Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e1213-il-50000-n5 Airfoil,e1213-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,22.2889 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e1213-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.5178,0.11822,0.11014,-0.0090,1.0000,0.1391 -12.500,-0.5028,0.11690,0.10880,-0.0088,1.0000,0.1443 -12.250,-0.5242,0.10971,0.10163,-0.0130,1.0000,0.1506 -12.000,-0.5004,0.10973,0.10163,-0.0116,1.0000,0.1549 -11.750,-0.5057,0.10520,0.09710,-0.0137,1.0000,0.1605 -11.500,-0.5092,0.10100,0.09291,-0.0156,1.0000,0.1657 -11.250,-0.4963,0.09926,0.09115,-0.0155,1.0000,0.1702 -11.000,-0.5340,0.09026,0.08220,-0.0211,1.0000,0.1777 -10.750,-0.5058,0.09081,0.08272,-0.0191,1.0000,0.1809 -10.500,-0.4995,0.08827,0.08018,-0.0197,1.0000,0.1860 -10.250,-0.5400,0.07923,0.07121,-0.0252,1.0000,0.1932 -10.000,-0.5142,0.07952,0.07149,-0.0235,1.0000,0.1966 -9.500,-0.5883,0.06325,0.05531,-0.0331,1.0000,0.2103 -9.250,-0.5687,0.06291,0.05498,-0.0318,1.0000,0.2143 -9.000,-0.6508,0.05304,0.04500,-0.0338,1.0000,0.2212 -8.750,-0.6662,0.04933,0.04116,-0.0329,1.0000,0.2261 -8.500,-0.6444,0.04904,0.04093,-0.0317,1.0000,0.2301 -8.250,-0.6460,0.04667,0.03847,-0.0304,1.0000,0.2355 -8.000,-0.6648,0.04290,0.03438,-0.0285,1.0000,0.2415 -7.750,-0.6452,0.04271,0.03433,-0.0269,1.0000,0.2449 -7.500,-0.6376,0.04193,0.03360,-0.0248,1.0000,0.2489 -7.250,-0.6188,0.03980,0.03120,-0.0266,0.9782,0.2558 -7.000,-0.5796,0.03839,0.02962,-0.0302,0.9499,0.2622 -6.750,-0.5381,0.03745,0.02858,-0.0333,0.9243,0.2683 -6.500,-0.5063,0.03541,0.02604,-0.0363,0.8999,0.2768 -6.250,-0.4672,0.03486,0.02551,-0.0380,0.8765,0.2816 -6.000,-0.4359,0.03409,0.02458,-0.0388,0.8531,0.2873 -5.750,-0.4124,0.03296,0.02307,-0.0388,0.8309,0.2942 -5.500,-0.3861,0.03236,0.02236,-0.0384,0.8103,0.2990 -5.250,-0.3608,0.03189,0.02177,-0.0377,0.7908,0.3039 -5.000,-0.3383,0.03125,0.02089,-0.0369,0.7725,0.3100 -4.750,-0.3162,0.03056,0.01994,-0.0361,0.7554,0.3160 -4.500,-0.2911,0.03022,0.01956,-0.0352,0.7392,0.3207 -4.250,-0.2669,0.02977,0.01895,-0.0344,0.7245,0.3264 -4.000,-0.2443,0.02923,0.01815,-0.0336,0.7088,0.3332 -3.750,-0.2194,0.02890,0.01780,-0.0328,0.6940,0.3383 -3.500,-0.1944,0.02858,0.01738,-0.0321,0.6807,0.3441 -3.250,-0.1700,0.02819,0.01680,-0.0314,0.6675,0.3509 -3.000,-0.1450,0.02789,0.01644,-0.0308,0.6539,0.3569 -2.750,-0.1193,0.02764,0.01612,-0.0300,0.6422,0.3634 -2.500,-0.0942,0.02737,0.01570,-0.0295,0.6295,0.3709 -2.250,-0.0685,0.02715,0.01545,-0.0289,0.6175,0.3775 -2.000,-0.0421,0.02694,0.01518,-0.0283,0.6067,0.3851 -1.750,-0.0162,0.02679,0.01492,-0.0280,0.5944,0.3939 -1.500,0.0111,0.02659,0.01470,-0.0274,0.5849,0.4017 -1.250,0.0371,0.02652,0.01459,-0.0271,0.5728,0.4113 -1.000,0.0644,0.02638,0.01443,-0.0267,0.5633,0.4206 -0.750,0.0906,0.02634,0.01435,-0.0263,0.5520,0.4322 -0.500,0.1171,0.02625,0.01428,-0.0258,0.5430,0.4431 -0.250,0.1428,0.02624,0.01429,-0.0253,0.5324,0.4562 0.000,0.1689,0.02617,0.01420,-0.0247,0.5237,0.4711 0.250,0.1938,0.02620,0.01435,-0.0241,0.5135,0.4870 0.500,0.2198,0.02612,0.01426,-0.0233,0.5059,0.5062 0.750,0.2435,0.02622,0.01454,-0.0226,0.4954,0.5276 1.000,0.2691,0.02612,0.01446,-0.0217,0.4882,0.5547 1.250,0.2913,0.02627,0.01488,-0.0207,0.4784,0.5849 1.500,0.3155,0.02620,0.01494,-0.0195,0.4710,0.6242 1.750,0.3380,0.02630,0.01530,-0.0182,0.4623,0.6724 2.000,0.3633,0.02632,0.01558,-0.0170,0.4542,0.7342 2.250,0.3994,0.02641,0.01586,-0.0175,0.4462,0.8119 2.500,0.4510,0.02672,0.01627,-0.0214,0.4355,0.8941 2.750,0.5054,0.02708,0.01655,-0.0263,0.4262,0.9620 3.000,0.5480,0.02751,0.01690,-0.0295,0.4170,1.0000 3.250,0.5689,0.02773,0.01687,-0.0283,0.4116,1.0000 3.500,0.5834,0.02854,0.01773,-0.0269,0.4031,1.0000 3.750,0.6037,0.02893,0.01799,-0.0257,0.3970,1.0000 4.000,0.6239,0.02940,0.01834,-0.0245,0.3912,1.0000 4.250,0.6394,0.03025,0.01923,-0.0232,0.3835,1.0000 4.500,0.6614,0.03062,0.01947,-0.0221,0.3779,1.0000 4.750,0.6802,0.03131,0.02013,-0.0209,0.3720,1.0000 5.000,0.6953,0.03228,0.02115,-0.0196,0.3649,1.0000 5.250,0.7178,0.03269,0.02146,-0.0186,0.3598,1.0000 5.500,0.7365,0.03346,0.02219,-0.0175,0.3544,1.0000 5.750,0.7481,0.03476,0.02359,-0.0161,0.3476,1.0000 6.000,0.7694,0.03532,0.02410,-0.0151,0.3427,1.0000 6.250,0.7946,0.03565,0.02429,-0.0144,0.3387,1.0000 6.500,0.7948,0.03779,0.02667,-0.0125,0.3315,1.0000 6.750,0.8112,0.03873,0.02761,-0.0114,0.3265,1.0000 7.000,0.8372,0.03902,0.02780,-0.0107,0.3229,1.0000 7.250,0.8353,0.04136,0.03031,-0.0088,0.3172,1.0000 7.500,0.8316,0.04374,0.03281,-0.0070,0.3114,1.0000 7.750,0.8503,0.04450,0.03353,-0.0061,0.3075,1.0000 8.000,0.8835,0.04433,0.03325,-0.0057,0.3046,1.0000 8.250,0.7624,0.05581,0.04513,-0.0027,0.2942,1.0000 8.500,0.7692,0.05786,0.04717,-0.0023,0.2903,1.0000 8.750,0.8005,0.05739,0.04666,-0.0011,0.2882,1.0000 9.250,0.7117,0.07497,0.06438,-0.0070,0.2715,1.0000 9.750,0.6555,0.09008,0.07956,-0.0128,0.2584,1.0000 10.000,0.6724,0.09136,0.08084,-0.0124,0.2558,1.0000 10.250,0.6959,0.09176,0.08121,-0.0114,0.2540,1.0000 10.750,0.6479,0.10611,0.09566,-0.0175,0.2432,1.0000 11.000,0.6610,0.10809,0.09765,-0.0175,0.2405,1.0000 11.250,0.6817,0.10904,0.09862,-0.0168,0.2385,1.0000 11.500,0.6556,0.11654,0.10616,-0.0204,0.2334,1.0000 11.750,0.6526,0.12092,0.11058,-0.0220,0.2303,1.0000