Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64012-il-100000 Airfoil,n64012-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,39.8512 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-n64012-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.6344,0.09389,0.08907,-0.0022,1.0000,0.1863 -9.500,-0.6503,0.08864,0.08393,-0.0052,1.0000,0.1966 -8.750,-0.8370,0.05259,0.04573,-0.0190,1.0000,0.0785 -8.500,-0.8234,0.04726,0.04030,-0.0187,1.0000,0.0764 -8.250,-0.8112,0.04310,0.03583,-0.0176,1.0000,0.0736 -8.000,-0.7984,0.03911,0.03130,-0.0160,1.0000,0.0705 -7.750,-0.7825,0.03581,0.02739,-0.0143,1.0000,0.0687 -7.500,-0.7617,0.03320,0.02441,-0.0133,1.0000,0.0688 -7.250,-0.7392,0.03123,0.02235,-0.0127,1.0000,0.0715 -7.000,-0.7163,0.02940,0.02029,-0.0119,1.0000,0.0742 -6.750,-0.6917,0.02753,0.01820,-0.0111,1.0000,0.0762 -6.500,-0.6670,0.02603,0.01645,-0.0103,1.0000,0.0785 -6.250,-0.6431,0.02405,0.01465,-0.0097,1.0000,0.0834 -6.000,-0.6228,0.02295,0.01354,-0.0085,1.0000,0.0900 -5.750,-0.6059,0.02161,0.01231,-0.0066,1.0000,0.0956 -5.500,-0.5941,0.02072,0.01150,-0.0041,1.0000,0.1039 -5.250,-0.5870,0.01978,0.01068,-0.0009,1.0000,0.1150 -5.000,-0.5810,0.01886,0.00986,0.0023,1.0000,0.1300 -4.750,-0.5771,0.01754,0.00890,0.0056,1.0000,0.1695 -4.500,-0.5895,0.01480,0.00836,0.0112,1.0000,0.5149 -4.250,-0.5801,0.01515,0.00888,0.0153,1.0000,0.6104 -4.000,-0.5669,0.01564,0.00939,0.0186,1.0000,0.6503 -3.750,-0.5486,0.01616,0.00985,0.0208,0.9984,0.6798 -3.500,-0.5115,0.01705,0.01070,0.0202,0.9888,0.7131 -3.250,-0.4779,0.01831,0.01198,0.0213,0.9798,0.7477 -3.000,-0.4428,0.01958,0.01322,0.0226,0.9718,0.7759 -2.750,-0.4084,0.02006,0.01360,0.0222,0.9628,0.7928 -2.500,-0.3609,0.02037,0.01378,0.0190,0.9571,0.8007 -2.250,-0.3273,0.02025,0.01353,0.0172,0.9473,0.8102 -2.000,-0.2807,0.02035,0.01352,0.0136,0.9416,0.8174 -1.750,-0.2454,0.02027,0.01334,0.0117,0.9325,0.8261 -1.500,-0.2014,0.02031,0.01330,0.0085,0.9262,0.8331 -1.250,-0.1686,0.02020,0.01313,0.0071,0.9173,0.8411 -1.000,-0.1304,0.02021,0.01308,0.0049,0.9101,0.8477 -0.750,-0.0981,0.02010,0.01294,0.0036,0.9016,0.8557 -0.500,-0.0639,0.02012,0.01293,0.0022,0.8935,0.8623 -0.250,-0.0322,0.02004,0.01283,0.0011,0.8860,0.8706 0.000,0.0000,0.02010,0.01289,0.0000,0.8778,0.8779 0.250,0.0322,0.02004,0.01282,-0.0011,0.8706,0.8859 0.500,0.0639,0.02012,0.01293,-0.0022,0.8623,0.8935 0.750,0.0981,0.02010,0.01293,-0.0036,0.8557,0.9016 1.000,0.1304,0.02021,0.01308,-0.0049,0.8476,0.9101 1.250,0.1686,0.02020,0.01313,-0.0070,0.8410,0.9173 1.500,0.2013,0.02031,0.01330,-0.0085,0.8330,0.9263 1.750,0.2454,0.02027,0.01334,-0.0117,0.8261,0.9325 2.000,0.2805,0.02035,0.01352,-0.0136,0.8174,0.9416 2.250,0.3274,0.02025,0.01352,-0.0173,0.8102,0.9473 2.500,0.3610,0.02037,0.01378,-0.0190,0.8007,0.9571 2.750,0.4086,0.02005,0.01359,-0.0222,0.7928,0.9628 3.000,0.4430,0.01958,0.01321,-0.0226,0.7759,0.9719 3.250,0.4779,0.01831,0.01197,-0.0213,0.7477,0.9799 3.500,0.5115,0.01705,0.01070,-0.0202,0.7132,0.9889 3.750,0.5486,0.01616,0.00985,-0.0208,0.6799,0.9985 4.000,0.5668,0.01564,0.00938,-0.0186,0.6503,1.0000 4.250,0.5800,0.01515,0.00889,-0.0153,0.6107,1.0000 4.500,0.5894,0.01479,0.00836,-0.0112,0.5167,1.0000 4.750,0.5771,0.01752,0.00889,-0.0056,0.1703,1.0000 5.000,0.5809,0.01885,0.00985,-0.0023,0.1302,1.0000 5.250,0.5869,0.01977,0.01067,0.0010,0.1150,1.0000 5.500,0.5941,0.02073,0.01150,0.0041,0.1045,1.0000 5.750,0.6059,0.02161,0.01231,0.0066,0.0956,1.0000 6.000,0.6228,0.02295,0.01353,0.0085,0.0900,1.0000 6.250,0.6432,0.02404,0.01465,0.0097,0.0836,1.0000 6.500,0.6670,0.02602,0.01645,0.0103,0.0785,1.0000 6.750,0.6917,0.02754,0.01821,0.0111,0.0761,1.0000 7.000,0.7163,0.02939,0.02029,0.0119,0.0743,1.0000 7.250,0.7392,0.03124,0.02236,0.0127,0.0716,1.0000 7.500,0.7617,0.03320,0.02442,0.0133,0.0688,1.0000 7.750,0.7825,0.03581,0.02738,0.0143,0.0686,1.0000 8.000,0.7984,0.03909,0.03129,0.0160,0.0705,1.0000 8.250,0.8111,0.04310,0.03583,0.0176,0.0736,1.0000 8.500,0.8234,0.04726,0.04030,0.0187,0.0764,1.0000 8.750,0.8363,0.05229,0.04546,0.0192,0.0783,1.0000 9.250,0.6891,0.08208,0.07750,0.0112,0.2094,1.0000 9.500,0.6511,0.08859,0.08386,0.0053,0.1965,1.0000 9.750,0.6349,0.09386,0.08904,0.0021,0.1862,1.0000