Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e59-il-100000-n5 Airfoil,e59-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,70.6492 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-e59-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.4062,0.11867,0.11398,-0.0234,1.0000,0.0326 -7.750,-0.4106,0.11668,0.11205,-0.0222,1.0000,0.0326 -7.500,-0.4152,0.11459,0.11002,-0.0211,1.0000,0.0326 -7.250,-0.4158,0.11141,0.10692,-0.0207,1.0000,0.0327 -7.000,-0.4117,0.10642,0.10195,-0.0179,1.0000,0.0333 -6.750,-0.4091,0.10314,0.09869,-0.0162,1.0000,0.0337 -6.500,-0.4089,0.10058,0.09615,-0.0155,1.0000,0.0340 -6.250,-0.3967,0.09696,0.09254,-0.0179,0.9976,0.0346 -6.000,-0.3808,0.09335,0.08893,-0.0210,0.9945,0.0359 -5.750,-0.3632,0.08970,0.08527,-0.0254,0.9905,0.0374 -5.500,-0.3400,0.08576,0.08131,-0.0322,0.9866,0.0408 -5.250,-0.2897,0.08048,0.07594,-0.0524,0.9806,0.0436 -4.750,-0.2486,0.06928,0.06467,-0.0596,0.9743,0.0319 -4.500,-0.2286,0.06542,0.06078,-0.0621,0.9714,0.0299 -4.250,-0.1874,0.05962,0.05487,-0.0720,0.9693,0.0284 -4.000,-0.1373,0.05306,0.04810,-0.0840,0.9674,0.0277 -3.750,-0.0764,0.04586,0.04055,-0.0978,0.9664,0.0297 -3.500,0.0020,0.03700,0.03096,-0.1142,0.9686,0.0306 -3.250,0.0701,0.03023,0.02305,-0.1256,0.9703,0.0330 -3.000,0.1107,0.02866,0.02124,-0.1295,0.9690,0.0380 -2.750,0.1595,0.02598,0.01766,-0.1342,0.9686,0.0431 -2.500,0.1944,0.02473,0.01619,-0.1363,0.9657,0.0498 -2.250,0.2305,0.02381,0.01481,-0.1380,0.9628,0.0570 -2.000,0.2668,0.02280,0.01370,-0.1401,0.9606,0.0633 -1.750,0.3035,0.02211,0.01281,-0.1419,0.9584,0.0690 -1.500,0.3392,0.02158,0.01221,-0.1437,0.9563,0.0759 -1.250,0.3679,0.02130,0.01189,-0.1441,0.9514,0.0873 -1.000,0.4024,0.02096,0.01152,-0.1457,0.9480,0.0985 -0.750,0.4395,0.02066,0.01131,-0.1477,0.9453,0.1233 -0.500,0.4736,0.02037,0.01122,-0.1493,0.9418,0.1985 -0.250,0.5062,0.01978,0.01134,-0.1509,0.9370,0.4225 0.000,0.5323,0.01891,0.01143,-0.1500,0.9331,0.7697 0.500,0.5859,0.01882,0.01123,-0.1494,0.9208,1.0000 0.750,0.6203,0.01894,0.01124,-0.1508,0.9172,1.0000 1.000,0.6480,0.01909,0.01134,-0.1509,0.9109,1.0000 1.250,0.6794,0.01919,0.01139,-0.1516,0.9053,1.0000 1.500,0.7148,0.01916,0.01134,-0.1530,0.9002,1.0000 1.750,0.7443,0.01912,0.01131,-0.1531,0.8911,1.0000 2.000,0.7756,0.01899,0.01122,-0.1535,0.8817,1.0000 2.250,0.8139,0.01866,0.01094,-0.1551,0.8749,1.0000 2.500,0.8439,0.01842,0.01078,-0.1550,0.8629,1.0000 2.750,0.8807,0.01760,0.01003,-0.1555,0.8472,1.0000 3.000,0.9081,0.01706,0.00955,-0.1543,0.8224,1.0000 3.250,0.9384,0.01667,0.00927,-0.1539,0.7982,1.0000 3.500,0.9742,0.01626,0.00895,-0.1547,0.7761,1.0000 3.750,1.0178,0.01565,0.00835,-0.1565,0.7321,1.0000 4.000,1.0774,0.01525,0.00756,-0.1613,0.6165,1.0000 4.250,1.1072,0.01609,0.00777,-0.1611,0.5182,1.0000 4.500,1.1249,0.01716,0.00838,-0.1590,0.4069,1.0000 5.000,1.1552,0.01997,0.01007,-0.1548,0.2087,1.0000 5.250,1.1703,0.02161,0.01110,-0.1529,0.1081,1.0000 5.500,1.1882,0.02291,0.01222,-0.1512,0.0813,1.0000 5.750,1.2073,0.02397,0.01331,-0.1496,0.0698,1.0000 6.000,1.2264,0.02497,0.01444,-0.1480,0.0637,1.0000 6.250,1.2439,0.02616,0.01574,-0.1462,0.0598,1.0000 6.500,1.2623,0.02723,0.01705,-0.1444,0.0548,1.0000 6.750,1.2777,0.02868,0.01853,-0.1425,0.0488,1.0000 7.000,1.2958,0.02994,0.01997,-0.1408,0.0433,1.0000 7.250,1.3107,0.03188,0.02190,-0.1389,0.0384,1.0000 7.500,1.3308,0.03369,0.02395,-0.1375,0.0336,1.0000 7.750,1.3507,0.03589,0.02619,-0.1364,0.0294,1.0000 8.000,1.3743,0.03842,0.02898,-0.1357,0.0259,1.0000 8.250,1.3992,0.04127,0.03233,-0.1348,0.0232,1.0000 8.500,1.4170,0.04363,0.03503,-0.1332,0.0206,1.0000 8.750,1.4298,0.04573,0.03734,-0.1313,0.0187,1.0000 9.000,1.4422,0.04942,0.04130,-0.1295,0.0177,1.0000 9.250,1.4495,0.05363,0.04598,-0.1267,0.0172,1.0000 9.500,1.4514,0.05735,0.05023,-0.1231,0.0168,1.0000 9.750,1.4470,0.06111,0.05449,-0.1189,0.0165,1.0000 10.000,1.4365,0.06466,0.05848,-0.1141,0.0161,1.0000 10.250,1.4226,0.06839,0.06260,-0.1096,0.0157,1.0000 10.500,1.4063,0.07248,0.06705,-0.1057,0.0156,1.0000 10.750,1.3883,0.07682,0.07171,-0.1025,0.0154,1.0000 11.000,1.3686,0.08160,0.07680,-0.1003,0.0153,1.0000 11.250,1.3476,0.08691,0.08237,-0.0992,0.0154,1.0000 11.500,1.3256,0.09287,0.08857,-0.0994,0.0155,1.0000 11.750,1.3039,0.09935,0.09527,-0.1011,0.0156,1.0000