Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e184-il-50000-n5 Airfoil,e184-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,31.7363 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e184-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.6554,0.08332,0.07727,0.0010,1.0000,0.0428 -8.250,-0.6564,0.07849,0.07241,-0.0011,1.0000,0.0426 -8.000,-0.6577,0.07353,0.06737,-0.0033,1.0000,0.0424 -7.750,-0.6576,0.06860,0.06228,-0.0052,1.0000,0.0424 -7.500,-0.6562,0.06364,0.05704,-0.0067,1.0000,0.0427 -7.000,-0.6394,0.05548,0.04860,-0.0079,1.0000,0.0453 -6.750,-0.6282,0.05129,0.04408,-0.0083,1.0000,0.0459 -6.500,-0.6154,0.04681,0.03911,-0.0083,1.0000,0.0455 -6.250,-0.5993,0.04278,0.03454,-0.0080,1.0000,0.0454 -6.000,-0.5802,0.03924,0.03050,-0.0076,1.0000,0.0456 -5.750,-0.5587,0.03613,0.02685,-0.0072,1.0000,0.0461 -5.500,-0.5351,0.03337,0.02367,-0.0069,1.0000,0.0470 -5.250,-0.5098,0.03093,0.02085,-0.0066,1.0000,0.0483 -5.000,-0.4833,0.02876,0.01836,-0.0063,1.0000,0.0501 -4.750,-0.4559,0.02685,0.01616,-0.0061,1.0000,0.0527 -4.500,-0.4295,0.02528,0.01444,-0.0060,1.0000,0.0583 -4.250,-0.4037,0.02404,0.01306,-0.0058,1.0000,0.0674 -4.000,-0.3790,0.02268,0.01167,-0.0055,1.0000,0.0772 -3.750,-0.3558,0.02132,0.01032,-0.0051,1.0000,0.0973 -3.500,-0.3375,0.01992,0.00933,-0.0045,1.0000,0.1664 -3.250,-0.3117,0.01799,0.00865,-0.0055,0.9786,0.3748 -3.000,-0.2829,0.01647,0.00845,-0.0047,0.9649,0.6555 -2.750,-0.1945,0.01624,0.00829,-0.0124,0.9731,0.9066 -2.500,-0.1208,0.01630,0.00775,-0.0207,0.9719,0.9829 -2.250,-0.0676,0.01614,0.00716,-0.0266,0.9565,1.0000 -2.000,-0.0321,0.01615,0.00682,-0.0289,0.9359,1.0000 -1.750,-0.0008,0.01621,0.00660,-0.0302,0.9182,1.0000 -1.500,0.0266,0.01633,0.00648,-0.0306,0.9024,1.0000 -1.250,0.0512,0.01648,0.00643,-0.0304,0.8877,1.0000 -1.000,0.0746,0.01665,0.00641,-0.0298,0.8743,1.0000 -0.750,0.0976,0.01684,0.00644,-0.0292,0.8617,1.0000 -0.500,0.1205,0.01704,0.00652,-0.0285,0.8498,1.0000 -0.250,0.1435,0.01725,0.00663,-0.0278,0.8385,1.0000 0.000,0.1664,0.01748,0.00676,-0.0271,0.8280,1.0000 0.250,0.1891,0.01772,0.00692,-0.0262,0.8183,1.0000 0.500,0.2123,0.01797,0.00712,-0.0255,0.8081,1.0000 0.750,0.2357,0.01825,0.00737,-0.0250,0.7981,1.0000 1.000,0.2587,0.01852,0.00764,-0.0241,0.7888,1.0000 1.250,0.2817,0.01881,0.00792,-0.0233,0.7796,1.0000 1.500,0.3053,0.01912,0.00826,-0.0227,0.7695,1.0000 1.750,0.3285,0.01944,0.00860,-0.0219,0.7600,1.0000 2.000,0.3512,0.01972,0.00897,-0.0208,0.7510,1.0000 2.250,0.3745,0.02007,0.00939,-0.0202,0.7399,1.0000 2.500,0.3973,0.02039,0.00980,-0.0192,0.7288,1.0000 2.750,0.4199,0.02069,0.01019,-0.0181,0.7174,1.0000 3.000,0.4422,0.02096,0.01056,-0.0168,0.7056,1.0000 3.250,0.4643,0.02120,0.01097,-0.0154,0.6929,1.0000 3.500,0.4862,0.02141,0.01132,-0.0138,0.6787,1.0000 3.750,0.5081,0.02160,0.01166,-0.0123,0.6629,1.0000 4.000,0.5298,0.02171,0.01193,-0.0105,0.6459,1.0000 4.250,0.5512,0.02170,0.01207,-0.0084,0.6279,1.0000 4.500,0.5728,0.02169,0.01226,-0.0065,0.6059,1.0000 4.750,0.5941,0.02154,0.01236,-0.0042,0.5818,1.0000 5.000,0.6156,0.02139,0.01242,-0.0021,0.5513,1.0000 5.250,0.6368,0.02119,0.01240,0.0002,0.5134,1.0000 5.500,0.6576,0.02110,0.01243,0.0024,0.4585,1.0000 5.750,0.6763,0.02131,0.01245,0.0048,0.3702,1.0000 6.000,0.6902,0.02270,0.01308,0.0067,0.2563,1.0000 6.250,0.7017,0.02502,0.01474,0.0076,0.1629,1.0000 6.500,0.7122,0.02750,0.01673,0.0085,0.0961,1.0000 6.750,0.7242,0.02974,0.01868,0.0097,0.0661,1.0000 7.000,0.7390,0.03158,0.02058,0.0111,0.0507,1.0000 7.250,0.7542,0.03343,0.02245,0.0126,0.0439,1.0000 7.500,0.7740,0.03542,0.02469,0.0144,0.0402,1.0000 7.750,0.7956,0.03758,0.02715,0.0160,0.0375,1.0000 8.000,0.8160,0.04008,0.02993,0.0173,0.0356,1.0000 8.250,0.8327,0.04266,0.03276,0.0183,0.0334,1.0000 8.500,0.8454,0.04582,0.03607,0.0191,0.0313,1.0000 8.750,0.8556,0.04908,0.03977,0.0201,0.0302,1.0000 9.000,0.8611,0.05249,0.04367,0.0210,0.0291,1.0000 9.250,0.8620,0.05619,0.04786,0.0217,0.0287,1.0000 9.500,0.8571,0.06008,0.05209,0.0222,0.0285,1.0000 9.750,0.8465,0.06395,0.05621,0.0225,0.0285,1.0000 10.000,0.8321,0.06792,0.06035,0.0221,0.0286,1.0000 10.250,0.8161,0.07256,0.06514,0.0203,0.0287,1.0000 10.500,0.8008,0.07770,0.07040,0.0176,0.0291,1.0000 10.750,0.7847,0.08369,0.07638,0.0139,0.0293,1.0000 11.000,0.7709,0.09002,0.08276,0.0099,0.0297,1.0000