Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe54-il-500000-n5 Airfoil,goe54-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,88.1176 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe54-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.5769,0.11907,0.11687,0.0461,1.0000,0.0122 -9.250,-0.5720,0.11533,0.11314,0.0445,1.0000,0.0123 -9.000,-0.5680,0.11124,0.10906,0.0425,1.0000,0.0124 -8.750,-0.5615,0.10823,0.10607,0.0412,1.0000,0.0127 -8.500,-0.5550,0.10512,0.10298,0.0398,1.0000,0.0129 -8.250,-0.5489,0.10185,0.09972,0.0381,1.0000,0.0131 -8.000,-0.5427,0.09862,0.09652,0.0363,1.0000,0.0133 -7.750,-0.5361,0.09544,0.09336,0.0344,1.0000,0.0140 -7.250,-0.5163,0.08822,0.08617,0.0276,1.0000,0.0157 -7.000,-0.5025,0.08451,0.08246,0.0236,1.0000,0.0160 -6.750,-0.4842,0.08019,0.07814,0.0178,1.0000,0.0175 -6.500,-0.4685,0.07657,0.07377,0.0137,0.7071,0.0175 -6.250,-0.4499,0.07255,0.06948,0.0092,0.6369,0.0175 -6.000,-0.4168,0.06581,0.06241,-0.0013,0.5811,0.0178 -5.750,-0.4028,0.06354,0.05995,-0.0014,0.5245,0.0181 -5.500,-0.3815,0.06071,0.05695,-0.0038,0.4940,0.0185 -5.250,-0.3571,0.05762,0.05371,-0.0067,0.4753,0.0192 -5.000,-0.3235,0.05352,0.04941,-0.0114,0.4636,0.0208 -4.750,-0.2876,0.04899,0.04458,-0.0157,0.4547,0.0210 -4.500,-0.2566,0.04513,0.04045,-0.0182,0.4461,0.0210 -4.250,-0.2341,0.04203,0.03727,-0.0194,0.4374,0.0212 -4.000,-0.2108,0.03981,0.03497,-0.0204,0.4283,0.0215 -3.750,-0.1848,0.03774,0.03278,-0.0214,0.4201,0.0219 -3.500,-0.1569,0.03568,0.03057,-0.0224,0.4122,0.0226 -3.250,-0.1199,0.03381,0.02831,-0.0228,0.4059,0.0247 -3.000,-0.0896,0.03162,0.02587,-0.0233,0.3992,0.0248 -2.750,-0.0601,0.02965,0.02364,-0.0237,0.3922,0.0248 -2.500,-0.0310,0.02786,0.02164,-0.0239,0.3855,0.0249 -2.250,-0.0045,0.02524,0.01894,-0.0249,0.3777,0.0252 -2.000,0.0225,0.02389,0.01751,-0.0254,0.3699,0.0257 -1.750,0.0507,0.02276,0.01625,-0.0257,0.3607,0.0264 -1.500,0.0799,0.02161,0.01493,-0.0258,0.3513,0.0273 -1.250,0.1116,0.02145,0.01443,-0.0250,0.3409,0.0294 -1.000,0.1412,0.02054,0.01327,-0.0249,0.3283,0.0295 -0.750,0.1702,0.01963,0.01214,-0.0249,0.3117,0.0295 -0.500,0.1992,0.01888,0.01117,-0.0249,0.2925,0.0296 -0.250,0.2280,0.01712,0.00925,-0.0253,0.2761,0.0301 0.250,0.2852,0.01549,0.00742,-0.0254,0.2569,0.0280 0.500,0.3142,0.01485,0.00663,-0.0252,0.2498,0.0274 0.750,0.3431,0.01430,0.00598,-0.0251,0.2446,0.0273 1.000,0.3717,0.01386,0.00544,-0.0249,0.2388,0.0275 1.250,0.4003,0.01351,0.00500,-0.0248,0.2337,0.0277 1.500,0.4287,0.01323,0.00467,-0.0246,0.2296,0.0284 1.750,0.4572,0.01302,0.00440,-0.0244,0.2252,0.0290 2.000,0.4855,0.01272,0.00408,-0.0243,0.2208,0.0289 2.250,0.5138,0.01249,0.00382,-0.0242,0.2170,0.0290 2.500,0.5421,0.01231,0.00363,-0.0240,0.2141,0.0292 2.750,0.5705,0.01218,0.00351,-0.0239,0.2118,0.0295 3.000,0.5990,0.01194,0.00330,-0.0239,0.2091,0.0301 3.250,0.6273,0.01185,0.00324,-0.0239,0.2061,0.0307 3.500,0.6556,0.01185,0.00325,-0.0239,0.2030,0.0319 3.750,0.6838,0.01189,0.00329,-0.0238,0.1998,0.0334 4.000,0.7121,0.01189,0.00331,-0.0237,0.1973,0.0339 4.250,0.7405,0.01188,0.00334,-0.0237,0.1946,0.0346 4.500,0.7686,0.01192,0.00341,-0.0236,0.1912,0.0353 4.750,0.7968,0.01196,0.00345,-0.0235,0.1876,0.0368 5.000,0.8248,0.01209,0.00357,-0.0235,0.1838,0.0392 5.250,0.8528,0.01218,0.00370,-0.0234,0.1807,0.0418 5.500,0.8807,0.01227,0.00381,-0.0233,0.1764,0.0449 5.750,0.9086,0.01241,0.00395,-0.0231,0.1717,0.0505 6.000,0.9322,0.01092,0.00422,-0.0226,0.1664,1.0000 6.250,0.9598,0.01113,0.00437,-0.0225,0.1574,1.0000 6.500,0.9873,0.01136,0.00457,-0.0224,0.1490,1.0000 6.750,1.0147,0.01163,0.00481,-0.0223,0.1420,1.0000 7.000,1.0421,0.01188,0.00506,-0.0222,0.1368,1.0000 7.250,1.0693,0.01217,0.00535,-0.0221,0.1322,1.0000 7.500,1.0964,0.01247,0.00566,-0.0220,0.1284,1.0000 7.750,1.1235,0.01275,0.00597,-0.0219,0.1250,1.0000 8.000,1.1503,0.01307,0.00631,-0.0218,0.1207,1.0000 8.250,1.1770,0.01343,0.00668,-0.0217,0.1167,1.0000 8.500,1.2037,0.01375,0.00706,-0.0216,0.1135,1.0000 8.750,1.2304,0.01405,0.00742,-0.0214,0.1100,1.0000 9.000,1.2567,0.01442,0.00783,-0.0213,0.1060,1.0000 9.250,1.2827,0.01487,0.00831,-0.0212,0.1012,1.0000 9.500,1.3091,0.01517,0.00869,-0.0210,0.0968,1.0000 9.750,1.3347,0.01565,0.00917,-0.0209,0.0859,1.0000 10.250,1.3815,0.01755,0.01088,-0.0207,0.0521,1.0000 10.500,1.4054,0.01831,0.01170,-0.0205,0.0477,1.0000 10.750,1.4295,0.01896,0.01242,-0.0203,0.0447,1.0000 11.000,1.4526,0.01977,0.01330,-0.0200,0.0416,1.0000 11.250,1.4756,0.02056,0.01417,-0.0198,0.0392,1.0000 11.500,1.4988,0.02125,0.01496,-0.0195,0.0372,1.0000 11.750,1.5208,0.02210,0.01589,-0.0193,0.0347,1.0000 12.000,1.5416,0.02313,0.01698,-0.0190,0.0324,1.0000 12.250,1.5633,0.02391,0.01787,-0.0187,0.0306,1.0000 12.500,1.5835,0.02488,0.01893,-0.0184,0.0284,1.0000 12.750,1.6020,0.02607,0.02020,-0.0180,0.0263,1.0000 13.000,1.6208,0.02711,0.02135,-0.0176,0.0240,1.0000 13.250,1.6364,0.02853,0.02283,-0.0173,0.0216,1.0000 13.500,1.6513,0.02993,0.02435,-0.0169,0.0195,1.0000 13.750,1.6623,0.03174,0.02626,-0.0165,0.0177,1.0000 14.000,1.6699,0.03384,0.02850,-0.0163,0.0164,1.0000 14.250,1.6694,0.03662,0.03144,-0.0162,0.0155,1.0000 14.500,1.6492,0.04487,0.03999,-0.0240,0.0155,1.0000 14.750,1.6139,0.05606,0.05144,-0.0325,0.0159,1.0000 15.000,1.5709,0.06649,0.06206,-0.0381,0.0166,1.0000 15.250,1.5291,0.07654,0.07226,-0.0430,0.0172,1.0000 15.500,1.4942,0.08558,0.08145,-0.0472,0.0176,1.0000