Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m2-il-500000-n5 Airfoil,m2-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,54.3659 Max Cl/Cd alpha,8 Url,http://airfoiltools.com/polar/csv?polar=xf-m2-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.000,-1.1224,0.05222,0.04966,-0.0173,1.0000,0.0057 -12.750,-1.1497,0.04597,0.04313,-0.0186,1.0000,0.0057 -12.500,-1.1677,0.04185,0.03875,-0.0169,1.0000,0.0057 -12.250,-1.1749,0.03847,0.03508,-0.0149,1.0000,0.0058 -12.000,-1.1738,0.03547,0.03180,-0.0134,1.0000,0.0059 -11.750,-1.1673,0.03291,0.02896,-0.0120,1.0000,0.0061 -11.500,-1.1565,0.03074,0.02652,-0.0108,1.0000,0.0063 -11.250,-1.1424,0.02892,0.02440,-0.0098,1.0000,0.0065 -11.000,-1.1283,0.02699,0.02224,-0.0087,1.0000,0.0067 -10.750,-1.1116,0.02541,0.02048,-0.0078,1.0000,0.0071 -10.500,-1.0919,0.02423,0.01915,-0.0072,1.0000,0.0074 -10.250,-1.0713,0.02313,0.01790,-0.0066,1.0000,0.0078 -10.000,-1.0502,0.02204,0.01665,-0.0060,1.0000,0.0082 -9.750,-1.0286,0.02098,0.01543,-0.0054,1.0000,0.0086 -9.500,-1.0063,0.02000,0.01427,-0.0049,1.0000,0.0090 -9.250,-0.9835,0.01907,0.01319,-0.0044,1.0000,0.0095 -9.000,-0.9607,0.01813,0.01213,-0.0039,1.0000,0.0104 -8.750,-0.9360,0.01758,0.01153,-0.0036,1.0000,0.0113 -8.500,-0.9111,0.01706,0.01094,-0.0034,1.0000,0.0123 -8.250,-0.8863,0.01647,0.01025,-0.0031,1.0000,0.0133 -8.000,-0.8615,0.01584,0.00958,-0.0028,1.0000,0.0147 -7.750,-0.8355,0.01552,0.00925,-0.0026,1.0000,0.0161 -7.500,-0.8095,0.01520,0.00888,-0.0025,1.0000,0.0178 -7.250,-0.7831,0.01493,0.00853,-0.0024,1.0000,0.0193 -7.000,-0.7578,0.01442,0.00795,-0.0021,1.0000,0.0206 -6.750,-0.7323,0.01395,0.00745,-0.0019,1.0000,0.0223 -6.500,-0.7062,0.01364,0.00712,-0.0017,1.0000,0.0240 -6.250,-0.6801,0.01331,0.00674,-0.0016,1.0000,0.0257 -6.000,-0.6542,0.01297,0.00633,-0.0013,1.0000,0.0271 -5.750,-0.6281,0.01269,0.00600,-0.0011,1.0000,0.0281 -5.500,-0.6022,0.01242,0.00569,-0.0008,1.0000,0.0287 -5.250,-0.5777,0.01186,0.00508,-0.0003,1.0000,0.0301 -5.000,-0.5533,0.01137,0.00454,0.0002,1.0000,0.0318 -4.750,-0.5288,0.01101,0.00416,0.0008,1.0000,0.0333 -4.500,-0.5045,0.01071,0.00384,0.0014,1.0000,0.0349 -4.250,-0.4803,0.01045,0.00355,0.0021,1.0000,0.0361 -4.000,-0.4560,0.01022,0.00328,0.0027,1.0000,0.0373 -3.750,-0.4248,0.01000,0.00302,0.0019,0.9978,0.0385 -3.500,-0.3880,0.00977,0.00278,-0.0002,0.9946,0.0405 -3.250,-0.3532,0.00951,0.00254,-0.0018,0.9893,0.0462 -3.000,-0.3189,0.00921,0.00238,-0.0034,0.9847,0.0687 -2.750,-0.2872,0.00904,0.00227,-0.0043,0.9786,0.0859 -2.500,-0.2553,0.00889,0.00215,-0.0052,0.9705,0.0949 -2.250,-0.2255,0.00879,0.00206,-0.0056,0.9606,0.1030 -2.000,-0.1981,0.00865,0.00196,-0.0054,0.9500,0.1126 -1.750,-0.1716,0.00854,0.00186,-0.0050,0.9386,0.1193 -1.500,-0.1457,0.00840,0.00176,-0.0045,0.9237,0.1302 -1.250,-0.1199,0.00823,0.00166,-0.0039,0.9050,0.1494 -1.000,-0.0961,0.00764,0.00145,-0.0032,0.8783,0.2706 -0.750,-0.0740,0.00705,0.00129,-0.0021,0.8371,0.4333 -0.500,-0.0499,0.00688,0.00120,-0.0012,0.7899,0.5057 -0.250,-0.0246,0.00661,0.00116,-0.0007,0.7516,0.6024 0.000,0.0000,0.00643,0.00116,0.0000,0.6973,0.6972 0.250,0.0246,0.00661,0.00116,0.0007,0.6024,0.7517 0.500,0.0500,0.00687,0.00120,0.0012,0.5069,0.7898 0.750,0.0741,0.00705,0.00129,0.0021,0.4332,0.8372 1.000,0.0961,0.00764,0.00145,0.0032,0.2691,0.8785 1.250,0.1199,0.00823,0.00166,0.0039,0.1498,0.9051 1.500,0.1457,0.00840,0.00176,0.0045,0.1304,0.9238 1.750,0.1717,0.00854,0.00186,0.0050,0.1194,0.9387 2.000,0.1982,0.00865,0.00196,0.0054,0.1126,0.9499 2.250,0.2256,0.00879,0.00206,0.0056,0.1030,0.9606 2.500,0.2553,0.00889,0.00215,0.0052,0.0949,0.9707 2.750,0.2873,0.00904,0.00227,0.0043,0.0860,0.9788 3.000,0.3190,0.00921,0.00238,0.0034,0.0689,0.9847 3.250,0.3532,0.00951,0.00254,0.0018,0.0462,0.9893 3.500,0.3880,0.00977,0.00278,0.0002,0.0405,0.9946 3.750,0.4248,0.01000,0.00302,-0.0019,0.0385,0.9978 4.000,0.4559,0.01022,0.00328,-0.0027,0.0373,1.0000 4.250,0.4802,0.01045,0.00355,-0.0021,0.0361,1.0000 4.500,0.5044,0.01071,0.00384,-0.0014,0.0349,1.0000 4.750,0.5287,0.01101,0.00416,-0.0008,0.0333,1.0000 5.000,0.5533,0.01137,0.00454,-0.0002,0.0318,1.0000 5.250,0.5777,0.01187,0.00508,0.0003,0.0300,1.0000 5.500,0.6022,0.01242,0.00569,0.0008,0.0287,1.0000 5.750,0.6282,0.01269,0.00600,0.0011,0.0281,1.0000 6.000,0.6542,0.01297,0.00633,0.0013,0.0271,1.0000 6.250,0.6802,0.01331,0.00674,0.0015,0.0257,1.0000 6.500,0.7062,0.01364,0.00712,0.0017,0.0240,1.0000 6.750,0.7324,0.01395,0.00745,0.0019,0.0223,1.0000 7.000,0.7578,0.01443,0.00795,0.0021,0.0206,1.0000 7.250,0.7832,0.01493,0.00853,0.0023,0.0193,1.0000 7.500,0.8095,0.01521,0.00889,0.0025,0.0178,1.0000 7.750,0.8357,0.01552,0.00925,0.0026,0.0161,1.0000 8.000,0.8617,0.01585,0.00958,0.0027,0.0147,1.0000 8.250,0.8864,0.01648,0.01025,0.0030,0.0133,1.0000 8.500,0.9112,0.01706,0.01094,0.0034,0.0123,1.0000 8.750,0.9361,0.01759,0.01154,0.0036,0.0113,1.0000 9.000,0.9608,0.01813,0.01213,0.0038,0.0104,1.0000 9.250,0.9837,0.01907,0.01319,0.0043,0.0094,1.0000 9.500,1.0065,0.02000,0.01427,0.0048,0.0090,1.0000 9.750,1.0288,0.02099,0.01543,0.0054,0.0086,1.0000 10.000,1.0504,0.02204,0.01665,0.0059,0.0082,1.0000 10.250,1.0715,0.02313,0.01790,0.0065,0.0078,1.0000 10.500,1.0921,0.02424,0.01916,0.0071,0.0074,1.0000 10.750,1.1118,0.02541,0.02048,0.0078,0.0071,1.0000 11.000,1.1285,0.02700,0.02225,0.0087,0.0067,1.0000 11.250,1.1427,0.02892,0.02441,0.0097,0.0065,1.0000 11.500,1.1568,0.03075,0.02652,0.0107,0.0063,1.0000 11.750,1.1677,0.03292,0.02896,0.0119,0.0061,1.0000 12.000,1.1742,0.03548,0.03180,0.0133,0.0059,1.0000 12.250,1.1753,0.03849,0.03511,0.0148,0.0058,1.0000 12.500,1.1682,0.04188,0.03878,0.0168,0.0057,1.0000 12.750,1.1502,0.04601,0.04317,0.0185,0.0057,1.0000 13.000,1.1226,0.05233,0.04977,0.0171,0.0057,1.0000