Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e182-il-50000-n5 Airfoil,e182-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,34.1231 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e182-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.5651,0.09276,0.08643,0.0023,1.0000,0.0459 -8.250,-0.5652,0.08797,0.08172,-0.0011,1.0000,0.0448 -8.000,-0.5671,0.08297,0.07678,-0.0052,1.0000,0.0437 -7.750,-0.5675,0.07755,0.07138,-0.0095,1.0000,0.0426 -7.500,-0.5673,0.07170,0.06547,-0.0136,1.0000,0.0414 -7.250,-0.5665,0.06553,0.05919,-0.0174,1.0000,0.0401 -7.000,-0.5646,0.05902,0.05230,-0.0206,1.0000,0.0385 -6.500,-0.5421,0.05010,0.04248,-0.0224,1.0000,0.0374 -6.250,-0.5275,0.04613,0.03812,-0.0226,1.0000,0.0374 -6.000,-0.5116,0.04232,0.03400,-0.0227,1.0000,0.0381 -5.750,-0.4936,0.03932,0.03076,-0.0227,1.0000,0.0396 -5.500,-0.4734,0.03678,0.02796,-0.0226,1.0000,0.0417 -5.250,-0.4519,0.03408,0.02484,-0.0222,1.0000,0.0431 -5.000,-0.4292,0.03151,0.02185,-0.0217,1.0000,0.0441 -4.750,-0.4062,0.02926,0.01922,-0.0210,1.0000,0.0455 -4.500,-0.3842,0.02737,0.01696,-0.0200,1.0000,0.0473 -4.250,-0.3646,0.02585,0.01515,-0.0185,1.0000,0.0495 -4.000,-0.3494,0.02460,0.01391,-0.0168,0.9995,0.0534 -3.750,-0.3113,0.02318,0.01230,-0.0191,0.9830,0.0652 -3.500,-0.2722,0.02161,0.01066,-0.0214,0.9696,0.0908 -3.250,-0.2368,0.01971,0.00951,-0.0240,0.9570,0.2096 -3.000,-0.2081,0.01801,0.00888,-0.0249,0.9441,0.4215 -2.750,-0.1795,0.01672,0.00875,-0.0234,0.9336,0.6991 -2.500,-0.0819,0.01636,0.00817,-0.0337,0.9376,0.9523 -2.250,-0.0182,0.01621,0.00749,-0.0410,0.9308,1.0000 -2.000,0.0124,0.01627,0.00717,-0.0422,0.9144,1.0000 -1.750,0.0400,0.01638,0.00697,-0.0426,0.8992,1.0000 -1.500,0.0656,0.01652,0.00685,-0.0426,0.8854,1.0000 -1.250,0.0900,0.01669,0.00679,-0.0422,0.8726,1.0000 -1.000,0.1138,0.01688,0.00675,-0.0416,0.8609,1.0000 -0.750,0.1369,0.01709,0.00678,-0.0409,0.8491,1.0000 -0.500,0.1601,0.01731,0.00684,-0.0403,0.8381,1.0000 -0.250,0.1834,0.01754,0.00694,-0.0396,0.8281,1.0000 0.000,0.2065,0.01778,0.00705,-0.0387,0.8186,1.0000 0.250,0.2299,0.01805,0.00723,-0.0381,0.8084,1.0000 0.500,0.2532,0.01832,0.00742,-0.0374,0.7992,1.0000 0.750,0.2765,0.01859,0.00763,-0.0366,0.7904,1.0000 1.000,0.2999,0.01891,0.00793,-0.0360,0.7807,1.0000 1.250,0.3233,0.01921,0.00819,-0.0352,0.7724,1.0000 1.500,0.3467,0.01953,0.00852,-0.0345,0.7632,1.0000 1.750,0.3701,0.01989,0.00889,-0.0339,0.7539,1.0000 2.000,0.3936,0.02017,0.00920,-0.0329,0.7460,1.0000 2.250,0.4172,0.02057,0.00966,-0.0324,0.7356,1.0000 2.500,0.4406,0.02093,0.01008,-0.0316,0.7261,1.0000 2.750,0.4639,0.02120,0.01044,-0.0304,0.7172,1.0000 3.000,0.4869,0.02158,0.01093,-0.0297,0.7057,1.0000 3.250,0.5098,0.02193,0.01139,-0.0287,0.6942,1.0000 3.500,0.5327,0.02221,0.01178,-0.0275,0.6827,1.0000 3.750,0.5557,0.02243,0.01216,-0.0261,0.6706,1.0000 4.000,0.5785,0.02260,0.01248,-0.0246,0.6574,1.0000 4.250,0.6010,0.02277,0.01280,-0.0231,0.6422,1.0000 4.500,0.6233,0.02290,0.01312,-0.0216,0.6250,1.0000 4.750,0.6457,0.02291,0.01332,-0.0198,0.6064,1.0000 5.000,0.6685,0.02274,0.01336,-0.0177,0.5870,1.0000 5.250,0.6904,0.02269,0.01354,-0.0159,0.5618,1.0000 5.500,0.7123,0.02251,0.01358,-0.0139,0.5328,1.0000 5.750,0.7338,0.02238,0.01366,-0.0119,0.4957,1.0000 6.000,0.7542,0.02228,0.01372,-0.0096,0.4429,1.0000 6.250,0.7705,0.02258,0.01368,-0.0069,0.3454,1.0000 6.500,0.7769,0.02467,0.01462,-0.0049,0.2064,1.0000 6.750,0.7824,0.02741,0.01644,-0.0038,0.1091,1.0000 7.000,0.7917,0.02974,0.01846,-0.0024,0.0719,1.0000 7.250,0.8022,0.03187,0.02047,-0.0009,0.0583,1.0000 7.500,0.8160,0.03366,0.02246,0.0008,0.0513,1.0000 7.750,0.8296,0.03556,0.02439,0.0023,0.0469,1.0000 8.000,0.8492,0.03724,0.02639,0.0038,0.0423,1.0000 8.250,0.8674,0.03903,0.02833,0.0050,0.0386,1.0000 8.500,0.8863,0.04128,0.03063,0.0061,0.0363,1.0000 8.750,0.9077,0.04389,0.03356,0.0072,0.0352,1.0000 9.000,0.9253,0.04683,0.03691,0.0083,0.0344,1.0000 9.250,0.9378,0.05006,0.04057,0.0093,0.0339,1.0000 9.500,0.9448,0.05361,0.04455,0.0104,0.0335,1.0000 9.750,0.9465,0.05726,0.04857,0.0113,0.0333,1.0000 10.000,0.9425,0.06105,0.05276,0.0121,0.0333,1.0000 10.250,0.9322,0.06472,0.05669,0.0129,0.0333,1.0000 10.500,0.9186,0.06874,0.06093,0.0127,0.0334,1.0000 10.750,0.9031,0.07329,0.06568,0.0115,0.0336,1.0000 11.000,0.8857,0.07853,0.07108,0.0091,0.0337,1.0000 11.250,0.8682,0.08437,0.07699,0.0059,0.0340,1.0000 11.500,0.8504,0.09099,0.08371,0.0017,0.0343,1.0000