Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe234-il-50000-n5 Airfoil,goe234-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,27.6736 Max Cl/Cd alpha,7.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe234-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.1359,0.12969,0.12291,-0.0629,0.9569,0.1486 -9.000,-0.1353,0.12803,0.12127,-0.0649,0.9487,0.1493 -8.750,-0.1319,0.11958,0.11273,-0.0705,0.9436,0.1067 -8.500,-0.1237,0.11480,0.10790,-0.0725,0.9375,0.0941 -8.250,-0.1105,0.11161,0.10470,-0.0736,0.9311,0.0920 -8.000,-0.0974,0.10806,0.10112,-0.0771,0.9264,0.0914 -7.750,-0.0990,0.10590,0.09899,-0.0768,0.9169,0.0910 -7.500,-0.0894,0.10257,0.09565,-0.0796,0.9112,0.0903 -7.250,-0.0938,0.10037,0.09348,-0.0790,0.9014,0.0891 -7.000,-0.0861,0.09631,0.08941,-0.0827,0.8950,0.0872 -6.750,-0.0928,0.09297,0.08610,-0.0838,0.8844,0.0856 -6.500,-0.0808,0.08801,0.08111,-0.0895,0.8786,0.0850 -6.250,-0.0786,0.08618,0.07930,-0.0890,0.8689,0.0859 -6.000,-0.0602,0.08275,0.07584,-0.0930,0.8633,0.0874 -5.750,-0.0542,0.07921,0.07229,-0.0961,0.8546,0.0879 -5.500,-0.0357,0.07298,0.06599,-0.1047,0.8478,0.0876 -5.250,0.0372,0.05568,0.04812,-0.1405,0.8451,0.0897 -5.000,0.1407,0.04582,0.03727,-0.1705,0.8443,0.0958 -4.750,0.1594,0.04547,0.03694,-0.1701,0.8353,0.0979 -4.500,0.2007,0.04430,0.03566,-0.1742,0.8308,0.1029 -4.250,0.2471,0.04314,0.03440,-0.1789,0.8277,0.1100 -4.000,0.2739,0.04288,0.03413,-0.1801,0.8199,0.1159 -3.750,0.3094,0.04246,0.03375,-0.1826,0.8141,0.1252 -3.500,0.3517,0.04201,0.03342,-0.1857,0.8105,0.1430 -3.250,0.3714,0.04274,0.03435,-0.1840,0.8033,0.1604 -2.750,0.4125,0.04508,0.03678,-0.1786,0.7913,0.2128 -2.500,0.4312,0.04625,0.03781,-0.1781,0.7819,0.2428 -2.000,0.4925,0.04792,0.03913,-0.1780,0.7725,0.2922 -1.750,0.5014,0.04903,0.04019,-0.1758,0.7622,0.3039 -1.500,0.5265,0.04951,0.04058,-0.1749,0.7570,0.3205 -1.250,0.5580,0.04959,0.04055,-0.1747,0.7539,0.3391 -1.000,0.5677,0.05058,0.04151,-0.1736,0.7431,0.3490 -0.750,0.6039,0.05012,0.04089,-0.1758,0.7388,0.3570 -0.500,0.6514,0.04927,0.03984,-0.1802,0.7362,0.3643 -0.250,0.6572,0.05030,0.04088,-0.1783,0.7252,0.3683 0.250,0.7383,0.04914,0.03946,-0.1838,0.7184,0.3835 0.500,0.7466,0.05044,0.04075,-0.1828,0.7071,0.3885 0.750,0.7850,0.04996,0.04017,-0.1850,0.7033,0.3959 1.000,0.8275,0.04916,0.03927,-0.1875,0.7008,0.4030 1.250,0.8352,0.05076,0.04086,-0.1867,0.6887,0.4066 1.500,0.8743,0.05000,0.04004,-0.1885,0.6853,0.4114 2.000,0.9221,0.05071,0.04070,-0.1891,0.6700,0.4178 2.250,0.9709,0.04958,0.03945,-0.1924,0.6672,0.4213 2.500,0.9792,0.05110,0.04098,-0.1912,0.6547,0.4238 2.750,1.0220,0.04970,0.03956,-0.1926,0.6509,0.4271 3.250,1.0780,0.04935,0.03918,-0.1930,0.6343,0.4305 3.750,1.1343,0.04909,0.03887,-0.1934,0.6174,0.4357 4.250,1.1874,0.04915,0.03894,-0.1934,0.6003,0.4404 4.500,1.2231,0.04838,0.03815,-0.1940,0.5943,0.4422 4.750,1.2354,0.04948,0.03933,-0.1926,0.5830,0.4433 5.000,1.2824,0.04786,0.03766,-0.1942,0.5791,0.4460 5.250,1.2808,0.05007,0.03997,-0.1915,0.5653,0.4476 5.500,1.3282,0.04843,0.03828,-0.1931,0.5611,0.4518 5.750,1.3257,0.05077,0.04072,-0.1903,0.5471,0.4533 6.250,1.3689,0.05141,0.04142,-0.1887,0.5284,0.4572 6.750,1.4121,0.05194,0.04202,-0.1869,0.5094,0.4608 7.000,1.4116,0.05421,0.04439,-0.1845,0.4959,0.4624 7.250,1.4548,0.05257,0.04271,-0.1850,0.4905,0.4670 7.500,1.4495,0.05537,0.04562,-0.1824,0.4766,0.4688 7.750,1.4554,0.05732,0.04764,-0.1806,0.4651,0.4710 8.000,1.4850,0.05678,0.04711,-0.1801,0.4580,0.4741 8.250,1.4832,0.05948,0.04991,-0.1780,0.4459,0.4756 8.500,1.5181,0.05846,0.04889,-0.1777,0.4399,0.4787 8.750,1.5102,0.06190,0.05244,-0.1754,0.4279,0.4798 9.000,1.5465,0.06075,0.05126,-0.1751,0.4225,0.4838 9.250,1.5323,0.06505,0.05569,-0.1728,0.4111,0.4852 9.500,1.5644,0.06430,0.05498,-0.1723,0.4062,0.4896 9.750,1.5467,0.06924,0.06008,-0.1701,0.3962,0.4908 10.000,1.5678,0.06977,0.06068,-0.1692,0.3910,0.4948 10.250,1.6065,0.06842,0.05934,-0.1689,0.3878,0.4998 10.500,1.5554,0.07763,0.06879,-0.1664,0.3765,0.4986 10.750,1.5850,0.07712,0.06833,-0.1657,0.3730,0.5025 11.250,1.5415,0.08963,0.08115,-0.1636,0.3574,0.5035 11.500,1.5713,0.08887,0.08050,-0.1626,0.3552,0.5075 12.000,1.4625,0.11391,0.10580,-0.1650,0.3352,0.5040 12.500,1.4333,0.12759,0.11970,-0.1674,0.3221,0.5056