Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag47c03-il-500000 Airfoil,ag47c03-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,65.1571 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-ag47c03-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.6441,0.11477,0.11258,0.0373,1.0000,0.0108 -8.000,-0.6493,0.10848,0.10633,0.0354,1.0000,0.0111 -7.750,-0.6454,0.10505,0.10291,0.0351,1.0000,0.0115 -7.500,-0.6403,0.10177,0.09962,0.0343,1.0000,0.0118 -7.250,-0.6360,0.09826,0.09613,0.0327,1.0000,0.0121 -7.000,-0.6319,0.09463,0.09251,0.0307,1.0000,0.0124 -6.750,-0.6278,0.09082,0.08873,0.0282,1.0000,0.0128 -6.500,-0.6217,0.08672,0.08465,0.0244,1.0000,0.0132 -6.250,-0.6109,0.08207,0.07999,0.0190,1.0000,0.0140 -6.000,-0.5965,0.07685,0.07476,0.0124,1.0000,0.0149 -5.750,-0.5751,0.07086,0.06873,0.0040,1.0000,0.0159 -5.500,-0.5493,0.06549,0.06328,-0.0028,1.0000,0.0165 -5.250,-0.5265,0.06012,0.05780,-0.0078,1.0000,0.0167 -5.000,-0.5038,0.05470,0.05224,-0.0118,1.0000,0.0168 -4.750,-0.4810,0.04941,0.04677,-0.0149,1.0000,0.0168 -4.500,-0.4654,0.03951,0.03652,-0.0196,1.0000,0.0177 -4.250,-0.4441,0.03621,0.03310,-0.0208,1.0000,0.0184 -4.000,-0.4205,0.03332,0.03005,-0.0217,1.0000,0.0192 -3.750,-0.3953,0.03030,0.02682,-0.0224,1.0000,0.0203 -3.500,-0.3687,0.02717,0.02339,-0.0228,1.0000,0.0219 -3.250,-0.3384,0.02657,0.02250,-0.0221,1.0000,0.0254 -3.000,-0.3110,0.01769,0.01275,-0.0221,1.0000,0.0151 -2.750,-0.2826,0.01381,0.00827,-0.0215,1.0000,0.0131 -2.500,-0.2550,0.01233,0.00659,-0.0210,1.0000,0.0138 -2.250,-0.2275,0.01129,0.00542,-0.0206,1.0000,0.0149 -2.000,-0.1999,0.01093,0.00501,-0.0204,1.0000,0.0166 -1.750,-0.1729,0.00951,0.00346,-0.0200,1.0000,0.0183 -1.500,-0.1453,0.00879,0.00270,-0.0198,1.0000,0.0214 -1.250,-0.1174,0.00821,0.00207,-0.0195,1.0000,0.0291 -1.000,-0.0898,0.00772,0.00169,-0.0194,1.0000,0.0561 -0.750,-0.0624,0.00717,0.00148,-0.0194,1.0000,0.1381 -0.500,-0.0354,0.00653,0.00134,-0.0196,1.0000,0.2807 -0.250,-0.0065,0.00551,0.00127,-0.0204,0.9910,0.5559 0.000,0.0231,0.00441,0.00127,-0.0201,0.9178,0.8945 0.250,0.0565,0.00455,0.00112,-0.0204,0.8208,1.0000 0.500,0.0818,0.00479,0.00105,-0.0196,0.7764,1.0000 0.750,0.1084,0.00496,0.00102,-0.0191,0.7508,1.0000 1.000,0.1354,0.00513,0.00101,-0.0188,0.7317,1.0000 1.250,0.1626,0.00527,0.00103,-0.0185,0.7153,1.0000 1.500,0.1900,0.00541,0.00105,-0.0182,0.7002,1.0000 1.750,0.2176,0.00549,0.00107,-0.0180,0.6837,1.0000 2.000,0.2453,0.00553,0.00107,-0.0178,0.6653,1.0000 2.250,0.2729,0.00558,0.00106,-0.0176,0.6435,1.0000 2.500,0.3004,0.00566,0.00106,-0.0174,0.6169,1.0000 2.750,0.3278,0.00578,0.00107,-0.0172,0.5853,1.0000 3.000,0.3550,0.00596,0.00110,-0.0169,0.5454,1.0000 3.250,0.3821,0.00617,0.00115,-0.0167,0.5029,1.0000 3.500,0.4091,0.00645,0.00125,-0.0166,0.4492,1.0000 3.750,0.4361,0.00678,0.00137,-0.0165,0.3935,1.0000 4.000,0.4630,0.00715,0.00151,-0.0164,0.3345,1.0000 4.250,0.4898,0.00759,0.00170,-0.0163,0.2699,1.0000 4.500,0.5166,0.00803,0.00191,-0.0163,0.2156,1.0000 4.750,0.5435,0.00847,0.00218,-0.0163,0.1697,1.0000 5.000,0.5704,0.00889,0.00245,-0.0162,0.1334,1.0000 5.250,0.5974,0.00928,0.00275,-0.0162,0.1095,1.0000 5.500,0.6243,0.00968,0.00307,-0.0161,0.0912,1.0000 5.750,0.6511,0.01011,0.00347,-0.0160,0.0764,1.0000 6.000,0.6781,0.01045,0.00381,-0.0159,0.0664,1.0000 6.250,0.7050,0.01082,0.00421,-0.0157,0.0573,1.0000 6.500,0.7316,0.01133,0.00472,-0.0156,0.0490,1.0000 6.750,0.7581,0.01179,0.00518,-0.0154,0.0419,1.0000 7.000,0.7845,0.01232,0.00581,-0.0152,0.0362,1.0000 7.250,0.8107,0.01288,0.00639,-0.0151,0.0308,1.0000 7.500,0.8359,0.01382,0.00745,-0.0147,0.0273,1.0000 7.750,0.8619,0.01446,0.00818,-0.0144,0.0246,1.0000 8.000,0.8875,0.01514,0.00892,-0.0142,0.0220,1.0000 8.250,0.9095,0.01718,0.01119,-0.0136,0.0193,1.0000 8.500,0.9347,0.01800,0.01216,-0.0133,0.0184,1.0000 8.750,0.9589,0.01921,0.01355,-0.0128,0.0173,1.0000 9.000,0.9827,0.02048,0.01501,-0.0124,0.0161,1.0000 9.250,1.0070,0.02122,0.01584,-0.0122,0.0148,1.0000 9.500,1.0280,0.02310,0.01791,-0.0118,0.0134,1.0000 9.750,1.0392,0.02848,0.02395,-0.0110,0.0126,1.0000 10.000,1.0594,0.03024,0.02599,-0.0106,0.0122,1.0000 10.250,1.0745,0.03330,0.02948,-0.0102,0.0117,1.0000 10.500,1.0854,0.03697,0.03356,-0.0100,0.0111,1.0000 10.750,1.0945,0.04044,0.03737,-0.0101,0.0104,1.0000 11.000,1.1090,0.04207,0.03914,-0.0102,0.0097,1.0000 11.250,1.1198,0.04414,0.04137,-0.0106,0.0092,1.0000 11.500,1.1142,0.04893,0.04645,-0.0122,0.0090,1.0000 11.750,0.9611,0.09330,0.09135,-0.0479,0.0127,1.0000 12.000,0.9513,0.10124,0.09929,-0.0518,0.0129,1.0000