Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx66a175-il-100000-n5 Airfoil,fx66a175-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,34.2299 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-fx66a175-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.250,-0.2195,0.09538,0.09001,-0.0753,0.7312,0.0214 -11.000,-0.2255,0.08890,0.08350,-0.0787,0.7215,0.0212 -10.750,-0.2723,0.07264,0.06718,-0.0890,0.7229,0.0194 -9.750,-0.3429,0.05241,0.04601,-0.1032,0.6897,0.0185 -9.500,-0.3566,0.04949,0.04283,-0.1036,0.6826,0.0185 -9.250,-0.3626,0.04668,0.03979,-0.1033,0.6753,0.0186 -9.000,-0.3625,0.04374,0.03657,-0.1032,0.6691,0.0190 -8.750,-0.3556,0.04161,0.03429,-0.1030,0.6621,0.0197 -8.500,-0.3444,0.03991,0.03237,-0.1028,0.6563,0.0207 -8.250,-0.3321,0.03804,0.03024,-0.1023,0.6502,0.0217 -8.000,-0.3180,0.03604,0.02790,-0.1017,0.6446,0.0227 -7.750,-0.3011,0.03398,0.02546,-0.1011,0.6397,0.0231 -7.500,-0.2819,0.03207,0.02323,-0.1004,0.6338,0.0238 -7.250,-0.2607,0.03044,0.02130,-0.0996,0.6286,0.0245 -7.000,-0.2386,0.02905,0.01967,-0.0988,0.6235,0.0254 -6.750,-0.2174,0.02768,0.01819,-0.0980,0.6183,0.0267 -6.500,-0.1974,0.02661,0.01709,-0.0973,0.6139,0.0291 -6.250,-0.1763,0.02579,0.01619,-0.0966,0.6093,0.0319 -6.000,-0.1556,0.02495,0.01525,-0.0956,0.6045,0.0343 -5.750,-0.1356,0.02410,0.01426,-0.0946,0.6005,0.0369 -5.500,-0.1151,0.02333,0.01337,-0.0939,0.5969,0.0423 -5.250,-0.0940,0.02258,0.01257,-0.0934,0.5923,0.0510 -5.000,-0.0728,0.02170,0.01168,-0.0929,0.5884,0.0684 -4.750,-0.0541,0.02032,0.01068,-0.0927,0.5852,0.1488 -4.500,-0.0387,0.01925,0.01087,-0.0916,0.5821,0.3883 -4.250,-0.0121,0.01983,0.01128,-0.0911,0.5781,0.4567 -4.000,0.0137,0.02058,0.01184,-0.0902,0.5746,0.4908 -3.750,0.0396,0.02121,0.01237,-0.0890,0.5715,0.5122 -3.500,0.0661,0.02156,0.01255,-0.0883,0.5690,0.5271 -3.250,0.0918,0.02172,0.01259,-0.0879,0.5654,0.5372 -3.000,0.1182,0.02175,0.01245,-0.0877,0.5619,0.5446 -2.750,0.1449,0.02173,0.01226,-0.0877,0.5587,0.5502 -2.500,0.1721,0.02172,0.01208,-0.0876,0.5560,0.5548 -2.250,0.1995,0.02167,0.01183,-0.0878,0.5533,0.5591 -2.000,0.2257,0.02166,0.01170,-0.0879,0.5498,0.5632 -1.750,0.2522,0.02168,0.01165,-0.0878,0.5468,0.5664 -1.500,0.2792,0.02169,0.01154,-0.0879,0.5442,0.5697 -1.250,0.3069,0.02169,0.01137,-0.0881,0.5419,0.5728 -1.000,0.3352,0.02170,0.01118,-0.0885,0.5400,0.5761 -0.750,0.3606,0.02180,0.01128,-0.0884,0.5370,0.5786 -0.500,0.3866,0.02190,0.01135,-0.0884,0.5342,0.5810 -0.250,0.4131,0.02199,0.01139,-0.0885,0.5317,0.5834 0.000,0.4403,0.02207,0.01138,-0.0886,0.5294,0.5860 0.250,0.4680,0.02214,0.01133,-0.0889,0.5273,0.5890 0.500,0.4960,0.02222,0.01130,-0.0892,0.5254,0.5921 0.750,0.5198,0.02246,0.01162,-0.0889,0.5222,0.5945 1.000,0.5449,0.02267,0.01186,-0.0888,0.5195,0.5972 1.250,0.5708,0.02286,0.01204,-0.0888,0.5172,0.5999 1.500,0.5976,0.02305,0.01218,-0.0889,0.5152,0.6029 1.750,0.6251,0.02321,0.01228,-0.0892,0.5133,0.6063 2.000,0.6528,0.02333,0.01239,-0.0894,0.5117,0.6092 2.250,0.6759,0.02368,0.01282,-0.0890,0.5090,0.6123 2.500,0.6985,0.02407,0.01329,-0.0886,0.5060,0.6157 2.750,0.7229,0.02439,0.01366,-0.0885,0.5034,0.6195 3.000,0.7480,0.02464,0.01395,-0.0883,0.5012,0.6229 3.250,0.7742,0.02484,0.01417,-0.0883,0.4993,0.6266 3.500,0.8012,0.02505,0.01438,-0.0885,0.4978,0.6306 3.750,0.8278,0.02536,0.01471,-0.0886,0.4963,0.6347 4.000,0.8449,0.02612,0.01568,-0.0876,0.4933,0.6385 4.250,0.8650,0.02674,0.01643,-0.0870,0.4905,0.6431 4.500,0.8875,0.02723,0.01700,-0.0866,0.4881,0.6485 4.750,0.9118,0.02759,0.01746,-0.0865,0.4861,0.6534 5.000,0.9378,0.02788,0.01782,-0.0865,0.4845,0.6591 5.250,0.9646,0.02818,0.01817,-0.0867,0.4831,0.6654 5.500,0.9847,0.02883,0.01901,-0.0861,0.4812,0.6718 6.000,1.0045,0.03126,0.02189,-0.0827,0.4748,0.6872 6.250,1.0225,0.03200,0.02279,-0.0819,0.4727,0.6981 6.500,1.0440,0.03250,0.02345,-0.0814,0.4710,0.7123 6.750,1.0684,0.03278,0.02393,-0.0812,0.4695,0.7324 7.250,1.0431,0.03728,0.02926,-0.0735,0.4601,1.0000 7.500,1.0501,0.03869,0.03072,-0.0718,0.4575,1.0000 7.750,1.0706,0.03937,0.03145,-0.0714,0.4559,1.0000 8.000,1.0981,0.03965,0.03178,-0.0716,0.4547,1.0000 9.000,0.9215,0.06588,0.05820,-0.0636,0.4140,1.0000 9.250,0.9448,0.06632,0.05871,-0.0634,0.4126,1.0000 9.500,0.9692,0.06668,0.05916,-0.0631,0.4115,1.0000 10.000,0.9628,0.07296,0.06557,-0.0627,0.3986,1.0000 10.500,0.9621,0.07874,0.07154,-0.0625,0.3860,1.0000 10.750,0.9859,0.07903,0.07196,-0.0621,0.3845,1.0000 11.250,0.9856,0.08492,0.07804,-0.0621,0.3715,1.0000 11.500,1.0110,0.08491,0.07817,-0.0617,0.3700,1.0000 12.000,1.0182,0.08968,0.08317,-0.0616,0.3566,1.0000 12.500,1.0621,0.08791,0.08175,-0.0599,0.3411,1.0000 13.000,1.0783,0.08830,0.08231,-0.0588,0.2977,1.0000 13.500,1.0777,0.09129,0.08347,-0.0574,0.0947,1.0000 13.750,1.0552,0.09764,0.08934,-0.0585,0.0463,1.0000 14.000,1.0469,0.10219,0.09372,-0.0592,0.0299,1.0000