Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64108-il-500000-n5 Airfoil,n64108-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,50.2803 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-n64108-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.6546,0.08420,0.08203,-0.0052,1.0000,0.0052 -9.500,-0.6629,0.07773,0.07559,-0.0098,1.0000,0.0052 -9.250,-0.6773,0.06924,0.06712,-0.0183,1.0000,0.0051 -9.000,-0.6969,0.06346,0.06128,-0.0222,1.0000,0.0051 -8.750,-0.7121,0.05696,0.05464,-0.0244,1.0000,0.0051 -8.500,-0.7217,0.05013,0.04757,-0.0255,1.0000,0.0051 -8.250,-0.7288,0.04216,0.03923,-0.0255,1.0000,0.0051 -8.000,-0.7505,0.02634,0.02218,-0.0231,1.0000,0.0054 -7.750,-0.7332,0.02365,0.01914,-0.0225,1.0000,0.0057 -7.500,-0.7113,0.02241,0.01771,-0.0221,1.0000,0.0059 -7.250,-0.6886,0.02127,0.01640,-0.0218,1.0000,0.0063 -7.000,-0.6662,0.01969,0.01458,-0.0213,1.0000,0.0068 -6.750,-0.6434,0.01816,0.01280,-0.0207,1.0000,0.0074 -6.500,-0.6188,0.01744,0.01194,-0.0203,1.0000,0.0083 -6.250,-0.5942,0.01673,0.01105,-0.0199,1.0000,0.0088 -6.000,-0.5729,0.01472,0.00881,-0.0190,1.0000,0.0097 -5.750,-0.5490,0.01407,0.00810,-0.0186,1.0000,0.0105 -5.500,-0.5230,0.01348,0.00746,-0.0185,0.9979,0.0113 -5.250,-0.4906,0.01286,0.00675,-0.0197,0.9881,0.0124 -5.000,-0.4578,0.01244,0.00626,-0.0211,0.9786,0.0138 -4.750,-0.4254,0.01189,0.00560,-0.0223,0.9684,0.0144 -4.500,-0.3946,0.01106,0.00467,-0.0232,0.9571,0.0153 -4.250,-0.3653,0.01039,0.00392,-0.0237,0.9449,0.0169 -4.000,-0.3372,0.01004,0.00352,-0.0239,0.9321,0.0187 -3.750,-0.3104,0.00971,0.00312,-0.0237,0.9191,0.0206 -3.500,-0.2839,0.00946,0.00276,-0.0234,0.9066,0.0229 -3.250,-0.2576,0.00921,0.00244,-0.0230,0.8943,0.0265 -3.000,-0.2313,0.00899,0.00218,-0.0227,0.8825,0.0329 -2.750,-0.2047,0.00881,0.00197,-0.0225,0.8708,0.0418 -2.500,-0.1783,0.00851,0.00175,-0.0223,0.8595,0.0768 -2.250,-0.1535,0.00767,0.00147,-0.0223,0.8483,0.2344 -2.000,-0.1293,0.00676,0.00122,-0.0222,0.8375,0.4316 -1.750,-0.1030,0.00646,0.00113,-0.0220,0.8273,0.5121 -1.500,-0.0768,0.00619,0.00108,-0.0218,0.8165,0.5899 -1.250,-0.0512,0.00595,0.00111,-0.0213,0.8059,0.6693 -1.000,-0.0246,0.00586,0.00111,-0.0209,0.7955,0.7068 -0.500,0.0303,0.00583,0.00106,-0.0206,0.7752,0.7350 -0.250,0.0581,0.00584,0.00104,-0.0206,0.7648,0.7454 0.000,0.0857,0.00584,0.00104,-0.0205,0.7545,0.7558 0.250,0.1132,0.00585,0.00105,-0.0204,0.7446,0.7664 0.500,0.1409,0.00586,0.00107,-0.0203,0.7346,0.7771 0.750,0.1685,0.00588,0.00110,-0.0202,0.7243,0.7877 1.000,0.1956,0.00593,0.00112,-0.0200,0.7055,0.7985 1.250,0.2222,0.00600,0.00115,-0.0196,0.6793,0.8095 1.500,0.2488,0.00608,0.00120,-0.0193,0.6510,0.8206 1.750,0.2743,0.00629,0.00123,-0.0187,0.5955,0.8317 2.000,0.2993,0.00659,0.00129,-0.0182,0.5238,0.8430 2.250,0.3246,0.00690,0.00140,-0.0178,0.4552,0.8550 2.750,0.3683,0.00888,0.00208,-0.0166,0.1017,0.8802 3.000,0.3929,0.00928,0.00233,-0.0161,0.0520,0.8935 3.250,0.4180,0.00951,0.00255,-0.0156,0.0377,0.9077 3.500,0.4432,0.00972,0.00281,-0.0150,0.0310,0.9229 3.750,0.4686,0.00997,0.00311,-0.0145,0.0257,0.9393 4.000,0.4966,0.01020,0.00341,-0.0146,0.0222,0.9568 4.500,0.5580,0.01122,0.00453,-0.0163,0.0165,1.0000 4.750,0.5841,0.01164,0.00502,-0.0161,0.0159,1.0000 5.000,0.6099,0.01213,0.00558,-0.0159,0.0152,1.0000 5.250,0.6352,0.01273,0.00625,-0.0156,0.0144,1.0000 5.500,0.6609,0.01324,0.00682,-0.0154,0.0132,1.0000 5.750,0.6865,0.01374,0.00735,-0.0152,0.0122,1.0000 6.000,0.7116,0.01436,0.00803,-0.0149,0.0114,1.0000 6.250,0.7355,0.01530,0.00907,-0.0145,0.0107,1.0000 6.500,0.7575,0.01699,0.01095,-0.0137,0.0098,1.0000 6.750,0.7832,0.01744,0.01149,-0.0135,0.0092,1.0000 7.000,0.8080,0.01821,0.01238,-0.0132,0.0084,1.0000 7.250,0.8317,0.01936,0.01371,-0.0127,0.0077,1.0000 7.500,0.8554,0.02037,0.01487,-0.0123,0.0071,1.0000 7.750,0.8789,0.02126,0.01588,-0.0120,0.0067,1.0000 8.000,0.9021,0.02209,0.01686,-0.0117,0.0063,1.0000 8.250,0.9181,0.02516,0.02032,-0.0106,0.0058,1.0000 8.500,0.9353,0.02781,0.02337,-0.0095,0.0056,1.0000 8.750,0.9433,0.03294,0.02912,-0.0077,0.0051,1.0000 9.000,0.9174,0.04657,0.04367,-0.0040,0.0046,1.0000 9.250,0.9014,0.05457,0.05206,-0.0025,0.0044,1.0000 9.500,0.8840,0.06089,0.05860,-0.0019,0.0044,1.0000 9.750,0.8581,0.06601,0.06383,-0.0013,0.0045,1.0000 10.000,0.8347,0.07196,0.06987,-0.0043,0.0045,1.0000 10.250,0.8111,0.08123,0.07922,-0.0123,0.0049,1.0000