Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx66a175-il-500000 Airfoil,fx66a175-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,103.285 Max Cl/Cd alpha,8.25 Url,http://airfoiltools.com/polar/csv?polar=xf-fx66a175-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.1273,0.11012,0.10653,-0.0687,0.6253,0.0185 -12.500,-0.1262,0.10566,0.10208,-0.0706,0.6211,0.0185 -12.250,-0.1385,0.09836,0.09481,-0.0731,0.6193,0.0192 -12.000,-0.1356,0.09494,0.09135,-0.0742,0.6147,0.0195 -11.750,-0.1306,0.09213,0.08851,-0.0751,0.6104,0.0200 -11.500,-0.1299,0.08795,0.08433,-0.0767,0.6066,0.0202 -11.250,-0.1270,0.08463,0.08100,-0.0779,0.6026,0.0210 -11.000,-0.1310,0.07936,0.07572,-0.0800,0.5999,0.0214 -10.750,-0.1363,0.07387,0.07022,-0.0823,0.5975,0.0222 -10.500,-0.1580,0.06322,0.05961,-0.0874,0.5971,0.0215 -9.000,-0.3741,0.03454,0.02944,-0.1069,0.5943,0.0122 -8.750,-0.3752,0.03080,0.02537,-0.1055,0.5905,0.0116 -8.500,-0.3665,0.02808,0.02228,-0.1042,0.5866,0.0117 -8.250,-0.3530,0.02568,0.01956,-0.1030,0.5829,0.0116 -8.000,-0.3351,0.02387,0.01752,-0.1022,0.5789,0.0119 -7.750,-0.3146,0.02261,0.01605,-0.1015,0.5748,0.0123 -7.500,-0.2926,0.02170,0.01494,-0.1008,0.5710,0.0127 -7.250,-0.2721,0.02022,0.01324,-0.1000,0.5675,0.0134 -7.000,-0.2527,0.01855,0.01149,-0.0991,0.5639,0.0141 -6.750,-0.2307,0.01764,0.01053,-0.0984,0.5603,0.0147 -6.500,-0.2082,0.01692,0.00971,-0.0978,0.5569,0.0153 -6.250,-0.1850,0.01632,0.00901,-0.0972,0.5536,0.0161 -6.000,-0.1616,0.01565,0.00829,-0.0967,0.5501,0.0169 -5.750,-0.1364,0.01525,0.00783,-0.0964,0.5467,0.0181 -5.500,-0.1143,0.01441,0.00686,-0.0958,0.5436,0.0196 -5.250,-0.0904,0.01384,0.00618,-0.0954,0.5406,0.0215 -5.000,-0.0646,0.01343,0.00571,-0.0952,0.5378,0.0238 -4.750,-0.0385,0.01303,0.00523,-0.0950,0.5349,0.0273 -4.500,-0.0135,0.01243,0.00466,-0.0947,0.5320,0.0471 -4.250,0.0074,0.01117,0.00400,-0.0945,0.5295,0.1943 -4.000,0.0287,0.01012,0.00362,-0.0942,0.5270,0.3877 -3.750,0.0568,0.01024,0.00376,-0.0942,0.5244,0.4366 -3.500,0.0855,0.01039,0.00385,-0.0943,0.5218,0.4571 -3.250,0.1139,0.01058,0.00398,-0.0943,0.5192,0.4720 -3.000,0.1422,0.01075,0.00410,-0.0943,0.5167,0.4826 -2.750,0.1704,0.01094,0.00420,-0.0942,0.5143,0.4928 -2.500,0.1988,0.01120,0.00436,-0.0943,0.5120,0.5021 -2.250,0.2269,0.01129,0.00446,-0.0943,0.5098,0.5089 -2.000,0.2552,0.01139,0.00453,-0.0943,0.5075,0.5152 -1.750,0.2837,0.01145,0.00449,-0.0945,0.5052,0.5184 -1.500,0.3120,0.01139,0.00442,-0.0947,0.5029,0.5210 -1.250,0.3403,0.01141,0.00441,-0.0948,0.5007,0.5237 -1.000,0.3688,0.01147,0.00440,-0.0950,0.4986,0.5262 -0.750,0.3974,0.01157,0.00441,-0.0953,0.4963,0.5282 -0.500,0.4256,0.01155,0.00438,-0.0955,0.4943,0.5301 -0.250,0.4540,0.01158,0.00437,-0.0957,0.4921,0.5320 0.000,0.4823,0.01158,0.00434,-0.0959,0.4899,0.5336 0.250,0.5105,0.01156,0.00431,-0.0960,0.4878,0.5351 0.500,0.5387,0.01157,0.00430,-0.0962,0.4857,0.5366 0.750,0.5670,0.01164,0.00432,-0.0965,0.4836,0.5382 1.000,0.5953,0.01173,0.00439,-0.0967,0.4815,0.5399 1.250,0.6232,0.01175,0.00443,-0.0968,0.4796,0.5417 1.500,0.6512,0.01179,0.00448,-0.0970,0.4776,0.5435 1.750,0.6793,0.01184,0.00452,-0.0972,0.4757,0.5452 2.000,0.7074,0.01190,0.00457,-0.0974,0.4738,0.5470 2.250,0.7354,0.01193,0.00459,-0.0976,0.4720,0.5489 2.500,0.7634,0.01199,0.00466,-0.0978,0.4703,0.5509 2.750,0.7918,0.01215,0.00480,-0.0981,0.4684,0.5528 3.000,0.8194,0.01223,0.00492,-0.0983,0.4670,0.5547 3.250,0.8469,0.01229,0.00505,-0.0984,0.4654,0.5568 3.500,0.8745,0.01238,0.00517,-0.0985,0.4637,0.5590 3.750,0.9022,0.01248,0.00529,-0.0987,0.4621,0.5611 4.000,0.9298,0.01256,0.00541,-0.0988,0.4605,0.5634 4.250,0.9574,0.01264,0.00554,-0.0990,0.4590,0.5660 4.500,0.9851,0.01275,0.00568,-0.0992,0.4576,0.5688 4.750,1.0130,0.01288,0.00584,-0.0994,0.4562,0.5720 5.000,1.0412,0.01310,0.00607,-0.0998,0.4547,0.5749 5.250,1.0686,0.01329,0.00631,-0.1000,0.4534,0.5776 5.500,1.0950,0.01338,0.00652,-0.0999,0.4521,0.5806 5.750,1.1215,0.01351,0.00675,-0.0999,0.4507,0.5842 6.000,1.1482,0.01366,0.00699,-0.1000,0.4492,0.5882 6.250,1.1750,0.01380,0.00722,-0.1001,0.4477,0.5922 6.500,1.2016,0.01392,0.00743,-0.1001,0.4461,0.5964 6.750,1.2286,0.01404,0.00763,-0.1002,0.4444,0.6014 7.000,1.2561,0.01408,0.00764,-0.1003,0.4402,0.6068 7.250,1.2759,0.01375,0.00749,-0.0989,0.4328,0.6125 7.500,1.3001,0.01363,0.00732,-0.0983,0.4253,0.6199 7.750,1.3208,0.01344,0.00736,-0.0971,0.4188,0.6282 8.000,1.3424,0.01333,0.00730,-0.0961,0.4104,0.6389 8.250,1.3613,0.01318,0.00727,-0.0945,0.3955,0.6532 8.500,1.3577,0.01389,0.00764,-0.0892,0.3157,0.6713 8.750,1.3309,0.01578,0.00916,-0.0806,0.2367,0.6978 9.000,1.2956,0.01773,0.01115,-0.0712,0.1770,0.8165 9.250,1.2693,0.02071,0.01404,-0.0661,0.1195,1.0000 9.500,1.2475,0.02383,0.01707,-0.0625,0.0891,1.0000 9.750,1.2158,0.02877,0.02189,-0.0602,0.0528,1.0000 10.000,1.1913,0.03360,0.02665,-0.0589,0.0255,1.0000 10.250,1.1744,0.03777,0.03083,-0.0579,0.0139,1.0000 10.500,1.1687,0.04091,0.03404,-0.0571,0.0115,1.0000 10.750,1.1658,0.04377,0.03699,-0.0565,0.0098,1.0000 11.000,1.1634,0.04661,0.03989,-0.0560,0.0091,1.0000 11.250,1.1592,0.04968,0.04304,-0.0555,0.0085,1.0000 11.500,1.1523,0.05313,0.04659,-0.0551,0.0079,1.0000 11.750,1.1494,0.05629,0.04983,-0.0548,0.0077,1.0000 12.000,1.1518,0.05892,0.05253,-0.0547,0.0075,1.0000 12.250,1.1501,0.06209,0.05578,-0.0546,0.0074,1.0000 12.500,1.1499,0.06513,0.05889,-0.0546,0.0072,1.0000 12.750,1.1492,0.06831,0.06214,-0.0547,0.0068,1.0000 13.000,1.1491,0.07142,0.06532,-0.0548,0.0067,1.0000 13.250,1.1486,0.07465,0.06861,-0.0549,0.0064,1.0000 13.500,1.1480,0.07793,0.07195,-0.0552,0.0060,1.0000 13.750,1.1473,0.08127,0.07536,-0.0554,0.0060,1.0000 14.000,1.1477,0.08445,0.07861,-0.0557,0.0058,1.0000 14.250,1.1454,0.08804,0.08225,-0.0561,0.0056,1.0000 14.500,1.1505,0.09068,0.08496,-0.0564,0.0059,1.0000