Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe494-il-500000-n5 Airfoil,goe494-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,121.923 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe494-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.3316,0.09708,0.09484,-0.0347,0.9974,0.0054 -8.250,-0.3189,0.09294,0.09071,-0.0384,0.9942,0.0054 -8.000,-0.3059,0.08912,0.08690,-0.0420,0.9905,0.0054 -7.750,-0.2919,0.08466,0.08244,-0.0466,0.9867,0.0055 -7.500,-0.2806,0.08035,0.07816,-0.0507,0.9800,0.0057 -7.250,-0.2645,0.07605,0.07384,-0.0558,0.9741,0.0057 -7.000,-0.2439,0.07317,0.07095,-0.0605,0.9696,0.0062 -6.750,-0.2186,0.06962,0.06739,-0.0667,0.9666,0.0070 -6.500,-0.1950,0.06479,0.06254,-0.0740,0.9595,0.0073 -6.250,-0.1616,0.05852,0.05623,-0.0849,0.9550,0.0075 -6.000,-0.1276,0.05156,0.04921,-0.0966,0.9471,0.0078 -5.750,-0.0768,0.04108,0.03858,-0.1151,0.9407,0.0086 -5.500,-0.0166,0.02557,0.02252,-0.1369,0.9322,0.0098 -5.250,0.0263,0.01420,0.00972,-0.1459,0.9274,0.0141 -5.000,0.0535,0.01500,0.01061,-0.1457,0.9217,0.0150 -4.750,0.0817,0.01522,0.01080,-0.1458,0.9164,0.0168 -4.500,0.1109,0.01444,0.00976,-0.1463,0.9112,0.0204 -4.250,0.1390,0.01407,0.00916,-0.1464,0.9050,0.0226 -3.750,0.1950,0.01248,0.00721,-0.1472,0.8923,0.0261 -3.500,0.2228,0.01216,0.00679,-0.1473,0.8860,0.0281 -3.250,0.2503,0.01168,0.00616,-0.1473,0.8791,0.0296 -3.000,0.2782,0.01112,0.00544,-0.1474,0.8725,0.0303 -2.750,0.3056,0.01060,0.00479,-0.1473,0.8642,0.0306 -2.500,0.3330,0.01024,0.00431,-0.1472,0.8553,0.0314 -2.250,0.3603,0.00981,0.00377,-0.1470,0.8453,0.0314 -2.000,0.3876,0.00938,0.00325,-0.1469,0.8349,0.0310 -1.750,0.4148,0.00903,0.00281,-0.1467,0.8242,0.0306 -1.500,0.4420,0.00874,0.00243,-0.1465,0.8132,0.0303 -1.250,0.4692,0.00851,0.00212,-0.1463,0.8030,0.0300 -1.000,0.4966,0.00830,0.00187,-0.1462,0.7939,0.0298 -0.750,0.5239,0.00814,0.00165,-0.1460,0.7861,0.0296 -0.500,0.5513,0.00802,0.00148,-0.1459,0.7785,0.0295 -0.250,0.5787,0.00792,0.00134,-0.1458,0.7717,0.0294 0.000,0.6061,0.00785,0.00124,-0.1456,0.7651,0.0295 0.250,0.6335,0.00782,0.00116,-0.1455,0.7594,0.0298 0.500,0.6607,0.00780,0.00112,-0.1453,0.7519,0.0303 0.750,0.6876,0.00781,0.00109,-0.1450,0.7433,0.0314 1.000,0.7145,0.00784,0.00109,-0.1447,0.7343,0.0334 1.250,0.7415,0.00779,0.00114,-0.1445,0.7256,0.0713 1.500,0.7679,0.00755,0.00128,-0.1444,0.7122,0.2461 1.750,0.7934,0.00756,0.00141,-0.1439,0.6919,0.3127 2.000,0.8191,0.00755,0.00155,-0.1435,0.6725,0.3889 2.250,0.8446,0.00723,0.00177,-0.1432,0.6545,0.6122 2.750,0.8876,0.00728,0.00201,-0.1404,0.5366,1.0000 3.000,0.9077,0.00801,0.00235,-0.1390,0.4541,1.0000 3.250,0.9216,0.00955,0.00299,-0.1368,0.2698,1.0000 3.500,0.9410,0.01055,0.00350,-0.1356,0.1691,1.0000 3.750,0.9592,0.01172,0.00410,-0.1342,0.0537,1.0000 4.000,0.9826,0.01224,0.00456,-0.1334,0.0315,1.0000 4.250,1.0068,0.01264,0.00496,-0.1327,0.0210,1.0000 4.500,1.0309,0.01307,0.00537,-0.1320,0.0146,1.0000 4.750,1.0541,0.01364,0.00602,-0.1310,0.0115,1.0000 5.000,1.0775,0.01415,0.00662,-0.1302,0.0101,1.0000 5.250,1.1009,0.01462,0.00713,-0.1294,0.0085,1.0000 5.500,1.1210,0.01558,0.00816,-0.1280,0.0071,1.0000 5.750,1.1428,0.01627,0.00893,-0.1269,0.0067,1.0000 6.000,1.1636,0.01712,0.00988,-0.1256,0.0062,1.0000 6.250,1.1836,0.01809,0.01094,-0.1242,0.0057,1.0000 6.500,1.2036,0.01907,0.01205,-0.1228,0.0054,1.0000 6.750,1.2249,0.01978,0.01279,-0.1218,0.0049,1.0000 7.000,1.2432,0.02115,0.01424,-0.1203,0.0044,1.0000 7.250,1.2633,0.02236,0.01561,-0.1190,0.0041,1.0000 7.500,1.2831,0.02401,0.01745,-0.1175,0.0039,1.0000 7.750,1.3031,0.02603,0.01971,-0.1161,0.0036,1.0000 8.000,1.3226,0.02847,0.02244,-0.1146,0.0034,1.0000 8.250,1.3404,0.03136,0.02566,-0.1128,0.0032,1.0000 8.500,1.3546,0.03506,0.02976,-0.1106,0.0031,1.0000 8.750,1.3622,0.04057,0.03580,-0.1072,0.0031,1.0000 9.000,1.3616,0.04707,0.04284,-0.1029,0.0031,1.0000 9.250,1.3561,0.05281,0.04905,-0.0987,0.0032,1.0000 9.500,1.3468,0.05789,0.05448,-0.0946,0.0033,1.0000 9.750,1.3330,0.06231,0.05917,-0.0903,0.0033,1.0000 10.000,1.3144,0.06591,0.06297,-0.0858,0.0034,1.0000 10.250,1.2938,0.06988,0.06709,-0.0823,0.0034,1.0000 10.500,1.2727,0.07434,0.07173,-0.0802,0.0034,1.0000 10.750,1.2509,0.07945,0.07701,-0.0795,0.0034,1.0000 11.000,1.2297,0.08508,0.08280,-0.0803,0.0034,1.0000 11.250,1.2062,0.09199,0.08985,-0.0827,0.0035,1.0000