Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag455ct02r-il-50000-n5 Airfoil,ag455ct02r-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,33.9538 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-ag455ct02r-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4520,0.09707,0.09077,0.0068,1.0000,0.1037 -8.000,-0.4531,0.09048,0.08415,0.0031,1.0000,0.0639 -7.750,-0.4576,0.08516,0.07887,-0.0004,1.0000,0.0531 -7.500,-0.4541,0.08089,0.07463,-0.0008,1.0000,0.0507 -7.250,-0.5395,0.08761,0.08111,0.0014,1.0000,0.0522 -7.000,-0.5305,0.08295,0.07646,-0.0015,1.0000,0.0491 -6.500,-0.5034,0.06997,0.06327,-0.0159,1.0000,0.0414 -6.250,-0.4898,0.06542,0.05866,-0.0181,1.0000,0.0406 -6.000,-0.4741,0.06059,0.05366,-0.0210,1.0000,0.0398 -5.750,-0.4559,0.05560,0.04845,-0.0241,1.0000,0.0395 -5.500,-0.4354,0.05065,0.04318,-0.0269,1.0000,0.0398 -5.250,-0.4128,0.04589,0.03797,-0.0293,1.0000,0.0405 -5.000,-0.3886,0.04163,0.03317,-0.0309,1.0000,0.0413 -4.750,-0.3634,0.03784,0.02881,-0.0318,1.0000,0.0418 -4.500,-0.3374,0.03441,0.02483,-0.0321,1.0000,0.0421 -4.250,-0.3114,0.03121,0.02121,-0.0323,1.0000,0.0428 -4.000,-0.2855,0.02860,0.01830,-0.0322,1.0000,0.0446 -3.750,-0.2591,0.02674,0.01614,-0.0319,1.0000,0.0496 -3.500,-0.2312,0.02488,0.01377,-0.0313,1.0000,0.0548 -3.250,-0.2053,0.02301,0.01188,-0.0306,1.0000,0.0597 -3.000,-0.1787,0.02163,0.01035,-0.0300,1.0000,0.0714 -2.750,-0.1522,0.02030,0.00894,-0.0293,1.0000,0.0865 -2.500,-0.1254,0.01904,0.00772,-0.0290,1.0000,0.1217 -2.250,-0.0995,0.01745,0.00673,-0.0290,1.0000,0.2239 -2.000,-0.0802,0.01541,0.00624,-0.0277,1.0000,0.5190 -1.750,-0.0464,0.01398,0.00570,-0.0262,1.0000,1.0000 -1.500,-0.0211,0.01395,0.00528,-0.0258,1.0000,1.0000 -1.250,0.0040,0.01394,0.00493,-0.0255,1.0000,1.0000 -1.000,0.0286,0.01396,0.00469,-0.0251,1.0000,1.0000 -0.750,0.0530,0.01400,0.00454,-0.0247,1.0000,1.0000 -0.500,0.0768,0.01407,0.00446,-0.0243,1.0000,1.0000 -0.250,0.1000,0.01419,0.00446,-0.0240,1.0000,1.0000 0.000,0.1237,0.01437,0.00453,-0.0240,0.9984,1.0000 0.250,0.1734,0.01458,0.00460,-0.0288,0.9654,1.0000 0.500,0.2195,0.01476,0.00467,-0.0326,0.9301,1.0000 0.750,0.2621,0.01492,0.00472,-0.0353,0.8934,1.0000 1.000,0.3006,0.01508,0.00478,-0.0369,0.8573,1.0000 1.250,0.3329,0.01529,0.00487,-0.0371,0.8215,1.0000 1.500,0.3615,0.01554,0.00499,-0.0365,0.7887,1.0000 1.750,0.3878,0.01583,0.00513,-0.0354,0.7581,1.0000 2.000,0.4130,0.01617,0.00534,-0.0342,0.7289,1.0000 2.250,0.4379,0.01655,0.00560,-0.0330,0.7009,1.0000 2.500,0.4628,0.01691,0.00596,-0.0321,0.6706,1.0000 2.750,0.4876,0.01723,0.00625,-0.0311,0.6410,1.0000 3.000,0.5124,0.01755,0.00653,-0.0300,0.6114,1.0000 3.250,0.5371,0.01786,0.00680,-0.0290,0.5816,1.0000 3.500,0.5619,0.01819,0.00708,-0.0280,0.5515,1.0000 3.750,0.5867,0.01855,0.00748,-0.0271,0.5197,1.0000 4.000,0.6114,0.01894,0.00784,-0.0262,0.4879,1.0000 4.250,0.6361,0.01937,0.00824,-0.0253,0.4563,1.0000 4.500,0.6607,0.01986,0.00868,-0.0245,0.4246,1.0000 4.750,0.6858,0.02040,0.00929,-0.0239,0.3921,1.0000 5.000,0.7106,0.02099,0.00988,-0.0233,0.3605,1.0000 5.250,0.7351,0.02165,0.01053,-0.0226,0.3300,1.0000 5.500,0.7594,0.02239,0.01126,-0.0221,0.3008,1.0000 5.750,0.7834,0.02319,0.01206,-0.0215,0.2724,1.0000 6.000,0.8071,0.02407,0.01304,-0.0210,0.2451,1.0000 6.250,0.8307,0.02503,0.01408,-0.0204,0.2193,1.0000 6.500,0.8538,0.02609,0.01523,-0.0199,0.1952,1.0000 6.750,0.8763,0.02724,0.01641,-0.0193,0.1736,1.0000 7.000,0.8986,0.02853,0.01784,-0.0187,0.1533,1.0000 7.250,0.9198,0.02988,0.01924,-0.0182,0.1351,1.0000 7.500,0.9414,0.03150,0.02110,-0.0175,0.1188,1.0000 7.750,0.9618,0.03318,0.02298,-0.0169,0.1036,1.0000 8.000,0.9815,0.03513,0.02511,-0.0161,0.0916,1.0000 8.250,1.0003,0.03716,0.02725,-0.0154,0.0818,1.0000 8.500,1.0178,0.03924,0.02961,-0.0148,0.0719,1.0000 8.750,1.0342,0.04248,0.03331,-0.0140,0.0661,1.0000 9.000,1.0488,0.04490,0.03602,-0.0134,0.0598,1.0000 9.250,1.0587,0.04844,0.04002,-0.0128,0.0549,1.0000 9.500,1.0646,0.05267,0.04477,-0.0124,0.0520,1.0000 9.750,1.0669,0.05690,0.04939,-0.0122,0.0500,1.0000 10.000,1.0689,0.06047,0.05317,-0.0121,0.0480,1.0000 10.250,1.0665,0.06444,0.05725,-0.0122,0.0464,1.0000 10.500,1.0499,0.06962,0.06276,-0.0133,0.0461,1.0000 10.750,1.0315,0.07534,0.06867,-0.0162,0.0462,1.0000 11.000,1.0135,0.08203,0.07550,-0.0209,0.0465,1.0000