Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca1410-il-50000 Airfoil,naca1410-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,31.1929 Max Cl/Cd alpha,5.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca1410-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.5190,0.09606,0.08875,0.0124,1.0000,0.3712 -8.000,-0.5138,0.09287,0.08559,0.0130,1.0000,0.3877 -7.750,-0.6636,0.06363,0.05616,-0.0284,1.0000,0.1667 -7.500,-0.6549,0.05879,0.05114,-0.0284,1.0000,0.1638 -7.250,-0.6487,0.05377,0.04587,-0.0285,1.0000,0.1604 -7.000,-0.6436,0.04872,0.04037,-0.0283,1.0000,0.1576 -6.750,-0.6330,0.04499,0.03623,-0.0274,1.0000,0.1602 -6.500,-0.6208,0.04144,0.03215,-0.0264,1.0000,0.1632 -6.250,-0.6054,0.03812,0.02822,-0.0252,1.0000,0.1650 -6.000,-0.5863,0.03523,0.02503,-0.0241,1.0000,0.1682 -5.750,-0.5653,0.03316,0.02282,-0.0230,1.0000,0.1753 -5.500,-0.5446,0.03113,0.02049,-0.0219,1.0000,0.1851 -5.250,-0.5221,0.02923,0.01822,-0.0208,1.0000,0.1956 -5.000,-0.4987,0.02742,0.01639,-0.0197,1.0000,0.2090 -4.750,-0.4761,0.02588,0.01491,-0.0186,1.0000,0.2303 -4.500,-0.4539,0.02443,0.01356,-0.0173,1.0000,0.2622 -4.250,-0.4321,0.02285,0.01222,-0.0160,1.0000,0.3107 -4.000,-0.4116,0.02133,0.01122,-0.0143,1.0000,0.3819 -3.750,-0.3947,0.02040,0.01086,-0.0115,1.0000,0.4712 -3.500,-0.3790,0.01945,0.01046,-0.0079,1.0000,0.5738 -3.250,-0.3655,0.01883,0.01038,-0.0029,1.0000,0.6774 -3.000,-0.3522,0.01862,0.01049,0.0030,1.0000,0.7764 -2.750,-0.3183,0.01900,0.01088,0.0063,1.0000,0.8739 -2.500,-0.1443,0.01990,0.01078,-0.0174,1.0000,0.9741 -2.250,-0.0704,0.01907,0.00959,-0.0285,1.0000,1.0000 -2.000,-0.0733,0.01848,0.00897,-0.0255,1.0000,1.0000 -1.750,-0.0774,0.01804,0.00848,-0.0219,1.0000,1.0000 -1.500,-0.0796,0.01776,0.00813,-0.0181,1.0000,1.0000 -1.250,-0.0780,0.01762,0.00789,-0.0147,1.0000,1.0000 -1.000,-0.0726,0.01759,0.00775,-0.0118,1.0000,1.0000 -0.750,-0.0637,0.01765,0.00769,-0.0094,1.0000,1.0000 -0.500,-0.0521,0.01779,0.00771,-0.0075,1.0000,1.0000 -0.250,-0.0384,0.01799,0.00781,-0.0059,1.0000,1.0000 0.000,-0.0235,0.01825,0.00799,-0.0047,1.0000,1.0000 0.250,-0.0078,0.01858,0.00824,-0.0037,1.0000,1.0000 0.500,0.0083,0.01897,0.00858,-0.0029,1.0000,1.0000 0.750,0.0247,0.01944,0.00900,-0.0023,1.0000,1.0000 1.000,0.0411,0.01998,0.00951,-0.0019,1.0000,1.0000 1.250,0.0575,0.02061,0.01011,-0.0017,1.0000,1.0000 1.500,0.0737,0.02131,0.01081,-0.0016,1.0000,1.0000 1.750,0.0959,0.02215,0.01166,-0.0029,0.9974,1.0000 2.000,0.1652,0.02338,0.01298,-0.0125,0.9751,1.0000 2.250,0.2277,0.02431,0.01403,-0.0204,0.9505,1.0000 2.500,0.2862,0.02502,0.01490,-0.0270,0.9248,1.0000 2.750,0.3508,0.02545,0.01553,-0.0340,0.8998,1.0000 3.000,0.4088,0.02562,0.01594,-0.0391,0.8729,1.0000 3.250,0.4605,0.02555,0.01611,-0.0424,0.8451,1.0000 3.500,0.5079,0.02526,0.01604,-0.0442,0.8164,1.0000 3.750,0.5495,0.02482,0.01580,-0.0442,0.7864,1.0000 4.000,0.5851,0.02434,0.01549,-0.0429,0.7547,1.0000 4.250,0.6168,0.02380,0.01506,-0.0406,0.7209,1.0000 4.500,0.6424,0.02346,0.01478,-0.0374,0.6826,1.0000 4.750,0.6673,0.02306,0.01435,-0.0339,0.6411,1.0000 5.000,0.6883,0.02298,0.01420,-0.0303,0.5934,1.0000 5.250,0.7075,0.02303,0.01410,-0.0266,0.5382,1.0000 5.500,0.7243,0.02322,0.01397,-0.0227,0.4725,1.0000 5.750,0.7375,0.02385,0.01417,-0.0189,0.3939,1.0000 6.000,0.7505,0.02512,0.01489,-0.0156,0.3142,1.0000 6.250,0.7679,0.02693,0.01620,-0.0134,0.2552,1.0000 6.500,0.7889,0.02874,0.01772,-0.0120,0.2181,1.0000 6.750,0.8132,0.03077,0.01975,-0.0110,0.1956,1.0000 7.000,0.8385,0.03299,0.02203,-0.0102,0.1817,1.0000 7.250,0.8626,0.03522,0.02428,-0.0095,0.1705,1.0000 7.500,0.8838,0.03736,0.02669,-0.0084,0.1604,1.0000 7.750,0.9044,0.04029,0.02995,-0.0074,0.1551,1.0000 8.000,0.9199,0.04354,0.03377,-0.0059,0.1517,1.0000 8.250,0.9349,0.04661,0.03720,-0.0045,0.1471,1.0000 8.500,0.9514,0.04983,0.04050,-0.0036,0.1419,1.0000 8.750,0.9555,0.05398,0.04523,-0.0018,0.1407,1.0000 9.000,0.9562,0.05864,0.05037,-0.0003,0.1408,1.0000 9.250,0.9525,0.06359,0.05571,0.0010,0.1412,1.0000 9.500,0.9447,0.06874,0.06118,0.0019,0.1417,1.0000 9.750,0.9350,0.07407,0.06672,0.0024,0.1422,1.0000 10.000,0.9255,0.07954,0.07237,0.0025,0.1430,1.0000 10.250,0.8529,0.09051,0.08353,-0.0025,0.1580,1.0000