Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-c5a-il-50000-n5 Airfoil,c5a-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,27.0615 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-c5a-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.6366,0.09895,0.09099,-0.0473,1.0000,0.0505 -11.750,-0.6691,0.08996,0.08196,-0.0523,1.0000,0.0495 -11.500,-0.7049,0.08257,0.07448,-0.0554,1.0000,0.0487 -11.250,-0.7389,0.07694,0.06869,-0.0561,1.0000,0.0482 -11.000,-0.7697,0.07265,0.06422,-0.0548,1.0000,0.0477 -10.750,-0.7977,0.06934,0.06072,-0.0518,1.0000,0.0474 -10.500,-0.8223,0.06662,0.05781,-0.0475,1.0000,0.0473 -10.250,-0.8382,0.06372,0.05468,-0.0439,1.0000,0.0472 -10.000,-0.8477,0.06091,0.05164,-0.0405,1.0000,0.0472 -9.750,-0.8526,0.05818,0.04867,-0.0374,1.0000,0.0474 -9.500,-0.8525,0.05566,0.04595,-0.0346,1.0000,0.0479 -9.250,-0.8494,0.05333,0.04341,-0.0321,1.0000,0.0488 -9.000,-0.8446,0.05107,0.04092,-0.0296,1.0000,0.0498 -8.750,-0.8379,0.04881,0.03839,-0.0271,1.0000,0.0510 -8.500,-0.8284,0.04655,0.03583,-0.0249,1.0000,0.0522 -8.250,-0.8153,0.04434,0.03329,-0.0229,1.0000,0.0532 -8.000,-0.7984,0.04223,0.03086,-0.0212,1.0000,0.0542 -7.750,-0.7782,0.04033,0.02863,-0.0198,1.0000,0.0553 -7.500,-0.7557,0.03857,0.02677,-0.0189,1.0000,0.0570 -7.250,-0.7360,0.03718,0.02538,-0.0177,1.0000,0.0599 -7.000,-0.7156,0.03596,0.02405,-0.0163,1.0000,0.0635 -6.750,-0.6944,0.03483,0.02268,-0.0148,1.0000,0.0668 -6.500,-0.6782,0.03360,0.02150,-0.0129,1.0000,0.0701 -6.250,-0.6643,0.03254,0.02039,-0.0108,1.0000,0.0754 -6.000,-0.6517,0.03145,0.01925,-0.0084,1.0000,0.0817 -5.750,-0.6399,0.03035,0.01815,-0.0061,1.0000,0.0897 -5.500,-0.6284,0.02919,0.01703,-0.0038,1.0000,0.1023 -5.250,-0.6180,0.02778,0.01578,-0.0014,1.0000,0.1295 -5.000,-0.6117,0.02571,0.01439,0.0010,1.0000,0.2017 -4.750,-0.6089,0.02356,0.01361,0.0043,1.0000,0.3939 -4.500,-0.5973,0.02330,0.01409,0.0086,1.0000,0.5449 -4.250,-0.5866,0.02389,0.01492,0.0138,1.0000,0.6404 -4.000,-0.5744,0.02482,0.01588,0.0192,1.0000,0.6963 -3.750,-0.5581,0.02526,0.01618,0.0227,1.0000,0.7255 -3.500,-0.5386,0.02565,0.01642,0.0255,1.0000,0.7460 -3.250,-0.5200,0.02595,0.01656,0.0283,1.0000,0.7668 -3.000,-0.5020,0.02611,0.01656,0.0308,1.0000,0.7868 -2.750,-0.4835,0.02618,0.01649,0.0330,1.0000,0.8049 -2.500,-0.4619,0.02622,0.01637,0.0345,1.0000,0.8188 -2.250,-0.4396,0.02614,0.01615,0.0354,1.0000,0.8302 -2.000,-0.4195,0.02596,0.01585,0.0365,1.0000,0.8421 -1.750,-0.4004,0.02576,0.01553,0.0376,1.0000,0.8545 -1.500,-0.3774,0.02568,0.01532,0.0381,1.0000,0.8652 -1.250,-0.3543,0.02558,0.01513,0.0385,1.0000,0.8761 -1.000,-0.3325,0.02547,0.01493,0.0389,1.0000,0.8877 -0.750,-0.3092,0.02540,0.01478,0.0390,1.0000,0.8994 -0.500,-0.2812,0.02543,0.01474,0.0382,1.0000,0.9094 -0.250,-0.2526,0.02547,0.01472,0.0371,0.9992,0.9202 0.000,-0.2081,0.02573,0.01490,0.0328,0.9933,0.9287 0.250,-0.1630,0.02599,0.01511,0.0283,0.9871,0.9365 0.500,-0.1193,0.02622,0.01531,0.0241,0.9808,0.9447 0.750,-0.0712,0.02653,0.01560,0.0190,0.9751,0.9519 1.000,-0.0281,0.02672,0.01581,0.0148,0.9678,0.9596 1.250,0.0215,0.02701,0.01613,0.0093,0.9618,0.9659 1.500,0.0659,0.02721,0.01639,0.0049,0.9539,0.9733 1.750,0.1140,0.02744,0.01670,-0.0003,0.9466,0.9793 2.000,0.1615,0.02762,0.01699,-0.0053,0.9380,0.9861 2.250,0.2078,0.02771,0.01721,-0.0100,0.9267,0.9927 2.500,0.2561,0.02776,0.01741,-0.0149,0.9154,0.9988 2.750,0.2917,0.02772,0.01751,-0.0173,0.9036,1.0000 3.000,0.3261,0.02759,0.01753,-0.0192,0.8906,1.0000 3.250,0.3534,0.02726,0.01734,-0.0193,0.8702,1.0000 3.500,0.4014,0.02645,0.01675,-0.0222,0.8474,1.0000 3.750,0.4422,0.02544,0.01593,-0.0233,0.8189,1.0000 4.000,0.4757,0.02461,0.01528,-0.0232,0.7910,1.0000 4.250,0.5049,0.02398,0.01484,-0.0225,0.7636,1.0000 4.500,0.5286,0.02342,0.01443,-0.0208,0.7282,1.0000 4.750,0.5677,0.02248,0.01345,-0.0205,0.6555,1.0000 5.000,0.6032,0.02229,0.01261,-0.0197,0.5053,1.0000 5.250,0.6063,0.02313,0.01262,-0.0150,0.3720,1.0000 5.500,0.6055,0.02413,0.01303,-0.0102,0.2890,1.0000 5.750,0.6090,0.02511,0.01365,-0.0064,0.2356,1.0000 6.000,0.6163,0.02614,0.01437,-0.0034,0.1981,1.0000 6.250,0.6278,0.02720,0.01525,-0.0011,0.1714,1.0000 6.500,0.6424,0.02828,0.01618,0.0007,0.1521,1.0000 6.750,0.6617,0.02935,0.01720,0.0018,0.1386,1.0000 7.000,0.6868,0.03047,0.01839,0.0021,0.1278,1.0000 7.250,0.7140,0.03165,0.01959,0.0020,0.1185,1.0000 7.500,0.7412,0.03284,0.02080,0.0019,0.1106,1.0000 7.750,0.7736,0.03430,0.02242,0.0011,0.1052,1.0000 8.000,0.8014,0.03573,0.02401,0.0010,0.0998,1.0000 8.250,0.8268,0.03722,0.02551,0.0009,0.0951,1.0000 8.500,0.8515,0.03907,0.02773,0.0013,0.0911,1.0000 8.750,0.8735,0.04092,0.02981,0.0019,0.0874,1.0000 9.000,0.8938,0.04259,0.03154,0.0024,0.0838,1.0000 9.250,0.9095,0.04491,0.03423,0.0039,0.0809,1.0000 9.500,0.9212,0.04750,0.03728,0.0058,0.0784,1.0000 9.750,0.9305,0.04987,0.03999,0.0078,0.0755,1.0000 10.000,0.9409,0.05196,0.04225,0.0094,0.0729,1.0000 10.250,0.9523,0.05431,0.04471,0.0107,0.0709,1.0000 10.500,0.9502,0.05751,0.04829,0.0136,0.0697,1.0000 10.750,0.9386,0.06090,0.05214,0.0172,0.0686,1.0000 11.000,0.9223,0.06423,0.05583,0.0208,0.0677,1.0000 11.250,0.9024,0.06776,0.05964,0.0241,0.0670,1.0000 11.500,0.8796,0.07176,0.06389,0.0264,0.0667,1.0000 11.750,0.8537,0.07647,0.06881,0.0273,0.0666,1.0000 12.000,0.8247,0.08223,0.07474,0.0264,0.0669,1.0000 12.250,0.7939,0.08938,0.08200,0.0234,0.0674,1.0000 12.500,0.7639,0.09811,0.09080,0.0182,0.0681,1.0000