Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe624-il-50000-n5 Airfoil,goe624-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,22.8101 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-goe624-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.2667,0.13335,0.12641,-0.0450,1.0000,0.1343 -10.750,-0.2770,0.13188,0.12504,-0.0436,1.0000,0.1344 -10.250,-0.2972,0.12254,0.11580,-0.0423,1.0000,0.0945 -10.000,-0.2882,0.11953,0.11278,-0.0427,0.9967,0.0921 -9.750,-0.2741,0.11515,0.10838,-0.0467,0.9899,0.0910 -9.500,-0.2612,0.11063,0.10384,-0.0510,0.9831,0.0896 -9.250,-0.2524,0.10588,0.09908,-0.0555,0.9751,0.0876 -9.000,-0.2677,0.09780,0.09098,-0.0647,0.9648,0.0830 -8.750,-0.2545,0.09347,0.08663,-0.0687,0.9574,0.0824 -8.500,-0.2484,0.08906,0.08221,-0.0727,0.9477,0.0819 -8.250,-0.2450,0.08351,0.07663,-0.0790,0.9387,0.0817 -8.000,-0.2482,0.07759,0.07065,-0.0848,0.9266,0.0817 -7.750,-0.2543,0.07182,0.06474,-0.0892,0.9148,0.0818 -7.500,-0.2544,0.06531,0.05794,-0.0945,0.9063,0.0822 -7.250,-0.2603,0.06070,0.05303,-0.0955,0.8939,0.0824 -7.000,-0.2536,0.05549,0.04731,-0.0979,0.8862,0.0828 -6.750,-0.2452,0.05242,0.04396,-0.0977,0.8758,0.0835 -6.500,-0.2189,0.04991,0.04126,-0.0994,0.8704,0.0848 -6.250,-0.2071,0.04829,0.03946,-0.0982,0.8595,0.0864 -6.000,-0.1818,0.04575,0.03655,-0.0994,0.8533,0.0893 -5.750,-0.1672,0.04346,0.03377,-0.0987,0.8432,0.0921 -5.500,-0.1409,0.04110,0.03096,-0.0993,0.8363,0.0948 -5.250,-0.1170,0.03981,0.02954,-0.0991,0.8279,0.0974 -5.000,-0.0922,0.03848,0.02796,-0.0989,0.8195,0.1018 -4.750,-0.0585,0.03676,0.02588,-0.0999,0.8144,0.1079 -4.500,-0.0415,0.03618,0.02524,-0.0984,0.8032,0.1125 -4.250,-0.0090,0.03485,0.02359,-0.0990,0.7975,0.1209 -4.000,0.0111,0.03439,0.02316,-0.0979,0.7876,0.1280 -3.750,0.0407,0.03354,0.02216,-0.0981,0.7808,0.1386 -3.500,0.0668,0.03300,0.02145,-0.0977,0.7731,0.1510 -3.000,0.1249,0.03182,0.02023,-0.0977,0.7596,0.1781 -2.750,0.1437,0.03169,0.02009,-0.0964,0.7487,0.1898 -2.500,0.1765,0.03103,0.01932,-0.0967,0.7429,0.2057 -2.250,0.1978,0.03091,0.01915,-0.0957,0.7332,0.2209 -2.000,0.2272,0.03036,0.01863,-0.0956,0.7266,0.2410 -1.750,0.2512,0.03005,0.01841,-0.0950,0.7183,0.2651 -1.500,0.2765,0.02964,0.01814,-0.0944,0.7104,0.3011 -1.250,0.3078,0.02879,0.01756,-0.0946,0.7056,0.3664 -1.000,0.3216,0.02868,0.01793,-0.0925,0.6946,0.4555 -0.750,0.3439,0.02759,0.01775,-0.0898,0.6895,0.6682 -0.500,0.4092,0.02739,0.01785,-0.0955,0.6805,0.9955 -0.250,0.4367,0.02743,0.01757,-0.0952,0.6736,1.0000 0.000,0.4564,0.02778,0.01769,-0.0940,0.6652,1.0000 0.250,0.4791,0.02802,0.01771,-0.0932,0.6573,1.0000 0.500,0.5109,0.02788,0.01730,-0.0933,0.6525,1.0000 0.750,0.5222,0.02871,0.01803,-0.0912,0.6415,1.0000 1.000,0.5528,0.02868,0.01778,-0.0913,0.6364,1.0000 1.250,0.5666,0.02948,0.01848,-0.0896,0.6267,1.0000 1.500,0.5936,0.02965,0.01848,-0.0893,0.6205,1.0000 1.750,0.6181,0.02998,0.01866,-0.0887,0.6141,1.0000 2.000,0.6337,0.03077,0.01938,-0.0873,0.6052,1.0000 2.250,0.6647,0.03079,0.01924,-0.0874,0.6006,1.0000 2.500,0.6755,0.03190,0.02032,-0.0855,0.5914,1.0000 2.750,0.7002,0.03226,0.02058,-0.0851,0.5853,1.0000 3.000,0.7338,0.03217,0.02034,-0.0855,0.5815,1.0000 3.250,0.7350,0.03388,0.02208,-0.0828,0.5711,1.0000 3.500,0.7637,0.03405,0.02216,-0.0827,0.5663,1.0000 3.750,0.7806,0.03493,0.02299,-0.0816,0.5598,1.0000 4.000,0.7914,0.03615,0.02421,-0.0798,0.5518,1.0000 4.250,0.8230,0.03616,0.02415,-0.0801,0.5479,1.0000 4.500,0.8214,0.03820,0.02622,-0.0773,0.5388,1.0000 4.750,0.8424,0.03882,0.02681,-0.0766,0.5332,1.0000 5.000,0.8777,0.03860,0.02653,-0.0771,0.5299,1.0000 5.250,0.8564,0.04184,0.02985,-0.0728,0.5188,1.0000 5.500,0.8862,0.04190,0.02987,-0.0727,0.5147,1.0000 5.750,0.9112,0.04229,0.03024,-0.0723,0.5102,1.0000 6.000,0.8919,0.04579,0.03382,-0.0689,0.4994,1.0000 6.250,0.9284,0.04523,0.03323,-0.0691,0.4964,1.0000 6.750,0.9315,0.04964,0.03771,-0.0657,0.4804,1.0000 7.000,0.9650,0.04917,0.03723,-0.0656,0.4772,1.0000 7.500,0.9543,0.05518,0.04335,-0.0624,0.4585,1.0000 8.000,0.9326,0.06313,0.05143,-0.0602,0.4366,1.0000 8.250,0.9509,0.06386,0.05219,-0.0594,0.4307,1.0000 8.500,0.9848,0.06279,0.05113,-0.0586,0.4280,1.0000 9.000,0.9884,0.06814,0.05659,-0.0571,0.4109,1.0000 9.250,1.0255,0.06661,0.05509,-0.0562,0.4090,1.0000 9.750,1.0237,0.07267,0.06127,-0.0549,0.3914,1.0000 10.250,1.0229,0.07886,0.06758,-0.0539,0.3743,1.0000 10.500,0.9924,0.08615,0.07498,-0.0544,0.3599,1.0000 10.750,1.0209,0.08548,0.07435,-0.0534,0.3575,1.0000 11.000,0.9913,0.09281,0.08177,-0.0541,0.3437,1.0000 11.250,1.0196,0.09209,0.08110,-0.0531,0.3412,1.0000 11.500,0.9889,0.09982,0.08891,-0.0542,0.3279,1.0000 11.750,1.0137,0.09967,0.08882,-0.0533,0.3254,1.0000 12.000,0.9827,0.10773,0.09694,-0.0549,0.3130,1.0000 12.250,1.0065,0.10766,0.09695,-0.0541,0.3101,1.0000