Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64110-il-200000 Airfoil,n64110-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,54.5052 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-n64110-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.6359,0.08386,0.08039,-0.0245,1.0000,0.0535 -9.500,-0.6542,0.07846,0.07495,-0.0288,1.0000,0.0535 -9.250,-0.6758,0.07463,0.07103,-0.0303,1.0000,0.0536 -9.000,-0.6966,0.07190,0.06806,-0.0306,1.0000,0.0541 -8.750,-0.7055,0.06921,0.06509,-0.0304,1.0000,0.0543 -8.500,-0.7063,0.06021,0.05619,-0.0316,1.0000,0.0560 -8.250,-0.6899,0.05746,0.05357,-0.0314,1.0000,0.0584 -8.000,-0.6831,0.05466,0.05066,-0.0311,1.0000,0.0620 -7.500,-0.6360,0.03501,0.03093,-0.0310,1.0000,0.0716 -7.250,-0.6254,0.03187,0.02765,-0.0304,1.0000,0.0758 -7.000,-0.6209,0.02783,0.02319,-0.0295,1.0000,0.0835 -6.750,-0.6054,0.02513,0.02049,-0.0289,1.0000,0.0871 -6.500,-0.5961,0.02232,0.01736,-0.0277,1.0000,0.0976 -6.250,-0.5967,0.02803,0.02096,-0.0217,1.0000,0.0425 -6.000,-0.5778,0.02578,0.01848,-0.0202,1.0000,0.0421 -5.750,-0.5596,0.02328,0.01577,-0.0186,1.0000,0.0419 -5.500,-0.5418,0.02184,0.01413,-0.0168,1.0000,0.0422 -5.250,-0.5247,0.01976,0.01191,-0.0149,1.0000,0.0430 -5.000,-0.5089,0.01818,0.01032,-0.0131,1.0000,0.0451 -4.750,-0.4933,0.01743,0.00958,-0.0113,1.0000,0.0482 -4.500,-0.4728,0.01656,0.00868,-0.0103,0.9991,0.0505 -4.250,-0.4331,0.01563,0.00768,-0.0129,0.9936,0.0541 -4.000,-0.3965,0.01438,0.00650,-0.0154,0.9872,0.0625 -3.750,-0.3570,0.01346,0.00557,-0.0183,0.9815,0.0765 -3.500,-0.3255,0.01116,0.00442,-0.0208,0.9740,0.2966 -3.250,-0.2937,0.00998,0.00450,-0.0221,0.9677,0.6084 -3.000,-0.2574,0.00997,0.00455,-0.0235,0.9603,0.6596 -2.750,-0.2196,0.01000,0.00458,-0.0252,0.9541,0.6901 -2.500,-0.1879,0.01016,0.00477,-0.0253,0.9452,0.7270 -2.250,-0.1601,0.01046,0.00516,-0.0241,0.9363,0.7610 -2.000,-0.1294,0.01053,0.00521,-0.0240,0.9283,0.7771 -1.750,-0.1021,0.01051,0.00514,-0.0237,0.9175,0.7877 -1.500,-0.0747,0.01049,0.00507,-0.0234,0.9076,0.7986 -1.250,-0.0479,0.01046,0.00500,-0.0227,0.8990,0.8067 -1.000,-0.0227,0.01043,0.00494,-0.0220,0.8879,0.8162 -0.750,0.0026,0.01041,0.00490,-0.0213,0.8779,0.8258 -0.500,0.0278,0.01038,0.00484,-0.0203,0.8694,0.8346 -0.250,0.0528,0.01037,0.00481,-0.0196,0.8590,0.8447 0.000,0.0775,0.01037,0.00481,-0.0187,0.8495,0.8548 0.250,0.1020,0.01035,0.00479,-0.0176,0.8412,0.8644 0.500,0.1266,0.01036,0.00481,-0.0168,0.8311,0.8750 0.750,0.1513,0.01037,0.00483,-0.0160,0.8227,0.8864 1.000,0.1755,0.01037,0.00485,-0.0148,0.8140,0.8971 1.250,0.2001,0.01038,0.00490,-0.0139,0.8048,0.9084 1.500,0.2258,0.01037,0.00490,-0.0131,0.7976,0.9200 1.750,0.2524,0.01038,0.00496,-0.0128,0.7877,0.9321 2.000,0.2814,0.01037,0.00498,-0.0128,0.7784,0.9442 2.250,0.3150,0.01035,0.00500,-0.0137,0.7692,0.9546 2.500,0.3524,0.01033,0.00504,-0.0156,0.7575,0.9633 2.750,0.3875,0.01002,0.00468,-0.0162,0.7295,0.9725 3.000,0.4253,0.00974,0.00432,-0.0176,0.6902,0.9806 3.250,0.4667,0.00967,0.00426,-0.0202,0.6639,0.9879 3.500,0.5064,0.00963,0.00418,-0.0226,0.6232,0.9970 3.750,0.5287,0.00970,0.00414,-0.0217,0.5678,1.0000 4.000,0.5357,0.01037,0.00412,-0.0181,0.3956,1.0000 4.250,0.5313,0.01306,0.00512,-0.0140,0.0989,1.0000 4.500,0.5497,0.01401,0.00592,-0.0128,0.0721,1.0000 4.750,0.5711,0.01482,0.00672,-0.0119,0.0611,1.0000 5.000,0.5909,0.01599,0.00784,-0.0109,0.0551,1.0000 5.250,0.6140,0.01684,0.00875,-0.0101,0.0505,1.0000 5.500,0.6364,0.01792,0.00976,-0.0095,0.0459,1.0000 5.750,0.6595,0.01967,0.01153,-0.0087,0.0435,1.0000 6.000,0.6852,0.02093,0.01290,-0.0082,0.0422,1.0000 6.250,0.7113,0.02253,0.01465,-0.0077,0.0413,1.0000 6.500,0.7371,0.02428,0.01661,-0.0072,0.0402,1.0000 6.750,0.7617,0.02584,0.01836,-0.0067,0.0382,1.0000 7.000,0.7855,0.02833,0.02118,-0.0059,0.0383,1.0000 7.250,0.8068,0.03189,0.02521,-0.0046,0.0400,1.0000 7.500,0.8232,0.03699,0.03065,-0.0036,0.0432,1.0000 8.250,0.8688,0.05525,0.05020,0.0008,0.0697,1.0000 8.500,0.8067,0.04766,0.04374,0.0057,0.0670,1.0000 8.750,0.7961,0.05150,0.04790,0.0073,0.0636,1.0000 9.000,0.7849,0.05567,0.05223,0.0083,0.0620,1.0000 9.250,0.7643,0.05962,0.05629,0.0097,0.0616,1.0000 9.500,0.7347,0.06456,0.06135,0.0091,0.0619,1.0000 9.750,0.6982,0.07183,0.06872,0.0055,0.0636,1.0000 10.000,0.6682,0.08065,0.07759,0.0001,0.0653,1.0000 10.250,0.6462,0.08995,0.08688,-0.0057,0.0659,1.0000