Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag47ct02r-il-200000 Airfoil,ag47ct02r-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,52.103 Max Cl/Cd alpha,3.25 Url,http://airfoiltools.com/polar/csv?polar=xf-ag47ct02r-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.5277,0.13541,0.13203,0.0241,1.0000,0.0265 -10.750,-0.5276,0.13221,0.12884,0.0226,1.0000,0.0266 -8.750,-0.6291,0.11004,0.10662,0.0307,1.0000,0.0287 -8.500,-0.6232,0.10657,0.10313,0.0303,1.0000,0.0299 -8.250,-0.6187,0.10295,0.09953,0.0288,1.0000,0.0307 -8.000,-0.6144,0.09927,0.09588,0.0269,1.0000,0.0316 -7.750,-0.6104,0.09552,0.09216,0.0247,1.0000,0.0325 -7.500,-0.6062,0.09166,0.08833,0.0219,1.0000,0.0335 -7.250,-0.5993,0.08740,0.08410,0.0175,1.0000,0.0346 -7.000,-0.5872,0.08249,0.07919,0.0106,1.0000,0.0360 -6.750,-0.5626,0.07651,0.07312,-0.0025,1.0000,0.0377 -6.500,-0.5401,0.07135,0.06777,-0.0099,1.0000,0.0382 -6.250,-0.5273,0.06422,0.06052,-0.0145,1.0000,0.0387 -6.000,-0.5189,0.05963,0.05602,-0.0140,1.0000,0.0400 -5.750,-0.5033,0.05632,0.05269,-0.0147,1.0000,0.0416 -5.500,-0.4832,0.05250,0.04878,-0.0168,1.0000,0.0438 -5.250,-0.4582,0.04811,0.04417,-0.0199,1.0000,0.0475 -5.000,-0.4290,0.04234,0.03782,-0.0240,1.0000,0.0522 -4.750,-0.4093,0.03913,0.03467,-0.0243,1.0000,0.0544 -4.500,-0.3852,0.03624,0.03160,-0.0250,1.0000,0.0586 -4.250,-0.3578,0.03249,0.02737,-0.0262,1.0000,0.0667 -4.000,-0.3295,0.03157,0.02607,-0.0260,1.0000,0.0768 -3.750,-0.2963,0.02204,0.01566,-0.0253,1.0000,0.0332 -3.500,-0.2678,0.01920,0.01233,-0.0248,1.0000,0.0324 -3.250,-0.2399,0.01748,0.01028,-0.0243,1.0000,0.0348 -3.000,-0.2118,0.01550,0.00800,-0.0236,1.0000,0.0346 -2.750,-0.1842,0.01403,0.00636,-0.0229,1.0000,0.0362 -2.500,-0.1573,0.01256,0.00479,-0.0223,1.0000,0.0406 -2.250,-0.1304,0.01170,0.00395,-0.0219,1.0000,0.0522 -2.000,-0.1035,0.01070,0.00307,-0.0216,1.0000,0.0804 -1.750,-0.0776,0.00907,0.00246,-0.0218,1.0000,0.2955 -1.500,-0.0640,0.00707,0.00240,-0.0185,1.0000,0.7954 -1.250,-0.0248,0.00673,0.00212,-0.0199,1.0000,1.0000 -1.000,0.0017,0.00672,0.00196,-0.0196,1.0000,1.0000 -0.750,0.0283,0.00672,0.00184,-0.0193,1.0000,1.0000 -0.500,0.0547,0.00673,0.00176,-0.0190,1.0000,1.0000 -0.250,0.0811,0.00674,0.00170,-0.0187,1.0000,1.0000 0.000,0.1074,0.00677,0.00169,-0.0184,1.0000,1.0000 0.250,0.1335,0.00681,0.00171,-0.0181,1.0000,1.0000 0.500,0.1596,0.00687,0.00177,-0.0179,1.0000,1.0000 0.750,0.2025,0.00694,0.00184,-0.0213,0.9785,1.0000 1.000,0.2508,0.00698,0.00186,-0.0253,0.9276,1.0000 1.250,0.2856,0.00708,0.00183,-0.0260,0.8606,1.0000 1.500,0.3100,0.00731,0.00186,-0.0244,0.8029,1.0000 1.750,0.3339,0.00760,0.00192,-0.0230,0.7576,1.0000 2.000,0.3585,0.00791,0.00204,-0.0219,0.7199,1.0000 2.250,0.3839,0.00818,0.00218,-0.0211,0.6835,1.0000 2.500,0.4097,0.00837,0.00229,-0.0204,0.6419,1.0000 2.750,0.4353,0.00859,0.00239,-0.0196,0.5917,1.0000 3.000,0.4605,0.00890,0.00248,-0.0188,0.5303,1.0000 3.250,0.4856,0.00932,0.00261,-0.0182,0.4581,1.0000 3.500,0.5106,0.00986,0.00282,-0.0177,0.3764,1.0000 3.750,0.5359,0.01050,0.00311,-0.0174,0.2966,1.0000 4.000,0.5613,0.01119,0.00354,-0.0171,0.2311,1.0000 4.250,0.5868,0.01191,0.00400,-0.0169,0.1828,1.0000 4.500,0.6126,0.01260,0.00455,-0.0166,0.1496,1.0000 4.750,0.6383,0.01334,0.00517,-0.0164,0.1258,1.0000 5.000,0.6642,0.01399,0.00584,-0.0161,0.1067,1.0000 5.250,0.6898,0.01479,0.00663,-0.0157,0.0927,1.0000 5.500,0.7153,0.01558,0.00743,-0.0153,0.0800,1.0000 5.750,0.7405,0.01661,0.00851,-0.0149,0.0702,1.0000 6.000,0.7649,0.01796,0.00983,-0.0144,0.0616,1.0000 6.250,0.7910,0.01858,0.01065,-0.0140,0.0538,1.0000 6.500,0.8148,0.02056,0.01273,-0.0134,0.0488,1.0000 6.750,0.8402,0.02184,0.01427,-0.0128,0.0442,1.0000 7.000,0.8639,0.02322,0.01570,-0.0124,0.0394,1.0000 7.250,0.8861,0.02628,0.01922,-0.0117,0.0372,1.0000 7.500,0.9083,0.02904,0.02249,-0.0109,0.0356,1.0000 7.750,0.9273,0.03286,0.02692,-0.0101,0.0345,1.0000 8.000,0.9453,0.03599,0.03055,-0.0096,0.0323,1.0000 8.250,0.9629,0.03862,0.03344,-0.0093,0.0305,1.0000 8.500,0.9595,0.04836,0.04417,-0.0097,0.0319,1.0000 8.750,0.9470,0.05861,0.05503,-0.0122,0.0341,1.0000 9.000,0.9349,0.06669,0.06334,-0.0158,0.0355,1.0000 9.250,0.9204,0.07392,0.07072,-0.0205,0.0366,1.0000 9.500,0.9064,0.08086,0.07768,-0.0263,0.0377,1.0000