Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq010-il-100000 Airfoil,hq010-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,39.7281 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-hq010-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.6401,0.10723,0.10239,0.0075,1.0000,0.1576 -10.000,-0.6718,0.10162,0.09693,0.0004,1.0000,0.1608 -9.250,-0.8257,0.06229,0.05678,-0.0213,1.0000,0.0670 -9.000,-0.8317,0.05797,0.05208,-0.0201,1.0000,0.0673 -8.750,-0.8345,0.05300,0.04672,-0.0188,1.0000,0.0678 -8.500,-0.8262,0.04814,0.04151,-0.0176,1.0000,0.0670 -8.250,-0.8177,0.04353,0.03648,-0.0162,1.0000,0.0666 -8.000,-0.8086,0.03959,0.03195,-0.0146,1.0000,0.0684 -7.750,-0.7899,0.03659,0.02896,-0.0142,1.0000,0.0720 -7.500,-0.7721,0.03346,0.02536,-0.0128,1.0000,0.0726 -7.250,-0.7514,0.03086,0.02237,-0.0117,1.0000,0.0741 -7.000,-0.7287,0.02862,0.01978,-0.0106,1.0000,0.0765 -6.750,-0.7056,0.02714,0.01785,-0.0095,1.0000,0.0805 -6.500,-0.6818,0.02490,0.01574,-0.0091,1.0000,0.0872 -6.250,-0.6569,0.02338,0.01401,-0.0082,1.0000,0.0930 -6.000,-0.6336,0.02155,0.01233,-0.0074,1.0000,0.1011 -5.750,-0.6124,0.02009,0.01092,-0.0062,1.0000,0.1140 -5.500,-0.5932,0.01875,0.00974,-0.0048,1.0000,0.1360 -5.250,-0.5760,0.01742,0.00875,-0.0031,1.0000,0.1746 -5.000,-0.5639,0.01572,0.00777,-0.0008,1.0000,0.2686 -4.750,-0.5537,0.01430,0.00720,0.0019,1.0000,0.4004 -4.500,-0.5407,0.01361,0.00708,0.0049,1.0000,0.5109 -4.250,-0.5255,0.01347,0.00719,0.0079,1.0000,0.5919 -4.000,-0.5100,0.01354,0.00729,0.0109,1.0000,0.6469 -3.750,-0.4950,0.01368,0.00745,0.0141,1.0000,0.6871 -3.500,-0.4805,0.01383,0.00760,0.0173,1.0000,0.7194 -3.250,-0.4669,0.01400,0.00776,0.0207,1.0000,0.7482 -3.000,-0.4548,0.01422,0.00798,0.0246,1.0000,0.7770 -2.750,-0.4438,0.01443,0.00819,0.0287,1.0000,0.8049 -2.500,-0.4320,0.01454,0.00824,0.0323,1.0000,0.8299 -2.250,-0.4172,0.01460,0.00825,0.0351,1.0000,0.8498 -2.000,-0.4021,0.01458,0.00816,0.0374,1.0000,0.8699 -1.750,-0.3816,0.01464,0.00817,0.0389,1.0000,0.8879 -1.500,-0.3562,0.01475,0.00820,0.0392,1.0000,0.9060 -1.250,-0.3251,0.01489,0.00825,0.0382,1.0000,0.9244 -1.000,-0.2740,0.01526,0.00852,0.0335,0.9971,0.9404 -0.750,-0.2040,0.01579,0.00893,0.0253,0.9941,0.9545 -0.500,-0.1299,0.01612,0.00919,0.0161,0.9917,0.9651 -0.250,-0.0632,0.01624,0.00926,0.0078,0.9868,0.9733 0.000,0.0001,0.01634,0.00935,0.0000,0.9814,0.9814 0.250,0.0633,0.01624,0.00926,-0.0078,0.9733,0.9868 0.500,0.1301,0.01611,0.00918,-0.0161,0.9649,0.9916 0.750,0.2041,0.01578,0.00893,-0.0254,0.9545,0.9941 1.000,0.2740,0.01526,0.00852,-0.0335,0.9405,0.9972 1.250,0.3252,0.01489,0.00825,-0.0382,0.9244,1.0000 1.500,0.3561,0.01475,0.00820,-0.0392,0.9061,1.0000 1.750,0.3816,0.01464,0.00817,-0.0389,0.8880,1.0000 2.000,0.4021,0.01458,0.00816,-0.0374,0.8700,1.0000 2.250,0.4172,0.01460,0.00825,-0.0351,0.8499,1.0000 2.500,0.4320,0.01454,0.00823,-0.0322,0.8299,1.0000 2.750,0.4437,0.01443,0.00819,-0.0287,0.8049,1.0000 3.000,0.4548,0.01422,0.00798,-0.0246,0.7770,1.0000 3.250,0.4668,0.01400,0.00776,-0.0207,0.7482,1.0000 3.500,0.4805,0.01383,0.00760,-0.0173,0.7195,1.0000 3.750,0.4949,0.01368,0.00745,-0.0141,0.6870,1.0000 4.000,0.5100,0.01354,0.00729,-0.0109,0.6468,1.0000 4.250,0.5255,0.01347,0.00719,-0.0079,0.5921,1.0000 4.500,0.5407,0.01361,0.00708,-0.0049,0.5110,1.0000 4.750,0.5538,0.01430,0.00720,-0.0019,0.4005,1.0000 5.000,0.5639,0.01571,0.00776,0.0008,0.2691,1.0000 5.250,0.5760,0.01742,0.00875,0.0031,0.1745,1.0000 5.500,0.5933,0.01875,0.00974,0.0048,0.1360,1.0000 5.750,0.6124,0.02010,0.01092,0.0062,0.1139,1.0000 6.000,0.6336,0.02155,0.01234,0.0074,0.1009,1.0000 6.250,0.6569,0.02338,0.01401,0.0082,0.0930,1.0000 6.500,0.6818,0.02489,0.01574,0.0091,0.0870,1.0000 6.750,0.7056,0.02714,0.01785,0.0095,0.0805,1.0000 7.000,0.7287,0.02862,0.01978,0.0106,0.0764,1.0000 7.250,0.7513,0.03086,0.02238,0.0117,0.0740,1.0000 7.500,0.7721,0.03347,0.02537,0.0128,0.0725,1.0000 7.750,0.7899,0.03660,0.02897,0.0142,0.0720,1.0000 8.000,0.8087,0.03952,0.03191,0.0147,0.0686,1.0000 8.250,0.8177,0.04353,0.03648,0.0162,0.0666,1.0000 8.500,0.8263,0.04813,0.04149,0.0176,0.0670,1.0000 8.750,0.8347,0.05290,0.04662,0.0188,0.0679,1.0000 9.000,0.8327,0.05835,0.05243,0.0199,0.0674,1.0000 9.250,0.8242,0.06200,0.05653,0.0215,0.0669,1.0000