Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ht22-il-500000-n5 Airfoil,ht22-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,63.1935 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-ht22-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.6856,0.11242,0.11017,0.0445,1.0001,0.0073 -9.000,-0.6825,0.10860,0.10636,0.0429,1.0001,0.0072 -8.750,-0.6801,0.10453,0.10230,0.0410,1.0001,0.0070 -8.500,-0.6781,0.10032,0.09811,0.0389,1.0001,0.0069 -8.250,-0.6767,0.09597,0.09378,0.0364,1.0001,0.0068 -8.000,-0.6755,0.09149,0.08932,0.0336,1.0001,0.0068 -7.750,-0.6739,0.08662,0.08447,0.0294,1.0001,0.0067 -7.500,-0.6666,0.08072,0.07857,0.0228,1.0001,0.0067 -7.250,-0.6561,0.07407,0.07190,0.0152,1.0001,0.0067 -7.000,-0.6423,0.06654,0.06430,0.0073,1.0001,0.0068 -6.750,-0.6257,0.05833,0.05595,-0.0001,1.0001,0.0070 -6.500,-0.6070,0.04952,0.04691,-0.0062,1.0001,0.0071 -6.250,-0.5875,0.03763,0.03452,-0.0112,1.0001,0.0074 -6.000,-0.5723,0.02058,0.01594,-0.0135,1.0001,0.0079 -5.750,-0.5470,0.01834,0.01333,-0.0134,1.0001,0.0082 -5.500,-0.5209,0.01683,0.01156,-0.0133,1.0001,0.0085 -5.250,-0.4944,0.01548,0.00996,-0.0131,1.0001,0.0089 -5.000,-0.4677,0.01427,0.00851,-0.0128,1.0001,0.0095 -4.750,-0.4407,0.01323,0.00728,-0.0125,1.0001,0.0100 -4.500,-0.4136,0.01242,0.00631,-0.0123,1.0001,0.0105 -4.250,-0.3866,0.01158,0.00536,-0.0121,1.0001,0.0111 -4.000,-0.3593,0.01117,0.00494,-0.0119,1.0001,0.0121 -3.750,-0.3319,0.01076,0.00449,-0.0117,1.0001,0.0131 -3.500,-0.3044,0.01024,0.00391,-0.0115,1.0001,0.0141 -3.250,-0.2769,0.00976,0.00338,-0.0113,1.0001,0.0150 -3.000,-0.2493,0.00931,0.00292,-0.0112,1.0001,0.0166 -2.750,-0.2217,0.00903,0.00264,-0.0110,1.0001,0.0187 -2.500,-0.1940,0.00872,0.00232,-0.0108,1.0001,0.0214 -2.250,-0.1662,0.00844,0.00206,-0.0107,1.0001,0.0247 -2.000,-0.1385,0.00821,0.00182,-0.0105,1.0001,0.0287 -1.750,-0.1108,0.00799,0.00165,-0.0104,1.0001,0.0359 -1.500,-0.0797,0.00778,0.00149,-0.0110,0.9803,0.0469 -1.250,-0.0448,0.00763,0.00134,-0.0122,0.9015,0.0694 -1.000,-0.0229,0.00770,0.00123,-0.0104,0.8077,0.1029 -0.750,0.0017,0.00770,0.00113,-0.0096,0.7200,0.1724 -0.500,0.0277,0.00750,0.00105,-0.0093,0.6444,0.2987 -0.250,0.0539,0.00712,0.00100,-0.0093,0.5815,0.4794 0.000,0.0793,0.00663,0.00099,-0.0089,0.5305,0.6769 0.250,0.0982,0.00608,0.00100,-0.0064,0.4924,0.8867 0.500,0.1336,0.00612,0.00097,-0.0078,0.4516,0.9999 0.750,0.1612,0.00629,0.00097,-0.0076,0.4206,0.9999 1.250,0.2167,0.00660,0.00101,-0.0074,0.3651,0.9999 1.500,0.2445,0.00676,0.00104,-0.0073,0.3386,0.9999 1.750,0.2722,0.00693,0.00110,-0.0072,0.3122,0.9999 2.000,0.2999,0.00712,0.00116,-0.0071,0.2844,0.9999 2.250,0.3276,0.00732,0.00123,-0.0070,0.2560,0.9999 2.500,0.3553,0.00754,0.00132,-0.0069,0.2266,0.9999 2.750,0.3829,0.00777,0.00145,-0.0068,0.1997,0.9999 3.000,0.4104,0.00802,0.00158,-0.0068,0.1713,0.9999 3.250,0.4379,0.00829,0.00173,-0.0067,0.1454,0.9999 3.500,0.4654,0.00858,0.00190,-0.0066,0.1210,0.9999 3.750,0.4929,0.00886,0.00211,-0.0065,0.1005,0.9999 4.000,0.5203,0.00915,0.00232,-0.0065,0.0841,0.9999 4.250,0.5477,0.00945,0.00255,-0.0064,0.0698,0.9999 4.500,0.5750,0.00975,0.00282,-0.0063,0.0584,0.9999 4.750,0.6024,0.01002,0.00308,-0.0062,0.0512,0.9999 5.000,0.6297,0.01033,0.00338,-0.0060,0.0450,0.9999 5.250,0.6569,0.01063,0.00369,-0.0059,0.0402,0.9999 5.500,0.6840,0.01101,0.00408,-0.0058,0.0353,0.9999 5.750,0.7111,0.01132,0.00444,-0.0056,0.0329,0.9999 6.000,0.7381,0.01168,0.00483,-0.0055,0.0304,0.9999 6.250,0.7648,0.01214,0.00531,-0.0053,0.0279,0.9999 6.500,0.7914,0.01263,0.00588,-0.0051,0.0263,0.9999 6.750,0.8181,0.01302,0.00634,-0.0050,0.0250,0.9999 7.000,0.8446,0.01345,0.00683,-0.0048,0.0236,0.9999 7.250,0.8709,0.01393,0.00737,-0.0046,0.0223,0.9999 7.500,0.8968,0.01452,0.00803,-0.0044,0.0211,0.9999 7.750,0.9218,0.01539,0.00899,-0.0042,0.0197,0.9999 8.000,0.9478,0.01586,0.00957,-0.0040,0.0190,0.9999 8.250,0.9733,0.01647,0.01028,-0.0037,0.0182,0.9999 8.500,0.9985,0.01713,0.01106,-0.0035,0.0174,0.9999 8.750,1.0235,0.01779,0.01183,-0.0032,0.0166,0.9999 9.000,1.0485,0.01842,0.01254,-0.0030,0.0157,0.9999 9.250,1.0719,0.01942,0.01363,-0.0028,0.0148,0.9999 9.500,1.0954,0.02040,0.01476,-0.0025,0.0142,0.9999 9.750,1.1189,0.02131,0.01585,-0.0021,0.0137,0.9999 10.000,1.1417,0.02233,0.01706,-0.0018,0.0131,0.9999 10.250,1.1641,0.02338,0.01828,-0.0015,0.0125,0.9999 10.500,1.1865,0.02432,0.01936,-0.0012,0.0119,0.9999 10.750,1.2089,0.02517,0.02032,-0.0010,0.0114,0.9999 11.000,1.2297,0.02631,0.02157,-0.0007,0.0108,0.9999 11.250,1.2468,0.02817,0.02364,-0.0004,0.0103,0.9999 11.500,1.2643,0.02983,0.02555,0.0000,0.0100,0.9999 11.750,1.2796,0.03178,0.02778,0.0003,0.0097,0.9999 12.000,1.2925,0.03399,0.03024,0.0005,0.0094,0.9999 12.250,1.3025,0.03644,0.03294,0.0006,0.0090,0.9999 12.500,1.3092,0.03917,0.03590,0.0004,0.0088,0.9999 12.750,1.3111,0.04236,0.03933,-0.0003,0.0086,0.9999 13.000,1.2965,0.04785,0.04507,-0.0042,0.0085,0.9999 13.250,1.2447,0.06728,0.06488,-0.0239,0.0089,0.9999 13.500,1.1810,0.08528,0.08302,-0.0356,0.0094,0.9999 13.750,1.1173,0.10295,0.10077,-0.0456,0.0099,0.9999