Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m25-il-50000-n5 Airfoil,m25-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,20.5018 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-m25-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.2917,0.12978,0.12414,0.0012,0.7931,0.0310 -9.250,-0.2831,0.12675,0.12110,-0.0004,0.7851,0.0316 -9.000,-0.2759,0.12399,0.11831,-0.0014,0.7784,0.0324 -8.750,-0.2667,0.12112,0.11544,-0.0032,0.7710,0.0333 -8.500,-0.2589,0.11849,0.11279,-0.0046,0.7646,0.0343 -8.250,-0.2496,0.11584,0.11014,-0.0066,0.7577,0.0354 -8.000,-0.2409,0.11345,0.10773,-0.0086,0.7512,0.0365 -7.750,-0.2327,0.11151,0.10579,-0.0110,0.7451,0.0373 -7.500,-0.2226,0.11002,0.10429,-0.0143,0.7386,0.0380 -7.250,-0.2109,0.10888,0.10310,-0.0179,0.7335,0.0384 -7.000,-0.1936,0.10786,0.10201,-0.0232,0.7266,0.0387 -6.750,-0.1762,0.10687,0.10093,-0.0277,0.7210,0.0389 -6.500,-0.1693,0.09963,0.09375,-0.0257,0.7162,0.0396 -6.250,-0.1584,0.09491,0.08903,-0.0259,0.7104,0.0408 -6.000,-0.1455,0.09170,0.08577,-0.0272,0.7057,0.0422 -5.750,-0.1288,0.08882,0.08285,-0.0298,0.7001,0.0440 -5.500,-0.1100,0.08625,0.08022,-0.0328,0.6944,0.0467 -5.250,-0.0833,0.08542,0.07922,-0.0377,0.6899,0.0499 -5.000,-0.0517,0.08451,0.07821,-0.0439,0.6835,0.0510 -4.750,-0.0460,0.07867,0.07241,-0.0422,0.6789,0.0528 -4.500,-0.0293,0.07557,0.06919,-0.0432,0.6750,0.0555 -4.250,-0.0040,0.07324,0.06677,-0.0465,0.6688,0.0594 -4.000,0.0380,0.07390,0.06709,-0.0527,0.6635,0.0628 -3.750,0.0477,0.06882,0.06203,-0.0518,0.6601,0.0647 -3.500,0.0687,0.06592,0.05910,-0.0536,0.6539,0.0706 -3.250,0.1102,0.06614,0.05897,-0.0583,0.6489,0.0759 -3.000,0.1211,0.06148,0.05427,-0.0574,0.6456,0.0790 -2.750,0.1491,0.05965,0.05231,-0.0599,0.6392,0.0855 -2.250,0.2120,0.05761,0.04968,-0.0635,0.6310,0.1022 -2.000,0.2289,0.05381,0.04595,-0.0644,0.6250,0.1066 -1.750,0.2654,0.05405,0.04581,-0.0664,0.6201,0.1167 -1.500,0.2818,0.05030,0.04198,-0.0659,0.6168,0.1219 -1.250,0.3104,0.04928,0.04079,-0.0676,0.6108,0.1338 -1.000,0.3346,0.04766,0.03903,-0.0682,0.6060,0.1508 -0.750,0.3603,0.04617,0.03731,-0.0683,0.6026,0.1672 -0.500,0.3878,0.04562,0.03655,-0.0696,0.5967,0.1889 -0.250,0.4107,0.04405,0.03487,-0.0699,0.5918,0.2104 0.500,0.4810,0.04050,0.03089,-0.0706,0.5777,0.3194 0.750,0.5086,0.03949,0.02967,-0.0706,0.5742,0.3349 1.250,0.5897,0.04146,0.03061,-0.0723,0.5636,0.1006 1.500,0.6177,0.04065,0.02957,-0.0721,0.5600,0.0930 1.750,0.6467,0.03999,0.02857,-0.0714,0.5574,0.0867 2.000,0.6690,0.04082,0.02936,-0.0728,0.5495,0.0843 2.250,0.7001,0.04046,0.02873,-0.0732,0.5458,0.0816 2.500,0.7335,0.03989,0.02783,-0.0735,0.5432,0.0794 2.750,0.7562,0.04121,0.02907,-0.0751,0.5352,0.0783 3.000,0.7855,0.04110,0.02875,-0.0753,0.5315,0.0777 3.250,0.8145,0.04068,0.02815,-0.0750,0.5289,0.0779 3.500,0.8285,0.04255,0.03008,-0.0758,0.5208,0.0799 3.750,0.8507,0.04283,0.03028,-0.0752,0.5170,0.0865 4.000,0.8744,0.04265,0.03003,-0.0742,0.5146,0.0934 4.250,0.8798,0.04537,0.03284,-0.0746,0.5060,0.0961 4.500,0.8991,0.04581,0.03317,-0.0737,0.5023,0.1000 4.750,0.9224,0.04571,0.03299,-0.0725,0.5000,0.1063 5.250,0.9376,0.05033,0.03774,-0.0724,0.4870,0.1208 5.500,0.9616,0.05032,0.03779,-0.0714,0.4850,0.1541 6.000,0.9867,0.05538,0.04387,-0.0752,0.4714,1.0000 6.250,1.0086,0.05592,0.04435,-0.0741,0.4695,1.0000 6.500,0.9758,0.06227,0.05075,-0.0738,0.4586,1.0000 6.750,0.9963,0.06302,0.05149,-0.0729,0.4562,1.0000 7.000,0.9725,0.06824,0.05675,-0.0722,0.4475,1.0000 7.250,0.9831,0.07014,0.05866,-0.0716,0.4441,1.0000 7.500,1.0012,0.07130,0.05986,-0.0709,0.4418,1.0000 7.750,0.9837,0.07609,0.06470,-0.0706,0.4346,1.0000 8.000,0.9915,0.07831,0.06697,-0.0701,0.4305,1.0000 8.250,1.0071,0.07979,0.06853,-0.0695,0.4280,1.0000 8.500,1.0254,0.08109,0.06997,-0.0689,0.4262,1.0000 9.000,1.0099,0.08899,0.07803,-0.0687,0.4151,1.0000 9.250,1.0270,0.09041,0.07960,-0.0682,0.4128,1.0000 9.500,1.0175,0.09474,0.08402,-0.0683,0.4082,1.0000 9.750,1.0157,0.09813,0.08753,-0.0683,0.4035,1.0000 10.000,1.0277,0.10011,0.08967,-0.0679,0.4003,1.0000 10.250,1.0357,0.10173,0.09144,-0.0671,0.3927,1.0000 10.500,1.1352,0.08085,0.07101,-0.0568,0.3371,1.0000 11.000,1.1340,0.08429,0.07472,-0.0553,0.2948,1.0000 11.250,1.1256,0.08847,0.07906,-0.0555,0.2796,1.0000 11.500,1.1137,0.09345,0.08418,-0.0562,0.2619,1.0000 11.750,1.1050,0.09807,0.08903,-0.0569,0.2426,1.0000 12.000,1.1002,0.10214,0.09327,-0.0573,0.1979,1.0000 12.250,1.0992,0.10211,0.09093,-0.0544,0.0448,1.0000 12.500,1.0945,0.10639,0.09526,-0.0549,0.0418,1.0000 12.750,1.0909,0.11053,0.09950,-0.0554,0.0395,1.0000 13.000,1.0881,0.11455,0.10362,-0.0559,0.0379,1.0000 13.250,1.0860,0.11844,0.10760,-0.0564,0.0367,1.0000