Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ames02-il-50000-n5 Airfoil,ames02-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,22.8043 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-ames02-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.6867,0.11430,0.10710,0.0227,1.0000,0.0572 -9.250,-0.6828,0.10986,0.10269,0.0214,1.0000,0.0553 -9.000,-0.6925,0.10213,0.09500,0.0147,1.0000,0.0519 -8.750,-0.6905,0.09746,0.09036,0.0125,1.0000,0.0512 -8.500,-0.6922,0.09185,0.08478,0.0084,1.0000,0.0505 -8.250,-0.6978,0.08580,0.07873,0.0035,1.0000,0.0497 -8.000,-0.7026,0.07966,0.07251,-0.0007,1.0000,0.0489 -7.750,-0.7061,0.07361,0.06631,-0.0042,1.0000,0.0484 -7.500,-0.7056,0.06805,0.06052,-0.0067,1.0000,0.0483 -7.250,-0.7004,0.06304,0.05523,-0.0083,1.0000,0.0485 -7.000,-0.6918,0.05823,0.05008,-0.0096,1.0000,0.0489 -6.750,-0.6799,0.05358,0.04500,-0.0104,1.0000,0.0491 -6.500,-0.6648,0.04912,0.04006,-0.0109,1.0000,0.0490 -6.250,-0.6465,0.04512,0.03555,-0.0111,1.0000,0.0492 -6.000,-0.6257,0.04152,0.03143,-0.0111,1.0000,0.0500 -5.750,-0.6029,0.03813,0.02732,-0.0109,1.0000,0.0519 -5.500,-0.5789,0.03597,0.02501,-0.0109,1.0000,0.0544 -5.250,-0.5531,0.03345,0.02204,-0.0106,1.0000,0.0565 -5.000,-0.5266,0.03121,0.01947,-0.0102,1.0000,0.0586 -4.750,-0.5001,0.02949,0.01757,-0.0099,1.0000,0.0628 -4.500,-0.4735,0.02783,0.01579,-0.0095,1.0000,0.0668 -4.250,-0.4465,0.02632,0.01414,-0.0089,1.0000,0.0721 -3.750,-0.3941,0.02382,0.01152,-0.0078,1.0000,0.0880 -3.500,-0.3683,0.02263,0.01039,-0.0074,1.0000,0.1000 -3.250,-0.3420,0.02148,0.00927,-0.0072,1.0000,0.1200 -3.000,-0.3171,0.02010,0.00820,-0.0069,1.0000,0.1596 -2.750,-0.2963,0.01785,0.00723,-0.0066,1.0000,0.3456 -2.500,-0.2833,0.01648,0.00728,-0.0023,1.0000,0.6476 -2.250,-0.2654,0.01611,0.00727,0.0020,1.0000,0.7871 -2.000,-0.2229,0.01604,0.00728,0.0024,1.0000,0.9163 -1.750,-0.1332,0.01609,0.00689,-0.0084,1.0000,0.9964 -1.500,-0.1095,0.01579,0.00642,-0.0087,1.0000,1.0000 -1.250,-0.0904,0.01554,0.00605,-0.0079,1.0000,1.0000 -1.000,-0.0714,0.01537,0.00574,-0.0070,1.0000,1.0000 -0.750,-0.0525,0.01526,0.00552,-0.0060,1.0000,1.0000 -0.500,-0.0336,0.01521,0.00538,-0.0049,1.0000,1.0000 -0.250,-0.0148,0.01521,0.00529,-0.0038,1.0000,1.0000 0.000,0.0041,0.01525,0.00527,-0.0026,1.0000,1.0000 0.250,0.0231,0.01534,0.00530,-0.0015,1.0000,1.0000 0.500,0.0426,0.01546,0.00539,-0.0004,1.0000,1.0000 0.750,0.0625,0.01562,0.00553,0.0005,1.0000,1.0000 1.000,0.0827,0.01581,0.00573,0.0013,1.0000,1.0000 1.250,0.1034,0.01605,0.00598,0.0020,1.0000,1.0000 1.500,0.1365,0.01632,0.00630,0.0003,0.9926,1.0000 1.750,0.2047,0.01648,0.00661,-0.0076,0.9631,1.0000 2.000,0.2587,0.01657,0.00686,-0.0122,0.9275,1.0000 2.250,0.2979,0.01664,0.00705,-0.0133,0.8852,1.0000 2.500,0.3250,0.01669,0.00717,-0.0118,0.8353,1.0000 2.750,0.3480,0.01672,0.00721,-0.0093,0.7759,1.0000 3.000,0.3688,0.01679,0.00717,-0.0061,0.6957,1.0000 3.250,0.3876,0.01710,0.00706,-0.0025,0.5790,1.0000 3.500,0.4064,0.01795,0.00718,0.0002,0.4427,1.0000 3.750,0.4282,0.01909,0.00766,0.0013,0.3378,1.0000 4.000,0.4518,0.02020,0.00833,0.0017,0.2714,1.0000 4.250,0.4764,0.02122,0.00910,0.0020,0.2266,1.0000 4.500,0.5019,0.02225,0.00998,0.0022,0.1942,1.0000 4.750,0.5275,0.02326,0.01090,0.0025,0.1693,1.0000 5.000,0.5531,0.02431,0.01185,0.0029,0.1505,1.0000 5.250,0.5790,0.02539,0.01295,0.0033,0.1346,1.0000 5.500,0.6047,0.02655,0.01415,0.0037,0.1218,1.0000 5.750,0.6303,0.02778,0.01539,0.0040,0.1113,1.0000 6.000,0.6558,0.02908,0.01675,0.0044,0.1022,1.0000 6.250,0.6816,0.03060,0.01851,0.0047,0.0943,1.0000 6.500,0.7068,0.03231,0.02042,0.0051,0.0878,1.0000 6.750,0.7312,0.03394,0.02210,0.0053,0.0826,1.0000 7.000,0.7553,0.03611,0.02468,0.0056,0.0775,1.0000 7.250,0.7780,0.03839,0.02728,0.0058,0.0734,1.0000 7.500,0.7994,0.04102,0.03030,0.0061,0.0699,1.0000 7.750,0.8191,0.04373,0.03334,0.0062,0.0669,1.0000 8.000,0.8347,0.04757,0.03777,0.0063,0.0644,1.0000 8.250,0.8501,0.05079,0.04132,0.0064,0.0625,1.0000 8.500,0.8603,0.05484,0.04579,0.0063,0.0609,1.0000 8.750,0.8597,0.06063,0.05217,0.0056,0.0596,1.0000 9.000,0.8548,0.06639,0.05833,0.0044,0.0588,1.0000 9.250,0.8435,0.07262,0.06485,0.0024,0.0586,1.0000 9.500,0.8249,0.07953,0.07195,-0.0010,0.0590,1.0000 9.750,0.8028,0.08731,0.07977,-0.0063,0.0596,1.0000