Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-du861372-il-100000 Airfoil,du861372-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,33.4101 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-du861372-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.8082,0.04972,0.04200,-0.0257,0.4160,0.1091 -8.500,-0.8107,0.04399,0.03498,-0.0210,0.4161,0.0903 -8.250,-0.7837,0.04011,0.03093,-0.0209,0.4162,0.0846 -8.000,-0.7651,0.03793,0.02788,-0.0184,0.4162,0.0776 -7.750,-0.7340,0.03496,0.02476,-0.0188,0.4162,0.0749 -7.500,-0.7026,0.03254,0.02210,-0.0190,0.4164,0.0721 -7.250,-0.6694,0.03065,0.01997,-0.0193,0.4165,0.0698 -7.000,-0.6361,0.02909,0.01830,-0.0198,0.4170,0.0696 -6.750,-0.6037,0.02773,0.01689,-0.0202,0.4176,0.0698 -6.500,-0.5737,0.02656,0.01570,-0.0203,0.4184,0.0693 -6.250,-0.5493,0.02555,0.01468,-0.0196,0.4193,0.0690 -6.000,-0.5300,0.02465,0.01376,-0.0182,0.4201,0.0690 -5.750,-0.5130,0.02382,0.01287,-0.0166,0.4212,0.0694 -5.500,-0.4960,0.02306,0.01204,-0.0150,0.4223,0.0703 -5.250,-0.4782,0.02235,0.01124,-0.0135,0.4235,0.0718 -5.000,-0.4592,0.02171,0.01050,-0.0122,0.4248,0.0744 -4.750,-0.4402,0.02103,0.00979,-0.0108,0.4262,0.0803 -4.500,-0.4249,0.02003,0.00918,-0.0091,0.4276,0.1390 -4.250,-0.4069,0.01927,0.00861,-0.0077,0.4291,0.1916 -4.000,-0.4029,0.01762,0.00796,-0.0046,0.4306,0.3726 -3.750,-0.3901,0.01679,0.00777,-0.0020,0.4322,0.4954 -3.500,-0.3674,0.01671,0.00808,-0.0003,0.4343,0.5771 -3.250,-0.3416,0.01676,0.00816,0.0005,0.4369,0.6116 -3.000,-0.3161,0.01675,0.00812,0.0012,0.4397,0.6342 -2.750,-0.2909,0.01674,0.00806,0.0018,0.4427,0.6522 -2.500,-0.2658,0.01675,0.00802,0.0024,0.4458,0.6691 -2.250,-0.2406,0.01689,0.00815,0.0032,0.4491,0.6892 -2.000,-0.2157,0.01687,0.00809,0.0037,0.4530,0.7034 -1.750,-0.1894,0.01686,0.00805,0.0041,0.4574,0.7115 -1.500,-0.1641,0.01692,0.00807,0.0047,0.4620,0.7235 -1.250,-0.1393,0.01704,0.00819,0.0055,0.4667,0.7378 -1.000,-0.1147,0.01716,0.00832,0.0063,0.4723,0.7523 -0.750,-0.0872,0.01739,0.00860,0.0070,0.4783,0.7613 -0.500,-0.0621,0.01744,0.00868,0.0077,0.4846,0.7717 -0.250,-0.0373,0.01777,0.00910,0.0091,0.4918,0.7876 0.250,0.0166,0.01812,0.00964,0.0108,0.5087,0.8078 0.500,0.0397,0.01818,0.00977,0.0119,0.5171,0.8200 0.750,0.0714,0.01843,0.01016,0.0121,0.5277,0.8289 1.000,0.0970,0.01852,0.01036,0.0130,0.5362,0.8402 1.250,0.1364,0.01911,0.01108,0.0127,0.5431,0.8598 1.500,0.1704,0.01931,0.01131,0.0123,0.5428,0.8736 1.750,0.2036,0.01934,0.01137,0.0114,0.5406,0.8822 2.000,0.3928,0.02012,0.01241,-0.0157,0.5537,0.9474 2.500,0.4483,0.01957,0.01193,-0.0170,0.5442,0.9559 2.750,0.4770,0.01933,0.01175,-0.0179,0.5383,0.9600 3.000,0.5007,0.01920,0.01164,-0.0177,0.5293,0.9645 3.250,0.5246,0.01908,0.01147,-0.0176,0.5116,0.9682 3.500,0.5543,0.01894,0.01125,-0.0185,0.4851,0.9718 3.750,0.5804,0.01894,0.01117,-0.0189,0.4555,0.9759 4.000,0.6011,0.01913,0.01121,-0.0182,0.4223,0.9796 4.250,0.6223,0.01950,0.01130,-0.0178,0.3946,0.9829 4.500,0.6525,0.01953,0.01148,-0.0190,0.3290,0.9865 4.750,0.6688,0.02194,0.01241,-0.0178,0.3101,0.9892 5.000,0.7079,0.02617,0.01620,-0.0207,0.2749,0.9903 5.250,0.7288,0.02775,0.01814,-0.0205,0.2480,0.9929 5.500,0.7493,0.02709,0.01809,-0.0200,0.2211,0.9970 5.750,0.7670,0.02589,0.01740,-0.0188,0.1938,1.0000 6.000,0.7729,0.02509,0.01699,-0.0157,0.1808,1.0000 6.250,0.7786,0.02488,0.01698,-0.0127,0.1665,1.0000 6.500,0.7832,0.02568,0.01772,-0.0095,0.1497,1.0000 6.750,0.7869,0.02665,0.01865,-0.0061,0.1360,1.0000 7.000,0.7887,0.02761,0.01950,-0.0025,0.1258,1.0000 7.250,0.7971,0.02828,0.02021,0.0004,0.1145,1.0000 7.500,0.8054,0.02928,0.02114,0.0033,0.1066,1.0000 7.750,0.8161,0.03008,0.02193,0.0059,0.0992,1.0000 8.000,0.8294,0.03134,0.02312,0.0079,0.0923,1.0000 8.250,0.8448,0.03246,0.02436,0.0098,0.0865,1.0000 8.500,0.8589,0.03386,0.02570,0.0116,0.0822,1.0000 8.750,0.8787,0.03606,0.02806,0.0127,0.0780,1.0000 9.000,0.8873,0.03747,0.02973,0.0156,0.0747,1.0000 9.250,0.8928,0.03898,0.03142,0.0187,0.0721,1.0000 9.500,0.8961,0.04068,0.03331,0.0221,0.0708,1.0000 9.750,0.8959,0.04241,0.03522,0.0258,0.0696,1.0000 10.000,0.8976,0.04466,0.03768,0.0289,0.0688,1.0000 10.250,0.9023,0.04760,0.04084,0.0308,0.0677,1.0000 10.500,0.9043,0.05142,0.04491,0.0323,0.0669,1.0000 11.000,0.8884,0.05964,0.05372,0.0362,0.0660,1.0000 11.250,0.8751,0.06332,0.05763,0.0383,0.0660,1.0000 11.500,0.8579,0.06711,0.06161,0.0402,0.0661,1.0000 11.750,0.8399,0.07020,0.06494,0.0414,0.0666,1.0000 12.000,0.7187,0.08569,0.08096,0.0358,0.0776,1.0000 12.250,0.7069,0.09190,0.08717,0.0335,0.0791,1.0000 12.500,0.7122,0.09702,0.09228,0.0330,0.0802,1.0000