Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe321-il-50000-n5 Airfoil,goe321-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,34.1421 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe321-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.2884,0.11383,0.10728,-0.0230,1.0000,0.1018 -9.000,-0.2913,0.11228,0.10583,-0.0263,1.0000,0.1052 -8.750,-0.3022,0.11164,0.10535,-0.0307,1.0000,0.1063 -8.500,-0.2855,0.10622,0.09998,-0.0297,1.0000,0.1083 -8.250,-0.2709,0.10240,0.09621,-0.0289,1.0000,0.1117 -8.000,-0.2677,0.09994,0.09388,-0.0295,1.0000,0.1145 -7.750,-0.2761,0.09861,0.09272,-0.0290,0.9999,0.1167 -7.500,-0.2663,0.09615,0.09022,-0.0435,0.9620,0.1219 -7.250,-0.2449,0.09100,0.08508,-0.0463,0.9471,0.1239 -7.000,-0.2217,0.08682,0.08088,-0.0464,0.9331,0.1278 -6.750,-0.2041,0.08358,0.07756,-0.0518,0.9150,0.1353 -6.250,-0.1720,0.07685,0.07074,-0.0572,0.8846,0.1478 -6.000,-0.1584,0.07393,0.06768,-0.0632,0.8698,0.1575 -5.750,-0.1414,0.07080,0.06454,-0.0623,0.8587,0.1632 -5.250,-0.1085,0.06579,0.05923,-0.0680,0.8354,0.1878 -5.000,-0.0928,0.06259,0.05602,-0.0676,0.8258,0.1951 -4.750,-0.0759,0.06011,0.05345,-0.0687,0.8161,0.2112 -4.250,-0.0013,0.05118,0.04333,-0.0804,0.7988,0.1035 -4.000,0.0280,0.04812,0.03970,-0.0823,0.7906,0.0908 -3.750,0.0506,0.04570,0.03717,-0.0826,0.7827,0.0883 -3.500,0.0758,0.04347,0.03466,-0.0832,0.7751,0.0854 -3.250,0.1024,0.04137,0.03219,-0.0838,0.7672,0.0827 -3.000,0.1310,0.03940,0.02973,-0.0841,0.7614,0.0807 -2.750,0.1562,0.03807,0.02818,-0.0844,0.7533,0.0816 -2.500,0.1832,0.03675,0.02659,-0.0845,0.7472,0.0829 -2.250,0.2105,0.03556,0.02510,-0.0847,0.7405,0.0834 -2.000,0.2381,0.03443,0.02367,-0.0847,0.7336,0.0830 -1.750,0.2670,0.03334,0.02226,-0.0846,0.7286,0.0830 -1.500,0.2937,0.03261,0.02132,-0.0846,0.7215,0.0834 -1.250,0.3214,0.03191,0.02039,-0.0845,0.7155,0.0848 -1.000,0.3502,0.03127,0.01950,-0.0842,0.7108,0.0880 -0.750,0.3759,0.03102,0.01907,-0.0841,0.7031,0.0906 -0.500,0.4036,0.03052,0.01839,-0.0836,0.6976,0.0924 -0.250,0.4312,0.03006,0.01786,-0.0833,0.6919,0.0948 0.000,0.4567,0.02987,0.01762,-0.0829,0.6844,0.0983 0.250,0.4845,0.02951,0.01710,-0.0822,0.6789,0.1050 0.500,0.5074,0.02944,0.01707,-0.0817,0.6698,0.1112 0.750,0.5342,0.02910,0.01662,-0.0809,0.6635,0.1194 1.000,0.5573,0.02912,0.01669,-0.0804,0.6547,0.1327 1.250,0.5840,0.02881,0.01643,-0.0799,0.6483,0.1568 1.500,0.6115,0.02668,0.01653,-0.0798,0.6408,1.0000 1.750,0.6370,0.02701,0.01649,-0.0790,0.6336,1.0000 2.000,0.6615,0.02741,0.01665,-0.0784,0.6264,1.0000 2.250,0.6854,0.02782,0.01690,-0.0777,0.6184,1.0000 2.500,0.7105,0.02812,0.01704,-0.0770,0.6113,1.0000 3.000,0.7582,0.02879,0.01751,-0.0755,0.5938,1.0000 3.250,0.7841,0.02878,0.01740,-0.0746,0.5846,1.0000 3.500,0.8066,0.02901,0.01756,-0.0736,0.5727,1.0000 3.750,0.8325,0.02884,0.01727,-0.0725,0.5617,1.0000 4.000,0.8595,0.02854,0.01685,-0.0714,0.5506,1.0000 4.250,0.8814,0.02875,0.01703,-0.0703,0.5372,1.0000 4.500,0.9047,0.02891,0.01716,-0.0693,0.5254,1.0000 4.750,0.9322,0.02876,0.01692,-0.0685,0.5162,1.0000 5.000,0.9521,0.02928,0.01749,-0.0675,0.5031,1.0000 5.250,0.9735,0.02966,0.01788,-0.0665,0.4907,1.0000 5.500,0.9975,0.02981,0.01801,-0.0656,0.4794,1.0000 5.750,1.0190,0.03013,0.01836,-0.0645,0.4667,1.0000 6.000,1.0375,0.03069,0.01897,-0.0634,0.4522,1.0000 6.250,1.0561,0.03120,0.01955,-0.0622,0.4374,1.0000 6.500,1.0745,0.03170,0.02008,-0.0610,0.4225,1.0000 6.750,1.0928,0.03218,0.02058,-0.0597,0.4075,1.0000 7.000,1.1113,0.03265,0.02106,-0.0585,0.3928,1.0000 7.250,1.1299,0.03315,0.02151,-0.0572,0.3789,1.0000 7.500,1.1484,0.03369,0.02200,-0.0559,0.3661,1.0000 7.750,1.1680,0.03421,0.02243,-0.0547,0.3548,1.0000 8.000,1.1855,0.03500,0.02319,-0.0535,0.3438,1.0000 8.250,1.2015,0.03599,0.02419,-0.0523,0.3336,1.0000 8.750,1.2353,0.03798,0.02616,-0.0501,0.3163,1.0000 9.000,1.2582,0.03863,0.02674,-0.0494,0.3094,1.0000 9.250,1.2675,0.04025,0.02852,-0.0480,0.3019,1.0000 9.500,1.2863,0.04122,0.02951,-0.0471,0.2957,1.0000 9.750,1.3029,0.04243,0.03078,-0.0461,0.2904,1.0000 10.000,1.3107,0.04420,0.03276,-0.0447,0.2854,1.0000 10.250,1.3268,0.04553,0.03418,-0.0439,0.2811,1.0000 10.500,1.3540,0.04629,0.03496,-0.0437,0.2775,1.0000 10.750,1.3542,0.04871,0.03762,-0.0422,0.2739,1.0000 11.000,1.3521,0.05142,0.04057,-0.0408,0.2703,1.0000 11.250,1.3565,0.05374,0.04308,-0.0398,0.2669,1.0000 11.500,1.3732,0.05512,0.04457,-0.0392,0.2637,1.0000 11.750,1.3894,0.05662,0.04617,-0.0386,0.2607,1.0000 12.000,1.3420,0.06385,0.05374,-0.0380,0.2574,1.0000 12.250,1.2534,0.07811,0.06825,-0.0410,0.2525,1.0000 12.500,1.2176,0.08721,0.07748,-0.0435,0.2487,1.0000 12.750,1.2275,0.08951,0.07991,-0.0432,0.2467,1.0000