Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa5-il-1000000-n5 Airfoil,usa5-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,99.7359 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-usa5-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.3567,0.12420,0.12254,-0.0196,1.0000,0.0035 -10.500,-0.3521,0.12098,0.11933,-0.0204,1.0000,0.0035 -8.500,-0.3205,0.09756,0.09603,-0.0251,0.9994,0.0042 -8.000,-0.2955,0.09048,0.08895,-0.0314,0.9915,0.0048 -7.750,-0.2823,0.08689,0.08537,-0.0350,0.9865,0.0046 -7.500,-0.2705,0.08313,0.08162,-0.0387,0.9800,0.0046 -7.250,-0.2538,0.07900,0.07748,-0.0441,0.9726,0.0054 -7.000,-0.2314,0.07464,0.07311,-0.0508,0.9678,0.0049 -6.750,-0.2037,0.06771,0.06615,-0.0610,0.9596,0.0034 -6.500,-0.1757,0.06283,0.06122,-0.0689,0.9507,0.0032 -6.250,-0.1503,0.05807,0.05639,-0.0756,0.9375,0.0031 -6.000,-0.1301,0.05388,0.05212,-0.0800,0.9224,0.0030 -5.000,-0.0932,0.01412,0.01028,-0.0863,0.8554,0.0029 -4.750,-0.0721,0.01246,0.00822,-0.0849,0.8407,0.0031 -4.500,-0.0493,0.01149,0.00694,-0.0838,0.8228,0.0033 -4.250,-0.0262,0.01083,0.00600,-0.0826,0.8010,0.0035 -4.000,-0.0030,0.01022,0.00513,-0.0815,0.7765,0.0036 -3.750,0.0199,0.00953,0.00418,-0.0803,0.7523,0.0040 -3.500,0.0439,0.00933,0.00381,-0.0795,0.7255,0.0044 -3.250,0.0671,0.00914,0.00342,-0.0784,0.6905,0.0049 -3.000,0.0913,0.00886,0.00295,-0.0774,0.6657,0.0053 -2.750,0.1161,0.00866,0.00260,-0.0767,0.6466,0.0058 -2.500,0.1406,0.00836,0.00212,-0.0758,0.6283,0.0070 -2.250,0.1656,0.00823,0.00189,-0.0751,0.6089,0.0086 -2.000,0.1902,0.00817,0.00169,-0.0744,0.5824,0.0104 -1.750,0.2148,0.00808,0.00150,-0.0736,0.5579,0.0168 -1.500,0.2391,0.00806,0.00137,-0.0728,0.5262,0.0283 -1.250,0.2627,0.00817,0.00129,-0.0719,0.4808,0.0345 -1.000,0.2864,0.00828,0.00124,-0.0711,0.4418,0.0419 -0.750,0.3110,0.00829,0.00122,-0.0704,0.4182,0.0627 -0.500,0.3365,0.00834,0.00123,-0.0699,0.4013,0.0769 -0.250,0.3622,0.00840,0.00121,-0.0694,0.3876,0.0814 0.000,0.3882,0.00844,0.00121,-0.0690,0.3767,0.0864 0.250,0.4141,0.00849,0.00120,-0.0686,0.3669,0.0898 0.500,0.4402,0.00855,0.00120,-0.0682,0.3579,0.0920 0.750,0.4662,0.00857,0.00120,-0.0678,0.3508,0.0960 1.000,0.4921,0.00861,0.00121,-0.0674,0.3436,0.0991 1.250,0.5182,0.00865,0.00123,-0.0670,0.3374,0.1021 1.500,0.5441,0.00870,0.00126,-0.0667,0.3306,0.1051 1.750,0.5700,0.00875,0.00129,-0.0663,0.3241,0.1090 2.000,0.5958,0.00880,0.00133,-0.0659,0.3170,0.1128 2.250,0.6215,0.00886,0.00138,-0.0654,0.3107,0.1171 2.750,0.6732,0.00894,0.00150,-0.0647,0.3008,0.1348 3.000,0.6984,0.00894,0.00160,-0.0642,0.2963,0.1809 3.250,0.7222,0.00876,0.00175,-0.0635,0.2916,0.3402 3.750,0.8687,0.00871,0.00255,-0.0861,0.1700,1.0000 4.000,0.8922,0.00899,0.00276,-0.0853,0.1555,1.0000 4.250,0.9157,0.00927,0.00297,-0.0845,0.1408,1.0000 4.500,0.9311,0.01038,0.00358,-0.0825,0.0428,1.0000 4.750,0.9528,0.01085,0.00397,-0.0813,0.0115,1.0000 5.000,0.9767,0.01108,0.00424,-0.0806,0.0093,1.0000 5.250,0.9997,0.01140,0.00459,-0.0797,0.0068,1.0000 5.500,1.0230,0.01168,0.00491,-0.0789,0.0059,1.0000 5.750,1.0459,0.01200,0.00525,-0.0780,0.0050,1.0000 6.000,1.0673,0.01247,0.00578,-0.0768,0.0041,1.0000 6.250,1.0902,0.01275,0.00609,-0.0759,0.0036,1.0000 6.500,1.1116,0.01319,0.00658,-0.0748,0.0033,1.0000 6.750,1.1332,0.01358,0.00700,-0.0737,0.0028,1.0000 7.000,1.1526,0.01420,0.00769,-0.0722,0.0026,1.0000 7.250,1.1706,0.01492,0.00850,-0.0705,0.0024,1.0000 7.500,1.1888,0.01559,0.00930,-0.0688,0.0022,1.0000 7.750,1.2051,0.01638,0.01018,-0.0668,0.0022,1.0000 8.000,1.2217,0.01710,0.01099,-0.0649,0.0020,1.0000 8.250,1.2384,0.01776,0.01172,-0.0630,0.0018,1.0000 8.500,1.2490,0.01888,0.01296,-0.0601,0.0017,1.0000 8.750,1.2698,0.01914,0.01323,-0.0592,0.0015,1.0000 9.000,1.2826,0.01999,0.01415,-0.0568,0.0015,1.0000 9.250,1.2910,0.02112,0.01538,-0.0537,0.0014,1.0000 9.500,1.2902,0.02279,0.01720,-0.0490,0.0013,1.0000 9.750,1.2939,0.02385,0.01837,-0.0450,0.0013,1.0000 10.000,1.2941,0.02537,0.02001,-0.0408,0.0013,1.0000 10.250,1.2955,0.02711,0.02187,-0.0370,0.0013,1.0000 10.500,1.2980,0.02971,0.02466,-0.0335,0.0011,1.0000 10.750,1.3051,0.03354,0.02874,-0.0305,0.0009,1.0000 11.000,1.3082,0.03654,0.03195,-0.0275,0.0009,1.0000 11.250,1.3069,0.03948,0.03510,-0.0243,0.0009,1.0000 11.500,1.3011,0.04246,0.03834,-0.0210,0.0008,1.0000 11.750,1.2927,0.04544,0.04153,-0.0181,0.0009,1.0000 12.000,1.2832,0.04848,0.04475,-0.0157,0.0009,1.0000 12.250,1.2684,0.05231,0.04879,-0.0137,0.0009,1.0000 12.500,1.2532,0.05635,0.05302,-0.0126,0.0009,1.0000 12.750,1.2391,0.06049,0.05733,-0.0123,0.0009,1.0000 13.000,1.2229,0.06523,0.06224,-0.0129,0.0009,1.0000 13.250,1.2045,0.07076,0.06794,-0.0143,0.0009,1.0000 13.500,1.1896,0.07602,0.07333,-0.0163,0.0009,1.0000 13.750,1.1736,0.08191,0.07937,-0.0189,0.0009,1.0000 14.000,1.1548,0.08881,0.08641,-0.0224,0.0009,1.0000