Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m5-il-100000 Airfoil,m5-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,47.345 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-m5-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.6010,0.11432,0.10963,0.0209,1.0000,0.0836 -9.000,-0.6125,0.11112,0.10651,0.0136,1.0000,0.0851 -8.750,-0.6262,0.10755,0.10298,0.0062,1.0000,0.0855 -8.500,-0.5954,0.10161,0.09702,0.0156,1.0000,0.0901 -8.250,-0.5920,0.09783,0.09325,0.0140,1.0000,0.0935 -8.000,-0.5958,0.09374,0.08920,0.0098,1.0000,0.0966 -7.750,-0.6088,0.09013,0.08549,-0.0012,1.0000,0.0996 -7.500,-0.6025,0.08422,0.07959,-0.0017,1.0000,0.1013 -7.250,-0.5878,0.08040,0.07584,0.0014,1.0000,0.1046 -7.000,-0.5792,0.07661,0.07199,-0.0005,1.0000,0.1101 -6.750,-0.5754,0.07179,0.06694,-0.0059,1.0000,0.1160 -6.500,-0.5603,0.06842,0.06367,-0.0037,1.0000,0.1221 -6.250,-0.5502,0.06420,0.05920,-0.0070,1.0000,0.1314 -6.000,-0.5344,0.06084,0.05587,-0.0062,1.0000,0.1377 -5.750,-0.5201,0.05698,0.05182,-0.0077,1.0000,0.1477 -5.500,-0.5037,0.05384,0.04843,-0.0087,1.0000,0.1609 -5.250,-0.4866,0.05082,0.04532,-0.0086,1.0000,0.1758 -5.000,-0.4689,0.04779,0.04227,-0.0083,1.0000,0.1917 -4.750,-0.4502,0.04492,0.03936,-0.0080,1.0000,0.2080 -4.500,-0.4308,0.04238,0.03676,-0.0077,1.0000,0.2278 -4.250,-0.4128,0.03983,0.03417,-0.0071,1.0000,0.2546 -4.000,-0.3602,0.03282,0.02507,-0.0099,1.0000,0.1298 -3.750,-0.3332,0.02884,0.02073,-0.0095,1.0000,0.1122 -3.500,-0.3095,0.02640,0.01804,-0.0089,1.0000,0.1082 -3.250,-0.2905,0.02480,0.01618,-0.0075,1.0000,0.1076 -3.000,-0.2772,0.02381,0.01499,-0.0054,1.0000,0.1094 -2.750,-0.2638,0.02286,0.01385,-0.0035,1.0000,0.1096 -2.500,-0.2349,0.02166,0.01238,-0.0043,0.9962,0.1099 -2.250,-0.1854,0.02026,0.01072,-0.0084,0.9866,0.1124 -2.000,-0.1364,0.01894,0.00939,-0.0128,0.9770,0.1192 -1.750,-0.0863,0.01801,0.00837,-0.0172,0.9677,0.1298 -1.500,-0.0408,0.01694,0.00745,-0.0207,0.9566,0.1433 -1.250,-0.0026,0.01604,0.00678,-0.0227,0.9425,0.1709 -1.000,0.1065,0.01316,0.00646,-0.0366,0.9490,1.0000 -0.750,0.1405,0.01324,0.00632,-0.0377,0.9275,1.0000 -0.500,0.1650,0.01338,0.00629,-0.0368,0.9050,1.0000 -0.250,0.1865,0.01353,0.00630,-0.0351,0.8858,1.0000 0.000,0.2069,0.01368,0.00632,-0.0333,0.8683,1.0000 0.250,0.2283,0.01384,0.00637,-0.0317,0.8512,1.0000 0.500,0.2498,0.01400,0.00642,-0.0301,0.8354,1.0000 0.750,0.2716,0.01416,0.00649,-0.0287,0.8203,1.0000 1.000,0.2938,0.01432,0.00657,-0.0273,0.8060,1.0000 1.250,0.3162,0.01449,0.00668,-0.0259,0.7921,1.0000 1.500,0.3388,0.01466,0.00679,-0.0246,0.7787,1.0000 1.750,0.3615,0.01484,0.00690,-0.0233,0.7659,1.0000 2.000,0.3852,0.01503,0.00706,-0.0223,0.7521,1.0000 2.250,0.4090,0.01524,0.00727,-0.0214,0.7385,1.0000 2.500,0.4329,0.01545,0.00747,-0.0204,0.7250,1.0000 2.750,0.4569,0.01568,0.00770,-0.0195,0.7117,1.0000 3.000,0.4808,0.01590,0.00793,-0.0186,0.6983,1.0000 3.250,0.5048,0.01613,0.00819,-0.0176,0.6851,1.0000 3.500,0.5288,0.01636,0.00844,-0.0166,0.6718,1.0000 3.750,0.5528,0.01658,0.00869,-0.0156,0.6583,1.0000 4.000,0.5768,0.01679,0.00893,-0.0146,0.6443,1.0000 4.250,0.6008,0.01697,0.00918,-0.0135,0.6289,1.0000 4.500,0.6247,0.01713,0.00939,-0.0124,0.6125,1.0000 4.750,0.6486,0.01725,0.00956,-0.0112,0.5952,1.0000 5.000,0.6717,0.01713,0.00944,-0.0094,0.5749,1.0000 5.250,0.6946,0.01691,0.00923,-0.0077,0.5477,1.0000 5.500,0.7178,0.01669,0.00902,-0.0061,0.5186,1.0000 5.750,0.7412,0.01656,0.00891,-0.0047,0.4874,1.0000 6.000,0.7647,0.01649,0.00895,-0.0035,0.4473,1.0000 6.250,0.7864,0.01661,0.00893,-0.0021,0.3711,1.0000 6.500,0.7946,0.01991,0.01049,-0.0006,0.1294,1.0000 6.750,0.8116,0.02183,0.01218,0.0007,0.0968,1.0000 7.000,0.8297,0.02347,0.01375,0.0021,0.0842,1.0000 7.250,0.8477,0.02530,0.01541,0.0035,0.0755,1.0000 7.500,0.8696,0.02669,0.01692,0.0047,0.0688,1.0000 7.750,0.8918,0.02880,0.01891,0.0057,0.0647,1.0000 8.000,0.9157,0.03125,0.02149,0.0066,0.0621,1.0000 8.250,0.9381,0.03314,0.02369,0.0077,0.0586,1.0000 8.500,0.9598,0.03557,0.02640,0.0087,0.0567,1.0000 8.750,0.9796,0.03852,0.02977,0.0098,0.0562,1.0000 9.000,0.9956,0.04200,0.03376,0.0112,0.0568,1.0000 9.250,1.0075,0.04588,0.03815,0.0127,0.0577,1.0000 9.500,1.0151,0.04980,0.04254,0.0142,0.0580,1.0000 9.750,1.0179,0.05394,0.04713,0.0156,0.0584,1.0000 10.000,1.0164,0.05849,0.05206,0.0170,0.0596,1.0000 10.250,1.0146,0.06353,0.05734,0.0179,0.0616,1.0000 10.500,0.9852,0.06903,0.06346,0.0193,0.0679,1.0000 10.750,0.9516,0.07418,0.06885,0.0192,0.0699,1.0000 11.000,0.9243,0.08045,0.07525,0.0164,0.0721,1.0000