Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hor04-il-1000000-n5 Airfoil,hor04-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,70.9422 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-hor04-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5316,0.10683,0.10534,0.0228,1.0000,0.0046 -9.000,-0.5290,0.10316,0.10167,0.0217,1.0000,0.0052 -8.750,-0.6640,0.10800,0.10645,0.0349,1.0000,0.0036 -8.500,-0.6585,0.10514,0.10360,0.0336,1.0000,0.0038 -8.250,-0.6520,0.10252,0.10098,0.0322,1.0000,0.0040 -8.000,-0.6469,0.09935,0.09782,0.0304,1.0000,0.0043 -7.750,-0.6428,0.09596,0.09444,0.0284,1.0000,0.0047 -7.500,-0.6368,0.09198,0.09048,0.0251,1.0000,0.0050 -7.250,-0.6265,0.08715,0.08565,0.0201,1.0000,0.0049 -7.000,-0.6134,0.08170,0.08019,0.0138,1.0000,0.0047 -6.750,-0.5967,0.07599,0.07446,0.0069,1.0000,0.0047 -6.500,-0.5763,0.07010,0.06854,-0.0003,1.0000,0.0049 -6.250,-0.5523,0.06395,0.06232,-0.0076,1.0000,0.0055 -6.000,-0.5237,0.05757,0.05583,-0.0146,1.0000,0.0061 -5.750,-0.4931,0.05329,0.05142,-0.0189,1.0000,0.0066 -5.500,-0.4636,0.04864,0.04663,-0.0229,1.0000,0.0067 -4.750,-0.3762,0.03255,0.02988,-0.0331,1.0000,0.0062 -4.500,-0.3438,0.02769,0.02470,-0.0353,1.0000,0.0060 -4.250,-0.3105,0.02314,0.01977,-0.0370,1.0000,0.0058 -4.000,-0.2753,0.01808,0.01419,-0.0384,1.0000,0.0056 -3.750,-0.2396,0.01266,0.00806,-0.0397,1.0000,0.0059 -3.500,-0.2100,0.01155,0.00678,-0.0400,1.0000,0.0064 -3.250,-0.1812,0.01108,0.00622,-0.0403,1.0000,0.0066 -3.000,-0.1510,0.00947,0.00439,-0.0409,1.0000,0.0074 -2.750,-0.1220,0.00893,0.00380,-0.0412,1.0000,0.0079 -2.500,-0.0929,0.00849,0.00332,-0.0415,1.0000,0.0082 -2.250,-0.0639,0.00811,0.00291,-0.0418,1.0000,0.0086 -2.000,-0.0351,0.00786,0.00266,-0.0420,1.0000,0.0092 -1.750,-0.0044,0.00757,0.00232,-0.0426,0.9859,0.0096 -1.500,0.0253,0.00737,0.00205,-0.0429,0.9602,0.0098 -1.250,0.0499,0.00732,0.00190,-0.0419,0.9213,0.0103 -1.000,0.0744,0.00734,0.00176,-0.0408,0.8792,0.0114 -0.750,0.1009,0.00737,0.00167,-0.0404,0.8367,0.0189 -0.500,0.1282,0.00744,0.00159,-0.0402,0.7977,0.0217 -0.250,0.1560,0.00752,0.00154,-0.0401,0.7549,0.0277 0.000,0.1840,0.00765,0.00150,-0.0402,0.6909,0.0464 0.250,0.2136,0.00719,0.00148,-0.0411,0.6157,0.3173 0.500,0.2424,0.00694,0.00154,-0.0418,0.5725,0.4920 0.750,0.2709,0.00697,0.00157,-0.0421,0.5007,0.5776 1.000,0.2991,0.00701,0.00165,-0.0426,0.4171,0.6985 1.250,0.3220,0.00690,0.00173,-0.0417,0.2835,0.9105 1.500,0.3490,0.00723,0.00173,-0.0417,0.1728,1.0000 1.750,0.3774,0.00766,0.00189,-0.0421,0.0981,1.0000 2.000,0.4058,0.00794,0.00202,-0.0423,0.0638,1.0000 2.250,0.4341,0.00814,0.00214,-0.0424,0.0482,1.0000 2.500,0.4624,0.00833,0.00228,-0.0426,0.0390,1.0000 2.750,0.4907,0.00848,0.00242,-0.0427,0.0357,1.0000 3.000,0.5189,0.00867,0.00261,-0.0428,0.0322,1.0000 3.250,0.5471,0.00889,0.00281,-0.0429,0.0272,1.0000 3.500,0.5752,0.00904,0.00296,-0.0430,0.0256,1.0000 3.750,0.6032,0.00923,0.00315,-0.0431,0.0230,1.0000 4.000,0.6313,0.00945,0.00336,-0.0432,0.0200,1.0000 4.250,0.6593,0.00972,0.00365,-0.0433,0.0172,1.0000 4.500,0.6872,0.00990,0.00386,-0.0434,0.0145,1.0000 4.750,0.7150,0.01022,0.00414,-0.0435,0.0100,1.0000 5.000,0.7428,0.01052,0.00448,-0.0435,0.0090,1.0000 5.250,0.7705,0.01087,0.00487,-0.0436,0.0081,1.0000 5.500,0.7981,0.01125,0.00528,-0.0437,0.0074,1.0000 5.750,0.8256,0.01173,0.00585,-0.0437,0.0065,1.0000 6.000,0.8527,0.01271,0.00700,-0.0437,0.0055,1.0000 6.250,0.8798,0.01323,0.00760,-0.0436,0.0054,1.0000 6.500,0.9069,0.01366,0.00810,-0.0437,0.0051,1.0000 6.750,0.9336,0.01431,0.00886,-0.0436,0.0048,1.0000 7.000,0.9600,0.01510,0.00978,-0.0435,0.0045,1.0000 7.250,0.9862,0.01597,0.01079,-0.0434,0.0042,1.0000 7.500,1.0122,0.01682,0.01182,-0.0433,0.0040,1.0000 7.750,1.0380,0.01764,0.01276,-0.0432,0.0037,1.0000 8.000,1.0636,0.01841,0.01365,-0.0431,0.0035,1.0000 8.250,1.0886,0.01940,0.01477,-0.0430,0.0032,1.0000 8.500,1.1087,0.02299,0.01891,-0.0425,0.0027,1.0000 8.750,1.1320,0.02440,0.02053,-0.0422,0.0027,1.0000 9.000,1.1536,0.02636,0.02276,-0.0419,0.0025,1.0000 9.250,1.1718,0.02951,0.02628,-0.0414,0.0024,1.0000 10.250,0.9634,0.11368,0.11227,-0.0756,0.0027,1.0000 10.500,0.9540,0.12093,0.11950,-0.0791,0.0027,1.0000