Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e379-il-100000 Airfoil,e379-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,74.5961 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e379-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.250,-0.0788,0.09222,0.08840,-0.0421,0.9097,0.0123 -7.000,-0.0648,0.09043,0.08654,-0.0439,0.8871,0.0127 -6.750,-0.0521,0.08893,0.08498,-0.0454,0.8670,0.0130 -6.500,-0.0374,0.08770,0.08370,-0.0473,0.8505,0.0133 -6.250,-0.0202,0.08683,0.08276,-0.0500,0.8358,0.0135 -6.000,0.0013,0.08631,0.08218,-0.0539,0.8223,0.0138 -5.750,0.0239,0.08547,0.08126,-0.0578,0.8098,0.0139 -5.500,0.0504,0.08492,0.08063,-0.0626,0.7981,0.0140 -5.250,0.0681,0.08145,0.07716,-0.0646,0.7884,0.0144 -5.000,0.0609,0.07366,0.06940,-0.0593,0.7821,0.0157 -4.750,0.0773,0.07072,0.06636,-0.0609,0.7724,0.0173 -4.500,0.0984,0.06844,0.06404,-0.0635,0.7639,0.0190 -4.250,0.1219,0.06622,0.06174,-0.0663,0.7563,0.0209 -4.000,0.1485,0.06413,0.05961,-0.0698,0.7477,0.0223 -3.750,0.1792,0.06245,0.05782,-0.0736,0.7408,0.0241 -3.500,0.2238,0.06250,0.05774,-0.0802,0.7321,0.0253 -3.250,0.2674,0.06255,0.05761,-0.0861,0.7245,0.0256 -2.750,0.3049,0.05473,0.04978,-0.0884,0.7119,0.0268 -2.500,0.3255,0.05163,0.04664,-0.0897,0.7054,0.0285 -2.250,0.3540,0.04956,0.04448,-0.0922,0.6995,0.0305 -2.000,0.3858,0.04783,0.04266,-0.0951,0.6927,0.0330 -1.750,0.4209,0.04656,0.04123,-0.0980,0.6872,0.0359 -1.500,0.4720,0.04805,0.04246,-0.1028,0.6798,0.0377 -1.250,0.4945,0.04438,0.03873,-0.1039,0.6756,0.0388 -1.000,0.5169,0.04167,0.03606,-0.1055,0.6688,0.0419 -0.750,0.5489,0.04031,0.03448,-0.1073,0.6637,0.0465 -0.250,0.6135,0.03787,0.03180,-0.1110,0.6520,0.0540 0.000,0.6176,0.01911,0.01334,-0.1054,0.6367,0.0635 0.250,0.6426,0.01783,0.01205,-0.1071,0.6309,0.0710 0.500,0.6734,0.01708,0.01114,-0.1084,0.6259,0.0786 0.750,0.7042,0.01611,0.00985,-0.1090,0.6223,0.0901 1.000,0.7333,0.01622,0.00991,-0.1107,0.6152,0.1020 1.250,0.7615,0.01526,0.00881,-0.1113,0.6112,0.1165 1.500,0.7904,0.01529,0.00866,-0.1120,0.6062,0.1392 1.750,0.8164,0.01492,0.00823,-0.1129,0.6003,0.1654 2.000,0.8428,0.01365,0.00682,-0.1130,0.5967,0.2096 2.250,0.8655,0.01345,0.00666,-0.1139,0.5903,0.2870 2.500,0.8927,0.01282,0.00602,-0.1140,0.5856,0.3314 2.750,0.9235,0.01238,0.00531,-0.1134,0.5825,0.3257 3.000,0.9511,0.01434,0.00713,-0.1137,0.5749,0.2134 3.250,0.9844,0.01435,0.00670,-0.1121,0.5712,0.0699 3.500,1.0099,0.01436,0.00650,-0.1115,0.5664,0.0532 3.750,1.0856,0.02924,0.02052,-0.1169,0.5706,0.0470 4.000,1.1111,0.02955,0.02072,-0.1170,0.5646,0.0531 4.250,1.1360,0.02961,0.02065,-0.1165,0.5593,0.0653 4.500,1.1643,0.02917,0.01998,-0.1156,0.5561,0.1082 4.750,1.1888,0.02961,0.02125,-0.1168,0.5480,1.0000 5.000,1.2150,0.02975,0.02116,-0.1160,0.5440,1.0000 5.250,1.2347,0.03103,0.02246,-0.1158,0.5368,1.0000 5.500,1.2596,0.03128,0.02262,-0.1151,0.5316,1.0000 5.750,1.2819,0.03198,0.02332,-0.1145,0.5256,1.0000 6.000,1.3040,0.03262,0.02399,-0.1140,0.5190,1.0000 6.250,1.3337,0.03206,0.02338,-0.1130,0.5158,1.0000 6.500,1.3592,0.03099,0.02225,-0.1115,0.5037,1.0000 6.750,1.3923,0.02648,0.01730,-0.1081,0.4783,1.0000 7.000,1.4179,0.02437,0.01497,-0.1061,0.4550,1.0000 7.250,1.4406,0.02285,0.01327,-0.1043,0.4263,1.0000 7.500,1.4633,0.02300,0.01354,-0.1036,0.4156,1.0000 7.750,1.4863,0.02317,0.01383,-0.1029,0.4060,1.0000 8.000,1.5089,0.02340,0.01423,-0.1022,0.3962,1.0000 8.250,1.5251,0.02337,0.01410,-0.1007,0.3531,1.0000 8.500,1.5428,0.02393,0.01464,-0.0996,0.3225,1.0000 8.750,1.5586,0.02477,0.01546,-0.0983,0.2911,1.0000 9.000,1.5622,0.02689,0.01822,-0.0956,0.2235,1.0000 9.250,1.5454,0.03053,0.02131,-0.0921,0.1484,1.0000 9.500,1.5305,0.03364,0.02426,-0.0888,0.1093,1.0000 9.750,1.5133,0.03731,0.02776,-0.0867,0.0771,1.0000 10.000,1.4915,0.04207,0.03229,-0.0856,0.0376,1.0000 10.250,1.4746,0.04678,0.03692,-0.0851,0.0221,1.0000 10.500,1.4664,0.05081,0.04109,-0.0847,0.0191,1.0000 10.750,1.4577,0.05500,0.04546,-0.0845,0.0168,1.0000 11.000,1.4507,0.05905,0.04971,-0.0844,0.0151,1.0000 11.250,1.4429,0.06331,0.05422,-0.0844,0.0141,1.0000 11.500,1.4359,0.06754,0.05865,-0.0845,0.0136,1.0000 11.750,1.4297,0.07176,0.06309,-0.0848,0.0135,1.0000 12.000,1.4224,0.07622,0.06778,-0.0852,0.0134,1.0000 12.250,1.4143,0.08104,0.07283,-0.0859,0.0135,1.0000 12.500,1.4060,0.08600,0.07801,-0.0867,0.0135,1.0000 12.750,1.3981,0.09104,0.08325,-0.0877,0.0135,1.0000