Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag38-il-200000 Airfoil,ag38-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,63.9912 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ag38-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5303,0.10789,0.10432,-0.0058,1.0000,0.0331 -9.750,-0.5274,0.10403,0.10049,-0.0088,1.0000,0.0332 -9.500,-0.5282,0.09764,0.09415,-0.0081,1.0000,0.0339 -9.250,-0.5206,0.09420,0.09069,-0.0064,1.0000,0.0348 -9.000,-0.5152,0.09094,0.08745,-0.0067,1.0000,0.0355 -8.750,-0.5117,0.08757,0.08411,-0.0081,1.0000,0.0363 -8.500,-0.5069,0.08383,0.08040,-0.0108,1.0000,0.0373 -8.250,-0.4997,0.07969,0.07628,-0.0147,1.0000,0.0384 -8.000,-0.4907,0.07523,0.07181,-0.0192,1.0000,0.0397 -7.750,-0.4788,0.07033,0.06686,-0.0246,1.0000,0.0415 -7.500,-0.4553,0.06454,0.06072,-0.0350,1.0000,0.0442 -7.250,-0.4446,0.05883,0.05478,-0.0377,1.0000,0.0448 -7.000,-0.4368,0.05403,0.05013,-0.0370,1.0000,0.0462 -6.750,-0.4234,0.05141,0.04753,-0.0364,1.0000,0.0479 -6.500,-0.4070,0.04834,0.04436,-0.0369,1.0000,0.0507 -6.250,-0.3827,0.04377,0.03906,-0.0396,1.0000,0.0580 -6.000,-0.3685,0.04067,0.03620,-0.0389,1.0000,0.0607 -5.750,-0.3487,0.03833,0.03374,-0.0386,1.0000,0.0658 -5.500,-0.3264,0.03478,0.02978,-0.0391,1.0000,0.0734 -5.250,-0.3060,0.03261,0.02759,-0.0386,1.0000,0.0776 -5.000,-0.2832,0.03008,0.02473,-0.0385,1.0000,0.0880 -4.750,-0.2602,0.02826,0.02264,-0.0381,1.0000,0.1009 -4.500,-0.2220,0.02061,0.01372,-0.0359,1.0000,0.0407 -4.250,-0.1960,0.01860,0.01136,-0.0350,1.0000,0.0401 -4.000,-0.1703,0.01746,0.00997,-0.0342,1.0000,0.0423 -3.750,-0.1440,0.01607,0.00837,-0.0334,1.0000,0.0427 -3.500,-0.1178,0.01507,0.00724,-0.0327,1.0000,0.0439 -3.250,-0.0909,0.01369,0.00588,-0.0324,1.0000,0.0478 -3.000,-0.0649,0.01312,0.00532,-0.0320,1.0000,0.0545 -2.750,-0.0378,0.01233,0.00456,-0.0318,1.0000,0.0627 -2.500,-0.0101,0.01171,0.00405,-0.0319,1.0000,0.0895 -2.250,0.0163,0.00865,0.00393,-0.0317,1.0000,0.8215 -2.000,0.0434,0.00852,0.00384,-0.0312,1.0000,1.0000 -1.750,0.0683,0.00866,0.00384,-0.0308,1.0000,1.0000 -1.500,0.0941,0.00883,0.00390,-0.0308,0.9996,1.0000 -1.250,0.1434,0.00884,0.00377,-0.0354,0.9904,1.0000 -1.000,0.1927,0.00879,0.00364,-0.0399,0.9803,1.0000 -0.750,0.2432,0.00868,0.00347,-0.0446,0.9702,1.0000 -0.500,0.2885,0.00853,0.00328,-0.0480,0.9562,1.0000 -0.250,0.3255,0.00838,0.00310,-0.0495,0.9345,1.0000 0.000,0.3589,0.00824,0.00293,-0.0502,0.9063,1.0000 0.250,0.3888,0.00811,0.00273,-0.0498,0.8657,1.0000 0.500,0.4175,0.00808,0.00253,-0.0491,0.8241,1.0000 0.750,0.4428,0.00827,0.00251,-0.0480,0.7803,1.0000 1.000,0.4679,0.00853,0.00258,-0.0470,0.7389,1.0000 1.250,0.4933,0.00877,0.00266,-0.0462,0.6996,1.0000 1.500,0.5190,0.00901,0.00274,-0.0456,0.6609,1.0000 1.750,0.5445,0.00930,0.00284,-0.0450,0.6280,1.0000 2.000,0.5703,0.00964,0.00302,-0.0444,0.5991,1.0000 2.250,0.5963,0.00996,0.00322,-0.0440,0.5714,1.0000 2.500,0.6225,0.01026,0.00344,-0.0437,0.5442,1.0000 2.750,0.6486,0.01055,0.00365,-0.0433,0.5160,1.0000 3.000,0.6747,0.01081,0.00388,-0.0430,0.4857,1.0000 3.250,0.7007,0.01106,0.00407,-0.0426,0.4504,1.0000 3.500,0.7263,0.01135,0.00426,-0.0422,0.4084,1.0000 3.750,0.7514,0.01176,0.00450,-0.0418,0.3623,1.0000 4.000,0.7761,0.01226,0.00485,-0.0415,0.3158,1.0000 4.250,0.8007,0.01283,0.00523,-0.0411,0.2708,1.0000 4.500,0.8251,0.01346,0.00568,-0.0408,0.2272,1.0000 4.750,0.8491,0.01417,0.00620,-0.0405,0.1844,1.0000 5.000,0.8725,0.01501,0.00686,-0.0401,0.1427,1.0000 5.250,0.8957,0.01595,0.00766,-0.0395,0.1099,1.0000 5.500,0.9178,0.01705,0.00860,-0.0389,0.0889,1.0000 5.750,0.9401,0.01812,0.00964,-0.0381,0.0759,1.0000 6.000,0.9635,0.01901,0.01062,-0.0375,0.0671,1.0000 6.250,0.9853,0.02022,0.01189,-0.0367,0.0603,1.0000 6.500,1.0078,0.02126,0.01296,-0.0360,0.0549,1.0000 6.750,1.0286,0.02316,0.01490,-0.0350,0.0512,1.0000 7.000,1.0518,0.02432,0.01625,-0.0343,0.0479,1.0000 7.250,1.0740,0.02545,0.01749,-0.0337,0.0444,1.0000 7.500,1.0943,0.02787,0.01998,-0.0329,0.0418,1.0000 7.750,1.1143,0.03037,0.02281,-0.0319,0.0404,1.0000 8.000,1.1340,0.03217,0.02496,-0.0307,0.0387,1.0000 8.250,1.1520,0.03403,0.02713,-0.0296,0.0365,1.0000 8.500,1.1683,0.03632,0.02970,-0.0284,0.0350,1.0000 8.750,1.1817,0.03898,0.03269,-0.0269,0.0340,1.0000 9.000,1.1917,0.04204,0.03606,-0.0254,0.0333,1.0000 9.250,1.1980,0.04555,0.03985,-0.0237,0.0325,1.0000 9.500,1.1949,0.05044,0.04510,-0.0217,0.0318,1.0000 9.750,1.1830,0.05581,0.05087,-0.0193,0.0315,1.0000 10.000,1.1667,0.06070,0.05609,-0.0170,0.0314,1.0000 10.250,1.1474,0.06452,0.06016,-0.0143,0.0314,1.0000 10.500,1.1279,0.06842,0.06426,-0.0131,0.0314,1.0000 10.750,1.1096,0.07275,0.06878,-0.0139,0.0315,1.0000 11.000,1.0914,0.07788,0.07410,-0.0166,0.0316,1.0000 11.250,1.0720,0.08440,0.08082,-0.0220,0.0320,1.0000