Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca64210-il-100000-n5 Airfoil,naca64210-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,44.594 Max Cl/Cd alpha,4.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca64210-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5647,0.09085,0.08579,-0.0230,1.0000,0.0284 -9.750,-0.5706,0.08447,0.07945,-0.0273,1.0000,0.0284 -9.500,-0.5803,0.07716,0.07218,-0.0331,1.0000,0.0279 -9.250,-0.5951,0.07077,0.06577,-0.0380,1.0000,0.0275 -9.000,-0.6126,0.06581,0.06076,-0.0406,1.0000,0.0272 -8.750,-0.6262,0.06142,0.05624,-0.0415,1.0000,0.0270 -8.500,-0.6339,0.05710,0.05172,-0.0420,1.0000,0.0273 -8.250,-0.6366,0.05299,0.04736,-0.0419,1.0000,0.0278 -8.000,-0.6353,0.04906,0.04311,-0.0414,1.0000,0.0286 -7.750,-0.6306,0.04524,0.03891,-0.0405,1.0000,0.0290 -7.500,-0.6229,0.04158,0.03485,-0.0394,1.0000,0.0292 -7.250,-0.6123,0.03829,0.03114,-0.0381,1.0000,0.0295 -7.000,-0.5994,0.03535,0.02776,-0.0367,1.0000,0.0299 -6.750,-0.5844,0.03287,0.02484,-0.0352,1.0000,0.0304 -6.500,-0.5689,0.03059,0.02219,-0.0338,1.0000,0.0319 -6.250,-0.5528,0.02867,0.02012,-0.0326,1.0000,0.0337 -6.000,-0.5351,0.02701,0.01825,-0.0312,1.0000,0.0347 -5.750,-0.5170,0.02545,0.01649,-0.0297,1.0000,0.0358 -5.500,-0.4988,0.02407,0.01495,-0.0282,1.0000,0.0369 -5.250,-0.4806,0.02285,0.01359,-0.0266,1.0000,0.0383 -5.000,-0.4509,0.02178,0.01233,-0.0273,0.9956,0.0416 -4.750,-0.4177,0.02037,0.01087,-0.0288,0.9888,0.0449 -4.500,-0.3842,0.01927,0.00977,-0.0305,0.9818,0.0484 -4.250,-0.3489,0.01843,0.00881,-0.0324,0.9752,0.0540 -4.000,-0.3160,0.01757,0.00792,-0.0340,0.9672,0.0625 -3.750,-0.2810,0.01678,0.00709,-0.0358,0.9605,0.0751 -3.500,-0.2480,0.01582,0.00635,-0.0375,0.9527,0.1167 -3.250,-0.2232,0.01370,0.00577,-0.0386,0.9441,0.4272 -3.000,-0.1935,0.01332,0.00586,-0.0387,0.9365,0.5844 -2.750,-0.1675,0.01335,0.00610,-0.0375,0.9268,0.6642 -2.500,-0.1433,0.01365,0.00656,-0.0353,0.9184,0.7316 -2.250,-0.1160,0.01373,0.00658,-0.0344,0.9093,0.7540 -2.000,-0.0868,0.01368,0.00640,-0.0346,0.9001,0.7658 -1.750,-0.0555,0.01362,0.00621,-0.0351,0.8924,0.7765 -1.500,-0.0282,0.01358,0.00610,-0.0348,0.8824,0.7852 -1.250,0.0008,0.01353,0.00594,-0.0349,0.8738,0.7950 -1.000,0.0291,0.01348,0.00583,-0.0349,0.8651,0.8048 -0.750,0.0561,0.01346,0.00576,-0.0345,0.8557,0.8139 -0.500,0.0846,0.01341,0.00566,-0.0345,0.8481,0.8241 -0.250,0.1105,0.01341,0.00563,-0.0340,0.8382,0.8348 0.000,0.1373,0.01339,0.00560,-0.0336,0.8298,0.8446 0.250,0.1640,0.01338,0.00557,-0.0332,0.8214,0.8553 0.500,0.1901,0.01339,0.00559,-0.0327,0.8125,0.8669 0.750,0.2173,0.01337,0.00557,-0.0323,0.8052,0.8786 1.000,0.2434,0.01339,0.00563,-0.0319,0.7958,0.8905 1.250,0.2715,0.01338,0.00566,-0.0317,0.7887,0.9026 1.500,0.2995,0.01341,0.00574,-0.0317,0.7798,0.9158 1.750,0.3299,0.01342,0.00580,-0.0322,0.7721,0.9290 2.000,0.3621,0.01345,0.00592,-0.0331,0.7640,0.9423 2.250,0.3968,0.01349,0.00604,-0.0346,0.7561,0.9555 2.500,0.4337,0.01350,0.00615,-0.0364,0.7477,0.9684 2.750,0.4710,0.01354,0.00633,-0.0385,0.7370,0.9830 3.000,0.5060,0.01359,0.00649,-0.0402,0.7266,1.0000 3.250,0.5274,0.01365,0.00660,-0.0389,0.7127,1.0000 3.500,0.5481,0.01352,0.00644,-0.0370,0.6835,1.0000 3.750,0.5673,0.01333,0.00608,-0.0344,0.6288,1.0000 4.000,0.5876,0.01341,0.00598,-0.0325,0.5661,1.0000 4.250,0.6096,0.01367,0.00610,-0.0312,0.5036,1.0000 4.500,0.6227,0.01480,0.00627,-0.0287,0.3163,1.0000 4.750,0.6328,0.01691,0.00725,-0.0270,0.1287,1.0000 5.000,0.6516,0.01814,0.00820,-0.0259,0.0816,1.0000 5.250,0.6723,0.01910,0.00910,-0.0251,0.0645,1.0000 5.500,0.6930,0.02006,0.01008,-0.0242,0.0564,1.0000 5.750,0.7138,0.02100,0.01105,-0.0233,0.0498,1.0000 6.000,0.7340,0.02206,0.01217,-0.0224,0.0451,1.0000 6.250,0.7549,0.02319,0.01341,-0.0214,0.0421,1.0000 6.500,0.7763,0.02444,0.01470,-0.0206,0.0397,1.0000 6.750,0.7982,0.02592,0.01616,-0.0200,0.0373,1.0000 7.000,0.8217,0.02754,0.01788,-0.0195,0.0350,1.0000 7.250,0.8463,0.02906,0.01961,-0.0190,0.0331,1.0000 7.500,0.8707,0.03099,0.02179,-0.0185,0.0318,1.0000 7.750,0.8941,0.03312,0.02418,-0.0180,0.0309,1.0000 8.000,0.9155,0.03547,0.02686,-0.0172,0.0301,1.0000 8.250,0.9345,0.03803,0.02976,-0.0163,0.0294,1.0000 8.500,0.9511,0.04038,0.03240,-0.0154,0.0284,1.0000 8.750,0.9655,0.04269,0.03490,-0.0146,0.0271,1.0000 9.000,0.9737,0.04666,0.03911,-0.0135,0.0260,1.0000 9.250,0.9798,0.04969,0.04265,-0.0118,0.0257,1.0000 9.500,0.9815,0.05320,0.04658,-0.0100,0.0255,1.0000 9.750,0.9785,0.05689,0.05065,-0.0082,0.0254,1.0000 10.000,0.9705,0.06061,0.05469,-0.0064,0.0253,1.0000 10.250,0.9566,0.06412,0.05845,-0.0043,0.0253,1.0000 10.500,0.9405,0.06789,0.06242,-0.0032,0.0253,1.0000 10.750,0.9227,0.07215,0.06687,-0.0034,0.0254,1.0000 11.000,0.9040,0.07706,0.07194,-0.0048,0.0255,1.0000 11.250,0.8852,0.08269,0.07770,-0.0075,0.0256,1.0000 11.500,0.8665,0.08919,0.08431,-0.0114,0.0257,1.0000 11.750,0.8498,0.09635,0.09154,-0.0159,0.0259,1.0000 12.000,0.8343,0.10449,0.09976,-0.0216,0.0262,1.0000