Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe561-il-100000-n5 Airfoil,goe561-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,8.62433 Max Cl/Cd alpha,-6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe561-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -15.750,0.4723,0.13520,0.12776,-0.1677,0.6818,0.0498 -15.500,0.4823,0.13313,0.12567,-0.1689,0.6733,0.0504 -15.250,0.4928,0.13098,0.12348,-0.1703,0.6656,0.0511 -15.000,0.5045,0.12882,0.12121,-0.1722,0.6586,0.0518 -14.750,0.5111,0.12696,0.11935,-0.1731,0.6514,0.0524 -14.500,0.5170,0.12517,0.11754,-0.1744,0.6449,0.0529 -14.250,0.5223,0.12353,0.11583,-0.1760,0.6396,0.0531 -14.000,0.5363,0.12082,0.11309,-0.1768,0.6341,0.0536 -13.750,0.5478,0.11865,0.11091,-0.1775,0.6280,0.0542 -13.500,0.5578,0.11664,0.10887,-0.1782,0.6227,0.0556 -13.250,0.5664,0.11477,0.10693,-0.1791,0.6184,0.0564 -13.000,0.5714,0.11306,0.10519,-0.1800,0.6142,0.0576 -12.750,0.5746,0.11150,0.10365,-0.1806,0.6097,0.0580 -12.500,0.5747,0.11010,0.10225,-0.1814,0.6058,0.0583 -12.250,0.5851,0.10781,0.09992,-0.1816,0.6012,0.0586 -12.000,0.5982,0.10552,0.09756,-0.1820,0.5977,0.0592 -11.750,0.6076,0.10354,0.09556,-0.1823,0.5942,0.0603 -11.500,0.6142,0.10183,0.09388,-0.1825,0.5904,0.0610 -11.250,0.6200,0.10013,0.09218,-0.1828,0.5872,0.0618 -11.000,0.6215,0.09849,0.09055,-0.1831,0.5843,0.0631 -10.750,0.6199,0.09706,0.08911,-0.1836,0.5815,0.0637 -10.500,0.6162,0.09557,0.08761,-0.1842,0.5792,0.0640 -10.250,0.6326,0.09320,0.08516,-0.1842,0.5762,0.0645 -10.000,0.6419,0.09138,0.08339,-0.1835,0.5729,0.0654 -9.750,0.6465,0.08980,0.08184,-0.1830,0.5698,0.0662 -9.500,0.6492,0.08821,0.08029,-0.1825,0.5670,0.0676 -9.250,0.6329,0.08701,0.07914,-0.1827,0.5651,0.0700 -9.000,0.6282,0.08544,0.07760,-0.1824,0.5628,0.0701 -8.750,0.6446,0.08333,0.07546,-0.1815,0.5600,0.0709 -8.500,0.6565,0.08165,0.07373,-0.1811,0.5576,0.0729 -8.250,0.6582,0.08001,0.07207,-0.1809,0.5556,0.0742 -8.000,0.6451,0.07870,0.07088,-0.1795,0.5533,0.0760 -7.750,0.6252,0.07728,0.06958,-0.1782,0.5511,0.0767 -7.500,0.6141,0.07549,0.06788,-0.1766,0.5489,0.0772 -7.250,0.6237,0.07401,0.06643,-0.1746,0.5461,0.0781 -7.000,0.6215,0.07255,0.06500,-0.1728,0.5439,0.0790 -6.750,0.6125,0.07102,0.06352,-0.1710,0.5418,0.0800 -6.500,0.5969,0.06945,0.06198,-0.1688,0.5398,0.0810 -6.250,0.5749,0.06807,0.06061,-0.1651,0.5381,0.0822 -6.000,0.5448,0.06707,0.05960,-0.1595,0.5365,0.0831 -5.750,0.5038,0.06625,0.05869,-0.1530,0.5351,0.0841 -5.500,0.4668,0.06582,0.05829,-0.1448,0.5332,0.0843 -5.250,0.4507,0.06482,0.05741,-0.1388,0.5305,0.0846 -5.000,0.4429,0.06372,0.05642,-0.1340,0.5279,0.0851 -4.750,0.4311,0.06279,0.05556,-0.1285,0.5253,0.0856 -4.500,0.4174,0.06188,0.05467,-0.1228,0.5229,0.0863 -4.250,0.4070,0.06083,0.05361,-0.1176,0.5205,0.0872 -4.000,0.4003,0.05961,0.05230,-0.1132,0.5182,0.0891 -3.750,0.3740,0.05876,0.05113,-0.1057,0.5166,0.0930 -3.500,0.3932,0.05661,0.04896,-0.1056,0.5146,0.0943 -3.250,0.3668,0.05644,0.04888,-0.0971,0.5121,0.0946 -3.000,0.3253,0.05702,0.04962,-0.0862,0.5086,0.0945 -2.750,0.2934,0.05744,0.05013,-0.0774,0.5050,0.0946 -2.500,0.2757,0.05733,0.05005,-0.0709,0.5018,0.0954 -2.250,0.2717,0.05663,0.04927,-0.0666,0.4991,0.0969 -2.000,0.2651,0.05601,0.04834,-0.0614,0.4969,0.1029 -1.750,0.2858,0.05389,0.04615,-0.0607,0.4951,0.1051 -1.500,0.1275,0.06432,0.05732,-0.0383,0.4824,0.0949 -1.250,0.1161,0.06463,0.05759,-0.0338,0.4783,0.0960 -1.000,0.1217,0.06345,0.05606,-0.0302,0.4763,0.1031 -0.750,0.1407,0.06126,0.05379,-0.0287,0.4750,0.1049 -0.250,0.1748,0.05527,0.04657,-0.0203,0.4724,0.0578 3.250,-0.0061,0.08046,0.07055,0.0309,0.3845,0.0530 3.750,0.0009,0.08337,0.07327,0.0333,0.3747,0.0528 4.250,0.0554,0.08263,0.07213,0.0324,0.3721,0.0526 4.500,0.0884,0.08214,0.07142,0.0311,0.3713,0.0526 5.000,0.0792,0.08817,0.07736,0.0325,0.3584,0.0529 5.500,0.1312,0.08939,0.07849,0.0293,0.3550,0.0553 6.500,0.2057,0.09630,0.08516,0.0228,0.3416,0.0580 6.750,0.2428,0.09685,0.08571,0.0193,0.3407,0.0589 7.250,0.2291,0.10552,0.09451,0.0184,0.3287,0.0594 7.500,0.2644,0.10653,0.09555,0.0148,0.3275,0.0612 7.750,0.3059,0.10763,0.09663,0.0099,0.3264,0.0645 8.000,0.3533,0.10908,0.09808,0.0035,0.3256,0.0676 8.500,0.3353,0.11942,0.10853,0.0017,0.3142,0.0689 8.750,0.3693,0.12127,0.11033,-0.0026,0.3129,0.0715 9.000,0.4031,0.12233,0.11133,-0.0058,0.3118,0.0740 9.250,0.4350,0.12355,0.11252,-0.0088,0.3110,0.0828 9.750,0.4137,0.13383,0.12291,-0.0101,0.3010,0.0852 10.000,0.4331,0.13589,0.12496,-0.0120,0.2996,0.0914 10.250,0.4577,0.13757,0.12670,-0.0143,0.2983,0.1115 10.750,0.6204,0.14905,0.14009,-0.0458,0.2963,1.0000 11.250,0.5948,0.15983,0.15098,-0.0467,0.2878,1.0000 11.500,0.6038,0.16194,0.15304,-0.0470,0.2863,1.0000