Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca0006-il-100000 Airfoil,naca0006-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,32.8558 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-naca0006-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5661,0.11269,0.10814,0.0140,1.0000,0.0914 -9.750,-0.5830,0.10909,0.10461,0.0097,1.0000,0.0925 -9.500,-0.7037,0.11447,0.10977,0.0241,1.0000,0.0814 -9.250,-0.6934,0.11087,0.10614,0.0257,1.0000,0.0859 -9.000,-0.6952,0.10675,0.10207,0.0227,1.0000,0.0898 -8.750,-0.7078,0.10227,0.09768,0.0146,1.0000,0.0921 -8.500,-0.7208,0.09688,0.09233,0.0047,1.0000,0.0927 -8.250,-0.6967,0.09341,0.08887,0.0159,1.0000,0.0987 -8.000,-0.6997,0.08881,0.08432,0.0114,1.0000,0.1029 -7.750,-0.7174,0.08268,0.07796,-0.0036,1.0000,0.1066 -7.500,-0.6995,0.07812,0.07361,0.0024,1.0000,0.1110 -7.250,-0.7061,0.07370,0.06878,-0.0067,1.0000,0.1208 -7.000,-0.6891,0.06863,0.06399,-0.0028,1.0000,0.1254 -6.750,-0.6168,0.05155,0.04715,-0.0071,1.0000,0.1467 -6.500,-0.6741,0.05985,0.05481,-0.0076,1.0000,0.1506 -6.250,-0.6605,0.05609,0.05099,-0.0071,1.0000,0.1655 -6.000,-0.6320,0.04340,0.03670,-0.0112,1.0000,0.0785 -5.750,-0.6107,0.03711,0.02979,-0.0103,1.0000,0.0638 -5.500,-0.5895,0.03283,0.02504,-0.0095,1.0000,0.0618 -5.250,-0.5658,0.02890,0.02053,-0.0084,1.0000,0.0592 -5.000,-0.5404,0.02585,0.01692,-0.0073,1.0000,0.0599 -4.750,-0.5137,0.02413,0.01460,-0.0061,1.0000,0.0658 -4.500,-0.4883,0.02113,0.01156,-0.0054,1.0000,0.0722 -4.250,-0.4629,0.01936,0.00971,-0.0046,1.0000,0.0856 -4.000,-0.4379,0.01784,0.00818,-0.0037,1.0000,0.1036 -3.750,-0.4139,0.01637,0.00674,-0.0027,1.0000,0.1222 -3.500,-0.3910,0.01504,0.00566,-0.0017,1.0000,0.1576 -3.250,-0.3789,0.01190,0.00470,0.0009,1.0000,0.5305 -3.000,-0.3625,0.01103,0.00463,0.0052,1.0000,0.7482 -2.750,-0.3350,0.01089,0.00457,0.0075,1.0000,0.8707 -2.500,-0.2163,0.01134,0.00448,-0.0080,1.0000,0.9997 -2.250,-0.1948,0.01103,0.00396,-0.0077,1.0000,1.0000 -2.000,-0.1733,0.01079,0.00356,-0.0072,1.0000,1.0000 -1.750,-0.1516,0.01060,0.00324,-0.0066,1.0000,1.0000 -1.500,-0.1297,0.01046,0.00297,-0.0059,1.0000,1.0000 -1.250,-0.1078,0.01034,0.00275,-0.0050,1.0000,1.0000 -1.000,-0.0859,0.01026,0.00258,-0.0042,1.0000,1.0000 -0.750,-0.0642,0.01020,0.00246,-0.0032,1.0000,1.0000 -0.500,-0.0427,0.01015,0.00237,-0.0022,1.0000,1.0000 -0.250,-0.0213,0.01013,0.00231,-0.0011,1.0000,1.0000 0.000,0.0000,0.01012,0.00230,0.0000,1.0000,1.0000 0.250,0.0213,0.01013,0.00231,0.0011,1.0000,1.0000 0.500,0.0427,0.01015,0.00237,0.0022,1.0000,1.0000 0.750,0.0642,0.01020,0.00246,0.0032,1.0000,1.0000 1.000,0.0859,0.01026,0.00258,0.0042,1.0000,1.0000 1.250,0.1078,0.01034,0.00274,0.0050,1.0000,1.0000 1.500,0.1297,0.01046,0.00297,0.0058,1.0000,1.0000 1.750,0.1516,0.01060,0.00324,0.0066,1.0000,1.0000 2.000,0.1734,0.01078,0.00356,0.0072,1.0000,1.0000 2.250,0.1949,0.01102,0.00396,0.0077,1.0000,1.0000 2.500,0.2162,0.01134,0.00448,0.0080,0.9999,1.0000 2.750,0.3350,0.01089,0.00457,-0.0075,0.8708,1.0000 3.000,0.3624,0.01103,0.00463,-0.0051,0.7484,1.0000 3.250,0.3788,0.01190,0.00470,-0.0009,0.5312,1.0000 3.500,0.3909,0.01504,0.00566,0.0017,0.1577,1.0000 3.750,0.4138,0.01637,0.00674,0.0027,0.1222,1.0000 4.000,0.4379,0.01784,0.00818,0.0037,0.1036,1.0000 4.250,0.4628,0.01936,0.00971,0.0046,0.0856,1.0000 4.500,0.4883,0.02113,0.01156,0.0054,0.0721,1.0000 4.750,0.5137,0.02414,0.01461,0.0061,0.0658,1.0000 5.000,0.5404,0.02585,0.01692,0.0073,0.0600,1.0000 5.250,0.5658,0.02891,0.02053,0.0084,0.0592,1.0000 5.500,0.5895,0.03284,0.02505,0.0095,0.0618,1.0000 5.750,0.6108,0.03711,0.02980,0.0103,0.0639,1.0000 6.750,0.6843,0.06381,0.05894,0.0064,0.1371,1.0000 7.000,0.6893,0.06864,0.06399,0.0028,0.1253,1.0000 7.250,0.7060,0.07370,0.06878,0.0066,0.1208,1.0000 7.500,0.6999,0.07812,0.07361,-0.0025,0.1110,1.0000 7.750,0.7174,0.08269,0.07798,0.0035,0.1066,1.0000 8.000,0.7000,0.08885,0.08436,-0.0116,0.1028,1.0000 8.250,0.6973,0.09343,0.08889,-0.0160,0.0986,1.0000 8.500,0.7210,0.09692,0.09237,-0.0049,0.0926,1.0000 8.750,0.7080,0.10232,0.09774,-0.0149,0.0921,1.0000 9.000,0.6956,0.10680,0.10212,-0.0229,0.0897,1.0000 9.250,0.6941,0.11091,0.10619,-0.0258,0.0858,1.0000 9.500,0.5989,0.10492,0.10051,-0.0054,0.0929,1.0000 9.750,0.5825,0.10893,0.10445,-0.0097,0.0925,1.0000