Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag13-il-200000-n5 Airfoil,ag13-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,58.9537 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-ag13-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5693,0.11590,0.11242,0.0187,1.0000,0.0163 -9.000,-0.5686,0.11080,0.10734,0.0170,1.0000,0.0166 -8.750,-0.5652,0.10653,0.10305,0.0153,1.0000,0.0167 -7.750,-0.5456,0.09171,0.08830,0.0110,1.0000,0.0143 -7.500,-0.5420,0.08767,0.08429,0.0087,1.0000,0.0133 -7.250,-0.5364,0.08297,0.07964,0.0047,1.0000,0.0124 -7.000,-0.5270,0.07688,0.07356,-0.0019,1.0000,0.0114 -6.250,-0.4677,0.05404,0.05053,-0.0278,1.0000,0.0097 -6.000,-0.4443,0.04577,0.04202,-0.0350,1.0000,0.0096 -5.500,-0.3962,0.03299,0.02846,-0.0438,1.0000,0.0111 -5.250,-0.3712,0.03080,0.02604,-0.0449,1.0000,0.0125 -5.000,-0.3438,0.02592,0.02055,-0.0464,1.0000,0.0127 -4.750,-0.3159,0.02208,0.01608,-0.0470,1.0000,0.0126 -4.500,-0.2883,0.01939,0.01286,-0.0471,1.0000,0.0127 -4.250,-0.2609,0.01738,0.01047,-0.0469,1.0000,0.0130 -4.000,-0.2337,0.01580,0.00862,-0.0466,1.0000,0.0137 -3.750,-0.2067,0.01452,0.00711,-0.0463,1.0000,0.0146 -3.500,-0.1798,0.01354,0.00598,-0.0459,1.0000,0.0159 -3.250,-0.1532,0.01265,0.00506,-0.0458,1.0000,0.0202 -3.000,-0.1262,0.01200,0.00430,-0.0455,1.0000,0.0244 -2.750,-0.0991,0.01132,0.00357,-0.0452,1.0000,0.0333 -2.500,-0.0723,0.01077,0.00307,-0.0450,1.0000,0.0563 -2.250,-0.0457,0.01029,0.00277,-0.0449,1.0000,0.1027 -2.000,-0.0192,0.00982,0.00256,-0.0448,1.0000,0.1679 -1.750,0.0073,0.00941,0.00242,-0.0448,1.0000,0.2467 -1.500,0.0337,0.00904,0.00234,-0.0447,1.0000,0.3302 -1.250,0.0696,0.00865,0.00224,-0.0466,0.9892,0.4310 -1.000,0.1057,0.00824,0.00218,-0.0484,0.9735,0.5392 -0.500,0.1736,0.00700,0.00197,-0.0496,0.9286,1.0000 -0.250,0.2074,0.00703,0.00184,-0.0504,0.8958,1.0000 0.000,0.2374,0.00709,0.00174,-0.0504,0.8579,1.0000 0.250,0.2642,0.00721,0.00166,-0.0496,0.8174,1.0000 0.500,0.2899,0.00737,0.00162,-0.0487,0.7766,1.0000 0.750,0.3156,0.00756,0.00160,-0.0478,0.7360,1.0000 1.000,0.3415,0.00777,0.00160,-0.0471,0.6961,1.0000 1.250,0.3676,0.00800,0.00162,-0.0465,0.6570,1.0000 1.500,0.3939,0.00823,0.00167,-0.0459,0.6187,1.0000 1.750,0.4203,0.00848,0.00176,-0.0455,0.5810,1.0000 2.000,0.4467,0.00875,0.00184,-0.0450,0.5436,1.0000 2.250,0.4733,0.00901,0.00195,-0.0447,0.5070,1.0000 2.500,0.4999,0.00929,0.00208,-0.0443,0.4712,1.0000 2.750,0.5265,0.00958,0.00223,-0.0441,0.4356,1.0000 3.000,0.5531,0.00989,0.00243,-0.0438,0.4003,1.0000 3.250,0.5796,0.01021,0.00263,-0.0435,0.3654,1.0000 3.500,0.6062,0.01055,0.00285,-0.0433,0.3312,1.0000 3.750,0.6327,0.01090,0.00310,-0.0431,0.2986,1.0000 4.000,0.6592,0.01128,0.00337,-0.0429,0.2669,1.0000 4.250,0.6856,0.01167,0.00372,-0.0427,0.2367,1.0000 4.500,0.7119,0.01208,0.00406,-0.0425,0.2084,1.0000 4.750,0.7381,0.01252,0.00443,-0.0422,0.1808,1.0000 5.000,0.7642,0.01297,0.00484,-0.0420,0.1569,1.0000 5.250,0.7901,0.01348,0.00532,-0.0418,0.1329,1.0000 5.500,0.8160,0.01398,0.00582,-0.0415,0.1123,1.0000 5.750,0.8416,0.01455,0.00636,-0.0413,0.0933,1.0000 6.000,0.8672,0.01513,0.00695,-0.0410,0.0767,1.0000 6.250,0.8924,0.01577,0.00760,-0.0407,0.0619,1.0000 6.500,0.9175,0.01646,0.00832,-0.0403,0.0493,1.0000 6.750,0.9422,0.01722,0.00917,-0.0399,0.0385,1.0000 7.000,0.9664,0.01811,0.01013,-0.0395,0.0298,1.0000 7.250,0.9898,0.01915,0.01122,-0.0390,0.0226,1.0000 7.500,1.0135,0.02011,0.01235,-0.0384,0.0182,1.0000 7.750,1.0339,0.02189,0.01426,-0.0376,0.0149,1.0000 8.000,1.0568,0.02297,0.01556,-0.0369,0.0129,1.0000 8.250,1.0792,0.02404,0.01678,-0.0364,0.0108,1.0000 8.500,1.0990,0.02567,0.01861,-0.0356,0.0097,1.0000 8.750,1.1138,0.02852,0.02171,-0.0344,0.0088,1.0000 9.000,1.1314,0.03066,0.02424,-0.0334,0.0085,1.0000 9.250,1.1464,0.03326,0.02721,-0.0322,0.0081,1.0000 9.500,1.1582,0.03632,0.03068,-0.0310,0.0078,1.0000 9.750,1.1658,0.03984,0.03464,-0.0298,0.0076,1.0000 10.000,1.1680,0.04377,0.03902,-0.0287,0.0074,1.0000 10.250,1.1640,0.04805,0.04372,-0.0277,0.0074,1.0000 10.500,1.1522,0.05239,0.04839,-0.0270,0.0073,1.0000 10.750,1.1356,0.05716,0.05342,-0.0280,0.0073,1.0000 11.000,1.1181,0.06361,0.06011,-0.0327,0.0074,1.0000 11.250,1.1006,0.07214,0.06884,-0.0404,0.0075,1.0000 11.500,1.0813,0.08243,0.07929,-0.0490,0.0076,1.0000 11.750,1.0589,0.09374,0.09070,-0.0568,0.0078,1.0000 12.000,1.0344,0.10536,0.10236,-0.0635,0.0080,1.0000