Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-davis-corrected-il-50000 Airfoil,davis-corrected-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,12.5174 Max Cl/Cd alpha,-0.75 Url,http://airfoiltools.com/polar/csv?polar=xf-davis-corrected-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.3610,0.10914,0.10205,-0.0106,1.0000,0.3587 -9.500,-0.5340,0.07657,0.06974,-0.0419,1.0000,0.1850 -9.250,-0.5505,0.07173,0.06491,-0.0417,1.0000,0.1831 -9.000,-0.5705,0.06706,0.06026,-0.0409,1.0000,0.1817 -8.750,-0.5941,0.06254,0.05572,-0.0393,1.0000,0.1801 -8.500,-0.6184,0.05854,0.05163,-0.0366,1.0000,0.1789 -8.250,-0.6420,0.05532,0.04832,-0.0328,1.0000,0.1785 -8.000,-0.6663,0.05306,0.04597,-0.0278,1.0000,0.1782 -7.750,-0.6898,0.05129,0.04407,-0.0226,1.0000,0.1783 -7.500,-0.7077,0.04944,0.04202,-0.0181,1.0000,0.1791 -7.250,-0.7208,0.04743,0.03973,-0.0142,1.0000,0.1807 -7.000,-0.7304,0.04533,0.03721,-0.0107,1.0000,0.1832 -6.750,-0.7296,0.04349,0.03522,-0.0082,1.0000,0.1869 -6.500,-0.7149,0.04215,0.03386,-0.0075,0.9975,0.1932 -6.250,-0.6764,0.03958,0.03082,-0.0114,0.9840,0.2047 -6.000,-0.6364,0.03769,0.02856,-0.0149,0.9706,0.2192 -5.750,-0.5963,0.03617,0.02688,-0.0180,0.9570,0.2362 -5.500,-0.5579,0.03491,0.02561,-0.0206,0.9438,0.2556 -5.250,-0.5200,0.03388,0.02462,-0.0230,0.9309,0.2796 -5.000,-0.4784,0.03283,0.02360,-0.0258,0.9190,0.3104 -4.750,-0.4440,0.03203,0.02288,-0.0272,0.9065,0.3451 -4.500,-0.4156,0.03145,0.02248,-0.0274,0.8941,0.3829 -4.250,-0.3767,0.03083,0.02209,-0.0290,0.8835,0.4357 -4.000,-0.3494,0.03048,0.02198,-0.0285,0.8717,0.4884 -3.750,-0.3263,0.03037,0.02213,-0.0270,0.8604,0.5431 -3.500,-0.2852,0.03030,0.02233,-0.0275,0.8511,0.6140 -3.250,-0.2671,0.03072,0.02296,-0.0245,0.8394,0.6645 -3.000,-0.2064,0.03137,0.02371,-0.0262,0.8317,0.7335 -2.750,-0.1829,0.03231,0.02464,-0.0239,0.8198,0.7785 -2.500,-0.0603,0.03374,0.02574,-0.0346,0.8117,0.8331 -2.250,0.0444,0.03458,0.02627,-0.0454,0.8005,0.8731 -2.000,0.1505,0.03459,0.02596,-0.0576,0.7904,0.9089 -1.750,0.2389,0.03408,0.02520,-0.0681,0.7796,0.9416 -1.500,0.3150,0.03354,0.02449,-0.0782,0.7679,0.9721 -1.250,0.3992,0.03209,0.02280,-0.0893,0.7583,1.0000 -1.000,0.4019,0.03291,0.02362,-0.0883,0.7476,1.0000 -0.750,0.4142,0.03309,0.02368,-0.0870,0.7404,1.0000 -0.500,0.4132,0.03423,0.02482,-0.0854,0.7305,1.0000 -0.250,0.4236,0.03466,0.02516,-0.0838,0.7233,1.0000 0.000,0.4191,0.03603,0.02651,-0.0815,0.7149,1.0000 0.250,0.4215,0.03697,0.02741,-0.0793,0.7074,1.0000 0.500,0.4292,0.03774,0.02810,-0.0773,0.7011,1.0000 0.750,0.4026,0.03996,0.03032,-0.0726,0.6931,1.0000 1.000,0.4074,0.04089,0.03119,-0.0701,0.6872,1.0000 1.250,0.3963,0.04251,0.03275,-0.0663,0.6817,1.0000 1.500,0.3458,0.04511,0.03530,-0.0584,0.6765,1.0000 1.750,0.3194,0.04682,0.03692,-0.0524,0.6723,1.0000 2.000,0.3262,0.04803,0.03805,-0.0503,0.6681,1.0000 2.250,0.3271,0.04953,0.03945,-0.0476,0.6646,1.0000 2.500,0.2951,0.05160,0.04142,-0.0418,0.6633,1.0000 2.750,0.2805,0.05347,0.04321,-0.0382,0.6625,1.0000 3.000,0.2769,0.05537,0.04503,-0.0360,0.6632,1.0000 3.250,0.2799,0.05731,0.04691,-0.0347,0.6644,1.0000 3.500,0.0965,0.06081,0.05048,-0.0220,0.8387,1.0000 3.750,0.1272,0.06373,0.05332,-0.0242,0.8310,1.0000 4.000,0.1405,0.06465,0.05419,-0.0234,0.8161,1.0000 4.250,0.1514,0.06581,0.05529,-0.0224,0.8028,1.0000 4.500,0.1850,0.06908,0.05851,-0.0249,0.7945,1.0000 4.750,0.1918,0.06962,0.05902,-0.0233,0.7803,1.0000 5.000,0.2022,0.07104,0.06041,-0.0224,0.7692,1.0000 5.250,0.2355,0.07412,0.06346,-0.0246,0.7592,1.0000 5.500,0.2371,0.07464,0.06395,-0.0225,0.7459,1.0000 5.750,0.2710,0.07837,0.06767,-0.0249,0.7394,1.0000 6.000,0.2718,0.07860,0.06789,-0.0227,0.7252,1.0000 6.250,0.2818,0.08030,0.06957,-0.0221,0.7152,1.0000 6.500,0.3081,0.08293,0.07222,-0.0232,0.7049,1.0000 6.750,0.3095,0.08400,0.07327,-0.0216,0.6943,1.0000 7.000,0.3423,0.08745,0.07676,-0.0235,0.6853,1.0000 7.250,0.3386,0.08797,0.07727,-0.0214,0.6732,1.0000 7.500,0.3752,0.09216,0.08150,-0.0238,0.6661,1.0000 7.750,0.3667,0.09217,0.08151,-0.0214,0.6533,1.0000 8.000,0.4019,0.09662,0.08601,-0.0236,0.6468,1.0000 8.250,0.3953,0.09660,0.08601,-0.0214,0.6333,1.0000 8.500,0.4125,0.09966,0.08910,-0.0219,0.6265,1.0000 8.750,0.4238,0.10134,0.09082,-0.0216,0.6136,1.0000 9.000,0.4278,0.10325,0.09277,-0.0210,0.6044,1.0000 9.250,0.4537,0.10653,0.09612,-0.0220,0.5940,1.0000 9.500,0.4498,0.10773,0.09734,-0.0208,0.5830,1.0000 9.750,0.4881,0.11270,0.10242,-0.0229,0.5743,1.0000 10.000,0.4753,0.11272,0.10245,-0.0211,0.5614,1.0000 10.250,0.4893,0.11592,0.10572,-0.0215,0.5529,1.0000