Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca2410-il-50000-n5 Airfoil,naca2410-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,36.0834 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-naca2410-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.5281,0.09780,0.09035,-0.0247,1.0000,0.0669 -9.500,-0.5327,0.09260,0.08522,-0.0275,1.0000,0.0666 -9.250,-0.5395,0.08706,0.07975,-0.0308,1.0000,0.0665 -9.000,-0.5500,0.08089,0.07366,-0.0352,1.0000,0.0664 -8.750,-0.5646,0.07404,0.06684,-0.0402,1.0000,0.0662 -8.500,-0.5783,0.06772,0.06048,-0.0435,1.0000,0.0663 -8.250,-0.5897,0.06196,0.05453,-0.0454,1.0000,0.0669 -8.000,-0.5969,0.05664,0.04892,-0.0463,1.0000,0.0679 -7.750,-0.5999,0.05161,0.04346,-0.0462,1.0000,0.0692 -7.500,-0.5976,0.04702,0.03831,-0.0456,1.0000,0.0703 -7.250,-0.5880,0.04363,0.03455,-0.0446,1.0000,0.0719 -7.000,-0.5725,0.04197,0.03285,-0.0436,1.0000,0.0753 -6.750,-0.5581,0.03956,0.03012,-0.0425,1.0000,0.0788 -6.500,-0.5426,0.03671,0.02675,-0.0414,1.0000,0.0814 -6.250,-0.5247,0.03417,0.02364,-0.0403,1.0000,0.0844 -6.000,-0.5058,0.03280,0.02230,-0.0393,1.0000,0.0887 -5.750,-0.4858,0.03123,0.02044,-0.0383,1.0000,0.0935 -5.500,-0.4641,0.02950,0.01829,-0.0372,1.0000,0.0973 -5.250,-0.4429,0.02812,0.01687,-0.0363,1.0000,0.1012 -5.000,-0.4214,0.02707,0.01570,-0.0353,1.0000,0.1083 -4.750,-0.3997,0.02603,0.01459,-0.0343,1.0000,0.1164 -4.500,-0.3773,0.02506,0.01344,-0.0333,1.0000,0.1254 -4.250,-0.3551,0.02414,0.01255,-0.0324,1.0000,0.1358 -4.000,-0.3325,0.02337,0.01176,-0.0316,1.0000,0.1532 -3.750,-0.3097,0.02263,0.01109,-0.0310,1.0000,0.1757 -3.500,-0.2874,0.02196,0.01051,-0.0304,1.0000,0.2070 -3.250,-0.2650,0.02136,0.01007,-0.0299,1.0000,0.2494 -3.000,-0.2428,0.02076,0.00971,-0.0293,1.0000,0.3017 -2.750,-0.2207,0.02017,0.00940,-0.0287,1.0000,0.3646 -2.500,-0.1990,0.01960,0.00921,-0.0279,1.0000,0.4437 -2.250,-0.1790,0.01905,0.00917,-0.0264,1.0000,0.5487 -2.000,-0.1620,0.01859,0.00925,-0.0236,1.0000,0.6772 -1.750,-0.1412,0.01832,0.00938,-0.0209,1.0000,0.8391 -1.500,-0.0892,0.01833,0.00923,-0.0260,0.9953,1.0000 -1.250,-0.0452,0.01857,0.00913,-0.0299,0.9850,1.0000 -1.000,-0.0023,0.01879,0.00909,-0.0336,0.9741,1.0000 -0.750,0.0392,0.01899,0.00906,-0.0369,0.9624,1.0000 -0.500,0.0792,0.01916,0.00906,-0.0398,0.9499,1.0000 -0.250,0.1181,0.01932,0.00908,-0.0424,0.9370,1.0000 0.000,0.1571,0.01946,0.00910,-0.0449,0.9241,1.0000 0.250,0.1968,0.01958,0.00914,-0.0474,0.9115,1.0000 0.500,0.2368,0.01967,0.00916,-0.0498,0.8991,1.0000 0.750,0.2749,0.01973,0.00916,-0.0517,0.8862,1.0000 1.000,0.3099,0.01978,0.00919,-0.0530,0.8720,1.0000 1.250,0.3432,0.01983,0.00923,-0.0538,0.8572,1.0000 1.500,0.3757,0.01987,0.00926,-0.0545,0.8421,1.0000 1.750,0.4065,0.01993,0.00933,-0.0547,0.8263,1.0000 2.000,0.4360,0.02000,0.00942,-0.0546,0.8097,1.0000 2.250,0.4649,0.02009,0.00953,-0.0544,0.7929,1.0000 2.500,0.4934,0.02018,0.00965,-0.0541,0.7757,1.0000 2.750,0.5219,0.02027,0.00978,-0.0538,0.7584,1.0000 3.000,0.5502,0.02038,0.00993,-0.0533,0.7408,1.0000 3.250,0.5783,0.02048,0.01007,-0.0527,0.7230,1.0000 3.500,0.6063,0.02059,0.01021,-0.0521,0.7050,1.0000 3.750,0.6315,0.02081,0.01050,-0.0512,0.6846,1.0000 4.000,0.6573,0.02100,0.01074,-0.0503,0.6642,1.0000 4.250,0.6840,0.02115,0.01093,-0.0493,0.6440,1.0000 4.500,0.7078,0.02143,0.01129,-0.0481,0.6208,1.0000 4.750,0.7332,0.02162,0.01150,-0.0470,0.5979,1.0000 5.000,0.7560,0.02191,0.01184,-0.0455,0.5712,1.0000 5.250,0.7784,0.02218,0.01216,-0.0440,0.5423,1.0000 5.500,0.7999,0.02248,0.01247,-0.0423,0.5106,1.0000 5.750,0.8205,0.02283,0.01279,-0.0405,0.4764,1.0000 6.000,0.8393,0.02326,0.01322,-0.0386,0.4371,1.0000 6.250,0.8562,0.02378,0.01366,-0.0364,0.3899,1.0000 6.500,0.8710,0.02449,0.01416,-0.0342,0.3336,1.0000 6.750,0.8846,0.02549,0.01487,-0.0320,0.2729,1.0000 7.000,0.8971,0.02683,0.01586,-0.0301,0.2178,1.0000 7.250,0.9094,0.02840,0.01715,-0.0283,0.1759,1.0000 7.500,0.9226,0.03001,0.01861,-0.0266,0.1485,1.0000 7.750,0.9365,0.03162,0.02013,-0.0249,0.1303,1.0000 8.000,0.9511,0.03319,0.02166,-0.0234,0.1167,1.0000 8.250,0.9664,0.03470,0.02319,-0.0219,0.1062,1.0000 8.500,0.9851,0.03627,0.02490,-0.0206,0.0990,1.0000 8.750,1.0044,0.03789,0.02660,-0.0195,0.0935,1.0000 9.000,1.0257,0.03967,0.02851,-0.0186,0.0884,1.0000 9.250,1.0445,0.04141,0.03046,-0.0176,0.0827,1.0000 9.500,1.0645,0.04332,0.03231,-0.0169,0.0785,1.0000 9.750,1.0844,0.04573,0.03509,-0.0159,0.0756,1.0000 10.250,1.1105,0.05035,0.04033,-0.0133,0.0687,1.0000 10.500,1.1254,0.05280,0.04278,-0.0125,0.0659,1.0000 10.750,1.1283,0.05603,0.04647,-0.0105,0.0644,1.0000 11.000,1.1240,0.05936,0.05026,-0.0082,0.0629,1.0000 11.250,1.1143,0.06264,0.05390,-0.0058,0.0615,1.0000 11.500,1.1019,0.06617,0.05773,-0.0039,0.0603,1.0000 11.750,1.0869,0.07008,0.06191,-0.0029,0.0594,1.0000 12.000,1.0684,0.07464,0.06672,-0.0028,0.0589,1.0000 12.250,1.0444,0.08032,0.07265,-0.0043,0.0589,1.0000 12.500,1.0122,0.08797,0.08054,-0.0079,0.0596,1.0000 12.750,0.9747,0.09801,0.09076,-0.0141,0.0610,1.0000