Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe462-il-200000 Airfoil,goe462-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,61.1652 Max Cl/Cd alpha,8 Url,http://airfoiltools.com/polar/csv?polar=xf-goe462-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,0.1715,0.10412,0.10099,-0.0820,0.8871,0.0276 -9.250,0.1970,0.10086,0.09759,-0.0868,0.8626,0.0286 -9.000,0.2117,0.09852,0.09513,-0.0886,0.8372,0.0295 -8.750,0.2226,0.09650,0.09300,-0.0894,0.8130,0.0306 -8.500,0.2317,0.09496,0.09136,-0.0900,0.7894,0.0313 -8.250,0.2381,0.09433,0.09063,-0.0907,0.7653,0.0317 -8.000,0.2430,0.09393,0.09013,-0.0913,0.7437,0.0318 -7.750,0.2471,0.09328,0.08942,-0.0914,0.7224,0.0319 -7.500,0.2633,0.08734,0.08336,-0.0904,0.7041,0.0326 -7.250,0.2733,0.08527,0.08118,-0.0900,0.6860,0.0332 -7.000,0.2824,0.08356,0.07938,-0.0897,0.6700,0.0340 -6.750,0.2910,0.08196,0.07771,-0.0895,0.6558,0.0351 -6.500,0.2990,0.08047,0.07614,-0.0895,0.6431,0.0364 -6.250,0.3097,0.07894,0.07453,-0.0903,0.6314,0.0382 -6.000,0.3256,0.07963,0.07519,-0.0956,0.6199,0.0395 -5.750,0.3365,0.07615,0.07164,-0.0955,0.6102,0.0400 -5.500,0.3477,0.07335,0.06877,-0.0944,0.5998,0.0408 -5.250,0.3614,0.07146,0.06684,-0.0947,0.5895,0.0420 -4.750,0.3937,0.06796,0.06322,-0.0975,0.5709,0.0457 -4.500,0.4284,0.06769,0.06281,-0.1062,0.5626,0.0485 -4.250,0.4468,0.06484,0.05997,-0.1084,0.5537,0.0490 -4.000,0.4553,0.06200,0.05704,-0.1059,0.5460,0.0501 -3.750,0.4724,0.06031,0.05534,-0.1062,0.5365,0.0526 -3.500,0.4998,0.05870,0.05362,-0.1100,0.5281,0.0574 -3.250,0.5435,0.05694,0.05175,-0.1193,0.5188,0.0592 -3.000,0.5535,0.05434,0.04910,-0.1172,0.5110,0.0603 -2.750,0.5745,0.05262,0.04734,-0.1181,0.5025,0.0626 -2.500,0.6420,0.05191,0.04641,-0.1320,0.4929,0.0697 -2.250,0.6489,0.04874,0.04323,-0.1292,0.4856,0.0706 -2.000,0.6695,0.04697,0.04138,-0.1295,0.4779,0.0726 -1.750,0.7007,0.04539,0.03971,-0.1325,0.4693,0.0770 -1.500,0.7551,0.04351,0.03763,-0.1415,0.4607,0.0815 -1.250,0.7768,0.04170,0.03577,-0.1417,0.4532,0.0832 -1.000,0.8091,0.04037,0.03430,-0.1444,0.4464,0.0873 -0.750,0.8697,0.03897,0.03269,-0.1537,0.4379,0.0924 -0.500,0.8923,0.03725,0.03083,-0.1539,0.4324,0.0939 -0.250,0.9231,0.03610,0.02966,-0.1558,0.4251,0.0977 0.000,0.9858,0.03532,0.02853,-0.1644,0.4182,0.1032 0.250,1.0070,0.03356,0.02677,-0.1643,0.4126,0.1048 0.500,1.0378,0.03267,0.02580,-0.1658,0.4066,0.1095 1.250,1.1489,0.03007,0.02275,-0.1737,0.3913,0.1312 1.500,1.1867,0.02948,0.02193,-0.1763,0.3868,0.1391 1.750,1.2289,0.03104,0.02318,-0.1784,0.3820,0.1485 2.000,1.2531,0.02911,0.02130,-0.1792,0.3774,0.1496 2.250,1.2793,0.02837,0.02051,-0.1797,0.3733,0.1521 2.500,1.3090,0.02820,0.02017,-0.1805,0.3696,0.1558 2.750,1.3450,0.02986,0.02163,-0.1813,0.3658,0.1607 3.000,1.3725,0.02872,0.02050,-0.1823,0.3620,0.1615 3.250,1.3986,0.02797,0.01975,-0.1828,0.3585,0.1632 3.500,1.4262,0.02777,0.01945,-0.1833,0.3553,0.1657 3.750,1.4554,0.02795,0.01947,-0.1839,0.3520,0.1694 4.000,1.4847,0.02940,0.02085,-0.1834,0.3485,0.1736 4.250,1.5110,0.02841,0.01992,-0.1842,0.3450,0.1745 4.500,1.5373,0.02806,0.01956,-0.1846,0.3419,0.1762 4.750,1.5641,0.02809,0.01951,-0.1848,0.3392,0.1799 5.000,1.5939,0.02952,0.02069,-0.1846,0.3364,0.1859 5.250,1.6184,0.02897,0.02031,-0.1849,0.3338,0.1870 5.500,1.6428,0.02889,0.02031,-0.1850,0.3310,0.1889 5.750,1.6677,0.02906,0.02050,-0.1848,0.3282,0.1924 6.000,1.6935,0.02996,0.02130,-0.1842,0.3255,0.1982 6.250,1.7204,0.02955,0.02081,-0.1849,0.3218,0.2004 6.500,1.7391,0.02957,0.02094,-0.1838,0.3163,0.2043 6.750,1.7590,0.03008,0.02140,-0.1822,0.3109,0.2100 7.000,1.7830,0.02970,0.02095,-0.1823,0.3065,0.2120 7.250,1.7993,0.02974,0.02110,-0.1808,0.3004,0.2154 7.500,1.8150,0.03022,0.02157,-0.1787,0.2948,0.2218 7.750,1.8357,0.03002,0.02128,-0.1783,0.2899,0.2242 8.000,1.8478,0.03021,0.02164,-0.1762,0.2844,0.2294 8.250,1.8576,0.03047,0.02193,-0.1736,0.2780,0.2352 8.500,1.8639,0.03074,0.02220,-0.1707,0.2719,0.2389 8.750,1.8679,0.03149,0.02306,-0.1672,0.2651,0.2459 9.000,1.8735,0.03196,0.02347,-0.1649,0.2584,0.2483 9.250,1.8802,0.03268,0.02434,-0.1628,0.2494,0.2537 9.500,1.8834,0.03390,0.02554,-0.1604,0.2409,0.2599 9.750,1.8893,0.03508,0.02677,-0.1588,0.2320,0.2656 10.000,1.8949,0.03651,0.02826,-0.1572,0.2245,0.2734 10.250,1.8945,0.03857,0.03030,-0.1553,0.2150,0.2834 10.500,1.8934,0.04078,0.03253,-0.1540,0.2016,0.2881 10.750,1.8864,0.04385,0.03556,-0.1526,0.1874,0.2979 11.000,1.8739,0.04775,0.03944,-0.1515,0.1710,0.3023 11.250,1.8520,0.05307,0.04472,-0.1506,0.1525,0.3101 11.500,1.8253,0.05949,0.05114,-0.1505,0.1350,0.3105 11.750,1.7982,0.06644,0.05815,-0.1510,0.1203,0.3108 12.000,1.7724,0.07370,0.06549,-0.1520,0.1080,0.3115 12.250,1.7460,0.08138,0.07329,-0.1533,0.0973,0.3119 12.500,1.7210,0.08920,0.08123,-0.1550,0.0885,0.3127 12.750,1.6961,0.09725,0.08942,-0.1570,0.0809,0.3133 13.000,1.6716,0.10551,0.09782,-0.1593,0.0739,0.3142