Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e426-il-50000-n5 Airfoil,e426-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.7134 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-e426-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.500,-0.6398,0.11347,0.10562,0.0040,1.0000,0.0907 -11.250,-0.6497,0.10707,0.09928,0.0005,1.0000,0.0936 -11.000,-0.6760,0.09727,0.08957,-0.0058,1.0000,0.0959 -10.750,-0.6618,0.09635,0.08864,-0.0048,1.0000,0.1000 -10.500,-0.6690,0.09085,0.08318,-0.0076,1.0000,0.1036 -10.250,-0.7075,0.07862,0.07104,-0.0165,1.0000,0.1059 -10.000,-0.7647,0.06584,0.05828,-0.0263,1.0000,0.1053 -9.750,-0.8058,0.05785,0.05008,-0.0296,1.0000,0.1062 -9.500,-0.8244,0.05217,0.04403,-0.0307,1.0000,0.1098 -9.250,-0.8035,0.05199,0.04388,-0.0296,1.0000,0.1158 -9.000,-0.8149,0.04659,0.03780,-0.0302,1.0000,0.1218 -8.750,-0.7896,0.04680,0.03819,-0.0291,1.0000,0.1277 -8.500,-0.7849,0.04345,0.03428,-0.0289,1.0000,0.1350 -8.250,-0.7635,0.04276,0.03365,-0.0281,1.0000,0.1410 -8.000,-0.7492,0.04076,0.03126,-0.0276,1.0000,0.1486 -7.750,-0.7305,0.03929,0.02967,-0.0270,1.0000,0.1547 -7.500,-0.7108,0.03791,0.02811,-0.0264,1.0000,0.1610 -7.250,-0.6940,0.03569,0.02535,-0.0260,1.0000,0.1670 -7.000,-0.6713,0.03441,0.02407,-0.0254,1.0000,0.1709 -6.750,-0.6494,0.03307,0.02257,-0.0248,1.0000,0.1760 -6.500,-0.6281,0.03153,0.02063,-0.0243,1.0000,0.1819 -6.250,-0.6049,0.03029,0.01934,-0.0237,1.0000,0.1862 -6.000,-0.5814,0.02916,0.01811,-0.0231,1.0000,0.1908 -5.750,-0.5581,0.02802,0.01674,-0.0225,1.0000,0.1969 -5.500,-0.5345,0.02704,0.01571,-0.0218,1.0000,0.2029 -5.250,-0.5109,0.02616,0.01478,-0.0211,1.0000,0.2098 -5.000,-0.4868,0.02525,0.01370,-0.0205,1.0000,0.2169 -4.750,-0.4632,0.02444,0.01296,-0.0197,1.0000,0.2233 -4.500,-0.4393,0.02371,0.01208,-0.0190,1.0000,0.2323 -4.250,-0.4162,0.02301,0.01152,-0.0181,1.0000,0.2412 -4.000,-0.3928,0.02237,0.01086,-0.0173,1.0000,0.2517 -3.750,-0.3697,0.02178,0.01030,-0.0165,1.0000,0.2635 -3.500,-0.3469,0.02120,0.00983,-0.0156,1.0000,0.2762 -3.250,-0.3239,0.02066,0.00939,-0.0149,1.0000,0.2915 -3.000,-0.3019,0.02016,0.00901,-0.0140,1.0000,0.3095 -2.750,-0.2804,0.01968,0.00867,-0.0130,1.0000,0.3304 -2.500,-0.2598,0.01922,0.00845,-0.0119,1.0000,0.3557 -2.250,-0.2400,0.01880,0.00827,-0.0108,1.0000,0.3886 -2.000,-0.2212,0.01846,0.00819,-0.0094,1.0000,0.4313 -1.750,-0.2038,0.01819,0.00821,-0.0078,1.0000,0.4829 -1.500,-0.1824,0.01801,0.00834,-0.0069,0.9959,0.5403 -1.250,-0.1416,0.01791,0.00852,-0.0093,0.9757,0.6083 -1.000,-0.1011,0.01784,0.00867,-0.0112,0.9556,0.6699 -0.750,-0.0619,0.01775,0.00876,-0.0126,0.9344,0.7237 -0.500,-0.0156,0.01761,0.00877,-0.0147,0.9114,0.7768 -0.250,0.0313,0.01743,0.00867,-0.0165,0.8807,0.8263 0.000,0.0796,0.01728,0.00853,-0.0183,0.8454,0.8764 0.250,0.1387,0.01718,0.00839,-0.0223,0.8091,0.9350 0.500,0.2038,0.01705,0.00812,-0.0283,0.7695,0.9850 0.750,0.2364,0.01704,0.00791,-0.0291,0.7338,1.0000 1.000,0.2547,0.01713,0.00781,-0.0272,0.7015,1.0000 1.250,0.2738,0.01726,0.00775,-0.0254,0.6689,1.0000 1.500,0.2937,0.01743,0.00773,-0.0237,0.6354,1.0000 1.750,0.3145,0.01764,0.00774,-0.0220,0.6011,1.0000 2.000,0.3358,0.01788,0.00778,-0.0205,0.5653,1.0000 2.250,0.3575,0.01816,0.00786,-0.0190,0.5286,1.0000 2.500,0.3797,0.01850,0.00797,-0.0177,0.4923,1.0000 2.750,0.4021,0.01889,0.00814,-0.0165,0.4573,1.0000 3.000,0.4251,0.01933,0.00839,-0.0154,0.4251,1.0000 3.250,0.4492,0.01982,0.00870,-0.0147,0.3970,1.0000 3.500,0.4737,0.02036,0.00905,-0.0140,0.3748,1.0000 3.750,0.4987,0.02091,0.00947,-0.0135,0.3553,1.0000 4.000,0.5238,0.02148,0.00993,-0.0129,0.3381,1.0000 4.250,0.5489,0.02207,0.01042,-0.0124,0.3236,1.0000 4.500,0.5740,0.02269,0.01099,-0.0119,0.3099,1.0000 4.750,0.5990,0.02332,0.01161,-0.0114,0.2969,1.0000 5.000,0.6242,0.02401,0.01227,-0.0109,0.2858,1.0000 5.250,0.6491,0.02471,0.01287,-0.0103,0.2756,1.0000 5.500,0.6740,0.02546,0.01374,-0.0099,0.2651,1.0000 5.750,0.6988,0.02626,0.01452,-0.0093,0.2561,1.0000 6.000,0.7234,0.02708,0.01542,-0.0088,0.2469,1.0000 6.250,0.7478,0.02800,0.01641,-0.0083,0.2387,1.0000 6.500,0.7718,0.02890,0.01736,-0.0078,0.2301,1.0000 6.750,0.7954,0.02993,0.01852,-0.0073,0.2222,1.0000 7.000,0.8188,0.03096,0.01967,-0.0067,0.2144,1.0000 7.250,0.8418,0.03206,0.02085,-0.0061,0.2073,1.0000 7.500,0.8634,0.03326,0.02226,-0.0055,0.1993,1.0000 7.750,0.8872,0.03428,0.02323,-0.0049,0.1935,1.0000 8.000,0.9054,0.03589,0.02527,-0.0042,0.1856,1.0000 8.250,0.9276,0.03691,0.02630,-0.0036,0.1794,1.0000 8.500,0.9449,0.03868,0.02839,-0.0028,0.1730,1.0000 8.750,0.9627,0.04017,0.03010,-0.0020,0.1664,1.0000 9.000,0.9846,0.04119,0.03106,-0.0014,0.1614,1.0000 9.250,0.9930,0.04383,0.03423,-0.0004,0.1550,1.0000 9.500,1.0102,0.04516,0.03566,0.0004,0.1496,1.0000 9.750,1.0238,0.04703,0.03771,0.0013,0.1450,1.0000 10.000,1.0234,0.05037,0.04150,0.0022,0.1401,1.0000 10.250,1.0347,0.05207,0.04333,0.0031,0.1356,1.0000 10.500,1.0472,0.05375,0.04507,0.0039,0.1320,1.0000 10.750,1.0203,0.05927,0.05104,0.0045,0.1294,1.0000 11.000,0.9791,0.06568,0.05770,0.0041,0.1282,1.0000 11.250,0.8814,0.08324,0.07534,-0.0078,0.1287,1.0000 11.500,0.8244,0.09952,0.09155,-0.0189,0.1257,1.0000