Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m8-il-100000-n5 Airfoil,m8-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,46.3077 Max Cl/Cd alpha,7 Url,http://airfoiltools.com/polar/csv?polar=xf-m8-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.1751,0.11238,0.10729,-0.0147,0.7316,0.0565 -9.000,-0.1727,0.11052,0.10546,-0.0171,0.7232,0.0567 -8.750,-0.1702,0.10849,0.10340,-0.0189,0.7156,0.0569 -8.500,-0.1515,0.10344,0.09832,-0.0179,0.7069,0.0575 -8.250,-0.1390,0.10034,0.09517,-0.0177,0.6979,0.0586 -8.000,-0.1288,0.09786,0.09266,-0.0181,0.6889,0.0603 -7.750,-0.1212,0.09566,0.09044,-0.0190,0.6802,0.0632 -7.500,-0.1260,0.09492,0.08972,-0.0220,0.6730,0.0657 -7.250,-0.1253,0.09349,0.08830,-0.0254,0.6655,0.0661 -7.000,-0.1167,0.09100,0.08575,-0.0286,0.6594,0.0662 -6.750,-0.1031,0.08701,0.08179,-0.0288,0.6517,0.0666 -6.500,-0.0880,0.08341,0.07815,-0.0272,0.6450,0.0675 -6.250,-0.0739,0.08080,0.07551,-0.0271,0.6390,0.0690 -6.000,-0.0596,0.07863,0.07334,-0.0285,0.6319,0.0731 -5.750,-0.0428,0.07694,0.07154,-0.0373,0.6265,0.0768 -5.500,-0.0299,0.07179,0.06633,-0.0373,0.6218,0.0653 -5.250,-0.0145,0.06802,0.06255,-0.0386,0.6154,0.0592 -5.000,0.0056,0.06448,0.05891,-0.0427,0.6099,0.0584 -4.500,0.0555,0.05608,0.05020,-0.0527,0.5994,0.0567 -4.250,0.0806,0.05257,0.04655,-0.0558,0.5935,0.0567 -4.000,0.1008,0.05159,0.04552,-0.0552,0.5881,0.0585 -3.750,0.1258,0.04962,0.04349,-0.0568,0.5813,0.0602 -3.500,0.1539,0.04644,0.04014,-0.0597,0.5751,0.0606 -3.250,0.1828,0.04302,0.03646,-0.0625,0.5701,0.0607 -3.000,0.2128,0.03968,0.03291,-0.0653,0.5638,0.0620 -2.750,0.2475,0.03288,0.02552,-0.0703,0.5584,0.0649 -2.500,0.2794,0.02610,0.01769,-0.0737,0.5537,0.0671 -2.250,0.3059,0.02545,0.01691,-0.0733,0.5480,0.0693 -2.000,0.3337,0.02435,0.01557,-0.0734,0.5411,0.0730 -1.750,0.3619,0.02313,0.01392,-0.0734,0.5353,0.0764 -1.500,0.3888,0.02258,0.01322,-0.0729,0.5300,0.0792 -1.250,0.4161,0.02227,0.01290,-0.0726,0.5228,0.0834 -1.000,0.4441,0.02174,0.01212,-0.0723,0.5168,0.0897 -0.750,0.4709,0.02163,0.01197,-0.0718,0.5118,0.0959 -0.500,0.4984,0.02149,0.01185,-0.0715,0.5046,0.1044 -0.250,0.5253,0.02169,0.01212,-0.0710,0.4981,0.1144 0.000,0.5513,0.02248,0.01305,-0.0701,0.4927,0.1226 0.250,0.5774,0.02319,0.01391,-0.0695,0.4842,0.1311 0.500,0.6044,0.02346,0.01410,-0.0689,0.4774,0.1466 0.750,0.6341,0.02358,0.01384,-0.0686,0.4706,0.1784 1.000,0.6604,0.02381,0.01401,-0.0682,0.4630,0.1909 1.250,0.6872,0.02389,0.01384,-0.0676,0.4572,0.2047 1.500,0.7133,0.02397,0.01388,-0.0673,0.4495,0.2149 1.750,0.7389,0.02384,0.01372,-0.0669,0.4426,0.2234 2.000,0.7647,0.02374,0.01356,-0.0664,0.4361,0.2323 2.250,0.7911,0.02384,0.01355,-0.0661,0.4286,0.2404 2.500,0.8166,0.02366,0.01335,-0.0656,0.4230,0.2479 2.750,0.8427,0.02379,0.01341,-0.0653,0.4170,0.2557 3.000,0.8683,0.02372,0.01336,-0.0650,0.4109,0.2598 3.250,0.8947,0.02370,0.01322,-0.0646,0.4056,0.2604 3.500,0.9207,0.02381,0.01330,-0.0643,0.3994,0.2595 3.750,0.9467,0.02390,0.01335,-0.0640,0.3930,0.2586 4.000,0.9728,0.02395,0.01327,-0.0636,0.3879,0.2577 4.250,0.9981,0.02415,0.01348,-0.0633,0.3816,0.2574 4.500,1.0233,0.02431,0.01364,-0.0629,0.3757,0.2573 4.750,1.0486,0.02443,0.01366,-0.0624,0.3707,0.2571 5.000,1.0727,0.02470,0.01396,-0.0620,0.3644,0.2566 5.250,1.0971,0.02497,0.01422,-0.0615,0.3579,0.2557 5.500,1.1225,0.02518,0.01431,-0.0611,0.3522,0.2550 5.750,1.1465,0.02556,0.01475,-0.0608,0.3452,0.2544 6.000,1.1710,0.02585,0.01506,-0.0606,0.3385,0.2541 6.250,1.1961,0.02611,0.01520,-0.0602,0.3328,0.2537 6.500,1.2185,0.02657,0.01580,-0.0598,0.3257,0.2533 6.750,1.2411,0.02695,0.01619,-0.0593,0.3193,0.2530 7.000,1.2642,0.02730,0.01647,-0.0587,0.3138,0.2527 7.250,1.2837,0.02787,0.01720,-0.0580,0.3068,0.2525 7.500,1.3037,0.02835,0.01770,-0.0572,0.3007,0.2523 7.750,1.3240,0.02880,0.01811,-0.0564,0.2955,0.2522 8.000,1.3402,0.02951,0.01897,-0.0553,0.2888,0.2523 8.250,1.3568,0.03011,0.01960,-0.0542,0.2832,0.2526 8.500,1.3740,0.03066,0.02012,-0.0531,0.2786,0.2531 8.750,1.3867,0.03153,0.02115,-0.0517,0.2731,0.2536 9.000,1.3994,0.03231,0.02199,-0.0503,0.2684,0.2541 9.250,1.4116,0.03301,0.02268,-0.0488,0.2650,0.2545 9.500,1.4218,0.03391,0.02362,-0.0471,0.2616,0.2546 9.750,1.4289,0.03510,0.02493,-0.0456,0.2579,0.2549 10.000,1.4373,0.03627,0.02619,-0.0444,0.2545,0.2550 10.250,1.4473,0.03739,0.02735,-0.0433,0.2517,0.2552 10.500,1.4600,0.03834,0.02829,-0.0423,0.2492,0.2554 10.750,1.4701,0.03961,0.02962,-0.0414,0.2468,0.2556 11.000,1.4740,0.04143,0.03158,-0.0406,0.2441,0.2558 11.250,1.4787,0.04325,0.03351,-0.0399,0.2414,0.2561 11.500,1.4848,0.04496,0.03532,-0.0392,0.2389,0.2565 11.750,1.4935,0.04645,0.03685,-0.0386,0.2366,0.2569 12.000,1.5064,0.04760,0.03802,-0.0380,0.2345,0.2575 12.250,1.5237,0.04840,0.03881,-0.0373,0.2327,0.2582 12.500,1.5147,0.05178,0.04241,-0.0371,0.2305,0.2586 12.750,1.5049,0.05543,0.04627,-0.0371,0.2284,0.2587 13.000,1.4932,0.05946,0.05048,-0.0374,0.2262,0.2590 13.250,1.4810,0.06372,0.05489,-0.0379,0.2241,0.2591 13.500,1.4732,0.06761,0.05891,-0.0384,0.2221,0.2596 13.750,1.4743,0.07046,0.06185,-0.0386,0.2204,0.2602