Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq09-il-1000000-n5 Airfoil,hq09-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,63.3674 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-hq09-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.9177,0.04166,0.03959,-0.0168,1.0000,0.0017 -9.750,-0.9427,0.03392,0.03136,-0.0142,1.0000,0.0017 -9.500,-0.9483,0.02845,0.02536,-0.0119,1.0000,0.0017 -9.250,-0.9410,0.02484,0.02128,-0.0101,1.0000,0.0016 -9.000,-0.9282,0.02202,0.01808,-0.0086,1.0000,0.0016 -8.750,-0.9116,0.01982,0.01557,-0.0074,1.0000,0.0016 -8.500,-0.8924,0.01813,0.01361,-0.0064,1.0000,0.0016 -8.250,-0.8716,0.01675,0.01203,-0.0055,1.0000,0.0016 -8.000,-0.8500,0.01551,0.01060,-0.0047,1.0000,0.0016 -7.750,-0.8274,0.01451,0.00944,-0.0040,1.0000,0.0016 -7.500,-0.8042,0.01365,0.00844,-0.0034,1.0000,0.0016 -7.250,-0.7804,0.01289,0.00756,-0.0028,1.0000,0.0016 -7.000,-0.7561,0.01224,0.00680,-0.0022,1.0000,0.0016 -6.750,-0.7314,0.01168,0.00615,-0.0018,1.0000,0.0017 -6.500,-0.7064,0.01119,0.00554,-0.0013,1.0000,0.0017 -6.250,-0.6812,0.01075,0.00504,-0.0009,1.0000,0.0017 -6.000,-0.6558,0.01036,0.00459,-0.0005,1.0000,0.0018 -5.750,-0.6303,0.01001,0.00419,-0.0001,1.0000,0.0019 -5.500,-0.6030,0.00970,0.00383,-0.0001,0.9971,0.0021 -5.250,-0.5694,0.00938,0.00347,-0.0015,0.9812,0.0024 -5.000,-0.5353,0.00895,0.00311,-0.0032,0.9655,0.0099 -4.750,-0.5035,0.00876,0.00288,-0.0041,0.9455,0.0109 -4.500,-0.4762,0.00862,0.00265,-0.0039,0.9216,0.0125 -4.250,-0.4508,0.00848,0.00245,-0.0034,0.8971,0.0154 -4.000,-0.4253,0.00834,0.00226,-0.0029,0.8755,0.0198 -3.750,-0.3997,0.00815,0.00206,-0.0024,0.8575,0.0334 -3.500,-0.3737,0.00791,0.00188,-0.0021,0.8416,0.0536 -3.250,-0.3472,0.00775,0.00172,-0.0019,0.8266,0.0696 -3.000,-0.3207,0.00756,0.00155,-0.0017,0.8110,0.0926 -2.750,-0.2945,0.00731,0.00136,-0.0014,0.7945,0.1285 -2.250,-0.2423,0.00667,0.00107,-0.0011,0.7671,0.2473 -2.000,-0.2158,0.00638,0.00095,-0.0010,0.7560,0.3031 -1.750,-0.1898,0.00601,0.00083,-0.0008,0.7457,0.3860 -1.500,-0.1634,0.00572,0.00072,-0.0007,0.7365,0.4540 -1.250,-0.1371,0.00544,0.00065,-0.0005,0.7265,0.5249 -1.000,-0.1106,0.00520,0.00062,-0.0003,0.7164,0.5932 -0.750,-0.0830,0.00515,0.00060,-0.0002,0.7062,0.6173 -0.500,-0.0554,0.00515,0.00058,-0.0001,0.6908,0.6323 -0.250,-0.0278,0.00515,0.00057,0.0000,0.6738,0.6469 0.000,0.0000,0.00515,0.00057,0.0000,0.6603,0.6603 0.250,0.0278,0.00515,0.00057,0.0000,0.6470,0.6739 0.500,0.0554,0.00515,0.00058,0.0001,0.6322,0.6908 0.750,0.0830,0.00515,0.00060,0.0002,0.6173,0.7062 1.000,0.1107,0.00521,0.00062,0.0003,0.5932,0.7163 1.250,0.1371,0.00543,0.00065,0.0005,0.5253,0.7266 1.500,0.1634,0.00572,0.00072,0.0007,0.4539,0.7365 1.750,0.1898,0.00601,0.00083,0.0008,0.3865,0.7458 2.000,0.2158,0.00638,0.00095,0.0010,0.3033,0.7563 2.250,0.2424,0.00667,0.00107,0.0011,0.2472,0.7671 2.500,0.2689,0.00693,0.00120,0.0012,0.2038,0.7792 2.750,0.2946,0.00731,0.00136,0.0014,0.1284,0.7943 3.000,0.3208,0.00756,0.00155,0.0017,0.0926,0.8108 3.250,0.3472,0.00775,0.00172,0.0019,0.0695,0.8266 3.500,0.3737,0.00791,0.00188,0.0021,0.0537,0.8415 3.750,0.3997,0.00814,0.00206,0.0024,0.0338,0.8577 4.000,0.4254,0.00835,0.00226,0.0029,0.0194,0.8759 4.250,0.4508,0.00848,0.00245,0.0034,0.0155,0.8975 4.500,0.4763,0.00862,0.00265,0.0039,0.0124,0.9217 4.750,0.5035,0.00876,0.00288,0.0041,0.0109,0.9454 5.000,0.5352,0.00895,0.00311,0.0032,0.0096,0.9655 5.250,0.5694,0.00939,0.00348,0.0015,0.0024,0.9812 5.500,0.6030,0.00969,0.00382,0.0001,0.0021,0.9970 5.750,0.6302,0.01001,0.00419,0.0001,0.0019,1.0000 6.000,0.6557,0.01037,0.00460,0.0005,0.0018,1.0000 6.250,0.6812,0.01075,0.00504,0.0009,0.0017,1.0000 6.500,0.7064,0.01119,0.00555,0.0013,0.0017,1.0000 6.750,0.7315,0.01169,0.00616,0.0018,0.0017,1.0000 7.000,0.7562,0.01224,0.00680,0.0022,0.0016,1.0000 7.250,0.7805,0.01290,0.00757,0.0027,0.0016,1.0000 7.500,0.8043,0.01366,0.00844,0.0033,0.0016,1.0000 7.750,0.8276,0.01450,0.00943,0.0040,0.0016,1.0000 8.000,0.8503,0.01551,0.01059,0.0047,0.0016,1.0000 8.250,0.8720,0.01670,0.01197,0.0055,0.0016,1.0000 8.500,0.8924,0.01819,0.01368,0.0064,0.0016,1.0000 8.750,0.9117,0.01987,0.01562,0.0074,0.0016,1.0000 9.000,0.9283,0.02209,0.01816,0.0086,0.0016,1.0000 9.250,0.9418,0.02477,0.02120,0.0100,0.0016,1.0000 9.500,0.9482,0.02859,0.02552,0.0118,0.0017,1.0000 9.750,0.9439,0.03382,0.03126,0.0140,0.0017,1.0000 10.000,0.9165,0.04197,0.03992,0.0167,0.0017,1.0000