Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-eh1070-il-50000-n5 Airfoil,eh1070-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,30.274 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-eh1070-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5100,0.10412,0.09787,0.0082,1.0000,0.0532 -9.000,-0.5986,0.10468,0.09805,0.0098,1.0000,0.0436 -8.750,-0.5958,0.10039,0.09380,0.0083,1.0000,0.0421 -8.500,-0.5953,0.09599,0.08947,0.0058,1.0000,0.0415 -8.250,-0.5954,0.09156,0.08510,0.0032,1.0000,0.0403 -8.000,-0.5978,0.08691,0.08053,-0.0002,1.0000,0.0397 -7.750,-0.5997,0.08222,0.07586,-0.0033,1.0000,0.0387 -7.500,-0.5994,0.07742,0.07105,-0.0062,1.0000,0.0382 -7.250,-0.5976,0.07256,0.06613,-0.0087,1.0000,0.0377 -7.000,-0.5937,0.06791,0.06137,-0.0106,1.0000,0.0378 -6.750,-0.5874,0.06343,0.05674,-0.0120,1.0000,0.0381 -6.500,-0.5789,0.05908,0.05218,-0.0130,1.0000,0.0390 -6.250,-0.5682,0.05472,0.04754,-0.0137,1.0000,0.0394 -6.000,-0.5553,0.05041,0.04288,-0.0139,1.0000,0.0393 -5.750,-0.5401,0.04614,0.03805,-0.0137,1.0000,0.0387 -5.500,-0.5227,0.04211,0.03355,-0.0133,1.0000,0.0383 -5.250,-0.5030,0.03845,0.02937,-0.0125,1.0000,0.0382 -5.000,-0.4814,0.03507,0.02545,-0.0116,1.0000,0.0386 -4.750,-0.4578,0.03207,0.02194,-0.0107,1.0000,0.0395 -4.500,-0.4327,0.02941,0.01880,-0.0097,1.0000,0.0409 -4.250,-0.4064,0.02708,0.01604,-0.0087,1.0000,0.0430 -4.000,-0.3806,0.02516,0.01389,-0.0078,1.0000,0.0483 -3.750,-0.3548,0.02380,0.01225,-0.0069,1.0000,0.0586 -3.500,-0.3297,0.02214,0.01055,-0.0060,1.0000,0.0680 -3.250,-0.3049,0.02068,0.00910,-0.0053,1.0000,0.0949 -3.000,-0.2840,0.01876,0.00761,-0.0043,1.0000,0.1754 -2.750,-0.2763,0.01590,0.00691,-0.0009,1.0000,0.5345 -2.500,-0.1741,0.01559,0.00678,-0.0091,1.0000,0.9703 -2.250,-0.1153,0.01527,0.00588,-0.0156,1.0000,1.0000 -2.000,-0.0958,0.01507,0.00545,-0.0146,1.0000,1.0000 -1.750,-0.0763,0.01491,0.00501,-0.0135,1.0000,1.0000 -1.500,-0.0572,0.01479,0.00472,-0.0124,1.0000,1.0000 -1.250,-0.0384,0.01469,0.00448,-0.0112,1.0000,1.0000 -1.000,-0.0201,0.01463,0.00431,-0.0098,1.0000,1.0000 -0.750,-0.0026,0.01459,0.00419,-0.0084,1.0000,1.0000 -0.500,0.0138,0.01459,0.00413,-0.0068,1.0000,1.0000 -0.250,0.0288,0.01464,0.00411,-0.0050,1.0000,1.0000 0.000,0.0422,0.01474,0.00418,-0.0030,1.0000,1.0000 0.250,0.0538,0.01492,0.00433,-0.0009,1.0000,1.0000 0.500,0.1034,0.01510,0.00449,-0.0060,0.9726,1.0000 0.750,0.1538,0.01525,0.00466,-0.0110,0.9445,1.0000 1.000,0.2010,0.01537,0.00483,-0.0150,0.9148,1.0000 1.250,0.2416,0.01550,0.00497,-0.0174,0.8824,1.0000 1.500,0.2766,0.01563,0.00512,-0.0184,0.8502,1.0000 1.750,0.3055,0.01581,0.00529,-0.0182,0.8184,1.0000 2.000,0.3307,0.01602,0.00558,-0.0171,0.7873,1.0000 2.250,0.3543,0.01626,0.00580,-0.0158,0.7579,1.0000 2.500,0.3772,0.01652,0.00606,-0.0143,0.7297,1.0000 2.750,0.3999,0.01680,0.00636,-0.0128,0.7022,1.0000 3.000,0.4227,0.01710,0.00669,-0.0114,0.6752,1.0000 3.250,0.4456,0.01741,0.00707,-0.0100,0.6485,1.0000 3.500,0.4686,0.01775,0.00760,-0.0087,0.6218,1.0000 3.750,0.4917,0.01810,0.00805,-0.0074,0.5949,1.0000 4.000,0.5149,0.01847,0.00854,-0.0061,0.5678,1.0000 4.250,0.5381,0.01886,0.00908,-0.0049,0.5404,1.0000 4.500,0.5611,0.01926,0.00964,-0.0036,0.5111,1.0000 4.750,0.5842,0.01966,0.01026,-0.0023,0.4777,1.0000 5.000,0.6058,0.02002,0.01078,-0.0006,0.4352,1.0000 5.250,0.6188,0.02044,0.01062,0.0021,0.3050,1.0000 5.500,0.6320,0.02296,0.01201,0.0033,0.1061,1.0000 5.750,0.6484,0.02553,0.01411,0.0042,0.0608,1.0000 6.000,0.6669,0.02744,0.01618,0.0055,0.0507,1.0000 6.250,0.6857,0.02939,0.01836,0.0071,0.0458,1.0000 6.500,0.7054,0.03127,0.02044,0.0085,0.0404,1.0000 6.750,0.7247,0.03347,0.02281,0.0096,0.0349,1.0000 7.000,0.7462,0.03582,0.02552,0.0109,0.0321,1.0000 7.250,0.7667,0.03864,0.02874,0.0120,0.0307,1.0000 7.500,0.7848,0.04182,0.03236,0.0131,0.0298,1.0000 7.750,0.7995,0.04534,0.03634,0.0141,0.0292,1.0000 8.000,0.8103,0.04916,0.04063,0.0149,0.0289,1.0000 8.250,0.8165,0.05325,0.04519,0.0156,0.0289,1.0000 8.500,0.8177,0.05755,0.04991,0.0159,0.0289,1.0000 8.750,0.8135,0.06201,0.05471,0.0158,0.0292,1.0000 9.000,0.8040,0.06658,0.05955,0.0151,0.0295,1.0000 9.250,0.7887,0.07112,0.06425,0.0139,0.0298,1.0000 9.500,0.7718,0.07641,0.06962,0.0105,0.0302,1.0000 9.750,0.7561,0.08304,0.07629,0.0052,0.0307,1.0000 10.000,0.7444,0.09023,0.08348,-0.0003,0.0313,1.0000