Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe802a-il-50000 Airfoil,goe802a-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,27.4709 Max Cl/Cd alpha,8.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe802a-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.3259,0.10883,0.10192,-0.0256,1.0000,0.0921 -8.500,-0.3282,0.10672,0.09990,-0.0273,1.0000,0.0930 -8.250,-0.3275,0.10397,0.09724,-0.0280,1.0000,0.0938 -8.000,-0.3224,0.10075,0.09407,-0.0277,1.0000,0.0952 -7.750,-0.3228,0.09823,0.09165,-0.0283,1.0000,0.0965 -7.500,-0.3255,0.09597,0.08949,-0.0295,1.0000,0.0975 -7.250,-0.3300,0.09396,0.08756,-0.0309,1.0000,0.0981 -7.000,-0.3294,0.09117,0.08485,-0.0301,1.0000,0.0989 -6.750,-0.3292,0.08858,0.08233,-0.0291,1.0000,0.1002 -6.500,-0.3307,0.08626,0.08005,-0.0289,1.0000,0.1016 -6.250,-0.3320,0.08402,0.07783,-0.0299,1.0000,0.1028 -6.000,-0.3305,0.08142,0.07525,-0.0299,1.0000,0.1038 -5.750,-0.3277,0.07875,0.07262,-0.0290,1.0000,0.1056 -5.500,-0.3229,0.07621,0.07003,-0.0302,1.0000,0.1077 -5.250,-0.3169,0.07343,0.06724,-0.0304,1.0000,0.1094 -5.000,-0.3089,0.07075,0.06448,-0.0312,1.0000,0.1127 -4.750,-0.3009,0.06795,0.06168,-0.0312,1.0000,0.1159 -4.500,-0.2910,0.06514,0.05882,-0.0319,1.0000,0.1209 -4.000,-0.2722,0.06022,0.05388,-0.0320,1.0000,0.1437 -3.750,-0.2613,0.05828,0.05194,-0.0320,1.0000,0.1593 -3.500,-0.2481,0.05650,0.05011,-0.0322,1.0000,0.1727 -3.250,-0.2326,0.05480,0.04833,-0.0330,1.0000,0.1863 -3.000,-0.2169,0.05308,0.04657,-0.0336,1.0000,0.1997 -2.750,-0.2004,0.05133,0.04479,-0.0341,1.0000,0.2126 -2.500,-0.1806,0.04961,0.04297,-0.0355,1.0000,0.2231 -2.250,-0.1591,0.04810,0.04132,-0.0370,1.0000,0.2282 -2.000,-0.1112,0.04604,0.03896,-0.0434,0.9926,0.2371 -1.750,-0.0507,0.04413,0.03671,-0.0515,0.9790,0.2478 -1.500,0.0104,0.04223,0.03441,-0.0591,0.9652,0.2480 -1.250,0.0683,0.04044,0.03229,-0.0656,0.9507,0.2450 -1.000,0.1216,0.03904,0.03052,-0.0709,0.9352,0.2409 -0.750,0.1727,0.03804,0.02906,-0.0753,0.9195,0.2360 -0.500,0.2206,0.03726,0.02790,-0.0789,0.9037,0.2329 -0.250,0.2665,0.03651,0.02686,-0.0820,0.8882,0.2335 0.000,0.3128,0.03567,0.02583,-0.0849,0.8735,0.2317 0.250,0.3735,0.03474,0.02448,-0.0890,0.8614,0.2180 0.500,0.4140,0.03417,0.02378,-0.0904,0.8454,0.2089 0.750,0.4513,0.03390,0.02332,-0.0911,0.8298,0.2028 1.000,0.4859,0.03362,0.02304,-0.0917,0.8147,0.2050 1.250,0.5212,0.03338,0.02280,-0.0923,0.8004,0.2118 1.500,0.5676,0.03261,0.02205,-0.0939,0.7895,0.2293 1.750,0.5950,0.03100,0.02228,-0.0933,0.7740,1.0000 2.000,0.6210,0.03155,0.02253,-0.0923,0.7584,1.0000 2.250,0.6473,0.03211,0.02285,-0.0915,0.7439,1.0000 2.500,0.6782,0.03238,0.02291,-0.0911,0.7313,1.0000 2.750,0.7104,0.03249,0.02286,-0.0907,0.7194,1.0000 3.000,0.7294,0.03352,0.02380,-0.0897,0.7046,1.0000 3.250,0.7509,0.03440,0.02462,-0.0888,0.6911,1.0000 3.500,0.7903,0.03390,0.02400,-0.0887,0.6825,1.0000 3.750,0.8050,0.03531,0.02540,-0.0875,0.6677,1.0000 4.000,0.8218,0.03664,0.02672,-0.0865,0.6542,1.0000 4.250,0.8522,0.03677,0.02681,-0.0858,0.6436,1.0000 4.500,0.8787,0.03709,0.02712,-0.0848,0.6311,1.0000 4.750,0.8959,0.03817,0.02821,-0.0834,0.6163,1.0000 5.000,0.9179,0.03881,0.02885,-0.0821,0.6025,1.0000 5.250,0.9532,0.03815,0.02817,-0.0810,0.5907,1.0000 5.500,0.9798,0.03832,0.02834,-0.0798,0.5773,1.0000 5.750,0.9946,0.03967,0.02975,-0.0784,0.5624,1.0000 6.000,1.0133,0.04069,0.03083,-0.0770,0.5484,1.0000 6.250,1.0433,0.04058,0.03075,-0.0758,0.5355,1.0000 6.500,1.0776,0.04005,0.03018,-0.0748,0.5224,1.0000 6.750,1.0927,0.04135,0.03158,-0.0732,0.5066,1.0000 7.000,1.1088,0.04253,0.03289,-0.0715,0.4907,1.0000 7.250,1.1267,0.04359,0.03403,-0.0699,0.4750,1.0000 7.500,1.1474,0.04433,0.03483,-0.0683,0.4590,1.0000 7.750,1.1696,0.04497,0.03551,-0.0668,0.4432,1.0000 8.000,1.1939,0.04551,0.03608,-0.0655,0.4280,1.0000 8.250,1.2217,0.04568,0.03628,-0.0642,0.4125,1.0000 8.500,1.2524,0.04559,0.03612,-0.0632,0.3969,1.0000 8.750,1.2573,0.04782,0.03856,-0.0610,0.3820,1.0000 9.000,1.2573,0.05052,0.04146,-0.0587,0.3682,1.0000 9.250,1.2701,0.05187,0.04292,-0.0568,0.3540,1.0000 9.500,1.2944,0.05211,0.04317,-0.0554,0.3397,1.0000 9.750,1.3275,0.05170,0.04269,-0.0545,0.3254,1.0000 10.000,1.3041,0.05641,0.04773,-0.0513,0.3164,1.0000 10.250,1.3183,0.05790,0.04929,-0.0497,0.3057,1.0000 10.500,0.9992,0.10528,0.09654,-0.0631,0.3213,1.0000 10.750,1.0419,0.10230,0.09372,-0.0591,0.3082,1.0000