Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e168-il-100000 Airfoil,e168-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,38.3577 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e168-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.750,-0.7162,0.13545,0.13032,0.0138,1.0000,0.0731 -13.500,-0.8147,0.10241,0.09733,-0.0062,1.0000,0.0604 -13.250,-0.8431,0.09234,0.08722,-0.0121,1.0000,0.0594 -13.000,-0.8739,0.08294,0.07773,-0.0182,1.0000,0.0579 -12.750,-0.9093,0.07414,0.06875,-0.0244,1.0000,0.0568 -12.500,-0.9423,0.06677,0.06118,-0.0290,1.0000,0.0555 -12.250,-0.9701,0.06115,0.05530,-0.0316,1.0000,0.0550 -12.000,-0.9929,0.05670,0.05059,-0.0323,1.0000,0.0546 -11.750,-1.0084,0.05332,0.04697,-0.0314,1.0000,0.0550 -11.500,-1.0197,0.05049,0.04392,-0.0293,1.0000,0.0560 -11.250,-1.0263,0.04769,0.04081,-0.0273,1.0000,0.0573 -11.000,-1.0282,0.04478,0.03751,-0.0253,1.0000,0.0586 -10.750,-1.0257,0.04207,0.03435,-0.0233,1.0000,0.0601 -10.500,-1.0124,0.03885,0.03107,-0.0224,1.0000,0.0632 -10.250,-0.9988,0.03704,0.02919,-0.0213,1.0000,0.0674 -10.000,-0.9861,0.03501,0.02680,-0.0196,1.0000,0.0716 -9.750,-0.9677,0.03259,0.02448,-0.0188,1.0000,0.0770 -9.500,-0.9531,0.03102,0.02264,-0.0172,1.0000,0.0843 -9.250,-0.9360,0.02907,0.02086,-0.0161,1.0000,0.0935 -9.000,-0.9206,0.02739,0.01919,-0.0147,1.0000,0.1054 -8.750,-0.9056,0.02586,0.01768,-0.0131,1.0000,0.1212 -8.500,-0.8907,0.02446,0.01637,-0.0115,1.0000,0.1410 -8.250,-0.8751,0.02339,0.01529,-0.0099,1.0000,0.1658 -8.000,-0.8586,0.02254,0.01460,-0.0085,1.0000,0.1914 -7.750,-0.8408,0.02192,0.01403,-0.0070,1.0000,0.2173 -7.500,-0.8219,0.02143,0.01354,-0.0056,1.0000,0.2421 -7.250,-0.8019,0.02105,0.01312,-0.0043,1.0000,0.2653 -7.000,-0.7808,0.02065,0.01274,-0.0031,1.0000,0.2857 -6.750,-0.7589,0.02033,0.01243,-0.0020,1.0000,0.3047 -6.500,-0.7369,0.01999,0.01204,-0.0009,1.0000,0.3233 -6.250,-0.7149,0.01964,0.01162,0.0003,1.0000,0.3413 -6.000,-0.6924,0.01929,0.01125,0.0014,1.0000,0.3582 -5.750,-0.6694,0.01895,0.01094,0.0024,1.0000,0.3742 -5.500,-0.6465,0.01862,0.01060,0.0035,1.0000,0.3898 -5.250,-0.6237,0.01827,0.01026,0.0045,1.0000,0.4052 -5.000,-0.6009,0.01793,0.00993,0.0056,1.0000,0.4204 -4.750,-0.5783,0.01759,0.00960,0.0067,1.0000,0.4355 -4.500,-0.5557,0.01726,0.00927,0.0077,1.0000,0.4506 -4.250,-0.5335,0.01694,0.00897,0.0088,1.0000,0.4655 -4.000,-0.5116,0.01663,0.00869,0.0100,1.0000,0.4805 -3.750,-0.4903,0.01634,0.00843,0.0111,1.0000,0.4956 -3.500,-0.4699,0.01607,0.00821,0.0124,1.0000,0.5106 -3.250,-0.4510,0.01585,0.00804,0.0139,1.0000,0.5257 -3.000,-0.4340,0.01567,0.00792,0.0155,1.0000,0.5407 -2.750,-0.4189,0.01557,0.00786,0.0172,1.0000,0.5557 -2.500,-0.4053,0.01555,0.00791,0.0189,1.0000,0.5705 -2.250,-0.3480,0.01554,0.00803,0.0128,0.9827,0.5923 -2.000,-0.2954,0.01543,0.00796,0.0078,0.9631,0.6154 -1.750,-0.2419,0.01526,0.00790,0.0031,0.9455,0.6373 -1.500,-0.1910,0.01505,0.00776,-0.0009,0.9276,0.6599 -1.250,-0.1468,0.01485,0.00762,-0.0034,0.9064,0.6816 -1.000,-0.1086,0.01469,0.00752,-0.0045,0.8830,0.7020 -0.750,-0.0772,0.01459,0.00743,-0.0042,0.8581,0.7234 -0.500,-0.0491,0.01453,0.00738,-0.0032,0.8343,0.7438 -0.250,-0.0244,0.01451,0.00738,-0.0017,0.8094,0.7645 0.000,0.0000,0.01449,0.00733,0.0000,0.7876,0.7876 0.250,0.0243,0.01451,0.00738,0.0017,0.7645,0.8094 0.500,0.0490,0.01453,0.00738,0.0032,0.7438,0.8343 0.750,0.0772,0.01459,0.00743,0.0043,0.7234,0.8581 1.000,0.1086,0.01469,0.00752,0.0045,0.7020,0.8830 1.250,0.1468,0.01485,0.00763,0.0034,0.6816,0.9064 1.500,0.1910,0.01505,0.00776,0.0009,0.6599,0.9276 1.750,0.2419,0.01526,0.00790,-0.0031,0.6373,0.9455 2.000,0.2954,0.01543,0.00796,-0.0078,0.6154,0.9631 2.250,0.3478,0.01554,0.00803,-0.0128,0.5923,0.9827 2.500,0.4052,0.01554,0.00791,-0.0189,0.5705,1.0000 2.750,0.4189,0.01557,0.00786,-0.0172,0.5556,1.0000 3.000,0.4340,0.01567,0.00792,-0.0155,0.5408,1.0000 3.250,0.4510,0.01584,0.00804,-0.0139,0.5256,1.0000 3.500,0.4699,0.01607,0.00821,-0.0124,0.5106,1.0000 3.750,0.4903,0.01634,0.00843,-0.0111,0.4955,1.0000 4.000,0.5116,0.01663,0.00869,-0.0100,0.4805,1.0000 4.250,0.5335,0.01693,0.00897,-0.0088,0.4655,1.0000 4.500,0.5557,0.01726,0.00927,-0.0077,0.4505,1.0000 4.750,0.5783,0.01759,0.00960,-0.0067,0.4355,1.0000 5.000,0.6009,0.01793,0.00993,-0.0056,0.4204,1.0000 5.250,0.6237,0.01827,0.01026,-0.0045,0.4052,1.0000 5.500,0.6465,0.01862,0.01060,-0.0035,0.3898,1.0000 5.750,0.6694,0.01895,0.01094,-0.0024,0.3741,1.0000 6.000,0.6924,0.01929,0.01125,-0.0013,0.3582,1.0000 6.250,0.7149,0.01964,0.01162,-0.0003,0.3413,1.0000 6.500,0.7369,0.01999,0.01204,0.0009,0.3233,1.0000 6.750,0.7589,0.02033,0.01244,0.0020,0.3047,1.0000 7.000,0.7808,0.02065,0.01274,0.0031,0.2857,1.0000 7.250,0.8019,0.02105,0.01312,0.0043,0.2653,1.0000 7.500,0.8219,0.02143,0.01354,0.0057,0.2421,1.0000 7.750,0.8408,0.02192,0.01403,0.0070,0.2173,1.0000 8.000,0.8586,0.02254,0.01459,0.0085,0.1913,1.0000 8.250,0.8751,0.02339,0.01530,0.0100,0.1657,1.0000 8.500,0.8907,0.02446,0.01637,0.0115,0.1410,1.0000 8.750,0.9056,0.02586,0.01768,0.0131,0.1211,1.0000 9.000,0.9205,0.02739,0.01919,0.0147,0.1052,1.0000 9.250,0.9359,0.02906,0.02086,0.0161,0.0934,1.0000 9.500,0.9532,0.03103,0.02264,0.0172,0.0844,1.0000 9.750,0.9680,0.03261,0.02451,0.0188,0.0772,1.0000 10.000,0.9863,0.03501,0.02680,0.0196,0.0717,1.0000 10.250,0.9987,0.03700,0.02916,0.0212,0.0674,1.0000 10.500,1.0124,0.03884,0.03106,0.0224,0.0631,1.0000 10.750,1.0259,0.04209,0.03437,0.0233,0.0601,1.0000 11.000,1.0285,0.04478,0.03750,0.0253,0.0587,1.0000 11.250,1.0263,0.04771,0.04083,0.0273,0.0573,1.0000 11.500,1.0197,0.05053,0.04396,0.0293,0.0560,1.0000 11.750,1.0083,0.05338,0.04704,0.0313,0.0551,1.0000 12.000,0.9933,0.05671,0.05060,0.0322,0.0546,1.0000 12.250,0.9730,0.06087,0.05500,0.0317,0.0546,1.0000 12.500,0.9460,0.06633,0.06071,0.0292,0.0548,1.0000 12.750,0.9096,0.07415,0.06877,0.0243,0.0567,1.0000 13.000,0.8747,0.08297,0.07776,0.0181,0.0580,1.0000 13.250,0.8442,0.09233,0.08721,0.0120,0.0595,1.0000 13.500,0.8157,0.10240,0.09731,0.0060,0.0604,1.0000