Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e858-il-100000-n5 Airfoil,e858-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,34.5522 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-e858-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -15.750,-0.4582,0.11505,0.10911,-0.0623,1.0000,0.0346 -15.500,-0.5023,0.10320,0.09699,-0.0681,1.0000,0.0347 -15.250,-0.5300,0.09521,0.08876,-0.0718,1.0000,0.0350 -15.000,-0.5324,0.09201,0.08558,-0.0726,1.0000,0.0355 -14.750,-0.5384,0.08832,0.08186,-0.0736,1.0000,0.0361 -14.500,-0.5464,0.08443,0.07792,-0.0746,1.0000,0.0367 -14.250,-0.5549,0.08062,0.07402,-0.0755,1.0000,0.0374 -14.000,-0.5617,0.07724,0.07055,-0.0760,1.0000,0.0380 -13.750,-0.5700,0.07383,0.06701,-0.0764,1.0000,0.0389 -13.500,-0.5734,0.07133,0.06450,-0.0761,1.0000,0.0396 -13.250,-0.5766,0.06913,0.06233,-0.0756,1.0000,0.0403 -13.000,-0.5817,0.06691,0.06011,-0.0750,1.0000,0.0411 -12.750,-0.5885,0.06470,0.05789,-0.0741,1.0000,0.0421 -12.500,-0.5816,0.06203,0.05510,-0.0759,0.9973,0.0439 -12.250,-0.5618,0.05919,0.05229,-0.0805,0.9917,0.0460 -12.000,-0.5431,0.05635,0.04934,-0.0844,0.9846,0.0489 -11.750,-0.5255,0.05373,0.04673,-0.0878,0.9766,0.0514 -11.500,-0.5101,0.05127,0.04422,-0.0903,0.9653,0.0545 -11.250,-0.5005,0.04883,0.04179,-0.0918,0.9495,0.0573 -10.750,-0.4785,0.04415,0.03702,-0.0951,0.9177,0.0652 -10.500,-0.4671,0.04178,0.03467,-0.0969,0.9021,0.0692 -10.250,-0.4537,0.03942,0.03226,-0.0991,0.8866,0.0746 -10.000,-0.4375,0.03711,0.02990,-0.1015,0.8711,0.0807 -9.750,-0.4188,0.03477,0.02748,-0.1045,0.8556,0.0880 -9.500,-0.3987,0.03242,0.02504,-0.1080,0.8395,0.0964 -9.000,-0.3570,0.02852,0.02093,-0.1137,0.8038,0.1169 -8.750,-0.3359,0.02709,0.01941,-0.1152,0.7856,0.1293 -8.500,-0.3168,0.02589,0.01813,-0.1159,0.7683,0.1434 -8.250,-0.2966,0.02483,0.01698,-0.1164,0.7520,0.1599 -8.000,-0.2762,0.02386,0.01595,-0.1167,0.7367,0.1785 -7.750,-0.2613,0.02306,0.01518,-0.1156,0.7214,0.1983 -7.500,-0.2409,0.02238,0.01450,-0.1153,0.7079,0.2234 -7.250,-0.2196,0.02191,0.01408,-0.1148,0.6943,0.2510 -7.000,-0.1982,0.02167,0.01384,-0.1140,0.6814,0.2773 -6.750,-0.1717,0.02159,0.01366,-0.1139,0.6696,0.3017 -6.500,-0.1498,0.02159,0.01358,-0.1128,0.6573,0.3208 -6.000,-0.1002,0.02171,0.01342,-0.1116,0.6351,0.3519 -5.750,-0.0742,0.02173,0.01317,-0.1113,0.6254,0.3661 -5.500,-0.0503,0.02196,0.01340,-0.1102,0.6148,0.3753 -5.250,-0.0259,0.02192,0.01308,-0.1097,0.6054,0.3871 -5.000,-0.0005,0.02217,0.01332,-0.1088,0.5960,0.3944 -4.750,0.0232,0.02220,0.01317,-0.1080,0.5869,0.4041 -4.500,0.0496,0.02230,0.01312,-0.1076,0.5790,0.4116 -4.250,0.0730,0.02244,0.01323,-0.1065,0.5703,0.4187 -4.000,0.0972,0.02238,0.01292,-0.1060,0.5627,0.4278 -3.750,0.1227,0.02250,0.01299,-0.1053,0.5554,0.4335 -3.500,0.1461,0.02261,0.01306,-0.1043,0.5473,0.4398 -3.250,0.1709,0.02259,0.01285,-0.1038,0.5404,0.4475 -3.000,0.1955,0.02256,0.01268,-0.1033,0.5338,0.4534 -2.750,0.2190,0.02262,0.01274,-0.1024,0.5267,0.4577 -2.500,0.2441,0.02263,0.01265,-0.1018,0.5207,0.4625 -2.250,0.2707,0.02263,0.01244,-0.1017,0.5154,0.4680 -2.000,0.2932,0.02256,0.01225,-0.1010,0.5089,0.4736 -1.750,0.3171,0.02256,0.01223,-0.1002,0.5028,0.4770 -1.500,0.3428,0.02259,0.01216,-0.0998,0.4976,0.4806 -1.250,0.3675,0.02265,0.01215,-0.0992,0.4924,0.4850 -1.000,0.3903,0.02269,0.01214,-0.0984,0.4867,0.4899 -0.750,0.4147,0.02272,0.01204,-0.0980,0.4817,0.4949 -0.500,0.4408,0.02275,0.01196,-0.0977,0.4774,0.4988 -0.250,0.4669,0.02285,0.01200,-0.0975,0.4734,0.5025 0.000,0.4884,0.02297,0.01215,-0.0964,0.4685,0.5068 0.250,0.5114,0.02307,0.01222,-0.0956,0.4637,0.5118 0.500,0.5361,0.02316,0.01220,-0.0952,0.4594,0.5168 0.750,0.5629,0.02326,0.01215,-0.0952,0.4557,0.5213 1.000,0.5858,0.02341,0.01233,-0.0943,0.4518,0.5251 1.250,0.6068,0.02360,0.01256,-0.0932,0.4477,0.5297 1.500,0.6294,0.02378,0.01273,-0.0924,0.4439,0.5351 1.750,0.6536,0.02395,0.01283,-0.0919,0.4404,0.5408 2.000,0.6791,0.02410,0.01292,-0.0917,0.4373,0.5455 2.250,0.7070,0.02429,0.01303,-0.0918,0.4344,0.5501 2.500,0.7236,0.02456,0.01340,-0.0900,0.4307,0.5554 2.750,0.7428,0.02482,0.01369,-0.0887,0.4269,0.5614 3.000,0.7642,0.02507,0.01393,-0.0878,0.4235,0.5676 3.250,0.7866,0.02529,0.01417,-0.0870,0.4206,0.5730 3.500,0.8112,0.02552,0.01437,-0.0866,0.4180,0.5792 3.750,0.8391,0.02578,0.01456,-0.0869,0.4157,0.5864 4.000,0.8556,0.02613,0.01499,-0.0851,0.4129,0.5928 4.250,0.8674,0.02650,0.01548,-0.0826,0.4098,0.5993 4.500,0.8819,0.02687,0.01591,-0.0806,0.4067,0.6074 4.750,0.8997,0.02722,0.01629,-0.0791,0.4038,0.6153 5.000,0.9207,0.02753,0.01663,-0.0782,0.4012,0.6234 5.250,0.9452,0.02784,0.01691,-0.0779,0.3988,0.6334 5.500,0.9723,0.02814,0.01721,-0.0781,0.3969,0.6435 5.750,0.9892,0.02866,0.01779,-0.0766,0.3947,0.6554 6.000,0.9937,0.02936,0.01868,-0.0733,0.3920,0.6663 6.250,1.0012,0.03005,0.01951,-0.0705,0.3892,0.6800 6.500,1.0114,0.03065,0.02024,-0.0682,0.3865,0.6949 6.750,1.0260,0.03114,0.02082,-0.0665,0.3839,0.7133 7.000,1.0445,0.03151,0.02130,-0.0653,0.3817,0.7377 7.250,1.0665,0.03177,0.02166,-0.0646,0.3798,0.7728 7.500,1.0949,0.03189,0.02196,-0.0649,0.3781,0.8455 7.750,1.1078,0.03271,0.02294,-0.0637,0.3759,1.0000 8.000,1.0923,0.03440,0.02479,-0.0589,0.3731,1.0000 8.250,1.0793,0.03623,0.02674,-0.0548,0.3700,1.0000 8.500,1.0735,0.03792,0.02850,-0.0519,0.3671,1.0000 8.750,1.0799,0.03914,0.02973,-0.0503,0.3645,1.0000 9.000,1.0974,0.03990,0.03045,-0.0497,0.3626,1.0000 9.250,1.1224,0.04033,0.03083,-0.0498,0.3610,1.0000 9.500,1.1530,0.04057,0.03100,-0.0504,0.3596,1.0000 10.000,0.9091,0.06438,0.05558,-0.0388,0.3408,1.0000 10.250,0.9555,0.06215,0.05327,-0.0388,0.3415,1.0000