Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e337-il-50000-n5 Airfoil,e337-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,25.7543 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e337-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.3837,0.11471,0.10812,-0.0156,1.0000,0.1058 -9.750,-0.4044,0.11225,0.10580,-0.0209,1.0000,0.1102 -9.500,-0.4215,0.10897,0.10263,-0.0259,1.0000,0.1108 -9.250,-0.3967,0.10391,0.09762,-0.0227,1.0000,0.1126 -9.000,-0.3841,0.10027,0.09402,-0.0218,1.0000,0.1154 -8.750,-0.3915,0.09177,0.08547,-0.0297,1.0000,0.0647 -8.500,-0.3914,0.08768,0.08145,-0.0306,1.0000,0.0607 -8.000,-0.4136,0.07957,0.07340,-0.0319,1.0000,0.0516 -7.500,-0.4461,0.07209,0.06567,-0.0293,1.0000,0.0445 -7.250,-0.4455,0.06912,0.06274,-0.0276,1.0000,0.0441 -7.000,-0.4506,0.06628,0.05985,-0.0251,1.0000,0.0441 -6.750,-0.4525,0.06374,0.05733,-0.0226,1.0000,0.0436 -6.500,-0.4579,0.06154,0.05513,-0.0194,1.0000,0.0433 -6.250,-0.4388,0.05757,0.05091,-0.0213,0.9727,0.0430 -6.000,-0.4144,0.05351,0.04652,-0.0233,0.9420,0.0424 -5.750,-0.3866,0.04949,0.04207,-0.0252,0.9175,0.0417 -5.500,-0.3587,0.04596,0.03808,-0.0263,0.8935,0.0410 -5.250,-0.3306,0.04268,0.03428,-0.0269,0.8714,0.0405 -5.000,-0.3034,0.03978,0.03083,-0.0267,0.8500,0.0404 -4.750,-0.2772,0.03731,0.02785,-0.0260,0.8285,0.0406 -4.500,-0.2501,0.03520,0.02524,-0.0253,0.8088,0.0415 -4.250,-0.2219,0.03337,0.02282,-0.0243,0.7903,0.0440 -4.000,-0.1932,0.03164,0.02080,-0.0240,0.7726,0.0465 -3.750,-0.1619,0.03014,0.01905,-0.0239,0.7558,0.0491 -3.500,-0.1251,0.02871,0.01727,-0.0244,0.7395,0.0533 -3.250,-0.0851,0.02743,0.01582,-0.0258,0.7237,0.0612 -3.000,-0.0508,0.02636,0.01457,-0.0262,0.7087,0.0715 -2.750,-0.0239,0.02551,0.01359,-0.0257,0.6946,0.0861 -2.500,0.1965,0.02284,0.01325,-0.0536,0.6726,1.0000 -2.250,0.2178,0.02280,0.01286,-0.0527,0.6596,1.0000 -2.000,0.2394,0.02279,0.01256,-0.0520,0.6472,1.0000 -1.750,0.2612,0.02281,0.01230,-0.0512,0.6359,1.0000 -1.250,0.3050,0.02291,0.01190,-0.0496,0.6148,1.0000 -1.000,0.3271,0.02300,0.01177,-0.0488,0.6052,1.0000 -0.750,0.3493,0.02309,0.01168,-0.0481,0.5963,1.0000 -0.500,0.3714,0.02324,0.01167,-0.0473,0.5870,1.0000 -0.250,0.3935,0.02336,0.01160,-0.0465,0.5791,1.0000 0.000,0.4159,0.02357,0.01170,-0.0459,0.5704,1.0000 0.250,0.4385,0.02373,0.01170,-0.0451,0.5631,1.0000 0.500,0.4608,0.02398,0.01188,-0.0445,0.5550,1.0000 0.750,0.4832,0.02419,0.01196,-0.0437,0.5480,1.0000 1.000,0.5052,0.02448,0.01218,-0.0430,0.5408,1.0000 1.250,0.5272,0.02476,0.01239,-0.0422,0.5338,1.0000 1.500,0.5494,0.02502,0.01254,-0.0414,0.5280,1.0000 1.750,0.5705,0.02542,0.01296,-0.0407,0.5205,1.0000 2.000,0.5926,0.02569,0.01314,-0.0398,0.5151,1.0000 2.250,0.6133,0.02615,0.01363,-0.0390,0.5085,1.0000 2.500,0.6342,0.02656,0.01402,-0.0381,0.5023,1.0000 2.750,0.6564,0.02683,0.01420,-0.0371,0.4977,1.0000 3.000,0.6750,0.02750,0.01498,-0.0362,0.4905,1.0000 3.250,0.6957,0.02793,0.01541,-0.0352,0.4852,1.0000 3.500,0.7167,0.02834,0.01579,-0.0342,0.4804,1.0000 3.750,0.7340,0.02910,0.01667,-0.0331,0.4736,1.0000 4.000,0.7544,0.02954,0.01710,-0.0320,0.4687,1.0000 4.250,0.7737,0.03011,0.01773,-0.0308,0.4639,1.0000 4.500,0.7892,0.03097,0.01873,-0.0295,0.4574,1.0000 4.750,0.8092,0.03142,0.01919,-0.0283,0.4527,1.0000 5.000,0.8263,0.03215,0.01999,-0.0270,0.4476,1.0000 5.250,0.8394,0.03317,0.02118,-0.0254,0.4414,1.0000 5.500,0.8591,0.03362,0.02166,-0.0241,0.4368,1.0000 5.750,0.8731,0.03454,0.02268,-0.0225,0.4316,1.0000 6.000,0.8829,0.03572,0.02402,-0.0205,0.4254,1.0000 6.250,0.9024,0.03615,0.02451,-0.0192,0.4210,1.0000 6.500,0.9108,0.03739,0.02589,-0.0170,0.4152,1.0000 6.750,0.9171,0.03872,0.02737,-0.0147,0.4092,1.0000 7.000,0.9376,0.03902,0.02771,-0.0134,0.4050,1.0000 7.250,0.9337,0.04095,0.02983,-0.0102,0.3984,1.0000 7.500,0.9383,0.04224,0.03125,-0.0076,0.3926,1.0000 7.750,0.9626,0.04225,0.03130,-0.0065,0.3888,1.0000 8.000,0.9310,0.04569,0.03493,-0.0011,0.3808,1.0000 8.250,0.9408,0.04650,0.03581,0.0011,0.3758,1.0000 8.750,0.8855,0.05245,0.04186,0.0106,0.3620,1.0000 9.000,0.9224,0.05158,0.04112,0.0111,0.3586,1.0000 9.250,0.8223,0.06073,0.05012,0.0161,0.3457,1.0000 9.500,0.8545,0.05946,0.04895,0.0180,0.3431,1.0000 10.000,0.8245,0.06708,0.05661,0.0194,0.3266,1.0000 11.000,0.7696,0.08385,0.07353,0.0188,0.2915,1.0000 11.250,0.7813,0.08515,0.07492,0.0194,0.2859,1.0000 11.750,0.7818,0.09071,0.08062,0.0194,0.2716,1.0000 12.000,0.7715,0.09500,0.08495,0.0185,0.2631,1.0000 12.250,0.7840,0.09623,0.08629,0.0190,0.2573,1.0000 12.500,0.7737,0.10068,0.09078,0.0180,0.2488,1.0000 12.750,0.7869,0.10183,0.09208,0.0185,0.2432,1.0000 13.000,0.7762,0.10654,0.09682,0.0171,0.2349,1.0000 13.250,0.7904,0.10748,0.09789,0.0177,0.2292,1.0000 13.500,0.7787,0.11260,0.10305,0.0160,0.2212,1.0000 13.750,0.7918,0.11376,0.10433,0.0163,0.2155,1.0000