Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e604-il-50000 Airfoil,e604-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,5.18241 Max Cl/Cd alpha,12 Url,http://airfoiltools.com/polar/csv?polar=xf-e604-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.6387,0.09930,0.09416,-0.0404,1.0000,0.1387 -8.500,-0.6387,0.09519,0.09005,-0.0392,1.0000,0.1310 -8.250,-0.6881,0.09139,0.08622,-0.0369,1.0000,0.1274 -8.000,-0.7623,0.08626,0.08056,-0.0351,1.0000,0.1213 -7.750,-0.7538,0.08203,0.07642,-0.0338,1.0000,0.1175 -7.500,-0.7688,0.07738,0.07152,-0.0324,1.0000,0.1134 -7.250,-0.7911,0.07167,0.06492,-0.0313,1.0000,0.1062 -7.000,-0.7865,0.06781,0.06086,-0.0302,1.0000,0.1049 -6.750,-0.7820,0.06403,0.05668,-0.0292,1.0000,0.1046 -6.500,-0.7739,0.06048,0.05267,-0.0284,1.0000,0.1048 -6.250,-0.7619,0.05732,0.04902,-0.0277,1.0000,0.1053 -6.000,-0.7469,0.05433,0.04548,-0.0270,1.0000,0.1064 -5.750,-0.7297,0.05165,0.04233,-0.0262,1.0000,0.1076 -5.500,-0.7132,0.04939,0.04018,-0.0254,1.0000,0.1129 -5.250,-0.6942,0.04756,0.03802,-0.0246,1.0000,0.1183 -5.000,-0.6746,0.04565,0.03584,-0.0236,1.0000,0.1246 -4.750,-0.6555,0.04432,0.03440,-0.0224,1.0000,0.1349 -4.500,-0.6369,0.04304,0.03319,-0.0209,1.0000,0.1466 -4.250,-0.6186,0.04205,0.03228,-0.0189,1.0000,0.1623 -4.000,-0.6010,0.04123,0.03151,-0.0168,1.0000,0.1851 -3.750,-0.5862,0.04011,0.03080,-0.0146,1.0000,0.2195 -3.500,-0.5715,0.03773,0.02952,-0.0138,1.0000,0.3080 -3.250,-0.5867,0.03975,0.03385,0.0005,1.0000,0.6462 -3.000,-0.5935,0.04295,0.03687,0.0125,1.0000,0.7101 -2.750,-0.5973,0.04506,0.03884,0.0228,1.0000,0.7481 -2.500,-0.5974,0.04654,0.04017,0.0317,1.0000,0.7834 -2.250,-0.5920,0.04769,0.04112,0.0389,1.0000,0.8172 -2.000,-0.5769,0.04884,0.04203,0.0439,1.0000,0.8521 -1.750,-0.2672,0.05885,0.05065,-0.0002,1.0000,0.9649 -1.500,-0.2197,0.05954,0.05104,-0.0070,1.0000,0.9802 -1.250,-0.1787,0.06015,0.05143,-0.0127,1.0000,0.9910 -1.000,-0.1433,0.06093,0.05199,-0.0175,1.0000,0.9996 -0.750,-0.1378,0.06092,0.05188,-0.0163,1.0000,1.0000 -0.500,-0.1341,0.06087,0.05174,-0.0147,1.0000,1.0000 -0.250,-0.1305,0.06084,0.05162,-0.0131,1.0000,1.0000 0.000,-0.1267,0.06083,0.05153,-0.0115,1.0000,1.0000 0.250,-0.1230,0.06083,0.05144,-0.0098,1.0000,1.0000 0.500,-0.1194,0.06084,0.05139,-0.0082,1.0000,1.0000 0.750,-0.1159,0.06086,0.05134,-0.0065,1.0000,1.0000 1.000,-0.1125,0.06088,0.05129,-0.0048,1.0000,1.0000 1.250,-0.1092,0.06091,0.05127,-0.0032,1.0000,1.0000 1.500,-0.1060,0.06093,0.05122,-0.0014,1.0000,1.0000 1.750,-0.0943,0.06125,0.05149,-0.0015,0.9972,1.0000 2.000,-0.0688,0.06229,0.05246,-0.0042,0.9878,1.0000 2.250,-0.0475,0.06326,0.05337,-0.0061,0.9780,1.0000 2.500,-0.0274,0.06439,0.05443,-0.0077,0.9684,1.0000 2.750,-0.0056,0.06569,0.05567,-0.0095,0.9573,1.0000 3.000,0.0069,0.06590,0.05585,-0.0094,0.9453,1.0000 3.250,0.0175,0.06631,0.05623,-0.0090,0.9342,1.0000 3.500,0.0319,0.06744,0.05731,-0.0093,0.9255,1.0000 3.750,0.0472,0.06827,0.05812,-0.0096,0.9130,1.0000 4.000,0.0509,0.06816,0.05799,-0.0079,0.9012,1.0000 4.250,0.0611,0.06909,0.05889,-0.0074,0.8925,1.0000 4.500,0.0751,0.06994,0.05972,-0.0074,0.8804,1.0000 4.750,0.0757,0.06970,0.05948,-0.0052,0.8689,1.0000 5.000,0.0932,0.07141,0.06115,-0.0060,0.8611,1.0000 5.250,0.1065,0.07195,0.06169,-0.0060,0.8482,1.0000 5.500,0.1164,0.07263,0.06237,-0.0059,0.8378,1.0000 5.750,0.1537,0.07599,0.06571,-0.0101,0.8294,1.0000 6.000,0.1607,0.07601,0.06575,-0.0096,0.8167,1.0000 6.250,0.1784,0.07766,0.06742,-0.0110,0.8074,1.0000 6.500,0.2147,0.08076,0.07053,-0.0151,0.7969,1.0000 6.750,0.2236,0.08142,0.07123,-0.0152,0.7846,1.0000 7.000,0.2446,0.08361,0.07345,-0.0172,0.7755,1.0000 7.250,0.2802,0.08677,0.07665,-0.0211,0.7641,1.0000 7.500,0.2883,0.08767,0.07760,-0.0213,0.7516,1.0000 7.750,0.3068,0.08989,0.07987,-0.0231,0.7415,1.0000 8.000,0.3489,0.09395,0.08398,-0.0278,0.7307,1.0000 8.250,0.3536,0.09468,0.08478,-0.0277,0.7175,1.0000 8.500,0.3663,0.09670,0.08687,-0.0289,0.7067,1.0000 8.750,0.3980,0.10024,0.09046,-0.0322,0.6967,1.0000 9.000,0.4199,0.10256,0.09288,-0.0342,0.6830,1.0000 9.250,0.4255,0.10416,0.09454,-0.0346,0.6707,1.0000 9.500,0.4417,0.10684,0.09730,-0.0363,0.6604,1.0000 9.750,0.4753,0.11060,0.10114,-0.0396,0.6488,1.0000 10.000,0.4903,0.11267,0.10331,-0.0408,0.6347,1.0000 10.250,0.4929,0.11459,0.10531,-0.0413,0.6234,1.0000 10.500,0.5100,0.11763,0.10842,-0.0431,0.6133,1.0000 10.750,0.5398,0.12123,0.11214,-0.0457,0.6006,1.0000 11.000,0.5602,0.12391,0.11492,-0.0473,0.5860,1.0000 11.250,0.5541,0.12568,0.11675,-0.0475,0.5757,1.0000 11.500,0.6324,0.12311,0.11429,-0.0472,0.5063,1.0000 11.750,0.6326,0.12739,0.11867,-0.0490,0.5061,1.0000 12.000,0.6577,0.12691,0.11827,-0.0485,0.4715,1.0000