Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca6412-il-50000 Airfoil,naca6412-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,9.81329 Max Cl/Cd alpha,3.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca6412-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.3304,0.13030,0.12383,-0.0292,1.0001,0.1748 -8.750,-0.3583,0.13182,0.12550,-0.0274,1.0001,0.1754 -8.500,-0.3148,0.12222,0.11582,-0.0254,1.0001,0.1826 -8.250,-0.3221,0.12090,0.11458,-0.0236,1.0001,0.1873 -8.000,-0.3420,0.12106,0.11486,-0.0218,1.0001,0.1909 -7.750,-0.3716,0.12225,0.11619,-0.0194,1.0001,0.1923 -7.500,-0.4036,0.12347,0.11758,-0.0172,1.0001,0.1930 -7.250,-0.3607,0.11491,0.10895,-0.0157,1.0001,0.1997 -7.000,-0.3705,0.11359,0.10771,-0.0133,1.0001,0.2039 -6.750,-0.3921,0.11331,0.10754,-0.0107,1.0001,0.2075 -6.500,-0.4215,0.11416,0.10853,-0.0116,1.0001,0.2104 -6.250,-0.4238,0.11077,0.10522,-0.0102,1.0001,0.2128 -6.000,-0.4156,0.10733,0.10179,-0.0065,1.0001,0.2177 -5.750,-0.4218,0.10560,0.10013,-0.0058,1.0001,0.2238 -5.500,-0.4384,0.10518,0.09978,-0.0126,1.0001,0.2297 -5.250,-0.4318,0.10107,0.09572,-0.0059,1.0001,0.2341 -5.000,-0.4327,0.09919,0.09386,-0.0060,1.0001,0.2435 -4.750,-0.4335,0.09652,0.09123,-0.0079,1.0001,0.2501 -4.500,-0.4305,0.09419,0.08894,-0.0058,1.0001,0.2592 -4.250,-0.4270,0.09151,0.08628,-0.0084,1.0001,0.2687 -4.000,-0.4173,0.08945,0.08418,-0.0133,1.0001,0.2837 -3.750,-0.3873,0.08592,0.08059,-0.0182,0.9930,0.3015 -3.500,-0.3563,0.08220,0.07685,-0.0206,0.9829,0.3215 -3.250,-0.3242,0.07938,0.07395,-0.0259,0.9723,0.3544 -3.000,-0.3042,0.07643,0.07101,-0.0252,0.9622,0.3773 -2.750,-0.2800,0.07380,0.06835,-0.0265,0.9523,0.4126 -2.500,-0.2622,0.07155,0.06613,-0.0247,0.9436,0.4643 -2.250,-0.0529,0.05589,0.04808,-0.0876,0.9317,0.2070 -2.000,-0.0005,0.05297,0.04454,-0.0944,0.9228,0.2079 -1.750,0.0439,0.05090,0.04195,-0.0990,0.9135,0.2138 -1.500,0.0783,0.04999,0.04076,-0.1014,0.9041,0.2246 -1.250,0.1235,0.04895,0.03939,-0.1053,0.8955,0.2381 -1.000,0.1507,0.04848,0.03863,-0.1063,0.8858,0.2517 -0.750,0.1967,0.04802,0.03794,-0.1099,0.8781,0.2739 -0.500,0.2151,0.04806,0.03785,-0.1095,0.8685,0.2907 -0.250,0.2630,0.04779,0.03739,-0.1132,0.8611,0.3230 0.000,0.2776,0.04812,0.03764,-0.1121,0.8515,0.3451 0.250,0.3266,0.04795,0.03740,-0.1158,0.8445,0.3941 0.500,0.3387,0.04843,0.03797,-0.1145,0.8354,0.4291 0.750,0.3841,0.04803,0.03809,-0.1175,0.8286,0.5310 1.000,0.3871,0.04738,0.03867,-0.1139,0.8205,0.9999 1.250,0.4254,0.04852,0.03904,-0.1163,0.8130,0.9999 1.500,0.4386,0.04991,0.04017,-0.1154,0.8050,0.9999 1.750,0.4645,0.05112,0.04112,-0.1160,0.7976,0.9999 2.000,0.4843,0.05252,0.04233,-0.1159,0.7905,0.9999 2.250,0.4988,0.05398,0.04366,-0.1153,0.7833,0.9999 2.500,0.5342,0.05516,0.04465,-0.1170,0.7765,0.9999 2.750,0.5333,0.05703,0.04647,-0.1147,0.7697,0.9999 3.000,0.5632,0.05831,0.04763,-0.1158,0.7628,0.9999 3.250,0.5723,0.06014,0.04939,-0.1148,0.7564,0.9999 3.500,0.5833,0.06193,0.05113,-0.1140,0.7502,0.9999 3.750,0.6202,0.06320,0.05230,-0.1157,0.7431,0.9999 4.000,0.6139,0.06554,0.05465,-0.1134,0.7382,0.9999 4.250,0.6273,0.06743,0.05651,-0.1130,0.7325,0.9999 4.500,0.6555,0.06903,0.05806,-0.1139,0.7252,0.9999 4.750,0.6527,0.07151,0.06055,-0.1123,0.7217,0.9999 5.000,0.6602,0.07377,0.06282,-0.1116,0.7175,0.9999 5.250,0.6929,0.07535,0.06437,-0.1128,0.7086,0.9999 5.500,0.6905,0.07809,0.06714,-0.1115,0.7067,0.9999 5.750,0.6933,0.08088,0.06996,-0.1109,0.7062,0.9999 6.000,0.7021,0.08387,0.07298,-0.1112,0.7080,0.9999 6.250,0.7197,0.08705,0.07620,-0.1123,0.7101,0.9999 6.500,0.6387,0.09319,0.08249,-0.1086,0.7826,0.9999 6.750,0.6586,0.09609,0.08541,-0.1095,0.7752,0.9999 7.000,0.6765,0.09828,0.08764,-0.1099,0.7629,0.9999 7.250,0.6788,0.10023,0.08962,-0.1086,0.7534,0.9999 7.500,0.7178,0.10418,0.09361,-0.1117,0.7437,0.9999 7.750,0.7125,0.10520,0.09468,-0.1093,0.7310,0.9999 8.000,0.7210,0.10767,0.09719,-0.1089,0.7213,0.9999 8.250,0.7611,0.11176,0.10136,-0.1119,0.7102,0.9999 8.500,0.7524,0.11275,0.10240,-0.1094,0.6972,0.9999 8.750,0.7588,0.11523,0.10494,-0.1088,0.6864,0.9999 9.000,0.7932,0.11926,0.10905,-0.1111,0.6760,0.9999 9.250,0.7950,0.12088,0.11076,-0.1098,0.6619,0.9999 9.500,0.7958,0.12308,0.11302,-0.1088,0.6495,0.9999 9.750,0.8108,0.12628,0.11631,-0.1093,0.6392,0.9999 10.000,0.8434,0.13017,0.12030,-0.1109,0.6255,0.9999 10.250,0.8399,0.13173,0.12194,-0.1095,0.6113,0.9999 10.500,0.8408,0.13412,0.12442,-0.1088,0.5981,0.9999