Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe511-il-100000-n5 Airfoil,goe511-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,41.6527 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe511-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,0.0248,0.10905,0.10409,-0.0882,0.9161,0.0747 -9.500,0.0222,0.10601,0.10106,-0.0934,0.9103,0.0777 -9.250,0.0065,0.10371,0.09883,-0.0954,0.8988,0.0781 -9.000,0.0457,0.09966,0.09475,-0.0940,0.8957,0.0800 -8.750,0.0655,0.09631,0.09140,-0.0967,0.8917,0.0828 -8.500,0.0594,0.09429,0.08942,-0.0958,0.8787,0.0851 -8.250,0.0338,0.09230,0.08748,-0.0979,0.8640,0.0872 -7.750,-0.0036,0.08764,0.08284,-0.0966,0.8338,0.0876 -7.250,-0.0083,0.07638,0.07148,-0.0949,0.8098,0.0617 -7.000,-0.0005,0.07431,0.06942,-0.0929,0.7963,0.0609 -6.750,0.0048,0.07114,0.06619,-0.0926,0.7841,0.0601 -6.500,0.0112,0.06720,0.06214,-0.0936,0.7736,0.0600 -6.000,0.0033,0.05484,0.04923,-0.0945,0.7500,0.0548 -5.750,0.0212,0.05130,0.04549,-0.0949,0.7393,0.0544 -5.500,0.0341,0.04732,0.04124,-0.0946,0.7273,0.0540 -5.250,0.0482,0.04176,0.03518,-0.0948,0.7178,0.0538 -5.000,0.0506,0.03730,0.03008,-0.0920,0.7050,0.0543 -4.750,0.0659,0.03373,0.02575,-0.0905,0.6937,0.0548 -4.250,0.1055,0.03021,0.02144,-0.0877,0.6669,0.0553 -4.000,0.1325,0.02884,0.01973,-0.0875,0.6548,0.0557 -3.750,0.1542,0.02782,0.01847,-0.0862,0.6416,0.0563 -3.500,0.1771,0.02693,0.01734,-0.0851,0.6292,0.0569 -3.250,0.2058,0.02611,0.01624,-0.0851,0.6180,0.0584 -3.000,0.2268,0.02548,0.01538,-0.0836,0.6063,0.0598 -2.750,0.2543,0.02478,0.01436,-0.0833,0.5963,0.0612 -2.500,0.2794,0.02423,0.01357,-0.0825,0.5862,0.0620 -2.250,0.3064,0.02371,0.01296,-0.0822,0.5773,0.0630 -2.000,0.3303,0.02333,0.01251,-0.0813,0.5680,0.0643 -1.750,0.3579,0.02299,0.01201,-0.0811,0.5599,0.0659 -1.500,0.3796,0.02277,0.01170,-0.0798,0.5511,0.0680 -1.250,0.4077,0.02253,0.01133,-0.0797,0.5436,0.0709 -1.000,0.4290,0.02239,0.01118,-0.0784,0.5358,0.0739 -0.750,0.4534,0.02227,0.01095,-0.0776,0.5286,0.0771 -0.500,0.4833,0.02213,0.01071,-0.0779,0.5223,0.0812 -0.250,0.5035,0.02210,0.01069,-0.0764,0.5150,0.0877 0.000,0.5302,0.02201,0.01061,-0.0761,0.5080,0.0998 0.250,0.5659,0.02182,0.01065,-0.0778,0.5015,0.1432 0.500,0.5837,0.02204,0.01100,-0.0758,0.4945,0.2089 0.750,0.6052,0.02229,0.01115,-0.0746,0.4882,0.2398 1.250,0.6489,0.02276,0.01155,-0.0724,0.4767,0.2870 1.500,0.6690,0.02296,0.01175,-0.0711,0.4708,0.3089 1.750,0.6939,0.02311,0.01184,-0.0707,0.4658,0.3301 2.000,0.7177,0.02327,0.01194,-0.0701,0.4607,0.3445 2.250,0.7353,0.02348,0.01214,-0.0683,0.4550,0.3529 2.500,0.7561,0.02363,0.01225,-0.0671,0.4497,0.3610 2.750,0.7798,0.02377,0.01228,-0.0664,0.4452,0.3714 3.000,0.7978,0.02397,0.01250,-0.0648,0.4404,0.3839 3.250,0.8147,0.02418,0.01276,-0.0631,0.4355,0.4022 3.500,0.8355,0.02421,0.01292,-0.0621,0.4312,0.4522 3.750,1.0337,0.02495,0.01448,-0.0977,0.4224,1.0000 4.000,1.0456,0.02532,0.01483,-0.0949,0.4183,1.0000 4.250,1.0599,0.02567,0.01512,-0.0926,0.4147,1.0000 4.500,1.0763,0.02600,0.01536,-0.0907,0.4114,1.0000 4.750,1.0963,0.02632,0.01555,-0.0895,0.4084,1.0000 5.000,1.1088,0.02674,0.01596,-0.0870,0.4049,1.0000 5.250,1.1189,0.02722,0.01646,-0.0841,0.4013,1.0000 5.500,1.1319,0.02767,0.01690,-0.0818,0.3979,1.0000 5.750,1.1474,0.02810,0.01728,-0.0799,0.3950,1.0000 6.000,1.1658,0.02849,0.01761,-0.0785,0.3925,1.0000 6.250,1.1876,0.02887,0.01790,-0.0778,0.3902,1.0000 6.500,1.1992,0.02946,0.01852,-0.0754,0.3876,1.0000 6.750,1.2071,0.03015,0.01927,-0.0725,0.3848,1.0000 7.000,1.2169,0.03080,0.01997,-0.0699,0.3820,1.0000 7.250,1.2289,0.03140,0.02058,-0.0677,0.3792,1.0000 7.500,1.2443,0.03192,0.02109,-0.0661,0.3766,1.0000 7.750,1.2632,0.03236,0.02148,-0.0650,0.3743,1.0000 8.000,1.2862,0.03278,0.02184,-0.0646,0.3724,1.0000 8.250,1.2912,0.03370,0.02285,-0.0616,0.3700,1.0000 8.500,1.2908,0.03482,0.02411,-0.0580,0.3675,1.0000 8.750,1.2937,0.03591,0.02530,-0.0550,0.3650,1.0000 9.000,1.2990,0.03694,0.02639,-0.0523,0.3625,1.0000 9.250,1.3092,0.03774,0.02722,-0.0504,0.3598,1.0000 9.500,1.3274,0.03819,0.02765,-0.0494,0.3572,1.0000 9.750,1.3572,0.03820,0.02755,-0.0499,0.3545,1.0000 10.000,1.3375,0.04027,0.02982,-0.0446,0.3512,1.0000 10.250,1.3168,0.04260,0.03234,-0.0397,0.3472,1.0000 10.500,1.3143,0.04414,0.03395,-0.0370,0.3434,1.0000 10.750,1.3303,0.04463,0.03444,-0.0360,0.3403,1.0000 11.000,1.3576,0.04458,0.03431,-0.0361,0.3378,1.0000 11.250,1.3548,0.04638,0.03620,-0.0336,0.3351,1.0000 11.500,1.2680,0.05455,0.04481,-0.0262,0.3295,1.0000 11.750,1.2257,0.06058,0.05102,-0.0234,0.3243,1.0000 12.000,1.2485,0.06059,0.05101,-0.0230,0.3222,1.0000 12.250,1.2839,0.05941,0.04979,-0.0230,0.3207,1.0000 12.500,1.3285,0.05752,0.04782,-0.0235,0.3192,1.0000 12.750,1.1124,0.08434,0.07520,-0.0203,0.3013,1.0000