Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hh02-il-500000-n5 Airfoil,hh02-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,72.1802 Max Cl/Cd alpha,7.25 Url,http://airfoiltools.com/polar/csv?polar=xf-hh02-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.7228,0.11757,0.11534,0.0623,0.8097,0.0076 -9.750,-0.7295,0.11097,0.10874,0.0593,0.8078,0.0077 -8.750,-0.9145,0.03054,0.02642,0.0111,0.7995,0.0077 -8.500,-0.8987,0.02698,0.02238,0.0115,0.7967,0.0080 -8.250,-0.8762,0.02555,0.02076,0.0117,0.7939,0.0082 -8.000,-0.8518,0.02472,0.01980,0.0120,0.7914,0.0085 -7.750,-0.8274,0.02388,0.01880,0.0122,0.7891,0.0088 -7.500,-0.8023,0.02276,0.01751,0.0124,0.7860,0.0092 -7.250,-0.7776,0.02136,0.01587,0.0127,0.7828,0.0096 -7.000,-0.7528,0.01995,0.01419,0.0131,0.7798,0.0100 -6.750,-0.7274,0.01879,0.01278,0.0134,0.7771,0.0104 -6.500,-0.7014,0.01788,0.01165,0.0138,0.7746,0.0107 -6.250,-0.6752,0.01681,0.01047,0.0140,0.7713,0.0112 -6.000,-0.6480,0.01622,0.00982,0.0140,0.7678,0.0117 -5.750,-0.6207,0.01568,0.00920,0.0142,0.7645,0.0122 -5.500,-0.5935,0.01512,0.00854,0.0144,0.7615,0.0129 -5.250,-0.5661,0.01460,0.00790,0.0145,0.7586,0.0136 -5.000,-0.5378,0.01421,0.00743,0.0145,0.7548,0.0144 -4.750,-0.5103,0.01357,0.00675,0.0146,0.7510,0.0155 -4.500,-0.4824,0.01318,0.00632,0.0147,0.7475,0.0164 -4.250,-0.4545,0.01278,0.00584,0.0148,0.7445,0.0174 -4.000,-0.4259,0.01241,0.00542,0.0147,0.7403,0.0185 -3.750,-0.3975,0.01199,0.00496,0.0147,0.7360,0.0201 -3.500,-0.3692,0.01168,0.00462,0.0147,0.7322,0.0217 -3.250,-0.3407,0.01139,0.00428,0.0147,0.7286,0.0234 -3.000,-0.3117,0.01114,0.00399,0.0146,0.7238,0.0250 -2.750,-0.2830,0.01081,0.00365,0.0146,0.7192,0.0283 -2.500,-0.2544,0.01060,0.00340,0.0146,0.7152,0.0317 -2.250,-0.2253,0.01036,0.00314,0.0144,0.7103,0.0359 -2.000,-0.1963,0.01015,0.00293,0.0143,0.7051,0.0417 -1.750,-0.1675,0.00993,0.00271,0.0143,0.7005,0.0515 -1.500,-0.1383,0.00969,0.00253,0.0141,0.6952,0.0707 -1.250,-0.1095,0.00932,0.00236,0.0138,0.6896,0.1265 -1.000,-0.0809,0.00894,0.00220,0.0136,0.6834,0.1973 -0.750,-0.0524,0.00843,0.00202,0.0134,0.6726,0.3034 -0.500,-0.0243,0.00793,0.00192,0.0132,0.6604,0.4336 -0.250,0.0043,0.00770,0.00188,0.0131,0.6508,0.5057 0.000,0.0331,0.00755,0.00186,0.0130,0.6423,0.5568 0.500,0.0910,0.00741,0.00184,0.0128,0.6253,0.6254 0.750,0.1203,0.00738,0.00183,0.0126,0.6157,0.6469 1.000,0.1494,0.00733,0.00181,0.0125,0.6064,0.6715 1.250,0.1786,0.00730,0.00179,0.0123,0.5959,0.6919 1.500,0.2080,0.00728,0.00178,0.0121,0.5845,0.7061 2.000,0.2666,0.00723,0.00176,0.0116,0.5577,0.7384 2.250,0.2953,0.00712,0.00175,0.0115,0.5414,0.7698 2.500,0.3207,0.00677,0.00180,0.0125,0.5238,0.9536 2.750,0.3572,0.00690,0.00186,0.0107,0.5025,0.9826 3.000,0.3938,0.00706,0.00193,0.0087,0.4773,0.9959 3.250,0.4263,0.00728,0.00203,0.0076,0.4464,1.0000 3.500,0.4566,0.00754,0.00214,0.0069,0.4121,1.0000 3.750,0.4871,0.00787,0.00230,0.0060,0.3737,1.0000 4.000,0.5174,0.00820,0.00248,0.0052,0.3419,1.0000 4.250,0.5475,0.00850,0.00267,0.0045,0.3147,1.0000 4.500,0.5773,0.00879,0.00286,0.0038,0.2920,1.0000 4.750,0.6069,0.00906,0.00305,0.0032,0.2727,1.0000 5.000,0.6365,0.00933,0.00327,0.0027,0.2548,1.0000 5.250,0.6660,0.00964,0.00349,0.0020,0.2359,1.0000 5.500,0.6954,0.00995,0.00373,0.0014,0.2146,1.0000 5.750,0.7247,0.01029,0.00399,0.0008,0.1944,1.0000 6.000,0.7538,0.01060,0.00425,0.0002,0.1796,1.0000 6.250,0.7828,0.01091,0.00453,-0.0004,0.1658,1.0000 6.500,0.8116,0.01125,0.00483,-0.0009,0.1521,1.0000 6.750,0.8404,0.01167,0.00518,-0.0015,0.1356,1.0000 7.000,0.8689,0.01206,0.00553,-0.0021,0.1219,1.0000 7.250,0.8972,0.01243,0.00588,-0.0026,0.1105,1.0000 7.500,0.9253,0.01285,0.00627,-0.0032,0.0983,1.0000 7.750,0.9532,0.01329,0.00670,-0.0037,0.0874,1.0000 8.000,0.9808,0.01377,0.00714,-0.0042,0.0770,1.0000 8.250,1.0081,0.01428,0.00763,-0.0047,0.0670,1.0000 8.500,1.0351,0.01481,0.00815,-0.0052,0.0582,1.0000 8.750,1.0617,0.01533,0.00867,-0.0056,0.0510,1.0000 9.000,1.0879,0.01593,0.00925,-0.0060,0.0432,1.0000 9.250,1.1134,0.01660,0.00989,-0.0064,0.0360,1.0000 9.500,1.1390,0.01717,0.01049,-0.0068,0.0311,1.0000 9.750,1.1638,0.01785,0.01119,-0.0071,0.0264,1.0000 10.000,1.1882,0.01855,0.01190,-0.0075,0.0226,1.0000 10.250,1.2121,0.01927,0.01267,-0.0078,0.0197,1.0000 10.500,1.2352,0.02008,0.01351,-0.0081,0.0167,1.0000 10.750,1.2575,0.02092,0.01440,-0.0084,0.0143,1.0000 11.000,1.2785,0.02189,0.01542,-0.0086,0.0122,1.0000 11.250,1.2986,0.02288,0.01649,-0.0088,0.0107,1.0000 11.500,1.3168,0.02398,0.01766,-0.0090,0.0094,1.0000 11.750,1.3322,0.02529,0.01903,-0.0089,0.0084,1.0000 12.000,1.3451,0.02650,0.02035,-0.0084,0.0079,1.0000 12.250,1.3552,0.02783,0.02178,-0.0076,0.0074,1.0000 12.500,1.3645,0.02932,0.02336,-0.0070,0.0070,1.0000 12.750,1.3723,0.03099,0.02512,-0.0064,0.0066,1.0000 13.000,1.3776,0.03296,0.02720,-0.0059,0.0062,1.0000 13.250,1.3816,0.03512,0.02947,-0.0056,0.0060,1.0000 13.500,1.3866,0.03722,0.03170,-0.0054,0.0058,1.0000 13.750,1.3901,0.03956,0.03416,-0.0054,0.0056,1.0000 14.000,1.3918,0.04217,0.03689,-0.0055,0.0054,1.0000 14.250,1.3918,0.04506,0.03992,-0.0059,0.0053,1.0000 14.500,1.3896,0.04834,0.04333,-0.0066,0.0052,1.0000 14.750,1.3858,0.05196,0.04708,-0.0075,0.0051,1.0000 15.000,1.3802,0.05599,0.05125,-0.0088,0.0050,1.0000 15.250,1.3729,0.06049,0.05589,-0.0105,0.0049,1.0000 15.500,1.3634,0.06552,0.06107,-0.0125,0.0049,1.0000 15.750,1.3521,0.07110,0.06679,-0.0150,0.0048,1.0000 16.000,1.3383,0.07727,0.07311,-0.0179,0.0048,1.0000 16.250,1.3226,0.08405,0.08004,-0.0211,0.0048,1.0000 16.500,1.3049,0.09135,0.08749,-0.0247,0.0048,1.0000 16.750,1.2855,0.09913,0.09541,-0.0285,0.0048,1.0000 17.000,1.2654,0.10717,0.10359,-0.0324,0.0048,1.0000 17.250,1.2447,0.11538,0.11193,-0.0364,0.0048,1.0000