Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh43-il-50000-n5 Airfoil,mh43-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,35.4885 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-mh43-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.5187,0.09540,0.08883,-0.0068,1.0000,0.0359 -8.500,-0.5201,0.09045,0.08397,-0.0101,1.0000,0.0348 -8.250,-0.5249,0.08457,0.07819,-0.0149,1.0000,0.0334 -7.750,-0.5309,0.07231,0.06589,-0.0258,1.0000,0.0314 -7.500,-0.5297,0.06769,0.06122,-0.0281,1.0000,0.0311 -7.250,-0.5275,0.06297,0.05640,-0.0302,1.0000,0.0308 -7.000,-0.5231,0.05829,0.05155,-0.0320,1.0000,0.0306 -6.750,-0.5162,0.05368,0.04669,-0.0333,1.0000,0.0304 -6.500,-0.5066,0.04915,0.04180,-0.0342,1.0000,0.0303 -6.250,-0.4940,0.04492,0.03716,-0.0346,1.0000,0.0303 -6.000,-0.4786,0.04094,0.03267,-0.0345,1.0000,0.0306 -5.750,-0.4605,0.03735,0.02852,-0.0341,1.0000,0.0311 -5.500,-0.4411,0.03409,0.02480,-0.0334,1.0000,0.0322 -5.250,-0.4220,0.03182,0.02239,-0.0330,1.0000,0.0362 -5.000,-0.4002,0.02967,0.01985,-0.0320,1.0000,0.0410 -4.750,-0.3774,0.02739,0.01716,-0.0307,1.0000,0.0445 -4.500,-0.3572,0.02556,0.01519,-0.0295,1.0000,0.0510 -4.250,-0.3372,0.02411,0.01365,-0.0282,1.0000,0.0651 -4.000,-0.3173,0.02256,0.01197,-0.0265,1.0000,0.0820 -3.750,-0.2976,0.02118,0.01078,-0.0255,1.0000,0.1208 -3.500,-0.2795,0.01991,0.00984,-0.0243,1.0000,0.1889 -3.250,-0.2632,0.01890,0.00926,-0.0230,1.0000,0.2819 -3.000,-0.2479,0.01803,0.00886,-0.0214,1.0000,0.3862 -2.750,-0.2342,0.01727,0.00863,-0.0189,1.0000,0.5087 -2.500,-0.2121,0.01663,0.00854,-0.0170,0.9925,0.6677 -2.250,-0.1712,0.01631,0.00836,-0.0176,0.9842,0.8436 -2.000,-0.0893,0.01614,0.00774,-0.0274,0.9844,0.9927 -1.750,-0.0455,0.01623,0.00740,-0.0314,0.9716,1.0000 -1.500,-0.0035,0.01632,0.00715,-0.0350,0.9586,1.0000 -1.250,0.0376,0.01642,0.00691,-0.0382,0.9459,1.0000 -1.000,0.0764,0.01654,0.00679,-0.0408,0.9329,1.0000 -0.750,0.1131,0.01667,0.00671,-0.0429,0.9197,1.0000 -0.500,0.1477,0.01682,0.00665,-0.0445,0.9064,1.0000 -0.250,0.1800,0.01698,0.00667,-0.0456,0.8930,1.0000 0.000,0.2103,0.01716,0.00673,-0.0462,0.8795,1.0000 0.250,0.2388,0.01736,0.00683,-0.0463,0.8659,1.0000 0.500,0.2660,0.01757,0.00696,-0.0462,0.8524,1.0000 0.750,0.2921,0.01779,0.00711,-0.0458,0.8388,1.0000 1.000,0.3174,0.01802,0.00728,-0.0452,0.8253,1.0000 1.250,0.3423,0.01825,0.00748,-0.0445,0.8118,1.0000 1.500,0.3667,0.01849,0.00770,-0.0437,0.7981,1.0000 1.750,0.3910,0.01872,0.00795,-0.0428,0.7843,1.0000 2.000,0.4151,0.01895,0.00819,-0.0418,0.7703,1.0000 2.250,0.4391,0.01918,0.00843,-0.0408,0.7561,1.0000 2.500,0.4631,0.01940,0.00868,-0.0397,0.7417,1.0000 2.750,0.4875,0.01960,0.00899,-0.0387,0.7270,1.0000 3.000,0.5119,0.01979,0.00924,-0.0376,0.7120,1.0000 3.250,0.5359,0.01999,0.00953,-0.0365,0.6960,1.0000 3.500,0.5596,0.02022,0.00985,-0.0354,0.6785,1.0000 3.750,0.5836,0.02039,0.01012,-0.0341,0.6610,1.0000 4.000,0.6079,0.02050,0.01040,-0.0328,0.6435,1.0000 4.250,0.6312,0.02071,0.01075,-0.0316,0.6222,1.0000 4.500,0.6550,0.02081,0.01096,-0.0301,0.6011,1.0000 4.750,0.6784,0.02095,0.01123,-0.0287,0.5771,1.0000 5.000,0.7014,0.02109,0.01150,-0.0272,0.5503,1.0000 5.250,0.7242,0.02125,0.01186,-0.0257,0.5204,1.0000 5.500,0.7463,0.02148,0.01221,-0.0241,0.4853,1.0000 5.750,0.7677,0.02177,0.01256,-0.0225,0.4456,1.0000 6.000,0.7882,0.02221,0.01296,-0.0209,0.4005,1.0000 6.250,0.8072,0.02287,0.01355,-0.0193,0.3488,1.0000 6.500,0.8245,0.02383,0.01434,-0.0178,0.2942,1.0000 6.750,0.8402,0.02510,0.01540,-0.0164,0.2398,1.0000 7.000,0.8549,0.02662,0.01673,-0.0152,0.1905,1.0000 7.250,0.8686,0.02836,0.01828,-0.0139,0.1503,1.0000 7.500,0.8818,0.03024,0.02001,-0.0126,0.1197,1.0000 7.750,0.8955,0.03218,0.02192,-0.0113,0.0959,1.0000 8.000,0.9086,0.03420,0.02401,-0.0100,0.0789,1.0000 8.250,0.9248,0.03637,0.02630,-0.0085,0.0678,1.0000 8.500,0.9397,0.03841,0.02852,-0.0074,0.0567,1.0000 8.750,0.9572,0.04097,0.03136,-0.0061,0.0494,1.0000 9.000,0.9741,0.04377,0.03438,-0.0049,0.0449,1.0000 9.250,0.9876,0.04716,0.03802,-0.0037,0.0411,1.0000 9.500,0.9943,0.05022,0.04158,-0.0025,0.0368,1.0000 9.750,0.9980,0.05302,0.04461,-0.0014,0.0336,1.0000 10.000,0.9997,0.05650,0.04829,-0.0003,0.0323,1.0000 10.500,0.9850,0.06443,0.05669,0.0016,0.0312,1.0000 10.750,0.9724,0.06853,0.06105,0.0015,0.0311,1.0000 11.000,0.9557,0.07335,0.06613,0.0002,0.0310,1.0000 11.250,0.9409,0.07845,0.07140,-0.0019,0.0311,1.0000 11.500,0.9251,0.08417,0.07728,-0.0050,0.0312,1.0000 11.750,0.9090,0.09055,0.08377,-0.0088,0.0314,1.0000 12.000,0.8751,0.10217,0.09570,-0.0181,0.0334,1.0000