Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n0012-il-100000 Airfoil,n0012-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,36.6846 Max Cl/Cd alpha,5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-n0012-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.5002,0.13756,0.13233,-0.0001,1.0000,0.1541 -12.500,-0.5184,0.13358,0.12838,-0.0027,1.0000,0.1558 -12.250,-0.7724,0.10051,0.09513,-0.0153,1.0000,0.0866 -12.000,-0.7713,0.09532,0.08992,-0.0162,1.0000,0.0856 -11.750,-0.7896,0.08685,0.08144,-0.0207,1.0000,0.0842 -11.500,-0.8377,0.07511,0.06959,-0.0287,1.0000,0.0813 -11.250,-0.9695,0.06291,0.05654,-0.0300,1.0000,0.0753 -11.000,-0.9842,0.05891,0.05220,-0.0278,1.0000,0.0751 -10.750,-0.9915,0.05467,0.04764,-0.0258,1.0000,0.0753 -10.500,-0.9911,0.05060,0.04330,-0.0241,1.0000,0.0759 -10.250,-0.9765,0.04806,0.04077,-0.0233,1.0000,0.0778 -10.000,-0.9659,0.04582,0.03837,-0.0219,1.0000,0.0802 -9.750,-0.9597,0.04303,0.03523,-0.0199,1.0000,0.0822 -9.500,-0.9523,0.04019,0.03192,-0.0177,1.0000,0.0841 -9.250,-0.9430,0.03777,0.02894,-0.0153,1.0000,0.0861 -9.000,-0.9245,0.03526,0.02644,-0.0145,1.0000,0.0896 -8.750,-0.9056,0.03367,0.02473,-0.0134,1.0000,0.0938 -8.500,-0.8883,0.03189,0.02255,-0.0117,1.0000,0.0978 -8.250,-0.8673,0.02998,0.02066,-0.0109,1.0000,0.1029 -8.000,-0.8471,0.02869,0.01923,-0.0096,1.0000,0.1091 -7.750,-0.8256,0.02707,0.01754,-0.0086,1.0000,0.1157 -7.500,-0.8050,0.02598,0.01635,-0.0074,1.0000,0.1242 -7.250,-0.7836,0.02464,0.01512,-0.0064,1.0000,0.1333 -7.000,-0.7631,0.02348,0.01396,-0.0051,1.0000,0.1447 -6.750,-0.7430,0.02242,0.01293,-0.0038,1.0000,0.1584 -6.500,-0.7235,0.02143,0.01204,-0.0023,1.0000,0.1748 -6.250,-0.7047,0.02050,0.01124,-0.0008,1.0000,0.1953 -6.000,-0.6862,0.01958,0.01046,0.0008,1.0000,0.2203 -5.750,-0.6682,0.01875,0.00981,0.0025,1.0000,0.2509 -5.500,-0.6504,0.01798,0.00927,0.0042,1.0000,0.2860 -5.250,-0.6324,0.01733,0.00880,0.0060,1.0000,0.3256 -5.000,-0.6141,0.01674,0.00844,0.0077,1.0000,0.3656 -4.750,-0.5953,0.01627,0.00813,0.0095,1.0000,0.4067 -4.500,-0.5761,0.01585,0.00789,0.0112,1.0000,0.4463 -4.250,-0.5565,0.01550,0.00770,0.0129,1.0000,0.4854 -4.000,-0.5366,0.01520,0.00752,0.0145,1.0000,0.5246 -3.750,-0.5162,0.01493,0.00743,0.0162,1.0000,0.5615 -3.500,-0.4957,0.01471,0.00736,0.0179,1.0000,0.5981 -3.250,-0.4751,0.01453,0.00732,0.0196,1.0000,0.6345 -3.000,-0.4545,0.01440,0.00731,0.0214,1.0000,0.6707 -2.750,-0.4340,0.01432,0.00735,0.0232,1.0000,0.7062 -2.500,-0.4137,0.01429,0.00742,0.0252,1.0000,0.7415 -2.250,-0.3935,0.01433,0.00757,0.0272,1.0000,0.7754 -2.000,-0.3737,0.01444,0.00777,0.0294,1.0000,0.8089 -1.750,-0.3539,0.01463,0.00801,0.0317,1.0000,0.8421 -1.500,-0.3320,0.01489,0.00831,0.0335,1.0000,0.8748 -1.250,-0.3021,0.01527,0.00870,0.0338,1.0000,0.9052 -1.000,-0.2578,0.01574,0.00913,0.0309,1.0000,0.9317 -0.750,-0.2041,0.01619,0.00952,0.0259,1.0000,0.9557 -0.500,-0.1345,0.01658,0.00986,0.0174,1.0000,0.9712 -0.250,-0.0651,0.01682,0.01007,0.0086,1.0000,0.9860 0.000,0.0000,0.01693,0.01017,0.0000,1.0000,1.0000 0.250,0.0651,0.01682,0.01007,-0.0086,0.9860,1.0000 0.500,0.1344,0.01658,0.00986,-0.0174,0.9712,1.0000 0.750,0.2040,0.01619,0.00952,-0.0258,0.9557,1.0000 1.000,0.2578,0.01574,0.00913,-0.0309,0.9317,1.0000 1.250,0.3020,0.01527,0.00870,-0.0338,0.9053,1.0000 1.500,0.3320,0.01489,0.00831,-0.0335,0.8748,1.0000 1.750,0.3538,0.01462,0.00801,-0.0317,0.8421,1.0000 2.000,0.3737,0.01444,0.00777,-0.0294,0.8089,1.0000 2.250,0.3934,0.01433,0.00757,-0.0272,0.7754,1.0000 2.500,0.4136,0.01429,0.00742,-0.0252,0.7415,1.0000 2.750,0.4339,0.01432,0.00735,-0.0232,0.7063,1.0000 3.000,0.4544,0.01440,0.00731,-0.0214,0.6707,1.0000 3.250,0.4750,0.01453,0.00731,-0.0196,0.6346,1.0000 3.500,0.4957,0.01471,0.00736,-0.0179,0.5981,1.0000 3.750,0.5162,0.01493,0.00742,-0.0162,0.5615,1.0000 4.000,0.5365,0.01520,0.00752,-0.0145,0.5247,1.0000 4.250,0.5565,0.01549,0.00770,-0.0128,0.4854,1.0000 4.500,0.5761,0.01585,0.00789,-0.0111,0.4463,1.0000 4.750,0.5953,0.01627,0.00813,-0.0094,0.4068,1.0000 5.000,0.6141,0.01674,0.00843,-0.0077,0.3656,1.0000 5.250,0.6323,0.01732,0.00880,-0.0060,0.3257,1.0000 5.500,0.6503,0.01798,0.00927,-0.0042,0.2860,1.0000 5.750,0.6681,0.01874,0.00981,-0.0025,0.2509,1.0000 6.000,0.6862,0.01958,0.01046,-0.0008,0.2203,1.0000 6.250,0.7046,0.02050,0.01124,0.0008,0.1953,1.0000 6.500,0.7235,0.02143,0.01204,0.0023,0.1748,1.0000 6.750,0.7430,0.02242,0.01293,0.0038,0.1584,1.0000 7.000,0.7631,0.02348,0.01396,0.0051,0.1447,1.0000 7.250,0.7836,0.02464,0.01512,0.0064,0.1333,1.0000 7.500,0.8050,0.02598,0.01635,0.0074,0.1242,1.0000 7.750,0.8256,0.02706,0.01754,0.0086,0.1157,1.0000 8.000,0.8471,0.02869,0.01923,0.0096,0.1091,1.0000 8.250,0.8673,0.02998,0.02066,0.0109,0.1029,1.0000 8.500,0.8884,0.03189,0.02255,0.0117,0.0978,1.0000 8.750,0.9057,0.03367,0.02473,0.0134,0.0938,1.0000 9.000,0.9246,0.03526,0.02644,0.0145,0.0896,1.0000 9.250,0.9431,0.03777,0.02894,0.0153,0.0861,1.0000 9.500,0.9524,0.04019,0.03192,0.0176,0.0841,1.0000 9.750,0.9598,0.04303,0.03523,0.0198,0.0822,1.0000 10.000,0.9661,0.04582,0.03837,0.0219,0.0801,1.0000 10.250,0.9768,0.04806,0.04076,0.0233,0.0778,1.0000 10.500,0.9913,0.05061,0.04331,0.0241,0.0759,1.0000 10.750,0.9917,0.05469,0.04765,0.0257,0.0753,1.0000 11.000,0.9845,0.05893,0.05222,0.0278,0.0751,1.0000 11.250,0.9697,0.06293,0.05656,0.0300,0.0753,1.0000 11.500,0.8378,0.07522,0.06970,0.0285,0.0813,1.0000 11.750,0.7898,0.08703,0.08162,0.0204,0.0842,1.0000