Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca0010-il-100000-n5 Airfoil,naca0010-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,33.5125 Max Cl/Cd alpha,4.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca0010-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.7784,0.09853,0.09336,0.0003,1.0000,0.0361 -11.750,-0.8751,0.07116,0.06575,-0.0210,1.0000,0.0324 -11.500,-0.9141,0.06246,0.05674,-0.0267,1.0000,0.0318 -11.250,-0.9337,0.05792,0.05197,-0.0274,1.0000,0.0320 -11.000,-0.9465,0.05463,0.04847,-0.0263,1.0000,0.0324 -10.750,-0.9536,0.05181,0.04544,-0.0247,1.0000,0.0331 -10.500,-0.9554,0.04902,0.04239,-0.0232,1.0000,0.0342 -10.250,-0.9559,0.04597,0.03897,-0.0216,1.0000,0.0356 -10.000,-0.9537,0.04279,0.03532,-0.0198,1.0000,0.0369 -9.750,-0.9471,0.03983,0.03182,-0.0181,1.0000,0.0381 -9.500,-0.9344,0.03741,0.02923,-0.0169,1.0000,0.0397 -9.250,-0.9180,0.03598,0.02773,-0.0160,1.0000,0.0417 -9.000,-0.9014,0.03432,0.02580,-0.0149,1.0000,0.0439 -8.750,-0.8836,0.03245,0.02361,-0.0138,1.0000,0.0460 -8.500,-0.8644,0.03092,0.02171,-0.0127,1.0000,0.0484 -8.250,-0.8449,0.02930,0.02010,-0.0119,1.0000,0.0509 -8.000,-0.8241,0.02803,0.01874,-0.0110,1.0000,0.0532 -7.750,-0.8027,0.02686,0.01741,-0.0101,1.0000,0.0562 -7.500,-0.7806,0.02580,0.01608,-0.0092,1.0000,0.0592 -7.250,-0.7599,0.02450,0.01479,-0.0083,1.0000,0.0618 -7.000,-0.7387,0.02348,0.01375,-0.0073,1.0000,0.0645 -6.750,-0.7171,0.02259,0.01277,-0.0063,1.0000,0.0683 -6.500,-0.6955,0.02174,0.01183,-0.0053,1.0000,0.0728 -6.250,-0.6751,0.02084,0.01093,-0.0042,1.0000,0.0778 -6.000,-0.6537,0.02006,0.01007,-0.0031,1.0000,0.0839 -5.750,-0.6331,0.01922,0.00928,-0.0020,1.0000,0.0920 -5.500,-0.6120,0.01846,0.00855,-0.0009,1.0000,0.1043 -5.250,-0.5908,0.01774,0.00790,0.0002,1.0000,0.1248 -5.000,-0.5698,0.01703,0.00734,0.0012,1.0000,0.1544 -4.750,-0.5486,0.01637,0.00685,0.0022,1.0000,0.1905 -4.500,-0.5273,0.01578,0.00644,0.0032,1.0000,0.2324 -4.250,-0.5062,0.01519,0.00608,0.0043,1.0000,0.2846 -4.000,-0.4856,0.01461,0.00581,0.0054,1.0000,0.3474 -3.750,-0.4647,0.01412,0.00559,0.0066,1.0000,0.4083 -3.500,-0.4429,0.01373,0.00538,0.0078,1.0000,0.4584 -3.250,-0.4208,0.01341,0.00522,0.0090,1.0000,0.5041 -3.000,-0.3986,0.01311,0.00509,0.0102,1.0000,0.5503 -2.750,-0.3763,0.01286,0.00501,0.0114,1.0000,0.5965 -2.500,-0.3538,0.01265,0.00495,0.0127,1.0000,0.6422 -2.250,-0.3310,0.01249,0.00494,0.0140,1.0000,0.6857 -2.000,-0.3077,0.01239,0.00496,0.0153,1.0000,0.7269 -1.750,-0.2847,0.01233,0.00501,0.0166,1.0000,0.7668 -1.500,-0.2611,0.01234,0.00510,0.0179,1.0000,0.8051 -1.250,-0.2362,0.01239,0.00522,0.0188,1.0000,0.8420 -1.000,-0.1959,0.01251,0.00535,0.0166,0.9941,0.8751 -0.750,-0.1497,0.01263,0.00546,0.0131,0.9856,0.9025 -0.500,-0.1007,0.01272,0.00554,0.0090,0.9767,0.9237 -0.250,-0.0505,0.01278,0.00559,0.0045,0.9669,0.9412 0.000,0.0000,0.01280,0.00560,0.0000,0.9554,0.9554 0.250,0.0505,0.01278,0.00559,-0.0045,0.9412,0.9669 0.500,0.1007,0.01272,0.00554,-0.0090,0.9237,0.9767 0.750,0.1497,0.01263,0.00546,-0.0131,0.9025,0.9856 1.000,0.1959,0.01251,0.00535,-0.0166,0.8751,0.9941 1.250,0.2362,0.01239,0.00522,-0.0188,0.8420,1.0000 1.500,0.2611,0.01234,0.00510,-0.0179,0.8052,1.0000 1.750,0.2846,0.01233,0.00501,-0.0166,0.7668,1.0000 2.000,0.3077,0.01239,0.00496,-0.0153,0.7269,1.0000 2.250,0.3310,0.01249,0.00494,-0.0140,0.6857,1.0000 2.500,0.3538,0.01265,0.00495,-0.0127,0.6422,1.0000 2.750,0.3763,0.01286,0.00501,-0.0114,0.5965,1.0000 3.000,0.3986,0.01311,0.00509,-0.0102,0.5503,1.0000 3.250,0.4208,0.01340,0.00522,-0.0090,0.5041,1.0000 3.500,0.4429,0.01373,0.00538,-0.0078,0.4584,1.0000 3.750,0.4646,0.01412,0.00559,-0.0066,0.4083,1.0000 4.000,0.4855,0.01461,0.00581,-0.0054,0.3474,1.0000 4.250,0.5062,0.01519,0.00608,-0.0043,0.2847,1.0000 4.500,0.5272,0.01578,0.00643,-0.0032,0.2324,1.0000 4.750,0.5486,0.01637,0.00685,-0.0022,0.1905,1.0000 5.000,0.5698,0.01703,0.00734,-0.0012,0.1544,1.0000 5.250,0.5908,0.01774,0.00790,-0.0002,0.1248,1.0000 5.500,0.6120,0.01846,0.00855,0.0009,0.1043,1.0000 5.750,0.6331,0.01922,0.00928,0.0020,0.0920,1.0000 6.000,0.6537,0.02006,0.01007,0.0031,0.0839,1.0000 6.250,0.6751,0.02084,0.01093,0.0042,0.0778,1.0000 6.500,0.6956,0.02173,0.01183,0.0053,0.0729,1.0000 6.750,0.7171,0.02259,0.01277,0.0063,0.0683,1.0000 7.000,0.7387,0.02348,0.01374,0.0073,0.0645,1.0000 7.250,0.7599,0.02450,0.01479,0.0083,0.0618,1.0000 7.500,0.7806,0.02580,0.01608,0.0092,0.0592,1.0000 7.750,0.8028,0.02686,0.01741,0.0101,0.0562,1.0000 8.000,0.8241,0.02803,0.01874,0.0110,0.0532,1.0000 8.250,0.8449,0.02930,0.02010,0.0119,0.0509,1.0000 8.500,0.8644,0.03092,0.02171,0.0126,0.0484,1.0000 8.750,0.8836,0.03245,0.02361,0.0138,0.0460,1.0000 9.000,0.9015,0.03432,0.02580,0.0149,0.0439,1.0000 9.250,0.9181,0.03598,0.02773,0.0160,0.0417,1.0000 9.500,0.9345,0.03741,0.02923,0.0169,0.0397,1.0000 9.750,0.9472,0.03984,0.03183,0.0180,0.0381,1.0000 10.000,0.9538,0.04280,0.03533,0.0198,0.0369,1.0000 10.250,0.9560,0.04598,0.03898,0.0216,0.0356,1.0000 10.500,0.9556,0.04904,0.04241,0.0232,0.0342,1.0000 10.750,0.9538,0.05183,0.04546,0.0246,0.0331,1.0000 11.000,0.9469,0.05465,0.04849,0.0262,0.0324,1.0000 11.250,0.9342,0.05793,0.05197,0.0273,0.0319,1.0000 11.500,0.9145,0.06251,0.05678,0.0265,0.0318,1.0000 11.750,0.8751,0.07130,0.06590,0.0208,0.0324,1.0000 12.000,0.7786,0.09881,0.09365,-0.0006,0.0361,1.0000