Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe223-il-50000-n5 Airfoil,goe223-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,15.8333 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe223-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.2596,0.10927,0.10280,-0.0745,0.9678,0.0681 -10.500,-0.2598,0.10240,0.09593,-0.0797,0.9615,0.0675 -10.250,-0.2695,0.09417,0.08767,-0.0859,0.9552,0.0666 -10.000,-0.2948,0.08486,0.07830,-0.0931,0.9468,0.0654 -9.750,-0.3313,0.07647,0.06979,-0.0996,0.9356,0.0643 -9.500,-0.3672,0.07000,0.06311,-0.1047,0.9231,0.0635 -9.250,-0.3783,0.06390,0.05666,-0.1121,0.9131,0.0633 -9.000,-0.3851,0.06053,0.05304,-0.1136,0.9021,0.0635 -8.750,-0.3664,0.05686,0.04902,-0.1180,0.8966,0.0649 -8.500,-0.3629,0.05456,0.04648,-0.1179,0.8861,0.0661 -8.250,-0.3359,0.05144,0.04291,-0.1216,0.8810,0.0679 -8.000,-0.3252,0.04959,0.04077,-0.1209,0.8711,0.0688 -7.750,-0.2937,0.04739,0.03820,-0.1228,0.8660,0.0699 -7.500,-0.2757,0.04613,0.03685,-0.1216,0.8575,0.0710 -7.250,-0.2470,0.04491,0.03562,-0.1220,0.8514,0.0735 -7.000,-0.2198,0.04382,0.03439,-0.1221,0.8450,0.0764 -6.750,-0.1991,0.04297,0.03342,-0.1210,0.8363,0.0787 -6.500,-0.1653,0.04194,0.03220,-0.1214,0.8318,0.0810 -6.250,-0.1524,0.04139,0.03168,-0.1193,0.8209,0.0828 -6.000,-0.1207,0.04028,0.03054,-0.1203,0.8157,0.0864 -5.750,-0.1046,0.03966,0.02985,-0.1194,0.8050,0.0905 -5.500,-0.0720,0.03843,0.02855,-0.1213,0.7993,0.0970 -5.250,-0.0522,0.03757,0.02764,-0.1216,0.7889,0.1036 -5.000,-0.0168,0.03589,0.02593,-0.1250,0.7829,0.1160 -4.750,0.0131,0.03385,0.02420,-0.1289,0.7737,0.1509 -4.500,0.0430,0.03408,0.02538,-0.1293,0.7664,0.3406 -4.250,0.0677,0.03500,0.02606,-0.1284,0.7570,0.3823 -4.000,0.0949,0.03595,0.02684,-0.1273,0.7495,0.4135 -3.750,0.1160,0.03674,0.02752,-0.1253,0.7409,0.4316 -3.500,0.1395,0.03734,0.02800,-0.1237,0.7331,0.4489 -3.250,0.1664,0.03777,0.02830,-0.1224,0.7274,0.4660 -3.000,0.1809,0.03847,0.02895,-0.1198,0.7172,0.4790 -2.750,0.2106,0.03850,0.02887,-0.1187,0.7132,0.4911 -2.500,0.2292,0.03863,0.02880,-0.1193,0.7024,0.4997 -2.250,0.2603,0.03826,0.02827,-0.1196,0.6981,0.5034 -2.000,0.2786,0.03848,0.02838,-0.1191,0.6894,0.5071 -1.750,0.3093,0.03818,0.02788,-0.1204,0.6837,0.5125 -1.500,0.3481,0.03754,0.02699,-0.1229,0.6804,0.5182 -1.250,0.3585,0.03827,0.02769,-0.1213,0.6707,0.5212 -1.000,0.3890,0.03806,0.02734,-0.1221,0.6665,0.5256 -0.750,0.4265,0.03761,0.02668,-0.1242,0.6638,0.5316 -0.500,0.4349,0.03870,0.02773,-0.1231,0.6541,0.5357 -0.250,0.4644,0.03861,0.02755,-0.1235,0.6503,0.5398 0.000,0.5001,0.03825,0.02706,-0.1249,0.6477,0.5450 0.250,0.5032,0.03979,0.02857,-0.1233,0.6382,0.5495 0.500,0.5324,0.03989,0.02858,-0.1241,0.6346,0.5545 0.750,0.5654,0.03974,0.02837,-0.1249,0.6322,0.5595 1.250,0.5916,0.04206,0.03058,-0.1238,0.6192,0.5697 1.500,0.6225,0.04201,0.03050,-0.1242,0.6167,0.5746 2.000,0.6411,0.04546,0.03394,-0.1228,0.6041,0.5847 2.250,0.6703,0.04564,0.03407,-0.1233,0.6013,0.5904 2.500,0.7028,0.04550,0.03389,-0.1239,0.5993,0.5967 3.000,0.7121,0.05035,0.03880,-0.1224,0.5857,0.6075 3.250,0.7431,0.05022,0.03866,-0.1227,0.5835,0.6146 3.750,0.7546,0.05489,0.04339,-0.1213,0.5693,0.6262 4.000,0.7902,0.05421,0.04270,-0.1217,0.5670,0.6353 4.500,0.8081,0.05785,0.04643,-0.1200,0.5520,0.6497 4.750,0.8280,0.05857,0.04718,-0.1196,0.5461,0.6591 5.250,0.8743,0.05889,0.04757,-0.1185,0.5339,0.6800 5.750,0.8999,0.06124,0.05006,-0.1167,0.5180,0.7029 6.000,0.8999,0.06386,0.05279,-0.1155,0.5087,0.7135 6.250,0.9156,0.06484,0.05387,-0.1148,0.5023,0.7285 6.500,0.9479,0.06385,0.05300,-0.1143,0.4993,0.7503 6.750,0.9842,0.06216,0.05147,-0.1136,0.4973,0.7811 7.250,0.9413,0.07081,0.06058,-0.1091,0.4713,0.8896 7.500,0.9683,0.07055,0.06031,-0.1090,0.4659,1.0000 7.750,1.0085,0.06901,0.05869,-0.1091,0.4631,1.0000 8.250,0.9893,0.07680,0.06657,-0.1075,0.4360,1.0000 8.500,1.0192,0.07608,0.06584,-0.1071,0.4311,1.0000 9.000,1.0431,0.07870,0.06849,-0.1058,0.4136,1.0000 9.500,1.0608,0.08220,0.07208,-0.1046,0.3961,1.0000 10.500,1.0540,0.09595,0.08604,-0.1037,0.3563,1.0000 10.750,1.0741,0.09647,0.08662,-0.1032,0.3526,1.0000 11.250,1.0829,0.10194,0.09220,-0.1030,0.3383,1.0000 11.750,1.0892,0.10794,0.09833,-0.1031,0.3245,1.0000 12.000,1.1132,0.10760,0.09806,-0.1024,0.3219,1.0000 12.500,1.1102,0.11544,0.10606,-0.1033,0.3086,1.0000 13.000,1.1168,0.12131,0.11208,-0.1038,0.2948,1.0000