Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe424-il-50000-n5 Airfoil,goe424-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,16.2157 Max Cl/Cd alpha,1.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe424-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.3790,0.08695,0.08038,-0.0827,0.9737,0.0732 -10.750,-0.3985,0.07966,0.07294,-0.0893,0.9610,0.0728 -10.500,-0.4206,0.07397,0.06703,-0.0932,0.9458,0.0726 -10.250,-0.4409,0.06959,0.06238,-0.0940,0.9285,0.0726 -9.750,-0.4651,0.06174,0.05370,-0.0931,0.8951,0.0734 -9.500,-0.4536,0.05875,0.05056,-0.0931,0.8813,0.0744 -9.250,-0.4413,0.05593,0.04750,-0.0929,0.8682,0.0752 -9.000,-0.4262,0.05298,0.04421,-0.0929,0.8572,0.0759 -8.750,-0.4119,0.05065,0.04161,-0.0922,0.8441,0.0773 -8.500,-0.3979,0.04854,0.03917,-0.0912,0.8309,0.0789 -8.250,-0.3796,0.04635,0.03657,-0.0906,0.8199,0.0805 -8.000,-0.3581,0.04430,0.03407,-0.0902,0.8094,0.0817 -7.750,-0.3381,0.04265,0.03203,-0.0893,0.7975,0.0826 -7.500,-0.3061,0.04076,0.03000,-0.0903,0.7898,0.0848 -7.250,-0.2835,0.03958,0.02871,-0.0897,0.7780,0.0870 -7.000,-0.2497,0.03810,0.02700,-0.0906,0.7712,0.0893 -6.750,-0.2263,0.03719,0.02592,-0.0898,0.7599,0.0908 -6.500,-0.1923,0.03607,0.02452,-0.0905,0.7533,0.0934 -6.250,-0.1695,0.03531,0.02376,-0.0898,0.7430,0.0960 -6.000,-0.1392,0.03437,0.02273,-0.0901,0.7365,0.0993 -5.750,-0.1187,0.03387,0.02214,-0.0889,0.7277,0.1017 -5.500,-0.0941,0.03326,0.02134,-0.0883,0.7211,0.1046 -5.250,-0.0725,0.03266,0.02064,-0.0875,0.7149,0.1085 -5.000,-0.0568,0.03221,0.02017,-0.0859,0.7073,0.1129 -4.750,-0.0339,0.03161,0.01942,-0.0852,0.7020,0.1187 -4.500,-0.0176,0.03122,0.01901,-0.0837,0.6955,0.1242 -4.250,-0.0007,0.03080,0.01861,-0.0823,0.6892,0.1337 -4.000,0.0204,0.02998,0.01804,-0.0817,0.6847,0.1605 -3.750,0.0345,0.02917,0.01773,-0.0802,0.6798,0.2546 -3.500,0.0405,0.02879,0.01814,-0.0769,0.6738,0.4115 -3.250,0.0583,0.02871,0.01832,-0.0748,0.6693,0.4974 -3.000,0.0817,0.02868,0.01836,-0.0732,0.6657,0.5641 -2.750,0.0922,0.02920,0.01900,-0.0701,0.6598,0.6094 -2.500,0.1077,0.02961,0.01945,-0.0675,0.6547,0.6523 -2.250,0.1302,0.02987,0.01969,-0.0658,0.6509,0.6909 -2.000,0.1581,0.03008,0.01985,-0.0648,0.6481,0.7264 -1.750,0.1701,0.03085,0.02066,-0.0620,0.6428,0.7537 -1.500,0.1855,0.03152,0.02133,-0.0596,0.6377,0.7831 -1.250,0.2147,0.03200,0.02174,-0.0588,0.6340,0.8153 -1.000,0.2513,0.03231,0.02191,-0.0595,0.6311,0.8456 -0.750,0.2868,0.03283,0.02228,-0.0608,0.6278,0.8675 -0.500,0.3002,0.03400,0.02347,-0.0597,0.6218,0.8871 -0.250,0.3340,0.03455,0.02387,-0.0615,0.6176,0.9046 0.000,0.3778,0.03479,0.02393,-0.0649,0.6145,0.9207 0.250,0.4266,0.03489,0.02382,-0.0690,0.6120,0.9357 0.500,0.4527,0.03628,0.02520,-0.0710,0.6066,0.9533 0.750,0.4871,0.03734,0.02621,-0.0743,0.6015,0.9697 1.000,0.5343,0.03774,0.02648,-0.0790,0.5979,0.9838 1.250,0.5875,0.03785,0.02644,-0.0845,0.5952,0.9964 1.500,0.6149,0.03792,0.02636,-0.0852,0.5929,1.0000 1.750,0.5015,0.04206,0.03071,-0.0667,0.5816,1.0000 2.000,0.5073,0.04261,0.03114,-0.0639,0.5780,1.0000 2.250,0.5303,0.04278,0.03116,-0.0633,0.5756,1.0000 3.750,0.4918,0.05464,0.04270,-0.0447,0.5389,1.0000 4.250,0.4823,0.05976,0.04778,-0.0413,0.5240,1.0000 4.500,0.5102,0.06009,0.04803,-0.0413,0.5212,1.0000 5.000,0.5090,0.06480,0.05271,-0.0388,0.5066,1.0000 5.250,0.5370,0.06514,0.05299,-0.0388,0.5036,1.0000 5.750,0.5409,0.06958,0.05742,-0.0368,0.4889,1.0000 6.000,0.5694,0.06985,0.05764,-0.0368,0.4859,1.0000 6.250,0.5559,0.07329,0.06111,-0.0354,0.4757,1.0000 6.500,0.5764,0.07412,0.06192,-0.0351,0.4709,1.0000 6.750,0.6062,0.07424,0.06200,-0.0351,0.4681,1.0000 7.000,0.5899,0.07797,0.06578,-0.0339,0.4568,1.0000 7.250,0.6148,0.07842,0.06621,-0.0337,0.4528,1.0000 7.750,0.6268,0.08245,0.07027,-0.0326,0.4381,1.0000 8.000,0.6550,0.08259,0.07040,-0.0325,0.4350,1.0000 8.250,0.6418,0.08630,0.07416,-0.0317,0.4239,1.0000 8.500,0.6657,0.08680,0.07467,-0.0315,0.4201,1.0000 9.000,0.6771,0.09108,0.07901,-0.0308,0.4055,1.0000 9.250,0.7040,0.09126,0.07920,-0.0306,0.4027,1.0000 9.500,0.6886,0.09556,0.08357,-0.0303,0.3916,1.0000 9.750,0.7127,0.09594,0.08397,-0.0301,0.3881,1.0000 10.000,0.7022,0.09990,0.08799,-0.0300,0.3782,1.0000 10.250,0.7209,0.10091,0.08902,-0.0298,0.3740,1.0000 10.500,0.7444,0.10137,0.08952,-0.0296,0.3712,1.0000 10.750,0.7287,0.10612,0.09434,-0.0298,0.3606,1.0000 11.000,0.7515,0.10658,0.09483,-0.0296,0.3573,1.0000