Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe565-il-500000 Airfoil,goe565-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,98.7322 Max Cl/Cd alpha,2.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe565-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4422,0.08955,0.08721,-0.0311,1.0000,0.0269 -9.000,-0.4435,0.08604,0.08373,-0.0322,1.0000,0.0277 -8.750,-0.7004,0.03033,0.02709,-0.0550,1.0000,0.0168 -8.500,-0.6998,0.02577,0.02197,-0.0533,1.0000,0.0174 -8.250,-0.6722,0.02312,0.01886,-0.0551,0.9979,0.0185 -8.000,-0.6448,0.02042,0.01574,-0.0567,0.9957,0.0198 -7.750,-0.6114,0.02011,0.01540,-0.0583,0.9941,0.0207 -7.500,-0.5815,0.01946,0.01463,-0.0591,0.9917,0.0220 -7.250,-0.5511,0.01836,0.01327,-0.0601,0.9892,0.0235 -7.000,-0.5206,0.01687,0.01154,-0.0612,0.9869,0.0252 -6.750,-0.4854,0.01706,0.01177,-0.0629,0.9851,0.0269 -6.500,-0.4502,0.01688,0.01150,-0.0646,0.9837,0.0292 -6.250,-0.4216,0.01591,0.01033,-0.0650,0.9808,0.0315 -6.000,-0.3911,0.01557,0.01001,-0.0658,0.9776,0.0336 -5.750,-0.3572,0.01551,0.00990,-0.0672,0.9751,0.0363 -5.500,-0.3217,0.01548,0.00976,-0.0687,0.9732,0.0386 -5.250,-0.2893,0.01398,0.00816,-0.0701,0.9717,0.0417 -5.000,-0.2533,0.01368,0.00783,-0.0720,0.9705,0.0445 -4.750,-0.2256,0.01333,0.00743,-0.0719,0.9659,0.0469 -4.500,-0.1919,0.01308,0.00711,-0.0731,0.9628,0.0489 -4.250,-0.1570,0.01205,0.00599,-0.0747,0.9605,0.0512 -4.000,-0.1194,0.01133,0.00527,-0.0768,0.9587,0.0543 -3.750,-0.0816,0.01082,0.00474,-0.0788,0.9569,0.0567 -3.500,-0.0523,0.01043,0.00432,-0.0790,0.9514,0.0586 -3.250,-0.0209,0.01010,0.00395,-0.0796,0.9468,0.0608 -3.000,0.0122,0.00971,0.00353,-0.0806,0.9436,0.0625 -2.750,0.0415,0.00929,0.00310,-0.0807,0.9388,0.0662 -2.500,0.0690,0.00903,0.00285,-0.0805,0.9323,0.0701 -2.000,0.1259,0.00854,0.00238,-0.0802,0.9179,0.0861 -1.750,0.1534,0.00820,0.00213,-0.0798,0.9087,0.1175 -1.500,0.1783,0.00757,0.00194,-0.0792,0.8982,0.2485 -1.250,0.2035,0.00731,0.00185,-0.0785,0.8874,0.3134 -1.000,0.2298,0.00706,0.00176,-0.0781,0.8779,0.3712 -0.750,0.2551,0.00669,0.00170,-0.0775,0.8679,0.4748 -0.500,0.2785,0.00634,0.00171,-0.0764,0.8561,0.5943 -0.250,0.3024,0.00607,0.00169,-0.0753,0.8445,0.6838 0.000,0.3245,0.00570,0.00167,-0.0738,0.8330,0.7819 0.250,0.3873,0.00537,0.00166,-0.0808,0.8239,0.9792 0.500,0.4311,0.00539,0.00162,-0.0841,0.8103,1.0000 0.750,0.4554,0.00545,0.00158,-0.0832,0.7929,1.0000 1.000,0.4797,0.00552,0.00157,-0.0822,0.7748,1.0000 1.250,0.5043,0.00561,0.00158,-0.0813,0.7581,1.0000 1.500,0.5286,0.00572,0.00160,-0.0803,0.7397,1.0000 1.750,0.5526,0.00585,0.00163,-0.0793,0.7198,1.0000 2.000,0.5768,0.00597,0.00168,-0.0784,0.6995,1.0000 2.250,0.6004,0.00612,0.00175,-0.0773,0.6761,1.0000 2.500,0.6230,0.00631,0.00180,-0.0760,0.6384,1.0000 2.750,0.6434,0.00662,0.00187,-0.0743,0.5826,1.0000 3.000,0.6641,0.00699,0.00200,-0.0728,0.5332,1.0000 3.250,0.6861,0.00732,0.00216,-0.0716,0.4946,1.0000 3.500,0.7084,0.00766,0.00233,-0.0704,0.4548,1.0000 3.750,0.7310,0.00800,0.00251,-0.0694,0.4144,1.0000 4.000,0.7534,0.00837,0.00270,-0.0683,0.3731,1.0000 4.250,0.7755,0.00879,0.00294,-0.0672,0.3318,1.0000 4.500,0.7975,0.00924,0.00319,-0.0661,0.2875,1.0000 4.750,0.8198,0.00968,0.00345,-0.0652,0.2459,1.0000 5.000,0.8418,0.01017,0.00374,-0.0642,0.2055,1.0000 5.250,0.8642,0.01062,0.00406,-0.0632,0.1795,1.0000 5.500,0.8873,0.01102,0.00438,-0.0624,0.1597,1.0000 5.750,0.9101,0.01145,0.00470,-0.0615,0.1345,1.0000 6.000,0.9283,0.01236,0.00522,-0.0599,0.0658,1.0000 6.250,0.9489,0.01304,0.00577,-0.0587,0.0465,1.0000 6.500,0.9713,0.01353,0.00627,-0.0577,0.0419,1.0000 6.750,0.9917,0.01424,0.00700,-0.0563,0.0372,1.0000 7.000,1.0141,0.01469,0.00752,-0.0553,0.0354,1.0000 7.250,1.0353,0.01525,0.00815,-0.0542,0.0330,1.0000 7.500,1.0544,0.01602,0.00895,-0.0527,0.0304,1.0000 7.750,1.0701,0.01712,0.01013,-0.0507,0.0282,1.0000 8.000,1.0912,0.01766,0.01074,-0.0496,0.0269,1.0000 8.250,1.1110,0.01831,0.01144,-0.0482,0.0252,1.0000 8.500,1.1299,0.01901,0.01218,-0.0469,0.0236,1.0000 8.750,1.1413,0.02060,0.01382,-0.0445,0.0219,1.0000 9.000,1.1601,0.02134,0.01465,-0.0430,0.0210,1.0000 9.250,1.1786,0.02208,0.01548,-0.0416,0.0201,1.0000 9.500,1.1959,0.02294,0.01642,-0.0400,0.0192,1.0000 9.750,1.2127,0.02374,0.01730,-0.0384,0.0183,1.0000 10.000,1.2283,0.02456,0.01815,-0.0368,0.0175,1.0000 10.250,1.2387,0.02658,0.02022,-0.0346,0.0165,1.0000 10.500,1.2514,0.02759,0.02138,-0.0324,0.0160,1.0000 10.750,1.2634,0.02864,0.02256,-0.0302,0.0156,1.0000 11.000,1.2742,0.02977,0.02383,-0.0279,0.0150,1.0000 11.250,1.2837,0.03105,0.02524,-0.0256,0.0145,1.0000 11.500,1.2918,0.03245,0.02678,-0.0233,0.0141,1.0000 11.750,1.2983,0.03383,0.02828,-0.0210,0.0137,1.0000 12.000,1.3040,0.03507,0.02962,-0.0188,0.0134,1.0000 12.250,1.3081,0.03670,0.03135,-0.0166,0.0131,1.0000 12.500,1.3105,0.03861,0.03337,-0.0146,0.0129,1.0000 12.750,1.3076,0.04144,0.03636,-0.0126,0.0126,1.0000 13.250,1.2864,0.04857,0.04398,-0.0090,0.0122,1.0000 13.500,1.2778,0.05171,0.04732,-0.0081,0.0121,1.0000 13.750,1.2686,0.05508,0.05090,-0.0078,0.0120,1.0000 14.000,1.2549,0.05944,0.05548,-0.0083,0.0118,1.0000 14.250,1.2387,0.06458,0.06082,-0.0096,0.0118,1.0000 14.500,1.2217,0.07026,0.06671,-0.0118,0.0117,1.0000 14.750,1.1996,0.07737,0.07401,-0.0151,0.0119,1.0000 15.000,1.1818,0.08435,0.08118,-0.0192,0.0117,1.0000 15.250,1.1598,0.09278,0.08978,-0.0244,0.0118,1.0000 15.500,1.1327,0.10293,0.10010,-0.0307,0.0120,1.0000 15.750,1.1084,0.11319,0.11051,-0.0372,0.0121,1.0000 16.000,1.0797,0.12510,0.12255,-0.0447,0.0123,1.0000