Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m8-il-500000-n5 Airfoil,m8-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,79.5718 Max Cl/Cd alpha,7.25 Url,http://airfoiltools.com/polar/csv?polar=xf-m8-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.2263,0.10770,0.10412,-0.0079,0.6066,0.0136 -9.750,-0.2195,0.10458,0.10098,-0.0092,0.5983,0.0138 -9.250,-0.2166,0.09618,0.09253,-0.0130,0.5842,0.0155 -9.000,-0.2081,0.09379,0.09013,-0.0140,0.5758,0.0157 -8.750,-0.1989,0.09165,0.08795,-0.0149,0.5683,0.0159 -8.500,-0.1902,0.08939,0.08568,-0.0159,0.5620,0.0163 -8.250,-0.1838,0.08682,0.08311,-0.0169,0.5565,0.0167 -8.000,-0.1815,0.08375,0.08002,-0.0180,0.5518,0.0173 -7.750,-0.1975,0.07823,0.07453,-0.0202,0.5494,0.0187 -7.500,-0.1847,0.07650,0.07279,-0.0215,0.5444,0.0190 -7.000,-0.2233,0.03054,0.02587,-0.0667,0.5479,0.0268 -6.750,-0.1970,0.02822,0.02339,-0.0685,0.5424,0.0273 -6.500,-0.1707,0.02583,0.02078,-0.0701,0.5371,0.0280 -6.000,-0.1181,0.02120,0.01556,-0.0724,0.5278,0.0294 -5.750,-0.0914,0.01949,0.01358,-0.0729,0.5232,0.0300 -5.500,-0.0644,0.01820,0.01206,-0.0730,0.5183,0.0306 -5.250,-0.0374,0.01730,0.01099,-0.0729,0.5136,0.0312 -5.000,-0.0100,0.01668,0.01028,-0.0727,0.5095,0.0318 -4.750,0.0177,0.01610,0.00963,-0.0724,0.5051,0.0324 -4.500,0.0454,0.01558,0.00901,-0.0722,0.5003,0.0330 -4.250,0.0732,0.01512,0.00843,-0.0719,0.4956,0.0336 -4.000,0.1011,0.01470,0.00790,-0.0716,0.4914,0.0344 -3.750,0.1292,0.01431,0.00742,-0.0713,0.4868,0.0352 -3.500,0.1573,0.01398,0.00699,-0.0710,0.4818,0.0357 -3.250,0.1853,0.01374,0.00666,-0.0706,0.4767,0.0364 -3.000,0.2134,0.01349,0.00637,-0.0703,0.4721,0.0373 -2.750,0.2417,0.01325,0.00609,-0.0700,0.4665,0.0381 -2.500,0.2699,0.01306,0.00583,-0.0697,0.4594,0.0391 -2.250,0.2982,0.01289,0.00559,-0.0694,0.4518,0.0403 -2.000,0.3265,0.01275,0.00536,-0.0691,0.4417,0.0415 -1.750,0.3547,0.01260,0.00516,-0.0688,0.4328,0.0431 -1.500,0.3829,0.01247,0.00496,-0.0686,0.4230,0.0449 -1.250,0.4112,0.01238,0.00482,-0.0683,0.4134,0.0471 -1.000,0.4394,0.01233,0.00468,-0.0680,0.4039,0.0495 -0.750,0.4676,0.01222,0.00456,-0.0677,0.3956,0.0530 -0.250,0.5238,0.01218,0.00445,-0.0672,0.3799,0.0628 0.000,0.5517,0.01224,0.00446,-0.0669,0.3720,0.0682 0.250,0.5797,0.01229,0.00449,-0.0667,0.3652,0.0744 0.500,0.6077,0.01233,0.00450,-0.0664,0.3587,0.0802 0.750,0.6355,0.01236,0.00449,-0.0662,0.3535,0.0872 1.000,0.6634,0.01232,0.00445,-0.0659,0.3496,0.0964 1.250,0.6914,0.01248,0.00473,-0.0657,0.3459,0.1182 1.500,0.7195,0.01282,0.00510,-0.0654,0.3418,0.1619 1.750,0.7471,0.01315,0.00538,-0.0650,0.3367,0.1676 2.000,0.7746,0.01332,0.00549,-0.0648,0.3319,0.1709 2.250,0.8023,0.01357,0.00577,-0.0645,0.3279,0.1734 2.500,0.8299,0.01367,0.00582,-0.0642,0.3243,0.1761 2.750,0.8573,0.01374,0.00582,-0.0640,0.3206,0.1781 3.000,0.8843,0.01394,0.00605,-0.0637,0.3168,0.1795 3.250,0.9114,0.01408,0.00619,-0.0635,0.3135,0.1811 3.500,0.9388,0.01415,0.00627,-0.0632,0.3104,0.1829 3.750,0.9661,0.01420,0.00630,-0.0630,0.3065,0.1843 4.000,0.9930,0.01427,0.00633,-0.0628,0.3022,0.1852 4.250,1.0194,0.01439,0.00641,-0.0625,0.2974,0.1868 4.500,1.0462,0.01448,0.00656,-0.0623,0.2929,0.1884 4.750,1.0730,0.01451,0.00659,-0.0620,0.2865,0.1885 5.000,1.0990,0.01462,0.00665,-0.0617,0.2790,0.1884 5.250,1.1254,0.01468,0.00670,-0.0615,0.2703,0.1882 5.500,1.1510,0.01483,0.00680,-0.0612,0.2588,0.1883 5.750,1.1757,0.01507,0.00696,-0.0608,0.2446,0.1885 6.250,1.2242,0.01559,0.00737,-0.0599,0.2260,0.1886 6.500,1.2480,0.01586,0.00761,-0.0594,0.2198,0.1886 6.750,1.2719,0.01611,0.00787,-0.0590,0.2154,0.1886 7.000,1.2959,0.01633,0.00810,-0.0585,0.2120,0.1885 7.250,1.3193,0.01658,0.00836,-0.0579,0.2089,0.1886 7.500,1.3420,0.01688,0.00868,-0.0573,0.2058,0.1887 7.750,1.3639,0.01721,0.00902,-0.0566,0.2029,0.1888 8.000,1.3856,0.01753,0.00936,-0.0559,0.2003,0.1889 8.250,1.4081,0.01777,0.00965,-0.0552,0.1989,0.1891 8.500,1.4299,0.01804,0.00998,-0.0545,0.1972,0.1892 8.750,1.4507,0.01834,0.01033,-0.0537,0.1953,0.1894 9.000,1.4704,0.01869,0.01073,-0.0527,0.1933,0.1896 9.250,1.4888,0.01909,0.01117,-0.0516,0.1914,0.1898 9.500,1.5054,0.01953,0.01166,-0.0503,0.1896,0.1899 9.750,1.5190,0.02002,0.01219,-0.0485,0.1881,0.1901 10.000,1.5269,0.02062,0.01283,-0.0460,0.1866,0.1903 10.250,1.5343,0.02141,0.01367,-0.0438,0.1851,0.1905 10.500,1.5437,0.02223,0.01456,-0.0421,0.1839,0.1907 10.750,1.5560,0.02297,0.01538,-0.0408,0.1832,0.1909 11.000,1.5682,0.02377,0.01626,-0.0397,0.1823,0.1910 11.250,1.5804,0.02463,0.01721,-0.0387,0.1808,0.1913 11.500,1.5916,0.02561,0.01825,-0.0378,0.1788,0.1917 11.750,1.6014,0.02675,0.01945,-0.0369,0.1764,0.1918 12.000,1.6100,0.02801,0.02077,-0.0360,0.1746,0.1921 12.250,1.6165,0.02947,0.02227,-0.0351,0.1722,0.1924 12.500,1.6228,0.03098,0.02383,-0.0343,0.1707,0.1929 12.750,1.6267,0.03274,0.02562,-0.0335,0.1682,0.1931 13.000,1.6377,0.03392,0.02691,-0.0329,0.1663,0.1937 13.250,1.6461,0.03536,0.02843,-0.0324,0.1645,0.1940 13.500,1.6524,0.03701,0.03015,-0.0319,0.1616,0.1944 13.750,1.6569,0.03888,0.03208,-0.0315,0.1593,0.1946 14.000,1.6592,0.04099,0.03423,-0.0311,0.1570,0.1947 14.250,1.6598,0.04331,0.03661,-0.0308,0.1548,0.1951 14.500,1.6633,0.04539,0.03878,-0.0306,0.1528,0.1952 14.750,1.6694,0.04725,0.04074,-0.0304,0.1510,0.1957 15.000,1.6731,0.04946,0.04303,-0.0304,0.1480,0.1961 15.250,1.6722,0.05228,0.04591,-0.0306,0.1440,0.1964 15.500,1.6665,0.05574,0.04940,-0.0310,0.1397,0.1968 15.750,1.6700,0.05814,0.05188,-0.0312,0.1358,0.1972 16.000,1.6665,0.06147,0.05527,-0.0318,0.1308,0.1973 16.250,1.6588,0.06541,0.05926,-0.0326,0.1253,0.1975 16.500,1.6527,0.06922,0.06312,-0.0334,0.1186,0.1977 17.000,1.6112,0.08131,0.07520,-0.0368,0.0959,0.1981 17.250,1.5838,0.08868,0.08256,-0.0393,0.0846,0.1978 17.500,1.5595,0.09580,0.08971,-0.0418,0.0757,0.1979