Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca641112-il-100000-n5 Airfoil,naca641112-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,39.9525 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca641112-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.500,-0.6717,0.08614,0.08095,-0.0256,1.0000,0.0319 -11.250,-0.6957,0.07784,0.07260,-0.0314,1.0000,0.0314 -11.000,-0.7207,0.07104,0.06568,-0.0358,1.0000,0.0311 -10.750,-0.7428,0.06567,0.06015,-0.0383,1.0000,0.0308 -10.500,-0.7628,0.06134,0.05564,-0.0392,1.0000,0.0309 -10.250,-0.7807,0.05768,0.05180,-0.0385,1.0000,0.0309 -10.000,-0.7943,0.05432,0.04820,-0.0369,1.0000,0.0310 -9.750,-0.8010,0.05083,0.04441,-0.0355,1.0000,0.0311 -9.500,-0.8028,0.04741,0.04065,-0.0341,1.0000,0.0312 -9.250,-0.7999,0.04418,0.03703,-0.0326,1.0000,0.0315 -9.000,-0.7924,0.04119,0.03365,-0.0312,1.0000,0.0319 -8.750,-0.7813,0.03843,0.03047,-0.0299,1.0000,0.0324 -8.500,-0.7672,0.03606,0.02769,-0.0287,1.0000,0.0332 -8.250,-0.7511,0.03400,0.02528,-0.0275,1.0000,0.0343 -8.000,-0.7328,0.03204,0.02327,-0.0269,1.0000,0.0357 -7.750,-0.7135,0.03046,0.02156,-0.0261,1.0000,0.0369 -7.500,-0.6933,0.02888,0.01982,-0.0251,1.0000,0.0380 -7.250,-0.6732,0.02745,0.01826,-0.0241,1.0000,0.0392 -7.000,-0.6540,0.02616,0.01686,-0.0228,1.0000,0.0406 -6.750,-0.6364,0.02513,0.01571,-0.0213,1.0000,0.0426 -6.500,-0.6217,0.02409,0.01464,-0.0194,1.0000,0.0447 -6.000,-0.5831,0.02221,0.01278,-0.0177,0.9926,0.0500 -5.750,-0.5490,0.02126,0.01169,-0.0196,0.9836,0.0545 -5.500,-0.5159,0.02021,0.01069,-0.0216,0.9746,0.0613 -5.250,-0.4838,0.01932,0.00972,-0.0231,0.9649,0.0693 -5.000,-0.4526,0.01845,0.00889,-0.0245,0.9550,0.0847 -4.750,-0.4225,0.01743,0.00805,-0.0258,0.9456,0.1213 -4.500,-0.3997,0.01567,0.00716,-0.0265,0.9348,0.2753 -4.250,-0.3799,0.01462,0.00706,-0.0256,0.9231,0.4755 -4.000,-0.3527,0.01452,0.00708,-0.0252,0.9132,0.5460 -3.750,-0.3252,0.01459,0.00719,-0.0246,0.9042,0.5971 -3.500,-0.3013,0.01485,0.00749,-0.0230,0.8934,0.6405 -3.250,-0.2762,0.01514,0.00779,-0.0215,0.8843,0.6719 -3.000,-0.2499,0.01524,0.00780,-0.0207,0.8752,0.6893 -2.750,-0.2233,0.01521,0.00766,-0.0202,0.8655,0.6977 -2.500,-0.1955,0.01513,0.00743,-0.0201,0.8577,0.7074 -2.250,-0.1692,0.01511,0.00736,-0.0196,0.8480,0.7143 -2.000,-0.1420,0.01503,0.00716,-0.0195,0.8398,0.7231 -1.750,-0.1152,0.01499,0.00706,-0.0191,0.8312,0.7289 -1.500,-0.0883,0.01492,0.00690,-0.0190,0.8230,0.7370 -1.250,-0.0615,0.01488,0.00682,-0.0186,0.8150,0.7430 -1.000,-0.0348,0.01484,0.00672,-0.0184,0.8068,0.7504 -0.750,-0.0080,0.01481,0.00665,-0.0181,0.7994,0.7572 -0.500,0.0185,0.01480,0.00662,-0.0178,0.7916,0.7648 -0.250,0.0452,0.01478,0.00657,-0.0175,0.7843,0.7721 0.000,0.0717,0.01479,0.00657,-0.0172,0.7767,0.7795 0.250,0.0983,0.01479,0.00657,-0.0169,0.7695,0.7873 0.500,0.1248,0.01481,0.00660,-0.0165,0.7628,0.7954 0.750,0.1511,0.01484,0.00666,-0.0162,0.7555,0.8034 1.000,0.1778,0.01486,0.00668,-0.0159,0.7493,0.8120 1.250,0.2040,0.01492,0.00681,-0.0156,0.7416,0.8200 1.500,0.2308,0.01495,0.00685,-0.0153,0.7363,0.8299 1.750,0.2564,0.01504,0.00703,-0.0148,0.7286,0.8380 2.000,0.2828,0.01508,0.00713,-0.0144,0.7225,0.8476 2.250,0.3087,0.01517,0.00731,-0.0140,0.7157,0.8573 2.500,0.3349,0.01523,0.00744,-0.0135,0.7085,0.8668 2.750,0.3608,0.01529,0.00760,-0.0131,0.7008,0.8775 3.000,0.3871,0.01533,0.00774,-0.0126,0.6929,0.8883 3.250,0.4141,0.01540,0.00794,-0.0123,0.6849,0.8989 3.500,0.4419,0.01540,0.00805,-0.0120,0.6762,0.9101 3.750,0.4694,0.01526,0.00797,-0.0114,0.6600,0.9221 4.000,0.4966,0.01499,0.00775,-0.0107,0.6320,0.9345 4.250,0.5258,0.01471,0.00745,-0.0103,0.5904,0.9463 4.500,0.5568,0.01462,0.00730,-0.0106,0.5399,0.9584 4.750,0.5893,0.01475,0.00734,-0.0115,0.4732,0.9710 5.000,0.6131,0.01599,0.00754,-0.0118,0.2752,0.9880 5.250,0.6256,0.01765,0.00844,-0.0108,0.1459,1.0000 5.500,0.6372,0.01873,0.00919,-0.0088,0.0996,1.0000 5.750,0.6530,0.01967,0.00998,-0.0074,0.0790,1.0000 6.000,0.6701,0.02060,0.01083,-0.0062,0.0686,1.0000 6.250,0.6893,0.02139,0.01168,-0.0051,0.0608,1.0000 6.500,0.7068,0.02238,0.01266,-0.0040,0.0555,1.0000 6.750,0.7259,0.02330,0.01366,-0.0030,0.0515,1.0000 7.000,0.7446,0.02428,0.01463,-0.0020,0.0476,1.0000 7.250,0.7633,0.02547,0.01582,-0.0011,0.0446,1.0000 7.500,0.7846,0.02664,0.01709,-0.0003,0.0423,1.0000 7.750,0.8068,0.02795,0.01849,0.0003,0.0404,1.0000 8.000,0.8291,0.02928,0.01988,0.0008,0.0386,1.0000 8.250,0.8508,0.03077,0.02135,0.0011,0.0367,1.0000 8.500,0.8732,0.03255,0.02328,0.0015,0.0349,1.0000 8.750,0.8953,0.03437,0.02539,0.0021,0.0338,1.0000 9.000,0.9157,0.03649,0.02779,0.0028,0.0329,1.0000 9.250,0.9334,0.03880,0.03041,0.0037,0.0321,1.0000 9.500,0.9480,0.04128,0.03322,0.0047,0.0315,1.0000 9.750,0.9590,0.04397,0.03625,0.0060,0.0310,1.0000 10.000,0.9666,0.04663,0.03923,0.0074,0.0305,1.0000 10.250,0.9724,0.04907,0.04191,0.0088,0.0298,1.0000 10.500,0.9766,0.05137,0.04441,0.0101,0.0291,1.0000 10.750,0.9774,0.05362,0.04680,0.0117,0.0284,1.0000 11.000,0.9729,0.05635,0.04969,0.0133,0.0280,1.0000 11.250,0.9643,0.05956,0.05307,0.0147,0.0277,1.0000 11.750,0.9343,0.06719,0.06112,0.0156,0.0275,1.0000 12.000,0.9166,0.07166,0.06580,0.0148,0.0276,1.0000