Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq259b-il-100000-n5 Airfoil,hq259b-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,56.2017 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-hq259b-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.4363,0.12013,0.11480,-0.0276,1.0000,0.0502 -10.500,-0.4405,0.11699,0.11173,-0.0312,1.0000,0.0508 -10.250,-0.4411,0.11348,0.10828,-0.0337,1.0000,0.0509 -10.000,-0.4409,0.10971,0.10455,-0.0359,1.0000,0.0510 -9.750,-0.4405,0.10589,0.10079,-0.0378,1.0000,0.0511 -9.500,-0.4410,0.10189,0.09684,-0.0398,1.0000,0.0511 -9.250,-0.4418,0.09787,0.09287,-0.0417,1.0000,0.0511 -9.000,-0.4226,0.09161,0.08652,-0.0368,1.0000,0.0373 -8.750,-0.4207,0.08819,0.08315,-0.0368,1.0000,0.0356 -8.500,-0.4235,0.08441,0.07944,-0.0378,1.0000,0.0343 -8.250,-0.4303,0.08048,0.07560,-0.0390,1.0000,0.0332 -8.000,-0.4424,0.07649,0.07173,-0.0402,1.0000,0.0323 -7.500,-0.4755,0.06247,0.05757,-0.0504,1.0000,0.0286 -6.750,-0.4827,0.05365,0.04862,-0.0478,1.0000,0.0304 -6.500,-0.4700,0.05078,0.04559,-0.0490,0.9978,0.0317 -6.250,-0.4437,0.04514,0.03951,-0.0539,0.9920,0.0319 -6.000,-0.4156,0.03972,0.03354,-0.0577,0.9863,0.0316 -5.750,-0.3850,0.03547,0.02873,-0.0607,0.9819,0.0320 -5.500,-0.3561,0.03262,0.02545,-0.0625,0.9765,0.0336 -5.250,-0.3240,0.02997,0.02227,-0.0644,0.9723,0.0359 -5.000,-0.2903,0.02735,0.01911,-0.0661,0.9694,0.0367 -4.750,-0.2619,0.02541,0.01671,-0.0665,0.9641,0.0375 -4.500,-0.2297,0.02398,0.01489,-0.0674,0.9600,0.0389 -4.250,-0.1975,0.02236,0.01324,-0.0689,0.9570,0.0421 -4.000,-0.1669,0.02125,0.01200,-0.0696,0.9529,0.0443 -3.750,-0.1382,0.02025,0.01088,-0.0698,0.9482,0.0464 -3.500,-0.1065,0.01937,0.00990,-0.0706,0.9447,0.0491 -3.250,-0.0732,0.01854,0.00907,-0.0720,0.9419,0.0543 -3.000,-0.0455,0.01801,0.00850,-0.0722,0.9366,0.0612 -2.750,-0.0154,0.01740,0.00784,-0.0729,0.9322,0.0697 -2.500,0.0176,0.01683,0.00732,-0.0742,0.9290,0.0937 -2.250,0.0509,0.01565,0.00679,-0.0762,0.9265,0.2262 -2.000,0.0688,0.01454,0.00706,-0.0746,0.9202,0.5828 -1.750,0.0943,0.01449,0.00724,-0.0735,0.9158,0.6854 -1.500,0.1214,0.01447,0.00733,-0.0725,0.9125,0.7483 -1.250,0.1385,0.01452,0.00747,-0.0695,0.9058,0.7981 -1.000,0.1634,0.01448,0.00742,-0.0683,0.9010,0.8315 -0.750,0.1952,0.01435,0.00720,-0.0686,0.8948,0.8492 -0.500,0.2279,0.01412,0.00689,-0.0690,0.8853,0.8660 0.000,0.2931,0.01362,0.00627,-0.0697,0.8650,0.9044 0.250,0.3283,0.01346,0.00609,-0.0709,0.8571,0.9290 0.500,0.3708,0.01332,0.00592,-0.0737,0.8508,0.9620 0.750,0.4050,0.01328,0.00583,-0.0751,0.8424,1.0000 1.000,0.4343,0.01330,0.00581,-0.0755,0.8338,1.0000 1.250,0.4653,0.01329,0.00574,-0.0760,0.8255,1.0000 1.500,0.4925,0.01335,0.00578,-0.0759,0.8149,1.0000 1.750,0.5214,0.01336,0.00579,-0.0760,0.8048,1.0000 2.000,0.5513,0.01334,0.00575,-0.0761,0.7946,1.0000 2.250,0.5786,0.01338,0.00579,-0.0758,0.7818,1.0000 2.500,0.6059,0.01341,0.00584,-0.0754,0.7680,1.0000 2.750,0.6333,0.01342,0.00589,-0.0750,0.7527,1.0000 3.000,0.6602,0.01346,0.00594,-0.0745,0.7353,1.0000 3.250,0.6861,0.01351,0.00603,-0.0738,0.7140,1.0000 3.500,0.7122,0.01355,0.00611,-0.0731,0.6893,1.0000 3.750,0.7372,0.01362,0.00619,-0.0722,0.6563,1.0000 4.000,0.7621,0.01371,0.00618,-0.0711,0.6071,1.0000 4.250,0.7857,0.01398,0.00609,-0.0696,0.5384,1.0000 4.500,0.8069,0.01457,0.00630,-0.0681,0.4777,1.0000 4.750,0.8283,0.01522,0.00668,-0.0670,0.4323,1.0000 5.000,0.8507,0.01579,0.00712,-0.0661,0.3972,1.0000 5.250,0.8735,0.01633,0.00759,-0.0653,0.3678,1.0000 5.500,0.8962,0.01687,0.00811,-0.0645,0.3393,1.0000 5.750,0.9185,0.01744,0.00863,-0.0636,0.3077,1.0000 6.000,0.9403,0.01804,0.00917,-0.0627,0.2736,1.0000 6.250,0.9611,0.01873,0.00975,-0.0618,0.2305,1.0000 6.500,0.9796,0.01971,0.01045,-0.0606,0.1755,1.0000 6.750,0.9976,0.02085,0.01130,-0.0595,0.1333,1.0000 7.000,1.0163,0.02194,0.01225,-0.0584,0.1075,1.0000 7.250,1.0347,0.02303,0.01327,-0.0573,0.0907,1.0000 7.500,1.0528,0.02413,0.01436,-0.0561,0.0778,1.0000 7.750,1.0709,0.02521,0.01558,-0.0548,0.0683,1.0000 8.000,1.0871,0.02648,0.01692,-0.0532,0.0615,1.0000 8.250,1.1033,0.02771,0.01822,-0.0518,0.0555,1.0000 8.500,1.1188,0.02906,0.01965,-0.0503,0.0507,1.0000 8.750,1.1355,0.03038,0.02111,-0.0489,0.0469,1.0000 9.000,1.1510,0.03182,0.02266,-0.0474,0.0441,1.0000 9.250,1.1661,0.03366,0.02452,-0.0461,0.0417,1.0000 9.500,1.1836,0.03515,0.02629,-0.0448,0.0390,1.0000 9.750,1.1993,0.03676,0.02810,-0.0435,0.0364,1.0000 10.000,1.2138,0.03853,0.03003,-0.0422,0.0347,1.0000 10.250,1.2255,0.04040,0.03195,-0.0407,0.0329,1.0000 10.500,1.2356,0.04266,0.03449,-0.0390,0.0312,1.0000 10.750,1.2428,0.04488,0.03708,-0.0370,0.0297,1.0000 11.000,1.2474,0.04746,0.03998,-0.0349,0.0286,1.0000 11.250,1.2482,0.05010,0.04290,-0.0327,0.0276,1.0000 11.500,1.2463,0.05263,0.04568,-0.0306,0.0268,1.0000 11.750,1.2432,0.05514,0.04837,-0.0290,0.0259,1.0000 12.000,1.2396,0.05778,0.05115,-0.0277,0.0252,1.0000 12.250,1.2334,0.06110,0.05459,-0.0268,0.0245,1.0000 12.500,1.2197,0.06531,0.05907,-0.0262,0.0241,1.0000 12.750,1.2030,0.07002,0.06410,-0.0265,0.0239,1.0000 13.000,1.1844,0.07541,0.06977,-0.0278,0.0237,1.0000 13.250,1.1641,0.08157,0.07619,-0.0302,0.0237,1.0000 13.500,1.1427,0.08858,0.08343,-0.0338,0.0237,1.0000 13.750,1.1210,0.09646,0.09151,-0.0385,0.0239,1.0000 14.000,1.0986,0.10538,0.10059,-0.0444,0.0241,1.0000