Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe456-il-1000000-n5 Airfoil,goe456-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,134.25 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe456-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.250,-0.3209,0.12966,0.12799,-0.0326,1.0000,0.0023 -11.000,-0.3182,0.12639,0.12474,-0.0328,1.0000,0.0023 -10.750,-0.3144,0.12402,0.12238,-0.0328,1.0000,0.0026 -10.500,-0.3093,0.12108,0.11945,-0.0336,0.9999,0.0026 -10.250,-0.2971,0.11725,0.11562,-0.0365,0.9990,0.0026 -10.000,-0.2847,0.11315,0.11152,-0.0397,0.9973,0.0025 -9.750,-0.2739,0.10987,0.10825,-0.0420,0.9931,0.0027 -9.500,-0.2625,0.10628,0.10466,-0.0447,0.9892,0.0029 -9.250,-0.2514,0.10270,0.10108,-0.0474,0.9836,0.0028 -9.000,-0.2383,0.09893,0.09731,-0.0506,0.9788,0.0028 -8.750,-0.2247,0.09522,0.09360,-0.0540,0.9727,0.0030 -8.500,-0.2077,0.09119,0.08956,-0.0585,0.9678,0.0033 -8.250,-0.1887,0.08702,0.08538,-0.0637,0.9614,0.0030 -8.000,-0.1626,0.08188,0.08022,-0.0714,0.9559,0.0039 -7.750,-0.1366,0.07691,0.07522,-0.0792,0.9455,0.0040 -7.500,-0.1135,0.07214,0.07040,-0.0862,0.9301,0.0040 -7.250,-0.1018,0.06870,0.06688,-0.0896,0.9098,0.0040 -7.000,-0.0952,0.06619,0.06429,-0.0913,0.8926,0.0032 -5.500,-0.0077,0.04286,0.04058,-0.1140,0.8246,0.0038 -5.250,0.0160,0.03766,0.03524,-0.1190,0.8168,0.0035 -5.000,0.0425,0.03148,0.02888,-0.1237,0.8088,0.0033 -4.750,0.0686,0.02182,0.01871,-0.1279,0.8020,0.0030 -4.500,0.0908,0.01460,0.01057,-0.1281,0.7944,0.0027 -4.250,0.1152,0.01174,0.00714,-0.1275,0.7869,0.0028 -4.000,0.1409,0.01045,0.00553,-0.1271,0.7784,0.0029 -3.750,0.1671,0.00961,0.00447,-0.1267,0.7703,0.0031 -3.500,0.1934,0.00900,0.00367,-0.1264,0.7615,0.0035 -3.250,0.2201,0.00861,0.00313,-0.1261,0.7514,0.0039 -3.000,0.2465,0.00814,0.00251,-0.1257,0.7402,0.0043 -2.750,0.2730,0.00795,0.00226,-0.1255,0.7279,0.0052 -2.500,0.2995,0.00775,0.00195,-0.1252,0.7147,0.0061 -2.250,0.3260,0.00759,0.00167,-0.1249,0.7013,0.0068 -2.000,0.3525,0.00738,0.00134,-0.1245,0.6876,0.0096 -1.750,0.3789,0.00732,0.00118,-0.1242,0.6737,0.0130 -1.500,0.4053,0.00722,0.00105,-0.1239,0.6605,0.0283 -1.000,0.4578,0.00692,0.00092,-0.1235,0.6380,0.1310 -0.750,0.4844,0.00694,0.00090,-0.1233,0.6262,0.1454 -0.500,0.5107,0.00700,0.00089,-0.1230,0.6113,0.1540 -0.250,0.5370,0.00705,0.00088,-0.1227,0.5968,0.1606 0.000,0.5636,0.00710,0.00088,-0.1225,0.5856,0.1694 0.250,0.5901,0.00714,0.00089,-0.1223,0.5760,0.1782 0.500,0.6171,0.00715,0.00090,-0.1222,0.5671,0.1889 0.750,0.6438,0.00718,0.00093,-0.1220,0.5589,0.2043 1.000,0.6703,0.00721,0.00098,-0.1218,0.5492,0.2259 1.250,0.6966,0.00724,0.00103,-0.1216,0.5368,0.2540 1.500,0.7228,0.00728,0.00110,-0.1214,0.5235,0.2868 1.750,0.7490,0.00731,0.00117,-0.1212,0.5122,0.3211 2.000,0.7752,0.00731,0.00126,-0.1210,0.5039,0.3662 2.250,0.7993,0.00687,0.00143,-0.1206,0.4961,0.6395 2.750,0.8592,0.00640,0.00166,-0.1218,0.4770,1.0000 3.000,0.8842,0.00659,0.00178,-0.1213,0.4539,1.0000 3.250,0.9041,0.00720,0.00203,-0.1200,0.3786,1.0000 3.500,0.9186,0.00831,0.00254,-0.1178,0.2597,1.0000 3.750,0.9386,0.00897,0.00292,-0.1166,0.2000,1.0000 4.000,0.9588,0.00961,0.00327,-0.1154,0.1452,1.0000 4.250,0.9711,0.01099,0.00409,-0.1128,0.0138,1.0000 4.500,0.9952,0.01126,0.00438,-0.1122,0.0087,1.0000 4.750,1.0190,0.01157,0.00473,-0.1115,0.0064,1.0000 5.000,1.0425,0.01189,0.00507,-0.1108,0.0051,1.0000 5.250,1.0649,0.01230,0.00552,-0.1098,0.0041,1.0000 5.500,1.0878,0.01265,0.00591,-0.1090,0.0034,1.0000 5.750,1.1100,0.01306,0.00634,-0.1081,0.0030,1.0000 6.000,1.1296,0.01370,0.00707,-0.1067,0.0025,1.0000 6.250,1.1499,0.01426,0.00771,-0.1054,0.0024,1.0000 6.500,1.1685,0.01495,0.00849,-0.1037,0.0021,1.0000 6.750,1.1847,0.01580,0.00944,-0.1017,0.0020,1.0000 7.000,1.1988,0.01676,0.01051,-0.0993,0.0019,1.0000 7.250,1.2153,0.01749,0.01130,-0.0975,0.0017,1.0000 7.500,1.2291,0.01837,0.01227,-0.0952,0.0016,1.0000 7.750,1.2480,0.01873,0.01264,-0.0939,0.0015,1.0000 8.000,1.2548,0.01990,0.01394,-0.0904,0.0014,1.0000 8.250,1.2591,0.02151,0.01568,-0.0865,0.0013,1.0000 8.500,1.2693,0.02293,0.01722,-0.0837,0.0013,1.0000 8.750,1.2876,0.02565,0.02011,-0.0821,0.0010,1.0000 9.000,1.3294,0.03065,0.02538,-0.0842,0.0009,1.0000 9.250,1.3496,0.03436,0.02937,-0.0827,0.0008,1.0000 9.500,1.3624,0.03799,0.03329,-0.0803,0.0008,1.0000 9.750,1.3685,0.04170,0.03729,-0.0770,0.0008,1.0000 10.000,1.3695,0.04516,0.04102,-0.0733,0.0008,1.0000 10.250,1.3652,0.04837,0.04448,-0.0691,0.0009,1.0000 10.500,1.3547,0.05110,0.04741,-0.0642,0.0009,1.0000 10.750,1.3414,0.05390,0.05041,-0.0596,0.0009,1.0000 11.000,1.3273,0.05680,0.05349,-0.0558,0.0009,1.0000 11.250,1.3109,0.06016,0.05704,-0.0526,0.0009,1.0000 11.500,1.2944,0.06376,0.06080,-0.0501,0.0010,1.0000 11.750,1.2767,0.06773,0.06494,-0.0485,0.0010,1.0000 12.000,1.2589,0.07202,0.06938,-0.0476,0.0010,1.0000 12.250,1.2397,0.07682,0.07434,-0.0477,0.0010,1.0000 12.500,1.2206,0.08202,0.07968,-0.0485,0.0010,1.0000 12.750,1.2012,0.08775,0.08555,-0.0503,0.0010,1.0000 13.000,1.1818,0.09404,0.09197,-0.0529,0.0010,1.0000