Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe404-il-50000-n5 Airfoil,goe404-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,31.5576 Max Cl/Cd alpha,7 Url,http://airfoiltools.com/polar/csv?polar=xf-goe404-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.2651,0.10374,0.09722,-0.0276,1.0000,0.1295 -7.500,-0.2776,0.10262,0.09624,-0.0248,1.0000,0.1300 -7.250,-0.2815,0.10075,0.09446,-0.0243,0.9963,0.1308 -7.000,-0.2607,0.09670,0.09040,-0.0298,0.9841,0.1321 -6.750,-0.2377,0.09243,0.08612,-0.0362,0.9709,0.1335 -6.250,-0.2003,0.07715,0.07045,-0.0599,0.9394,0.0899 -6.000,-0.1754,0.07307,0.06631,-0.0642,0.9264,0.0886 -5.750,-0.1502,0.06858,0.06171,-0.0694,0.9141,0.0871 -5.500,-0.1254,0.06393,0.05689,-0.0747,0.9017,0.0858 -5.250,-0.1060,0.05991,0.05268,-0.0780,0.8869,0.0853 -5.000,-0.0838,0.05631,0.04886,-0.0809,0.8736,0.0863 -4.750,-0.0564,0.05243,0.04467,-0.0843,0.8631,0.0879 -4.500,-0.0366,0.04908,0.04099,-0.0857,0.8486,0.0890 -4.250,-0.0134,0.04572,0.03720,-0.0870,0.8359,0.0898 -4.000,0.0152,0.04263,0.03370,-0.0884,0.8258,0.0913 -3.750,0.0378,0.04131,0.03232,-0.0880,0.8118,0.0939 -3.500,0.0637,0.03936,0.03005,-0.0882,0.7995,0.0977 -3.250,0.0937,0.03669,0.02673,-0.0888,0.7893,0.1016 -3.000,0.1179,0.03566,0.02569,-0.0883,0.7756,0.1051 -2.750,0.1460,0.03417,0.02380,-0.0881,0.7640,0.1113 -2.500,0.1748,0.03290,0.02235,-0.0880,0.7526,0.1172 -2.250,0.2013,0.03192,0.02105,-0.0875,0.7392,0.1249 -2.000,0.2298,0.03098,0.01998,-0.0872,0.7276,0.1324 -1.750,0.2585,0.03020,0.01881,-0.0868,0.7152,0.1417 -1.500,0.2844,0.02955,0.01820,-0.0862,0.7020,0.1489 -1.250,0.3150,0.02888,0.01715,-0.0859,0.6910,0.1574 -1.000,0.3410,0.02835,0.01663,-0.0853,0.6771,0.1636 -0.750,0.3683,0.02796,0.01607,-0.0847,0.6646,0.1708 -0.500,0.3982,0.02749,0.01542,-0.0843,0.6535,0.1774 -0.250,0.4244,0.02727,0.01515,-0.0838,0.6401,0.1838 0.000,0.4532,0.02704,0.01472,-0.0833,0.6293,0.1919 0.250,0.4793,0.02681,0.01450,-0.0827,0.6174,0.1989 0.500,0.5055,0.02673,0.01432,-0.0821,0.6064,0.2081 0.750,0.5321,0.02651,0.01412,-0.0815,0.5963,0.2193 1.000,0.5567,0.02649,0.01411,-0.0809,0.5856,0.2321 1.250,0.5835,0.02629,0.01396,-0.0804,0.5768,0.2532 1.500,0.6075,0.02611,0.01412,-0.0800,0.5671,0.3022 1.750,0.6454,0.02451,0.01410,-0.0809,0.5585,1.0000 2.000,0.6696,0.02498,0.01432,-0.0801,0.5498,1.0000 2.250,0.6946,0.02538,0.01450,-0.0794,0.5416,1.0000 2.500,0.7203,0.02577,0.01468,-0.0788,0.5346,1.0000 2.750,0.7430,0.02636,0.01518,-0.0781,0.5265,1.0000 3.000,0.7697,0.02672,0.01536,-0.0776,0.5206,1.0000 3.250,0.7919,0.02738,0.01595,-0.0768,0.5134,1.0000 3.500,0.8155,0.02793,0.01643,-0.0762,0.5065,1.0000 3.750,0.8430,0.02826,0.01660,-0.0758,0.5014,1.0000 4.000,0.8624,0.02915,0.01751,-0.0749,0.4943,1.0000 4.250,0.8855,0.02980,0.01813,-0.0742,0.4884,1.0000 4.500,0.9128,0.03018,0.01838,-0.0738,0.4836,1.0000 4.750,0.9307,0.03113,0.01938,-0.0728,0.4764,1.0000 5.000,0.9533,0.03171,0.01993,-0.0719,0.4695,1.0000 5.250,0.9816,0.03189,0.01997,-0.0715,0.4636,1.0000 5.500,0.9954,0.03295,0.02113,-0.0700,0.4545,1.0000 5.750,1.0242,0.03294,0.02098,-0.0695,0.4472,1.0000 6.000,1.0380,0.03389,0.02201,-0.0678,0.4375,1.0000 6.250,1.0644,0.03401,0.02202,-0.0671,0.4297,1.0000 6.500,1.0798,0.03493,0.02302,-0.0657,0.4215,1.0000 6.750,1.0996,0.03560,0.02370,-0.0646,0.4143,1.0000 7.000,1.1285,0.03576,0.02375,-0.0643,0.4086,1.0000 7.250,1.1338,0.03733,0.02554,-0.0621,0.4001,1.0000 7.500,1.1576,0.03773,0.02591,-0.0613,0.3934,1.0000 7.750,1.1720,0.03873,0.02699,-0.0598,0.3863,1.0000 8.000,1.1825,0.03991,0.02828,-0.0580,0.3783,1.0000 8.250,1.2139,0.03979,0.02806,-0.0578,0.3721,1.0000 8.500,1.2060,0.04205,0.03058,-0.0546,0.3630,1.0000 8.750,1.2289,0.04235,0.03085,-0.0537,0.3560,1.0000 9.000,1.2275,0.04416,0.03281,-0.0510,0.3480,1.0000 9.250,1.2327,0.04548,0.03422,-0.0488,0.3402,1.0000 9.500,1.2506,0.04605,0.03478,-0.0476,0.3334,1.0000 9.750,1.2275,0.04955,0.03848,-0.0444,0.3242,1.0000 10.000,1.2646,0.04861,0.03745,-0.0439,0.3181,1.0000 10.250,1.2110,0.05531,0.04443,-0.0413,0.3075,1.0000 10.500,1.2444,0.05435,0.04342,-0.0402,0.3019,1.0000 10.750,1.1777,0.06416,0.05348,-0.0403,0.2897,1.0000 11.000,1.2109,0.06289,0.05219,-0.0388,0.2855,1.0000 11.250,1.1336,0.07623,0.06573,-0.0418,0.2717,1.0000 11.500,1.1662,0.07464,0.06415,-0.0400,0.2690,1.0000 12.000,1.1079,0.09034,0.07997,-0.0438,0.2516,1.0000