Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe499-il-50000-n5 Airfoil,goe499-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,44.9242 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe499-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.3593,0.11573,0.10945,-0.0266,1.0000,0.0997 -7.500,-0.3757,0.11581,0.10965,-0.0247,1.0000,0.1002 -7.250,-0.3892,0.11543,0.10938,-0.0239,1.0000,0.1006 -7.000,-0.3967,0.11436,0.10840,-0.0249,1.0000,0.1009 -6.750,-0.3831,0.10782,0.10185,-0.0202,1.0000,0.1030 -6.500,-0.3815,0.10505,0.09909,-0.0184,1.0000,0.1057 -6.250,-0.3838,0.10307,0.09717,-0.0176,1.0000,0.1101 -6.000,-0.3895,0.10209,0.09627,-0.0205,1.0000,0.1143 -5.750,-0.3873,0.10012,0.09438,-0.0262,1.0000,0.1155 -5.500,-0.3809,0.09556,0.08980,-0.0194,0.9991,0.1197 -5.250,-0.3621,0.09184,0.08601,-0.0237,0.9949,0.1238 -5.000,-0.3290,0.08798,0.08205,-0.0383,0.9888,0.1293 -4.750,-0.2983,0.08320,0.07718,-0.0475,0.9847,0.1299 -4.250,-0.2380,0.06983,0.06349,-0.0604,0.9779,0.0846 -4.000,-0.2059,0.06505,0.05857,-0.0667,0.9745,0.0802 -3.750,-0.1275,0.05431,0.04724,-0.0895,0.9728,0.0737 -3.500,-0.1076,0.05360,0.04653,-0.0891,0.9688,0.0790 -3.250,-0.0506,0.04815,0.04058,-0.1006,0.9670,0.0804 -3.000,0.0148,0.04186,0.03353,-0.1135,0.9663,0.0776 -2.750,0.0721,0.03734,0.02815,-0.1225,0.9654,0.0764 -2.500,0.1148,0.03472,0.02486,-0.1270,0.9627,0.0764 -2.250,0.1529,0.03303,0.02265,-0.1300,0.9591,0.0772 -2.000,0.1915,0.03177,0.02096,-0.1327,0.9555,0.0789 -1.750,0.2306,0.03082,0.01962,-0.1353,0.9512,0.0817 -1.500,0.2662,0.03007,0.01847,-0.1369,0.9443,0.0856 -1.250,0.3096,0.02956,0.01779,-0.1401,0.9387,0.0941 -1.000,0.3429,0.02923,0.01734,-0.1414,0.9299,0.1107 -0.750,0.3864,0.02872,0.01681,-0.1445,0.9243,0.1448 -0.500,0.4182,0.02844,0.01668,-0.1455,0.9159,0.2085 -0.250,0.4565,0.02838,0.01677,-0.1478,0.9102,0.2956 0.000,0.4845,0.02830,0.01689,-0.1482,0.9017,0.3613 0.250,0.5228,0.02807,0.01697,-0.1502,0.8966,0.4424 0.500,0.5482,0.02794,0.01710,-0.1498,0.8876,0.5307 0.750,0.5732,0.02702,0.01691,-0.1487,0.8804,0.8653 1.000,0.6040,0.02723,0.01685,-0.1494,0.8717,1.0000 1.250,0.6329,0.02752,0.01696,-0.1497,0.8624,1.0000 1.500,0.6708,0.02765,0.01695,-0.1514,0.8560,1.0000 1.750,0.6965,0.02796,0.01718,-0.1511,0.8453,1.0000 2.000,0.7255,0.02820,0.01736,-0.1513,0.8356,1.0000 2.250,0.7625,0.02822,0.01739,-0.1526,0.8285,1.0000 2.500,0.7878,0.02851,0.01769,-0.1522,0.8170,1.0000 2.750,0.8149,0.02874,0.01796,-0.1519,0.8059,1.0000 3.000,0.8474,0.02879,0.01811,-0.1525,0.7969,1.0000 3.250,0.8786,0.02884,0.01826,-0.1527,0.7870,1.0000 3.500,0.9039,0.02909,0.01862,-0.1521,0.7746,1.0000 3.750,0.9303,0.02930,0.01897,-0.1516,0.7625,1.0000 4.000,0.9584,0.02945,0.01933,-0.1513,0.7511,1.0000 4.250,0.9944,0.02928,0.01939,-0.1521,0.7428,1.0000 4.500,1.0190,0.02957,0.01989,-0.1513,0.7297,1.0000 4.750,1.0438,0.02987,0.02047,-0.1505,0.7168,1.0000 5.000,1.0692,0.03017,0.02105,-0.1498,0.7042,1.0000 5.250,1.0993,0.02892,0.02007,-0.1476,0.6776,1.0000 5.500,1.1292,0.02651,0.01767,-0.1433,0.6127,1.0000 5.750,1.1559,0.02573,0.01634,-0.1393,0.5038,1.0000 6.000,1.1534,0.02745,0.01703,-0.1335,0.3373,1.0000 6.250,1.1336,0.03185,0.01930,-0.1278,0.0922,1.0000 6.500,1.1421,0.03408,0.02128,-0.1253,0.0593,1.0000 6.750,1.1522,0.03594,0.02322,-0.1229,0.0518,1.0000 7.000,1.1609,0.03785,0.02528,-0.1204,0.0470,1.0000 7.250,1.1691,0.03974,0.02735,-0.1180,0.0427,1.0000 7.500,1.1743,0.04193,0.02968,-0.1155,0.0397,1.0000 7.750,1.1802,0.04415,0.03207,-0.1130,0.0383,1.0000 8.000,1.1903,0.04614,0.03438,-0.1107,0.0372,1.0000 8.250,1.2069,0.04801,0.03648,-0.1088,0.0359,1.0000 8.500,1.2339,0.04976,0.03842,-0.1075,0.0336,1.0000 8.750,1.2835,0.05239,0.04101,-0.1090,0.0303,1.0000 9.000,1.3423,0.05627,0.04522,-0.1119,0.0295,1.0000 9.250,1.3719,0.05999,0.04937,-0.1117,0.0293,1.0000 9.500,1.3905,0.06378,0.05360,-0.1104,0.0293,1.0000 9.750,1.4001,0.06747,0.05784,-0.1082,0.0292,1.0000 10.000,1.4025,0.07105,0.06186,-0.1055,0.0290,1.0000 10.250,1.3983,0.07451,0.06572,-0.1022,0.0288,1.0000 10.500,1.3900,0.07797,0.06955,-0.0989,0.0286,1.0000 10.750,1.3788,0.08161,0.07353,-0.0958,0.0285,1.0000 11.000,1.3649,0.08546,0.07770,-0.0932,0.0284,1.0000 11.250,1.3499,0.08964,0.08218,-0.0913,0.0285,1.0000 11.500,1.3334,0.09411,0.08693,-0.0900,0.0285,1.0000 11.750,1.3166,0.09892,0.09199,-0.0895,0.0286,1.0000 12.000,1.2984,0.10412,0.09743,-0.0898,0.0287,1.0000 12.250,1.2801,0.10973,0.10325,-0.0910,0.0288,1.0000