Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag13-il-200000 Airfoil,ag13-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,62.1161 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-ag13-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.5461,0.09873,0.09533,0.0147,1.0000,0.0321 -7.750,-0.5415,0.09506,0.09169,0.0125,1.0000,0.0332 -7.500,-0.5370,0.09131,0.08798,0.0096,1.0000,0.0345 -7.250,-0.5297,0.08716,0.08387,0.0039,1.0000,0.0359 -7.000,-0.5103,0.08172,0.07843,-0.0088,1.0000,0.0371 -6.750,-0.4894,0.07602,0.07267,-0.0179,1.0000,0.0374 -6.500,-0.4742,0.06859,0.06518,-0.0253,1.0000,0.0378 -6.250,-0.4709,0.06454,0.06120,-0.0230,1.0000,0.0393 -6.000,-0.4565,0.06144,0.05811,-0.0237,1.0000,0.0410 -5.750,-0.4360,0.05708,0.05367,-0.0277,1.0000,0.0437 -5.500,-0.3936,0.05052,0.04645,-0.0396,1.0000,0.0500 -5.250,-0.3830,0.04483,0.04097,-0.0401,1.0000,0.0530 -5.000,-0.3522,0.04070,0.03620,-0.0447,1.0000,0.0639 -4.750,-0.3336,0.03725,0.03296,-0.0446,1.0000,0.0666 -4.500,-0.2944,0.01941,0.01501,-0.0445,1.0000,0.0780 -4.250,-0.2677,0.02466,0.01883,-0.0473,1.0000,0.0360 -4.000,-0.2393,0.02040,0.01402,-0.0477,1.0000,0.0316 -3.750,-0.2101,0.01745,0.01048,-0.0472,1.0000,0.0295 -3.500,-0.1823,0.01563,0.00838,-0.0468,1.0000,0.0301 -3.250,-0.1550,0.01427,0.00687,-0.0462,1.0000,0.0328 -3.000,-0.1281,0.01320,0.00568,-0.0458,1.0000,0.0392 -2.750,-0.1010,0.01207,0.00456,-0.0454,1.0000,0.0479 -2.500,-0.0735,0.01106,0.00359,-0.0452,1.0000,0.0766 -2.250,-0.0460,0.00987,0.00296,-0.0454,1.0000,0.1869 -2.000,-0.0196,0.00911,0.00278,-0.0456,1.0000,0.3406 -1.750,0.0062,0.00852,0.00269,-0.0453,1.0000,0.4828 -1.500,0.0305,0.00789,0.00262,-0.0445,1.0000,0.6366 -1.250,0.0512,0.00696,0.00245,-0.0419,1.0000,1.0000 -1.000,0.0781,0.00700,0.00234,-0.0417,1.0000,1.0000 -0.750,0.1048,0.00705,0.00227,-0.0416,1.0000,1.0000 -0.500,0.1314,0.00713,0.00225,-0.0415,1.0000,1.0000 -0.250,0.1580,0.00722,0.00226,-0.0414,1.0000,1.0000 0.000,0.1845,0.00734,0.00233,-0.0414,1.0000,1.0000 0.250,0.2349,0.00738,0.00231,-0.0462,0.9841,1.0000 0.500,0.2810,0.00738,0.00228,-0.0499,0.9643,1.0000 0.750,0.3224,0.00735,0.00223,-0.0523,0.9386,1.0000 1.000,0.3567,0.00735,0.00217,-0.0530,0.9049,1.0000 1.250,0.3847,0.00740,0.00213,-0.0522,0.8649,1.0000 1.500,0.4095,0.00753,0.00212,-0.0508,0.8216,1.0000 1.750,0.4337,0.00773,0.00215,-0.0494,0.7773,1.0000 2.000,0.4584,0.00797,0.00220,-0.0482,0.7322,1.0000 2.250,0.4834,0.00824,0.00228,-0.0471,0.6873,1.0000 2.500,0.5087,0.00853,0.00238,-0.0463,0.6432,1.0000 2.750,0.5343,0.00885,0.00251,-0.0455,0.5993,1.0000 3.000,0.5600,0.00918,0.00270,-0.0449,0.5556,1.0000 3.250,0.5858,0.00952,0.00288,-0.0444,0.5117,1.0000 3.500,0.6117,0.00988,0.00309,-0.0439,0.4680,1.0000 3.750,0.6376,0.01027,0.00333,-0.0434,0.4248,1.0000 4.000,0.6634,0.01068,0.00363,-0.0430,0.3817,1.0000 4.250,0.6893,0.01113,0.00393,-0.0427,0.3396,1.0000 4.500,0.7151,0.01160,0.00428,-0.0424,0.2989,1.0000 4.750,0.7408,0.01212,0.00467,-0.0421,0.2593,1.0000 5.000,0.7664,0.01267,0.00512,-0.0418,0.2229,1.0000 5.250,0.7917,0.01332,0.00565,-0.0415,0.1882,1.0000 5.500,0.8171,0.01397,0.00624,-0.0411,0.1568,1.0000 5.750,0.8422,0.01470,0.00690,-0.0408,0.1287,1.0000 6.000,0.8668,0.01556,0.00769,-0.0404,0.1054,1.0000 6.250,0.8915,0.01639,0.00850,-0.0399,0.0847,1.0000 6.500,0.9151,0.01756,0.00965,-0.0393,0.0678,1.0000 6.750,0.9391,0.01859,0.01076,-0.0387,0.0528,1.0000 7.000,0.9618,0.02008,0.01237,-0.0379,0.0420,1.0000 7.250,0.9830,0.02199,0.01432,-0.0371,0.0333,1.0000 7.500,1.0064,0.02362,0.01621,-0.0360,0.0289,1.0000 7.750,1.0270,0.02564,0.01831,-0.0353,0.0245,1.0000 8.000,1.0470,0.02835,0.02142,-0.0342,0.0221,1.0000 8.250,1.0662,0.03126,0.02476,-0.0329,0.0208,1.0000 8.500,1.0821,0.03489,0.02890,-0.0316,0.0200,1.0000 8.750,1.0930,0.03935,0.03394,-0.0302,0.0198,1.0000 9.000,1.0971,0.04468,0.03986,-0.0289,0.0201,1.0000 9.250,1.0942,0.05048,0.04619,-0.0280,0.0205,1.0000 9.500,1.0848,0.05631,0.05243,-0.0276,0.0210,1.0000 9.750,1.0698,0.06180,0.05823,-0.0278,0.0214,1.0000 10.000,1.0500,0.06687,0.06350,-0.0292,0.0216,1.0000 10.250,1.0301,0.07358,0.07038,-0.0349,0.0217,1.0000 10.500,1.0102,0.08311,0.08004,-0.0442,0.0219,1.0000 10.750,0.9892,0.09478,0.09177,-0.0536,0.0223,1.0000 11.000,0.9696,0.10542,0.10239,-0.0598,0.0229,1.0000 11.250,0.8472,0.09676,0.09383,-0.0419,0.0227,1.0000