Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m2-il-200000-n5 Airfoil,m2-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,36.8106 Max Cl/Cd alpha,5.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-m2-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.7792,0.08418,0.08082,0.0020,1.0000,0.0158 -10.000,-0.8379,0.06515,0.06167,-0.0136,1.0000,0.0149 -9.750,-0.8940,0.05106,0.04707,-0.0150,1.0000,0.0146 -9.500,-0.9019,0.04549,0.04111,-0.0142,1.0000,0.0149 -9.250,-0.9011,0.04091,0.03610,-0.0131,1.0000,0.0153 -9.000,-0.8947,0.03692,0.03165,-0.0118,1.0000,0.0160 -8.750,-0.8841,0.03331,0.02755,-0.0106,1.0000,0.0169 -8.500,-0.8688,0.03045,0.02419,-0.0095,1.0000,0.0183 -8.250,-0.8492,0.02852,0.02181,-0.0086,1.0000,0.0197 -8.000,-0.8309,0.02630,0.01936,-0.0078,1.0000,0.0210 -7.750,-0.8090,0.02514,0.01808,-0.0073,1.0000,0.0223 -7.500,-0.7862,0.02402,0.01674,-0.0068,1.0000,0.0242 -7.250,-0.7627,0.02295,0.01543,-0.0062,1.0000,0.0267 -7.000,-0.7384,0.02200,0.01422,-0.0057,1.0000,0.0284 -6.750,-0.7161,0.02029,0.01236,-0.0051,1.0000,0.0307 -6.500,-0.6923,0.01944,0.01146,-0.0047,1.0000,0.0332 -6.250,-0.6680,0.01859,0.01047,-0.0042,1.0000,0.0354 -6.000,-0.6433,0.01786,0.00961,-0.0037,1.0000,0.0377 -5.750,-0.6186,0.01721,0.00882,-0.0032,1.0000,0.0393 -5.500,-0.5953,0.01621,0.00778,-0.0025,1.0000,0.0411 -5.250,-0.5713,0.01552,0.00709,-0.0020,1.0000,0.0438 -5.000,-0.5469,0.01497,0.00647,-0.0015,1.0000,0.0463 -4.750,-0.5225,0.01445,0.00588,-0.0009,1.0000,0.0484 -4.500,-0.4981,0.01399,0.00535,-0.0003,1.0000,0.0506 -4.250,-0.4740,0.01352,0.00490,0.0003,1.0000,0.0545 -4.000,-0.4497,0.01314,0.00453,0.0009,1.0000,0.0609 -3.750,-0.4255,0.01281,0.00425,0.0016,1.0000,0.0733 -3.500,-0.4011,0.01257,0.00403,0.0022,1.0000,0.0895 -3.250,-0.3768,0.01235,0.00381,0.0028,1.0000,0.1037 -3.000,-0.3526,0.01209,0.00359,0.0033,1.0000,0.1151 -2.750,-0.3284,0.01186,0.00338,0.0039,1.0000,0.1246 -2.500,-0.3040,0.01167,0.00320,0.0045,1.0000,0.1344 -2.250,-0.2799,0.01141,0.00302,0.0050,1.0000,0.1520 -2.000,-0.2557,0.01111,0.00286,0.0055,1.0000,0.1825 -1.750,-0.2315,0.00997,0.00265,0.0053,0.9991,0.4068 -1.500,-0.1971,0.00935,0.00257,0.0035,0.9943,0.5324 -1.250,-0.1626,0.00876,0.00259,0.0021,0.9876,0.6650 -1.000,-0.1280,0.00844,0.00264,0.0011,0.9790,0.7590 -0.750,-0.0937,0.00831,0.00272,0.0003,0.9676,0.8165 -0.500,-0.0608,0.00830,0.00283,0.0000,0.9540,0.8626 -0.250,-0.0293,0.00833,0.00290,-0.0002,0.9394,0.8969 0.000,0.0000,0.00834,0.00291,0.0000,0.9209,0.9209 0.250,0.0293,0.00833,0.00290,0.0002,0.8969,0.9394 0.500,0.0609,0.00830,0.00283,0.0000,0.8629,0.9540 0.750,0.0937,0.00831,0.00272,-0.0003,0.8165,0.9676 1.000,0.1280,0.00844,0.00264,-0.0011,0.7591,0.9790 1.250,0.1628,0.00876,0.00259,-0.0021,0.6650,0.9877 1.500,0.1972,0.00935,0.00257,-0.0035,0.5329,0.9944 1.750,0.2315,0.00997,0.00265,-0.0053,0.4069,0.9991 2.000,0.2557,0.01111,0.00286,-0.0055,0.1823,1.0000 2.250,0.2798,0.01141,0.00302,-0.0050,0.1521,1.0000 2.500,0.3040,0.01167,0.00320,-0.0045,0.1344,1.0000 2.750,0.3283,0.01186,0.00338,-0.0039,0.1246,1.0000 3.000,0.3526,0.01209,0.00359,-0.0033,0.1151,1.0000 3.250,0.3767,0.01235,0.00381,-0.0027,0.1038,1.0000 3.500,0.4010,0.01257,0.00403,-0.0021,0.0896,1.0000 3.750,0.4254,0.01281,0.00425,-0.0015,0.0732,1.0000 4.000,0.4496,0.01314,0.00453,-0.0009,0.0609,1.0000 4.250,0.4739,0.01352,0.00490,-0.0003,0.0545,1.0000 4.500,0.4981,0.01399,0.00535,0.0003,0.0506,1.0000 4.750,0.5225,0.01445,0.00588,0.0009,0.0484,1.0000 5.000,0.5469,0.01497,0.00647,0.0015,0.0463,1.0000 5.250,0.5713,0.01552,0.00709,0.0020,0.0438,1.0000 5.500,0.5953,0.01621,0.00778,0.0025,0.0411,1.0000 5.750,0.6186,0.01721,0.00882,0.0032,0.0393,1.0000 6.000,0.6434,0.01786,0.00961,0.0037,0.0377,1.0000 6.250,0.6680,0.01859,0.01047,0.0042,0.0354,1.0000 6.500,0.6923,0.01944,0.01146,0.0047,0.0332,1.0000 6.750,0.7162,0.02029,0.01236,0.0051,0.0307,1.0000 7.000,0.7385,0.02200,0.01422,0.0057,0.0284,1.0000 7.250,0.7628,0.02295,0.01543,0.0062,0.0267,1.0000 7.500,0.7863,0.02402,0.01675,0.0068,0.0242,1.0000 7.750,0.8091,0.02514,0.01808,0.0073,0.0223,1.0000 8.000,0.8311,0.02630,0.01937,0.0078,0.0210,1.0000 8.250,0.8493,0.02854,0.02183,0.0085,0.0197,1.0000 8.500,0.8689,0.03046,0.02421,0.0094,0.0183,1.0000 8.750,0.8843,0.03332,0.02756,0.0105,0.0169,1.0000 9.000,0.8948,0.03694,0.03167,0.0118,0.0160,1.0000 9.250,0.9013,0.04093,0.03612,0.0130,0.0153,1.0000 9.500,0.9020,0.04552,0.04114,0.0141,0.0149,1.0000 9.750,0.8942,0.05111,0.04712,0.0149,0.0146,1.0000 10.000,0.8377,0.06531,0.06183,0.0135,0.0149,1.0000 10.250,0.7796,0.08434,0.08098,-0.0023,0.0158,1.0000