Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag09-il-1000000 Airfoil,ag09-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,87.0037 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-ag09-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.6011,0.09874,0.09720,0.0249,1.0000,0.0099 -8.000,-0.5971,0.09477,0.09323,0.0226,1.0000,0.0099 -7.750,-0.5931,0.09071,0.08920,0.0198,1.0000,0.0100 -5.500,-0.4340,0.01803,0.01450,-0.0340,1.0000,0.0090 -5.250,-0.4074,0.01562,0.01169,-0.0340,1.0000,0.0095 -5.000,-0.3802,0.01448,0.01032,-0.0339,1.0000,0.0098 -4.750,-0.3531,0.01307,0.00865,-0.0338,1.0000,0.0101 -4.500,-0.3262,0.01076,0.00596,-0.0338,1.0000,0.0105 -4.250,-0.2989,0.00975,0.00481,-0.0336,1.0000,0.0112 -4.000,-0.2714,0.00931,0.00433,-0.0335,1.0000,0.0121 -3.750,-0.2437,0.00877,0.00373,-0.0333,1.0000,0.0130 -3.500,-0.2161,0.00835,0.00326,-0.0331,1.0000,0.0142 -3.250,-0.1885,0.00788,0.00271,-0.0329,1.0000,0.0153 -3.000,-0.1608,0.00737,0.00216,-0.0328,1.0000,0.0185 -2.750,-0.1334,0.00717,0.00195,-0.0326,1.0000,0.0211 -2.500,-0.1060,0.00684,0.00164,-0.0323,1.0000,0.0280 -2.250,-0.0787,0.00662,0.00143,-0.0321,1.0000,0.0363 -2.000,-0.0518,0.00645,0.00129,-0.0318,1.0000,0.0462 -1.750,-0.0212,0.00628,0.00118,-0.0324,0.9967,0.0596 -1.500,0.0155,0.00610,0.00108,-0.0343,0.9843,0.0756 -1.250,0.0496,0.00597,0.00098,-0.0355,0.9618,0.0937 -1.000,0.0766,0.00588,0.00091,-0.0350,0.9267,0.1154 -0.500,0.1262,0.00582,0.00080,-0.0331,0.8423,0.1854 -0.250,0.1525,0.00575,0.00075,-0.0327,0.7993,0.2524 0.000,0.1791,0.00535,0.00074,-0.0326,0.7565,0.4422 0.250,0.2000,0.00418,0.00077,-0.0312,0.7142,0.8814 0.500,0.2285,0.00415,0.00072,-0.0310,0.6677,1.0000 0.750,0.2560,0.00435,0.00072,-0.0308,0.6205,1.0000 1.000,0.2835,0.00456,0.00073,-0.0307,0.5734,1.0000 1.250,0.3111,0.00477,0.00075,-0.0306,0.5275,1.0000 1.500,0.3388,0.00499,0.00079,-0.0305,0.4827,1.0000 1.750,0.3664,0.00521,0.00085,-0.0304,0.4417,1.0000 2.000,0.3941,0.00542,0.00091,-0.0304,0.4050,1.0000 2.250,0.4218,0.00563,0.00098,-0.0303,0.3700,1.0000 2.500,0.4495,0.00583,0.00106,-0.0302,0.3395,1.0000 2.750,0.4772,0.00605,0.00117,-0.0302,0.3092,1.0000 3.000,0.5049,0.00626,0.00127,-0.0301,0.2819,1.0000 3.250,0.5325,0.00647,0.00138,-0.0301,0.2561,1.0000 3.500,0.5601,0.00669,0.00151,-0.0300,0.2308,1.0000 3.750,0.5876,0.00692,0.00167,-0.0300,0.2073,1.0000 4.250,0.6424,0.00742,0.00199,-0.0298,0.1605,1.0000 4.500,0.6697,0.00770,0.00218,-0.0298,0.1373,1.0000 4.750,0.6969,0.00801,0.00241,-0.0297,0.1129,1.0000 5.000,0.7238,0.00837,0.00266,-0.0296,0.0879,1.0000 5.250,0.7506,0.00878,0.00295,-0.0295,0.0630,1.0000 5.500,0.7772,0.00924,0.00328,-0.0294,0.0410,1.0000 5.750,0.8038,0.00968,0.00366,-0.0292,0.0260,1.0000 6.000,0.8301,0.01031,0.00425,-0.0290,0.0144,1.0000 6.250,0.8568,0.01070,0.00468,-0.0288,0.0118,1.0000 6.500,0.8827,0.01147,0.00555,-0.0284,0.0093,1.0000 6.750,0.9090,0.01197,0.00613,-0.0281,0.0085,1.0000 7.000,0.9349,0.01255,0.00679,-0.0278,0.0078,1.0000 7.250,0.9607,0.01313,0.00742,-0.0275,0.0072,1.0000 7.500,0.9854,0.01398,0.00837,-0.0271,0.0067,1.0000 7.750,1.0085,0.01534,0.00990,-0.0265,0.0064,1.0000 8.000,1.0288,0.01743,0.01223,-0.0256,0.0061,1.0000 8.250,1.0525,0.01843,0.01336,-0.0251,0.0060,1.0000 8.500,1.0759,0.01943,0.01450,-0.0246,0.0059,1.0000 8.750,1.0986,0.02058,0.01582,-0.0240,0.0058,1.0000 9.000,1.1203,0.02195,0.01737,-0.0233,0.0055,1.0000 9.250,1.1406,0.02360,0.01922,-0.0226,0.0053,1.0000 9.500,1.1590,0.02557,0.02144,-0.0217,0.0051,1.0000 9.750,1.1743,0.02811,0.02427,-0.0207,0.0049,1.0000 10.000,1.1842,0.03161,0.02815,-0.0195,0.0049,1.0000 10.250,1.1830,0.03686,0.03391,-0.0180,0.0049,1.0000 10.500,1.1685,0.04340,0.04094,-0.0170,0.0051,1.0000 10.750,1.1478,0.04899,0.04685,-0.0165,0.0052,1.0000 11.000,1.1281,0.05455,0.05260,-0.0197,0.0053,1.0000 11.250,1.1123,0.06371,0.06196,-0.0299,0.0053,1.0000 11.500,1.0961,0.07528,0.07367,-0.0407,0.0053,1.0000 11.750,1.0749,0.08668,0.08515,-0.0484,0.0053,1.0000