Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe255-il-50000-n5 Airfoil,goe255-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,15.1863 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe255-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.3668,0.11081,0.10449,-0.0596,1.0000,0.0592 -11.750,-0.3973,0.10472,0.09854,-0.0598,1.0000,0.0592 -11.500,-0.4401,0.09668,0.09062,-0.0613,0.9997,0.0585 -11.250,-0.4945,0.08060,0.07432,-0.0731,0.9922,0.0569 -11.000,-0.5206,0.07078,0.06418,-0.0823,0.9827,0.0568 -10.750,-0.5307,0.06415,0.05725,-0.0893,0.9722,0.0576 -10.500,-0.5372,0.05921,0.05201,-0.0941,0.9601,0.0590 -10.250,-0.5401,0.05527,0.04771,-0.0966,0.9474,0.0611 -10.000,-0.5341,0.05221,0.04440,-0.0979,0.9356,0.0640 -9.750,-0.5198,0.05009,0.04223,-0.0991,0.9258,0.0679 -9.500,-0.5051,0.04732,0.03909,-0.1004,0.9172,0.0732 -9.250,-0.4953,0.04556,0.03734,-0.0999,0.9066,0.0783 -9.000,-0.4772,0.04330,0.03481,-0.1010,0.8994,0.0875 -8.750,-0.4650,0.04178,0.03332,-0.1005,0.8899,0.0965 -8.500,-0.4493,0.04025,0.03175,-0.1006,0.8816,0.1089 -8.250,-0.4292,0.03881,0.03019,-0.1012,0.8742,0.1260 -8.000,-0.4123,0.03783,0.02915,-0.1010,0.8657,0.1440 -7.750,-0.3883,0.03694,0.02821,-0.1017,0.8591,0.1650 -7.500,-0.3687,0.03613,0.02727,-0.1014,0.8512,0.1846 -7.250,-0.3437,0.03516,0.02613,-0.1018,0.8447,0.2054 -7.000,-0.3177,0.03447,0.02543,-0.1020,0.8386,0.2240 -6.750,-0.2956,0.03402,0.02497,-0.1014,0.8309,0.2417 -6.500,-0.2632,0.03353,0.02443,-0.1023,0.8265,0.2612 -6.250,-0.2446,0.03350,0.02436,-0.1010,0.8176,0.2770 -6.000,-0.2140,0.03329,0.02403,-0.1014,0.8122,0.2956 -5.750,-0.1892,0.03326,0.02386,-0.1011,0.8053,0.3132 -5.500,-0.1644,0.03323,0.02364,-0.1008,0.7982,0.3320 -5.250,-0.1315,0.03321,0.02349,-0.1014,0.7939,0.3513 -5.000,-0.1147,0.03347,0.02364,-0.0998,0.7850,0.3673 -4.750,-0.0862,0.03336,0.02336,-0.1000,0.7798,0.3847 -4.500,-0.0529,0.03306,0.02287,-0.1009,0.7763,0.4021 -4.250,-0.0399,0.03333,0.02302,-0.0990,0.7667,0.4152 -4.000,-0.0097,0.03310,0.02261,-0.0995,0.7621,0.4310 -3.750,0.0143,0.03312,0.02250,-0.0990,0.7562,0.4449 -3.500,0.0336,0.03332,0.02265,-0.0979,0.7489,0.4563 -3.250,0.0641,0.03315,0.02235,-0.0983,0.7450,0.4703 -3.000,0.0847,0.03338,0.02243,-0.0977,0.7389,0.4828 -2.750,0.1027,0.03374,0.02275,-0.0965,0.7324,0.4936 -2.500,0.1311,0.03373,0.02264,-0.0967,0.7287,0.5059 -2.250,0.1636,0.03359,0.02235,-0.0975,0.7261,0.5189 -2.000,0.1672,0.03460,0.02337,-0.0946,0.7168,0.5275 -1.750,0.1941,0.03470,0.02339,-0.0947,0.7128,0.5393 -1.500,0.2256,0.03466,0.02323,-0.0954,0.7100,0.5528 -1.250,0.2289,0.03586,0.02445,-0.0927,0.7020,0.5624 -1.000,0.2501,0.03632,0.02488,-0.0921,0.6978,0.5748 -0.750,0.2776,0.03652,0.02502,-0.0924,0.6950,0.5884 -0.250,0.3001,0.03843,0.02694,-0.0893,0.6834,0.6085 0.000,0.3256,0.03877,0.02723,-0.0894,0.6799,0.6203 0.250,0.3560,0.03889,0.02732,-0.0900,0.6776,0.6325 0.750,0.3711,0.04136,0.02987,-0.0865,0.6648,0.6553 1.000,0.4045,0.04106,0.02959,-0.0870,0.6617,0.6727 1.500,0.4312,0.04266,0.03137,-0.0841,0.6479,0.7121 1.750,0.4667,0.04182,0.03065,-0.0841,0.6450,0.7493 2.250,0.5035,0.04240,0.03161,-0.0817,0.6300,1.0000 2.500,0.5081,0.04405,0.03315,-0.0803,0.6195,1.0000 2.750,0.5421,0.04394,0.03286,-0.0812,0.6153,1.0000 3.000,0.5784,0.04365,0.03242,-0.0822,0.6124,1.0000 3.250,0.5731,0.04612,0.03486,-0.0800,0.6013,1.0000 3.500,0.6087,0.04580,0.03443,-0.0807,0.5982,1.0000 3.750,0.6069,0.04803,0.03664,-0.0787,0.5872,1.0000 4.000,0.6399,0.04781,0.03635,-0.0791,0.5834,1.0000 4.500,0.6728,0.04968,0.03816,-0.0776,0.5683,1.0000 4.750,0.7083,0.04914,0.03757,-0.0779,0.5653,1.0000 5.000,0.7074,0.05133,0.03978,-0.0761,0.5527,1.0000 5.250,0.7371,0.05116,0.03958,-0.0759,0.5481,1.0000 5.500,0.7427,0.05287,0.04131,-0.0745,0.5365,1.0000 5.750,0.7782,0.05215,0.04057,-0.0746,0.5336,1.0000 6.000,0.7764,0.05458,0.04304,-0.0729,0.5199,1.0000 6.250,0.8111,0.05385,0.04231,-0.0729,0.5170,1.0000 6.500,0.8089,0.05639,0.04489,-0.0712,0.5029,1.0000 6.750,0.8436,0.05555,0.04405,-0.0711,0.5001,1.0000 7.000,0.8391,0.05841,0.04695,-0.0696,0.4857,1.0000 7.250,0.8732,0.05761,0.04617,-0.0693,0.4831,1.0000 7.750,0.8568,0.06476,0.05341,-0.0668,0.4553,1.0000 8.000,0.8860,0.06438,0.05306,-0.0664,0.4521,1.0000 8.250,0.8754,0.06848,0.05721,-0.0655,0.4389,1.0000 8.500,0.9038,0.06820,0.05698,-0.0651,0.4362,1.0000 8.750,0.8888,0.07309,0.06192,-0.0644,0.4236,1.0000 9.000,0.9173,0.07271,0.06160,-0.0640,0.4210,1.0000 9.250,0.9027,0.07757,0.06651,-0.0634,0.4088,1.0000 9.500,0.9316,0.07694,0.06594,-0.0628,0.4056,1.0000 9.750,0.9217,0.08112,0.07019,-0.0624,0.3940,1.0000 10.250,0.9421,0.08442,0.07361,-0.0613,0.3795,1.0000 10.500,0.9742,0.08310,0.07237,-0.0605,0.3769,1.0000 11.000,0.9859,0.08782,0.07725,-0.0597,0.3626,1.0000 11.500,0.9936,0.09327,0.08287,-0.0592,0.3482,1.0000 12.000,0.9998,0.09903,0.08880,-0.0589,0.3333,1.0000 12.250,1.0307,0.09762,0.08751,-0.0579,0.3310,1.0000 12.750,1.0291,0.10471,0.09479,-0.0580,0.3153,1.0000