Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ah85l120-il-100000 Airfoil,ah85l120-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,37.6378 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-ah85l120-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.8300,0.05182,0.04570,-0.0083,1.0000,0.0866 -7.500,-0.8351,0.04637,0.03919,-0.0014,1.0000,0.0621 -7.250,-0.8284,0.04247,0.03508,0.0015,1.0000,0.0592 -7.000,-0.8212,0.03927,0.03142,0.0050,1.0000,0.0570 -6.750,-0.8110,0.03704,0.02882,0.0080,1.0000,0.0581 -6.500,-0.7975,0.03485,0.02625,0.0106,1.0000,0.0588 -6.250,-0.7795,0.03241,0.02343,0.0128,1.0000,0.0583 -6.000,-0.7579,0.03027,0.02096,0.0144,1.0000,0.0581 -5.750,-0.7341,0.02842,0.01886,0.0156,1.0000,0.0593 -5.500,-0.7102,0.02688,0.01716,0.0167,1.0000,0.0610 -5.250,-0.6884,0.02536,0.01557,0.0180,1.0000,0.0649 -5.000,-0.6718,0.02416,0.01443,0.0198,1.0000,0.0715 -4.750,-0.6572,0.02303,0.01328,0.0222,1.0000,0.0782 -4.500,-0.6456,0.02191,0.01219,0.0251,1.0000,0.0906 -4.250,-0.6366,0.02060,0.01111,0.0282,1.0000,0.1192 -4.000,-0.6498,0.01713,0.00984,0.0349,1.0000,0.4205 -3.750,-0.6492,0.01767,0.01200,0.0445,1.0000,0.7547 -3.500,-0.6397,0.01901,0.01321,0.0506,1.0000,0.8092 -3.250,-0.6166,0.02097,0.01502,0.0555,1.0000,0.8523 -3.000,-0.4619,0.02552,0.01891,0.0385,1.0000,0.8977 -2.750,-0.4070,0.02598,0.01908,0.0336,1.0000,0.9147 -2.500,-0.3441,0.02627,0.01912,0.0269,1.0000,0.9293 -2.250,-0.2902,0.02626,0.01893,0.0213,1.0000,0.9416 -2.000,-0.2430,0.02605,0.01854,0.0165,1.0000,0.9508 -1.750,-0.2084,0.02584,0.01823,0.0139,1.0000,0.9602 -1.500,-0.1766,0.02571,0.01800,0.0118,1.0000,0.9700 -1.250,-0.1341,0.02546,0.01766,0.0075,1.0000,0.9772 -1.000,-0.0978,0.02531,0.01745,0.0043,1.0000,0.9848 -0.750,-0.0597,0.02519,0.01729,0.0007,1.0000,0.9920 -0.500,-0.0202,0.02511,0.01717,-0.0033,1.0000,0.9986 -0.250,-0.0059,0.02509,0.01714,-0.0024,1.0000,1.0000 0.000,0.0000,0.02508,0.01713,0.0000,1.0000,1.0000 0.250,0.0059,0.02509,0.01715,0.0025,1.0000,1.0000 0.500,0.0202,0.02511,0.01717,0.0033,0.9986,1.0000 0.750,0.0591,0.02518,0.01728,-0.0005,0.9921,1.0000 1.000,0.0970,0.02531,0.01745,-0.0041,0.9849,1.0000 1.250,0.1345,0.02545,0.01766,-0.0075,0.9771,1.0000 1.500,0.1762,0.02570,0.01800,-0.0117,0.9700,1.0000 1.750,0.2079,0.02583,0.01821,-0.0138,0.9603,1.0000 2.000,0.2437,0.02603,0.01852,-0.0166,0.9506,1.0000 2.250,0.2899,0.02624,0.01890,-0.0212,0.9412,1.0000 2.500,0.3437,0.02626,0.01911,-0.0268,0.9293,1.0000 2.750,0.4050,0.02601,0.01910,-0.0333,0.9152,1.0000 3.000,0.4621,0.02550,0.01889,-0.0385,0.8974,1.0000 3.250,0.6166,0.02108,0.01513,-0.0557,0.8542,1.0000 3.500,0.6400,0.01905,0.01325,-0.0508,0.8103,1.0000 3.750,0.6508,0.01768,0.01200,-0.0449,0.7587,1.0000 4.000,0.6485,0.01723,0.00985,-0.0346,0.4058,1.0000 4.250,0.6367,0.02060,0.01111,-0.0282,0.1188,1.0000 4.500,0.6457,0.02193,0.01220,-0.0251,0.0888,1.0000 4.750,0.6570,0.02305,0.01329,-0.0222,0.0779,1.0000 5.000,0.6720,0.02419,0.01446,-0.0198,0.0721,1.0000 5.250,0.6889,0.02555,0.01573,-0.0181,0.0644,1.0000 5.500,0.7105,0.02692,0.01722,-0.0167,0.0606,1.0000 5.750,0.7345,0.02850,0.01897,-0.0155,0.0587,1.0000 6.000,0.7585,0.03042,0.02113,-0.0143,0.0575,1.0000 6.250,0.7797,0.03255,0.02359,-0.0127,0.0578,1.0000 6.500,0.7966,0.03462,0.02601,-0.0105,0.0572,1.0000 6.750,0.8101,0.03647,0.02812,-0.0082,0.0548,1.0000 7.000,0.8207,0.03923,0.03140,-0.0050,0.0557,1.0000 7.250,0.8283,0.04253,0.03515,-0.0015,0.0592,1.0000 7.500,0.8348,0.04627,0.03910,0.0014,0.0619,1.0000 7.750,0.8354,0.05106,0.04453,0.0064,0.0750,1.0000 10.500,0.5978,0.09636,0.09169,0.0342,0.1474,1.0000 10.750,0.5777,0.10250,0.09772,0.0298,0.1428,1.0000 11.000,0.5693,0.10682,0.10198,0.0271,0.1361,1.0000 11.250,0.4723,0.09889,0.09451,0.0373,0.1453,1.0000 11.500,0.4282,0.10377,0.09929,0.0317,0.1437,1.0000