Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx76120-il-50000-n5 Airfoil,fx76120-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.692 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-fx76120-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.7463,0.09139,0.08329,-0.0265,1.0000,0.0817 -12.250,-0.8020,0.07751,0.06929,-0.0356,1.0000,0.0804 -12.000,-0.8451,0.06853,0.06012,-0.0406,1.0000,0.0797 -11.750,-0.8746,0.06273,0.05410,-0.0421,1.0000,0.0797 -11.500,-0.8976,0.05838,0.04951,-0.0416,1.0000,0.0805 -11.250,-0.9159,0.05484,0.04568,-0.0397,1.0000,0.0815 -11.000,-0.9318,0.05172,0.04223,-0.0367,1.0000,0.0830 -10.750,-0.9282,0.04950,0.03994,-0.0348,1.0000,0.0852 -10.500,-0.9213,0.04767,0.03805,-0.0331,1.0000,0.0878 -10.250,-0.9171,0.04562,0.03581,-0.0310,1.0000,0.0911 -10.000,-0.9144,0.04325,0.03306,-0.0287,1.0000,0.0951 -9.750,-0.9025,0.04164,0.03146,-0.0271,1.0000,0.0990 -9.500,-0.8914,0.04007,0.02977,-0.0253,1.0000,0.1036 -9.250,-0.8811,0.03822,0.02762,-0.0233,1.0000,0.1096 -9.000,-0.8674,0.03702,0.02650,-0.0216,1.0000,0.1153 -8.750,-0.8541,0.03544,0.02466,-0.0197,1.0000,0.1230 -8.500,-0.8403,0.03436,0.02367,-0.0179,1.0000,0.1306 -8.250,-0.8258,0.03311,0.02230,-0.0160,1.0000,0.1399 -8.000,-0.8113,0.03196,0.02100,-0.0141,1.0000,0.1515 -7.750,-0.7969,0.03102,0.02013,-0.0122,1.0000,0.1630 -7.500,-0.7821,0.03009,0.01920,-0.0102,1.0000,0.1761 -7.250,-0.7670,0.02923,0.01829,-0.0083,1.0000,0.1908 -7.000,-0.7517,0.02843,0.01748,-0.0063,1.0000,0.2066 -6.750,-0.7358,0.02769,0.01671,-0.0044,1.0000,0.2228 -6.500,-0.7194,0.02699,0.01599,-0.0025,1.0000,0.2397 -6.250,-0.7027,0.02633,0.01531,-0.0007,1.0000,0.2570 -6.000,-0.6855,0.02570,0.01465,0.0011,1.0000,0.2746 -5.750,-0.6679,0.02510,0.01402,0.0029,1.0000,0.2926 -5.500,-0.6498,0.02452,0.01345,0.0046,1.0000,0.3106 -5.250,-0.6313,0.02396,0.01293,0.0062,1.0000,0.3286 -5.000,-0.6125,0.02342,0.01243,0.0079,1.0000,0.3473 -4.750,-0.5934,0.02290,0.01195,0.0094,1.0000,0.3666 -4.500,-0.5740,0.02240,0.01149,0.0110,1.0000,0.3873 -4.250,-0.5546,0.02192,0.01102,0.0125,1.0000,0.4098 -4.000,-0.5352,0.02146,0.01067,0.0141,1.0000,0.4328 -3.750,-0.5160,0.02102,0.01031,0.0157,1.0000,0.4591 -3.500,-0.4969,0.02061,0.01005,0.0173,1.0000,0.4867 -3.250,-0.4786,0.02025,0.00981,0.0192,1.0000,0.5171 -3.000,-0.4607,0.01994,0.00965,0.0212,1.0000,0.5511 -2.750,-0.4425,0.01967,0.00954,0.0233,1.0000,0.5881 -2.500,-0.4239,0.01947,0.00950,0.0253,1.0000,0.6282 -2.250,-0.4037,0.01936,0.00957,0.0273,1.0000,0.6697 -2.000,-0.3824,0.01934,0.00969,0.0290,1.0000,0.7132 -1.750,-0.3578,0.01943,0.00990,0.0302,1.0000,0.7564 -1.500,-0.3300,0.01960,0.01014,0.0308,1.0000,0.7982 -1.250,-0.2972,0.01986,0.01043,0.0303,1.0000,0.8374 -1.000,-0.2606,0.02017,0.01072,0.0289,1.0000,0.8738 -0.750,-0.2167,0.02052,0.01105,0.0259,0.9997,0.9055 -0.500,-0.1479,0.02094,0.01140,0.0179,0.9891,0.9289 -0.250,-0.0733,0.02124,0.01165,0.0089,0.9778,0.9470 0.000,0.0001,0.02133,0.01173,0.0000,0.9634,0.9634 0.250,0.0732,0.02124,0.01166,-0.0089,0.9471,0.9780 0.500,0.1482,0.02093,0.01139,-0.0180,0.9289,0.9892 0.750,0.2169,0.02052,0.01104,-0.0259,0.9052,0.9997 1.000,0.2606,0.02017,0.01072,-0.0289,0.8737,1.0000 1.250,0.2971,0.01986,0.01043,-0.0303,0.8375,1.0000 1.500,0.3300,0.01960,0.01014,-0.0308,0.7982,1.0000 1.750,0.3578,0.01942,0.00990,-0.0302,0.7562,1.0000 2.000,0.3824,0.01934,0.00969,-0.0290,0.7132,1.0000 2.250,0.4037,0.01936,0.00956,-0.0272,0.6697,1.0000 2.500,0.4239,0.01947,0.00949,-0.0253,0.6285,1.0000 2.750,0.4425,0.01967,0.00954,-0.0233,0.5881,1.0000 3.000,0.4607,0.01994,0.00965,-0.0212,0.5512,1.0000 3.250,0.4786,0.02025,0.00981,-0.0192,0.5172,1.0000 3.500,0.4968,0.02061,0.01005,-0.0173,0.4866,1.0000 3.750,0.5160,0.02102,0.01030,-0.0157,0.4589,1.0000 4.000,0.5352,0.02145,0.01067,-0.0141,0.4329,1.0000 4.250,0.5546,0.02192,0.01102,-0.0125,0.4099,1.0000 4.500,0.5741,0.02240,0.01149,-0.0110,0.3875,1.0000 4.750,0.5934,0.02290,0.01195,-0.0094,0.3666,1.0000 5.000,0.6125,0.02342,0.01243,-0.0079,0.3472,1.0000 5.250,0.6313,0.02396,0.01293,-0.0062,0.3286,1.0000 5.500,0.6498,0.02452,0.01345,-0.0046,0.3107,1.0000 5.750,0.6679,0.02510,0.01402,-0.0029,0.2926,1.0000 6.000,0.6855,0.02570,0.01465,-0.0011,0.2746,1.0000 6.250,0.7028,0.02633,0.01531,0.0007,0.2571,1.0000 6.500,0.7195,0.02699,0.01599,0.0025,0.2398,1.0000 6.750,0.7357,0.02768,0.01671,0.0044,0.2227,1.0000 7.000,0.7516,0.02842,0.01747,0.0063,0.2064,1.0000 7.250,0.7670,0.02923,0.01831,0.0083,0.1908,1.0000 7.500,0.7821,0.03009,0.01920,0.0102,0.1762,1.0000 7.750,0.7970,0.03102,0.02012,0.0122,0.1630,1.0000 8.000,0.8115,0.03196,0.02102,0.0141,0.1516,1.0000 8.250,0.8260,0.03311,0.02231,0.0160,0.1400,1.0000 8.500,0.8403,0.03435,0.02366,0.0179,0.1305,1.0000 8.750,0.8541,0.03543,0.02465,0.0197,0.1229,1.0000 9.000,0.8674,0.03700,0.02649,0.0216,0.1152,1.0000 9.250,0.8810,0.03820,0.02759,0.0233,0.1094,1.0000 9.500,0.8915,0.04005,0.02977,0.0252,0.1036,1.0000 9.750,0.9028,0.04165,0.03147,0.0270,0.0990,1.0000 10.000,0.9149,0.04327,0.03308,0.0286,0.0952,1.0000 10.250,0.9175,0.04563,0.03583,0.0310,0.0912,1.0000 10.500,0.9215,0.04769,0.03807,0.0330,0.0878,1.0000 10.750,0.9286,0.04950,0.03993,0.0348,0.0851,1.0000 11.000,0.9315,0.05175,0.04226,0.0367,0.0829,1.0000 11.250,0.9163,0.05484,0.04568,0.0396,0.0815,1.0000 11.500,0.8977,0.05842,0.04954,0.0415,0.0804,1.0000 11.750,0.8753,0.06272,0.05408,0.0420,0.0797,1.0000 12.000,0.8451,0.06860,0.06019,0.0405,0.0796,1.0000 12.250,0.8020,0.07760,0.06938,0.0354,0.0803,1.0000 12.500,0.7457,0.09170,0.08360,0.0261,0.0816,1.0000