Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ht23-il-200000-n5 Airfoil,ht23-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,50.5201 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ht23-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.6651,0.08463,0.08128,0.0194,1.0000,0.0175 -7.750,-0.6603,0.08059,0.07724,0.0163,1.0000,0.0170 -7.500,-0.6536,0.07505,0.07169,0.0109,1.0000,0.0165 -7.250,-0.6450,0.06838,0.06496,0.0045,1.0000,0.0158 -6.750,-0.6268,0.04363,0.03932,-0.0100,1.0000,0.0132 -6.500,-0.6110,0.03789,0.03311,-0.0114,1.0000,0.0131 -6.250,-0.5924,0.03258,0.02721,-0.0122,1.0000,0.0131 -6.000,-0.5708,0.02827,0.02226,-0.0123,1.0000,0.0132 -5.750,-0.5478,0.02503,0.01854,-0.0123,1.0000,0.0135 -5.500,-0.5231,0.02298,0.01620,-0.0122,1.0000,0.0140 -5.250,-0.4974,0.02186,0.01492,-0.0121,1.0000,0.0150 -5.000,-0.4711,0.02046,0.01324,-0.0118,1.0000,0.0163 -4.750,-0.4444,0.01881,0.01126,-0.0114,1.0000,0.0170 -4.500,-0.4175,0.01738,0.00959,-0.0110,1.0000,0.0175 -4.250,-0.3910,0.01604,0.00812,-0.0106,1.0000,0.0182 -4.000,-0.3646,0.01500,0.00706,-0.0103,1.0000,0.0193 -3.750,-0.3377,0.01421,0.00621,-0.0100,1.0000,0.0207 -3.500,-0.3105,0.01364,0.00557,-0.0098,1.0000,0.0234 -3.250,-0.2836,0.01287,0.00481,-0.0096,1.0000,0.0266 -3.000,-0.2563,0.01231,0.00420,-0.0093,1.0000,0.0304 -2.750,-0.2289,0.01177,0.00366,-0.0092,1.0000,0.0385 -2.500,-0.2015,0.01127,0.00320,-0.0090,1.0000,0.0535 -2.250,-0.1744,0.01068,0.00285,-0.0089,1.0000,0.0966 -2.000,-0.1476,0.01005,0.00259,-0.0089,1.0000,0.1835 -1.750,-0.1212,0.00941,0.00242,-0.0089,1.0000,0.2980 -1.500,-0.0957,0.00869,0.00230,-0.0087,1.0000,0.4458 -1.250,-0.0723,0.00791,0.00224,-0.0077,1.0000,0.6225 -1.000,-0.0479,0.00725,0.00226,-0.0060,0.9676,0.8162 -0.750,0.0051,0.00710,0.00217,-0.0101,0.8771,0.9825 -0.500,0.0335,0.00732,0.00201,-0.0094,0.7768,1.0000 -0.250,0.0569,0.00762,0.00190,-0.0079,0.6997,1.0000 0.000,0.0820,0.00789,0.00183,-0.0071,0.6406,1.0000 0.250,0.1081,0.00813,0.00179,-0.0065,0.5942,1.0000 0.500,0.1347,0.00835,0.00177,-0.0061,0.5559,1.0000 0.750,0.1616,0.00855,0.00177,-0.0058,0.5224,1.0000 1.000,0.1888,0.00874,0.00178,-0.0055,0.4928,1.0000 1.250,0.2160,0.00893,0.00181,-0.0053,0.4664,1.0000 1.500,0.2433,0.00912,0.00187,-0.0051,0.4421,1.0000 1.750,0.2708,0.00930,0.00193,-0.0049,0.4193,1.0000 2.000,0.2982,0.00950,0.00201,-0.0048,0.3985,1.0000 2.250,0.3257,0.00968,0.00211,-0.0046,0.3779,1.0000 2.500,0.3532,0.00988,0.00223,-0.0045,0.3584,1.0000 2.750,0.3807,0.01008,0.00236,-0.0043,0.3395,1.0000 3.000,0.4082,0.01028,0.00250,-0.0042,0.3203,1.0000 3.250,0.4357,0.01050,0.00266,-0.0041,0.3014,1.0000 3.500,0.4631,0.01074,0.00286,-0.0039,0.2824,1.0000 3.750,0.4906,0.01097,0.00305,-0.0038,0.2624,1.0000 4.000,0.5179,0.01124,0.00326,-0.0037,0.2417,1.0000 4.250,0.5452,0.01152,0.00349,-0.0036,0.2202,1.0000 4.750,0.5994,0.01220,0.00405,-0.0034,0.1730,1.0000 5.000,0.6264,0.01258,0.00438,-0.0034,0.1511,1.0000 5.250,0.6532,0.01300,0.00476,-0.0033,0.1303,1.0000 5.500,0.6800,0.01346,0.00517,-0.0032,0.1094,1.0000 5.750,0.7065,0.01399,0.00564,-0.0031,0.0901,1.0000 6.000,0.7328,0.01456,0.00619,-0.0030,0.0748,1.0000 6.250,0.7590,0.01518,0.00681,-0.0029,0.0624,1.0000 6.500,0.7851,0.01581,0.00747,-0.0027,0.0537,1.0000 6.750,0.8109,0.01649,0.00823,-0.0025,0.0482,1.0000 7.000,0.8365,0.01720,0.00900,-0.0023,0.0433,1.0000 7.250,0.8616,0.01803,0.00993,-0.0021,0.0395,1.0000 7.500,0.8867,0.01880,0.01084,-0.0018,0.0366,1.0000 7.750,0.9113,0.01966,0.01180,-0.0016,0.0342,1.0000 8.000,0.9341,0.02095,0.01312,-0.0013,0.0317,1.0000 8.250,0.9585,0.02180,0.01418,-0.0009,0.0299,1.0000 8.500,0.9819,0.02287,0.01542,-0.0006,0.0282,1.0000 8.750,1.0047,0.02403,0.01673,-0.0002,0.0268,1.0000 9.000,1.0268,0.02525,0.01807,0.0002,0.0255,1.0000 9.250,1.0461,0.02711,0.02003,0.0006,0.0241,1.0000 9.500,1.0675,0.02843,0.02165,0.0010,0.0230,1.0000 9.750,1.0870,0.03012,0.02361,0.0015,0.0219,1.0000 10.000,1.1049,0.03204,0.02581,0.0020,0.0210,1.0000 10.250,1.1213,0.03406,0.02809,0.0024,0.0203,1.0000 10.500,1.1367,0.03600,0.03025,0.0028,0.0195,1.0000 10.750,1.1507,0.03786,0.03227,0.0030,0.0188,1.0000 11.000,1.1593,0.04053,0.03511,0.0033,0.0181,1.0000 11.250,1.1624,0.04380,0.03876,0.0034,0.0177,1.0000 11.500,1.1594,0.04748,0.04282,0.0029,0.0173,1.0000 11.750,1.1465,0.05190,0.04752,0.0013,0.0171,1.0000 12.000,1.1307,0.05862,0.05451,-0.0051,0.0171,1.0000 12.250,1.1121,0.06724,0.06336,-0.0132,0.0172,1.0000 12.500,1.0891,0.07687,0.07313,-0.0211,0.0173,1.0000 12.750,1.0625,0.08716,0.08354,-0.0284,0.0176,1.0000 13.000,1.0329,0.09814,0.09459,-0.0353,0.0179,1.0000