Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m2-il-200000 Airfoil,m2-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,31.9756 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-m2-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5685,0.09901,0.09561,0.0025,1.0000,0.0643 -9.750,-0.5802,0.09328,0.08991,-0.0009,1.0000,0.0668 -9.500,-0.7164,0.09353,0.09008,0.0039,1.0000,0.0592 -9.250,-0.7127,0.09008,0.08663,0.0032,1.0000,0.0607 -9.000,-0.7188,0.08422,0.08081,-0.0020,1.0000,0.0618 -8.750,-0.7317,0.07823,0.07477,-0.0070,1.0000,0.0626 -8.500,-0.7396,0.07299,0.06943,-0.0099,1.0000,0.0644 -8.250,-0.7630,0.06890,0.06464,-0.0132,1.0000,0.0688 -8.000,-0.7615,0.06112,0.05683,-0.0139,1.0000,0.0702 -7.750,-0.7464,0.05756,0.05336,-0.0135,1.0000,0.0718 -7.500,-0.7322,0.05499,0.05076,-0.0131,1.0000,0.0752 -7.250,-0.7433,0.03798,0.03193,-0.0101,1.0000,0.0459 -7.000,-0.7283,0.03288,0.02648,-0.0091,1.0000,0.0448 -6.750,-0.7098,0.02918,0.02227,-0.0079,1.0000,0.0450 -6.500,-0.6902,0.02573,0.01833,-0.0069,1.0000,0.0469 -6.250,-0.6672,0.02373,0.01618,-0.0063,1.0000,0.0488 -6.000,-0.6428,0.02205,0.01427,-0.0057,1.0000,0.0505 -5.750,-0.6179,0.02080,0.01284,-0.0051,1.0000,0.0533 -5.500,-0.5925,0.01967,0.01150,-0.0044,1.0000,0.0559 -5.250,-0.5676,0.01823,0.00990,-0.0037,1.0000,0.0576 -5.000,-0.5435,0.01706,0.00876,-0.0031,1.0000,0.0609 -4.750,-0.5187,0.01642,0.00808,-0.0025,1.0000,0.0648 -4.500,-0.4942,0.01566,0.00724,-0.0017,1.0000,0.0680 -4.250,-0.4710,0.01473,0.00635,-0.0009,1.0000,0.0720 -4.000,-0.4469,0.01425,0.00589,-0.0001,1.0000,0.0788 -3.750,-0.4234,0.01366,0.00534,0.0007,1.0000,0.0892 -3.500,-0.4005,0.01292,0.00469,0.0016,1.0000,0.1132 -3.250,-0.3772,0.01241,0.00423,0.0023,1.0000,0.1393 -3.000,-0.3537,0.01194,0.00387,0.0030,1.0000,0.1582 -2.750,-0.3300,0.01154,0.00355,0.0036,1.0000,0.1807 -2.500,-0.3071,0.01074,0.00316,0.0041,1.0000,0.2512 -2.250,-0.2896,0.00910,0.00303,0.0054,1.0000,0.5904 -2.000,-0.2698,0.00857,0.00310,0.0076,1.0000,0.7276 -1.750,-0.2504,0.00839,0.00323,0.0102,1.0000,0.8162 -1.500,-0.2307,0.00849,0.00350,0.0131,1.0000,0.8841 -1.250,-0.2063,0.00868,0.00370,0.0147,1.0000,0.9355 -1.000,-0.1657,0.00883,0.00380,0.0126,1.0000,0.9661 -0.750,-0.1119,0.00896,0.00386,0.0073,1.0000,0.9835 -0.500,-0.0519,0.00901,0.00388,0.0006,1.0000,0.9931 -0.250,-0.0057,0.00899,0.00383,-0.0036,1.0000,1.0000 0.000,0.0000,0.00896,0.00380,0.0000,1.0000,1.0000 0.250,0.0057,0.00899,0.00383,0.0036,1.0000,1.0000 0.500,0.0520,0.00901,0.00387,-0.0006,0.9931,1.0000 0.750,0.1119,0.00896,0.00386,-0.0073,0.9835,1.0000 1.000,0.1657,0.00883,0.00380,-0.0126,0.9661,1.0000 1.250,0.2062,0.00867,0.00370,-0.0147,0.9355,1.0000 1.500,0.2308,0.00849,0.00350,-0.0132,0.8849,1.0000 1.750,0.2503,0.00838,0.00323,-0.0102,0.8160,1.0000 2.000,0.2698,0.00857,0.00310,-0.0076,0.7277,1.0000 2.250,0.2896,0.00910,0.00303,-0.0054,0.5906,1.0000 2.500,0.3071,0.01074,0.00316,-0.0041,0.2518,1.0000 2.750,0.3299,0.01154,0.00355,-0.0036,0.1807,1.0000 3.000,0.3537,0.01194,0.00387,-0.0030,0.1582,1.0000 3.250,0.3771,0.01241,0.00423,-0.0023,0.1393,1.0000 3.500,0.4005,0.01292,0.00469,-0.0016,0.1132,1.0000 3.750,0.4234,0.01365,0.00534,-0.0007,0.0893,1.0000 4.000,0.4468,0.01425,0.00589,0.0001,0.0788,1.0000 4.250,0.4710,0.01473,0.00635,0.0009,0.0720,1.0000 4.500,0.4942,0.01566,0.00724,0.0017,0.0680,1.0000 4.750,0.5187,0.01642,0.00808,0.0025,0.0648,1.0000 5.000,0.5435,0.01706,0.00876,0.0031,0.0609,1.0000 5.250,0.5676,0.01823,0.00990,0.0037,0.0576,1.0000 5.500,0.5925,0.01967,0.01150,0.0044,0.0559,1.0000 5.750,0.6179,0.02081,0.01285,0.0051,0.0533,1.0000 6.000,0.6429,0.02205,0.01427,0.0057,0.0505,1.0000 6.250,0.6672,0.02373,0.01617,0.0063,0.0488,1.0000 6.500,0.6902,0.02573,0.01833,0.0069,0.0469,1.0000 6.750,0.7098,0.02918,0.02227,0.0079,0.0450,1.0000 7.000,0.7283,0.03288,0.02648,0.0091,0.0448,1.0000 7.250,0.7434,0.03796,0.03191,0.0101,0.0459,1.0000 7.500,0.7322,0.05500,0.05078,0.0131,0.0753,1.0000 7.750,0.7465,0.05757,0.05337,0.0135,0.0718,1.0000 8.000,0.7617,0.06112,0.05683,0.0138,0.0702,1.0000 8.250,0.7631,0.06890,0.06464,0.0132,0.0688,1.0000 8.500,0.7399,0.07301,0.06945,0.0098,0.0644,1.0000 8.750,0.7321,0.07825,0.07479,0.0069,0.0626,1.0000 9.000,0.7194,0.08423,0.08082,0.0019,0.0617,1.0000