Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe795-il-50000-n5 Airfoil,goe795-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,37.7778 Max Cl/Cd alpha,5.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-goe795-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.3681,0.11131,0.10445,-0.0264,1.0000,0.1064 -9.750,-0.3651,0.10498,0.09806,-0.0282,1.0000,0.0722 -9.250,-0.4574,0.10360,0.09641,-0.0293,1.0000,0.0631 -9.000,-0.4504,0.09993,0.09275,-0.0287,1.0000,0.0610 -8.750,-0.4498,0.09628,0.08916,-0.0293,1.0000,0.0593 -8.500,-0.4520,0.09258,0.08553,-0.0303,1.0000,0.0577 -8.250,-0.4572,0.08882,0.08187,-0.0315,1.0000,0.0563 -8.000,-0.4660,0.08499,0.07815,-0.0329,1.0000,0.0550 -7.500,-0.4846,0.07345,0.06665,-0.0409,1.0000,0.0511 -7.250,-0.4839,0.06952,0.06271,-0.0412,1.0000,0.0507 -7.000,-0.4829,0.06550,0.05863,-0.0414,1.0000,0.0504 -6.750,-0.4812,0.06134,0.05438,-0.0415,1.0000,0.0502 -6.500,-0.4781,0.05724,0.05012,-0.0414,1.0000,0.0499 -6.250,-0.4742,0.05290,0.04551,-0.0412,1.0000,0.0502 -6.000,-0.4682,0.04864,0.04084,-0.0406,1.0000,0.0510 -5.750,-0.4593,0.04553,0.03754,-0.0395,1.0000,0.0526 -5.500,-0.4467,0.04377,0.03573,-0.0382,1.0000,0.0552 -5.250,-0.4343,0.04073,0.03227,-0.0370,1.0000,0.0565 -5.000,-0.4204,0.03762,0.02870,-0.0356,1.0000,0.0572 -4.750,-0.4046,0.03477,0.02537,-0.0342,1.0000,0.0583 -4.500,-0.3869,0.03219,0.02229,-0.0327,1.0000,0.0600 -4.250,-0.3673,0.02987,0.01943,-0.0313,1.0000,0.0624 -4.000,-0.3472,0.02804,0.01727,-0.0299,1.0000,0.0653 -3.750,-0.3276,0.02690,0.01600,-0.0286,1.0000,0.0716 -3.500,-0.3076,0.02592,0.01484,-0.0274,1.0000,0.0817 -3.250,-0.2880,0.02520,0.01399,-0.0262,1.0000,0.0968 -3.000,-0.2653,0.02413,0.01270,-0.0252,1.0000,0.1092 -2.750,-0.2415,0.02317,0.01159,-0.0244,1.0000,0.1234 -2.500,-0.2196,0.02257,0.01096,-0.0236,1.0000,0.1476 -2.250,-0.1977,0.02200,0.01038,-0.0227,1.0000,0.1738 -2.000,-0.1766,0.02152,0.00995,-0.0219,1.0000,0.2067 -1.750,-0.1546,0.02100,0.00962,-0.0215,0.9993,0.2653 -1.500,-0.1204,0.02006,0.00938,-0.0235,0.9930,0.3911 -1.250,-0.0576,0.01829,0.00915,-0.0295,0.9939,1.0000 -1.000,-0.0196,0.01859,0.00898,-0.0321,0.9850,1.0000 -0.750,0.0171,0.01888,0.00894,-0.0344,0.9762,1.0000 -0.500,0.0549,0.01920,0.00898,-0.0369,0.9679,1.0000 -0.250,0.0901,0.01946,0.00902,-0.0389,0.9584,1.0000 0.000,0.1243,0.01972,0.00908,-0.0407,0.9488,1.0000 0.250,0.1613,0.02000,0.00919,-0.0429,0.9401,1.0000 0.500,0.1966,0.02025,0.00933,-0.0447,0.9304,1.0000 0.750,0.2296,0.02048,0.00948,-0.0461,0.9198,1.0000 1.000,0.2648,0.02070,0.00962,-0.0478,0.9094,1.0000 1.250,0.3035,0.02083,0.00971,-0.0500,0.8983,1.0000 1.500,0.3442,0.02085,0.00973,-0.0523,0.8861,1.0000 1.750,0.3849,0.02081,0.00972,-0.0546,0.8734,1.0000 2.000,0.4205,0.02082,0.00976,-0.0558,0.8599,1.0000 2.250,0.4532,0.02086,0.00986,-0.0565,0.8466,1.0000 2.500,0.4849,0.02093,0.01003,-0.0569,0.8333,1.0000 2.750,0.5162,0.02100,0.01019,-0.0573,0.8199,1.0000 3.000,0.5474,0.02106,0.01035,-0.0575,0.8062,1.0000 3.250,0.5787,0.02110,0.01052,-0.0577,0.7919,1.0000 3.500,0.6104,0.02112,0.01072,-0.0578,0.7771,1.0000 3.750,0.6369,0.02124,0.01099,-0.0571,0.7593,1.0000 4.000,0.6660,0.02127,0.01117,-0.0566,0.7405,1.0000 4.250,0.6949,0.02119,0.01122,-0.0557,0.7169,1.0000 4.500,0.7213,0.02109,0.01123,-0.0542,0.6879,1.0000 4.750,0.7459,0.02105,0.01134,-0.0524,0.6556,1.0000 5.000,0.7676,0.02110,0.01148,-0.0503,0.6189,1.0000 5.250,0.7877,0.02118,0.01158,-0.0478,0.5744,1.0000 5.500,0.8059,0.02137,0.01168,-0.0450,0.5202,1.0000 5.750,0.8228,0.02178,0.01187,-0.0423,0.4595,1.0000 6.000,0.8378,0.02247,0.01230,-0.0395,0.3972,1.0000 6.250,0.8512,0.02340,0.01306,-0.0369,0.3386,1.0000 6.500,0.8641,0.02448,0.01397,-0.0345,0.2816,1.0000 6.750,0.8752,0.02576,0.01500,-0.0320,0.2187,1.0000 7.000,0.8854,0.02732,0.01620,-0.0296,0.1738,1.0000 7.250,0.8982,0.02895,0.01769,-0.0275,0.1469,1.0000 7.500,0.9131,0.03057,0.01928,-0.0256,0.1300,1.0000 7.750,0.9312,0.03216,0.02094,-0.0241,0.1166,1.0000 8.000,0.9481,0.03369,0.02251,-0.0226,0.1022,1.0000 8.250,0.9654,0.03538,0.02440,-0.0211,0.0889,1.0000 8.500,0.9790,0.03707,0.02624,-0.0193,0.0744,1.0000 8.750,0.9918,0.03902,0.02827,-0.0176,0.0623,1.0000 9.000,1.0047,0.04110,0.03046,-0.0159,0.0531,1.0000 9.250,1.0204,0.04381,0.03353,-0.0143,0.0458,1.0000 9.500,1.0349,0.04668,0.03655,-0.0130,0.0421,1.0000 9.750,1.0455,0.05030,0.04052,-0.0112,0.0394,1.0000 10.000,1.0480,0.05352,0.04426,-0.0087,0.0372,1.0000 10.250,1.0448,0.05657,0.04768,-0.0060,0.0350,1.0000 10.500,1.0393,0.05928,0.05064,-0.0033,0.0333,1.0000 10.750,1.0314,0.06226,0.05383,-0.0010,0.0321,1.0000 11.000,1.0216,0.06553,0.05730,0.0007,0.0314,1.0000 11.250,1.0095,0.06918,0.06115,0.0017,0.0310,1.0000 11.500,0.9941,0.07345,0.06563,0.0019,0.0308,1.0000 11.750,0.9750,0.07848,0.07090,0.0009,0.0309,1.0000 12.000,0.9507,0.08491,0.07757,-0.0018,0.0315,1.0000 12.250,0.9111,0.09578,0.08870,-0.0086,0.0341,1.0000