Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe417-il-50000-n5 Airfoil,goe417-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,44.3683 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe417-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.500,-0.2793,0.10622,0.09992,-0.0228,1.0000,0.0558 -7.250,-0.2859,0.10501,0.09882,-0.0210,1.0000,0.0569 -7.000,-0.2919,0.10385,0.09776,-0.0197,1.0000,0.0581 -6.750,-0.2964,0.10289,0.09690,-0.0196,1.0000,0.0593 -6.500,-0.2990,0.10222,0.09632,-0.0207,1.0000,0.0601 -6.250,-0.2978,0.10163,0.09579,-0.0233,1.0000,0.0607 -6.000,-0.2915,0.10071,0.09490,-0.0269,1.0000,0.0610 -5.750,-0.2934,0.09511,0.08939,-0.0218,1.0000,0.0621 -5.500,-0.2929,0.09139,0.08574,-0.0184,1.0000,0.0643 -5.250,-0.2895,0.08891,0.08330,-0.0179,1.0000,0.0670 -5.000,-0.2830,0.08675,0.08117,-0.0191,1.0000,0.0711 -4.750,-0.2533,0.08697,0.08126,-0.0306,1.0000,0.0753 -4.500,-0.2486,0.08095,0.07537,-0.0271,0.9962,0.0779 -4.250,-0.2220,0.07710,0.07148,-0.0309,0.9899,0.0843 -4.000,-0.1709,0.07380,0.06800,-0.0436,0.9823,0.0912 -3.750,-0.1501,0.06948,0.06368,-0.0445,0.9766,0.0971 -3.500,-0.1102,0.06604,0.06010,-0.0522,0.9689,0.1075 -3.250,-0.0717,0.06273,0.05666,-0.0585,0.9619,0.1214 -3.000,-0.0328,0.05949,0.05329,-0.0645,0.9547,0.1356 -2.750,0.0042,0.05641,0.05006,-0.0694,0.9473,0.1504 -2.500,0.0375,0.05314,0.04671,-0.0728,0.9401,0.1676 -1.500,0.2344,0.04072,0.03280,-0.0955,0.9102,0.0999 -1.250,0.2793,0.03808,0.02967,-0.0988,0.8998,0.0867 -1.000,0.3247,0.03563,0.02681,-0.1022,0.8900,0.0810 -0.750,0.3737,0.03338,0.02396,-0.1055,0.8807,0.0775 -0.500,0.4105,0.03190,0.02223,-0.1071,0.8684,0.0811 -0.250,0.4487,0.03045,0.02041,-0.1085,0.8568,0.0810 0.000,0.4870,0.02912,0.01869,-0.1098,0.8462,0.0798 0.250,0.5288,0.02782,0.01701,-0.1114,0.8376,0.0794 0.500,0.5629,0.02696,0.01581,-0.1118,0.8250,0.0798 0.750,0.5964,0.02619,0.01480,-0.1120,0.8121,0.0807 1.000,0.6291,0.02549,0.01394,-0.1121,0.7988,0.0837 1.250,0.6607,0.02494,0.01321,-0.1120,0.7848,0.0899 1.500,0.6917,0.02434,0.01260,-0.1120,0.7700,0.0959 1.750,0.7221,0.02386,0.01204,-0.1117,0.7543,0.1012 2.000,0.7526,0.02341,0.01157,-0.1114,0.7377,0.1099 2.250,0.7837,0.02296,0.01119,-0.1113,0.7208,0.1338 2.500,0.8124,0.02136,0.01099,-0.1110,0.7020,1.0000 2.750,0.8408,0.02139,0.01071,-0.1103,0.6818,1.0000 3.000,0.8708,0.02139,0.01046,-0.1098,0.6624,1.0000 3.250,0.8983,0.02154,0.01041,-0.1091,0.6412,1.0000 3.500,0.9259,0.02172,0.01042,-0.1085,0.6201,1.0000 3.750,0.9529,0.02200,0.01051,-0.1078,0.5995,1.0000 4.000,0.9779,0.02238,0.01077,-0.1070,0.5781,1.0000 4.250,1.0035,0.02277,0.01107,-0.1062,0.5584,1.0000 4.500,1.0278,0.02324,0.01144,-0.1054,0.5390,1.0000 4.750,1.0512,0.02373,0.01187,-0.1044,0.5194,1.0000 5.000,1.0746,0.02422,0.01232,-0.1035,0.5006,1.0000 5.500,1.1196,0.02528,0.01327,-0.1014,0.4638,1.0000 5.750,1.1416,0.02586,0.01384,-0.1003,0.4466,1.0000 6.000,1.1637,0.02647,0.01450,-0.0993,0.4306,1.0000 6.250,1.1858,0.02711,0.01516,-0.0983,0.4157,1.0000 6.500,1.2079,0.02778,0.01589,-0.0974,0.4018,1.0000 6.750,1.2300,0.02849,0.01667,-0.0965,0.3886,1.0000 7.000,1.2522,0.02923,0.01752,-0.0956,0.3760,1.0000 7.250,1.2746,0.03000,0.01838,-0.0947,0.3641,1.0000 7.500,1.2951,0.03086,0.01942,-0.0937,0.3517,1.0000 7.750,1.3156,0.03176,0.02050,-0.0927,0.3398,1.0000 8.000,1.3366,0.03269,0.02164,-0.0917,0.3289,1.0000 8.250,1.3590,0.03359,0.02267,-0.0909,0.3191,1.0000 8.500,1.3775,0.03474,0.02414,-0.0897,0.3089,1.0000 8.750,1.3987,0.03585,0.02549,-0.0888,0.3006,1.0000 9.000,1.4165,0.03676,0.02661,-0.0874,0.2899,1.0000 9.250,1.4265,0.03757,0.02771,-0.0849,0.2760,1.0000 9.500,1.4334,0.03831,0.02868,-0.0821,0.2613,1.0000 9.750,1.4347,0.03898,0.02948,-0.0786,0.2446,1.0000 10.000,1.4299,0.03997,0.03071,-0.0746,0.2258,1.0000 10.250,1.4235,0.04118,0.03202,-0.0707,0.2058,1.0000 10.500,1.4163,0.04284,0.03371,-0.0674,0.1834,1.0000 10.750,1.4082,0.04507,0.03592,-0.0647,0.1590,1.0000 11.000,1.3998,0.04793,0.03879,-0.0626,0.1295,1.0000 11.500,1.3705,0.05621,0.04673,-0.0602,0.0655,1.0000 11.750,1.3539,0.06124,0.05170,-0.0601,0.0597,1.0000 12.000,1.3379,0.06661,0.05711,-0.0607,0.0558,1.0000 12.250,1.3242,0.07203,0.06272,-0.0616,0.0526,1.0000 12.500,1.3100,0.07783,0.06869,-0.0631,0.0502,1.0000 12.750,1.2961,0.08380,0.07483,-0.0649,0.0484,1.0000 13.000,1.2820,0.09000,0.08117,-0.0669,0.0468,1.0000 13.250,1.2686,0.09619,0.08746,-0.0690,0.0453,1.0000