Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s2060-il-50000-n5 Airfoil,s2060-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,36.8941 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-s2060-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5041,0.09280,0.08569,-0.0270,1.0000,0.0461 -8.750,-0.5062,0.08840,0.08138,-0.0291,1.0000,0.0460 -8.500,-0.5105,0.08379,0.07686,-0.0316,1.0000,0.0459 -8.250,-0.5164,0.07896,0.07212,-0.0346,1.0000,0.0457 -8.000,-0.5202,0.07371,0.06690,-0.0381,1.0000,0.0455 -7.750,-0.5240,0.06860,0.06178,-0.0408,1.0000,0.0452 -7.500,-0.5277,0.06343,0.05652,-0.0431,1.0000,0.0451 -7.250,-0.5294,0.05832,0.05125,-0.0448,1.0000,0.0450 -7.000,-0.5280,0.05334,0.04600,-0.0458,1.0000,0.0452 -6.750,-0.5235,0.04826,0.04050,-0.0465,1.0000,0.0457 -6.500,-0.5147,0.04339,0.03502,-0.0466,1.0000,0.0466 -6.250,-0.5007,0.04112,0.03271,-0.0460,1.0000,0.0503 -6.000,-0.4849,0.03829,0.02948,-0.0455,1.0000,0.0550 -5.750,-0.4668,0.03439,0.02469,-0.0450,1.0000,0.0590 -5.500,-0.4485,0.03279,0.02307,-0.0442,1.0000,0.0664 -5.250,-0.4273,0.03015,0.01986,-0.0434,1.0000,0.0732 -5.000,-0.4064,0.02862,0.01812,-0.0425,1.0000,0.0827 -4.750,-0.3846,0.02693,0.01623,-0.0416,1.0000,0.0906 -4.500,-0.3623,0.02557,0.01462,-0.0406,1.0000,0.1014 -4.250,-0.3398,0.02437,0.01321,-0.0395,1.0000,0.1118 -4.000,-0.3178,0.02330,0.01205,-0.0384,1.0000,0.1236 -3.750,-0.2954,0.02240,0.01104,-0.0375,1.0000,0.1399 -3.500,-0.2729,0.02149,0.01011,-0.0365,1.0000,0.1566 -3.250,-0.2505,0.02070,0.00937,-0.0358,1.0000,0.1847 -3.000,-0.2280,0.01986,0.00866,-0.0352,1.0000,0.2208 -2.750,-0.2056,0.01901,0.00807,-0.0347,1.0000,0.2840 -2.500,-0.1843,0.01807,0.00768,-0.0339,1.0000,0.3915 -2.250,-0.1674,0.01722,0.00761,-0.0315,1.0000,0.5510 -2.000,-0.1548,0.01676,0.00765,-0.0274,1.0000,0.7077 -1.750,-0.1380,0.01645,0.00758,-0.0238,1.0000,0.8479 -1.500,-0.0962,0.01620,0.00712,-0.0265,1.0000,1.0000 -1.250,-0.0752,0.01628,0.00691,-0.0260,1.0000,1.0000 -1.000,-0.0539,0.01640,0.00679,-0.0255,1.0000,1.0000 -0.750,-0.0326,0.01655,0.00670,-0.0251,1.0000,1.0000 -0.500,-0.0113,0.01674,0.00670,-0.0246,1.0000,1.0000 -0.250,0.0102,0.01697,0.00677,-0.0242,0.9999,1.0000 0.000,0.0517,0.01736,0.00700,-0.0277,0.9893,1.0000 0.250,0.0928,0.01775,0.00724,-0.0309,0.9786,1.0000 0.500,0.1341,0.01811,0.00751,-0.0342,0.9675,1.0000 0.750,0.1762,0.01845,0.00778,-0.0374,0.9561,1.0000 1.000,0.2158,0.01872,0.00802,-0.0401,0.9433,1.0000 1.250,0.2552,0.01894,0.00825,-0.0427,0.9298,1.0000 1.500,0.2949,0.01913,0.00847,-0.0451,0.9159,1.0000 1.750,0.3352,0.01927,0.00868,-0.0475,0.9016,1.0000 2.000,0.3761,0.01935,0.00884,-0.0498,0.8868,1.0000 2.250,0.4141,0.01938,0.00897,-0.0514,0.8706,1.0000 2.500,0.4473,0.01941,0.00913,-0.0520,0.8515,1.0000 2.750,0.4827,0.01936,0.00921,-0.0527,0.8324,1.0000 3.000,0.5160,0.01929,0.00928,-0.0529,0.8115,1.0000 3.250,0.5479,0.01921,0.00938,-0.0528,0.7883,1.0000 3.500,0.5775,0.01916,0.00946,-0.0522,0.7619,1.0000 3.750,0.6069,0.01909,0.00953,-0.0514,0.7328,1.0000 4.000,0.6356,0.01906,0.00959,-0.0504,0.7001,1.0000 4.250,0.6625,0.01911,0.00976,-0.0491,0.6620,1.0000 4.500,0.6885,0.01925,0.00992,-0.0476,0.6194,1.0000 4.750,0.7129,0.01951,0.01015,-0.0460,0.5719,1.0000 5.000,0.7353,0.01993,0.01050,-0.0442,0.5196,1.0000 5.250,0.7563,0.02051,0.01101,-0.0424,0.4642,1.0000 5.500,0.7758,0.02125,0.01159,-0.0406,0.4063,1.0000 5.750,0.7937,0.02216,0.01229,-0.0388,0.3445,1.0000 6.000,0.8101,0.02326,0.01314,-0.0370,0.2781,1.0000 6.250,0.8254,0.02464,0.01417,-0.0355,0.2076,1.0000 6.500,0.8399,0.02641,0.01540,-0.0342,0.1335,1.0000 6.750,0.8561,0.02838,0.01714,-0.0330,0.0918,1.0000 7.000,0.8731,0.03023,0.01888,-0.0317,0.0721,1.0000 7.250,0.8918,0.03203,0.02080,-0.0303,0.0624,1.0000 7.500,0.9110,0.03399,0.02283,-0.0290,0.0573,1.0000 7.750,0.9337,0.03605,0.02519,-0.0279,0.0533,1.0000 8.000,0.9551,0.03818,0.02750,-0.0270,0.0499,1.0000 8.250,0.9745,0.04062,0.02998,-0.0262,0.0466,1.0000 8.500,0.9935,0.04318,0.03313,-0.0251,0.0437,1.0000 8.750,1.0097,0.04620,0.03659,-0.0238,0.0421,1.0000 9.000,1.0221,0.04954,0.04038,-0.0224,0.0411,1.0000 9.250,1.0300,0.05312,0.04440,-0.0209,0.0404,1.0000 9.500,1.0328,0.05690,0.04861,-0.0193,0.0400,1.0000 9.750,1.0301,0.06087,0.05297,-0.0176,0.0397,1.0000 10.000,1.0216,0.06496,0.05741,-0.0161,0.0396,1.0000 10.250,1.0060,0.06899,0.06172,-0.0144,0.0397,1.0000 10.500,0.9864,0.07346,0.06642,-0.0138,0.0399,1.0000 10.750,0.9636,0.07880,0.07195,-0.0151,0.0402,1.0000 11.000,0.9386,0.08545,0.07876,-0.0187,0.0407,1.0000 11.250,0.9132,0.09378,0.08718,-0.0245,0.0414,1.0000