Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe533-il-50000-n5 Airfoil,goe533-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,29.4468 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe533-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.2585,0.11203,0.10520,-0.0386,1.0000,0.1485 -9.250,-0.2801,0.11118,0.10454,-0.0401,1.0000,0.1501 -9.000,-0.2933,0.10939,0.10294,-0.0403,1.0000,0.1504 -8.500,-0.3049,0.09641,0.09002,-0.0429,1.0000,0.0884 -8.250,-0.3057,0.09466,0.08838,-0.0401,1.0000,0.0873 -8.000,-0.3114,0.09254,0.08638,-0.0395,0.9965,0.0866 -7.750,-0.2929,0.08762,0.08146,-0.0458,0.9814,0.0853 -7.250,-0.2786,0.06940,0.06292,-0.0736,0.9403,0.0770 -7.000,-0.2573,0.06483,0.05822,-0.0786,0.9269,0.0762 -6.750,-0.2369,0.05987,0.05305,-0.0844,0.9136,0.0753 -6.500,-0.2142,0.05478,0.04763,-0.0903,0.9019,0.0746 -6.250,-0.1928,0.05036,0.04280,-0.0946,0.8887,0.0749 -6.000,-0.1711,0.04661,0.03855,-0.0977,0.8754,0.0757 -5.750,-0.1441,0.04320,0.03456,-0.1005,0.8648,0.0764 -5.500,-0.1158,0.04045,0.03134,-0.1024,0.8542,0.0767 -5.250,-0.0890,0.03817,0.02861,-0.1034,0.8430,0.0770 -5.000,-0.0570,0.03603,0.02613,-0.1048,0.8344,0.0777 -4.750,-0.0314,0.03456,0.02447,-0.1049,0.8230,0.0788 -4.500,0.0016,0.03315,0.02286,-0.1059,0.8152,0.0814 -4.250,0.0264,0.03210,0.02158,-0.1056,0.8036,0.0839 -4.000,0.0570,0.03089,0.02006,-0.1058,0.7950,0.0863 -3.750,0.0843,0.02992,0.01883,-0.1054,0.7849,0.0880 -3.500,0.1121,0.02900,0.01781,-0.1050,0.7760,0.0901 -3.250,0.1391,0.02827,0.01702,-0.1046,0.7666,0.0935 -3.000,0.1657,0.02771,0.01632,-0.1040,0.7574,0.0990 -2.750,0.1935,0.02706,0.01558,-0.1037,0.7486,0.1049 -2.500,0.2190,0.02656,0.01502,-0.1032,0.7393,0.1116 -2.250,0.2472,0.02597,0.01435,-0.1031,0.7308,0.1220 -2.000,0.2729,0.02545,0.01387,-0.1029,0.7215,0.1420 -1.750,0.3017,0.02436,0.01324,-0.1035,0.7133,0.2208 -1.500,0.3214,0.02357,0.01358,-0.1020,0.7043,0.4980 -1.250,0.3404,0.02357,0.01390,-0.0990,0.6961,0.6201 -1.000,0.3543,0.02369,0.01420,-0.0950,0.6876,0.7157 -0.750,0.3667,0.02353,0.01421,-0.0903,0.6794,0.7873 -0.500,0.3856,0.02329,0.01401,-0.0872,0.6719,0.8466 -0.250,0.4201,0.02317,0.01385,-0.0878,0.6625,0.9041 0.000,0.4722,0.02309,0.01352,-0.0925,0.6542,1.0000 0.250,0.4972,0.02345,0.01365,-0.0929,0.6448,1.0000 0.500,0.5286,0.02363,0.01353,-0.0938,0.6379,1.0000 0.750,0.5520,0.02413,0.01388,-0.0938,0.6279,1.0000 1.000,0.5836,0.02431,0.01380,-0.0944,0.6213,1.0000 1.250,0.6055,0.02491,0.01430,-0.0941,0.6115,1.0000 1.500,0.6351,0.02517,0.01435,-0.0944,0.6046,1.0000 1.750,0.6580,0.02575,0.01484,-0.0940,0.5957,1.0000 2.000,0.6848,0.02613,0.01508,-0.0939,0.5883,1.0000 2.250,0.7103,0.02660,0.01544,-0.0937,0.5809,1.0000 2.500,0.7332,0.02718,0.01595,-0.0933,0.5725,1.0000 2.750,0.7638,0.02738,0.01599,-0.0934,0.5671,1.0000 3.000,0.7805,0.02830,0.01695,-0.0924,0.5575,1.0000 3.250,0.8085,0.02862,0.01716,-0.0923,0.5515,1.0000 3.500,0.8280,0.02942,0.01796,-0.0915,0.5435,1.0000 3.750,0.8518,0.02997,0.01848,-0.0911,0.5366,1.0000 4.000,0.8803,0.03027,0.01869,-0.0910,0.5314,1.0000 4.250,0.8938,0.03144,0.01994,-0.0897,0.5225,1.0000 4.500,0.9218,0.03174,0.02019,-0.0895,0.5173,1.0000 4.750,0.9370,0.03283,0.02134,-0.0884,0.5096,1.0000 5.000,0.9586,0.03351,0.02203,-0.0877,0.5031,1.0000 5.250,0.9900,0.03362,0.02209,-0.0878,0.4989,1.0000 5.500,0.9947,0.03533,0.02393,-0.0858,0.4896,1.0000 5.750,1.0243,0.03540,0.02397,-0.0856,0.4841,1.0000 6.000,1.0334,0.03674,0.02541,-0.0838,0.4753,1.0000 6.250,1.0606,0.03680,0.02545,-0.0833,0.4685,1.0000 6.500,1.0725,0.03780,0.02651,-0.0816,0.4595,1.0000 6.750,1.0986,0.03784,0.02656,-0.0809,0.4522,1.0000 7.000,1.1096,0.03891,0.02771,-0.0792,0.4438,1.0000 7.250,1.1294,0.03945,0.02829,-0.0782,0.4366,1.0000 7.500,1.1535,0.03984,0.02870,-0.0775,0.4309,1.0000 7.750,1.1489,0.04201,0.03103,-0.0748,0.4223,1.0000 8.000,1.1845,0.04163,0.03065,-0.0750,0.4175,1.0000 8.250,1.1603,0.04495,0.03412,-0.0708,0.4081,1.0000 8.500,1.1874,0.04503,0.03425,-0.0703,0.4025,1.0000 8.750,1.1709,0.04823,0.03756,-0.0675,0.3940,1.0000 9.000,1.1797,0.04970,0.03912,-0.0662,0.3871,1.0000 9.250,1.2256,0.04839,0.03786,-0.0664,0.3836,1.0000 9.500,1.1634,0.05613,0.04574,-0.0636,0.3705,1.0000 9.750,1.2047,0.05470,0.04437,-0.0629,0.3675,1.0000 10.000,1.1471,0.06364,0.05343,-0.0627,0.3531,1.0000 10.250,1.1867,0.06193,0.05179,-0.0614,0.3506,1.0000 10.750,1.1716,0.06975,0.05978,-0.0611,0.3335,1.0000 11.250,1.1518,0.07909,0.06930,-0.0620,0.3166,1.0000