Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag37-il-100000 Airfoil,ag37-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,49.2649 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-ag37-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4051,0.09290,0.08827,-0.0131,1.0000,0.0925 -9.500,-0.4221,0.09001,0.08546,-0.0179,1.0000,0.0935 -9.250,-0.4393,0.08661,0.08215,-0.0231,1.0000,0.0939 -9.000,-0.3975,0.08074,0.07622,-0.0140,1.0000,0.0995 -8.750,-0.3990,0.07716,0.07268,-0.0151,1.0000,0.1033 -8.500,-0.4135,0.07367,0.06928,-0.0188,1.0000,0.1064 -8.250,-0.4354,0.06867,0.06418,-0.0310,1.0000,0.1080 -7.750,-0.4696,0.07102,0.06627,-0.0278,1.0000,0.1099 -7.500,-0.4574,0.06810,0.06340,-0.0256,1.0000,0.1143 -7.250,-0.4461,0.06322,0.05833,-0.0322,1.0000,0.1239 -7.000,-0.4329,0.06037,0.05557,-0.0298,1.0000,0.1290 -6.750,-0.4190,0.05635,0.05142,-0.0325,1.0000,0.1398 -6.500,-0.4036,0.05295,0.04787,-0.0341,1.0000,0.1531 -6.250,-0.3882,0.04997,0.04481,-0.0341,1.0000,0.1676 -6.000,-0.3733,0.04734,0.04223,-0.0329,1.0000,0.1841 -5.500,-0.3045,0.03338,0.02629,-0.0391,1.0000,0.0927 -5.250,-0.2784,0.02869,0.02105,-0.0385,1.0000,0.0760 -5.000,-0.2522,0.02540,0.01716,-0.0376,1.0000,0.0702 -4.750,-0.2264,0.02323,0.01455,-0.0367,1.0000,0.0699 -4.500,-0.2017,0.02178,0.01292,-0.0359,1.0000,0.0744 -4.250,-0.1755,0.02020,0.01104,-0.0350,1.0000,0.0764 -4.000,-0.1494,0.01898,0.00956,-0.0340,1.0000,0.0797 -3.750,-0.1245,0.01764,0.00834,-0.0335,1.0000,0.0897 -3.500,-0.0990,0.01647,0.00726,-0.0328,1.0000,0.1003 -3.250,-0.0735,0.01548,0.00640,-0.0322,1.0000,0.1259 -3.000,-0.0476,0.01223,0.00558,-0.0321,1.0000,0.6006 -2.750,-0.0179,0.01141,0.00536,-0.0306,1.0000,1.0000 -2.500,0.0053,0.01152,0.00521,-0.0299,1.0000,1.0000 -2.250,0.0282,0.01168,0.00515,-0.0294,1.0000,1.0000 -2.000,0.0508,0.01188,0.00518,-0.0289,1.0000,1.0000 -1.750,0.0731,0.01214,0.00530,-0.0285,1.0000,1.0000 -1.500,0.0949,0.01247,0.00551,-0.0282,1.0000,1.0000 -1.250,0.1328,0.01281,0.00574,-0.0312,0.9940,1.0000 -1.000,0.1926,0.01295,0.00577,-0.0380,0.9760,1.0000 -0.750,0.2522,0.01295,0.00570,-0.0445,0.9580,1.0000 -0.500,0.3070,0.01282,0.00554,-0.0497,0.9374,1.0000 -0.250,0.3545,0.01260,0.00531,-0.0531,0.9135,1.0000 0.000,0.3927,0.01240,0.00507,-0.0543,0.8842,1.0000 0.250,0.4271,0.01224,0.00484,-0.0546,0.8555,1.0000 0.500,0.4560,0.01226,0.00476,-0.0538,0.8240,1.0000 0.750,0.4823,0.01241,0.00481,-0.0527,0.7926,1.0000 1.000,0.5075,0.01262,0.00491,-0.0515,0.7625,1.0000 1.250,0.5325,0.01287,0.00504,-0.0504,0.7339,1.0000 1.500,0.5575,0.01312,0.00519,-0.0494,0.7062,1.0000 1.750,0.5826,0.01338,0.00537,-0.0484,0.6790,1.0000 2.000,0.6077,0.01363,0.00553,-0.0475,0.6524,1.0000 2.250,0.6328,0.01395,0.00573,-0.0466,0.6263,1.0000 2.500,0.6580,0.01436,0.00604,-0.0458,0.6001,1.0000 2.750,0.6831,0.01482,0.00645,-0.0451,0.5741,1.0000 3.000,0.7082,0.01529,0.00684,-0.0443,0.5487,1.0000 3.250,0.7332,0.01574,0.00722,-0.0436,0.5234,1.0000 3.500,0.7580,0.01613,0.00761,-0.0429,0.4965,1.0000 3.750,0.7827,0.01648,0.00799,-0.0422,0.4693,1.0000 4.000,0.8071,0.01676,0.00828,-0.0414,0.4412,1.0000 4.250,0.8312,0.01704,0.00854,-0.0406,0.4118,1.0000 4.500,0.8548,0.01738,0.00883,-0.0398,0.3808,1.0000 4.750,0.8779,0.01782,0.00925,-0.0390,0.3470,1.0000 5.000,0.9003,0.01835,0.00972,-0.0381,0.3100,1.0000 5.250,0.9218,0.01900,0.01029,-0.0372,0.2682,1.0000 5.500,0.9418,0.01993,0.01100,-0.0362,0.2216,1.0000 5.750,0.9610,0.02121,0.01211,-0.0350,0.1748,1.0000 6.000,0.9800,0.02268,0.01336,-0.0339,0.1419,1.0000 6.250,1.0000,0.02430,0.01490,-0.0328,0.1206,1.0000 6.500,1.0208,0.02592,0.01649,-0.0318,0.1057,1.0000 6.750,1.0421,0.02768,0.01827,-0.0310,0.0946,1.0000 7.000,1.0646,0.02999,0.02043,-0.0304,0.0865,1.0000 7.250,1.0856,0.03154,0.02239,-0.0293,0.0793,1.0000 7.500,1.1079,0.03449,0.02523,-0.0290,0.0738,1.0000 7.750,1.1264,0.03680,0.02813,-0.0275,0.0705,1.0000 8.000,1.1440,0.03904,0.03068,-0.0263,0.0660,1.0000 8.250,1.1611,0.04205,0.03377,-0.0256,0.0626,1.0000 8.500,1.1708,0.04656,0.03877,-0.0241,0.0613,1.0000 8.750,1.1750,0.05023,0.04305,-0.0219,0.0605,1.0000 9.000,1.1737,0.05417,0.04756,-0.0196,0.0596,1.0000 9.250,1.1665,0.05837,0.05225,-0.0174,0.0587,1.0000 9.500,1.1537,0.06276,0.05703,-0.0154,0.0584,1.0000 9.750,1.1348,0.06711,0.06169,-0.0134,0.0585,1.0000 10.000,1.1122,0.07163,0.06642,-0.0123,0.0589,1.0000 10.250,1.0885,0.07698,0.07194,-0.0132,0.0595,1.0000 10.500,1.0656,0.08328,0.07838,-0.0160,0.0602,1.0000 10.750,1.0451,0.09040,0.08558,-0.0196,0.0609,1.0000 11.000,1.0286,0.09796,0.09319,-0.0231,0.0615,1.0000