Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe566-il-500000 Airfoil,goe566-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,88.494 Max Cl/Cd alpha,2.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe566-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.4534,0.08225,0.07997,-0.0361,1.0000,0.0257 -8.750,-0.4732,0.07565,0.07343,-0.0389,1.0000,0.0260 -8.500,-0.4845,0.07181,0.06962,-0.0404,1.0000,0.0262 -8.250,-0.4878,0.06825,0.06607,-0.0415,1.0000,0.0264 -8.000,-0.4860,0.06653,0.06436,-0.0404,1.0000,0.0268 -7.750,-0.4930,0.06336,0.06118,-0.0399,1.0000,0.0270 -7.500,-0.5026,0.06144,0.05926,-0.0371,1.0000,0.0273 -7.250,-0.4879,0.05755,0.05529,-0.0404,0.9975,0.0281 -7.000,-0.4554,0.04896,0.04624,-0.0492,0.9920,0.0325 -6.750,-0.4349,0.04250,0.03935,-0.0530,0.9867,0.0326 -6.250,-0.3996,0.02873,0.02480,-0.0577,0.9767,0.0342 -6.000,-0.3706,0.02590,0.02172,-0.0592,0.9736,0.0348 -5.750,-0.3378,0.02449,0.02019,-0.0610,0.9717,0.0364 -5.500,-0.3137,0.01862,0.01328,-0.0604,0.9669,0.0337 -5.250,-0.2842,0.01754,0.01215,-0.0612,0.9624,0.0352 -5.000,-0.2519,0.01641,0.01088,-0.0623,0.9591,0.0362 -4.750,-0.2191,0.01527,0.00958,-0.0633,0.9561,0.0372 -4.500,-0.1923,0.01453,0.00873,-0.0630,0.9495,0.0384 -4.250,-0.1625,0.01378,0.00786,-0.0633,0.9444,0.0395 -4.000,-0.1332,0.01304,0.00702,-0.0634,0.9393,0.0401 -3.750,-0.1072,0.01246,0.00637,-0.0628,0.9319,0.0407 -3.500,-0.0787,0.01209,0.00592,-0.0627,0.9264,0.0414 -3.250,-0.0554,0.01108,0.00485,-0.0617,0.9179,0.0428 -3.000,-0.0298,0.01047,0.00419,-0.0610,0.9106,0.0440 -2.750,-0.0059,0.01007,0.00377,-0.0600,0.9005,0.0451 -2.500,0.0191,0.00974,0.00340,-0.0592,0.8910,0.0465 -2.250,0.0444,0.00945,0.00306,-0.0584,0.8811,0.0480 -2.000,0.0693,0.00921,0.00279,-0.0575,0.8696,0.0500 -1.750,0.0950,0.00903,0.00255,-0.0568,0.8588,0.0522 -1.500,0.1203,0.00874,0.00221,-0.0560,0.8482,0.0566 -1.250,0.1461,0.00854,0.00200,-0.0553,0.8370,0.0635 -1.000,0.1700,0.00807,0.00184,-0.0545,0.8246,0.1509 -0.750,0.1922,0.00740,0.00171,-0.0535,0.8124,0.3246 -0.500,0.2067,0.00624,0.00169,-0.0510,0.8019,0.6810 -0.250,0.2256,0.00576,0.00172,-0.0485,0.7916,0.8387 0.000,0.2825,0.00564,0.00180,-0.0542,0.7812,0.9503 0.250,0.3330,0.00573,0.00182,-0.0588,0.7697,0.9779 0.500,0.3877,0.00584,0.00181,-0.0644,0.7523,0.9946 1.000,0.4508,0.00593,0.00168,-0.0659,0.7121,1.0000 1.250,0.4735,0.00600,0.00165,-0.0648,0.6920,1.0000 1.500,0.4963,0.00609,0.00165,-0.0636,0.6728,1.0000 1.750,0.5194,0.00619,0.00166,-0.0626,0.6527,1.0000 2.000,0.5424,0.00631,0.00169,-0.0615,0.6304,1.0000 2.250,0.5652,0.00646,0.00174,-0.0604,0.6054,1.0000 2.500,0.5876,0.00664,0.00180,-0.0592,0.5737,1.0000 2.750,0.6091,0.00689,0.00187,-0.0578,0.5287,1.0000 3.000,0.6287,0.00729,0.00199,-0.0562,0.4667,1.0000 3.250,0.6483,0.00776,0.00218,-0.0546,0.4104,1.0000 3.500,0.6693,0.00815,0.00238,-0.0533,0.3676,1.0000 3.750,0.6910,0.00851,0.00257,-0.0522,0.3325,1.0000 4.000,0.7129,0.00885,0.00277,-0.0511,0.3026,1.0000 4.250,0.7353,0.00917,0.00298,-0.0500,0.2791,1.0000 4.500,0.7584,0.00944,0.00318,-0.0491,0.2643,1.0000 4.750,0.7817,0.00969,0.00339,-0.0482,0.2540,1.0000 5.250,0.8286,0.01016,0.00382,-0.0466,0.2324,1.0000 5.500,0.8522,0.01039,0.00404,-0.0458,0.2236,1.0000 5.750,0.8753,0.01066,0.00427,-0.0449,0.2117,1.0000 6.000,0.8988,0.01091,0.00450,-0.0441,0.1981,1.0000 6.250,0.9224,0.01116,0.00473,-0.0433,0.1827,1.0000 6.500,0.9452,0.01147,0.00496,-0.0425,0.1567,1.0000 6.750,0.9645,0.01211,0.00534,-0.0412,0.1125,1.0000 7.000,0.9839,0.01276,0.00586,-0.0398,0.0900,1.0000 7.250,1.0048,0.01328,0.00634,-0.0387,0.0750,1.0000 7.500,1.0243,0.01394,0.00684,-0.0373,0.0488,1.0000 7.750,1.0435,0.01463,0.00746,-0.0359,0.0385,1.0000 8.000,1.0628,0.01530,0.00816,-0.0345,0.0338,1.0000 8.250,1.0824,0.01593,0.00886,-0.0332,0.0311,1.0000 8.500,1.0981,0.01688,0.00986,-0.0313,0.0281,1.0000 8.750,1.1154,0.01764,0.01071,-0.0296,0.0264,1.0000 9.000,1.1340,0.01826,0.01139,-0.0282,0.0247,1.0000 9.250,1.1509,0.01898,0.01217,-0.0266,0.0231,1.0000 9.500,1.1623,0.02011,0.01334,-0.0242,0.0217,1.0000 9.750,1.1717,0.02140,0.01473,-0.0215,0.0208,1.0000 10.000,1.1872,0.02207,0.01550,-0.0197,0.0201,1.0000 10.250,1.2000,0.02281,0.01631,-0.0174,0.0191,1.0000 10.500,1.2110,0.02365,0.01722,-0.0150,0.0184,1.0000 10.750,1.2220,0.02446,0.01809,-0.0127,0.0176,1.0000 11.000,1.2302,0.02553,0.01920,-0.0103,0.0169,1.0000 11.250,1.2291,0.02786,0.02162,-0.0071,0.0162,1.0000 11.500,1.2398,0.02876,0.02263,-0.0052,0.0159,1.0000 11.750,1.2486,0.02995,0.02395,-0.0033,0.0154,1.0000 12.000,1.2557,0.03138,0.02551,-0.0013,0.0151,1.0000 12.250,1.2619,0.03294,0.02719,0.0005,0.0147,1.0000 12.500,1.2670,0.03461,0.02898,0.0022,0.0143,1.0000 12.750,1.2715,0.03630,0.03080,0.0037,0.0140,1.0000 13.000,1.2745,0.03821,0.03282,0.0051,0.0137,1.0000 13.250,1.2772,0.04011,0.03481,0.0062,0.0133,1.0000 13.500,1.2786,0.04226,0.03706,0.0071,0.0131,1.0000 13.750,1.2782,0.04468,0.03952,0.0077,0.0126,1.0000 14.000,1.2708,0.04842,0.04344,0.0085,0.0125,1.0000 14.250,1.2595,0.05275,0.04798,0.0089,0.0123,1.0000 14.500,1.2548,0.05576,0.05116,0.0083,0.0122,1.0000 14.750,1.2464,0.05971,0.05531,0.0073,0.0120,1.0000 15.000,1.2349,0.06441,0.06019,0.0060,0.0120,1.0000 15.250,1.2256,0.06899,0.06494,0.0040,0.0118,1.0000 15.500,1.2099,0.07497,0.07111,0.0014,0.0118,1.0000 15.750,1.1942,0.08135,0.07766,-0.0018,0.0118,1.0000 16.000,1.1771,0.08848,0.08498,-0.0059,0.0117,1.0000 16.250,1.1596,0.09590,0.09256,-0.0100,0.0118,1.0000 16.500,1.1393,0.10441,0.10123,-0.0152,0.0118,1.0000 16.750,1.1179,0.11354,0.11052,-0.0207,0.0119,1.0000 17.000,1.0970,0.12278,0.11991,-0.0263,0.0120,1.0000 17.250,1.0722,0.13342,0.13068,-0.0328,0.0121,1.0000 17.500,1.0435,0.14557,0.14297,-0.0401,0.0123,1.0000