Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ah85l120-il-50000 Airfoil,ah85l120-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,21.3825 Max Cl/Cd alpha,5.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-ah85l120-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.5175,0.11100,0.10405,-0.0097,1.0000,0.3471 -10.000,-0.6095,0.08900,0.08240,-0.0370,1.0000,0.1657 -9.750,-0.6437,0.08203,0.07548,-0.0412,1.0000,0.1530 -9.500,-0.6846,0.07745,0.07091,-0.0410,1.0000,0.1487 -9.250,-0.7073,0.07324,0.06663,-0.0390,1.0000,0.1391 -9.000,-0.7391,0.06999,0.06325,-0.0355,1.0000,0.1344 -8.750,-0.7545,0.06629,0.05942,-0.0319,1.0000,0.1264 -8.500,-0.7764,0.06315,0.05603,-0.0270,1.0000,0.1210 -8.250,-0.7946,0.06083,0.05331,-0.0216,1.0000,0.1157 -8.000,-0.7964,0.05732,0.04965,-0.0180,1.0000,0.1120 -7.750,-0.8074,0.05407,0.04595,-0.0129,1.0000,0.1076 -7.500,-0.8165,0.05206,0.04319,-0.0073,1.0000,0.1031 -7.250,-0.8078,0.04854,0.03940,-0.0045,1.0000,0.1015 -7.000,-0.7995,0.04548,0.03597,-0.0015,1.0000,0.1004 -6.750,-0.7885,0.04275,0.03282,0.0014,1.0000,0.1003 -6.500,-0.7761,0.04047,0.03005,0.0043,1.0000,0.1022 -6.250,-0.7578,0.03774,0.02710,0.0060,1.0000,0.1069 -6.000,-0.7325,0.03534,0.02446,0.0070,1.0000,0.1100 -5.750,-0.7019,0.03318,0.02194,0.0077,1.0000,0.1159 -5.500,-0.6680,0.03127,0.01996,0.0075,1.0000,0.1314 -5.250,-0.6228,0.02906,0.01797,0.0061,1.0000,0.1602 -5.000,-0.3436,0.03753,0.02865,-0.0053,1.0000,0.8812 -4.750,-0.2615,0.03624,0.02670,-0.0151,1.0000,0.9259 -4.500,-0.1865,0.03425,0.02422,-0.0253,1.0000,0.9610 -4.250,-0.1074,0.03183,0.02134,-0.0374,1.0000,0.9926 -4.000,-0.0794,0.03074,0.02006,-0.0401,1.0000,1.0000 -3.750,-0.0745,0.03035,0.01960,-0.0380,1.0000,1.0000 -3.500,-0.0703,0.03004,0.01920,-0.0357,1.0000,1.0000 -3.250,-0.0666,0.02977,0.01886,-0.0333,1.0000,1.0000 -3.000,-0.0629,0.02954,0.01856,-0.0308,1.0000,1.0000 -2.750,-0.0590,0.02933,0.01828,-0.0282,1.0000,1.0000 -2.500,-0.0548,0.02913,0.01800,-0.0256,1.0000,1.0000 -2.250,-0.0503,0.02895,0.01777,-0.0230,1.0000,1.0000 -2.000,-0.0454,0.02879,0.01755,-0.0205,1.0000,1.0000 -1.750,-0.0404,0.02865,0.01737,-0.0179,1.0000,1.0000 -1.500,-0.0350,0.02853,0.01720,-0.0153,1.0000,1.0000 -1.250,-0.0295,0.02842,0.01707,-0.0128,1.0000,1.0000 -1.000,-0.0238,0.02833,0.01695,-0.0102,1.0000,1.0000 -0.750,-0.0180,0.02826,0.01686,-0.0076,1.0000,1.0000 -0.500,-0.0120,0.02822,0.01679,-0.0051,1.0000,1.0000 -0.250,-0.0060,0.02819,0.01674,-0.0025,1.0000,1.0000 0.000,0.0000,0.02818,0.01674,0.0000,1.0000,1.0000 0.250,0.0061,0.02819,0.01675,0.0026,1.0000,1.0000 0.500,0.0121,0.02822,0.01679,0.0051,1.0000,1.0000 0.750,0.0181,0.02826,0.01685,0.0077,1.0000,1.0000 1.000,0.0239,0.02833,0.01695,0.0102,1.0000,1.0000 1.250,0.0296,0.02842,0.01706,0.0128,1.0000,1.0000 1.500,0.0351,0.02852,0.01719,0.0153,1.0000,1.0000 1.750,0.0404,0.02864,0.01735,0.0179,1.0000,1.0000 2.000,0.0455,0.02878,0.01754,0.0205,1.0000,1.0000 2.250,0.0503,0.02894,0.01777,0.0230,1.0000,1.0000 2.500,0.0549,0.02912,0.01799,0.0256,1.0000,1.0000 2.750,0.0591,0.02931,0.01826,0.0282,1.0000,1.0000 3.000,0.0629,0.02952,0.01853,0.0308,1.0000,1.0000 3.250,0.0667,0.02975,0.01884,0.0333,1.0000,1.0000 3.500,0.0704,0.03002,0.01918,0.0358,1.0000,1.0000 3.750,0.0745,0.03033,0.01956,0.0381,1.0000,1.0000 4.000,0.0794,0.03071,0.02003,0.0401,1.0000,1.0000 4.250,0.1051,0.03174,0.02127,0.0379,0.9935,1.0000 4.500,0.1865,0.03423,0.02419,0.0253,0.9611,1.0000 4.750,0.2619,0.03620,0.02665,0.0150,0.9254,1.0000 5.000,0.3432,0.03752,0.02863,0.0053,0.8815,1.0000 5.250,0.6233,0.02915,0.01805,-0.0060,0.1570,1.0000 5.500,0.6664,0.03122,0.01991,-0.0072,0.1304,1.0000 5.750,0.7017,0.03320,0.02201,-0.0075,0.1149,1.0000 6.000,0.7330,0.03545,0.02456,-0.0070,0.1090,1.0000 6.250,0.7587,0.03800,0.02723,-0.0063,0.1050,1.0000 6.500,0.7762,0.04051,0.03009,-0.0043,0.1022,1.0000 6.750,0.7886,0.04283,0.03292,-0.0014,0.1003,1.0000 7.000,0.7988,0.04558,0.03611,0.0017,0.0999,1.0000 7.250,0.8075,0.04856,0.03943,0.0046,0.1014,1.0000 7.500,0.8159,0.05197,0.04311,0.0074,0.1030,1.0000 7.750,0.8067,0.05420,0.04604,0.0131,0.1076,1.0000 8.000,0.7959,0.05735,0.04968,0.0181,0.1117,1.0000 8.250,0.7933,0.06083,0.05333,0.0218,0.1155,1.0000 8.500,0.7753,0.06325,0.05614,0.0272,0.1211,1.0000 8.750,0.7529,0.06647,0.05960,0.0321,0.1265,1.0000 9.000,0.7375,0.07009,0.06335,0.0356,0.1346,1.0000 9.250,0.7061,0.07340,0.06679,0.0390,0.1394,1.0000 9.500,0.6846,0.07747,0.07092,0.0410,0.1487,1.0000 9.750,0.6427,0.08232,0.07576,0.0411,0.1538,1.0000 10.000,0.6050,0.08992,0.08329,0.0363,0.1676,1.0000 10.250,0.5079,0.07830,0.07214,0.0441,0.1467,1.0000 10.500,0.5162,0.11450,0.10749,0.0096,0.3338,1.0000