Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe777-il-100000 Airfoil,goe777-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,15.4727 Max Cl/Cd alpha,2 Url,http://airfoiltools.com/polar/csv?polar=xf-goe777-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.1795,0.10894,0.10339,-0.0604,0.7063,0.1886 -10.750,-0.4347,0.06315,0.05675,-0.0895,0.7158,0.1087 -10.500,-0.4358,0.05959,0.05300,-0.0890,0.7125,0.1082 -10.250,-0.4423,0.05607,0.04925,-0.0881,0.7091,0.1080 -10.000,-0.4477,0.05284,0.04568,-0.0867,0.7056,0.1081 -9.750,-0.4497,0.04993,0.04236,-0.0850,0.7023,0.1083 -9.500,-0.4447,0.04732,0.03936,-0.0834,0.6991,0.1088 -9.250,-0.4238,0.04512,0.03715,-0.0831,0.6956,0.1102 -9.000,-0.4047,0.04368,0.03561,-0.0824,0.6924,0.1123 -8.750,-0.3894,0.04221,0.03395,-0.0815,0.6890,0.1147 -8.500,-0.3759,0.04067,0.03209,-0.0802,0.6857,0.1170 -8.250,-0.3622,0.03937,0.03032,-0.0787,0.6826,0.1192 -8.000,-0.3393,0.03782,0.02880,-0.0785,0.6796,0.1219 -7.750,-0.3162,0.03697,0.02792,-0.0781,0.6768,0.1258 -7.500,-0.2963,0.03612,0.02672,-0.0769,0.6740,0.1300 -7.250,-0.2725,0.03497,0.02550,-0.0764,0.6713,0.1340 -7.000,-0.2492,0.03445,0.02495,-0.0759,0.6685,0.1390 -6.750,-0.2288,0.03416,0.02447,-0.0753,0.6653,0.1441 -6.500,-0.2049,0.03358,0.02411,-0.0754,0.6624,0.1495 -6.250,-0.1830,0.03339,0.02383,-0.0748,0.6591,0.1558 -6.000,-0.1590,0.03285,0.02337,-0.0744,0.6558,0.1621 -5.750,-0.1347,0.03255,0.02303,-0.0738,0.6529,0.1697 -5.500,-0.1096,0.03209,0.02261,-0.0732,0.6504,0.1773 -5.250,-0.0849,0.03194,0.02240,-0.0725,0.6479,0.1863 -5.000,-0.0711,0.03236,0.02306,-0.0716,0.6428,0.1935 -4.750,-0.0542,0.03263,0.02339,-0.0705,0.6373,0.2030 -4.500,-0.0323,0.03228,0.02317,-0.0694,0.6328,0.2151 -4.250,-0.0068,0.03167,0.02264,-0.0683,0.6294,0.2332 -4.000,0.0176,0.03103,0.02220,-0.0670,0.6266,0.2664 -3.750,0.0175,0.03204,0.02369,-0.0647,0.6202,0.3133 -3.500,0.0200,0.03223,0.02458,-0.0618,0.6147,0.4220 -3.250,0.0343,0.03220,0.02512,-0.0589,0.6107,0.5386 -3.000,0.0597,0.03213,0.02510,-0.0569,0.6077,0.6068 -2.750,0.0898,0.03196,0.02488,-0.0552,0.6054,0.6527 -2.500,0.0693,0.03524,0.02840,-0.0521,0.5946,0.6699 -2.250,0.0895,0.03558,0.02877,-0.0500,0.5897,0.7017 -2.000,0.1196,0.03525,0.02836,-0.0483,0.5868,0.7346 -1.750,0.1534,0.03478,0.02784,-0.0466,0.5847,0.7646 -1.500,0.1159,0.03908,0.03241,-0.0426,0.5704,0.7777 -1.250,0.1431,0.03884,0.03214,-0.0400,0.5670,0.8092 -1.000,0.1777,0.03824,0.03147,-0.0378,0.5649,0.8392 -0.750,0.1364,0.04254,0.03598,-0.0335,0.5490,0.8561 -0.500,0.1764,0.04195,0.03530,-0.0324,0.5463,0.8854 -0.250,0.2269,0.04120,0.03440,-0.0328,0.5444,0.9121 0.000,0.2617,0.04289,0.03605,-0.0350,0.5373,0.9328 0.250,0.3754,0.04061,0.03341,-0.0436,0.5394,0.9440 0.500,0.3808,0.04436,0.03728,-0.0461,0.5248,0.9611 0.750,0.4066,0.04727,0.04020,-0.0504,0.5141,0.9754 1.000,0.5035,0.04391,0.03654,-0.0565,0.5172,0.9787 1.250,0.6037,0.04054,0.03279,-0.0638,0.5202,0.9808 1.500,0.6071,0.04531,0.03780,-0.0679,0.5041,0.9986 1.750,0.6429,0.04417,0.03651,-0.0684,0.5026,1.0000 2.000,0.6678,0.04316,0.03535,-0.0673,0.5013,1.0000 2.250,0.3108,0.06254,0.05515,-0.0387,0.4677,1.0000 2.500,0.3415,0.06260,0.05507,-0.0386,0.4654,1.0000 2.750,0.3783,0.06222,0.05455,-0.0386,0.4638,1.0000 3.000,0.3025,0.07180,0.06426,-0.0373,0.4561,1.0000 3.250,0.2979,0.07517,0.06759,-0.0370,0.4533,1.0000 3.500,0.3068,0.07740,0.06976,-0.0369,0.4507,1.0000 3.750,0.2755,0.08508,0.07754,-0.0381,0.4668,1.0000 4.000,0.2313,0.09327,0.08586,-0.0393,0.4953,1.0000 4.250,0.2391,0.09481,0.08735,-0.0389,0.4893,1.0000 4.500,0.2580,0.09662,0.08909,-0.0391,0.4863,1.0000 4.750,0.2812,0.09864,0.09103,-0.0394,0.4843,1.0000 5.000,0.3097,0.10098,0.09329,-0.0401,0.4828,1.0000 5.250,0.3431,0.10382,0.09605,-0.0411,0.4817,1.0000 5.500,0.3719,0.10718,0.09934,-0.0420,0.4810,1.0000 5.750,0.3035,0.10720,0.09945,-0.0388,0.4713,1.0000 6.000,0.3209,0.10907,0.10127,-0.0389,0.4680,1.0000 6.250,0.3428,0.11117,0.10332,-0.0393,0.4658,1.0000 6.500,0.3694,0.11369,0.10577,-0.0399,0.4643,1.0000 6.750,0.4024,0.11689,0.10892,-0.0409,0.4632,1.0000 7.000,0.3604,0.11792,0.10999,-0.0392,0.4568,1.0000 7.250,0.3714,0.11969,0.11174,-0.0393,0.4520,1.0000