Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m1-il-100000 Airfoil,m1-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,27.5837 Max Cl/Cd alpha,2.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-m1-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.5694,0.12858,0.12376,0.0177,1.0000,0.0858 -10.750,-0.5843,0.12561,0.12084,0.0142,1.0000,0.0873 -10.500,-0.7075,0.12961,0.12462,0.0310,1.0000,0.0779 -10.250,-0.7023,0.12581,0.12079,0.0305,1.0000,0.0813 -10.000,-0.7028,0.12182,0.11683,0.0280,1.0000,0.0848 -9.750,-0.7139,0.11787,0.11299,0.0217,1.0000,0.0872 -9.500,-0.7280,0.11353,0.10874,0.0139,1.0000,0.0878 -9.250,-0.7036,0.10861,0.10373,0.0219,1.0000,0.0918 -9.000,-0.7003,0.10478,0.09992,0.0209,1.0000,0.0960 -8.750,-0.7087,0.10019,0.09539,0.0155,1.0000,0.0997 -8.500,-0.7281,0.09452,0.08977,0.0046,1.0000,0.1010 -8.250,-0.7085,0.09118,0.08646,0.0122,1.0000,0.1068 -8.000,-0.7124,0.08633,0.08161,0.0070,1.0000,0.1120 -7.750,-0.7327,0.08062,0.07556,-0.0049,1.0000,0.1151 -7.500,-0.7091,0.07697,0.07219,0.0014,1.0000,0.1255 -6.250,-0.6694,0.05598,0.05065,-0.0054,1.0000,0.1861 -6.000,-0.6539,0.05262,0.04732,-0.0043,1.0000,0.2024 -5.750,-0.6190,0.03834,0.03075,-0.0094,1.0000,0.0894 -5.500,-0.5953,0.03445,0.02656,-0.0088,1.0000,0.0847 -5.250,-0.5707,0.03034,0.02185,-0.0079,1.0000,0.0791 -5.000,-0.5431,0.02772,0.01834,-0.0065,1.0000,0.0750 -4.750,-0.5178,0.02484,0.01521,-0.0060,1.0000,0.0775 -4.500,-0.4917,0.02313,0.01336,-0.0055,1.0000,0.0831 -4.250,-0.4643,0.02135,0.01130,-0.0048,1.0000,0.0852 -4.000,-0.4376,0.01976,0.00956,-0.0041,1.0000,0.0898 -3.750,-0.4119,0.01847,0.00833,-0.0036,1.0000,0.0973 -3.500,-0.3862,0.01727,0.00707,-0.0027,1.0000,0.1025 -3.250,-0.3620,0.01615,0.00607,-0.0019,1.0000,0.1116 -3.000,-0.3377,0.01518,0.00520,-0.0011,1.0000,0.1306 -2.750,-0.3207,0.01230,0.00420,0.0003,1.0000,0.4463 -2.500,-0.3048,0.01105,0.00454,0.0066,1.0000,0.8794 -2.250,-0.1925,0.01154,0.00452,-0.0083,1.0000,1.0000 -2.000,-0.1710,0.01128,0.00411,-0.0077,1.0000,1.0000 -1.750,-0.1494,0.01107,0.00377,-0.0071,1.0000,1.0000 -1.500,-0.1277,0.01091,0.00346,-0.0063,1.0000,1.0000 -1.250,-0.1060,0.01077,0.00324,-0.0054,1.0000,1.0000 -1.000,-0.0844,0.01067,0.00306,-0.0045,1.0000,1.0000 -0.750,-0.0630,0.01059,0.00292,-0.0034,1.0000,1.0000 -0.500,-0.0418,0.01054,0.00282,-0.0024,1.0000,1.0000 -0.250,-0.0209,0.01051,0.00276,-0.0012,1.0000,1.0000 0.000,0.0000,0.01050,0.00275,0.0000,1.0000,1.0000 0.250,0.0209,0.01051,0.00276,0.0012,1.0000,1.0000 0.500,0.0418,0.01054,0.00282,0.0024,1.0000,1.0000 0.750,0.0630,0.01059,0.00292,0.0034,1.0000,1.0000 1.000,0.0845,0.01067,0.00306,0.0045,1.0000,1.0000 1.250,0.1060,0.01077,0.00324,0.0054,1.0000,1.0000 1.500,0.1277,0.01090,0.00346,0.0063,1.0000,1.0000 1.750,0.1494,0.01107,0.00377,0.0070,1.0000,1.0000 2.000,0.1710,0.01128,0.00411,0.0077,1.0000,1.0000 2.250,0.1925,0.01153,0.00452,0.0083,1.0000,1.0000 2.500,0.3048,0.01105,0.00454,-0.0066,0.8792,1.0000 2.750,0.3207,0.01230,0.00420,-0.0003,0.4452,1.0000 3.000,0.3377,0.01518,0.00520,0.0011,0.1306,1.0000 3.250,0.3620,0.01615,0.00607,0.0019,0.1116,1.0000 3.500,0.3862,0.01727,0.00707,0.0027,0.1025,1.0000 3.750,0.4119,0.01847,0.00833,0.0036,0.0973,1.0000 4.000,0.4376,0.01976,0.00956,0.0041,0.0898,1.0000 4.250,0.4643,0.02135,0.01130,0.0048,0.0853,1.0000 4.500,0.4917,0.02313,0.01336,0.0055,0.0831,1.0000 4.750,0.5179,0.02484,0.01522,0.0060,0.0777,1.0000 5.000,0.5431,0.02772,0.01834,0.0065,0.0750,1.0000 5.250,0.5708,0.03034,0.02185,0.0079,0.0791,1.0000 5.500,0.5953,0.03445,0.02656,0.0088,0.0847,1.0000 5.750,0.6190,0.03835,0.03076,0.0094,0.0893,1.0000 7.000,0.7045,0.06725,0.06219,0.0048,0.1441,1.0000 7.250,0.7066,0.07196,0.06712,0.0010,0.1326,1.0000 7.500,0.7092,0.07699,0.07222,-0.0015,0.1254,1.0000 7.750,0.7327,0.08063,0.07557,0.0049,0.1151,1.0000 8.000,0.7126,0.08636,0.08165,-0.0071,0.1120,1.0000 8.250,0.7093,0.09114,0.08642,-0.0121,0.1065,1.0000 8.500,0.7282,0.09455,0.08979,-0.0047,0.1010,1.0000 8.750,0.7090,0.10023,0.09544,-0.0157,0.0997,1.0000 9.000,0.7009,0.10481,0.09995,-0.0211,0.0959,1.0000 9.250,0.7045,0.10863,0.10375,-0.0219,0.0917,1.0000 9.500,0.7282,0.11358,0.10878,-0.0141,0.0878,1.0000 9.750,0.7141,0.11791,0.11303,-0.0219,0.0872,1.0000 10.000,0.7034,0.12186,0.11687,-0.0282,0.0847,1.0000