Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe323-il-50000-n5 Airfoil,goe323-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,29.3056 Max Cl/Cd alpha,7.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe323-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.3005,0.11487,0.10895,-0.0131,1.0000,0.1044 -9.000,-0.2946,0.11284,0.10685,-0.0179,0.9006,0.1091 -8.750,-0.3009,0.11240,0.10636,-0.0245,0.8692,0.1108 -8.500,-0.2858,0.10729,0.10120,-0.0236,0.8520,0.1124 -8.250,-0.2694,0.10322,0.09704,-0.0221,0.8373,0.1154 -8.000,-0.2603,0.10037,0.09412,-0.0227,0.8246,0.1189 -7.750,-0.2555,0.09797,0.09168,-0.0248,0.8133,0.1232 -7.500,-0.2612,0.09719,0.09087,-0.0344,0.8027,0.1269 -7.250,-0.2498,0.09297,0.08663,-0.0340,0.7951,0.1286 -7.000,-0.2334,0.08925,0.08289,-0.0311,0.7874,0.1325 -6.750,-0.2231,0.08664,0.08022,-0.0334,0.7802,0.1393 -6.500,-0.2153,0.08399,0.07751,-0.0412,0.7732,0.1453 -6.250,-0.2001,0.08060,0.07413,-0.0383,0.7666,0.1502 -5.750,-0.1728,0.07486,0.06827,-0.0449,0.7546,0.1642 -5.500,-0.1567,0.07214,0.06552,-0.0456,0.7490,0.1711 -5.250,-0.1409,0.06931,0.06256,-0.0493,0.7443,0.1805 -5.000,-0.1229,0.06672,0.05995,-0.0504,0.7384,0.1890 -4.750,-0.1054,0.06395,0.05712,-0.0524,0.7330,0.1993 -4.500,-0.0872,0.06149,0.05456,-0.0542,0.7284,0.2142 -4.250,-0.0693,0.05912,0.05217,-0.0549,0.7233,0.2317 -3.750,0.0176,0.04955,0.04114,-0.0688,0.7141,0.0938 -3.500,0.0414,0.04717,0.03858,-0.0693,0.7099,0.0901 -3.250,0.0691,0.04470,0.03574,-0.0708,0.7044,0.0852 -3.000,0.0982,0.04279,0.03331,-0.0716,0.6997,0.0815 -2.750,0.1244,0.04112,0.03133,-0.0718,0.6957,0.0813 -2.500,0.1515,0.03976,0.02963,-0.0723,0.6908,0.0819 -2.250,0.1783,0.03853,0.02808,-0.0726,0.6855,0.0822 -2.000,0.2049,0.03726,0.02655,-0.0725,0.6810,0.0819 -1.750,0.2317,0.03615,0.02517,-0.0724,0.6767,0.0817 -1.500,0.2583,0.03531,0.02414,-0.0726,0.6707,0.0816 -1.250,0.2854,0.03448,0.02305,-0.0723,0.6656,0.0818 -1.000,0.3126,0.03366,0.02200,-0.0718,0.6614,0.0832 -0.750,0.3378,0.03323,0.02159,-0.0721,0.6540,0.0858 -0.500,0.3647,0.03270,0.02092,-0.0716,0.6483,0.0884 -0.250,0.3914,0.03227,0.02033,-0.0710,0.6424,0.0900 0.000,0.4182,0.03202,0.01993,-0.0707,0.6349,0.0917 0.250,0.4459,0.03159,0.01931,-0.0698,0.6297,0.0942 0.500,0.4703,0.03155,0.01927,-0.0695,0.6219,0.0985 0.750,0.4955,0.03135,0.01904,-0.0689,0.6156,0.1045 1.000,0.5213,0.03118,0.01872,-0.0680,0.6101,0.1099 1.250,0.5444,0.03132,0.01894,-0.0678,0.6016,0.1172 1.500,0.5707,0.03106,0.01866,-0.0670,0.5962,0.1320 1.750,0.5939,0.03126,0.01904,-0.0668,0.5877,0.1573 2.000,0.6249,0.02914,0.01888,-0.0667,0.5812,1.0000 2.250,0.6492,0.02956,0.01899,-0.0659,0.5740,1.0000 2.500,0.6724,0.03004,0.01929,-0.0653,0.5655,1.0000 2.750,0.6999,0.02998,0.01899,-0.0642,0.5606,1.0000 3.000,0.7195,0.03088,0.01986,-0.0638,0.5494,1.0000 3.250,0.7470,0.03076,0.01955,-0.0628,0.5441,1.0000 3.500,0.7663,0.03165,0.02045,-0.0624,0.5327,1.0000 3.750,0.7941,0.03146,0.02010,-0.0613,0.5273,1.0000 4.000,0.8128,0.03237,0.02103,-0.0608,0.5155,1.0000 4.500,0.8591,0.03303,0.02161,-0.0593,0.4980,1.0000 4.750,0.8818,0.03339,0.02194,-0.0585,0.4890,1.0000 5.000,0.9054,0.03361,0.02215,-0.0576,0.4803,1.0000 5.250,0.9244,0.03437,0.02294,-0.0569,0.4695,1.0000 5.500,0.9517,0.03411,0.02261,-0.0560,0.4627,1.0000 5.750,0.9678,0.03517,0.02375,-0.0553,0.4509,1.0000 6.000,0.9931,0.03514,0.02369,-0.0544,0.4436,1.0000 6.250,1.0116,0.03587,0.02446,-0.0536,0.4332,1.0000 6.500,1.0284,0.03679,0.02544,-0.0528,0.4229,1.0000 6.750,1.0548,0.03661,0.02523,-0.0519,0.4161,1.0000 7.000,1.0676,0.03796,0.02667,-0.0511,0.4053,1.0000 7.250,1.0972,0.03744,0.02609,-0.0501,0.3996,1.0000 7.500,1.1061,0.03919,0.02797,-0.0494,0.3889,1.0000 7.750,1.1351,0.03878,0.02751,-0.0484,0.3832,1.0000 8.000,1.1426,0.04064,0.02948,-0.0476,0.3731,1.0000 8.250,1.1709,0.04034,0.02916,-0.0466,0.3674,1.0000 8.500,1.1746,0.04257,0.03152,-0.0457,0.3580,1.0000 8.750,1.2071,0.04196,0.03086,-0.0448,0.3531,1.0000 9.000,1.1988,0.04525,0.03432,-0.0438,0.3438,1.0000 9.250,1.2298,0.04483,0.03389,-0.0429,0.3383,1.0000 9.500,1.2166,0.04860,0.03782,-0.0420,0.3300,1.0000 9.750,1.2355,0.04931,0.03856,-0.0411,0.3241,1.0000 10.000,1.2510,0.05047,0.03977,-0.0403,0.3186,1.0000 10.250,1.2221,0.05669,0.04617,-0.0410,0.3098,1.0000 10.500,1.2661,0.05439,0.04389,-0.0391,0.3058,1.0000 10.750,1.1869,0.06766,0.05735,-0.0426,0.2941,1.0000 11.000,1.2325,0.06442,0.05416,-0.0402,0.2906,1.0000 11.250,1.1423,0.08097,0.07081,-0.0456,0.2771,1.0000 11.500,1.1910,0.07650,0.06643,-0.0425,0.2744,1.0000 12.000,1.1579,0.08806,0.07812,-0.0450,0.2581,1.0000 12.500,1.1258,0.10033,0.09052,-0.0482,0.2423,1.0000