Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe147-il-500000-n5 Airfoil,goe147-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,86.3419 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe147-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4926,0.08813,0.08608,0.0063,1.0000,0.0062 -8.000,-0.4919,0.08361,0.08159,0.0034,1.0000,0.0062 -7.500,-0.5003,0.02917,0.02600,-0.0520,1.0000,0.0060 -7.250,-0.4751,0.02230,0.01844,-0.0559,1.0000,0.0061 -7.000,-0.4491,0.02014,0.01600,-0.0568,1.0000,0.0064 -6.750,-0.4225,0.01899,0.01472,-0.0571,1.0000,0.0067 -6.500,-0.3956,0.01796,0.01354,-0.0573,1.0000,0.0071 -6.250,-0.3686,0.01683,0.01221,-0.0575,1.0000,0.0075 -6.000,-0.3414,0.01563,0.01079,-0.0576,1.0000,0.0079 -5.750,-0.3140,0.01454,0.00951,-0.0576,1.0000,0.0082 -5.500,-0.2857,0.01368,0.00847,-0.0577,0.9976,0.0086 -5.250,-0.2511,0.01260,0.00720,-0.0593,0.9785,0.0091 -5.000,-0.2156,0.01185,0.00633,-0.0609,0.9491,0.0099 -4.750,-0.1856,0.01146,0.00578,-0.0610,0.8995,0.0108 -4.500,-0.1612,0.01126,0.00533,-0.0598,0.8485,0.0119 -4.250,-0.1353,0.01105,0.00486,-0.0590,0.8047,0.0128 -4.000,-0.1084,0.01063,0.00417,-0.0585,0.7646,0.0144 -3.750,-0.0812,0.01042,0.00374,-0.0581,0.7229,0.0165 -3.500,-0.0537,0.01031,0.00341,-0.0578,0.6815,0.0192 -3.250,-0.0259,0.01010,0.00300,-0.0576,0.6477,0.0245 -3.000,0.0022,0.00991,0.00266,-0.0575,0.6239,0.0325 -2.750,0.0303,0.00966,0.00257,-0.0575,0.6055,0.0814 -2.500,0.0587,0.00978,0.00258,-0.0573,0.5891,0.0898 -2.250,0.0870,0.00994,0.00262,-0.0572,0.5733,0.0960 -2.000,0.1153,0.00997,0.00255,-0.0571,0.5588,0.0997 -1.750,0.1436,0.00996,0.00248,-0.0570,0.5434,0.1037 -1.500,0.1719,0.00992,0.00235,-0.0569,0.5286,0.1050 -1.250,0.2002,0.00992,0.00226,-0.0568,0.5126,0.1072 -1.000,0.2285,0.00992,0.00217,-0.0568,0.4984,0.1089 -0.750,0.2568,0.00987,0.00206,-0.0567,0.4843,0.1094 -0.500,0.2852,0.00985,0.00196,-0.0566,0.4679,0.1099 -0.250,0.3134,0.00985,0.00187,-0.0566,0.4497,0.1104 0.000,0.3417,0.00986,0.00180,-0.0565,0.4286,0.1108 0.250,0.3698,0.00993,0.00175,-0.0565,0.3998,0.1113 0.500,0.3977,0.01004,0.00171,-0.0565,0.3641,0.1122 0.750,0.4256,0.01015,0.00170,-0.0565,0.3372,0.1137 1.250,0.4816,0.01035,0.00175,-0.0564,0.3024,0.1176 1.500,0.5097,0.01043,0.00180,-0.0564,0.2898,0.1191 1.750,0.5378,0.01051,0.00185,-0.0564,0.2786,0.1208 2.000,0.5659,0.01061,0.00191,-0.0563,0.2689,0.1228 2.250,0.5939,0.01070,0.00198,-0.0563,0.2595,0.1249 2.500,0.6220,0.01078,0.00207,-0.0563,0.2522,0.1288 2.750,0.6499,0.01087,0.00217,-0.0563,0.2445,0.1362 3.000,0.6780,0.01090,0.00231,-0.0563,0.2379,0.1709 3.250,0.7059,0.01099,0.00246,-0.0563,0.2307,0.1997 3.500,0.7338,0.01108,0.00259,-0.0562,0.2244,0.2218 3.750,0.7616,0.01117,0.00274,-0.0562,0.2173,0.2451 4.000,0.7898,0.01084,0.00297,-0.0567,0.2107,0.5026 4.250,0.8106,0.00991,0.00310,-0.0550,0.2041,1.0000 4.500,0.8382,0.01011,0.00327,-0.0549,0.1968,1.0000 4.750,0.8658,0.01031,0.00346,-0.0548,0.1883,1.0000 5.000,0.8932,0.01053,0.00365,-0.0547,0.1798,1.0000 5.250,0.9205,0.01078,0.00387,-0.0547,0.1700,1.0000 5.500,0.9477,0.01102,0.00410,-0.0546,0.1603,1.0000 5.750,0.9748,0.01129,0.00436,-0.0545,0.1523,1.0000 6.250,1.0282,0.01192,0.00494,-0.0542,0.1354,1.0000 6.500,1.0547,0.01226,0.00526,-0.0541,0.1280,1.0000 6.750,1.0811,0.01259,0.00561,-0.0539,0.1212,1.0000 7.000,1.1073,0.01296,0.00597,-0.0537,0.1131,1.0000 7.250,1.1332,0.01336,0.00635,-0.0535,0.1039,1.0000 7.500,1.1592,0.01372,0.00671,-0.0533,0.0921,1.0000 7.750,1.1782,0.01542,0.00799,-0.0527,0.0235,1.0000 8.000,1.2025,0.01609,0.00869,-0.0523,0.0150,1.0000 8.250,1.2265,0.01676,0.00942,-0.0518,0.0116,1.0000 8.500,1.2508,0.01735,0.01010,-0.0514,0.0101,1.0000 8.750,1.2745,0.01799,0.01082,-0.0510,0.0088,1.0000 9.000,1.2970,0.01881,0.01172,-0.0504,0.0079,1.0000 9.250,1.3189,0.01969,0.01272,-0.0498,0.0072,1.0000 9.500,1.3409,0.02050,0.01363,-0.0492,0.0068,1.0000 9.750,1.3621,0.02134,0.01460,-0.0485,0.0062,1.0000 10.000,1.3827,0.02222,0.01556,-0.0478,0.0058,1.0000 10.250,1.4012,0.02330,0.01673,-0.0470,0.0053,1.0000 10.500,1.4176,0.02458,0.01815,-0.0459,0.0050,1.0000 10.750,1.4340,0.02575,0.01944,-0.0449,0.0048,1.0000 11.000,1.4483,0.02704,0.02088,-0.0437,0.0046,1.0000 11.250,1.4604,0.02845,0.02242,-0.0423,0.0044,1.0000 11.500,1.4697,0.02998,0.02408,-0.0407,0.0042,1.0000 11.750,1.4744,0.03161,0.02584,-0.0387,0.0041,1.0000 12.000,1.4737,0.03351,0.02787,-0.0366,0.0040,1.0000 12.250,1.4719,0.03594,0.03044,-0.0356,0.0039,1.0000 12.500,1.4682,0.03914,0.03381,-0.0359,0.0038,1.0000 12.750,1.4634,0.04313,0.03795,-0.0374,0.0038,1.0000 13.000,1.4563,0.04792,0.04290,-0.0398,0.0037,1.0000 13.250,1.4472,0.05328,0.04840,-0.0425,0.0037,1.0000 13.500,1.4348,0.05916,0.05443,-0.0453,0.0036,1.0000 13.750,1.4203,0.06533,0.06074,-0.0480,0.0036,1.0000 14.000,1.4044,0.07176,0.06731,-0.0508,0.0036,1.0000 14.250,1.3880,0.07829,0.07396,-0.0535,0.0036,1.0000 14.500,1.3718,0.08483,0.08062,-0.0561,0.0036,1.0000