Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh60-il-50000 Airfoil,mh60-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,27.5498 Max Cl/Cd alpha,7 Url,http://www.airfoiltools.com/polar/csv?polar=xf-mh60-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4834,0.10057,0.09461,0.0149,1.0000,0.2722 -8.000,-0.4850,0.09725,0.09138,0.0134,1.0000,0.2811 -7.750,-0.4997,0.09547,0.08975,0.0111,1.0000,0.2926 -7.500,-0.4756,0.08976,0.08402,0.0115,1.0000,0.2965 -7.250,-0.4710,0.08598,0.08031,0.0102,1.0000,0.3010 -7.000,-0.5492,0.06228,0.05594,-0.0280,1.0000,0.1091 -6.750,-0.5327,0.05773,0.05145,-0.0281,1.0000,0.1066 -6.500,-0.5231,0.05268,0.04617,-0.0293,1.0000,0.1033 -6.250,-0.5192,0.04662,0.03903,-0.0305,1.0000,0.0954 -6.000,-0.5046,0.04279,0.03479,-0.0300,1.0000,0.0954 -5.750,-0.4898,0.03933,0.03086,-0.0289,1.0000,0.0956 -5.500,-0.4755,0.03623,0.02740,-0.0272,1.0000,0.0959 -5.250,-0.4618,0.03338,0.02440,-0.0253,1.0000,0.0981 -5.000,-0.4480,0.03146,0.02232,-0.0232,1.0000,0.1052 -4.750,-0.4333,0.02942,0.02002,-0.0211,1.0000,0.1131 -4.500,-0.4161,0.02747,0.01783,-0.0190,1.0000,0.1248 -4.250,-0.3996,0.02587,0.01629,-0.0171,1.0000,0.1465 -4.000,-0.3827,0.02421,0.01476,-0.0151,1.0000,0.1837 -3.750,-0.3671,0.02233,0.01343,-0.0128,1.0000,0.2706 -3.500,-0.3574,0.02105,0.01288,-0.0094,1.0000,0.3994 -3.250,-0.3475,0.02043,0.01267,-0.0057,1.0000,0.4970 -3.000,-0.3358,0.01987,0.01246,-0.0020,1.0000,0.5836 -2.750,-0.3236,0.01929,0.01223,0.0020,1.0000,0.6723 -2.500,-0.3098,0.01872,0.01206,0.0065,1.0000,0.7817 -2.250,-0.1308,0.01871,0.01125,-0.0195,1.0000,1.0000 -2.000,-0.1454,0.01845,0.01073,-0.0156,1.0000,1.0000 -1.750,-0.1420,0.01853,0.01050,-0.0134,1.0000,1.0000 -1.500,-0.1331,0.01872,0.01038,-0.0118,1.0000,1.0000 -1.250,-0.1216,0.01900,0.01038,-0.0104,1.0000,1.0000 -1.000,-0.1086,0.01933,0.01047,-0.0094,1.0000,1.0000 -0.750,-0.0848,0.01982,0.01073,-0.0104,0.9964,1.0000 -0.500,-0.0281,0.02077,0.01137,-0.0173,0.9811,1.0000 -0.250,0.0239,0.02163,0.01202,-0.0232,0.9648,1.0000 0.000,0.0757,0.02247,0.01269,-0.0289,0.9480,1.0000 0.250,0.1287,0.02329,0.01336,-0.0345,0.9311,1.0000 0.500,0.1823,0.02405,0.01403,-0.0400,0.9141,1.0000 0.750,0.2233,0.02473,0.01465,-0.0431,0.8955,1.0000 1.000,0.2712,0.02536,0.01525,-0.0471,0.8772,1.0000 1.250,0.3188,0.02591,0.01580,-0.0505,0.8596,1.0000 1.500,0.3465,0.02658,0.01645,-0.0506,0.8402,1.0000 1.750,0.3781,0.02715,0.01702,-0.0511,0.8212,1.0000 2.000,0.4126,0.02758,0.01747,-0.0514,0.8034,1.0000 2.250,0.4345,0.02822,0.01812,-0.0502,0.7838,1.0000 2.500,0.4593,0.02874,0.01868,-0.0491,0.7647,1.0000 2.750,0.4869,0.02906,0.01902,-0.0479,0.7471,1.0000 3.000,0.5089,0.02955,0.01955,-0.0462,0.7282,1.0000 3.250,0.5301,0.03004,0.02007,-0.0445,0.7087,1.0000 3.500,0.5552,0.03021,0.02032,-0.0426,0.6909,1.0000 3.750,0.5808,0.03022,0.02038,-0.0404,0.6742,1.0000 4.000,0.5991,0.03086,0.02109,-0.0387,0.6529,1.0000 4.250,0.6234,0.03088,0.02116,-0.0364,0.6348,1.0000 4.500,0.6491,0.03064,0.02100,-0.0339,0.6179,1.0000 4.750,0.6689,0.03115,0.02160,-0.0322,0.5964,1.0000 5.000,0.6940,0.03092,0.02143,-0.0297,0.5778,1.0000 5.250,0.7186,0.03075,0.02134,-0.0273,0.5588,1.0000 5.500,0.7409,0.03096,0.02164,-0.0253,0.5371,1.0000 5.750,0.7679,0.03043,0.02111,-0.0226,0.5183,1.0000 6.000,0.7889,0.03102,0.02181,-0.0210,0.4947,1.0000 6.250,0.8136,0.03100,0.02180,-0.0188,0.4732,1.0000 6.500,0.8369,0.03136,0.02225,-0.0170,0.4503,1.0000 6.750,0.8590,0.03197,0.02292,-0.0154,0.4268,1.0000 7.000,0.8849,0.03212,0.02299,-0.0134,0.4050,1.0000 7.250,0.9042,0.03331,0.02434,-0.0122,0.3810,1.0000 7.500,0.9263,0.03419,0.02525,-0.0107,0.3590,1.0000 7.750,0.9479,0.03519,0.02636,-0.0093,0.3369,1.0000 8.000,0.9673,0.03652,0.02780,-0.0080,0.3156,1.0000 8.250,0.9877,0.03780,0.02916,-0.0067,0.2951,1.0000 8.500,1.0070,0.03918,0.03060,-0.0053,0.2750,1.0000 8.750,1.0222,0.04113,0.03277,-0.0041,0.2562,1.0000 9.000,1.0465,0.04193,0.03338,-0.0026,0.2354,1.0000 9.250,1.0566,0.04455,0.03633,-0.0013,0.2193,1.0000 9.500,1.0657,0.04696,0.03904,0.0001,0.2026,1.0000 9.750,1.0744,0.04960,0.04188,0.0015,0.1879,1.0000 10.000,1.0806,0.05241,0.04487,0.0029,0.1745,1.0000 10.250,1.0852,0.05518,0.04780,0.0043,0.1620,1.0000 10.500,1.0937,0.05820,0.05088,0.0055,0.1512,1.0000 10.750,1.0705,0.06342,0.05650,0.0064,0.1498,1.0000 11.000,1.0431,0.06874,0.06203,0.0067,0.1502,1.0000 11.250,1.0139,0.07463,0.06801,0.0058,0.1514,1.0000 11.500,0.9867,0.08154,0.07495,0.0034,0.1527,1.0000