Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq1510-il-50000 Airfoil,hq1510-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,34.2851 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-hq1510-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.4554,0.10107,0.09425,-0.0060,1.0000,0.3082 -8.500,-0.4488,0.09775,0.09097,-0.0054,1.0000,0.3244 -8.250,-0.4560,0.09571,0.08903,-0.0049,1.0000,0.3448 -8.000,-0.4374,0.09149,0.08480,-0.0036,1.0000,0.3649 -7.750,-0.4314,0.08826,0.08162,-0.0028,1.0000,0.3826 -7.500,-0.4278,0.08493,0.07835,-0.0024,1.0000,0.3947 -7.250,-0.5311,0.06929,0.06302,-0.0327,1.0000,0.1841 -7.000,-0.5507,0.06035,0.05374,-0.0393,1.0000,0.1447 -6.750,-0.5519,0.05451,0.04751,-0.0403,1.0000,0.1304 -6.500,-0.5513,0.04930,0.04152,-0.0402,1.0000,0.1197 -6.250,-0.5393,0.04530,0.03732,-0.0390,1.0000,0.1175 -6.000,-0.5276,0.04168,0.03325,-0.0377,1.0000,0.1172 -5.750,-0.5147,0.03865,0.02946,-0.0362,1.0000,0.1200 -5.500,-0.4982,0.03570,0.02651,-0.0348,1.0000,0.1259 -5.250,-0.4796,0.03296,0.02330,-0.0333,1.0000,0.1303 -5.000,-0.4613,0.03074,0.02086,-0.0318,1.0000,0.1427 -4.750,-0.4406,0.02853,0.01841,-0.0303,1.0000,0.1548 -4.500,-0.4203,0.02685,0.01652,-0.0288,1.0000,0.1747 -4.250,-0.3986,0.02506,0.01479,-0.0273,1.0000,0.1947 -4.000,-0.3783,0.02358,0.01343,-0.0257,1.0000,0.2260 -3.750,-0.3571,0.02188,0.01194,-0.0242,1.0000,0.2729 -3.500,-0.3448,0.01929,0.01101,-0.0213,1.0000,0.4482 -3.250,-0.3520,0.01935,0.01217,-0.0104,1.0000,0.7015 -3.000,-0.3532,0.01975,0.01258,-0.0016,1.0000,0.7838 -2.750,-0.3494,0.01988,0.01265,0.0060,1.0000,0.8470 -2.500,-0.0523,0.02079,0.01176,-0.0336,1.0000,1.0000 -2.250,-0.0607,0.02056,0.01151,-0.0298,1.0000,1.0000 -2.000,-0.0715,0.02034,0.01127,-0.0257,1.0000,1.0000 -1.750,-0.0839,0.02009,0.01099,-0.0214,1.0000,1.0000 -1.500,-0.0974,0.01979,0.01066,-0.0169,1.0000,1.0000 -1.250,-0.1101,0.01944,0.01027,-0.0125,1.0000,1.0000 -1.000,-0.1156,0.01917,0.00989,-0.0090,1.0000,1.0000 -0.750,-0.1081,0.01911,0.00966,-0.0075,1.0000,1.0000 -0.500,-0.0933,0.01921,0.00958,-0.0069,1.0000,1.0000 -0.250,-0.0756,0.01942,0.00959,-0.0068,1.0000,1.0000 0.000,-0.0568,0.01970,0.00971,-0.0067,1.0000,1.0000 0.250,-0.0374,0.02004,0.00991,-0.0067,1.0000,1.0000 0.500,-0.0179,0.02044,0.01018,-0.0067,1.0000,1.0000 0.750,0.0016,0.02088,0.01051,-0.0068,1.0000,1.0000 1.000,0.0210,0.02137,0.01089,-0.0068,1.0000,1.0000 1.250,0.0402,0.02191,0.01136,-0.0069,1.0000,1.0000 1.500,0.0591,0.02250,0.01189,-0.0069,1.0000,1.0000 1.750,0.0778,0.02315,0.01250,-0.0071,1.0000,1.0000 2.000,0.1120,0.02422,0.01354,-0.0102,0.9930,1.0000 2.250,0.1662,0.02563,0.01498,-0.0169,0.9738,1.0000 2.500,0.2255,0.02695,0.01639,-0.0240,0.9499,1.0000 2.750,0.2861,0.02804,0.01758,-0.0308,0.9253,1.0000 3.000,0.3344,0.02883,0.01849,-0.0351,0.9019,1.0000 3.250,0.3809,0.02951,0.01935,-0.0387,0.8787,1.0000 3.500,0.4390,0.02996,0.02002,-0.0437,0.8559,1.0000 3.750,0.4832,0.03025,0.02052,-0.0460,0.8304,1.0000 4.000,0.5331,0.03024,0.02081,-0.0487,0.8040,1.0000 4.250,0.5840,0.02983,0.02069,-0.0505,0.7764,1.0000 4.500,0.6320,0.02903,0.02022,-0.0510,0.7473,1.0000 4.750,0.6788,0.02779,0.01926,-0.0503,0.7164,1.0000 5.000,0.7130,0.02682,0.01849,-0.0480,0.6794,1.0000 5.250,0.7475,0.02559,0.01739,-0.0451,0.6389,1.0000 5.500,0.7768,0.02459,0.01645,-0.0419,0.5927,1.0000 5.750,0.8014,0.02403,0.01576,-0.0385,0.5413,1.0000 6.000,0.8225,0.02399,0.01549,-0.0353,0.4859,1.0000 6.250,0.8405,0.02453,0.01573,-0.0323,0.4267,1.0000 6.500,0.8567,0.02560,0.01637,-0.0295,0.3640,1.0000 6.750,0.8720,0.02733,0.01775,-0.0270,0.3004,1.0000 7.000,0.8899,0.02940,0.01938,-0.0251,0.2484,1.0000 7.250,0.9121,0.03170,0.02163,-0.0239,0.2144,1.0000 7.500,0.9345,0.03384,0.02374,-0.0228,0.1909,1.0000 7.750,0.9553,0.03591,0.02596,-0.0217,0.1726,1.0000 8.000,0.9776,0.03871,0.02902,-0.0207,0.1615,1.0000 8.250,0.9973,0.04137,0.03186,-0.0196,0.1506,1.0000 8.500,1.0176,0.04401,0.03459,-0.0187,0.1397,1.0000 8.750,1.0254,0.04794,0.03930,-0.0166,0.1359,1.0000 9.000,1.0317,0.05204,0.04394,-0.0147,0.1324,1.0000 9.250,1.0441,0.05547,0.04746,-0.0135,0.1251,1.0000 9.500,1.0356,0.05991,0.05248,-0.0112,0.1226,1.0000 9.750,1.0243,0.06478,0.05777,-0.0094,0.1221,1.0000 10.000,1.0084,0.06983,0.06312,-0.0080,0.1229,1.0000 10.250,0.9895,0.07486,0.06836,-0.0069,0.1240,1.0000 10.500,0.9699,0.07982,0.07342,-0.0062,0.1252,1.0000 10.750,0.9549,0.08537,0.07903,-0.0066,0.1262,1.0000 11.000,0.7550,0.13147,0.12448,-0.0516,0.3207,1.0000