Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag47c03-il-50000-n5 Airfoil,ag47c03-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,30.7178 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-ag47c03-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.6410,0.12755,0.12071,0.0358,1.0000,0.0879 -8.250,-0.6457,0.12532,0.11856,0.0313,1.0000,0.0893 -8.000,-0.6493,0.12272,0.11605,0.0267,1.0000,0.0898 -7.750,-0.6266,0.11579,0.10908,0.0322,1.0000,0.0946 -7.500,-0.6220,0.11220,0.10554,0.0307,1.0000,0.0978 -7.250,-0.6234,0.10925,0.10266,0.0268,1.0000,0.1018 -7.000,-0.6288,0.10662,0.10013,0.0179,1.0000,0.1034 -6.750,-0.6178,0.10130,0.09486,0.0199,1.0000,0.1048 -6.500,-0.6074,0.09696,0.09054,0.0202,1.0000,0.1069 -6.250,-0.5985,0.09284,0.08644,0.0179,1.0000,0.1092 -5.750,-0.5672,0.07871,0.07210,-0.0021,1.0000,0.0636 -5.500,-0.5496,0.07265,0.06592,-0.0045,1.0000,0.0485 -5.250,-0.5359,0.06818,0.06141,-0.0060,1.0000,0.0463 -5.000,-0.5184,0.06311,0.05623,-0.0093,1.0000,0.0442 -4.750,-0.4981,0.05769,0.05060,-0.0132,1.0000,0.0422 -4.500,-0.4749,0.05200,0.04457,-0.0169,1.0000,0.0402 -4.250,-0.4488,0.04636,0.03837,-0.0200,1.0000,0.0385 -4.000,-0.4225,0.04186,0.03328,-0.0217,1.0000,0.0378 -3.750,-0.3996,0.03864,0.02987,-0.0225,1.0000,0.0397 -3.500,-0.3740,0.03572,0.02654,-0.0231,1.0000,0.0427 -3.250,-0.3463,0.03257,0.02285,-0.0236,1.0000,0.0448 -3.000,-0.3179,0.02958,0.01930,-0.0236,1.0000,0.0458 -2.750,-0.2892,0.02697,0.01615,-0.0233,1.0000,0.0475 -2.500,-0.2615,0.02480,0.01365,-0.0229,1.0000,0.0519 -2.250,-0.2343,0.02321,0.01184,-0.0224,1.0000,0.0599 -2.000,-0.2070,0.02145,0.00991,-0.0216,1.0000,0.0662 -1.750,-0.1801,0.02020,0.00852,-0.0211,1.0000,0.0832 -1.500,-0.1527,0.01888,0.00716,-0.0207,1.0000,0.1080 -1.250,-0.1256,0.01737,0.00601,-0.0206,1.0000,0.1762 -1.000,-0.1074,0.01471,0.00538,-0.0191,1.0000,0.5568 -0.750,-0.0697,0.01349,0.00470,-0.0188,1.0000,1.0000 -0.500,-0.0431,0.01344,0.00422,-0.0186,1.0000,1.0000 -0.250,-0.0166,0.01341,0.00389,-0.0183,1.0000,1.0000 0.000,0.0097,0.01339,0.00363,-0.0181,1.0000,1.0000 0.250,0.0360,0.01339,0.00344,-0.0178,1.0000,1.0000 0.500,0.0621,0.01340,0.00328,-0.0176,1.0000,1.0000 0.750,0.0880,0.01343,0.00321,-0.0174,1.0000,1.0000 1.000,0.1136,0.01348,0.00319,-0.0173,1.0000,1.0000 1.250,0.1389,0.01355,0.00323,-0.0171,1.0000,1.0000 1.500,0.1637,0.01365,0.00333,-0.0169,1.0000,1.0000 1.750,0.1875,0.01379,0.00351,-0.0168,1.0000,1.0000 2.000,0.2173,0.01401,0.00378,-0.0181,0.9891,1.0000 2.250,0.2659,0.01426,0.00408,-0.0226,0.9454,1.0000 2.500,0.3111,0.01448,0.00437,-0.0259,0.8998,1.0000 2.750,0.3492,0.01472,0.00461,-0.0272,0.8530,1.0000 3.000,0.3794,0.01501,0.00484,-0.0267,0.8083,1.0000 3.250,0.4045,0.01536,0.00509,-0.0251,0.7663,1.0000 3.500,0.4277,0.01578,0.00545,-0.0231,0.7262,1.0000 3.750,0.4506,0.01623,0.00582,-0.0213,0.6848,1.0000 4.000,0.4738,0.01655,0.00616,-0.0197,0.6365,1.0000 4.250,0.4968,0.01683,0.00641,-0.0180,0.5829,1.0000 4.500,0.5195,0.01716,0.00662,-0.0164,0.5198,1.0000 4.750,0.5421,0.01765,0.00694,-0.0148,0.4454,1.0000 5.000,0.5649,0.01839,0.00735,-0.0137,0.3639,1.0000 5.250,0.5884,0.01938,0.00800,-0.0130,0.2880,1.0000 5.500,0.6124,0.02051,0.00888,-0.0127,0.2308,1.0000 5.750,0.6374,0.02172,0.00994,-0.0125,0.1909,1.0000 6.000,0.6621,0.02295,0.01120,-0.0122,0.1626,1.0000 6.250,0.6863,0.02425,0.01246,-0.0117,0.1412,1.0000 6.500,0.7107,0.02556,0.01391,-0.0112,0.1226,1.0000 6.750,0.7352,0.02714,0.01561,-0.0105,0.1100,1.0000 7.000,0.7592,0.02861,0.01724,-0.0101,0.0958,1.0000 7.250,0.7831,0.03053,0.01934,-0.0095,0.0875,1.0000 7.500,0.8073,0.03261,0.02177,-0.0089,0.0790,1.0000 7.750,0.8300,0.03481,0.02436,-0.0086,0.0701,1.0000 8.000,0.8522,0.03739,0.02724,-0.0082,0.0653,1.0000 8.250,0.8724,0.04094,0.03125,-0.0079,0.0620,1.0000 8.500,0.8897,0.04490,0.03597,-0.0079,0.0571,1.0000 8.750,0.9070,0.04735,0.03862,-0.0079,0.0524,1.0000 9.000,0.9194,0.05183,0.04347,-0.0082,0.0507,1.0000 9.250,0.9244,0.05777,0.05017,-0.0094,0.0500,1.0000 9.500,0.9239,0.06402,0.05692,-0.0114,0.0496,1.0000 9.750,0.9183,0.07045,0.06368,-0.0143,0.0495,1.0000 10.000,0.9088,0.07700,0.07037,-0.0181,0.0496,1.0000 10.250,0.8965,0.08360,0.07705,-0.0230,0.0499,1.0000 10.500,0.8856,0.09089,0.08434,-0.0291,0.0503,1.0000