Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe458-il-500000-n5 Airfoil,goe458-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,115.291 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe458-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.1732,0.10012,0.09800,-0.0500,0.9850,0.0045 -9.750,-0.2934,0.11551,0.11329,-0.0342,1.0000,0.0056 -9.500,-0.2878,0.11187,0.10966,-0.0356,0.9993,0.0050 -9.250,-0.2745,0.10783,0.10562,-0.0390,0.9971,0.0044 -9.000,-0.2617,0.10387,0.10166,-0.0423,0.9931,0.0040 -8.750,-0.2484,0.09982,0.09762,-0.0458,0.9889,0.0045 -8.500,-0.2358,0.09611,0.09391,-0.0490,0.9838,0.0041 -8.250,-0.2224,0.09228,0.09008,-0.0524,0.9785,0.0045 -8.000,-0.2099,0.08859,0.08640,-0.0557,0.9723,0.0042 -7.750,-0.1899,0.08475,0.08256,-0.0611,0.9670,0.0057 -7.500,-0.1658,0.08188,0.07968,-0.0670,0.9594,0.0064 -7.250,-0.1446,0.07758,0.07537,-0.0730,0.9529,0.0064 -7.000,-0.1238,0.07347,0.07124,-0.0788,0.9435,0.0065 -6.750,-0.1023,0.06906,0.06680,-0.0848,0.9336,0.0064 -6.500,-0.0856,0.06417,0.06187,-0.0902,0.9223,0.0061 -6.250,-0.0687,0.05979,0.05745,-0.0955,0.9099,0.0058 -6.000,-0.0510,0.05584,0.05341,-0.1003,0.8980,0.0056 -5.750,-0.0324,0.05161,0.04911,-0.1051,0.8866,0.0055 -5.500,-0.0119,0.04746,0.04488,-0.1097,0.8762,0.0053 -5.250,0.0109,0.04298,0.04029,-0.1144,0.8666,0.0052 -5.000,0.0364,0.03795,0.03510,-0.1191,0.8578,0.0050 -4.750,0.0637,0.03255,0.02950,-0.1234,0.8494,0.0049 -4.500,0.0916,0.02550,0.02207,-0.1269,0.8413,0.0047 -4.250,0.1175,0.02054,0.01655,-0.1283,0.8342,0.0046 -4.000,0.1429,0.01723,0.01268,-0.1284,0.8266,0.0046 -3.750,0.1689,0.01469,0.00958,-0.1280,0.8196,0.0047 -3.500,0.1953,0.01270,0.00709,-0.1274,0.8116,0.0055 -3.250,0.2225,0.01226,0.00642,-0.1271,0.8037,0.0064 -3.000,0.2480,0.01115,0.00516,-0.1268,0.7955,0.0076 -2.750,0.2746,0.01111,0.00510,-0.1268,0.7869,0.0106 -2.500,0.3012,0.01044,0.00420,-0.1264,0.7784,0.0113 -2.250,0.3277,0.00983,0.00344,-0.1259,0.7685,0.0119 -2.000,0.3542,0.00941,0.00290,-0.1255,0.7582,0.0135 -1.750,0.3810,0.00937,0.00278,-0.1253,0.7472,0.0152 -1.500,0.4071,0.00890,0.00218,-0.1249,0.7363,0.0175 -1.250,0.4334,0.00871,0.00189,-0.1246,0.7244,0.0194 -0.750,0.4861,0.00853,0.00142,-0.1239,0.6985,0.0212 -0.500,0.5125,0.00852,0.00130,-0.1236,0.6860,0.0210 -0.250,0.5389,0.00852,0.00122,-0.1233,0.6743,0.0208 0.000,0.5650,0.00856,0.00117,-0.1229,0.6611,0.0206 0.250,0.5907,0.00863,0.00115,-0.1224,0.6456,0.0206 0.500,0.6164,0.00871,0.00116,-0.1220,0.6309,0.0208 0.750,0.6424,0.00878,0.00117,-0.1217,0.6182,0.0213 1.250,0.6941,0.00872,0.00123,-0.1211,0.5961,0.1184 1.500,0.7200,0.00873,0.00132,-0.1208,0.5862,0.1551 1.750,0.7456,0.00863,0.00147,-0.1205,0.5761,0.2469 2.000,0.7765,0.00725,0.00176,-0.1218,0.5648,1.0000 2.250,0.8020,0.00739,0.00184,-0.1214,0.5525,1.0000 2.500,0.8276,0.00753,0.00194,-0.1210,0.5412,1.0000 2.750,0.8532,0.00767,0.00204,-0.1206,0.5321,1.0000 3.000,0.8792,0.00779,0.00215,-0.1203,0.5231,1.0000 3.250,0.9049,0.00792,0.00228,-0.1200,0.5143,1.0000 3.500,0.9304,0.00807,0.00248,-0.1196,0.5045,1.0000 3.750,0.9525,0.00840,0.00265,-0.1186,0.4641,1.0000 4.000,0.9641,0.00956,0.00312,-0.1158,0.3283,1.0000 4.250,0.9752,0.01098,0.00385,-0.1132,0.2047,1.0000 4.500,0.9778,0.01322,0.00507,-0.1093,0.0054,1.0000 4.750,1.0001,0.01367,0.00563,-0.1082,0.0030,1.0000 5.000,1.0223,0.01410,0.00614,-0.1072,0.0027,1.0000 5.250,1.0431,0.01465,0.00680,-0.1059,0.0025,1.0000 5.500,1.0622,0.01536,0.00762,-0.1043,0.0024,1.0000 5.750,1.0799,0.01617,0.00852,-0.1025,0.0023,1.0000 6.000,1.0959,0.01708,0.00953,-0.1004,0.0023,1.0000 6.250,1.1099,0.01810,0.01065,-0.0980,0.0023,1.0000 6.500,1.1222,0.01923,0.01187,-0.0953,0.0023,1.0000 6.750,1.1324,0.02051,0.01336,-0.0923,0.0024,1.0000 7.000,1.1432,0.02174,0.01467,-0.0894,0.0024,1.0000 7.250,1.1558,0.02316,0.01617,-0.0869,0.0024,1.0000 7.500,1.1728,0.02483,0.01792,-0.0851,0.0025,1.0000 7.750,1.1956,0.02675,0.01994,-0.0844,0.0025,1.0000 8.000,1.2233,0.02924,0.02257,-0.0845,0.0026,1.0000 8.250,1.2489,0.03222,0.02574,-0.0842,0.0028,1.0000 9.000,1.3058,0.03804,0.03202,-0.0804,0.0034,1.0000 9.250,1.3197,0.04045,0.03468,-0.0783,0.0035,1.0000 9.500,1.3295,0.04312,0.03760,-0.0758,0.0036,1.0000 9.750,1.3340,0.04576,0.04048,-0.0728,0.0035,1.0000 10.000,1.3333,0.04835,0.04331,-0.0692,0.0035,1.0000 10.250,1.3280,0.05084,0.04607,-0.0652,0.0035,1.0000 10.500,1.3196,0.05343,0.04886,-0.0613,0.0035,1.0000 10.750,1.3100,0.05620,0.05184,-0.0577,0.0035,1.0000 11.000,1.2983,0.05913,0.05496,-0.0547,0.0035,1.0000 11.250,1.2851,0.06235,0.05837,-0.0522,0.0034,1.0000 11.500,1.2711,0.06590,0.06211,-0.0502,0.0034,1.0000 11.750,1.2558,0.06977,0.06616,-0.0490,0.0034,1.0000 12.000,1.2397,0.07405,0.07062,-0.0483,0.0034,1.0000 12.250,1.2237,0.07861,0.07535,-0.0485,0.0034,1.0000 12.500,1.2065,0.08373,0.08064,-0.0494,0.0034,1.0000 12.750,1.1897,0.08918,0.08624,-0.0510,0.0035,1.0000 13.000,1.1724,0.09521,0.09243,-0.0533,0.0035,1.0000 13.250,1.1549,0.10175,0.09912,-0.0565,0.0035,1.0000 13.500,1.1370,0.10909,0.10662,-0.0605,0.0035,1.0000