Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe563-il-200000 Airfoil,goe563-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,73.3198 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-goe563-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.4500,0.10745,0.10359,-0.0262,1.0000,0.0571 -10.000,-0.4639,0.10352,0.09973,-0.0320,1.0000,0.0594 -9.750,-0.4776,0.09926,0.09555,-0.0373,1.0000,0.0599 -9.500,-0.4770,0.09383,0.09016,-0.0369,1.0000,0.0606 -9.250,-0.4587,0.09188,0.08818,-0.0327,1.0000,0.0622 -9.000,-0.4502,0.08978,0.08609,-0.0316,1.0000,0.0647 -8.750,-0.4509,0.08673,0.08308,-0.0323,1.0000,0.0669 -8.500,-0.4620,0.08302,0.07944,-0.0348,1.0000,0.0698 -8.250,-0.4074,0.06737,0.06408,-0.0385,1.0000,0.0740 -8.000,-0.4024,0.06512,0.06185,-0.0362,1.0000,0.0755 -7.750,-0.5358,0.07041,0.06668,-0.0437,1.0000,0.0720 -7.500,-0.5279,0.06547,0.06197,-0.0411,1.0000,0.0736 -7.250,-0.5215,0.06393,0.06049,-0.0380,1.0000,0.0749 -7.000,-0.5205,0.06180,0.05835,-0.0360,1.0000,0.0765 -6.750,-0.5213,0.05904,0.05554,-0.0348,1.0000,0.0787 -6.500,-0.5344,0.05637,0.05207,-0.0356,1.0000,0.0851 -6.250,-0.5306,0.04991,0.04584,-0.0347,1.0000,0.0868 -6.000,-0.5203,0.04791,0.04390,-0.0329,1.0000,0.0885 -5.750,-0.5222,0.03377,0.02825,-0.0317,1.0000,0.0593 -5.500,-0.5094,0.02996,0.02412,-0.0303,1.0000,0.0581 -5.250,-0.4932,0.02724,0.02095,-0.0289,1.0000,0.0584 -5.000,-0.4700,0.02542,0.01868,-0.0283,0.9990,0.0595 -4.750,-0.4360,0.02344,0.01628,-0.0298,0.9958,0.0600 -4.500,-0.4043,0.02088,0.01344,-0.0311,0.9932,0.0619 -4.250,-0.3705,0.01996,0.01242,-0.0326,0.9891,0.0644 -4.000,-0.3344,0.01897,0.01127,-0.0343,0.9855,0.0662 -3.750,-0.2981,0.01814,0.01029,-0.0361,0.9821,0.0686 -3.500,-0.2648,0.01759,0.00959,-0.0371,0.9768,0.0716 -3.250,-0.2291,0.01667,0.00870,-0.0389,0.9729,0.0756 -3.000,-0.1904,0.01618,0.00823,-0.0411,0.9697,0.0806 -2.750,-0.1611,0.01566,0.00767,-0.0415,0.9630,0.0866 -2.500,-0.1237,0.01522,0.00728,-0.0434,0.9587,0.0999 -2.250,-0.0851,0.01450,0.00678,-0.0459,0.9557,0.1333 -2.000,-0.0592,0.01410,0.00653,-0.0456,0.9478,0.1702 -1.750,-0.0219,0.01364,0.00630,-0.0477,0.9436,0.2213 -1.500,0.0072,0.01260,0.00626,-0.0486,0.9388,0.4526 -1.250,0.0268,0.01169,0.00634,-0.0466,0.9315,0.6937 -1.000,0.1455,0.01128,0.00650,-0.0642,0.9444,1.0000 -0.750,0.1956,0.01115,0.00625,-0.0686,0.9415,1.0000 -0.500,0.2319,0.01099,0.00600,-0.0701,0.9321,1.0000 -0.250,0.2861,0.01060,0.00553,-0.0750,0.9273,1.0000 0.000,0.3190,0.01038,0.00526,-0.0756,0.9166,1.0000 0.250,0.3608,0.01010,0.00492,-0.0780,0.9110,1.0000 0.500,0.3854,0.01001,0.00480,-0.0771,0.8994,1.0000 0.750,0.4127,0.00990,0.00466,-0.0766,0.8891,1.0000 1.000,0.4443,0.00971,0.00444,-0.0768,0.8807,1.0000 1.250,0.4677,0.00965,0.00436,-0.0755,0.8681,1.0000 1.500,0.4918,0.00958,0.00428,-0.0743,0.8555,1.0000 1.750,0.5164,0.00950,0.00417,-0.0731,0.8416,1.0000 2.000,0.5409,0.00940,0.00405,-0.0718,0.8257,1.0000 2.250,0.5653,0.00932,0.00393,-0.0705,0.8084,1.0000 2.500,0.5890,0.00928,0.00385,-0.0691,0.7884,1.0000 2.750,0.6122,0.00927,0.00380,-0.0676,0.7656,1.0000 3.000,0.6354,0.00931,0.00379,-0.0661,0.7411,1.0000 3.250,0.6589,0.00939,0.00379,-0.0648,0.7167,1.0000 3.500,0.6813,0.00951,0.00386,-0.0633,0.6890,1.0000 3.750,0.7034,0.00967,0.00395,-0.0618,0.6574,1.0000 4.000,0.7244,0.00988,0.00405,-0.0600,0.6176,1.0000 4.250,0.7436,0.01022,0.00416,-0.0579,0.5670,1.0000 4.500,0.7608,0.01069,0.00434,-0.0556,0.5056,1.0000 4.750,0.7777,0.01124,0.00461,-0.0533,0.4451,1.0000 5.000,0.7952,0.01180,0.00493,-0.0514,0.3934,1.0000 5.250,0.8131,0.01240,0.00530,-0.0495,0.3493,1.0000 5.500,0.8316,0.01300,0.00570,-0.0478,0.3108,1.0000 5.750,0.8513,0.01352,0.00612,-0.0464,0.2771,1.0000 6.000,0.8711,0.01405,0.00653,-0.0450,0.2433,1.0000 6.250,0.8906,0.01462,0.00696,-0.0436,0.2095,1.0000 6.500,0.9103,0.01521,0.00743,-0.0422,0.1762,1.0000 6.750,0.9283,0.01596,0.00800,-0.0407,0.1397,1.0000 7.000,0.9432,0.01708,0.00886,-0.0387,0.0985,1.0000 7.250,0.9596,0.01810,0.00975,-0.0367,0.0752,1.0000 7.500,0.9771,0.01897,0.01058,-0.0350,0.0650,1.0000 7.750,0.9925,0.02005,0.01161,-0.0330,0.0587,1.0000 8.000,1.0107,0.02089,0.01254,-0.0313,0.0538,1.0000 8.250,1.0247,0.02228,0.01387,-0.0293,0.0494,1.0000 8.500,1.0431,0.02334,0.01505,-0.0277,0.0467,1.0000 8.750,1.0614,0.02452,0.01630,-0.0262,0.0440,1.0000 9.000,1.0792,0.02584,0.01761,-0.0249,0.0414,1.0000 9.250,1.0995,0.02807,0.01993,-0.0240,0.0390,1.0000 9.500,1.1191,0.02952,0.02159,-0.0227,0.0375,1.0000 9.750,1.1383,0.03129,0.02356,-0.0215,0.0361,1.0000 10.000,1.1558,0.03302,0.02546,-0.0202,0.0347,1.0000 10.250,1.1716,0.03477,0.02731,-0.0189,0.0332,1.0000 10.500,1.1874,0.03829,0.03098,-0.0181,0.0317,1.0000 10.750,1.1935,0.04170,0.03475,-0.0158,0.0312,1.0000 11.000,1.1961,0.04392,0.03732,-0.0128,0.0309,1.0000 11.250,1.1948,0.04664,0.04037,-0.0097,0.0307,1.0000 11.500,1.1866,0.04935,0.04340,-0.0058,0.0306,1.0000 11.750,1.1750,0.05227,0.04658,-0.0021,0.0306,1.0000 12.000,1.1608,0.05550,0.05007,0.0010,0.0307,1.0000 12.250,1.1435,0.05917,0.05399,0.0034,0.0308,1.0000 12.500,1.1259,0.06340,0.05843,0.0048,0.0310,1.0000 12.750,1.1058,0.06801,0.06324,0.0054,0.0311,1.0000