Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e176-il-50000-n5 Airfoil,e176-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,38.6905 Max Cl/Cd alpha,7.5 Url,http://airfoiltools.com/polar/csv?polar=xf-e176-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.3942,0.10489,0.09825,-0.0191,1.0000,0.1067 -8.500,-0.3906,0.10170,0.09512,-0.0207,1.0000,0.1087 -8.250,-0.3991,0.09965,0.09321,-0.0244,1.0000,0.1133 -7.750,-0.3931,0.08774,0.08137,-0.0316,1.0000,0.0587 -7.500,-0.3871,0.08418,0.07787,-0.0325,1.0000,0.0575 -7.250,-0.3834,0.08036,0.07412,-0.0351,1.0000,0.0570 -7.000,-0.3787,0.07657,0.07039,-0.0374,1.0000,0.0557 -6.750,-0.3745,0.07258,0.06645,-0.0401,1.0000,0.0549 -6.500,-0.3706,0.06855,0.06241,-0.0425,1.0000,0.0540 -6.250,-0.3678,0.06466,0.05853,-0.0443,1.0000,0.0526 -6.000,-0.3668,0.06079,0.05464,-0.0454,1.0000,0.0514 -5.750,-0.3673,0.05694,0.05068,-0.0460,1.0000,0.0497 -5.250,-0.3304,0.04711,0.03986,-0.0529,0.9864,0.0462 -5.000,-0.2971,0.04262,0.03490,-0.0571,0.9746,0.0459 -4.750,-0.2625,0.03861,0.03031,-0.0607,0.9636,0.0457 -4.500,-0.2256,0.03507,0.02614,-0.0639,0.9541,0.0459 -4.250,-0.1890,0.03215,0.02259,-0.0663,0.9445,0.0463 -4.000,-0.1543,0.02964,0.01967,-0.0681,0.9346,0.0475 -3.750,-0.1190,0.02789,0.01770,-0.0700,0.9257,0.0517 -3.500,-0.0841,0.02642,0.01580,-0.0712,0.9162,0.0577 -3.250,-0.0517,0.02498,0.01412,-0.0718,0.9063,0.0620 -3.000,-0.0173,0.02377,0.01271,-0.0728,0.8977,0.0696 -2.750,0.0147,0.02272,0.01148,-0.0734,0.8881,0.0862 -2.500,0.0440,0.02153,0.01063,-0.0741,0.8782,0.1528 -2.250,0.0711,0.01988,0.01009,-0.0746,0.8697,0.3625 -2.000,0.0881,0.01858,0.01001,-0.0715,0.8603,0.6549 -1.750,0.1540,0.01778,0.00922,-0.0770,0.8554,1.0000 -1.500,0.1810,0.01794,0.00894,-0.0769,0.8454,1.0000 -1.250,0.2065,0.01815,0.00879,-0.0766,0.8352,1.0000 -1.000,0.2333,0.01834,0.00866,-0.0765,0.8263,1.0000 -0.750,0.2595,0.01855,0.00857,-0.0762,0.8174,1.0000 -0.500,0.2842,0.01882,0.00860,-0.0758,0.8080,1.0000 -0.250,0.3115,0.01902,0.00857,-0.0756,0.8005,1.0000 0.000,0.3356,0.01933,0.00871,-0.0751,0.7912,1.0000 0.250,0.3611,0.01961,0.00882,-0.0747,0.7831,1.0000 0.500,0.3873,0.01989,0.00895,-0.0745,0.7752,1.0000 0.750,0.4122,0.02024,0.00919,-0.0742,0.7668,1.0000 1.000,0.4391,0.02051,0.00934,-0.0739,0.7599,1.0000 1.250,0.4631,0.02092,0.00970,-0.0735,0.7512,1.0000 1.500,0.4904,0.02117,0.00987,-0.0732,0.7449,1.0000 1.750,0.5137,0.02165,0.01032,-0.0728,0.7359,1.0000 2.000,0.5406,0.02193,0.01058,-0.0725,0.7296,1.0000 2.250,0.5639,0.02243,0.01109,-0.0721,0.7208,1.0000 2.500,0.5896,0.02280,0.01146,-0.0717,0.7137,1.0000 2.750,0.6139,0.02324,0.01194,-0.0712,0.7055,1.0000 3.000,0.6382,0.02370,0.01248,-0.0708,0.6975,1.0000 3.250,0.6637,0.02407,0.01290,-0.0703,0.6900,1.0000 3.500,0.6866,0.02461,0.01353,-0.0698,0.6808,1.0000 3.750,0.7140,0.02483,0.01381,-0.0692,0.6741,1.0000 4.000,0.7358,0.02542,0.01453,-0.0685,0.6635,1.0000 4.250,0.7593,0.02587,0.01515,-0.0678,0.6537,1.0000 4.500,0.7869,0.02598,0.01537,-0.0671,0.6457,1.0000 4.750,0.8089,0.02647,0.01601,-0.0662,0.6339,1.0000 5.000,0.8317,0.02685,0.01656,-0.0652,0.6219,1.0000 5.250,0.8552,0.02711,0.01706,-0.0641,0.6094,1.0000 5.500,0.8791,0.02728,0.01741,-0.0630,0.5961,1.0000 5.750,0.9029,0.02737,0.01770,-0.0617,0.5817,1.0000 6.000,0.9268,0.02736,0.01790,-0.0603,0.5660,1.0000 6.250,0.9516,0.02716,0.01791,-0.0587,0.5489,1.0000 6.500,0.9724,0.02720,0.01825,-0.0570,0.5278,1.0000 6.750,0.9954,0.02691,0.01817,-0.0551,0.5046,1.0000 7.000,1.0148,0.02689,0.01837,-0.0531,0.4760,1.0000 7.250,1.0325,0.02697,0.01866,-0.0509,0.4402,1.0000 7.500,1.0489,0.02711,0.01886,-0.0484,0.3941,1.0000 7.750,1.0606,0.02772,0.01930,-0.0457,0.3310,1.0000 8.000,1.0650,0.02917,0.02028,-0.0427,0.2625,1.0000 8.250,1.0630,0.03139,0.02209,-0.0400,0.2030,1.0000 8.500,1.0572,0.03396,0.02421,-0.0374,0.1505,1.0000 8.750,1.0496,0.03664,0.02647,-0.0351,0.1092,1.0000 9.000,1.0448,0.03945,0.02901,-0.0333,0.0806,1.0000 9.250,1.0428,0.04226,0.03174,-0.0318,0.0640,1.0000 9.500,1.0421,0.04511,0.03457,-0.0305,0.0551,1.0000 9.750,1.0444,0.04777,0.03731,-0.0293,0.0489,1.0000 10.000,1.0491,0.05035,0.03997,-0.0279,0.0447,1.0000 10.250,1.0582,0.05262,0.04245,-0.0267,0.0403,1.0000 10.500,1.0647,0.05511,0.04498,-0.0258,0.0369,1.0000 10.750,1.0786,0.05735,0.04745,-0.0244,0.0341,1.0000 11.000,1.0951,0.05974,0.05019,-0.0230,0.0320,1.0000 11.250,1.1078,0.06272,0.05351,-0.0219,0.0307,1.0000 11.500,1.1142,0.06615,0.05733,-0.0212,0.0300,1.0000 11.750,1.1147,0.07005,0.06154,-0.0210,0.0294,1.0000 12.000,1.1107,0.07436,0.06615,-0.0214,0.0292,1.0000 12.250,1.1024,0.07915,0.07123,-0.0223,0.0290,1.0000 12.500,1.0905,0.08451,0.07686,-0.0238,0.0289,1.0000 12.750,1.0755,0.09049,0.08310,-0.0262,0.0290,1.0000 13.000,1.0580,0.09724,0.09008,-0.0295,0.0292,1.0000 13.250,1.0374,0.10499,0.09804,-0.0338,0.0295,1.0000 13.500,1.0155,0.11388,0.10711,-0.0393,0.0300,1.0000