Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe564-il-500000 Airfoil,goe564-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,95.6667 Max Cl/Cd alpha,1.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe564-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.3711,0.08674,0.08453,-0.0349,1.0000,0.0284 -9.500,-0.3756,0.08239,0.08020,-0.0355,1.0000,0.0284 -8.250,-0.5620,0.06436,0.06224,-0.0378,1.0000,0.0228 -8.000,-0.5656,0.06194,0.05982,-0.0371,1.0000,0.0230 -7.750,-0.6169,0.02708,0.02320,-0.0523,0.9932,0.0210 -7.500,-0.5893,0.02494,0.02060,-0.0535,0.9898,0.0219 -7.250,-0.5649,0.02174,0.01706,-0.0548,0.9870,0.0235 -7.000,-0.5319,0.02127,0.01654,-0.0564,0.9852,0.0248 -6.750,-0.4996,0.02000,0.01504,-0.0579,0.9838,0.0262 -6.500,-0.4727,0.01897,0.01378,-0.0579,0.9797,0.0275 -6.250,-0.4433,0.01766,0.01217,-0.0586,0.9767,0.0289 -6.000,-0.4137,0.01621,0.01062,-0.0595,0.9746,0.0310 -5.750,-0.3805,0.01552,0.00983,-0.0609,0.9729,0.0326 -5.500,-0.3461,0.01480,0.00900,-0.0623,0.9716,0.0343 -5.250,-0.3173,0.01435,0.00845,-0.0625,0.9679,0.0358 -5.000,-0.2884,0.01352,0.00748,-0.0628,0.9642,0.0371 -4.750,-0.2572,0.01251,0.00640,-0.0636,0.9618,0.0392 -4.500,-0.2231,0.01203,0.00590,-0.0650,0.9601,0.0415 -4.250,-0.1883,0.01157,0.00539,-0.0664,0.9587,0.0434 -4.000,-0.1529,0.01114,0.00491,-0.0680,0.9577,0.0452 -3.750,-0.1289,0.01079,0.00452,-0.0671,0.9522,0.0469 -3.500,-0.0974,0.01030,0.00404,-0.0679,0.9493,0.0512 -3.250,-0.0626,0.00997,0.00371,-0.0693,0.9474,0.0557 -3.000,-0.0273,0.00960,0.00340,-0.0708,0.9458,0.0691 -2.750,0.0081,0.00932,0.00324,-0.0724,0.9442,0.0988 -2.500,0.0374,0.00920,0.00314,-0.0726,0.9400,0.1121 -2.250,0.0670,0.00903,0.00300,-0.0728,0.9353,0.1220 -2.000,0.1006,0.00880,0.00279,-0.0739,0.9320,0.1313 -1.750,0.1341,0.00858,0.00257,-0.0749,0.9269,0.1405 -1.500,0.1632,0.00831,0.00234,-0.0749,0.9178,0.1515 -1.250,0.1922,0.00807,0.00214,-0.0749,0.9085,0.1688 -1.000,0.2224,0.00776,0.00196,-0.0752,0.9007,0.2039 -0.750,0.2445,0.00710,0.00187,-0.0742,0.8901,0.3764 -0.500,0.2607,0.00607,0.00185,-0.0718,0.8792,0.6859 -0.250,0.2921,0.00549,0.00192,-0.0717,0.8683,0.9136 0.000,0.3537,0.00551,0.00188,-0.0785,0.8525,0.9666 0.250,0.3981,0.00558,0.00187,-0.0818,0.8369,0.9837 0.500,0.4436,0.00563,0.00184,-0.0855,0.8230,0.9932 0.750,0.4885,0.00567,0.00180,-0.0892,0.8074,1.0000 1.000,0.5108,0.00571,0.00177,-0.0879,0.7890,1.0000 1.250,0.5330,0.00577,0.00175,-0.0865,0.7681,1.0000 1.500,0.5541,0.00586,0.00173,-0.0849,0.7391,1.0000 1.750,0.5740,0.00600,0.00171,-0.0830,0.6999,1.0000 2.000,0.5923,0.00625,0.00174,-0.0808,0.6561,1.0000 2.250,0.6115,0.00652,0.00182,-0.0788,0.6224,1.0000 2.500,0.6323,0.00673,0.00192,-0.0772,0.5949,1.0000 2.750,0.6533,0.00695,0.00202,-0.0757,0.5659,1.0000 3.000,0.6737,0.00719,0.00214,-0.0741,0.5291,1.0000 3.250,0.6919,0.00754,0.00226,-0.0720,0.4737,1.0000 3.500,0.7082,0.00806,0.00246,-0.0697,0.4039,1.0000 3.750,0.7251,0.00863,0.00271,-0.0676,0.3360,1.0000 4.000,0.7432,0.00916,0.00297,-0.0657,0.2807,1.0000 4.250,0.7637,0.00955,0.00321,-0.0643,0.2514,1.0000 4.500,0.7855,0.00985,0.00344,-0.0631,0.2326,1.0000 4.750,0.8076,0.01014,0.00366,-0.0619,0.2175,1.0000 5.000,0.8299,0.01041,0.00390,-0.0608,0.2044,1.0000 5.250,0.8524,0.01069,0.00414,-0.0598,0.1922,1.0000 5.500,0.8749,0.01096,0.00437,-0.0587,0.1796,1.0000 5.750,0.8976,0.01123,0.00462,-0.0577,0.1659,1.0000 6.000,0.9203,0.01150,0.00486,-0.0567,0.1501,1.0000 6.250,0.9423,0.01184,0.00511,-0.0557,0.1259,1.0000 6.500,0.9625,0.01234,0.00544,-0.0543,0.0983,1.0000 6.750,0.9827,0.01284,0.00587,-0.0530,0.0817,1.0000 7.000,1.0019,0.01346,0.00637,-0.0514,0.0537,1.0000 7.250,1.0198,0.01422,0.00698,-0.0497,0.0370,1.0000 7.500,1.0376,0.01501,0.00778,-0.0478,0.0311,1.0000 7.750,1.0577,0.01555,0.00840,-0.0464,0.0285,1.0000 8.000,1.0757,0.01627,0.00917,-0.0447,0.0258,1.0000 8.250,1.0902,0.01729,0.01026,-0.0424,0.0238,1.0000 8.500,1.1092,0.01787,0.01092,-0.0409,0.0226,1.0000 8.750,1.1265,0.01858,0.01170,-0.0391,0.0214,1.0000 9.000,1.1432,0.01931,0.01248,-0.0373,0.0202,1.0000 9.250,1.1554,0.02042,0.01362,-0.0348,0.0189,1.0000 9.500,1.1664,0.02169,0.01500,-0.0322,0.0180,1.0000 9.750,1.1822,0.02233,0.01573,-0.0302,0.0173,1.0000 10.000,1.1950,0.02322,0.01671,-0.0278,0.0167,1.0000 10.250,1.2075,0.02410,0.01768,-0.0255,0.0160,1.0000 10.500,1.2190,0.02510,0.01876,-0.0231,0.0155,1.0000 10.750,1.2302,0.02605,0.01977,-0.0208,0.0150,1.0000 11.000,1.2393,0.02735,0.02115,-0.0183,0.0145,1.0000 11.250,1.2453,0.02948,0.02338,-0.0158,0.0140,1.0000 11.500,1.2520,0.03129,0.02536,-0.0133,0.0136,1.0000 11.750,1.2597,0.03237,0.02659,-0.0110,0.0133,1.0000 12.000,1.2652,0.03394,0.02833,-0.0085,0.0130,1.0000 12.250,1.2694,0.03555,0.03010,-0.0062,0.0126,1.0000 12.500,1.2718,0.03731,0.03201,-0.0040,0.0123,1.0000 12.750,1.2721,0.03942,0.03429,-0.0019,0.0121,1.0000 13.000,1.2717,0.04148,0.03649,-0.0001,0.0118,1.0000 13.250,1.2691,0.04391,0.03908,0.0015,0.0117,1.0000 13.500,1.2645,0.04663,0.04198,0.0029,0.0116,1.0000 13.750,1.2579,0.04965,0.04516,0.0037,0.0114,1.0000 14.000,1.2515,0.05277,0.04842,0.0041,0.0113,1.0000 14.250,1.2444,0.05615,0.05194,0.0039,0.0111,1.0000 14.500,1.2314,0.06074,0.05673,0.0031,0.0111,1.0000 14.750,1.2139,0.06634,0.06253,0.0014,0.0111,1.0000 15.000,1.1966,0.07233,0.06872,-0.0011,0.0111,1.0000 15.250,1.1826,0.07814,0.07466,-0.0041,0.0110,1.0000 15.500,1.1609,0.08598,0.08271,-0.0085,0.0111,1.0000 15.750,1.1381,0.09473,0.09166,-0.0139,0.0111,1.0000 16.000,1.1067,0.10621,0.10335,-0.0212,0.0113,1.0000 16.250,1.0177,0.13449,0.13206,-0.0392,0.0123,1.0000