Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e337-il-50000 Airfoil,e337-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,15.9739 Max Cl/Cd alpha,1 Url,http://airfoiltools.com/polar/csv?polar=xf-e337-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.3934,0.11671,0.11036,-0.0108,1.0000,0.2062 -9.500,-0.3737,0.11211,0.10579,-0.0094,1.0000,0.2182 -9.250,-0.4017,0.11108,0.10492,-0.0127,1.0000,0.2232 -9.000,-0.3862,0.10699,0.10087,-0.0114,1.0000,0.2386 -8.750,-0.3772,0.10341,0.09736,-0.0105,1.0000,0.2541 -8.500,-0.3715,0.10017,0.09421,-0.0099,1.0000,0.2699 -8.250,-0.3779,0.09756,0.09172,-0.0096,1.0000,0.2872 -8.000,-0.3545,0.09342,0.08763,-0.0073,1.0000,0.3095 -7.750,-0.3551,0.09101,0.08533,-0.0059,1.0000,0.3339 -7.500,-0.3382,0.08775,0.08215,-0.0037,1.0000,0.3618 -7.250,-0.3301,0.08522,0.07972,-0.0011,1.0000,0.3967 -7.000,-0.3106,0.08235,0.07692,0.0025,1.0000,0.4441 -6.750,-0.2991,0.08040,0.07507,0.0065,1.0000,0.4965 -6.500,-0.2487,0.07672,0.07141,0.0097,1.0000,0.5735 -6.250,-0.1954,0.07297,0.06766,0.0113,1.0000,0.6646 -5.500,-0.2041,0.06556,0.06075,0.0131,1.0000,0.6623 -5.250,-0.2678,0.06581,0.06145,0.0184,1.0000,0.6271 -5.000,-0.3073,0.06735,0.06327,0.0258,1.0000,0.6296 -4.750,-0.3832,0.06161,0.05764,0.0122,0.9626,0.5229 -4.500,-0.3918,0.05075,0.04456,-0.0200,0.9285,0.2186 -4.250,-0.3349,0.04566,0.03809,-0.0239,0.9148,0.1375 -4.000,-0.2857,0.04195,0.03364,-0.0267,0.9011,0.1195 -3.750,-0.2437,0.03936,0.03028,-0.0279,0.8862,0.1127 -3.500,-0.2011,0.03700,0.02743,-0.0295,0.8713,0.1125 -3.250,0.1885,0.02410,0.01691,-0.0772,0.8786,1.0000 -3.000,0.2173,0.02409,0.01632,-0.0775,0.8546,1.0000 -2.750,0.2396,0.02427,0.01609,-0.0768,0.8333,1.0000 -2.500,0.2596,0.02453,0.01602,-0.0757,0.8139,1.0000 -2.250,0.2793,0.02484,0.01603,-0.0746,0.7965,1.0000 -2.000,0.2989,0.02518,0.01612,-0.0735,0.7810,1.0000 -1.750,0.3190,0.02556,0.01625,-0.0725,0.7669,1.0000 -1.500,0.3398,0.02593,0.01639,-0.0715,0.7541,1.0000 -1.250,0.3597,0.02638,0.01665,-0.0705,0.7413,1.0000 -1.000,0.3790,0.02696,0.01708,-0.0697,0.7290,1.0000 -0.750,0.3984,0.02752,0.01749,-0.0687,0.7184,1.0000 -0.500,0.4183,0.02799,0.01779,-0.0675,0.7084,1.0000 -0.250,0.4365,0.02880,0.01852,-0.0669,0.6976,1.0000 0.000,0.4565,0.02936,0.01893,-0.0657,0.6894,1.0000 0.250,0.4740,0.03025,0.01977,-0.0650,0.6794,1.0000 0.500,0.4924,0.03105,0.02048,-0.0640,0.6712,1.0000 0.750,0.5096,0.03198,0.02136,-0.0631,0.6626,1.0000 1.000,0.5265,0.03296,0.02229,-0.0621,0.6549,1.0000 1.250,0.5418,0.03409,0.02339,-0.0611,0.6468,1.0000 1.500,0.5587,0.03508,0.02432,-0.0599,0.6400,1.0000 1.750,0.5682,0.03675,0.02602,-0.0589,0.6321,1.0000 2.000,0.5895,0.03736,0.02654,-0.0576,0.6264,1.0000 2.250,0.5879,0.03991,0.02918,-0.0561,0.6184,1.0000 2.500,0.6026,0.04109,0.03033,-0.0547,0.6124,1.0000 2.750,0.6043,0.04327,0.03253,-0.0529,0.6063,1.0000 3.000,0.5970,0.04592,0.03522,-0.0505,0.6000,1.0000 3.250,0.6187,0.04672,0.03597,-0.0493,0.5947,1.0000 3.500,0.5927,0.05048,0.03977,-0.0458,0.5903,1.0000 3.750,0.5599,0.05416,0.04344,-0.0414,0.5872,1.0000 4.000,0.5260,0.05724,0.04649,-0.0361,0.5858,1.0000 4.250,0.4980,0.06008,0.04930,-0.0315,0.5866,1.0000 4.500,0.4803,0.06269,0.05188,-0.0282,0.5880,1.0000 4.750,0.4710,0.06518,0.05435,-0.0259,0.5901,1.0000 5.000,0.4741,0.06773,0.05690,-0.0250,0.5944,1.0000 5.250,0.3199,0.07423,0.06346,-0.0187,0.7414,1.0000 5.500,0.3274,0.07560,0.06480,-0.0172,0.7272,1.0000 5.750,0.3348,0.07717,0.06633,-0.0158,0.7149,1.0000 6.000,0.3548,0.07973,0.06888,-0.0162,0.7053,1.0000 6.250,0.3758,0.08206,0.07120,-0.0163,0.6916,1.0000 6.500,0.3768,0.08307,0.07218,-0.0141,0.6777,1.0000 6.750,0.3801,0.08458,0.07368,-0.0125,0.6660,1.0000 7.000,0.4039,0.08766,0.07677,-0.0133,0.6574,1.0000 7.250,0.4153,0.08941,0.07853,-0.0124,0.6436,1.0000 7.500,0.4144,0.09059,0.07971,-0.0104,0.6307,1.0000 7.750,0.4223,0.09272,0.08184,-0.0096,0.6212,1.0000 8.000,0.4525,0.09623,0.08539,-0.0108,0.6102,1.0000 8.250,0.4468,0.09700,0.08615,-0.0086,0.5971,1.0000 8.500,0.4496,0.09889,0.08805,-0.0076,0.5870,1.0000 8.750,0.4832,0.10305,0.09230,-0.0091,0.5778,1.0000 9.000,0.4744,0.10361,0.09286,-0.0070,0.5648,1.0000 9.250,0.4766,0.10561,0.09488,-0.0061,0.5548,1.0000