Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n0012-il-100000-n5 Airfoil,n0012-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,36.0989 Max Cl/Cd alpha,5.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-n0012-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -14.000,-0.8751,0.09584,0.09008,-0.0133,1.0000,0.0392 -13.750,-0.9212,0.08276,0.07678,-0.0224,1.0000,0.0386 -13.500,-0.9550,0.07345,0.06721,-0.0287,1.0000,0.0383 -13.250,-0.9811,0.06643,0.05992,-0.0328,1.0000,0.0384 -13.000,-1.0020,0.06089,0.05410,-0.0352,1.0000,0.0386 -12.750,-1.0192,0.05635,0.04927,-0.0361,1.0000,0.0389 -12.500,-1.0332,0.05253,0.04514,-0.0358,1.0000,0.0394 -12.250,-1.0442,0.04926,0.04152,-0.0345,1.0000,0.0399 -12.000,-1.0447,0.04681,0.03892,-0.0330,1.0000,0.0405 -11.750,-1.0402,0.04492,0.03695,-0.0314,1.0000,0.0413 -11.500,-1.0359,0.04320,0.03513,-0.0296,1.0000,0.0422 -11.250,-1.0301,0.04152,0.03330,-0.0277,1.0000,0.0434 -11.000,-1.0224,0.03971,0.03125,-0.0260,1.0000,0.0450 -10.750,-1.0131,0.03782,0.02903,-0.0243,1.0000,0.0467 -10.500,-0.9997,0.03620,0.02733,-0.0230,1.0000,0.0481 -10.250,-0.9851,0.03484,0.02594,-0.0217,1.0000,0.0497 -10.000,-0.9701,0.03353,0.02451,-0.0204,1.0000,0.0518 -9.750,-0.9540,0.03219,0.02292,-0.0190,1.0000,0.0544 -9.500,-0.9377,0.03089,0.02157,-0.0178,1.0000,0.0567 -9.250,-0.9208,0.02978,0.02043,-0.0165,1.0000,0.0592 -9.000,-0.9030,0.02869,0.01922,-0.0152,1.0000,0.0626 -8.750,-0.8854,0.02758,0.01803,-0.0139,1.0000,0.0660 -8.500,-0.8678,0.02663,0.01706,-0.0126,1.0000,0.0697 -8.250,-0.8488,0.02572,0.01601,-0.0114,1.0000,0.0744 -8.000,-0.8315,0.02476,0.01510,-0.0100,1.0000,0.0790 -7.750,-0.8125,0.02394,0.01420,-0.0086,1.0000,0.0850 -7.500,-0.7946,0.02308,0.01337,-0.0072,1.0000,0.0913 -7.250,-0.7753,0.02235,0.01257,-0.0059,1.0000,0.0993 -7.000,-0.7571,0.02157,0.01185,-0.0045,1.0000,0.1083 -6.750,-0.7385,0.02085,0.01115,-0.0030,1.0000,0.1189 -6.500,-0.7196,0.02017,0.01051,-0.0016,1.0000,0.1316 -6.250,-0.7005,0.01953,0.00992,-0.0002,1.0000,0.1470 -6.000,-0.6813,0.01892,0.00936,0.0012,1.0000,0.1653 -5.750,-0.6617,0.01835,0.00887,0.0025,1.0000,0.1867 -5.500,-0.6423,0.01779,0.00842,0.0038,1.0000,0.2113 -5.250,-0.6226,0.01728,0.00803,0.0051,1.0000,0.2383 -5.000,-0.6027,0.01681,0.00766,0.0064,1.0000,0.2677 -4.750,-0.5826,0.01637,0.00735,0.0077,1.0000,0.2988 -4.500,-0.5623,0.01598,0.00708,0.0090,1.0000,0.3309 -4.250,-0.5419,0.01562,0.00684,0.0103,1.0000,0.3635 -4.000,-0.5212,0.01530,0.00665,0.0115,1.0000,0.3966 -3.750,-0.5004,0.01501,0.00649,0.0127,1.0000,0.4296 -3.500,-0.4793,0.01476,0.00636,0.0139,1.0000,0.4626 -3.250,-0.4580,0.01454,0.00625,0.0151,1.0000,0.4955 -3.000,-0.4365,0.01435,0.00619,0.0162,1.0000,0.5284 -2.750,-0.4120,0.01419,0.00616,0.0168,0.9987,0.5620 -2.500,-0.3736,0.01405,0.00614,0.0146,0.9910,0.5999 -2.250,-0.3346,0.01394,0.00616,0.0124,0.9831,0.6367 -2.000,-0.2976,0.01384,0.00616,0.0107,0.9737,0.6713 -1.750,-0.2601,0.01376,0.00618,0.0091,0.9644,0.7043 -1.500,-0.2196,0.01370,0.00622,0.0069,0.9562,0.7357 -1.250,-0.1837,0.01365,0.00624,0.0057,0.9448,0.7644 -1.000,-0.1475,0.01362,0.00626,0.0046,0.9332,0.7918 -0.750,-0.1093,0.01360,0.00630,0.0031,0.9219,0.8157 -0.500,-0.0724,0.01359,0.00631,0.0020,0.9087,0.8382 -0.250,-0.0370,0.01358,0.00632,0.0011,0.8932,0.8589 0.000,0.0000,0.01358,0.00633,0.0000,0.8767,0.8767 0.250,0.0370,0.01358,0.00632,-0.0011,0.8589,0.8932 0.500,0.0724,0.01359,0.00631,-0.0020,0.8382,0.9087 0.750,0.1093,0.01360,0.00630,-0.0031,0.8157,0.9219 1.000,0.1475,0.01362,0.00626,-0.0046,0.7918,0.9332 1.250,0.1837,0.01365,0.00624,-0.0057,0.7644,0.9448 1.500,0.2196,0.01370,0.00622,-0.0069,0.7358,0.9562 1.750,0.2601,0.01376,0.00618,-0.0091,0.7043,0.9644 2.000,0.2976,0.01383,0.00615,-0.0107,0.6713,0.9737 2.250,0.3346,0.01394,0.00616,-0.0124,0.6367,0.9832 2.500,0.3736,0.01405,0.00614,-0.0146,0.5999,0.9910 2.750,0.4120,0.01419,0.00616,-0.0168,0.5620,0.9987 3.000,0.4365,0.01435,0.00619,-0.0162,0.5284,1.0000 3.250,0.4579,0.01454,0.00625,-0.0151,0.4956,1.0000 3.500,0.4792,0.01476,0.00636,-0.0139,0.4627,1.0000 3.750,0.5003,0.01501,0.00648,-0.0127,0.4297,1.0000 4.000,0.5212,0.01530,0.00664,-0.0115,0.3967,1.0000 4.250,0.5418,0.01562,0.00684,-0.0103,0.3636,1.0000 4.500,0.5623,0.01598,0.00708,-0.0090,0.3309,1.0000 4.750,0.5825,0.01637,0.00735,-0.0077,0.2989,1.0000 5.000,0.6026,0.01680,0.00766,-0.0064,0.2678,1.0000 5.250,0.6225,0.01727,0.00802,-0.0051,0.2383,1.0000 5.500,0.6422,0.01779,0.00842,-0.0038,0.2113,1.0000 5.750,0.6617,0.01835,0.00886,-0.0025,0.1868,1.0000 6.000,0.6812,0.01892,0.00936,-0.0012,0.1653,1.0000 6.250,0.7005,0.01953,0.00991,0.0002,0.1470,1.0000 6.500,0.7195,0.02017,0.01051,0.0016,0.1316,1.0000 6.750,0.7385,0.02085,0.01115,0.0030,0.1189,1.0000 7.000,0.7571,0.02157,0.01184,0.0045,0.1083,1.0000 7.250,0.7753,0.02235,0.01257,0.0059,0.0993,1.0000 7.500,0.7946,0.02308,0.01337,0.0072,0.0913,1.0000 7.750,0.8125,0.02394,0.01419,0.0086,0.0850,1.0000 8.000,0.8315,0.02476,0.01510,0.0100,0.0790,1.0000 8.250,0.8489,0.02571,0.01601,0.0113,0.0744,1.0000 8.500,0.8678,0.02662,0.01706,0.0126,0.0697,1.0000 8.750,0.8855,0.02758,0.01803,0.0139,0.0660,1.0000 9.000,0.9031,0.02869,0.01922,0.0152,0.0626,1.0000 9.250,0.9210,0.02978,0.02043,0.0165,0.0592,1.0000 9.500,0.9379,0.03089,0.02157,0.0177,0.0567,1.0000 9.750,0.9542,0.03220,0.02292,0.0190,0.0544,1.0000 10.000,0.9703,0.03354,0.02451,0.0203,0.0518,1.0000 10.250,0.9853,0.03484,0.02594,0.0216,0.0497,1.0000 10.500,0.9999,0.03620,0.02733,0.0229,0.0481,1.0000 10.750,1.0133,0.03783,0.02903,0.0242,0.0467,1.0000 11.000,1.0227,0.03972,0.03125,0.0259,0.0450,1.0000 11.250,1.0305,0.04152,0.03330,0.0276,0.0434,1.0000 11.500,1.0363,0.04320,0.03513,0.0295,0.0422,1.0000 11.750,1.0408,0.04492,0.03696,0.0313,0.0412,1.0000 12.000,1.0454,0.04682,0.03893,0.0329,0.0405,1.0000 12.250,1.0447,0.04928,0.04154,0.0344,0.0399,1.0000 12.500,1.0338,0.05256,0.04517,0.0357,0.0394,1.0000 12.750,1.0198,0.05638,0.04931,0.0359,0.0389,1.0000 13.000,1.0026,0.06093,0.05415,0.0350,0.0385,1.0000 13.250,0.9817,0.06649,0.05999,0.0326,0.0383,1.0000 13.500,0.9556,0.07354,0.06731,0.0285,0.0383,1.0000 13.750,0.9215,0.08293,0.07695,0.0221,0.0386,1.0000 14.000,0.8751,0.09617,0.09041,0.0128,0.0392,1.0000