Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ht22-il-1000000 Airfoil,ht22-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,75.4573 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-ht22-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.5589,0.07998,0.07852,0.0224,1.0001,0.0106 -7.750,-0.5620,0.07527,0.07382,0.0205,1.0001,0.0106 -7.500,-0.5662,0.07050,0.06907,0.0181,1.0001,0.0106 -7.250,-0.5686,0.06508,0.06366,0.0135,1.0001,0.0107 -7.000,-0.5651,0.05870,0.05725,0.0075,1.0001,0.0107 -6.750,-0.5583,0.05165,0.05014,0.0016,1.0001,0.0107 -6.500,-0.5484,0.04437,0.04277,-0.0034,1.0001,0.0107 -6.250,-0.5364,0.03671,0.03497,-0.0075,1.0001,0.0107 -6.000,-0.5294,0.02812,0.02616,-0.0113,1.0001,0.0114 -5.750,-0.5104,0.02464,0.02256,-0.0124,1.0001,0.0118 -5.500,-0.5184,0.02527,0.02211,-0.0132,1.0001,0.0114 -5.250,-0.4955,0.01733,0.01331,-0.0130,1.0001,0.0097 -5.000,-0.4691,0.01492,0.01050,-0.0128,1.0001,0.0101 -4.750,-0.4423,0.01314,0.00842,-0.0124,1.0001,0.0104 -4.500,-0.4147,0.01236,0.00749,-0.0122,1.0001,0.0107 -4.250,-0.3884,0.01036,0.00525,-0.0119,1.0001,0.0116 -4.000,-0.3609,0.00989,0.00475,-0.0117,1.0001,0.0123 -3.750,-0.3333,0.00941,0.00422,-0.0115,1.0001,0.0130 -3.500,-0.3056,0.00893,0.00370,-0.0113,1.0001,0.0138 -3.250,-0.2777,0.00868,0.00343,-0.0112,1.0001,0.0146 -3.000,-0.2502,0.00795,0.00265,-0.0110,1.0001,0.0167 -2.750,-0.2223,0.00767,0.00237,-0.0109,1.0001,0.0184 -2.500,-0.1943,0.00745,0.00213,-0.0107,1.0001,0.0199 -2.250,-0.1663,0.00703,0.00170,-0.0106,1.0001,0.0237 -2.000,-0.1384,0.00689,0.00158,-0.0104,1.0001,0.0271 -1.750,-0.1104,0.00660,0.00131,-0.0103,1.0001,0.0349 -1.500,-0.0824,0.00638,0.00115,-0.0102,1.0001,0.0464 -1.250,-0.0546,0.00616,0.00104,-0.0100,1.0001,0.0718 -1.000,-0.0223,0.00582,0.00094,-0.0111,0.9837,0.1378 -0.750,0.0072,0.00543,0.00086,-0.0113,0.8995,0.2808 -0.500,0.0292,0.00517,0.00080,-0.0099,0.7991,0.4593 -0.250,0.0537,0.00474,0.00077,-0.0094,0.7052,0.6899 0.000,0.0725,0.00427,0.00078,-0.0070,0.6294,0.9146 0.250,0.1059,0.00442,0.00073,-0.0079,0.5594,0.9999 0.500,0.1336,0.00463,0.00073,-0.0078,0.5074,0.9999 0.750,0.1614,0.00482,0.00073,-0.0077,0.4651,0.9999 1.000,0.1893,0.00498,0.00075,-0.0076,0.4299,0.9999 1.250,0.2172,0.00514,0.00077,-0.0076,0.3990,0.9999 1.500,0.2452,0.00529,0.00080,-0.0075,0.3702,0.9999 1.750,0.2731,0.00545,0.00084,-0.0074,0.3422,0.9999 2.000,0.3010,0.00561,0.00089,-0.0073,0.3141,0.9999 2.250,0.3289,0.00578,0.00095,-0.0073,0.2883,0.9999 2.500,0.3568,0.00597,0.00103,-0.0072,0.2587,0.9999 2.750,0.3846,0.00617,0.00112,-0.0072,0.2291,0.9999 3.000,0.4123,0.00641,0.00123,-0.0071,0.1970,0.9999 3.250,0.4401,0.00665,0.00135,-0.0071,0.1693,0.9999 3.500,0.4677,0.00692,0.00149,-0.0070,0.1410,0.9999 3.750,0.4954,0.00719,0.00166,-0.0070,0.1156,0.9999 4.000,0.5230,0.00747,0.00184,-0.0069,0.0947,0.9999 4.250,0.5505,0.00774,0.00203,-0.0068,0.0774,0.9999 4.500,0.5781,0.00802,0.00225,-0.0068,0.0633,0.9999 4.750,0.6056,0.00830,0.00249,-0.0067,0.0527,0.9999 5.000,0.6331,0.00860,0.00276,-0.0066,0.0447,0.9999 5.250,0.6605,0.00890,0.00303,-0.0064,0.0392,0.9999 5.500,0.6878,0.00926,0.00343,-0.0063,0.0350,0.9999 5.750,0.7153,0.00951,0.00371,-0.0062,0.0329,0.9999 6.000,0.7425,0.00984,0.00404,-0.0061,0.0301,0.9999 6.250,0.7690,0.01052,0.00480,-0.0059,0.0268,0.9999 6.500,0.7962,0.01078,0.00511,-0.0057,0.0262,0.9999 6.750,0.8232,0.01112,0.00550,-0.0055,0.0252,0.9999 7.000,0.8501,0.01147,0.00589,-0.0054,0.0238,0.9999 7.250,0.8768,0.01183,0.00627,-0.0052,0.0225,0.9999 7.500,0.9028,0.01248,0.00698,-0.0050,0.0210,0.9999 7.750,0.9272,0.01368,0.00834,-0.0047,0.0197,0.9999 8.000,0.9538,0.01399,0.00870,-0.0045,0.0193,0.9999 8.250,0.9802,0.01432,0.00909,-0.0043,0.0185,0.9999 8.500,1.0062,0.01478,0.00962,-0.0041,0.0176,0.9999 8.750,1.0320,0.01526,0.01016,-0.0039,0.0168,0.9999 9.000,1.0574,0.01579,0.01074,-0.0037,0.0160,0.9999 9.250,1.0798,0.01724,0.01232,-0.0033,0.0149,0.9999 9.500,1.1029,0.01842,0.01368,-0.0030,0.0143,0.9999 9.750,1.1285,0.01876,0.01409,-0.0028,0.0138,0.9999 10.000,1.1531,0.01937,0.01481,-0.0025,0.0132,0.9999 10.250,1.1772,0.02005,0.01558,-0.0022,0.0126,0.9999 10.500,1.2012,0.02068,0.01629,-0.0020,0.0120,0.9999 10.750,1.2249,0.02134,0.01701,-0.0017,0.0115,0.9999 11.000,1.2450,0.02281,0.01861,-0.0014,0.0109,0.9999 11.250,1.2596,0.02542,0.02153,-0.0008,0.0103,0.9999 11.500,1.2826,0.02601,0.02224,-0.0005,0.0100,0.9999 11.750,1.3036,0.02698,0.02334,-0.0002,0.0097,0.9999 12.000,1.3225,0.02827,0.02479,0.0001,0.0093,0.9999 12.250,1.3406,0.02959,0.02624,0.0005,0.0089,0.9999 12.500,1.3584,0.03085,0.02762,0.0008,0.0086,0.9999 12.750,1.3753,0.03214,0.02901,0.0010,0.0083,0.9999 13.000,1.3893,0.03378,0.03077,0.0013,0.0081,0.9999 13.250,1.3946,0.03653,0.03370,0.0013,0.0078,0.9999 13.500,1.3841,0.04089,0.03830,0.0008,0.0076,0.9999 13.750,1.3658,0.04841,0.04608,-0.0070,0.0077,0.9999 14.000,1.3418,0.06126,0.05917,-0.0198,0.0078,0.9999