.0312 -5.750,-0.1317,0.08519,0.07955,-0.0233,0.5913,0.0326 -5.500,-0.1017,0.08414,0.07840,-0.0296,0.5886,0.0333 -5.250,-0.0733,0.08245,0.07658,-0.0345,0.5862,0.0335 -5.000,-0.0496,0.07930,0.07334,-0.0376,0.5841,0.0338 -4.750,-0.0481,0.07267,0.06680,-0.0353,0.5824,0.0349 -4.500,-0.0331,0.06921,0.06330,-0.0358,0.5807,0.0365 -4.250,-0.0116,0.06643,0.06041,-0.0377,0.5791,0.0382 -4.000,0.0126,0.06383,0.05768,-0.0399,0.5776,0.0403 -3.750,0.0423,0.06171,0.05540,-0.0429,0.5756,0.0436 -3.500,0.0919,0.06206,0.05541,-0.0487,0.5730,0.0459 -3.250,0.1015,0.05700,0.05043,-0.0483,0.5708,0.0470 -3.000,0.1216,0.05417,0.04754,-0.0490,0.5686,0.0490 -2.750,0.1471,0.05202,0.04526,-0.0502,0.5667,0.0519 -2.500,0.1974,0.05348,0.04620,-0.0538,0.5650,0.0579 -2.250,0.2107,0.04880,0.04156,-0.0538,0.5636,0.0592 -2.000,0.2317,0.04632,0.03899,-0.0541,0.5623,0.0615 -1.750,0.2590,0.04470,0.03726,-0.0551,0.5602,0.0651 -1.500,0.3044,0.04618,0.03829,-0.0571,0.5575,0.0706 -1.250,0.3225,0.04237,0.03453,-0.0577,0.5552,0.0721 -1.000,0.3442,0.04035,0.03249,-0.0580,0.5532,0.0765 -0.750,0.3826,0.04119,0.03291,-0.0588,0.5514,0.0844 -0.250,0.4304,0.03686,0.02838,-0.0594,0.5483,0.0878 0.750,0.5427,0.03352,0.02453,-0.0613,0.5390,0.1022 1.000,0.5701,0.03294,0.02380,-0.0615,0.5367,0.1153 1.250,0.5976,0.03206,0.02278,-0.0616,0.5348,0.1170 1.500,0.6346,0.03022,0.02027,-0.0606,0.5332,0.0571 1.750,0.6622,0.02942,0.01930,-0.0605,0.5317,0.0559 2.000,0.6891,0.02922,0.01910,-0.0612,0.5280,0.0548 2.250,0.7164,0.02890,0.01870,-0.0615,0.5247,0.0539 2.500,0.7443,0.02846,0.01813,-0.0616,0.5220,0.0534 2.750,0.7726,0.02797,0.01749,-0.0616,0.5197,0.0534 3.000,0.8015,0.02749,0.01686,-0.0616,0.5179,0.0539 3.250,0.8331,0.02730,0.01650,-0.0623,0.5159,0.0578 3.500,0.8588,0.02784,0.01722,-0.0634,0.5111,0.0610 3.750,0.8834,0.02795,0.01731,-0.0633,0.5078,0.0624 4.000,0.9074,0.02790,0.01719,-0.0627,0.5054,0.0643 4.250,0.9320,0.02779,0.01698,-0.0621,0.5034,0.0670 4.500,0.9575,0.02768,0.01675,-0.0615,0.5017,0.0710 4.750,0.9762,0.02886,0.01811,-0.0618,0.4962,0.0779 5.000,0.9984,0.02936,0.01869,-0.0616,0.4925,0.0993 5.250,1.0187,0.02891,0.01898,-0.0608,0.4900,0.5816 5.750,1.1180,0.02904,0.01974,-0.0706,0.4843,1.0000 6.000,1.1313,0.03055,0.02141,-0.0701,0.4782,1.0000 6.250,1.1532,0.03088,0.02176,-0.0695,0.4753,1.0000 6.500,1.1778,0.03088,0.02177,-0.0688,0.4732,1.0000 6.750,1.2040,0.03073,0.02164,-0.0682,0.4716,1.0000 7.000,1.2033,0.03326,0.02444,-0.0670,0.4620,1.0000 7.250,1.2406,0.03064,0.02173,-0.0660,0.4538,1.0000 7.500,1.2603,0.03043,0.02160,-0.0649,0.4451,1.0000 7.750,1.2720,0.03095,0.02227,-0.0636,0.4346,1.0000 8.000,1.2851,0.03113,0.02258,-0.0622,0.4221,1.0000 8.250,1.2816,0.03295,0.02452,-0.0606,0.4076,1.0000 8.500,1.2663,0.03599,0.02763,-0.0586,0.3973,1.0000 8.750,1.2548,0.03918,0.03087,-0.0574,0.3847,1.0000 9.000,1.2454,0.04245,0.03418,-0.0565,0.3695,1.0000 9.250,1.2640,0.04217,0.03377,-0.0553,0.3421,1.0000 9.500,1.2719,0.04281,0.03398,-0.0536,0.2985,1.0000 9.750,1.2613,0.04613,0.03713,-0.0523,0.2694,1.0000 10.000,1.2471,0.04995,0.04075,-0.0512,0.2358,1.0000 10.500,1.2013,0.05979,0.04996,-0.0493,0.1454,1.0000 10.750,1.1791,0.06504,0.05491,-0.0487,0.0968,1.0000 11.000,1.1589,0.07030,0.05990,-0.0483,0.0448,1.0000 11.250,1.1488,0.07456,0.06406,-0.0480,0.0331,1.0000 11.500,1.1465,0.07796,0.06756,-0.0478,0.0293,1.0000 11.750,1.1464,0.08115,0.07088,-0.0477,0.0277,1.0000 12.000,1.1460,0.08444,0.07432,-0.0476,0.0265,1.0000 12.250,1.1447,0.08790,0.07794,-0.0476,0.0255,1.0000 12.500,1.1424,0.09157,0.08176,-0.0478,0.0247,1.0000 12.750,1.1388,0.09549,0.08584,-0.0480,0.0237,1.0000 13.000,1.1334,0.09972,0.09021,-0.0484,0.0228,1.0000 13.250,1.1271,0.10416,0.09480,-0.0489,0.0219,1.0000