Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e340-il-500000-n5 Airfoil,e340-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,74.3355 Max Cl/Cd alpha,10.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e340-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.5889,0.08829,0.08614,0.0032,0.8742,0.0064 -10.000,-0.6073,0.08034,0.07793,-0.0036,0.8082,0.0063 -9.500,-0.6447,0.06917,0.06637,-0.0073,0.7524,0.0062 -9.250,-0.6635,0.06443,0.06143,-0.0059,0.7325,0.0062 -9.000,-0.6790,0.06002,0.05682,-0.0034,0.7151,0.0061 -8.750,-0.6904,0.05529,0.05184,-0.0007,0.7001,0.0061 -8.500,-0.6978,0.05024,0.04651,0.0023,0.6864,0.0061 -8.250,-0.7032,0.04467,0.04058,0.0058,0.6740,0.0061 -8.000,-0.7138,0.03663,0.03196,0.0110,0.6650,0.0061 -7.750,-0.7138,0.03078,0.02542,0.0153,0.6540,0.0063 -7.500,-0.7008,0.02794,0.02210,0.0178,0.6399,0.0063 -7.250,-0.6840,0.02571,0.01948,0.0196,0.6258,0.0063 -7.000,-0.6644,0.02382,0.01725,0.0211,0.6122,0.0063 -6.750,-0.6424,0.02231,0.01544,0.0222,0.5989,0.0063 -6.500,-0.6189,0.02098,0.01384,0.0230,0.5865,0.0063 -6.250,-0.5943,0.01984,0.01247,0.0237,0.5747,0.0063 -6.000,-0.5690,0.01885,0.01129,0.0242,0.5637,0.0063 -5.750,-0.5435,0.01800,0.01027,0.0247,0.5529,0.0064 -5.500,-0.5179,0.01724,0.00936,0.0252,0.5415,0.0064 -5.250,-0.4928,0.01648,0.00850,0.0258,0.5308,0.0065 -5.000,-0.4682,0.01576,0.00768,0.0264,0.5211,0.0066 -4.750,-0.4436,0.01518,0.00703,0.0271,0.5118,0.0067 -4.500,-0.4189,0.01470,0.00647,0.0277,0.5033,0.0069 -4.250,-0.3941,0.01427,0.00599,0.0283,0.4946,0.0071 -4.000,-0.3691,0.01391,0.00556,0.0289,0.4865,0.0074 -3.750,-0.3440,0.01357,0.00515,0.0295,0.4776,0.0078 -3.500,-0.3188,0.01327,0.00478,0.0301,0.4698,0.0083 -3.250,-0.2935,0.01298,0.00443,0.0307,0.4619,0.0089 -3.000,-0.2681,0.01272,0.00412,0.0312,0.4551,0.0101 -2.750,-0.2424,0.01249,0.00385,0.0317,0.4485,0.0117 -2.500,-0.2170,0.01228,0.00361,0.0322,0.4417,0.0147 -2.250,-0.1919,0.01205,0.00339,0.0327,0.4355,0.0237 -2.000,-0.1674,0.01176,0.00321,0.0334,0.4288,0.0498 -1.750,-0.1436,0.01147,0.00305,0.0341,0.4227,0.0916 -1.500,-0.1205,0.01109,0.00290,0.0349,0.4177,0.1571 -1.250,-0.1182,0.00948,0.00253,0.0393,0.4135,0.4807 -1.000,-0.1131,0.00854,0.00316,0.0450,0.4093,0.8540 -0.750,-0.0927,0.00888,0.00343,0.0471,0.4048,0.8776 -0.500,-0.0655,0.00923,0.00372,0.0477,0.3996,0.8884 -0.250,-0.0437,0.00951,0.00392,0.0493,0.3944,0.8991 0.000,0.0021,0.01026,0.00458,0.0464,0.3889,0.9038 0.250,0.0352,0.01063,0.00489,0.0458,0.3843,0.9096 0.500,0.0557,0.01066,0.00485,0.0474,0.3799,0.9144 0.750,0.0859,0.01073,0.00483,0.0469,0.3752,0.9151 1.000,0.1158,0.01077,0.00482,0.0464,0.3712,0.9158 1.250,0.1453,0.01081,0.00481,0.0460,0.3672,0.9165 1.500,0.1745,0.01086,0.00480,0.0457,0.3633,0.9173 1.750,0.2029,0.01091,0.00480,0.0455,0.3597,0.9183 2.000,0.2310,0.01096,0.00480,0.0454,0.3564,0.9193 2.250,0.2580,0.01098,0.00480,0.0455,0.3527,0.9206 2.500,0.2837,0.01100,0.00478,0.0459,0.3488,0.9220 2.750,0.3068,0.01101,0.00476,0.0467,0.3453,0.9240 3.000,0.3173,0.01092,0.00463,0.0501,0.3423,0.9281 3.250,0.3459,0.01095,0.00465,0.0498,0.3392,0.9285 3.500,0.3740,0.01098,0.00468,0.0497,0.3362,0.9290 3.750,0.4018,0.01102,0.00472,0.0495,0.3330,0.9295 4.000,0.4298,0.01110,0.00477,0.0493,0.3298,0.9301 4.250,0.4574,0.01120,0.00483,0.0492,0.3264,0.9308 4.500,0.4848,0.01124,0.00489,0.0491,0.3234,0.9314 4.750,0.5116,0.01128,0.00496,0.0492,0.3200,0.9321 5.000,0.5379,0.01134,0.00501,0.0493,0.3164,0.9328 5.250,0.5635,0.01142,0.00508,0.0495,0.3134,0.9337 5.500,0.5886,0.01151,0.00517,0.0499,0.3104,0.9346 5.750,0.6142,0.01156,0.00526,0.0501,0.3074,0.9358 6.000,0.6384,0.01161,0.00533,0.0507,0.3039,0.9370 6.250,0.6614,0.01166,0.00539,0.0514,0.3005,0.9383 6.500,0.6831,0.01172,0.00546,0.0524,0.2969,0.9397 6.750,0.7050,0.01177,0.00552,0.0533,0.2935,0.9411 7.000,0.7298,0.01182,0.00562,0.0536,0.2897,0.9419 7.250,0.7562,0.01193,0.00576,0.0536,0.2855,0.9424 7.500,0.7821,0.01207,0.00590,0.0537,0.2812,0.9430 7.750,0.8086,0.01219,0.00607,0.0536,0.2769,0.9436 8.000,0.8347,0.01231,0.00624,0.0536,0.2716,0.9444 8.250,0.8596,0.01247,0.00641,0.0538,0.2668,0.9451 8.500,0.8847,0.01260,0.00660,0.0540,0.2623,0.9459 8.750,0.9094,0.01274,0.00678,0.0542,0.2562,0.9467 9.000,0.9329,0.01294,0.00698,0.0546,0.2498,0.9477 9.250,0.9570,0.01309,0.00719,0.0549,0.2430,0.9487 9.500,0.9794,0.01332,0.00743,0.0554,0.2362,0.9499 9.750,1.0024,0.01352,0.00767,0.0558,0.2282,0.9511 10.000,1.0240,0.01379,0.00794,0.0564,0.2196,0.9524 10.250,1.0459,0.01407,0.00825,0.0569,0.2101,0.9536 10.500,1.0680,0.01441,0.00861,0.0573,0.2007,0.9544 10.750,1.0884,0.01483,0.00904,0.0579,0.1896,0.9555 11.000,1.1075,0.01531,0.00952,0.0586,0.1784,0.9569 11.250,1.1256,0.01583,0.01004,0.0595,0.1668,0.9584 11.500,1.1419,0.01641,0.01062,0.0604,0.1542,0.9601 11.750,1.1558,0.01711,0.01130,0.0616,0.1410,0.9622 12.000,1.1659,0.01786,0.01204,0.0633,0.1288,0.9644 12.250,1.1755,0.01876,0.01296,0.0648,0.1180,0.9665 12.500,1.1834,0.01987,0.01409,0.0660,0.1078,0.9691 12.750,1.1891,0.02128,0.01552,0.0667,0.0989,0.9722 13.000,1.1952,0.02302,0.01730,0.0666,0.0906,0.9747 13.250,1.2019,0.02504,0.01938,0.0658,0.0833,0.9773 13.500,1.2050,0.02762,0.02201,0.0645,0.0767,0.9807 13.750,1.2083,0.03022,0.02468,0.0632,0.0709,0.9854 14.000,1.2069,0.03335,0.02787,0.0618,0.0662,0.9901 14.250,1.2072,0.03644,0.03104,0.0603,0.0620,0.9941 14.750,1.2033,0.04372,0.03847,0.0558,0.0548,0.9971 15.000,1.1983,0.04761,0.04245,0.0536,0.0515,0.9983 15.500,1.1768,0.05516,0.05013,0.0518,0.0468,1.0000 15.750,1.1673,0.05905,0.05408,0.0507,0.0444,1.0000 16.000,1.1568,0.06326,0.05835,0.0494,0.0420,1.0000 16.250,1.1494,0.06716,0.06232,0.0481,0.0398,1.0000 16.500,1.1422,0.07115,0.06636,0.0467,0.0373,1.0000 16.750,1.1326,0.07552,0.07078,0.0451,0.0351,1.0000 17.000,1.1264,0.07950,0.07483,0.0436,0.0333,1.0000 17.250,1.1199,0.08357,0.07896,0.0421,0.0310,1.0000 17.750,1.1061,0.09197,0.08747,0.0388,0.0273,1.0000 18.000,1.0994,0.09622,0.09176,0.0371,0.0253,1.0000