Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe393-il-50000-n5 Airfoil,goe393-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,39.4407 Max Cl/Cd alpha,7.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe393-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4466,0.11107,0.10438,0.0084,1.0000,0.0902 -8.000,-0.4451,0.10917,0.10255,0.0048,1.0000,0.0912 -7.750,-0.4401,0.10701,0.10046,-0.0006,1.0000,0.0918 -7.500,-0.4307,0.10310,0.09661,-0.0038,1.0000,0.0925 -7.250,-0.4177,0.09724,0.09076,0.0014,1.0000,0.0964 -7.000,-0.4073,0.09392,0.08747,-0.0007,1.0000,0.1000 -6.750,-0.3960,0.09090,0.08447,-0.0051,1.0000,0.1034 -6.500,-0.3802,0.08840,0.08195,-0.0131,1.0000,0.1054 -6.250,-0.3607,0.08550,0.07896,-0.0204,1.0000,0.1060 -6.000,-0.3521,0.08010,0.07367,-0.0168,1.0000,0.1077 -5.750,-0.3390,0.07652,0.07012,-0.0162,1.0000,0.1128 -5.500,-0.3099,0.07443,0.06782,-0.0266,1.0000,0.1199 -5.250,-0.2962,0.06990,0.06338,-0.0264,1.0000,0.1213 -5.000,-0.2804,0.06620,0.05970,-0.0267,1.0000,0.1234 -4.750,-0.2604,0.06288,0.05636,-0.0287,1.0000,0.1257 -4.500,-0.2378,0.05963,0.05302,-0.0314,1.0000,0.1272 -4.000,-0.1745,0.05099,0.04382,-0.0408,1.0000,0.0905 -3.750,-0.1544,0.04793,0.04075,-0.0415,1.0000,0.0874 -3.500,-0.1318,0.04498,0.03767,-0.0430,1.0000,0.0845 -3.250,-0.1022,0.04183,0.03428,-0.0459,0.9932,0.0820 -3.000,-0.0524,0.03800,0.02995,-0.0521,0.9671,0.0804 -2.750,-0.0100,0.03575,0.02746,-0.0562,0.9391,0.0842 -2.500,0.0323,0.03336,0.02466,-0.0598,0.9113,0.0877 -2.250,0.0723,0.03100,0.02182,-0.0624,0.8851,0.0881 -2.000,0.1092,0.02896,0.01927,-0.0640,0.8606,0.0892 -1.750,0.1429,0.02721,0.01696,-0.0647,0.8375,0.0910 -1.500,0.1731,0.02586,0.01523,-0.0646,0.8165,0.0936 -1.250,0.2011,0.02495,0.01407,-0.0642,0.7965,0.0979 -1.000,0.2292,0.02418,0.01290,-0.0637,0.7779,0.1075 -0.750,0.2558,0.02356,0.01203,-0.0630,0.7606,0.1180 -0.500,0.2836,0.02285,0.01106,-0.0623,0.7447,0.1283 -0.250,0.3115,0.02248,0.01042,-0.0618,0.7296,0.1480 0.000,0.3385,0.02210,0.01000,-0.0614,0.7151,0.1679 0.250,0.3656,0.02177,0.00954,-0.0608,0.7016,0.1830 0.500,0.3924,0.02153,0.00915,-0.0601,0.6889,0.1941 0.750,0.4187,0.02133,0.00889,-0.0594,0.6769,0.2032 1.000,0.4448,0.02122,0.00877,-0.0589,0.6645,0.2173 1.250,0.4711,0.02115,0.00872,-0.0584,0.6523,0.2313 1.500,0.4976,0.02110,0.00871,-0.0580,0.6409,0.2473 1.750,0.5239,0.02100,0.00875,-0.0575,0.6303,0.2783 2.000,0.5536,0.01960,0.00877,-0.0576,0.6192,1.0000 2.250,0.5802,0.01998,0.00894,-0.0572,0.6081,1.0000 2.500,0.6068,0.02036,0.00916,-0.0567,0.5980,1.0000 2.750,0.6332,0.02073,0.00942,-0.0562,0.5883,1.0000 3.000,0.6595,0.02118,0.00983,-0.0559,0.5777,1.0000 3.250,0.6857,0.02160,0.01020,-0.0554,0.5686,1.0000 3.500,0.7118,0.02205,0.01065,-0.0550,0.5592,1.0000 3.750,0.7378,0.02257,0.01121,-0.0548,0.5497,1.0000 4.000,0.7639,0.02300,0.01163,-0.0542,0.5420,1.0000 4.250,0.7895,0.02361,0.01237,-0.0540,0.5322,1.0000 4.500,0.8153,0.02410,0.01288,-0.0535,0.5248,1.0000 4.750,0.8407,0.02475,0.01368,-0.0533,0.5156,1.0000 5.000,0.8661,0.02534,0.01440,-0.0529,0.5077,1.0000 5.250,0.8912,0.02584,0.01502,-0.0523,0.4981,1.0000 5.500,0.9154,0.02620,0.01549,-0.0515,0.4846,1.0000 5.750,0.9393,0.02617,0.01549,-0.0501,0.4678,1.0000 6.000,0.9628,0.02615,0.01557,-0.0488,0.4491,1.0000 6.250,0.9861,0.02634,0.01592,-0.0478,0.4313,1.0000 6.500,1.0097,0.02661,0.01635,-0.0469,0.4154,1.0000 6.750,1.0332,0.02693,0.01685,-0.0459,0.3993,1.0000 7.000,1.0562,0.02720,0.01733,-0.0449,0.3813,1.0000 7.250,1.0786,0.02746,0.01773,-0.0437,0.3604,1.0000 7.500,1.1000,0.02789,0.01835,-0.0426,0.3355,1.0000 7.750,1.1203,0.02845,0.01907,-0.0414,0.3065,1.0000 8.000,1.1387,0.02922,0.01995,-0.0402,0.2700,1.0000 8.250,1.1547,0.03029,0.02094,-0.0390,0.2300,1.0000 8.500,1.1674,0.03181,0.02224,-0.0378,0.1934,1.0000 8.750,1.1773,0.03379,0.02401,-0.0366,0.1667,1.0000 9.000,1.1847,0.03605,0.02611,-0.0354,0.1467,1.0000 9.250,1.1917,0.03836,0.02848,-0.0342,0.1267,1.0000 9.500,1.1961,0.04082,0.03097,-0.0331,0.1101,1.0000 9.750,1.1985,0.04339,0.03359,-0.0319,0.0966,1.0000 10.000,1.1991,0.04602,0.03632,-0.0305,0.0865,1.0000 10.250,1.1978,0.04877,0.03904,-0.0295,0.0786,1.0000 10.500,1.2004,0.05160,0.04211,-0.0286,0.0708,1.0000 10.750,1.2016,0.05446,0.04496,-0.0280,0.0657,1.0000 11.000,1.2049,0.05751,0.04828,-0.0274,0.0604,1.0000 11.250,1.2057,0.06068,0.05161,-0.0275,0.0563,1.0000 11.500,1.2069,0.06368,0.05459,-0.0274,0.0534,1.0000 11.750,1.2094,0.06732,0.05856,-0.0269,0.0510,1.0000 12.000,1.2072,0.07147,0.06302,-0.0272,0.0490,1.0000 12.250,1.2019,0.07596,0.06775,-0.0282,0.0474,1.0000 12.500,1.1949,0.08068,0.07267,-0.0297,0.0461,1.0000 12.750,1.1869,0.08557,0.07771,-0.0314,0.0450,1.0000 13.000,1.1794,0.09043,0.08268,-0.0332,0.0439,1.0000 13.250,1.1731,0.09519,0.08748,-0.0346,0.0429,1.0000 13.500,1.1561,0.10234,0.09486,-0.0382,0.0428,1.0000 13.750,1.1379,0.11008,0.10280,-0.0424,0.0429,1.0000