Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e584-il-50000 Airfoil,e584-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,4.47547 Max Cl/Cd alpha,11 Url,http://airfoiltools.com/polar/csv?polar=xf-e584-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4685,0.13409,0.12922,-0.0169,1.0000,0.2277 -8.000,-0.4321,0.12894,0.12402,-0.0161,0.9976,0.2387 -7.750,-0.4754,0.12878,0.12400,-0.0152,0.9979,0.2448 -7.500,-0.4432,0.12415,0.11933,-0.0156,0.9943,0.2585 -7.000,-0.4679,0.12021,0.11552,-0.0117,0.9944,0.2769 -6.750,-0.5176,0.12003,0.11548,-0.0057,1.0000,0.2790 -6.500,-0.5744,0.11921,0.11479,-0.0033,1.0000,0.2802 -6.250,-0.5153,0.11435,0.10989,-0.0010,1.0000,0.3029 -6.000,-0.5496,0.11314,0.10877,0.0022,1.0000,0.3132 -5.750,-0.5485,0.11053,0.10620,0.0051,1.0000,0.3292 -5.500,-0.5562,0.10819,0.10391,0.0084,1.0000,0.3458 -3.750,-0.4404,0.09477,0.09060,0.0337,1.0000,0.6492 -3.500,-0.5996,0.07072,0.06491,-0.0102,1.0000,0.2268 -3.250,-0.5535,0.06122,0.05387,-0.0146,1.0000,0.1230 -3.000,-0.5295,0.05781,0.04956,-0.0143,1.0000,0.1109 -2.750,-0.5106,0.05537,0.04680,-0.0138,1.0000,0.1097 -2.500,-0.4903,0.05323,0.04427,-0.0133,1.0000,0.1088 -2.250,-0.4694,0.05139,0.04205,-0.0127,1.0000,0.1079 -2.000,-0.4477,0.04975,0.04003,-0.0120,1.0000,0.1074 -1.750,-0.4258,0.04847,0.03837,-0.0112,1.0000,0.1084 -1.500,-0.4038,0.04749,0.03698,-0.0103,1.0000,0.1134 -1.250,-0.3838,0.04663,0.03614,-0.0096,1.0000,0.1208 -1.000,-0.3624,0.04606,0.03537,-0.0085,1.0000,0.1298 -0.750,-0.3417,0.04573,0.03506,-0.0072,1.0000,0.1461 -0.500,-0.2122,0.04777,0.04056,-0.0152,1.0000,1.0000 -0.250,-0.2036,0.04807,0.04048,-0.0132,1.0000,1.0000 0.000,-0.1953,0.04837,0.04045,-0.0114,1.0000,1.0000 0.250,-0.1871,0.04870,0.04051,-0.0096,1.0000,1.0000 0.500,-0.1788,0.04903,0.04060,-0.0078,1.0000,1.0000 0.750,-0.1705,0.04939,0.04074,-0.0061,1.0000,1.0000 1.000,-0.1619,0.04978,0.04092,-0.0044,0.9999,1.0000 1.250,-0.1340,0.05161,0.04246,-0.0067,0.9931,1.0000 1.500,-0.1075,0.05318,0.04379,-0.0086,0.9841,1.0000 1.750,-0.0849,0.05441,0.04481,-0.0098,0.9745,1.0000 2.000,-0.0637,0.05569,0.04589,-0.0107,0.9648,1.0000 2.250,-0.0402,0.05744,0.04746,-0.0120,0.9561,1.0000 2.500,-0.0161,0.05900,0.04885,-0.0133,0.9446,1.0000 2.750,-0.0001,0.05972,0.04944,-0.0132,0.9329,1.0000 3.000,0.0172,0.06092,0.05051,-0.0133,0.9228,1.0000 3.250,0.0464,0.06338,0.05281,-0.0154,0.9133,1.0000 3.500,0.0579,0.06373,0.05308,-0.0145,0.9007,1.0000 3.750,0.0751,0.06512,0.05437,-0.0146,0.8915,1.0000 4.000,0.1028,0.06734,0.05647,-0.0165,0.8809,1.0000 4.250,0.1127,0.06786,0.05693,-0.0154,0.8691,1.0000 4.500,0.1429,0.07084,0.05979,-0.0178,0.8619,1.0000 4.750,0.1546,0.07130,0.06022,-0.0171,0.8488,1.0000 5.000,0.1673,0.07251,0.06138,-0.0167,0.8389,1.0000 5.250,0.1990,0.07538,0.06418,-0.0192,0.8295,1.0000 5.500,0.2047,0.07577,0.06456,-0.0178,0.8177,1.0000 5.750,0.2332,0.07880,0.06753,-0.0199,0.8103,1.0000 6.000,0.2463,0.07969,0.06842,-0.0196,0.7973,1.0000 6.250,0.2567,0.08096,0.06968,-0.0191,0.7865,1.0000 6.500,0.2924,0.08453,0.07323,-0.0222,0.7780,1.0000 6.750,0.2953,0.08483,0.07354,-0.0207,0.7651,1.0000 7.000,0.3091,0.08670,0.07542,-0.0209,0.7558,1.0000 7.250,0.3399,0.08970,0.07842,-0.0232,0.7452,1.0000 7.500,0.3430,0.09045,0.07921,-0.0220,0.7331,1.0000 7.750,0.3615,0.09291,0.08169,-0.0229,0.7246,1.0000 8.000,0.3859,0.09540,0.08420,-0.0244,0.7131,1.0000 8.250,0.3901,0.09655,0.08539,-0.0236,0.7016,1.0000 8.500,0.4055,0.09888,0.08776,-0.0242,0.6925,1.0000 8.750,0.4355,0.10211,0.09106,-0.0263,0.6822,1.0000 9.000,0.4374,0.10318,0.09217,-0.0255,0.6705,1.0000 9.250,0.4465,0.10529,0.09434,-0.0257,0.6614,1.0000 9.500,0.4791,0.10914,0.09825,-0.0281,0.6526,1.0000 9.750,0.4780,0.11014,0.09932,-0.0273,0.6415,1.0000 10.000,0.4857,0.11244,0.10170,-0.0276,0.6334,1.0000 10.250,0.5188,0.11646,0.10580,-0.0299,0.6242,1.0000 10.500,0.5135,0.11735,0.10676,-0.0290,0.6137,1.0000 10.750,0.5229,0.11997,0.10945,-0.0296,0.6062,1.0000 11.000,0.5546,0.12392,0.11352,-0.0318,0.5959,1.0000 11.250,0.5475,0.12487,0.11454,-0.0311,0.5857,1.0000 11.500,0.5597,0.12786,0.11762,-0.0320,0.5788,1.0000 11.750,0.5847,0.13123,0.12109,-0.0335,0.5673,1.0000 12.000,0.5784,0.13264,0.12257,-0.0333,0.5581,1.0000 12.250,0.6031,0.13670,0.12676,-0.0351,0.5504,1.0000