Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s8064-il-100000-n5 Airfoil,s8064-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,46.4317 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-s8064-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.750,-0.5239,0.09509,0.09012,-0.0475,1.0000,0.0206 -11.500,-0.5413,0.08517,0.08023,-0.0530,1.0000,0.0200 -11.250,-0.5718,0.07388,0.06890,-0.0612,1.0000,0.0194 -11.000,-0.6011,0.06633,0.06121,-0.0662,1.0000,0.0189 -10.750,-0.6297,0.06097,0.05570,-0.0679,1.0000,0.0187 -10.500,-0.6605,0.05714,0.05173,-0.0664,1.0000,0.0183 -10.250,-0.6919,0.05501,0.04947,-0.0617,1.0000,0.0181 -10.000,-0.7215,0.05381,0.04819,-0.0555,1.0000,0.0181 -9.750,-0.7495,0.05245,0.04669,-0.0488,1.0000,0.0180 -9.500,-0.7699,0.05049,0.04454,-0.0434,1.0000,0.0180 -9.250,-0.7712,0.04753,0.04127,-0.0418,0.9962,0.0182 -9.000,-0.7664,0.04414,0.03743,-0.0409,0.9915,0.0183 -8.750,-0.7567,0.04116,0.03405,-0.0400,0.9873,0.0186 -8.500,-0.7414,0.03837,0.03086,-0.0397,0.9842,0.0189 -8.250,-0.7271,0.03597,0.02810,-0.0385,0.9805,0.0195 -8.000,-0.7088,0.03381,0.02559,-0.0377,0.9772,0.0200 -7.750,-0.6868,0.03176,0.02323,-0.0374,0.9745,0.0208 -7.500,-0.6618,0.02992,0.02110,-0.0375,0.9723,0.0219 -7.250,-0.6421,0.02837,0.01938,-0.0366,0.9692,0.0235 -7.000,-0.6229,0.02739,0.01833,-0.0359,0.9655,0.0260 -6.750,-0.5995,0.02632,0.01706,-0.0356,0.9625,0.0298 -6.500,-0.5765,0.02505,0.01576,-0.0355,0.9597,0.0338 -6.250,-0.5554,0.02403,0.01466,-0.0347,0.9565,0.0412 -6.000,-0.5379,0.02325,0.01389,-0.0334,0.9522,0.0533 -5.750,-0.5151,0.02249,0.01313,-0.0331,0.9488,0.0715 -5.500,-0.4898,0.02168,0.01238,-0.0332,0.9459,0.0948 -5.250,-0.4686,0.02099,0.01178,-0.0326,0.9423,0.1220 -5.000,-0.4515,0.02036,0.01128,-0.0310,0.9376,0.1583 -4.750,-0.4288,0.01960,0.01077,-0.0308,0.9340,0.2179 -4.500,-0.4051,0.01873,0.01036,-0.0308,0.9312,0.3139 -4.250,-0.3929,0.01809,0.01016,-0.0281,0.9259,0.4120 -4.000,-0.3742,0.01764,0.01009,-0.0264,0.9215,0.5087 -3.750,-0.3477,0.01744,0.01013,-0.0259,0.9185,0.5889 -3.500,-0.3166,0.01751,0.01034,-0.0259,0.9163,0.6507 -3.250,-0.3034,0.01764,0.01046,-0.0227,0.9098,0.6886 -3.000,-0.2769,0.01780,0.01056,-0.0221,0.9059,0.7228 -2.750,-0.2460,0.01797,0.01062,-0.0223,0.9032,0.7511 -2.500,-0.2259,0.01815,0.01074,-0.0204,0.8980,0.7732 -2.250,-0.2037,0.01830,0.01082,-0.0190,0.8929,0.7945 -2.000,-0.1718,0.01849,0.01092,-0.0192,0.8899,0.8125 -1.750,-0.1380,0.01863,0.01097,-0.0200,0.8876,0.8277 -1.500,-0.1231,0.01874,0.01104,-0.0174,0.8801,0.8414 -1.250,-0.0931,0.01880,0.01102,-0.0177,0.8763,0.8534 -1.000,-0.0554,0.01888,0.01102,-0.0195,0.8739,0.8618 -0.750,-0.0351,0.01897,0.01108,-0.0181,0.8672,0.8723 -0.500,-0.0062,0.01900,0.01105,-0.0183,0.8626,0.8823 -0.250,0.0338,0.01905,0.01105,-0.0206,0.8600,0.8885 0.000,0.0564,0.01912,0.01110,-0.0198,0.8534,0.8983 0.250,0.0922,0.01918,0.01115,-0.0215,0.8488,0.9044 0.500,0.1262,0.01914,0.01109,-0.0227,0.8454,0.9123 0.750,0.1615,0.01923,0.01119,-0.0244,0.8401,0.9177 1.000,0.1910,0.01927,0.01124,-0.0250,0.8339,0.9255 1.250,0.2321,0.01920,0.01120,-0.0276,0.8306,0.9299 1.500,0.2635,0.01929,0.01133,-0.0287,0.8235,0.9364 1.750,0.2972,0.01922,0.01131,-0.0299,0.8179,0.9428 2.000,0.3416,0.01905,0.01121,-0.0330,0.8147,0.9458 2.250,0.3713,0.01911,0.01135,-0.0339,0.8048,0.9527 2.500,0.4109,0.01883,0.01116,-0.0359,0.8003,0.9572 2.750,0.4453,0.01877,0.01121,-0.0375,0.7897,0.9624 3.000,0.4789,0.01856,0.01110,-0.0386,0.7801,0.9686 3.250,0.5183,0.01808,0.01075,-0.0404,0.7718,0.9727 3.500,0.5533,0.01772,0.01051,-0.0416,0.7581,0.9781 3.750,0.5852,0.01736,0.01027,-0.0422,0.7410,0.9846 4.000,0.6209,0.01689,0.00993,-0.0433,0.7196,0.9898 4.250,0.6567,0.01638,0.00950,-0.0442,0.6929,0.9947 4.500,0.6938,0.01590,0.00900,-0.0452,0.6564,0.9987 5.000,0.7313,0.01575,0.00864,-0.0410,0.5609,1.0000 5.250,0.7420,0.01600,0.00864,-0.0376,0.4996,1.0000 5.500,0.7468,0.01649,0.00877,-0.0334,0.4299,1.0000 5.750,0.7482,0.01717,0.00906,-0.0288,0.3602,1.0000 6.000,0.7497,0.01797,0.00948,-0.0244,0.2945,1.0000 6.250,0.7530,0.01883,0.01001,-0.0205,0.2356,1.0000 6.500,0.7592,0.01970,0.01059,-0.0172,0.1877,1.0000 6.750,0.7681,0.02055,0.01123,-0.0143,0.1514,1.0000 7.000,0.7786,0.02138,0.01193,-0.0117,0.1262,1.0000 7.250,0.7896,0.02222,0.01269,-0.0092,0.1085,1.0000 7.500,0.8005,0.02304,0.01347,-0.0067,0.0950,1.0000 7.750,0.8118,0.02390,0.01436,-0.0043,0.0854,1.0000 8.000,0.8220,0.02490,0.01530,-0.0019,0.0777,1.0000 8.250,0.8359,0.02577,0.01627,0.0000,0.0696,1.0000 8.500,0.8479,0.02686,0.01737,0.0020,0.0634,1.0000 8.750,0.8623,0.02781,0.01841,0.0036,0.0565,1.0000 9.000,0.8756,0.02896,0.01959,0.0053,0.0506,1.0000 9.250,0.8894,0.02996,0.02070,0.0068,0.0446,1.0000 9.500,0.9027,0.03126,0.02207,0.0084,0.0400,1.0000 9.750,0.9175,0.03257,0.02352,0.0098,0.0361,1.0000 10.000,0.9298,0.03403,0.02500,0.0112,0.0334,1.0000 10.250,0.9461,0.03582,0.02699,0.0124,0.0308,1.0000 10.500,0.9595,0.03738,0.02877,0.0138,0.0282,1.0000 10.750,0.9696,0.03888,0.03037,0.0153,0.0264,1.0000 11.000,0.9794,0.04073,0.03229,0.0166,0.0252,1.0000 11.250,0.9896,0.04325,0.03510,0.0181,0.0242,1.0000 11.500,0.9958,0.04589,0.03810,0.0197,0.0235,1.0000 11.750,0.9966,0.04880,0.04135,0.0217,0.0229,1.0000 12.000,0.9926,0.05191,0.04480,0.0236,0.0224,1.0000 12.250,0.9850,0.05522,0.04841,0.0253,0.0221,1.0000 12.500,0.9735,0.05885,0.05234,0.0267,0.0219,1.0000 12.750,0.9594,0.06276,0.05651,0.0275,0.0216,1.0000 13.000,0.9420,0.06727,0.06128,0.0276,0.0215,1.0000 13.250,0.9226,0.07230,0.06656,0.0267,0.0215,1.0000 13.500,0.8991,0.07850,0.07300,0.0246,0.0218,1.0000 13.750,0.8719,0.08599,0.08069,0.0209,0.0218,1.0000 14.000,0.8424,0.09520,0.09009,0.0153,0.0223,1.0000 14.250,0.8096,0.10707,0.10209,0.0076,0.0229,1.0000