Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e184-il-50000 Airfoil,e184-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,30.8634 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-e184-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.6625,0.14376,0.13753,0.0399,1.0000,0.1802 -10.500,-0.6333,0.13638,0.13008,0.0419,1.0000,0.1899 -10.250,-0.6529,0.13563,0.12946,0.0374,1.0000,0.1942 -10.000,-0.6299,0.12946,0.12325,0.0388,1.0000,0.2063 -9.750,-0.6189,0.12486,0.11866,0.0387,1.0000,0.2164 -9.500,-0.6390,0.12373,0.11766,0.0346,1.0000,0.2222 -9.250,-0.6254,0.11896,0.11288,0.0351,1.0000,0.2357 -9.000,-0.6101,0.11404,0.10796,0.0355,1.0000,0.2476 -8.750,-0.6018,0.10981,0.10376,0.0351,1.0000,0.2576 -8.500,-0.6008,0.10620,0.10021,0.0340,1.0000,0.2686 -8.000,-0.6002,0.09939,0.09354,0.0323,1.0000,0.2946 -7.500,-0.5838,0.09168,0.08586,0.0325,1.0000,0.3247 -7.250,-0.5750,0.08793,0.08214,0.0327,1.0000,0.3413 -7.000,-0.5778,0.08504,0.07934,0.0326,1.0000,0.3616 -6.750,-0.5702,0.08121,0.07557,0.0332,1.0000,0.3803 -6.000,-0.5829,0.05184,0.04496,-0.0079,1.0000,0.1351 -5.750,-0.5656,0.04628,0.03878,-0.0087,1.0000,0.1213 -5.500,-0.5468,0.04143,0.03323,-0.0087,1.0000,0.1132 -5.250,-0.5246,0.03794,0.02898,-0.0081,1.0000,0.1102 -5.000,-0.5015,0.03473,0.02552,-0.0079,1.0000,0.1136 -4.750,-0.4766,0.03205,0.02254,-0.0076,1.0000,0.1173 -4.500,-0.4500,0.02940,0.01944,-0.0071,1.0000,0.1198 -4.250,-0.4224,0.02715,0.01666,-0.0065,1.0000,0.1246 -4.000,-0.3954,0.02497,0.01450,-0.0062,1.0000,0.1362 -3.750,-0.3714,0.02319,0.01283,-0.0055,1.0000,0.1623 -3.500,-0.3473,0.02094,0.01097,-0.0046,1.0000,0.2331 -3.250,-0.1651,0.01699,0.00929,-0.0211,1.0000,1.0000 -3.000,-0.1450,0.01650,0.00843,-0.0222,1.0000,1.0000 -2.750,-0.1238,0.01621,0.00786,-0.0230,1.0000,1.0000 -2.500,-0.1048,0.01609,0.00748,-0.0233,1.0000,1.0000 -2.250,-0.0930,0.01612,0.00732,-0.0223,1.0000,1.0000 -2.000,-0.0932,0.01634,0.00736,-0.0191,1.0000,1.0000 -1.750,-0.0941,0.01660,0.00740,-0.0157,1.0000,1.0000 -1.500,-0.0921,0.01686,0.00747,-0.0126,1.0000,1.0000 -1.250,-0.0873,0.01713,0.00756,-0.0099,1.0000,1.0000 -1.000,-0.0801,0.01742,0.00766,-0.0076,1.0000,1.0000 -0.750,-0.0713,0.01772,0.00779,-0.0055,1.0000,1.0000 -0.500,-0.0612,0.01804,0.00796,-0.0037,1.0000,1.0000 -0.250,-0.0498,0.01839,0.00815,-0.0021,1.0000,1.0000 0.000,-0.0353,0.01877,0.00841,-0.0011,0.9992,1.0000 0.250,0.0087,0.01942,0.00891,-0.0057,0.9883,1.0000 0.500,0.0518,0.02011,0.00951,-0.0101,0.9775,1.0000 0.750,0.0950,0.02083,0.01018,-0.0144,0.9668,1.0000 1.000,0.1398,0.02159,0.01092,-0.0190,0.9559,1.0000 1.250,0.1783,0.02231,0.01164,-0.0222,0.9445,1.0000 1.500,0.2146,0.02306,0.01241,-0.0250,0.9326,1.0000 1.750,0.2515,0.02384,0.01326,-0.0279,0.9203,1.0000 2.000,0.2892,0.02463,0.01415,-0.0307,0.9074,1.0000 2.250,0.3272,0.02544,0.01506,-0.0334,0.8936,1.0000 2.500,0.3660,0.02623,0.01604,-0.0362,0.8788,1.0000 2.750,0.4038,0.02700,0.01698,-0.0383,0.8630,1.0000 3.000,0.4432,0.02774,0.01792,-0.0403,0.8461,1.0000 3.250,0.4648,0.02855,0.01888,-0.0394,0.8271,1.0000 3.500,0.4990,0.02914,0.01974,-0.0397,0.8068,1.0000 3.750,0.5231,0.02978,0.02058,-0.0384,0.7849,1.0000 4.000,0.5549,0.02998,0.02103,-0.0367,0.7619,1.0000 4.250,0.5770,0.03020,0.02148,-0.0338,0.7362,1.0000 4.500,0.5985,0.03012,0.02167,-0.0299,0.7089,1.0000 4.750,0.6194,0.02962,0.02141,-0.0251,0.6801,1.0000 5.000,0.6395,0.02858,0.02058,-0.0192,0.6501,1.0000 5.500,0.6745,0.02557,0.01796,-0.0064,0.5687,1.0000 5.750,0.6908,0.02327,0.01576,0.0010,0.4992,1.0000 6.000,0.7006,0.02270,0.01417,0.0077,0.3448,1.0000 6.250,0.7074,0.02598,0.01611,0.0106,0.2130,1.0000 6.500,0.7207,0.02906,0.01857,0.0126,0.1426,1.0000 6.750,0.7424,0.03171,0.02103,0.0144,0.1139,1.0000 7.000,0.7662,0.03441,0.02378,0.0158,0.0995,1.0000 7.250,0.7884,0.03737,0.02703,0.0170,0.0907,1.0000 7.500,0.8100,0.04067,0.03077,0.0181,0.0871,1.0000 7.750,0.8289,0.04436,0.03487,0.0191,0.0857,1.0000 8.000,0.8425,0.04857,0.03967,0.0200,0.0862,1.0000 8.250,0.8499,0.05326,0.04497,0.0207,0.0881,1.0000 8.500,0.8522,0.05811,0.05029,0.0210,0.0901,1.0000 8.750,0.8504,0.06298,0.05552,0.0210,0.0919,1.0000 9.000,0.8469,0.06787,0.06062,0.0209,0.0935,1.0000 9.250,0.8484,0.07290,0.06575,0.0208,0.0952,1.0000 9.500,0.7948,0.07902,0.07221,0.0166,0.1014,1.0000 9.750,0.7706,0.08563,0.07882,0.0123,0.1048,1.0000 10.000,0.7833,0.09065,0.08382,0.0131,0.1087,1.0000 10.250,0.7309,0.10302,0.09601,-0.0005,0.1193,1.0000 10.500,0.7090,0.11340,0.10627,-0.0088,0.1433,1.0000