Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca001234-il-50000-n5 Airfoil,naca001234-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,27.5104 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca001234-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.250,-0.6643,0.09163,0.08449,-0.0416,1.0000,0.0343 -11.000,-0.6781,0.08662,0.07943,-0.0435,1.0000,0.0341 -10.750,-0.6931,0.08207,0.07481,-0.0446,1.0000,0.0339 -10.500,-0.7096,0.07798,0.07062,-0.0446,1.0000,0.0338 -10.250,-0.7264,0.07437,0.06689,-0.0435,1.0000,0.0337 -10.000,-0.7432,0.07118,0.06357,-0.0411,1.0000,0.0336 -9.750,-0.7590,0.06825,0.06046,-0.0379,1.0000,0.0336 -9.500,-0.7711,0.06518,0.05717,-0.0347,1.0000,0.0336 -9.250,-0.7802,0.06214,0.05386,-0.0314,1.0000,0.0337 -9.000,-0.7863,0.05912,0.05054,-0.0279,1.0000,0.0338 -8.750,-0.7892,0.05612,0.04721,-0.0245,1.0000,0.0339 -8.500,-0.7887,0.05315,0.04388,-0.0212,1.0000,0.0340 -8.250,-0.7850,0.05026,0.04060,-0.0179,1.0000,0.0341 -8.000,-0.7778,0.04748,0.03740,-0.0149,1.0000,0.0344 -7.750,-0.7658,0.04439,0.03393,-0.0127,1.0000,0.0350 -7.500,-0.7516,0.04180,0.03118,-0.0110,1.0000,0.0368 -7.250,-0.7351,0.03970,0.02888,-0.0093,1.0000,0.0394 -7.000,-0.7138,0.03756,0.02640,-0.0079,1.0000,0.0420 -6.750,-0.6864,0.03544,0.02395,-0.0071,1.0000,0.0441 -6.500,-0.6617,0.03334,0.02182,-0.0064,1.0000,0.0479 -6.250,-0.6431,0.03194,0.02029,-0.0047,1.0000,0.0540 -6.000,-0.6267,0.03054,0.01868,-0.0024,1.0000,0.0589 -5.750,-0.6150,0.02917,0.01726,0.0003,1.0000,0.0663 -5.500,-0.6040,0.02787,0.01586,0.0030,1.0000,0.0801 -5.250,-0.5945,0.02630,0.01441,0.0060,1.0000,0.1030 -5.000,-0.5951,0.02361,0.01298,0.0098,1.0000,0.2462 -4.750,-0.5978,0.02174,0.01255,0.0155,1.0000,0.4871 -4.500,-0.5832,0.02195,0.01366,0.0214,1.0000,0.6804 -4.250,-0.5547,0.02370,0.01537,0.0261,1.0000,0.7746 -4.000,-0.5299,0.02391,0.01523,0.0274,1.0000,0.7993 -3.750,-0.4966,0.02422,0.01514,0.0271,1.0000,0.8189 -3.500,-0.4698,0.02434,0.01496,0.0276,1.0000,0.8391 -3.250,-0.4374,0.02451,0.01482,0.0269,1.0000,0.8561 -3.000,-0.4027,0.02465,0.01464,0.0256,1.0000,0.8715 -2.750,-0.3678,0.02474,0.01447,0.0241,1.0000,0.8862 -2.500,-0.3312,0.02478,0.01427,0.0220,1.0000,0.9000 -2.250,-0.2946,0.02478,0.01403,0.0197,1.0000,0.9134 -2.000,-0.2583,0.02475,0.01382,0.0173,1.0000,0.9263 -1.750,-0.2221,0.02471,0.01362,0.0148,1.0000,0.9390 -1.500,-0.1859,0.02466,0.01342,0.0122,1.0000,0.9516 -1.250,-0.1453,0.02459,0.01323,0.0086,1.0000,0.9623 -1.000,-0.1063,0.02450,0.01304,0.0052,1.0000,0.9733 -0.750,-0.0670,0.02441,0.01289,0.0016,1.0000,0.9840 -0.500,-0.0267,0.02432,0.01275,-0.0023,1.0000,0.9942 -0.250,-0.0012,0.02424,0.01266,-0.0034,1.0000,1.0000 0.000,0.0000,0.02422,0.01265,0.0000,1.0000,1.0000 0.250,0.0012,0.02424,0.01266,0.0034,1.0000,1.0000 0.500,0.0267,0.02431,0.01275,0.0023,0.9942,1.0000 0.750,0.0669,0.02441,0.01289,-0.0016,0.9840,1.0000 1.000,0.1063,0.02450,0.01304,-0.0052,0.9733,1.0000 1.250,0.1452,0.02458,0.01322,-0.0086,0.9623,1.0000 1.500,0.1858,0.02466,0.01341,-0.0122,0.9516,1.0000 1.750,0.2220,0.02471,0.01362,-0.0148,0.9390,1.0000 2.000,0.2582,0.02475,0.01381,-0.0173,0.9264,1.0000 2.250,0.2945,0.02477,0.01402,-0.0196,0.9134,1.0000 2.500,0.3312,0.02477,0.01426,-0.0219,0.9001,1.0000 2.750,0.3678,0.02473,0.01446,-0.0241,0.8863,1.0000 3.000,0.4026,0.02465,0.01464,-0.0256,0.8715,1.0000 3.250,0.4373,0.02451,0.01482,-0.0269,0.8561,1.0000 3.500,0.4698,0.02434,0.01495,-0.0276,0.8391,1.0000 3.750,0.4965,0.02421,0.01513,-0.0271,0.8189,1.0000 4.000,0.5298,0.02390,0.01522,-0.0274,0.7993,1.0000 4.250,0.5547,0.02369,0.01537,-0.0261,0.7746,1.0000 4.500,0.5831,0.02195,0.01366,-0.0214,0.6804,1.0000 4.750,0.5978,0.02173,0.01255,-0.0155,0.4874,1.0000 5.000,0.5951,0.02359,0.01297,-0.0098,0.2474,1.0000 5.250,0.5945,0.02629,0.01440,-0.0060,0.1031,1.0000 5.500,0.6040,0.02786,0.01585,-0.0030,0.0802,1.0000 5.750,0.6150,0.02916,0.01725,-0.0003,0.0664,1.0000 6.000,0.6266,0.03053,0.01868,0.0024,0.0589,1.0000 6.250,0.6431,0.03194,0.02028,0.0047,0.0540,1.0000 6.500,0.6616,0.03334,0.02181,0.0064,0.0479,1.0000 6.750,0.6864,0.03544,0.02394,0.0071,0.0441,1.0000 7.000,0.7137,0.03755,0.02639,0.0079,0.0420,1.0000 7.250,0.7351,0.03970,0.02887,0.0093,0.0394,1.0000 7.500,0.7516,0.04179,0.03117,0.0110,0.0368,1.0000 7.750,0.7658,0.04438,0.03392,0.0127,0.0350,1.0000 8.000,0.7777,0.04748,0.03739,0.0149,0.0344,1.0000 8.250,0.7850,0.05025,0.04059,0.0179,0.0341,1.0000 8.500,0.7887,0.05314,0.04387,0.0212,0.0340,1.0000 8.750,0.7892,0.05612,0.04720,0.0245,0.0339,1.0000 9.000,0.7864,0.05912,0.05054,0.0279,0.0338,1.0000 9.250,0.7804,0.06215,0.05387,0.0314,0.0337,1.0000 9.500,0.7713,0.06519,0.05718,0.0347,0.0336,1.0000 9.750,0.7593,0.06826,0.06048,0.0378,0.0336,1.0000 10.000,0.7437,0.07121,0.06359,0.0410,0.0336,1.0000 10.250,0.7267,0.07439,0.06692,0.0434,0.0337,1.0000 10.500,0.7099,0.07802,0.07066,0.0445,0.0338,1.0000 10.750,0.6937,0.08210,0.07484,0.0445,0.0340,1.0000 11.000,0.6784,0.08668,0.07950,0.0434,0.0341,1.0000 11.250,0.6649,0.09169,0.08455,0.0415,0.0343,1.0000