Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag26-il-100000 Airfoil,ag26-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,54.4674 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ag26-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4820,0.10313,0.09833,0.0008,1.0000,0.0752 -8.000,-0.4803,0.10009,0.09534,-0.0025,1.0000,0.0783 -7.750,-0.4852,0.09782,0.09318,-0.0112,1.0000,0.0801 -7.500,-0.4793,0.09285,0.08828,-0.0161,1.0000,0.0812 -7.250,-0.4665,0.08897,0.08439,-0.0087,1.0000,0.0840 -7.000,-0.4569,0.08552,0.08097,-0.0102,1.0000,0.0878 -6.750,-0.4424,0.08052,0.07591,-0.0313,1.0000,0.0939 -6.500,-0.4357,0.07621,0.07172,-0.0252,1.0000,0.0958 -6.250,-0.4240,0.07320,0.06874,-0.0229,1.0000,0.0997 -6.000,-0.4032,0.06712,0.06252,-0.0373,1.0000,0.1086 -5.750,-0.3929,0.06429,0.05980,-0.0328,1.0000,0.1117 -5.500,-0.3713,0.05919,0.05454,-0.0412,1.0000,0.1229 -5.250,-0.3582,0.05664,0.05207,-0.0385,1.0000,0.1294 -5.000,-0.3401,0.05307,0.04846,-0.0409,1.0000,0.1433 -4.750,-0.3187,0.04919,0.04441,-0.0452,1.0000,0.1646 -4.500,-0.3009,0.04614,0.04132,-0.0452,1.0000,0.1794 -4.250,-0.2380,0.03062,0.02394,-0.0576,1.0000,0.0699 -4.000,-0.2095,0.02685,0.01962,-0.0578,1.0000,0.0624 -3.750,-0.1808,0.02358,0.01570,-0.0579,1.0000,0.0596 -3.500,-0.1529,0.02122,0.01288,-0.0575,1.0000,0.0601 -3.250,-0.1258,0.01999,0.01122,-0.0568,1.0000,0.0669 -3.000,-0.0992,0.01800,0.00922,-0.0565,1.0000,0.0742 -2.750,-0.0724,0.01663,0.00783,-0.0561,1.0000,0.0883 -2.500,-0.0449,0.01530,0.00661,-0.0559,1.0000,0.1175 -2.250,-0.0156,0.01361,0.00557,-0.0566,1.0000,0.2332 -2.000,0.0109,0.01226,0.00537,-0.0567,1.0000,0.4934 -1.750,0.0317,0.01138,0.00526,-0.0545,1.0000,0.7082 -1.500,0.0473,0.01079,0.00500,-0.0513,1.0000,1.0000 -1.250,0.0740,0.01095,0.00484,-0.0516,1.0000,1.0000 -1.000,0.1000,0.01114,0.00476,-0.0518,1.0000,1.0000 -0.750,0.1254,0.01138,0.00480,-0.0520,1.0000,1.0000 -0.500,0.1503,0.01167,0.00492,-0.0523,1.0000,1.0000 -0.250,0.1747,0.01201,0.00512,-0.0526,1.0000,1.0000 0.000,0.2035,0.01239,0.00537,-0.0538,0.9977,1.0000 0.250,0.2591,0.01268,0.00554,-0.0598,0.9839,1.0000 0.500,0.3137,0.01286,0.00565,-0.0654,0.9693,1.0000 0.750,0.3647,0.01294,0.00569,-0.0700,0.9529,1.0000 1.000,0.4115,0.01294,0.00568,-0.0735,0.9353,1.0000 1.250,0.4544,0.01287,0.00561,-0.0758,0.9171,1.0000 1.500,0.4911,0.01279,0.00556,-0.0767,0.8973,1.0000 1.750,0.5219,0.01273,0.00550,-0.0762,0.8750,1.0000 2.000,0.5492,0.01271,0.00547,-0.0751,0.8511,1.0000 2.250,0.5750,0.01271,0.00544,-0.0735,0.8266,1.0000 2.500,0.5996,0.01274,0.00548,-0.0718,0.8007,1.0000 2.750,0.6238,0.01282,0.00551,-0.0700,0.7728,1.0000 3.000,0.6479,0.01293,0.00558,-0.0684,0.7429,1.0000 3.250,0.6721,0.01308,0.00567,-0.0667,0.7111,1.0000 3.500,0.6963,0.01327,0.00575,-0.0652,0.6781,1.0000 3.750,0.7204,0.01350,0.00596,-0.0637,0.6407,1.0000 4.000,0.7445,0.01379,0.00615,-0.0624,0.6016,1.0000 4.250,0.7686,0.01414,0.00638,-0.0611,0.5606,1.0000 4.500,0.7925,0.01455,0.00666,-0.0599,0.5179,1.0000 4.750,0.8163,0.01503,0.00700,-0.0588,0.4745,1.0000 5.000,0.8399,0.01560,0.00745,-0.0578,0.4310,1.0000 5.250,0.8632,0.01626,0.00795,-0.0569,0.3882,1.0000 5.500,0.8864,0.01700,0.00854,-0.0560,0.3454,1.0000 5.750,0.9093,0.01783,0.00922,-0.0551,0.3038,1.0000 6.000,0.9318,0.01878,0.01001,-0.0543,0.2646,1.0000 6.250,0.9543,0.01979,0.01098,-0.0535,0.2272,1.0000 6.500,0.9764,0.02096,0.01198,-0.0527,0.1963,1.0000 6.750,0.9985,0.02217,0.01310,-0.0518,0.1684,1.0000 7.000,1.0207,0.02343,0.01438,-0.0510,0.1441,1.0000 7.250,1.0423,0.02482,0.01583,-0.0501,0.1216,1.0000 7.500,1.0635,0.02660,0.01748,-0.0492,0.1033,1.0000 7.750,1.0841,0.02839,0.01945,-0.0481,0.0859,1.0000 8.000,1.1046,0.03058,0.02185,-0.0469,0.0725,1.0000 8.250,1.1243,0.03310,0.02449,-0.0459,0.0622,1.0000 8.500,1.1436,0.03540,0.02702,-0.0446,0.0544,1.0000 8.750,1.1593,0.03872,0.03079,-0.0432,0.0486,1.0000 9.000,1.1737,0.04233,0.03490,-0.0415,0.0456,1.0000 9.250,1.1854,0.04606,0.03902,-0.0400,0.0436,1.0000 9.500,1.1930,0.05048,0.04364,-0.0388,0.0415,1.0000 9.750,1.1896,0.05578,0.04946,-0.0371,0.0405,1.0000 10.000,1.1831,0.05978,0.05401,-0.0352,0.0397,1.0000 10.250,1.1714,0.06428,0.05892,-0.0336,0.0394,1.0000 10.500,1.1547,0.06871,0.06363,-0.0322,0.0395,1.0000 10.750,1.1353,0.07328,0.06841,-0.0318,0.0397,1.0000 11.000,1.1153,0.07857,0.07387,-0.0331,0.0401,1.0000 11.250,1.0967,0.08471,0.08012,-0.0356,0.0405,1.0000 11.500,0.9231,0.09019,0.08610,-0.0326,0.0499,1.0000