Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe433-il-50000 Airfoil,goe433-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,5.66052 Max Cl/Cd alpha,2.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe433-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.2082,0.13172,0.12411,-0.0361,1.0000,0.2756 -10.500,-0.2104,0.13065,0.12313,-0.0344,1.0000,0.2824 -10.250,-0.2462,0.13383,0.12646,-0.0320,1.0000,0.2875 -10.000,-0.2433,0.13058,0.12329,-0.0299,1.0000,0.2901 -9.750,-0.2332,0.12775,0.12052,-0.0274,1.0000,0.2946 -9.500,-0.2400,0.12708,0.11994,-0.0247,1.0000,0.2999 -9.250,-0.2662,0.12852,0.12151,-0.0217,1.0000,0.3057 -8.750,-0.2826,0.12604,0.11921,-0.0167,1.0000,0.3120 -8.500,-0.2833,0.12486,0.11810,-0.0142,1.0000,0.3176 -8.250,-0.3038,0.12547,0.11881,-0.0115,1.0000,0.3245 -8.000,-0.3588,0.12926,0.12275,-0.0083,1.0000,0.3276 -7.750,-0.3230,0.12317,0.11666,-0.0075,1.0000,0.3320 -7.500,-0.3217,0.12170,0.11522,-0.0056,1.0000,0.3378 -7.250,-0.3467,0.12231,0.11592,-0.0032,1.0000,0.3453 -7.000,-0.3482,0.11998,0.11362,-0.0041,0.9970,0.3499 -6.750,-0.3108,0.11617,0.10974,-0.0080,0.9903,0.3622 -6.500,-0.3117,0.11416,0.10776,-0.0105,0.9828,0.3700 -6.250,-0.2781,0.11071,0.10424,-0.0139,0.9761,0.3810 -6.000,-0.2958,0.11003,0.10362,-0.0144,0.9680,0.3888 -5.750,-0.2549,0.10626,0.09977,-0.0177,0.9609,0.4018 -5.500,-0.2656,0.10502,0.09858,-0.0174,0.9529,0.4096 -5.250,-0.2384,0.10236,0.09586,-0.0198,0.9456,0.4224 -5.000,-0.2692,0.10228,0.09587,-0.0166,0.9371,0.4283 -4.750,-0.3494,0.08386,0.07716,-0.0454,0.9331,0.2877 -4.500,-0.3349,0.08266,0.07599,-0.0430,0.9255,0.2912 -4.250,-0.3156,0.07633,0.06949,-0.0522,0.9184,0.2823 -4.000,-0.2746,0.06807,0.06089,-0.0678,0.9118,0.2796 -3.750,-0.2320,0.05996,0.05220,-0.0836,0.9042,0.2855 -3.500,-0.1880,0.05811,0.05021,-0.0889,0.8960,0.2940 -3.250,-0.1521,0.05525,0.04696,-0.0957,0.8875,0.3056 -3.000,-0.1190,0.05490,0.04664,-0.0973,0.8791,0.3149 -2.750,-0.0798,0.05330,0.04471,-0.1028,0.8705,0.3299 -2.500,-0.0543,0.05358,0.04506,-0.1028,0.8616,0.3406 -2.250,-0.0193,0.05343,0.04483,-0.1052,0.8532,0.3552 -2.000,0.0082,0.05313,0.04439,-0.1072,0.8440,0.3704 -1.750,0.0515,0.05336,0.04456,-0.1101,0.8356,0.3894 -1.500,0.0567,0.05418,0.04549,-0.1074,0.8267,0.3986 -1.250,0.0994,0.05450,0.04577,-0.1099,0.8183,0.4189 -1.000,0.1110,0.05510,0.04635,-0.1092,0.8092,0.4323 -0.750,0.1431,0.05553,0.04675,-0.1105,0.8008,0.4517 -0.500,0.1675,0.05622,0.04742,-0.1110,0.7928,0.4707 -0.250,0.1855,0.05691,0.04809,-0.1110,0.7844,0.4892 0.000,0.2301,0.05731,0.04852,-0.1125,0.7768,0.5159 0.250,0.2272,0.05854,0.04974,-0.1108,0.7692,0.5304 0.500,0.2503,0.05927,0.05051,-0.1107,0.7620,0.5529 0.750,0.2779,0.06001,0.05126,-0.1109,0.7546,0.5786 1.000,0.2820,0.06127,0.05256,-0.1096,0.7482,0.5961 1.250,0.3051,0.06219,0.05349,-0.1099,0.7422,0.6218 1.500,0.3330,0.06304,0.05436,-0.1101,0.7356,0.6492 1.750,0.3333,0.06464,0.05600,-0.1088,0.7308,0.6672 2.000,0.3426,0.06604,0.05745,-0.1077,0.7269,0.6887 2.250,0.3539,0.06747,0.05894,-0.1067,0.7244,0.7124 2.500,0.3865,0.06828,0.05977,-0.1068,0.7170,0.7481 2.750,0.3866,0.07006,0.06163,-0.1052,0.7158,0.7701 3.000,0.3949,0.07185,0.06348,-0.1044,0.7165,0.7977 3.250,0.3005,0.07847,0.07036,-0.1032,0.8249,0.7727 3.500,0.3338,0.08078,0.07274,-0.1046,0.8180,0.8160 3.750,0.3317,0.08130,0.07335,-0.1019,0.8127,0.8442 4.000,0.3426,0.08182,0.07401,-0.1003,0.8026,0.8910 4.250,0.3736,0.08443,0.07665,-0.1036,0.7959,1.0000 4.500,0.3875,0.08553,0.07767,-0.1052,0.7826,1.0000 4.750,0.4459,0.09075,0.08268,-0.1135,0.7769,1.0000 5.000,0.4380,0.09064,0.08255,-0.1115,0.7639,1.0000 5.250,0.4948,0.09590,0.08762,-0.1184,0.7571,1.0000 5.500,0.4828,0.09569,0.08738,-0.1156,0.7439,1.0000 5.750,0.5285,0.10040,0.09194,-0.1203,0.7371,1.0000 6.000,0.5270,0.10086,0.09237,-0.1186,0.7223,1.0000 6.250,0.5381,0.10321,0.09466,-0.1188,0.7122,1.0000 6.500,0.5806,0.10704,0.09841,-0.1220,0.6999,1.0000 6.750,0.5771,0.10796,0.09931,-0.1201,0.6849,1.0000 7.000,0.5882,0.11030,0.10162,-0.1200,0.6719,1.0000 7.250,0.6321,0.11464,0.10589,-0.1229,0.6602,1.0000 7.500,0.6383,0.11597,0.10722,-0.1219,0.6434,1.0000 7.750,0.6362,0.11776,0.10902,-0.1208,0.6292,1.0000 8.000,0.6548,0.12098,0.11223,-0.1214,0.6176,1.0000 8.500,0.6790,0.12586,0.11712,-0.1213,0.5878,1.0000 8.750,0.6936,0.12940,0.12066,-0.1218,0.5785,1.0000 9.000,0.7229,0.13259,0.12385,-0.1226,0.5637,1.0000 9.250,0.7069,0.13461,0.12589,-0.1217,0.5539,1.0000 9.500,0.7555,0.13963,0.13091,-0.1236,0.5429,1.0000 9.750,0.7259,0.14064,0.13194,-0.1224,0.5352,1.0000 10.000,0.7555,0.14441,0.13572,-0.1234,0.5259,1.0000