Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe429-il-50000-n5 Airfoil,goe429-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.8956 Max Cl/Cd alpha,7 Url,http://airfoiltools.com/polar/csv?polar=xf-goe429-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,-0.8610,0.10084,0.09378,0.0158,1.0000,0.0759 -12.000,-0.9023,0.08763,0.08049,0.0067,1.0000,0.0752 -11.750,-0.9393,0.07703,0.06975,-0.0010,1.0000,0.0745 -11.500,-0.9702,0.06893,0.06142,-0.0065,1.0000,0.0743 -11.250,-0.9957,0.06275,0.05494,-0.0098,1.0000,0.0749 -11.000,-1.0165,0.05770,0.04945,-0.0107,1.0000,0.0762 -10.750,-1.0057,0.05575,0.04759,-0.0102,1.0000,0.0801 -10.500,-1.0033,0.05278,0.04439,-0.0102,1.0000,0.0844 -10.250,-1.0059,0.04888,0.03985,-0.0102,1.0000,0.0890 -10.000,-0.9890,0.04728,0.03838,-0.0098,1.0000,0.0947 -9.750,-0.9797,0.04456,0.03522,-0.0096,1.0000,0.1014 -9.500,-0.9628,0.04262,0.03326,-0.0092,1.0000,0.1077 -9.250,-0.9465,0.04049,0.03084,-0.0088,1.0000,0.1147 -9.000,-0.9275,0.03860,0.02884,-0.0085,1.0000,0.1212 -8.750,-0.9074,0.03691,0.02694,-0.0081,1.0000,0.1283 -8.500,-0.8863,0.03525,0.02515,-0.0078,1.0000,0.1352 -8.250,-0.8644,0.03385,0.02362,-0.0074,1.0000,0.1429 -8.000,-0.8417,0.03249,0.02219,-0.0070,1.0000,0.1502 -7.750,-0.8186,0.03121,0.02068,-0.0067,1.0000,0.1596 -7.500,-0.7953,0.03011,0.01962,-0.0064,1.0000,0.1685 -7.250,-0.7715,0.02897,0.01841,-0.0061,1.0000,0.1790 -7.000,-0.7476,0.02789,0.01727,-0.0058,1.0000,0.1922 -6.750,-0.7236,0.02683,0.01616,-0.0055,1.0000,0.2072 -6.500,-0.6997,0.02582,0.01519,-0.0052,1.0000,0.2250 -6.250,-0.6758,0.02487,0.01430,-0.0049,1.0000,0.2467 -6.000,-0.6515,0.02400,0.01348,-0.0046,1.0000,0.2713 -5.750,-0.6270,0.02328,0.01282,-0.0043,1.0000,0.2976 -5.500,-0.6021,0.02267,0.01229,-0.0040,1.0000,0.3242 -5.250,-0.5767,0.02214,0.01178,-0.0037,1.0000,0.3509 -5.000,-0.5510,0.02167,0.01132,-0.0034,1.0000,0.3775 -4.750,-0.5253,0.02126,0.01096,-0.0030,1.0000,0.4025 -4.500,-0.4994,0.02089,0.01063,-0.0027,1.0000,0.4302 -4.250,-0.4740,0.02060,0.01040,-0.0022,1.0000,0.4609 -4.000,-0.4489,0.02037,0.01029,-0.0014,1.0000,0.4894 -3.750,-0.4235,0.02013,0.01014,-0.0007,1.0000,0.5142 -3.500,-0.3978,0.01988,0.00993,-0.0002,1.0000,0.5357 -3.250,-0.3721,0.01963,0.00970,0.0003,1.0000,0.5565 -3.000,-0.3469,0.01944,0.00956,0.0008,1.0000,0.5759 -2.750,-0.3224,0.01929,0.00945,0.0015,1.0000,0.5948 -2.500,-0.2989,0.01915,0.00935,0.0022,1.0000,0.6139 -2.250,-0.2769,0.01902,0.00926,0.0030,1.0000,0.6333 -2.000,-0.2566,0.01893,0.00917,0.0039,1.0000,0.6531 -1.750,-0.2375,0.01887,0.00916,0.0051,1.0000,0.6716 -1.500,-0.2052,0.01886,0.00918,0.0039,0.9885,0.6921 -1.250,-0.1616,0.01885,0.00918,0.0008,0.9696,0.7160 -1.000,-0.1213,0.01884,0.00924,-0.0012,0.9499,0.7384 -0.750,-0.0828,0.01882,0.00927,-0.0027,0.9304,0.7616 -0.500,-0.0487,0.01879,0.00929,-0.0032,0.9095,0.7835 -0.250,-0.0184,0.01875,0.00930,-0.0028,0.8873,0.8034 0.000,0.0101,0.01871,0.00928,-0.0018,0.8651,0.8229 0.250,0.0356,0.01865,0.00926,-0.0004,0.8406,0.8429 0.500,0.0615,0.01857,0.00920,0.0011,0.8171,0.8632 0.750,0.0892,0.01849,0.00914,0.0022,0.7912,0.8837 1.000,0.1195,0.01840,0.00905,0.0028,0.7662,0.9058 1.250,0.1530,0.01833,0.00898,0.0026,0.7386,0.9293 1.500,0.1904,0.01827,0.00889,0.0014,0.7084,0.9537 1.750,0.2291,0.01821,0.00880,-0.0003,0.6751,0.9811 2.000,0.2597,0.01818,0.00869,-0.0009,0.6408,1.0000 2.250,0.2799,0.01822,0.00863,0.0003,0.6068,1.0000 2.500,0.3025,0.01832,0.00860,0.0012,0.5685,1.0000 2.750,0.3262,0.01847,0.00858,0.0021,0.5276,1.0000 3.000,0.3505,0.01873,0.00863,0.0028,0.4866,1.0000 3.250,0.3753,0.01910,0.00874,0.0035,0.4485,1.0000 3.500,0.4006,0.01957,0.00899,0.0039,0.4157,1.0000 3.750,0.4264,0.02012,0.00938,0.0041,0.3880,1.0000 4.000,0.4526,0.02071,0.00982,0.0042,0.3652,1.0000 4.250,0.4793,0.02132,0.01034,0.0043,0.3465,1.0000 4.500,0.5060,0.02196,0.01093,0.0044,0.3313,1.0000 4.750,0.5329,0.02262,0.01160,0.0044,0.3174,1.0000 5.000,0.5599,0.02329,0.01232,0.0045,0.3049,1.0000 5.250,0.5864,0.02397,0.01303,0.0046,0.2923,1.0000 5.500,0.6123,0.02459,0.01366,0.0047,0.2772,1.0000 5.750,0.6377,0.02516,0.01425,0.0049,0.2605,1.0000 6.000,0.6628,0.02573,0.01488,0.0050,0.2443,1.0000 6.250,0.6877,0.02632,0.01553,0.0051,0.2283,1.0000 6.500,0.7124,0.02695,0.01624,0.0052,0.2127,1.0000 6.750,0.7364,0.02757,0.01697,0.0054,0.1943,1.0000 7.000,0.7598,0.02825,0.01773,0.0055,0.1755,1.0000 7.250,0.7826,0.02910,0.01862,0.0057,0.1574,1.0000 7.500,0.8051,0.03023,0.01990,0.0060,0.1378,1.0000 7.750,0.8265,0.03153,0.02127,0.0063,0.1219,1.0000 8.000,0.8473,0.03289,0.02264,0.0067,0.1106,1.0000 8.250,0.8677,0.03428,0.02407,0.0070,0.1019,1.0000 8.500,0.8879,0.03595,0.02590,0.0075,0.0959,1.0000 8.750,0.9073,0.03766,0.02776,0.0080,0.0915,1.0000 9.000,0.9259,0.03927,0.02941,0.0084,0.0885,1.0000 9.250,0.9430,0.04150,0.03192,0.0089,0.0854,1.0000 9.500,0.9580,0.04378,0.03447,0.0093,0.0823,1.0000 9.750,0.9721,0.04577,0.03659,0.0096,0.0795,1.0000 10.000,0.9867,0.04751,0.03833,0.0101,0.0773,1.0000 10.250,0.9931,0.05084,0.04202,0.0103,0.0759,1.0000 10.500,0.9933,0.05469,0.04627,0.0103,0.0749,1.0000 10.750,0.9851,0.05907,0.05099,0.0098,0.0742,1.0000 11.000,0.9656,0.06440,0.05661,0.0081,0.0740,1.0000 11.250,0.9343,0.07230,0.06475,0.0030,0.0742,1.0000 11.500,0.8841,0.08545,0.07811,-0.0070,0.0751,1.0000