Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-bacj-il-50000-n5 Airfoil,bacj-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,20.3706 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-bacj-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.5574,0.10061,0.09271,-0.0392,1.0000,0.0669 -10.500,-0.5689,0.09498,0.08716,-0.0414,1.0000,0.0663 -10.250,-0.5905,0.08703,0.07925,-0.0455,1.0000,0.0659 -10.000,-0.6245,0.07855,0.07080,-0.0500,1.0000,0.0632 -9.500,-0.7217,0.06637,0.05839,-0.0515,1.0000,0.0602 -9.250,-0.7208,0.06523,0.05733,-0.0491,1.0000,0.0625 -9.000,-0.7775,0.06082,0.05251,-0.0433,1.0000,0.0596 -8.750,-0.7808,0.05903,0.05072,-0.0406,1.0000,0.0610 -8.500,-0.7856,0.05702,0.04865,-0.0376,1.0000,0.0625 -8.250,-0.7968,0.05416,0.04554,-0.0342,1.0000,0.0625 -8.000,-0.8027,0.05155,0.04268,-0.0309,1.0000,0.0631 -7.750,-0.8056,0.04890,0.03973,-0.0278,1.0000,0.0632 -7.500,-0.8051,0.04644,0.03697,-0.0248,1.0000,0.0646 -7.250,-0.8012,0.04402,0.03424,-0.0220,1.0000,0.0654 -7.000,-0.7948,0.04173,0.03159,-0.0193,1.0000,0.0671 -6.750,-0.7854,0.03951,0.02899,-0.0169,1.0000,0.0690 -6.500,-0.7723,0.03775,0.02684,-0.0148,1.0000,0.0703 -6.250,-0.7576,0.03612,0.02501,-0.0129,1.0000,0.0727 -6.000,-0.7427,0.03487,0.02377,-0.0111,1.0000,0.0763 -5.750,-0.7267,0.03356,0.02222,-0.0091,1.0000,0.0827 -5.500,-0.7090,0.03234,0.02092,-0.0076,1.0000,0.0874 -5.250,-0.6917,0.03132,0.01986,-0.0058,1.0000,0.0939 -5.000,-0.6712,0.03028,0.01858,-0.0043,1.0000,0.0999 -4.750,-0.6540,0.02924,0.01761,-0.0024,1.0000,0.1083 -4.500,-0.6386,0.02832,0.01672,-0.0004,1.0000,0.1224 -4.250,-0.6236,0.02746,0.01587,0.0018,1.0000,0.1348 -4.000,-0.6096,0.02664,0.01508,0.0040,1.0000,0.1498 -3.750,-0.5964,0.02578,0.01429,0.0065,1.0000,0.1710 -3.500,-0.5843,0.02492,0.01358,0.0089,1.0000,0.2027 -3.250,-0.5714,0.02397,0.01288,0.0110,1.0000,0.2452 -3.000,-0.5592,0.02284,0.01223,0.0130,1.0000,0.3178 -2.750,-0.5498,0.02179,0.01231,0.0166,1.0000,0.4570 -2.500,-0.5391,0.02199,0.01308,0.0214,1.0000,0.5936 -2.250,-0.5276,0.02226,0.01325,0.0254,1.0000,0.6570 -2.000,-0.5149,0.02253,0.01338,0.0292,1.0000,0.6979 -1.750,-0.5009,0.02277,0.01354,0.0325,1.0000,0.7281 -1.500,-0.4872,0.02297,0.01366,0.0359,1.0000,0.7572 -1.250,-0.4714,0.02305,0.01359,0.0388,1.0000,0.7814 -1.000,-0.4523,0.02306,0.01350,0.0410,1.0000,0.8041 -0.750,-0.4331,0.02302,0.01341,0.0433,1.0000,0.8306 -0.500,-0.4102,0.02289,0.01322,0.0447,1.0000,0.8575 -0.250,-0.3783,0.02276,0.01309,0.0444,1.0000,0.8863 0.000,-0.3325,0.02276,0.01300,0.0410,1.0000,0.9105 0.250,-0.2907,0.02282,0.01298,0.0376,1.0000,0.9217 0.500,-0.2504,0.02301,0.01312,0.0341,0.9972,0.9294 0.750,-0.2039,0.02333,0.01339,0.0295,0.9925,0.9347 1.000,-0.1599,0.02364,0.01366,0.0253,0.9876,0.9408 1.250,-0.1111,0.02415,0.01416,0.0203,0.9829,0.9460 1.500,-0.0686,0.02440,0.01449,0.0163,0.9776,0.9525 1.750,-0.0240,0.02481,0.01494,0.0121,0.9722,0.9587 2.000,0.0194,0.02519,0.01541,0.0080,0.9656,0.9656 2.250,0.0632,0.02556,0.01588,0.0040,0.9580,0.9723 2.500,0.1062,0.02590,0.01638,0.0000,0.9496,0.9826 2.750,0.1535,0.02632,0.01696,-0.0044,0.9385,0.9916 3.000,0.1862,0.02705,0.01778,-0.0060,0.9230,1.0000 3.250,0.2258,0.02679,0.01770,-0.0082,0.9010,1.0000 3.500,0.2665,0.02656,0.01771,-0.0104,0.8818,1.0000 3.750,0.3075,0.02585,0.01731,-0.0118,0.8543,1.0000 4.000,0.3612,0.02265,0.01437,-0.0107,0.7566,1.0000 4.250,0.4437,0.02290,0.01181,-0.0142,0.1935,1.0000 4.500,0.4452,0.02385,0.01225,-0.0103,0.1359,1.0000 4.750,0.4551,0.02476,0.01290,-0.0077,0.1098,1.0000 5.000,0.4705,0.02557,0.01362,-0.0060,0.1011,1.0000 5.250,0.4917,0.02648,0.01454,-0.0051,0.0902,1.0000 5.500,0.5196,0.02745,0.01561,-0.0052,0.0822,1.0000 5.750,0.5575,0.02862,0.01684,-0.0069,0.0772,1.0000 6.000,0.6155,0.03068,0.01898,-0.0122,0.0703,1.0000 6.250,0.6596,0.03238,0.02090,-0.0151,0.0668,1.0000 6.500,0.6907,0.03405,0.02266,-0.0160,0.0626,1.0000 6.750,0.7232,0.03628,0.02500,-0.0172,0.0608,1.0000 7.000,0.7483,0.03863,0.02762,-0.0171,0.0598,1.0000 7.250,0.7654,0.04083,0.03022,-0.0154,0.0591,1.0000 7.500,0.7795,0.04302,0.03272,-0.0134,0.0588,1.0000 7.750,0.7902,0.04542,0.03546,-0.0110,0.0585,1.0000 8.000,0.7958,0.04790,0.03833,-0.0079,0.0577,1.0000 8.250,0.8014,0.05049,0.04123,-0.0052,0.0577,1.0000 8.500,0.8012,0.05327,0.04437,-0.0019,0.0568,1.0000 8.750,0.7982,0.05606,0.04749,0.0013,0.0552,1.0000 9.000,0.7950,0.05887,0.05054,0.0041,0.0549,1.0000 9.250,0.7867,0.06200,0.05389,0.0070,0.0542,1.0000 9.500,0.7776,0.06558,0.05770,0.0093,0.0548,1.0000 9.750,0.7631,0.06963,0.06197,0.0108,0.0548,1.0000 10.000,0.7543,0.07328,0.06574,0.0111,0.0558,1.0000 10.250,0.7350,0.07833,0.07093,0.0102,0.0556,1.0000 10.500,0.7183,0.08400,0.07671,0.0078,0.0564,1.0000 10.750,0.7066,0.08974,0.08246,0.0044,0.0573,1.0000 11.000,0.7002,0.09541,0.08815,0.0009,0.0582,1.0000