Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe435-il-50000-n5 Airfoil,goe435-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,7.9224 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe435-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,-0.0748,0.11803,0.10923,-0.0895,0.9141,0.1721 -12.000,-0.0889,0.11367,0.10482,-0.0917,0.9045,0.1838 -11.750,-0.0553,0.11369,0.10483,-0.0918,0.8961,0.1873 -11.250,-0.0375,0.10991,0.10095,-0.0935,0.8789,0.2021 -11.000,-0.0172,0.10879,0.09976,-0.0939,0.8715,0.2078 -10.750,-0.0261,0.10571,0.09660,-0.0953,0.8637,0.2158 -10.500,0.0036,0.10602,0.09692,-0.0943,0.8544,0.2205 -10.250,0.0051,0.10391,0.09473,-0.0952,0.8476,0.2289 -10.000,0.0260,0.10353,0.09434,-0.0945,0.8391,0.2346 -9.750,0.0411,0.10282,0.09361,-0.0941,0.8302,0.2417 -9.500,0.0411,0.10067,0.09141,-0.0947,0.8235,0.2482 -9.250,0.0713,0.10081,0.09154,-0.0935,0.8155,0.2546 -9.000,0.0743,0.09907,0.08977,-0.0938,0.8071,0.2582 -8.750,0.0753,0.09666,0.08729,-0.0945,0.8005,0.2600 -8.500,0.0782,0.09399,0.08453,-0.0952,0.7952,0.2608 -8.250,0.0759,0.09185,0.08239,-0.0957,0.7857,0.2614 -8.000,0.0766,0.08930,0.07979,-0.0963,0.7782,0.2618 -7.750,0.0812,0.08666,0.07707,-0.0969,0.7723,0.2618 -7.500,0.0849,0.08446,0.07484,-0.0973,0.7649,0.2616 -7.250,0.0859,0.08234,0.07272,-0.0974,0.7561,0.2613 -7.000,0.0877,0.07973,0.07006,-0.0978,0.7496,0.2611 -6.750,0.0882,0.07667,0.06692,-0.0985,0.7446,0.2611 -6.500,0.0744,0.07412,0.06441,-0.0984,0.7355,0.2612 -6.250,0.0416,0.06964,0.05990,-0.0986,0.7272,0.2620 -6.000,0.0250,0.06605,0.05627,-0.0984,0.7214,0.2633 -5.750,0.0280,0.06373,0.05389,-0.0983,0.7172,0.2645 -5.500,-0.0229,0.06114,0.05136,-0.0955,0.7041,0.2660 -5.250,-0.0571,0.05606,0.04611,-0.0970,0.6969,0.2684 -5.000,-0.0606,0.05222,0.04205,-0.0990,0.6926,0.2707 -4.750,-0.0908,0.05117,0.04092,-0.0962,0.6809,0.2722 -4.500,-0.0873,0.04965,0.03924,-0.0964,0.6744,0.2743 -4.250,-0.0675,0.04791,0.03728,-0.0980,0.6703,0.2768 -4.000,-0.0382,0.04672,0.03597,-0.0995,0.6674,0.2792 -3.750,-0.0564,0.04800,0.03731,-0.0953,0.6557,0.2800 -3.500,-0.0386,0.04802,0.03736,-0.0946,0.6502,0.2819 -3.250,-0.0114,0.04767,0.03699,-0.0949,0.6467,0.2844 -3.000,0.0206,0.04706,0.03633,-0.0960,0.6441,0.2878 -2.750,-0.0068,0.04890,0.03821,-0.0916,0.6317,0.2893 -2.500,0.0178,0.04850,0.03771,-0.0924,0.6272,0.2941 -2.250,0.0477,0.04841,0.03770,-0.0925,0.6240,0.2978 -2.000,0.0828,0.04806,0.03738,-0.0933,0.6217,0.3033 -1.750,0.0566,0.05066,0.04004,-0.0899,0.6085,0.3055 -1.500,0.0864,0.05042,0.03979,-0.0906,0.6047,0.3127 -1.250,0.1198,0.05017,0.03958,-0.0909,0.6019,0.3200 -1.000,0.1140,0.05218,0.04159,-0.0899,0.5908,0.3270 -0.750,0.1385,0.05249,0.04198,-0.0895,0.5856,0.3348 -0.500,0.1743,0.05198,0.04142,-0.0903,0.5824,0.3487 -0.250,0.1765,0.05383,0.04330,-0.0893,0.5725,0.3575 0.000,0.1988,0.05433,0.04378,-0.0893,0.5662,0.3702 0.250,0.2341,0.05394,0.04328,-0.0901,0.5627,0.3867 0.500,0.2706,0.05339,0.04268,-0.0902,0.5602,0.4010 1.000,0.2866,0.05654,0.04590,-0.0883,0.5427,0.4182 1.250,0.3243,0.05594,0.04517,-0.0891,0.5400,0.4325 1.750,0.3379,0.05931,0.04866,-0.0868,0.5220,0.4466 2.000,0.3744,0.05872,0.04797,-0.0873,0.5191,0.4582 2.500,0.3857,0.06237,0.05175,-0.0850,0.5005,0.4709 2.750,0.4215,0.06183,0.05112,-0.0855,0.4975,0.4838 3.000,0.4532,0.06115,0.05051,-0.0841,0.4954,0.4931 3.500,0.4648,0.06534,0.05468,-0.0835,0.4753,0.5072 3.750,0.4507,0.06931,0.05873,-0.0828,0.4612,0.5104 4.000,0.4724,0.06960,0.05909,-0.0816,0.4563,0.5173 4.250,0.5036,0.06916,0.05863,-0.0813,0.4534,0.5266 4.500,0.5411,0.06830,0.05768,-0.0817,0.4514,0.5367 4.750,0.5145,0.07374,0.06324,-0.0810,0.4348,0.5382 5.000,0.5431,0.07330,0.06284,-0.0800,0.4322,0.5466 5.500,0.5514,0.07849,0.06804,-0.0800,0.4144,0.5585 5.750,0.5822,0.07791,0.06746,-0.0795,0.4122,0.5665 6.000,0.5568,0.08388,0.07353,-0.0796,0.3981,0.5682 6.250,0.5839,0.08378,0.07342,-0.0791,0.3953,0.5761 6.750,0.5896,0.08988,0.07953,-0.0800,0.3796,0.5859 7.000,0.6175,0.08976,0.07939,-0.0798,0.3772,0.5915 7.250,0.5921,0.09627,0.08600,-0.0804,0.3654,0.5930 7.500,0.6149,0.09678,0.08651,-0.0803,0.3621,0.5980 7.750,0.6429,0.09674,0.08643,-0.0802,0.3598,0.6037 8.000,0.6141,0.10410,0.09390,-0.0815,0.3485,0.6053 8.250,0.6360,0.10504,0.09479,-0.0818,0.3452,0.6116 8.500,0.6620,0.10517,0.09492,-0.0817,0.3430,0.6180 8.750,0.6339,0.11261,0.10247,-0.0831,0.3328,0.6196 9.000,0.6478,0.11437,0.10428,-0.0832,0.3291,0.6258 9.250,0.6703,0.11511,0.10500,-0.0832,0.3267,0.6341 9.500,0.6969,0.11529,0.10517,-0.0832,0.3249,0.6432 9.750,0.6603,0.12421,0.11423,-0.0855,0.3144,0.6441 10.000,0.6742,0.12601,0.11609,-0.0856,0.3113,0.6518