Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx711525-il-50000-n5 Airfoil,fx711525-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.8173 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-fx711525-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.250,-0.8253,0.08567,0.07716,-0.0267,1.0000,0.0491 -13.000,-0.8442,0.07974,0.07101,-0.0294,1.0000,0.0490 -12.750,-0.8613,0.07445,0.06547,-0.0315,1.0000,0.0491 -12.500,-0.8718,0.07003,0.06085,-0.0326,1.0000,0.0494 -12.250,-0.8734,0.06659,0.05725,-0.0332,1.0000,0.0497 -12.000,-0.8725,0.06341,0.05390,-0.0334,1.0000,0.0503 -11.750,-0.8691,0.06043,0.05075,-0.0335,1.0000,0.0509 -11.500,-0.8628,0.05761,0.04775,-0.0333,1.0000,0.0518 -11.250,-0.8532,0.05497,0.04488,-0.0330,1.0000,0.0530 -11.000,-0.8391,0.05253,0.04215,-0.0325,1.0000,0.0544 -10.750,-0.8200,0.05078,0.04037,-0.0320,1.0000,0.0562 -10.500,-0.8006,0.04913,0.03863,-0.0313,1.0000,0.0586 -10.250,-0.7814,0.04754,0.03694,-0.0306,1.0000,0.0620 -10.000,-0.7656,0.04600,0.03535,-0.0299,1.0000,0.0658 -9.750,-0.7522,0.04438,0.03373,-0.0293,1.0000,0.0708 -9.500,-0.7388,0.04278,0.03211,-0.0285,1.0000,0.0769 -9.250,-0.7276,0.04112,0.03046,-0.0278,1.0000,0.0846 -9.000,-0.7200,0.03936,0.02879,-0.0272,1.0000,0.0951 -8.750,-0.7127,0.03763,0.02718,-0.0265,1.0000,0.1075 -8.500,-0.7055,0.03594,0.02557,-0.0257,1.0000,0.1235 -8.250,-0.7010,0.03415,0.02400,-0.0245,1.0000,0.1404 -8.000,-0.6984,0.03245,0.02249,-0.0230,1.0000,0.1602 -7.750,-0.6967,0.03090,0.02116,-0.0210,1.0000,0.1841 -7.500,-0.6959,0.02937,0.01992,-0.0189,1.0000,0.2150 -7.250,-0.6969,0.02797,0.01891,-0.0164,1.0000,0.2540 -7.000,-0.7000,0.02691,0.01827,-0.0130,1.0000,0.2987 -6.750,-0.7061,0.02633,0.01803,-0.0086,1.0000,0.3421 -6.500,-0.6880,0.02613,0.01814,-0.0074,0.9834,0.4044 -6.250,-0.6554,0.02646,0.01853,-0.0080,0.9694,0.4592 -6.000,-0.6218,0.02700,0.01895,-0.0085,0.9572,0.4989 -5.750,-0.5894,0.02750,0.01927,-0.0090,0.9460,0.5297 -5.500,-0.5524,0.02819,0.01978,-0.0097,0.9374,0.5539 -5.250,-0.5191,0.02892,0.02033,-0.0095,0.9276,0.5733 -5.000,-0.4823,0.02945,0.02068,-0.0102,0.9199,0.5904 -4.750,-0.4555,0.02972,0.02077,-0.0098,0.9097,0.6065 -4.500,-0.4143,0.03044,0.02133,-0.0104,0.9032,0.6160 -4.250,-0.3902,0.03039,0.02113,-0.0099,0.8939,0.6292 -4.000,-0.3603,0.03052,0.02111,-0.0099,0.8860,0.6400 -3.750,-0.3334,0.03051,0.02096,-0.0097,0.8785,0.6502 -3.500,-0.3104,0.03043,0.02075,-0.0091,0.8700,0.6606 -3.250,-0.2831,0.03032,0.02051,-0.0090,0.8633,0.6694 -3.000,-0.2608,0.03029,0.02039,-0.0082,0.8551,0.6786 -2.750,-0.2390,0.03010,0.02010,-0.0075,0.8476,0.6879 -2.500,-0.2119,0.03008,0.01998,-0.0073,0.8414,0.6954 -2.250,-0.1977,0.02980,0.01962,-0.0060,0.8329,0.7053 -2.000,-0.1686,0.02979,0.01954,-0.0059,0.8268,0.7113 -1.750,-0.1531,0.02961,0.01929,-0.0046,0.8190,0.7210 -1.500,-0.1286,0.02958,0.01921,-0.0041,0.8121,0.7274 -1.250,-0.1036,0.02950,0.01907,-0.0036,0.8063,0.7348 -1.000,-0.0876,0.02940,0.01894,-0.0025,0.7978,0.7430 -0.750,-0.0607,0.02937,0.01888,-0.0023,0.7919,0.7491 -0.500,-0.0460,0.02927,0.01874,-0.0011,0.7842,0.7580 -0.250,-0.0200,0.02928,0.01875,-0.0008,0.7776,0.7633 0.000,0.0000,0.02925,0.01870,0.0000,0.7709,0.7709 0.250,0.0200,0.02928,0.01875,0.0008,0.7633,0.7776 0.500,0.0460,0.02926,0.01873,0.0011,0.7580,0.7842 0.750,0.0608,0.02937,0.01888,0.0023,0.7490,0.7919 1.000,0.0876,0.02940,0.01894,0.0025,0.7430,0.7978 1.250,0.1036,0.02950,0.01907,0.0036,0.7348,0.8063 1.500,0.1286,0.02958,0.01921,0.0041,0.7274,0.8121 1.750,0.1531,0.02961,0.01928,0.0046,0.7210,0.8190 2.000,0.1686,0.02979,0.01954,0.0058,0.7113,0.8268 2.250,0.1977,0.02980,0.01962,0.0060,0.7054,0.8329 2.500,0.2120,0.03008,0.01998,0.0073,0.6954,0.8414 2.750,0.2391,0.03010,0.02009,0.0075,0.6879,0.8477 3.000,0.2608,0.03029,0.02038,0.0082,0.6786,0.8551 3.250,0.2830,0.03032,0.02051,0.0090,0.6694,0.8633 3.500,0.3105,0.03042,0.02074,0.0091,0.6607,0.8700 3.750,0.3334,0.03051,0.02095,0.0097,0.6503,0.8785 4.000,0.3604,0.03051,0.02110,0.0099,0.6401,0.8861 4.250,0.3903,0.03039,0.02113,0.0099,0.6292,0.8939 4.500,0.4144,0.03044,0.02133,0.0103,0.6161,0.9032 4.750,0.4556,0.02971,0.02076,0.0097,0.6065,0.9097 5.000,0.4824,0.02945,0.02067,0.0102,0.5904,0.9199 5.250,0.5192,0.02891,0.02032,0.0095,0.5733,0.9277 5.500,0.5524,0.02819,0.01978,0.0096,0.5540,0.9375 5.750,0.5895,0.02750,0.01926,0.0089,0.5297,0.9461 6.000,0.6220,0.02699,0.01894,0.0085,0.4988,0.9573 6.250,0.6556,0.02645,0.01852,0.0080,0.4591,0.9695 6.500,0.6881,0.02613,0.01814,0.0074,0.4045,0.9835 6.750,0.7061,0.02633,0.01802,0.0086,0.3421,1.0000 7.000,0.6999,0.02691,0.01827,0.0130,0.2985,1.0000 7.250,0.6969,0.02797,0.01891,0.0164,0.2537,1.0000 7.500,0.6961,0.02936,0.01992,0.0189,0.2150,1.0000 7.750,0.6969,0.03090,0.02115,0.0210,0.1841,1.0000 8.000,0.6985,0.03245,0.02250,0.0230,0.1598,1.0000 8.250,0.7012,0.03416,0.02400,0.0245,0.1404,1.0000 8.500,0.7059,0.03593,0.02556,0.0256,0.1237,1.0000 8.750,0.7129,0.03764,0.02719,0.0265,0.1073,1.0000 9.000,0.7201,0.03937,0.02880,0.0272,0.0947,1.0000 9.250,0.7280,0.04112,0.03045,0.0277,0.0845,1.0000 9.500,0.7390,0.04279,0.03211,0.0285,0.0766,1.0000 9.750,0.7525,0.04439,0.03373,0.0292,0.0706,1.0000 10.000,0.7665,0.04598,0.03532,0.0299,0.0659,1.0000 10.250,0.7817,0.04755,0.03694,0.0305,0.0618,1.0000 10.500,0.8015,0.04910,0.03860,0.0312,0.0587,1.0000 10.750,0.8207,0.05078,0.04036,0.0319,0.0561,1.0000 11.000,0.8400,0.05249,0.04209,0.0324,0.0545,1.0000 11.250,0.8539,0.05499,0.04491,0.0329,0.0529,1.0000 11.500,0.8637,0.05761,0.04775,0.0332,0.0519,1.0000 11.750,0.8699,0.06043,0.05075,0.0334,0.0509,1.0000 12.000,0.8733,0.06342,0.05392,0.0333,0.0503,1.0000 12.250,0.8748,0.06657,0.05722,0.0331,0.0497,1.0000 12.500,0.8738,0.06995,0.06075,0.0326,0.0493,1.0000 12.750,0.8625,0.07442,0.06544,0.0314,0.0491,1.0000 13.000,0.8456,0.07972,0.07099,0.0293,0.0491,1.0000 13.250,0.8244,0.08594,0.07745,0.0264,0.0491,1.0000 13.500,0.7633,0.09946,0.09142,0.0176,0.0504,1.0000 13.750,0.7003,0.11803,0.11022,0.0056,0.0521,1.0000