Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe492-il-50000-n5 Airfoil,goe492-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,39.0221 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe492-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.4111,0.10993,0.10302,-0.0308,1.0000,0.0889 -8.500,-0.4206,0.10879,0.10202,-0.0327,1.0000,0.0898 -8.250,-0.4274,0.10698,0.10034,-0.0336,1.0000,0.0901 -8.000,-0.4040,0.10016,0.09347,-0.0305,1.0000,0.0942 -7.750,-0.4040,0.09748,0.09087,-0.0301,1.0000,0.0957 -7.500,-0.4069,0.09499,0.08847,-0.0297,1.0000,0.0975 -7.250,-0.4099,0.09243,0.08602,-0.0297,1.0000,0.0988 -6.750,-0.4082,0.08271,0.07640,-0.0394,1.0000,0.0492 -6.500,-0.4051,0.07945,0.07318,-0.0368,1.0000,0.0469 -6.250,-0.4018,0.07587,0.06965,-0.0378,1.0000,0.0452 -6.000,-0.3967,0.07197,0.06577,-0.0397,1.0000,0.0435 -5.500,-0.3685,0.05999,0.05345,-0.0509,1.0000,0.0383 -5.250,-0.3557,0.05571,0.04905,-0.0524,1.0000,0.0381 -5.000,-0.3379,0.05091,0.04395,-0.0551,1.0000,0.0381 -4.750,-0.3252,0.04829,0.04136,-0.0550,1.0000,0.0413 -4.500,-0.3035,0.04422,0.03695,-0.0572,1.0000,0.0436 -4.250,-0.2777,0.03968,0.03182,-0.0596,1.0000,0.0446 -4.000,-0.2502,0.03549,0.02696,-0.0614,1.0000,0.0458 -3.750,-0.2205,0.03196,0.02248,-0.0626,1.0000,0.0494 -3.500,-0.1967,0.02963,0.01993,-0.0629,1.0000,0.0567 -3.250,-0.1679,0.02713,0.01662,-0.0629,1.0000,0.0624 -3.000,-0.1429,0.02554,0.01473,-0.0628,1.0000,0.0771 -2.750,-0.1172,0.02402,0.01291,-0.0624,1.0000,0.0885 -2.500,-0.0930,0.02299,0.01163,-0.0619,1.0000,0.1055 -2.250,-0.0668,0.02212,0.01050,-0.0616,1.0000,0.1158 -2.000,-0.0412,0.02144,0.00966,-0.0613,1.0000,0.1300 -1.750,-0.0159,0.02084,0.00925,-0.0614,1.0000,0.1658 -1.500,0.0091,0.02045,0.00906,-0.0613,1.0000,0.2629 -1.250,0.0374,0.02005,0.00879,-0.0620,0.9978,0.3597 -1.000,0.0667,0.01879,0.00886,-0.0625,0.9927,0.6301 -0.750,0.1045,0.01836,0.00852,-0.0646,0.9829,1.0000 -0.500,0.1422,0.01873,0.00849,-0.0671,0.9750,1.0000 -0.250,0.1804,0.01910,0.00854,-0.0696,0.9673,1.0000 0.000,0.2152,0.01941,0.00861,-0.0715,0.9578,1.0000 0.250,0.2501,0.01973,0.00871,-0.0734,0.9486,1.0000 0.500,0.2892,0.02007,0.00890,-0.0760,0.9408,1.0000 0.750,0.3218,0.02036,0.00908,-0.0774,0.9302,1.0000 1.000,0.3552,0.02064,0.00931,-0.0789,0.9201,1.0000 1.250,0.3910,0.02092,0.00955,-0.0807,0.9107,1.0000 1.500,0.4268,0.02117,0.00982,-0.0825,0.9013,1.0000 1.750,0.4582,0.02144,0.01015,-0.0835,0.8901,1.0000 2.000,0.4909,0.02169,0.01047,-0.0846,0.8795,1.0000 2.250,0.5271,0.02190,0.01080,-0.0863,0.8704,1.0000 2.500,0.5603,0.02212,0.01121,-0.0874,0.8602,1.0000 3.000,0.6190,0.02266,0.01213,-0.0881,0.8370,1.0000 3.250,0.6492,0.02292,0.01270,-0.0885,0.8259,1.0000 3.500,0.6816,0.02312,0.01321,-0.0892,0.8156,1.0000 3.750,0.7127,0.02335,0.01379,-0.0896,0.8047,1.0000 4.000,0.7410,0.02360,0.01444,-0.0894,0.7915,1.0000 4.250,0.7762,0.02251,0.01391,-0.0876,0.7583,1.0000 4.500,0.7941,0.02035,0.01013,-0.0760,0.4103,1.0000 4.750,0.7879,0.02471,0.01206,-0.0717,0.0795,1.0000 5.000,0.8033,0.02666,0.01388,-0.0697,0.0589,1.0000 5.250,0.8194,0.02832,0.01570,-0.0678,0.0479,1.0000 5.500,0.8353,0.03016,0.01775,-0.0657,0.0438,1.0000 5.750,0.8565,0.03189,0.01981,-0.0641,0.0397,1.0000 6.000,0.8834,0.03411,0.02209,-0.0634,0.0348,1.0000 6.250,0.9191,0.03656,0.02485,-0.0632,0.0327,1.0000 6.500,0.9525,0.03953,0.02816,-0.0629,0.0317,1.0000 6.750,0.9796,0.04264,0.03169,-0.0620,0.0306,1.0000 7.000,1.0010,0.04571,0.03513,-0.0608,0.0289,1.0000 7.250,1.0189,0.04935,0.03897,-0.0599,0.0273,1.0000 7.500,1.0333,0.05335,0.04333,-0.0583,0.0268,1.0000 8.000,1.0548,0.06041,0.05155,-0.0539,0.0274,1.0000 8.250,1.0576,0.06411,0.05587,-0.0509,0.0282,1.0000 8.500,1.0570,0.06817,0.06040,-0.0483,0.0290,1.0000 8.750,1.0519,0.07231,0.06493,-0.0460,0.0297,1.0000 9.000,1.0438,0.07638,0.06930,-0.0439,0.0304,1.0000 9.250,1.0317,0.08030,0.07345,-0.0419,0.0309,1.0000 9.500,1.0162,0.08414,0.07746,-0.0402,0.0313,1.0000 9.750,0.9998,0.08828,0.08175,-0.0396,0.0317,1.0000 10.000,0.9830,0.09294,0.08652,-0.0403,0.0320,1.0000 10.250,0.9667,0.09818,0.09185,-0.0423,0.0323,1.0000