Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca001034a08cli02-il-50000-n5 Airfoil,naca001034a08cli02-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,30.7892 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-naca001034a08cli02-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4111,0.09209,0.08559,-0.0421,1.0000,0.0419 -9.250,-0.5166,0.09266,0.08584,-0.0426,1.0000,0.0420 -9.000,-0.5197,0.08840,0.08164,-0.0438,1.0000,0.0410 -8.750,-0.5282,0.08422,0.07752,-0.0452,1.0000,0.0402 -8.500,-0.5411,0.08068,0.07403,-0.0451,1.0000,0.0396 -8.250,-0.5536,0.07724,0.07061,-0.0442,1.0000,0.0389 -8.000,-0.5648,0.07377,0.06711,-0.0431,1.0000,0.0382 -7.750,-0.5745,0.07031,0.06359,-0.0416,1.0000,0.0375 -7.500,-0.5824,0.06684,0.06001,-0.0398,1.0000,0.0367 -7.250,-0.5882,0.06334,0.05635,-0.0377,1.0000,0.0359 -7.000,-0.5914,0.05982,0.05260,-0.0355,1.0000,0.0351 -6.750,-0.5919,0.05629,0.04878,-0.0332,1.0000,0.0343 -6.500,-0.5890,0.05283,0.04497,-0.0308,1.0000,0.0335 -6.250,-0.5830,0.04947,0.04119,-0.0284,1.0000,0.0329 -6.000,-0.5739,0.04629,0.03755,-0.0260,1.0000,0.0324 -5.750,-0.5622,0.04342,0.03429,-0.0240,1.0000,0.0327 -5.500,-0.5486,0.04089,0.03145,-0.0223,1.0000,0.0344 -5.250,-0.5325,0.03850,0.02866,-0.0206,1.0000,0.0363 -5.000,-0.5137,0.03613,0.02572,-0.0189,1.0000,0.0378 -4.750,-0.4924,0.03383,0.02299,-0.0174,1.0000,0.0385 -4.500,-0.4692,0.03175,0.02054,-0.0160,1.0000,0.0395 -4.250,-0.4449,0.02995,0.01841,-0.0147,1.0000,0.0410 -4.000,-0.4212,0.02846,0.01666,-0.0133,1.0000,0.0441 -3.750,-0.3999,0.02704,0.01517,-0.0122,1.0000,0.0514 -3.500,-0.3775,0.02593,0.01374,-0.0108,1.0000,0.0565 -3.250,-0.3551,0.02465,0.01235,-0.0100,1.0000,0.0645 -3.000,-0.3328,0.02344,0.01114,-0.0093,1.0000,0.0906 -2.750,-0.2494,0.02077,0.01211,-0.0123,1.0000,0.9596 -2.500,-0.1863,0.02076,0.01138,-0.0199,1.0000,0.9862 -2.250,-0.1484,0.02056,0.01076,-0.0233,1.0000,1.0000 -2.000,-0.1463,0.02031,0.01027,-0.0198,1.0000,1.0000 -1.750,-0.1417,0.02013,0.00989,-0.0166,1.0000,1.0000 -1.500,-0.1343,0.02003,0.00958,-0.0138,1.0000,1.0000 -1.250,-0.1248,0.01999,0.00933,-0.0114,1.0000,1.0000 -1.000,-0.1131,0.02001,0.00916,-0.0093,1.0000,1.0000 -0.750,-0.0995,0.02008,0.00904,-0.0075,1.0000,1.0000 -0.500,-0.0844,0.02021,0.00896,-0.0060,1.0000,1.0000 -0.250,-0.0642,0.02040,0.00900,-0.0055,0.9986,1.0000 0.000,-0.0278,0.02076,0.00919,-0.0082,0.9918,1.0000 0.250,0.0085,0.02113,0.00943,-0.0109,0.9848,1.0000 0.500,0.0453,0.02151,0.00969,-0.0136,0.9777,1.0000 0.750,0.0798,0.02184,0.00995,-0.0158,0.9692,1.0000 1.000,0.1140,0.02218,0.01026,-0.0180,0.9606,1.0000 1.250,0.1510,0.02255,0.01062,-0.0206,0.9527,1.0000 1.500,0.1850,0.02286,0.01095,-0.0226,0.9432,1.0000 1.750,0.2179,0.02316,0.01130,-0.0243,0.9331,1.0000 2.000,0.2525,0.02346,0.01170,-0.0263,0.9233,1.0000 2.250,0.2913,0.02375,0.01210,-0.0290,0.9145,1.0000 2.500,0.3222,0.02399,0.01247,-0.0300,0.9027,1.0000 2.750,0.3537,0.02422,0.01285,-0.0312,0.8908,1.0000 3.000,0.3859,0.02443,0.01330,-0.0324,0.8788,1.0000 3.250,0.4182,0.02461,0.01369,-0.0335,0.8662,1.0000 3.500,0.4508,0.02474,0.01407,-0.0345,0.8531,1.0000 3.750,0.4837,0.02481,0.01449,-0.0354,0.8393,1.0000 4.000,0.5171,0.02481,0.01482,-0.0363,0.8248,1.0000 4.250,0.5513,0.02470,0.01508,-0.0369,0.8095,1.0000 4.500,0.5832,0.02454,0.01533,-0.0370,0.7921,1.0000 4.750,0.6116,0.02439,0.01570,-0.0363,0.7715,1.0000 5.000,0.6515,0.02116,0.01255,-0.0308,0.6384,1.0000 5.250,0.6599,0.02246,0.01173,-0.0243,0.2867,1.0000 5.500,0.6587,0.02562,0.01341,-0.0205,0.1003,1.0000 5.750,0.6718,0.02755,0.01518,-0.0181,0.0731,1.0000 6.000,0.6872,0.02913,0.01682,-0.0162,0.0572,1.0000 6.250,0.7041,0.03099,0.01875,-0.0144,0.0512,1.0000 6.500,0.7299,0.03272,0.02082,-0.0133,0.0461,1.0000 6.750,0.7573,0.03515,0.02320,-0.0133,0.0389,1.0000 7.000,0.7903,0.03751,0.02614,-0.0131,0.0362,1.0000 7.250,0.8196,0.04047,0.02954,-0.0126,0.0348,1.0000 7.500,0.8422,0.04362,0.03317,-0.0114,0.0338,1.0000 7.750,0.8586,0.04669,0.03670,-0.0095,0.0325,1.0000 8.000,0.8702,0.04965,0.04007,-0.0074,0.0307,1.0000 8.250,0.8791,0.05261,0.04333,-0.0053,0.0291,1.0000 8.500,0.8847,0.05588,0.04690,-0.0031,0.0281,1.0000 8.750,0.8868,0.05939,0.05078,-0.0006,0.0279,1.0000 9.000,0.8852,0.06293,0.05469,0.0022,0.0280,1.0000 9.250,0.8788,0.06650,0.05861,0.0050,0.0282,1.0000 9.500,0.8675,0.07009,0.06251,0.0079,0.0285,1.0000 9.750,0.8512,0.07354,0.06621,0.0107,0.0288,1.0000 10.000,0.8331,0.07735,0.07022,0.0124,0.0292,1.0000 10.250,0.8138,0.08171,0.07474,0.0128,0.0295,1.0000 10.500,0.7943,0.08676,0.07992,0.0115,0.0299,1.0000 10.750,0.7756,0.09268,0.08594,0.0086,0.0304,1.0000 11.000,0.7589,0.09956,0.09286,0.0043,0.0309,1.0000