Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca64210-il-200000-n5 Airfoil,naca64210-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,54.0493 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca64210-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.5901,0.08787,0.08426,-0.0228,1.0000,0.0159 -10.250,-0.5981,0.08071,0.07716,-0.0273,1.0000,0.0158 -10.000,-0.6122,0.07136,0.06779,-0.0346,1.0000,0.0157 -9.750,-0.6291,0.06478,0.06116,-0.0398,1.0000,0.0155 -9.500,-0.6482,0.05958,0.05586,-0.0427,1.0000,0.0154 -9.250,-0.6665,0.05543,0.05158,-0.0429,1.0000,0.0153 -9.000,-0.6792,0.05047,0.04637,-0.0429,1.0000,0.0154 -8.750,-0.6866,0.04550,0.04106,-0.0423,1.0000,0.0155 -8.500,-0.6885,0.04078,0.03591,-0.0412,1.0000,0.0157 -8.250,-0.6848,0.03663,0.03126,-0.0399,1.0000,0.0159 -8.000,-0.6773,0.03295,0.02721,-0.0387,1.0000,0.0163 -7.750,-0.6637,0.03068,0.02471,-0.0376,1.0000,0.0167 -7.500,-0.6476,0.02915,0.02299,-0.0366,1.0000,0.0174 -7.250,-0.6307,0.02789,0.02156,-0.0355,1.0000,0.0183 -7.000,-0.6138,0.02655,0.02002,-0.0342,1.0000,0.0195 -6.750,-0.5976,0.02481,0.01798,-0.0325,1.0000,0.0203 -6.500,-0.5689,0.02284,0.01567,-0.0333,0.9951,0.0211 -6.250,-0.5362,0.02126,0.01380,-0.0346,0.9886,0.0219 -6.000,-0.5042,0.01955,0.01192,-0.0361,0.9826,0.0235 -5.750,-0.4713,0.01856,0.01088,-0.0377,0.9762,0.0252 -5.500,-0.4397,0.01750,0.00973,-0.0388,0.9684,0.0264 -5.250,-0.4071,0.01653,0.00867,-0.0401,0.9615,0.0280 -5.000,-0.3758,0.01570,0.00772,-0.0411,0.9531,0.0298 -4.750,-0.3449,0.01497,0.00692,-0.0420,0.9445,0.0318 -4.500,-0.3143,0.01417,0.00611,-0.0430,0.9361,0.0361 -4.250,-0.2854,0.01364,0.00548,-0.0434,0.9259,0.0399 -4.000,-0.2566,0.01315,0.00490,-0.0438,0.9164,0.0446 -3.750,-0.2281,0.01271,0.00443,-0.0441,0.9069,0.0543 -3.500,-0.2015,0.01222,0.00401,-0.0440,0.8963,0.0736 -3.250,-0.1765,0.01137,0.00355,-0.0441,0.8860,0.1704 -3.000,-0.1545,0.01003,0.00315,-0.0440,0.8762,0.4012 -2.750,-0.1300,0.00960,0.00310,-0.0434,0.8661,0.5226 -2.500,-0.1042,0.00944,0.00307,-0.0428,0.8564,0.5805 -2.250,-0.0794,0.00935,0.00314,-0.0418,0.8475,0.6470 -2.000,-0.0547,0.00935,0.00324,-0.0407,0.8376,0.6914 -1.750,-0.0280,0.00934,0.00319,-0.0403,0.8285,0.7070 -1.500,-0.0007,0.00932,0.00310,-0.0400,0.8200,0.7177 -1.250,0.0265,0.00929,0.00303,-0.0397,0.8106,0.7257 -1.000,0.0540,0.00928,0.00295,-0.0396,0.8020,0.7346 -0.750,0.0811,0.00927,0.00291,-0.0393,0.7930,0.7430 -0.500,0.1085,0.00926,0.00288,-0.0391,0.7845,0.7518 -0.250,0.1359,0.00927,0.00285,-0.0389,0.7764,0.7607 0.000,0.1630,0.00927,0.00286,-0.0387,0.7674,0.7694 0.250,0.1902,0.00929,0.00286,-0.0385,0.7594,0.7791 0.500,0.2172,0.00931,0.00289,-0.0382,0.7507,0.7884 0.750,0.2443,0.00933,0.00293,-0.0380,0.7431,0.7975 1.000,0.2714,0.00936,0.00298,-0.0377,0.7349,0.8077 1.250,0.2980,0.00940,0.00305,-0.0374,0.7268,0.8175 1.500,0.3246,0.00944,0.00312,-0.0370,0.7192,0.8275 1.750,0.3514,0.00948,0.00322,-0.0367,0.7113,0.8380 2.000,0.3777,0.00953,0.00332,-0.0362,0.7034,0.8487 2.250,0.4035,0.00957,0.00343,-0.0356,0.6931,0.8595 2.500,0.4292,0.00962,0.00353,-0.0350,0.6830,0.8708 2.750,0.4543,0.00965,0.00360,-0.0342,0.6676,0.8829 3.000,0.4774,0.00967,0.00355,-0.0328,0.6320,0.8958 3.250,0.4997,0.00977,0.00349,-0.0314,0.5797,0.9099 3.500,0.5237,0.00992,0.00355,-0.0304,0.5385,0.9250 3.750,0.5486,0.01015,0.00365,-0.0298,0.4833,0.9413 4.000,0.5704,0.01113,0.00391,-0.0292,0.3180,0.9619 4.250,0.5955,0.01260,0.00459,-0.0301,0.1517,1.0000 4.500,0.6162,0.01362,0.00519,-0.0295,0.0759,1.0000 4.750,0.6398,0.01429,0.00573,-0.0292,0.0529,1.0000 5.000,0.6641,0.01487,0.00632,-0.0289,0.0432,1.0000 5.250,0.6876,0.01555,0.00701,-0.0285,0.0371,1.0000 5.500,0.7112,0.01622,0.00775,-0.0280,0.0340,1.0000 5.750,0.7346,0.01688,0.00848,-0.0276,0.0310,1.0000 6.000,0.7574,0.01762,0.00926,-0.0271,0.0280,1.0000 6.250,0.7773,0.01879,0.01044,-0.0262,0.0258,1.0000 6.500,0.8000,0.01964,0.01139,-0.0255,0.0248,1.0000 6.750,0.8223,0.02063,0.01247,-0.0249,0.0237,1.0000 7.000,0.8449,0.02174,0.01366,-0.0242,0.0228,1.0000 7.250,0.8676,0.02295,0.01499,-0.0236,0.0219,1.0000 7.500,0.8906,0.02425,0.01641,-0.0230,0.0211,1.0000 7.750,0.9132,0.02540,0.01766,-0.0226,0.0202,1.0000 8.000,0.9348,0.02666,0.01898,-0.0221,0.0192,1.0000 8.250,0.9552,0.02891,0.02140,-0.0215,0.0183,1.0000 8.500,0.9759,0.03068,0.02345,-0.0207,0.0179,1.0000 8.750,0.9945,0.03282,0.02596,-0.0198,0.0175,1.0000 9.000,1.0101,0.03538,0.02890,-0.0185,0.0170,1.0000 9.250,1.0228,0.03804,0.03195,-0.0171,0.0164,1.0000 9.500,1.0328,0.04064,0.03490,-0.0155,0.0156,1.0000 9.750,1.0419,0.04278,0.03729,-0.0141,0.0149,1.0000 10.000,1.0474,0.04519,0.03995,-0.0125,0.0145,1.0000 10.250,1.0469,0.04809,0.04312,-0.0106,0.0142,1.0000 10.500,1.0407,0.05081,0.04607,-0.0081,0.0140,1.0000 10.750,1.0288,0.05390,0.04939,-0.0058,0.0139,1.0000 11.000,1.0147,0.05732,0.05302,-0.0045,0.0138,1.0000 11.250,0.9954,0.06179,0.05772,-0.0042,0.0138,1.0000 11.500,0.9752,0.06683,0.06296,-0.0054,0.0138,1.0000 11.750,0.9483,0.07378,0.07014,-0.0084,0.0139,1.0000 12.000,0.8925,0.08877,0.08543,-0.0180,0.0144,1.0000