Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e337-il-500000-n5 Airfoil,e337-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,84.1374 Max Cl/Cd alpha,9.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e337-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.3998,0.11123,0.10893,-0.0154,1.0000,0.0091 -10.750,-0.3936,0.10941,0.10714,-0.0149,1.0000,0.0095 -10.250,-0.3942,0.10057,0.09835,-0.0188,1.0000,0.0094 -9.500,-0.3477,0.08443,0.08175,-0.0384,0.8131,0.0084 -9.250,-0.3592,0.07884,0.07602,-0.0414,0.7742,0.0087 -9.000,-0.3652,0.07531,0.07238,-0.0436,0.7425,0.0082 -8.750,-0.3820,0.07028,0.06724,-0.0463,0.7220,0.0083 -8.500,-0.3980,0.06631,0.06317,-0.0461,0.7044,0.0084 -8.250,-0.4146,0.06297,0.05971,-0.0439,0.6895,0.0079 -7.750,-0.4315,0.05532,0.05175,-0.0401,0.6628,0.0077 -7.500,-0.4355,0.05111,0.04733,-0.0377,0.6518,0.0075 -7.250,-0.4536,0.04196,0.03774,-0.0325,0.6458,0.0069 -7.000,-0.4509,0.03767,0.03315,-0.0293,0.6352,0.0069 -6.750,-0.4284,0.03915,0.03462,-0.0295,0.6202,0.0074 -6.250,-0.4293,0.02487,0.01898,-0.0190,0.6063,0.0069 -5.750,-0.3910,0.02116,0.01454,-0.0156,0.5838,0.0067 -5.500,-0.3693,0.01971,0.01281,-0.0144,0.5732,0.0067 -5.250,-0.3460,0.01844,0.01127,-0.0134,0.5626,0.0067 -5.000,-0.3214,0.01732,0.00992,-0.0126,0.5531,0.0067 -4.750,-0.2964,0.01641,0.00881,-0.0119,0.5439,0.0067 -4.500,-0.2712,0.01567,0.00792,-0.0113,0.5345,0.0067 -4.250,-0.2462,0.01500,0.00712,-0.0106,0.5252,0.0067 -4.000,-0.2216,0.01441,0.00643,-0.0099,0.5159,0.0068 -3.750,-0.1978,0.01378,0.00572,-0.0090,0.5076,0.0069 -3.500,-0.1740,0.01330,0.00517,-0.0081,0.4997,0.0071 -3.250,-0.1497,0.01292,0.00473,-0.0074,0.4924,0.0073 -3.000,-0.1253,0.01261,0.00435,-0.0066,0.4845,0.0075 -2.750,-0.1006,0.01235,0.00403,-0.0059,0.4770,0.0078 -2.500,-0.0759,0.01210,0.00372,-0.0051,0.4694,0.0083 -2.250,-0.0509,0.01190,0.00346,-0.0045,0.4629,0.0088 -2.000,-0.0260,0.01168,0.00320,-0.0038,0.4564,0.0101 -1.750,-0.0010,0.01153,0.00299,-0.0032,0.4502,0.0120 -1.500,0.0241,0.01133,0.00281,-0.0025,0.4443,0.0195 -1.250,0.0486,0.01115,0.00268,-0.0019,0.4377,0.0388 -1.000,0.0722,0.01088,0.00258,-0.0011,0.4323,0.0872 -0.750,0.0909,0.01021,0.00244,0.0005,0.4274,0.2442 -0.500,0.0764,0.00810,0.00263,0.0093,0.4242,0.8455 0.000,0.1243,0.00862,0.00303,0.0119,0.4145,0.8960 0.250,0.1511,0.00896,0.00331,0.0128,0.4090,0.9085 0.500,0.1742,0.00922,0.00349,0.0142,0.4044,0.9189 0.750,0.2152,0.00966,0.00387,0.0121,0.3996,0.9249 1.000,0.2440,0.00981,0.00395,0.0120,0.3949,0.9291 1.250,0.2643,0.00980,0.00388,0.0136,0.3907,0.9319 1.500,0.2859,0.00980,0.00382,0.0148,0.3867,0.9341 1.750,0.3143,0.00982,0.00380,0.0147,0.3826,0.9347 2.000,0.3425,0.00987,0.00379,0.0145,0.3785,0.9355 2.250,0.3700,0.00992,0.00379,0.0145,0.3744,0.9363 2.500,0.3975,0.00997,0.00381,0.0145,0.3708,0.9371 2.750,0.4251,0.01002,0.00383,0.0145,0.3669,0.9381 3.000,0.4518,0.01007,0.00385,0.0146,0.3631,0.9390 3.250,0.4776,0.01013,0.00387,0.0149,0.3591,0.9400 3.500,0.5033,0.01018,0.00390,0.0152,0.3558,0.9411 3.750,0.5290,0.01023,0.00394,0.0156,0.3523,0.9425 4.000,0.5537,0.01028,0.00398,0.0161,0.3486,0.9438 4.250,0.5775,0.01034,0.00402,0.0168,0.3449,0.9451 4.500,0.6006,0.01040,0.00406,0.0176,0.3417,0.9465 4.750,0.6242,0.01043,0.00411,0.0183,0.3384,0.9478 5.000,0.6498,0.01049,0.00418,0.0186,0.3346,0.9488 5.250,0.6769,0.01059,0.00427,0.0185,0.3309,0.9496 5.500,0.7032,0.01071,0.00437,0.0186,0.3274,0.9503 5.750,0.7303,0.01078,0.00447,0.0186,0.3238,0.9510 6.000,0.7568,0.01087,0.00459,0.0186,0.3200,0.9518 6.250,0.7827,0.01098,0.00471,0.0188,0.3159,0.9527 6.500,0.8080,0.01111,0.00484,0.0190,0.3119,0.9536 6.750,0.8340,0.01120,0.00497,0.0191,0.3071,0.9546 7.000,0.8589,0.01132,0.00510,0.0194,0.3018,0.9557 7.250,0.8829,0.01147,0.00525,0.0199,0.2978,0.9570 7.500,0.9079,0.01157,0.00542,0.0202,0.2935,0.9582 7.750,0.9316,0.01169,0.00557,0.0207,0.2890,0.9598 8.000,0.9537,0.01185,0.00574,0.0215,0.2842,0.9615 8.250,0.9782,0.01198,0.00592,0.0219,0.2780,0.9626 8.500,1.0033,0.01218,0.00613,0.0220,0.2709,0.9635 8.750,1.0289,0.01236,0.00636,0.0220,0.2648,0.9645 9.000,1.0534,0.01259,0.00661,0.0222,0.2569,0.9656 9.250,1.0778,0.01281,0.00687,0.0224,0.2494,0.9669 9.500,1.1006,0.01310,0.00716,0.0228,0.2410,0.9684 9.750,1.1237,0.01336,0.00746,0.0232,0.2319,0.9701 10.000,1.1445,0.01369,0.00780,0.0239,0.2220,0.9721 10.250,1.1630,0.01405,0.00816,0.0250,0.2121,0.9746 10.750,1.2082,0.01505,0.00915,0.0252,0.1868,0.9776 11.000,1.2288,0.01563,0.00973,0.0255,0.1740,0.9799 11.250,1.2462,0.01628,0.01036,0.0263,0.1609,0.9829 11.500,1.2624,0.01700,0.01108,0.0271,0.1480,0.9860 11.750,1.2804,0.01794,0.01200,0.0270,0.1337,0.9883 12.000,1.2966,0.01897,0.01302,0.0271,0.1206,0.9912 12.250,1.3108,0.02006,0.01412,0.0272,0.1106,0.9952 12.500,1.3179,0.02129,0.01537,0.0283,0.1017,1.0000 13.000,1.3076,0.02413,0.01825,0.0339,0.0890,1.0000 13.250,1.3048,0.02613,0.02028,0.0351,0.0820,1.0000 13.500,1.3006,0.02852,0.02270,0.0359,0.0757,1.0000 13.750,1.3003,0.03076,0.02501,0.0363,0.0711,1.0000 14.000,1.2967,0.03344,0.02774,0.0364,0.0667,1.0000 14.250,1.2915,0.03638,0.03074,0.0364,0.0621,1.0000 14.500,1.2853,0.03950,0.03391,0.0363,0.0580,1.0000 14.750,1.2771,0.04291,0.03738,0.0360,0.0550,1.0000 15.000,1.2713,0.04612,0.04066,0.0356,0.0518,1.0000 15.250,1.2621,0.04976,0.04436,0.0351,0.0487,1.0000 15.500,1.2534,0.05341,0.04808,0.0344,0.0466,1.0000 15.750,1.2468,0.05699,0.05173,0.0337,0.0440,1.0000 16.000,1.2395,0.06071,0.05553,0.0328,0.0417,1.0000 16.250,1.2308,0.06471,0.05958,0.0318,0.0395,1.0000 16.500,1.2232,0.06869,0.06363,0.0307,0.0372,1.0000 16.750,1.2170,0.07252,0.06754,0.0295,0.0350,1.0000 17.000,1.2095,0.07663,0.07172,0.0282,0.0332,1.0000 17.250,1.2008,0.08099,0.07613,0.0268,0.0311,1.0000 17.500,1.1964,0.08477,0.07999,0.0255,0.0296,1.0000