Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca001064-il-50000-n5 Airfoil,naca001064-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,25.1668 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca001064-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.6931,0.09210,0.08460,-0.0246,1.0000,0.0631 -10.500,-0.7120,0.08500,0.07750,-0.0291,1.0000,0.0625 -10.250,-0.7341,0.07902,0.07146,-0.0316,1.0000,0.0620 -10.000,-0.7570,0.07415,0.06650,-0.0318,1.0000,0.0616 -9.750,-0.7776,0.06990,0.06214,-0.0304,1.0000,0.0615 -9.500,-0.7925,0.06566,0.05768,-0.0287,1.0000,0.0615 -9.250,-0.8032,0.06158,0.05331,-0.0267,1.0000,0.0619 -9.000,-0.8106,0.05771,0.04906,-0.0243,1.0000,0.0630 -8.750,-0.8154,0.05401,0.04482,-0.0215,1.0000,0.0646 -8.500,-0.8156,0.05059,0.04088,-0.0187,1.0000,0.0661 -8.250,-0.8048,0.04783,0.03799,-0.0172,1.0000,0.0679 -8.000,-0.7934,0.04518,0.03506,-0.0153,1.0000,0.0693 -7.750,-0.7804,0.04282,0.03241,-0.0135,1.0000,0.0715 -7.500,-0.7668,0.04067,0.02989,-0.0116,1.0000,0.0751 -7.250,-0.7515,0.03841,0.02711,-0.0096,1.0000,0.0781 -7.000,-0.7322,0.03616,0.02453,-0.0082,1.0000,0.0800 -6.750,-0.7109,0.03428,0.02252,-0.0072,1.0000,0.0824 -6.500,-0.6891,0.03270,0.02078,-0.0062,1.0000,0.0858 -6.250,-0.6670,0.03135,0.01915,-0.0051,1.0000,0.0915 -6.000,-0.6434,0.02994,0.01770,-0.0043,1.0000,0.0964 -5.750,-0.6191,0.02868,0.01635,-0.0035,1.0000,0.1013 -5.500,-0.5943,0.02756,0.01503,-0.0025,1.0000,0.1075 -5.250,-0.5729,0.02645,0.01397,-0.0014,1.0000,0.1150 -5.000,-0.5527,0.02547,0.01299,-0.0001,1.0000,0.1276 -4.750,-0.5340,0.02449,0.01207,0.0014,1.0000,0.1465 -4.500,-0.5166,0.02341,0.01113,0.0031,1.0000,0.1733 -4.000,-0.4908,0.02061,0.00952,0.0074,1.0000,0.3395 -3.750,-0.4827,0.01919,0.00951,0.0120,1.0000,0.5714 -3.500,-0.4534,0.01935,0.01013,0.0146,1.0000,0.7361 -3.250,-0.4216,0.01983,0.01053,0.0159,1.0000,0.8088 -3.000,-0.3796,0.02058,0.01107,0.0155,1.0000,0.8653 -2.750,-0.3209,0.02132,0.01146,0.0114,1.0000,0.9063 -2.500,-0.2444,0.02173,0.01150,0.0029,1.0000,0.9381 -2.250,-0.1882,0.02165,0.01117,-0.0028,1.0000,0.9598 -2.000,-0.1443,0.02137,0.01071,-0.0067,1.0000,0.9733 -1.750,-0.1013,0.02105,0.01025,-0.0105,1.0000,0.9849 -1.500,-0.0585,0.02069,0.00979,-0.0145,1.0000,0.9952 -1.250,-0.0334,0.02042,0.00947,-0.0151,1.0000,1.0000 -1.000,-0.0253,0.02026,0.00929,-0.0124,1.0000,1.0000 -0.750,-0.0180,0.02013,0.00916,-0.0095,1.0000,1.0000 -0.500,-0.0116,0.02005,0.00907,-0.0064,1.0000,1.0000 -0.250,-0.0056,0.02000,0.00902,-0.0032,1.0000,1.0000 0.000,0.0000,0.01998,0.00900,0.0000,1.0000,1.0000 0.250,0.0056,0.02000,0.00902,0.0032,1.0000,1.0000 0.500,0.0115,0.02005,0.00907,0.0064,1.0000,1.0000 0.750,0.0180,0.02013,0.00916,0.0095,1.0000,1.0000 1.000,0.0253,0.02025,0.00929,0.0124,1.0000,1.0000 1.250,0.0334,0.02041,0.00946,0.0151,1.0000,1.0000 1.500,0.0585,0.02068,0.00978,0.0145,0.9952,1.0000 1.750,0.1013,0.02104,0.01025,0.0105,0.9849,1.0000 2.000,0.1443,0.02137,0.01071,0.0067,0.9733,1.0000 2.250,0.1881,0.02165,0.01117,0.0028,0.9599,1.0000 2.500,0.2443,0.02173,0.01149,-0.0029,0.9382,1.0000 2.750,0.3209,0.02132,0.01146,-0.0114,0.9063,1.0000 3.000,0.3796,0.02058,0.01106,-0.0155,0.8654,1.0000 3.250,0.4215,0.01983,0.01052,-0.0159,0.8089,1.0000 3.500,0.4534,0.01934,0.01013,-0.0146,0.7362,1.0000 3.750,0.4827,0.01918,0.00951,-0.0120,0.5717,1.0000 4.000,0.4908,0.02060,0.00951,-0.0074,0.3397,1.0000 4.500,0.5166,0.02341,0.01113,-0.0031,0.1734,1.0000 4.750,0.5340,0.02449,0.01207,-0.0014,0.1464,1.0000 5.000,0.5527,0.02547,0.01299,0.0001,0.1276,1.0000 5.250,0.5729,0.02645,0.01397,0.0014,0.1150,1.0000 5.500,0.5943,0.02756,0.01502,0.0025,0.1075,1.0000 5.750,0.6191,0.02868,0.01635,0.0035,0.1013,1.0000 6.000,0.6434,0.02994,0.01770,0.0043,0.0964,1.0000 6.250,0.6670,0.03135,0.01915,0.0051,0.0915,1.0000 6.500,0.6891,0.03270,0.02078,0.0062,0.0858,1.0000 6.750,0.7109,0.03428,0.02252,0.0072,0.0824,1.0000 7.000,0.7322,0.03616,0.02453,0.0082,0.0800,1.0000 7.250,0.7515,0.03841,0.02711,0.0096,0.0781,1.0000 7.500,0.7668,0.04066,0.02989,0.0116,0.0751,1.0000 7.750,0.7804,0.04281,0.03241,0.0135,0.0715,1.0000 8.000,0.7935,0.04518,0.03506,0.0153,0.0693,1.0000 8.250,0.8048,0.04783,0.03799,0.0172,0.0679,1.0000 8.500,0.8157,0.05059,0.04088,0.0187,0.0661,1.0000 8.750,0.8154,0.05402,0.04483,0.0215,0.0646,1.0000 9.000,0.8107,0.05772,0.04907,0.0243,0.0630,1.0000 9.250,0.8034,0.06159,0.05332,0.0266,0.0619,1.0000 9.500,0.7927,0.06567,0.05769,0.0287,0.0615,1.0000 9.750,0.7779,0.06992,0.06216,0.0303,0.0615,1.0000 10.000,0.7572,0.07419,0.06653,0.0317,0.0616,1.0000 10.250,0.7345,0.07907,0.07151,0.0315,0.0620,1.0000 10.500,0.7124,0.08506,0.07755,0.0289,0.0625,1.0000 10.750,0.6936,0.09218,0.08468,0.0244,0.0631,1.0000