Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64012-il-50000-n5 Airfoil,n64012-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,27.1156 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-n64012-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.500,-0.6974,0.09710,0.08992,-0.0133,1.0000,0.0538 -11.250,-0.7193,0.08896,0.08175,-0.0189,1.0000,0.0530 -11.000,-0.7439,0.08174,0.07445,-0.0234,1.0000,0.0516 -10.750,-0.7686,0.07581,0.06839,-0.0264,1.0000,0.0512 -10.500,-0.7902,0.07104,0.06345,-0.0277,1.0000,0.0510 -10.250,-0.8083,0.06711,0.05938,-0.0275,1.0000,0.0510 -10.000,-0.8218,0.06365,0.05571,-0.0263,1.0000,0.0512 -9.750,-0.8291,0.06020,0.05196,-0.0252,1.0000,0.0518 -9.500,-0.8316,0.05685,0.04830,-0.0240,1.0000,0.0525 -9.250,-0.8301,0.05351,0.04460,-0.0228,1.0000,0.0532 -9.000,-0.8241,0.05023,0.04092,-0.0215,1.0000,0.0538 -8.750,-0.8137,0.04711,0.03739,-0.0204,1.0000,0.0545 -8.500,-0.7992,0.04420,0.03405,-0.0194,1.0000,0.0554 -8.250,-0.7815,0.04162,0.03100,-0.0184,1.0000,0.0570 -8.000,-0.7609,0.03926,0.02852,-0.0179,1.0000,0.0598 -7.750,-0.7384,0.03737,0.02648,-0.0175,1.0000,0.0630 -7.500,-0.7118,0.03543,0.02433,-0.0171,1.0000,0.0661 -7.250,-0.6829,0.03377,0.02237,-0.0167,1.0000,0.0699 -7.000,-0.6578,0.03225,0.02098,-0.0164,1.0000,0.0755 -6.750,-0.6325,0.03100,0.01954,-0.0156,1.0000,0.0817 -6.500,-0.6125,0.02967,0.01824,-0.0145,1.0000,0.0877 -6.250,-0.5954,0.02854,0.01705,-0.0131,1.0000,0.0977 -6.000,-0.5822,0.02726,0.01584,-0.0113,1.0000,0.1087 -5.750,-0.5710,0.02596,0.01464,-0.0094,1.0000,0.1239 -5.250,-0.5628,0.02261,0.01223,-0.0040,1.0000,0.2232 -5.000,-0.5677,0.02094,0.01195,0.0008,1.0000,0.3965 -4.750,-0.5612,0.02086,0.01224,0.0052,1.0000,0.5260 -4.500,-0.5530,0.02107,0.01249,0.0094,1.0000,0.5861 -4.250,-0.5444,0.02156,0.01301,0.0139,1.0000,0.6331 -4.000,-0.5367,0.02240,0.01390,0.0194,1.0000,0.6777 -3.750,-0.5224,0.02340,0.01486,0.0243,0.9987,0.7126 -3.500,-0.4882,0.02399,0.01524,0.0242,0.9879,0.7386 -3.250,-0.4513,0.02403,0.01502,0.0223,0.9778,0.7521 -3.000,-0.4117,0.02407,0.01482,0.0201,0.9688,0.7609 -2.750,-0.3734,0.02395,0.01449,0.0176,0.9596,0.7711 -2.500,-0.3351,0.02385,0.01420,0.0151,0.9505,0.7807 -2.250,-0.2973,0.02378,0.01394,0.0128,0.9413,0.7885 -2.000,-0.2599,0.02360,0.01361,0.0102,0.9329,0.7977 -1.750,-0.2235,0.02355,0.01344,0.0084,0.9235,0.8042 -1.500,-0.1925,0.02338,0.01316,0.0070,0.9135,0.8134 -1.250,-0.1532,0.02335,0.01304,0.0046,0.9058,0.8194 -1.000,-0.1269,0.02323,0.01285,0.0042,0.8952,0.8290 -0.750,-0.0887,0.02321,0.01278,0.0022,0.8877,0.8352 -0.500,-0.0630,0.02314,0.01267,0.0020,0.8776,0.8448 -0.250,-0.0298,0.02314,0.01266,0.0007,0.8692,0.8518 0.000,0.0000,0.02311,0.01261,0.0000,0.8609,0.8609 0.250,0.0298,0.02314,0.01266,-0.0007,0.8518,0.8692 0.500,0.0630,0.02313,0.01267,-0.0020,0.8447,0.8776 0.750,0.0888,0.02321,0.01278,-0.0022,0.8351,0.8878 1.000,0.1269,0.02323,0.01285,-0.0042,0.8290,0.8951 1.250,0.1532,0.02334,0.01304,-0.0046,0.8194,0.9058 1.500,0.1926,0.02338,0.01316,-0.0070,0.8134,0.9135 1.750,0.2235,0.02354,0.01343,-0.0084,0.8042,0.9235 2.000,0.2599,0.02360,0.01361,-0.0102,0.7977,0.9329 2.250,0.2973,0.02378,0.01395,-0.0128,0.7885,0.9413 2.500,0.3352,0.02385,0.01420,-0.0151,0.7807,0.9505 2.750,0.3734,0.02395,0.01448,-0.0176,0.7711,0.9596 3.000,0.4116,0.02406,0.01482,-0.0201,0.7610,0.9687 3.250,0.4513,0.02402,0.01502,-0.0223,0.7521,0.9778 3.500,0.4882,0.02399,0.01524,-0.0242,0.7386,0.9879 3.750,0.5224,0.02339,0.01485,-0.0242,0.7124,0.9986 4.000,0.5367,0.02240,0.01387,-0.0194,0.6778,1.0000 4.250,0.5444,0.02156,0.01301,-0.0139,0.6331,1.0000 4.500,0.5530,0.02106,0.01248,-0.0093,0.5858,1.0000 4.750,0.5612,0.02086,0.01224,-0.0052,0.5257,1.0000 5.000,0.5678,0.02094,0.01195,-0.0008,0.3969,1.0000 5.250,0.5628,0.02261,0.01223,0.0040,0.2230,1.0000 5.500,0.5638,0.02446,0.01343,0.0070,0.1540,1.0000 5.750,0.5711,0.02596,0.01464,0.0094,0.1239,1.0000 6.000,0.5822,0.02726,0.01585,0.0113,0.1085,1.0000 6.250,0.5955,0.02853,0.01704,0.0130,0.0977,1.0000 6.500,0.6126,0.02967,0.01824,0.0145,0.0877,1.0000 6.750,0.6326,0.03099,0.01954,0.0156,0.0817,1.0000 7.000,0.6578,0.03224,0.02097,0.0164,0.0755,1.0000 7.250,0.6831,0.03378,0.02238,0.0167,0.0698,1.0000 7.500,0.7119,0.03544,0.02435,0.0171,0.0660,1.0000 7.750,0.7384,0.03737,0.02649,0.0175,0.0630,1.0000 8.000,0.7609,0.03927,0.02851,0.0179,0.0597,1.0000 8.250,0.7817,0.04163,0.03101,0.0184,0.0570,1.0000 8.500,0.7992,0.04422,0.03408,0.0193,0.0554,1.0000 8.750,0.8138,0.04711,0.03739,0.0204,0.0545,1.0000 9.000,0.8243,0.05023,0.04091,0.0215,0.0538,1.0000 9.250,0.8303,0.05353,0.04461,0.0227,0.0532,1.0000 9.500,0.8319,0.05687,0.04831,0.0240,0.0525,1.0000 9.750,0.8292,0.06025,0.05201,0.0252,0.0518,1.0000 10.000,0.8221,0.06370,0.05576,0.0262,0.0512,1.0000 10.250,0.8088,0.06711,0.05938,0.0274,0.0508,1.0000 10.500,0.7906,0.07109,0.06351,0.0276,0.0510,1.0000 10.750,0.7686,0.07594,0.06852,0.0262,0.0513,1.0000 11.000,0.7442,0.08188,0.07459,0.0232,0.0519,1.0000 11.250,0.7193,0.08911,0.08190,0.0186,0.0527,1.0000 11.500,0.6975,0.09734,0.09015,0.0130,0.0537,1.0000