Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe766-il-50000 Airfoil,goe766-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,19.1604 Max Cl/Cd alpha,2.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-goe766-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.4683,0.10005,0.09265,0.0171,1.0000,0.3967 -8.250,-0.4376,0.09490,0.08748,0.0172,1.0000,0.4046 -8.000,-0.6502,0.06920,0.06168,-0.0149,1.0000,0.1908 -7.750,-0.6327,0.06488,0.05740,-0.0144,1.0000,0.1867 -7.500,-0.6631,0.05790,0.04979,-0.0144,1.0000,0.1734 -7.250,-0.6567,0.05399,0.04571,-0.0133,1.0000,0.1723 -7.000,-0.6500,0.05029,0.04177,-0.0119,1.0000,0.1711 -6.750,-0.6420,0.04679,0.03797,-0.0102,1.0000,0.1699 -6.500,-0.6323,0.04355,0.03437,-0.0084,1.0000,0.1693 -6.250,-0.6208,0.04078,0.03121,-0.0065,1.0000,0.1708 -6.000,-0.6080,0.03836,0.02830,-0.0043,1.0000,0.1734 -5.750,-0.5906,0.03590,0.02568,-0.0028,1.0000,0.1768 -5.500,-0.5704,0.03385,0.02357,-0.0015,1.0000,0.1811 -5.250,-0.5512,0.03206,0.02150,0.0002,1.0000,0.1877 -5.000,-0.5306,0.03022,0.01953,0.0016,1.0000,0.1954 -4.750,-0.5086,0.02866,0.01784,0.0029,1.0000,0.2052 -4.500,-0.4859,0.02709,0.01634,0.0041,1.0000,0.2184 -4.250,-0.4625,0.02561,0.01490,0.0052,1.0000,0.2362 -4.000,-0.4386,0.02415,0.01360,0.0064,1.0000,0.2624 -3.750,-0.4158,0.02272,0.01255,0.0076,1.0000,0.3027 -3.500,-0.3955,0.02129,0.01163,0.0093,1.0000,0.3669 -3.250,-0.3824,0.01967,0.01098,0.0124,1.0000,0.4731 -3.000,-0.3756,0.01874,0.01148,0.0195,1.0000,0.6856 -2.750,-0.2809,0.02135,0.01409,0.0181,1.0000,0.8837 -2.500,-0.1007,0.02249,0.01436,-0.0052,1.0000,0.9578 -2.250,0.0191,0.02126,0.01274,-0.0231,1.0000,1.0000 -2.000,0.0263,0.02083,0.01235,-0.0216,1.0000,1.0000 -1.750,0.0298,0.02058,0.01218,-0.0196,1.0000,1.0000 -1.500,0.0187,0.02073,0.01250,-0.0161,1.0000,1.0000 -1.250,0.0115,0.02174,0.01359,-0.0163,0.9844,1.0000 -1.000,0.1415,0.02116,0.01285,-0.0357,0.9328,1.0000 -0.750,0.2261,0.02051,0.01200,-0.0457,0.8780,1.0000 -0.500,0.2639,0.02036,0.01160,-0.0470,0.8303,1.0000 -0.250,0.2852,0.02046,0.01149,-0.0455,0.7921,1.0000 0.000,0.3039,0.02064,0.01146,-0.0435,0.7608,1.0000 0.250,0.3216,0.02089,0.01155,-0.0416,0.7323,1.0000 0.500,0.3403,0.02120,0.01170,-0.0397,0.7081,1.0000 0.750,0.3581,0.02159,0.01200,-0.0380,0.6842,1.0000 1.000,0.3770,0.02203,0.01233,-0.0364,0.6628,1.0000 1.250,0.3961,0.02252,0.01272,-0.0348,0.6433,1.0000 1.500,0.4149,0.02306,0.01317,-0.0332,0.6249,1.0000 1.750,0.4336,0.02366,0.01372,-0.0317,0.6079,1.0000 2.000,0.4523,0.02434,0.01436,-0.0302,0.5920,1.0000 2.250,0.4710,0.02507,0.01505,-0.0288,0.5775,1.0000 2.500,0.4902,0.02576,0.01567,-0.0272,0.5644,1.0000 2.750,0.5089,0.02656,0.01646,-0.0258,0.5512,1.0000 3.000,0.5262,0.02759,0.01756,-0.0245,0.5387,1.0000 3.250,0.5453,0.02847,0.01840,-0.0231,0.5280,1.0000 3.500,0.5633,0.02945,0.01942,-0.0217,0.5165,1.0000 3.750,0.5793,0.03072,0.02079,-0.0204,0.5058,1.0000 4.000,0.6000,0.03154,0.02154,-0.0189,0.4964,1.0000 4.250,0.6126,0.03316,0.02333,-0.0177,0.4853,1.0000 4.500,0.6335,0.03402,0.02414,-0.0161,0.4764,1.0000 4.750,0.6446,0.03579,0.02609,-0.0148,0.4653,1.0000 5.000,0.6603,0.03716,0.02750,-0.0133,0.4555,1.0000 5.250,0.6772,0.03834,0.02873,-0.0117,0.4449,1.0000 5.500,0.6848,0.04051,0.03105,-0.0102,0.4342,1.0000 5.750,0.7109,0.04081,0.03127,-0.0083,0.4239,1.0000 6.000,0.7113,0.04360,0.03427,-0.0069,0.4122,1.0000 6.250,0.7201,0.04562,0.03638,-0.0052,0.4013,1.0000 6.500,0.7516,0.04526,0.03594,-0.0031,0.3891,1.0000 6.750,0.7398,0.04925,0.04018,-0.0018,0.3774,1.0000 7.000,0.7416,0.05191,0.04292,-0.0002,0.3656,1.0000 7.250,0.7651,0.05221,0.04323,0.0020,0.3522,1.0000 7.500,0.7965,0.05155,0.04254,0.0043,0.3375,1.0000 7.750,0.7333,0.06127,0.05246,0.0037,0.3317,1.0000 8.000,0.7536,0.06180,0.05303,0.0060,0.3180,1.0000 8.250,0.6832,0.07253,0.06366,0.0028,0.3175,1.0000 8.500,0.6443,0.08020,0.07123,-0.0001,0.3154,1.0000 8.750,0.7450,0.07131,0.06258,0.0092,0.2880,1.0000 9.000,0.6800,0.08306,0.07419,0.0033,0.2899,1.0000 9.250,0.6568,0.08978,0.08085,0.0007,0.2875,1.0000 9.500,0.6370,0.09617,0.08719,-0.0019,0.2870,1.0000 9.750,0.6284,0.10205,0.09309,-0.0041,0.2902,1.0000 10.000,0.6340,0.10681,0.09786,-0.0049,0.2887,1.0000 10.250,0.5775,0.12193,0.11297,-0.0168,0.3720,1.0000