Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag36-il-50000 Airfoil,ag36-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,32.7008 Max Cl/Cd alpha,5.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-ag36-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.4895,0.09444,0.08799,0.0018,1.0000,0.2663 -8.500,-0.4906,0.09167,0.08531,0.0005,1.0000,0.2801 -8.250,-0.4815,0.08789,0.08157,0.0013,1.0000,0.2953 -8.000,-0.4654,0.08392,0.07761,0.0039,1.0000,0.3141 -7.750,-0.4681,0.08157,0.07535,0.0029,1.0000,0.3373 -7.500,-0.4518,0.07772,0.07151,0.0064,1.0000,0.3621 -7.250,-0.4444,0.07457,0.06842,0.0083,1.0000,0.3888 -7.000,-0.4371,0.07152,0.06543,0.0103,1.0000,0.4172 -6.750,-0.4279,0.06850,0.06246,0.0130,1.0000,0.4486 -6.000,-0.3460,0.04091,0.03273,-0.0394,1.0000,0.1416 -5.750,-0.3203,0.03673,0.02781,-0.0401,1.0000,0.1316 -5.500,-0.2961,0.03370,0.02428,-0.0398,1.0000,0.1317 -5.250,-0.2707,0.03111,0.02107,-0.0394,1.0000,0.1339 -5.000,-0.2453,0.02859,0.01818,-0.0387,1.0000,0.1358 -4.750,-0.2208,0.02659,0.01607,-0.0379,1.0000,0.1425 -4.500,-0.1956,0.02490,0.01416,-0.0370,1.0000,0.1550 -4.250,-0.1695,0.02325,0.01237,-0.0361,1.0000,0.1690 -4.000,-0.1442,0.02185,0.01102,-0.0351,1.0000,0.1986 -3.750,-0.1172,0.02024,0.00969,-0.0344,1.0000,0.2615 -3.500,-0.0799,0.01576,0.00810,-0.0323,1.0000,1.0000 -3.250,-0.0584,0.01582,0.00759,-0.0314,1.0000,1.0000 -3.000,-0.0373,0.01591,0.00728,-0.0305,1.0000,1.0000 -2.750,-0.0163,0.01605,0.00709,-0.0298,1.0000,1.0000 -2.500,0.0047,0.01624,0.00697,-0.0291,1.0000,1.0000 -2.250,0.0255,0.01647,0.00697,-0.0285,1.0000,1.0000 -2.000,0.0461,0.01676,0.00706,-0.0280,1.0000,1.0000 -1.750,0.0663,0.01711,0.00725,-0.0276,1.0000,1.0000 -1.500,0.0859,0.01756,0.00755,-0.0273,1.0000,1.0000 -1.250,0.1046,0.01811,0.00797,-0.0272,1.0000,1.0000 -1.000,0.1225,0.01878,0.00855,-0.0273,1.0000,1.0000 -0.750,0.1396,0.01958,0.00926,-0.0276,1.0000,1.0000 -0.500,0.1594,0.02046,0.01007,-0.0285,0.9985,1.0000 -0.250,0.2249,0.02143,0.01094,-0.0374,0.9764,1.0000 0.000,0.2889,0.02223,0.01170,-0.0455,0.9552,1.0000 0.250,0.3414,0.02282,0.01232,-0.0511,0.9316,1.0000 0.500,0.3974,0.02325,0.01279,-0.0568,0.9099,1.0000 0.750,0.4475,0.02355,0.01319,-0.0610,0.8875,1.0000 1.000,0.4936,0.02373,0.01345,-0.0640,0.8657,1.0000 1.250,0.5360,0.02383,0.01365,-0.0659,0.8438,1.0000 1.500,0.5717,0.02398,0.01392,-0.0664,0.8211,1.0000 1.750,0.6067,0.02402,0.01405,-0.0663,0.7987,1.0000 2.000,0.6342,0.02428,0.01439,-0.0652,0.7742,1.0000 2.250,0.6634,0.02434,0.01452,-0.0637,0.7510,1.0000 2.500,0.6891,0.02451,0.01480,-0.0619,0.7259,1.0000 2.750,0.7130,0.02476,0.01513,-0.0600,0.6994,1.0000 3.000,0.7371,0.02494,0.01538,-0.0579,0.6728,1.0000 3.250,0.7615,0.02505,0.01554,-0.0557,0.6458,1.0000 3.500,0.7858,0.02523,0.01578,-0.0534,0.6180,1.0000 3.750,0.8094,0.02561,0.01618,-0.0513,0.5883,1.0000 4.000,0.8323,0.02616,0.01674,-0.0492,0.5569,1.0000 4.250,0.8552,0.02675,0.01732,-0.0472,0.5247,1.0000 4.500,0.8783,0.02730,0.01787,-0.0451,0.4921,1.0000 4.750,0.8990,0.02801,0.01870,-0.0433,0.4563,1.0000 5.000,0.9219,0.02836,0.01898,-0.0413,0.4221,1.0000 5.250,0.9429,0.02897,0.01961,-0.0394,0.3857,1.0000 5.500,0.9650,0.02951,0.02002,-0.0375,0.3500,1.0000 5.750,0.9844,0.03057,0.02108,-0.0357,0.3122,1.0000 6.000,1.0039,0.03173,0.02209,-0.0339,0.2748,1.0000 6.250,1.0221,0.03308,0.02326,-0.0321,0.2368,1.0000 6.500,1.0377,0.03495,0.02514,-0.0302,0.2008,1.0000 6.750,1.0543,0.03711,0.02721,-0.0285,0.1699,1.0000 7.000,1.0703,0.03979,0.03001,-0.0270,0.1465,1.0000 7.250,1.0866,0.04270,0.03308,-0.0255,0.1297,1.0000 7.500,1.1000,0.04624,0.03697,-0.0240,0.1188,1.0000 7.750,1.1151,0.04980,0.04064,-0.0228,0.1103,1.0000 8.000,1.1171,0.05394,0.04546,-0.0208,0.1052,1.0000 8.250,1.1319,0.05752,0.04907,-0.0199,0.0996,1.0000 8.500,1.1319,0.06265,0.05458,-0.0185,0.0982,1.0000 8.750,1.1227,0.06769,0.06009,-0.0169,0.0979,1.0000 9.000,1.1096,0.07281,0.06557,-0.0158,0.0979,1.0000 9.250,1.0942,0.07798,0.07099,-0.0150,0.0982,1.0000 9.500,1.0773,0.08307,0.07624,-0.0145,0.0986,1.0000 9.750,0.9701,0.09871,0.09220,-0.0275,0.1143,1.0000