Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m2-il-50000-n5 Airfoil,m2-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,21.5905 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-m2-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.7111,0.09164,0.08465,-0.0031,1.0000,0.0559 -9.250,-0.7256,0.08452,0.07754,-0.0087,1.0000,0.0549 -9.000,-0.7416,0.07871,0.07167,-0.0114,1.0000,0.0542 -8.750,-0.7501,0.07370,0.06654,-0.0129,1.0000,0.0546 -8.500,-0.7547,0.06900,0.06166,-0.0137,1.0000,0.0554 -8.250,-0.7566,0.06431,0.05672,-0.0141,1.0000,0.0562 -8.000,-0.7555,0.05958,0.05165,-0.0141,1.0000,0.0569 -7.750,-0.7508,0.05493,0.04660,-0.0137,1.0000,0.0575 -7.500,-0.7424,0.05061,0.04180,-0.0131,1.0000,0.0590 -7.250,-0.7319,0.04644,0.03692,-0.0121,1.0000,0.0620 -7.000,-0.7161,0.04336,0.03351,-0.0114,1.0000,0.0649 -6.750,-0.6972,0.04065,0.03045,-0.0107,1.0000,0.0671 -6.500,-0.6769,0.03804,0.02743,-0.0099,1.0000,0.0703 -6.250,-0.6553,0.03560,0.02428,-0.0089,1.0000,0.0757 -6.000,-0.6324,0.03354,0.02213,-0.0084,1.0000,0.0790 -5.750,-0.6079,0.03156,0.01988,-0.0078,1.0000,0.0823 -5.500,-0.5821,0.02970,0.01768,-0.0071,1.0000,0.0864 -5.250,-0.5565,0.02811,0.01589,-0.0064,1.0000,0.0916 -5.000,-0.5316,0.02699,0.01460,-0.0058,1.0000,0.1013 -4.750,-0.5065,0.02564,0.01325,-0.0051,1.0000,0.1097 -4.500,-0.4813,0.02436,0.01185,-0.0043,1.0000,0.1202 -4.250,-0.4574,0.02316,0.01058,-0.0035,1.0000,0.1349 -4.000,-0.4344,0.02206,0.00949,-0.0028,1.0000,0.1540 -3.750,-0.4118,0.02101,0.00856,-0.0022,1.0000,0.1867 -3.500,-0.3920,0.01963,0.00762,-0.0015,1.0000,0.2414 -3.250,-0.3796,0.01762,0.00712,0.0010,1.0000,0.4732 -3.000,-0.3638,0.01685,0.00719,0.0051,1.0000,0.6700 -2.750,-0.3393,0.01672,0.00724,0.0078,1.0000,0.7763 -2.500,-0.3042,0.01683,0.00726,0.0082,1.0000,0.8462 -2.250,-0.2662,0.01695,0.00718,0.0073,1.0000,0.8949 -2.000,-0.2200,0.01705,0.00706,0.0044,1.0000,0.9407 -1.750,-0.1459,0.01704,0.00673,-0.0045,1.0000,0.9794 -1.500,-0.0903,0.01677,0.00628,-0.0107,1.0000,1.0000 -1.250,-0.0740,0.01653,0.00596,-0.0093,1.0000,1.0000 -1.000,-0.0582,0.01635,0.00572,-0.0078,1.0000,1.0000 -0.750,-0.0429,0.01620,0.00554,-0.0061,1.0000,1.0000 -0.500,-0.0283,0.01611,0.00542,-0.0041,1.0000,1.0000 -0.250,-0.0141,0.01605,0.00534,-0.0021,1.0000,1.0000 0.000,0.0000,0.01603,0.00532,0.0000,1.0000,1.0000 0.250,0.0141,0.01605,0.00534,0.0021,1.0000,1.0000 0.500,0.0283,0.01611,0.00542,0.0041,1.0000,1.0000 0.750,0.0430,0.01620,0.00554,0.0061,1.0000,1.0000 1.000,0.0582,0.01634,0.00572,0.0078,1.0000,1.0000 1.250,0.0740,0.01653,0.00596,0.0093,1.0000,1.0000 1.500,0.0903,0.01677,0.00628,0.0107,1.0000,1.0000 1.750,0.1459,0.01704,0.00673,0.0045,0.9794,1.0000 2.000,0.2199,0.01705,0.00705,-0.0044,0.9408,1.0000 2.250,0.2662,0.01694,0.00718,-0.0073,0.8949,1.0000 2.500,0.3042,0.01683,0.00726,-0.0082,0.8462,1.0000 2.750,0.3393,0.01672,0.00723,-0.0078,0.7764,1.0000 3.000,0.3638,0.01685,0.00719,-0.0051,0.6701,1.0000 3.250,0.3796,0.01762,0.00712,-0.0010,0.4734,1.0000 3.500,0.3920,0.01962,0.00761,0.0015,0.2414,1.0000 3.750,0.4118,0.02101,0.00855,0.0022,0.1866,1.0000 4.000,0.4344,0.02206,0.00949,0.0028,0.1539,1.0000 4.250,0.4574,0.02316,0.01058,0.0035,0.1349,1.0000 4.500,0.4813,0.02436,0.01185,0.0043,0.1202,1.0000 4.750,0.5065,0.02564,0.01325,0.0051,0.1097,1.0000 5.000,0.5317,0.02699,0.01460,0.0058,0.1013,1.0000 5.250,0.5565,0.02811,0.01588,0.0064,0.0916,1.0000 5.500,0.5821,0.02970,0.01768,0.0071,0.0864,1.0000 5.750,0.6079,0.03156,0.01988,0.0078,0.0823,1.0000 6.000,0.6324,0.03354,0.02213,0.0084,0.0790,1.0000 6.250,0.6553,0.03560,0.02429,0.0089,0.0757,1.0000 6.500,0.6769,0.03804,0.02743,0.0099,0.0703,1.0000 6.750,0.6972,0.04066,0.03046,0.0107,0.0671,1.0000 7.000,0.7162,0.04337,0.03352,0.0114,0.0649,1.0000 7.250,0.7320,0.04644,0.03693,0.0121,0.0620,1.0000 7.500,0.7425,0.05062,0.04181,0.0130,0.0590,1.0000 7.750,0.7509,0.05494,0.04661,0.0137,0.0575,1.0000 8.000,0.7556,0.05959,0.05167,0.0141,0.0569,1.0000 8.250,0.7568,0.06433,0.05674,0.0141,0.0562,1.0000 8.500,0.7550,0.06902,0.06168,0.0137,0.0554,1.0000 8.750,0.7505,0.07368,0.06652,0.0129,0.0545,1.0000 9.000,0.7423,0.07868,0.07164,0.0114,0.0542,1.0000 9.250,0.7261,0.08454,0.07757,0.0086,0.0548,1.0000 9.500,0.7117,0.09166,0.08467,0.0030,0.0558,1.0000