Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca65410-il-500000-n5 Airfoil,naca65410-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,87.5107 Max Cl/Cd alpha,2.5 Url,http://airfoiltools.com/polar/csv?polar=xf-naca65410-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4574,0.08633,0.08402,-0.0422,1.0000,0.0069 -9.500,-0.4645,0.08114,0.07888,-0.0445,1.0000,0.0069 -9.250,-0.4726,0.07614,0.07392,-0.0470,1.0000,0.0069 -9.000,-0.4867,0.07053,0.06836,-0.0502,1.0000,0.0069 -8.750,-0.4994,0.06306,0.06090,-0.0593,0.9911,0.0067 -8.500,-0.4981,0.05329,0.05091,-0.0701,0.9783,0.0067 -8.000,-0.5154,0.02055,0.01579,-0.0794,0.9496,0.0081 -7.750,-0.4873,0.02035,0.01556,-0.0802,0.9424,0.0085 -7.500,-0.4576,0.02039,0.01558,-0.0811,0.9364,0.0089 -7.250,-0.4328,0.01913,0.01408,-0.0812,0.9280,0.0096 -7.000,-0.4085,0.01735,0.01195,-0.0810,0.9203,0.0104 -6.750,-0.3837,0.01604,0.01036,-0.0808,0.9121,0.0110 -6.500,-0.3593,0.01485,0.00898,-0.0805,0.9044,0.0117 -6.250,-0.3334,0.01434,0.00838,-0.0804,0.8967,0.0123 -6.000,-0.3071,0.01407,0.00806,-0.0804,0.8893,0.0132 -5.750,-0.2808,0.01366,0.00754,-0.0803,0.8819,0.0143 -5.500,-0.2550,0.01312,0.00688,-0.0801,0.8744,0.0152 -5.250,-0.2289,0.01263,0.00627,-0.0799,0.8673,0.0159 -5.000,-0.2041,0.01179,0.00535,-0.0796,0.8601,0.0170 -4.750,-0.1777,0.01146,0.00496,-0.0796,0.8531,0.0182 -4.500,-0.1511,0.01116,0.00462,-0.0795,0.8460,0.0195 -4.250,-0.1247,0.01078,0.00416,-0.0794,0.8390,0.0206 -4.000,-0.0979,0.01044,0.00376,-0.0794,0.8324,0.0217 -3.750,-0.0709,0.01019,0.00343,-0.0794,0.8258,0.0227 -3.500,-0.0440,0.00979,0.00296,-0.0794,0.8194,0.0247 -3.250,-0.0169,0.00950,0.00262,-0.0794,0.8126,0.0268 -3.000,0.0106,0.00930,0.00236,-0.0795,0.8063,0.0291 -2.750,0.0383,0.00913,0.00214,-0.0796,0.7999,0.0318 -2.500,0.0659,0.00898,0.00193,-0.0796,0.7942,0.0360 -2.250,0.0937,0.00880,0.00177,-0.0798,0.7878,0.0455 -2.000,0.1212,0.00849,0.00161,-0.0800,0.7816,0.0998 -1.750,0.1481,0.00769,0.00140,-0.0806,0.7756,0.2903 -1.500,0.1742,0.00666,0.00132,-0.0812,0.7696,0.5808 -1.250,0.2012,0.00650,0.00139,-0.0811,0.7642,0.6637 -1.000,0.2289,0.00647,0.00141,-0.0810,0.7580,0.6913 -0.750,0.2565,0.00648,0.00143,-0.0810,0.7524,0.7128 -0.500,0.2845,0.00649,0.00144,-0.0810,0.7467,0.7270 -0.250,0.3126,0.00650,0.00144,-0.0811,0.7408,0.7336 0.000,0.3408,0.00653,0.00144,-0.0812,0.7354,0.7400 0.250,0.3688,0.00655,0.00146,-0.0813,0.7295,0.7463 0.750,0.4249,0.00661,0.00153,-0.0815,0.7182,0.7590 1.000,0.4530,0.00664,0.00157,-0.0816,0.7124,0.7659 1.250,0.4808,0.00668,0.00163,-0.0816,0.7070,0.7721 1.500,0.5087,0.00672,0.00169,-0.0817,0.7000,0.7789 1.750,0.5357,0.00677,0.00174,-0.0815,0.6859,0.7854 2.000,0.5624,0.00685,0.00180,-0.0813,0.6698,0.7927 2.250,0.5893,0.00692,0.00188,-0.0811,0.6565,0.7997 2.500,0.6152,0.00703,0.00195,-0.0807,0.6317,0.8069 2.750,0.6385,0.00730,0.00203,-0.0798,0.5789,0.8141 3.000,0.6586,0.00786,0.00221,-0.0784,0.4828,0.8224 3.250,0.6742,0.00898,0.00268,-0.0766,0.3350,0.8307 3.500,0.6917,0.01005,0.00319,-0.0752,0.2058,0.8397 3.750,0.7093,0.01104,0.00372,-0.0738,0.0939,0.8482 4.000,0.7308,0.01166,0.00411,-0.0729,0.0445,0.8570 4.250,0.7546,0.01198,0.00443,-0.0722,0.0337,0.8665 4.500,0.7783,0.01224,0.00474,-0.0715,0.0298,0.8762 4.750,0.8012,0.01259,0.00513,-0.0707,0.0255,0.8866 5.250,0.8463,0.01321,0.00590,-0.0688,0.0215,0.9101 5.500,0.8676,0.01353,0.00629,-0.0676,0.0198,0.9240 6.250,0.9327,0.01497,0.00792,-0.0647,0.0159,1.0000 6.500,0.9556,0.01553,0.00853,-0.0642,0.0154,1.0000 6.750,0.9778,0.01613,0.00919,-0.0635,0.0148,1.0000 7.000,0.9993,0.01679,0.00992,-0.0627,0.0143,1.0000 7.250,1.0205,0.01747,0.01068,-0.0618,0.0138,1.0000 7.500,1.0414,0.01819,0.01145,-0.0609,0.0133,1.0000 7.750,1.0623,0.01886,0.01217,-0.0601,0.0128,1.0000 8.000,1.0832,0.01951,0.01285,-0.0593,0.0122,1.0000 8.250,1.1012,0.02055,0.01395,-0.0581,0.0116,1.0000 8.500,1.1184,0.02198,0.01552,-0.0568,0.0112,1.0000 8.750,1.1384,0.02292,0.01657,-0.0559,0.0109,1.0000 9.000,1.1582,0.02388,0.01765,-0.0549,0.0106,1.0000 9.250,1.1775,0.02484,0.01873,-0.0539,0.0102,1.0000 9.500,1.1958,0.02581,0.01983,-0.0528,0.0097,1.0000 9.750,1.2125,0.02670,0.02084,-0.0515,0.0093,1.0000 10.000,1.2280,0.02773,0.02199,-0.0501,0.0089,1.0000 10.250,1.2420,0.02874,0.02310,-0.0484,0.0087,1.0000 10.500,1.2548,0.02968,0.02417,-0.0467,0.0084,1.0000 10.750,1.2661,0.03081,0.02540,-0.0449,0.0082,1.0000 11.000,1.2749,0.03222,0.02694,-0.0430,0.0079,1.0000 11.250,1.2784,0.03473,0.02970,-0.0406,0.0076,1.0000 11.500,1.2860,0.03628,0.03146,-0.0388,0.0074,1.0000 11.750,1.2902,0.03832,0.03375,-0.0368,0.0071,1.0000 12.000,1.2914,0.04067,0.03634,-0.0348,0.0068,1.0000 12.250,1.2888,0.04343,0.03935,-0.0328,0.0065,1.0000 12.500,1.2854,0.04619,0.04234,-0.0312,0.0063,1.0000 12.750,1.2771,0.04963,0.04602,-0.0297,0.0061,1.0000 13.000,1.2661,0.05348,0.05011,-0.0287,0.0060,1.0000 13.250,1.2542,0.05760,0.05444,-0.0283,0.0059,1.0000 13.500,1.2386,0.06247,0.05952,-0.0286,0.0058,1.0000 13.750,1.2195,0.06822,0.06549,-0.0298,0.0058,1.0000 14.000,1.1869,0.07678,0.07433,-0.0327,0.0058,1.0000 14.250,1.1356,0.09042,0.08829,-0.0398,0.0059,1.0000