Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-eh1090-il-50000 Airfoil,eh1090-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,29.1732 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-eh1090-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.5506,0.10074,0.09424,0.0176,1.0000,0.2938 -8.250,-0.5472,0.09741,0.09096,0.0179,1.0000,0.3105 -8.000,-0.5593,0.09514,0.08880,0.0176,1.0000,0.3286 -7.750,-0.5390,0.09089,0.08450,0.0197,1.0000,0.3540 -7.250,-0.5276,0.08370,0.07740,0.0211,1.0000,0.3891 -7.000,-0.6258,0.06597,0.05938,-0.0143,1.0000,0.1633 -6.750,-0.6135,0.05812,0.05122,-0.0161,1.0000,0.1297 -6.500,-0.6071,0.05226,0.04484,-0.0166,1.0000,0.1170 -6.250,-0.5993,0.04714,0.03875,-0.0159,1.0000,0.1077 -6.000,-0.5844,0.04332,0.03443,-0.0147,1.0000,0.1079 -5.750,-0.5656,0.04000,0.03117,-0.0139,1.0000,0.1137 -5.500,-0.5464,0.03666,0.02735,-0.0126,1.0000,0.1155 -5.250,-0.5246,0.03344,0.02357,-0.0112,1.0000,0.1179 -5.000,-0.5017,0.03067,0.02045,-0.0100,1.0000,0.1258 -4.750,-0.4785,0.02843,0.01798,-0.0088,1.0000,0.1418 -4.500,-0.4527,0.02610,0.01537,-0.0075,1.0000,0.1621 -4.250,-0.4281,0.02391,0.01343,-0.0063,1.0000,0.1999 -4.000,-0.4042,0.02178,0.01167,-0.0050,1.0000,0.2637 -3.750,-0.3851,0.01932,0.01012,-0.0030,1.0000,0.3805 -3.500,-0.3800,0.01724,0.01041,0.0063,1.0000,0.7399 -3.250,-0.1273,0.01908,0.01009,-0.0239,1.0000,1.0000 -3.000,-0.1127,0.01847,0.00925,-0.0234,1.0000,1.0000 -2.750,-0.0973,0.01798,0.00859,-0.0228,1.0000,1.0000 -2.500,-0.0815,0.01757,0.00804,-0.0220,1.0000,1.0000 -2.250,-0.0658,0.01723,0.00757,-0.0210,1.0000,1.0000 -2.000,-0.0505,0.01695,0.00720,-0.0199,1.0000,1.0000 -1.750,-0.0360,0.01673,0.00690,-0.0185,1.0000,1.0000 -1.500,-0.0229,0.01657,0.00665,-0.0169,1.0000,1.0000 -1.250,-0.0125,0.01647,0.00653,-0.0148,1.0000,1.0000 -1.000,-0.0061,0.01646,0.00650,-0.0120,1.0000,1.0000 -0.750,-0.0046,0.01655,0.00658,-0.0086,1.0000,1.0000 -0.500,-0.0083,0.01676,0.00677,-0.0046,1.0000,1.0000 -0.250,-0.0130,0.01707,0.00702,-0.0006,1.0000,1.0000 0.000,-0.0153,0.01745,0.00733,0.0027,1.0000,1.0000 0.250,-0.0144,0.01790,0.00770,0.0054,1.0000,1.0000 0.500,-0.0102,0.01841,0.00812,0.0073,1.0000,1.0000 0.750,0.0371,0.01925,0.00893,0.0013,0.9855,1.0000 1.000,0.1118,0.02008,0.00979,-0.0091,0.9597,1.0000 1.250,0.1847,0.02066,0.01045,-0.0186,0.9339,1.0000 1.500,0.2629,0.02095,0.01088,-0.0285,0.9088,1.0000 1.750,0.3271,0.02105,0.01114,-0.0349,0.8830,1.0000 2.000,0.3759,0.02115,0.01136,-0.0381,0.8570,1.0000 2.250,0.4111,0.02136,0.01165,-0.0387,0.8309,1.0000 2.500,0.4371,0.02170,0.01210,-0.0376,0.8050,1.0000 2.750,0.4600,0.02210,0.01255,-0.0359,0.7800,1.0000 3.000,0.4823,0.02248,0.01299,-0.0340,0.7565,1.0000 3.250,0.5040,0.02284,0.01340,-0.0318,0.7338,1.0000 3.500,0.5230,0.02338,0.01406,-0.0296,0.7098,1.0000 3.750,0.5432,0.02383,0.01458,-0.0273,0.6873,1.0000 4.000,0.5637,0.02426,0.01508,-0.0249,0.6648,1.0000 4.250,0.5830,0.02485,0.01577,-0.0228,0.6410,1.0000 4.500,0.6036,0.02532,0.01631,-0.0205,0.6182,1.0000 4.750,0.6246,0.02573,0.01680,-0.0181,0.5947,1.0000 5.000,0.6444,0.02631,0.01757,-0.0159,0.5693,1.0000 5.250,0.6649,0.02680,0.01817,-0.0136,0.5433,1.0000 5.500,0.6857,0.02721,0.01868,-0.0112,0.5160,1.0000 5.750,0.7067,0.02755,0.01912,-0.0088,0.4871,1.0000 6.000,0.7283,0.02784,0.01948,-0.0062,0.4567,1.0000 6.250,0.7481,0.02795,0.01972,-0.0034,0.4188,1.0000 6.500,0.7672,0.02731,0.01889,0.0002,0.3699,1.0000 6.750,0.7798,0.02673,0.01802,0.0041,0.3012,1.0000 7.000,0.7845,0.02781,0.01838,0.0081,0.2074,1.0000 7.250,0.7957,0.03046,0.02057,0.0108,0.1486,1.0000 7.500,0.8125,0.03289,0.02287,0.0125,0.1205,1.0000 7.750,0.8345,0.03581,0.02589,0.0139,0.1071,1.0000 8.000,0.8555,0.03895,0.02911,0.0150,0.0986,1.0000 8.250,0.8716,0.04183,0.03242,0.0164,0.0913,1.0000 8.500,0.8881,0.04545,0.03615,0.0173,0.0865,1.0000 8.750,0.8971,0.04949,0.04086,0.0188,0.0856,1.0000 9.000,0.9017,0.05383,0.04571,0.0201,0.0855,1.0000 9.250,0.9027,0.05841,0.05068,0.0211,0.0858,1.0000 9.500,0.9017,0.06313,0.05569,0.0219,0.0865,1.0000 9.750,0.9013,0.06821,0.06099,0.0223,0.0872,1.0000 10.000,0.8467,0.07284,0.06617,0.0217,0.0903,1.0000 10.250,0.8051,0.07979,0.07313,0.0171,0.0934,1.0000 10.500,0.7783,0.08794,0.08126,0.0110,0.0964,1.0000 10.750,0.7667,0.09516,0.08844,0.0071,0.0985,1.0000 11.000,0.7671,0.10095,0.09424,0.0054,0.1004,1.0000