Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca651412-il-100000 Airfoil,naca651412-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,52.9769 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca651412-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.4187,0.09531,0.09040,-0.0462,1.0000,0.1221 -9.250,-0.4491,0.09178,0.08705,-0.0503,1.0000,0.1257 -9.000,-0.4840,0.08843,0.08386,-0.0527,1.0000,0.1261 -8.750,-0.4399,0.08610,0.08147,-0.0463,1.0000,0.1364 -8.500,-0.4676,0.08335,0.07887,-0.0462,1.0000,0.1385 -8.250,-0.4966,0.08129,0.07695,-0.0437,1.0000,0.1383 -8.000,-0.5279,0.07959,0.07536,-0.0404,1.0000,0.1379 -7.750,-0.5599,0.07751,0.07332,-0.0382,1.0000,0.1387 -7.500,-0.5999,0.07559,0.07132,-0.0370,1.0000,0.1404 -7.250,-0.6076,0.07194,0.06772,-0.0350,1.0000,0.1437 -7.000,-0.6006,0.07009,0.06594,-0.0319,1.0000,0.1503 -6.750,-0.6271,0.06678,0.06239,-0.0324,1.0000,0.1577 -6.500,-0.6164,0.06476,0.06051,-0.0293,1.0000,0.1666 -6.000,-0.5851,0.05792,0.05353,-0.0331,0.9913,0.2074 -5.250,-0.4736,0.03763,0.02968,-0.0465,0.9751,0.0832 -5.000,-0.4391,0.03427,0.02599,-0.0486,0.9716,0.0821 -4.750,-0.4081,0.03165,0.02306,-0.0496,0.9674,0.0799 -4.500,-0.3762,0.02967,0.02074,-0.0503,0.9625,0.0785 -4.250,-0.3393,0.02813,0.01887,-0.0519,0.9584,0.0795 -4.000,-0.3051,0.02726,0.01771,-0.0531,0.9539,0.0829 -3.750,-0.2781,0.02593,0.01635,-0.0530,0.9488,0.0850 -3.500,-0.2451,0.02482,0.01536,-0.0542,0.9444,0.0892 -3.250,-0.2072,0.02414,0.01464,-0.0563,0.9410,0.0985 -3.000,-0.1882,0.02344,0.01407,-0.0552,0.9341,0.1072 -2.750,-0.1559,0.02275,0.01341,-0.0565,0.9296,0.1275 -2.500,-0.1366,0.02042,0.01382,-0.0546,0.9265,0.6949 -2.250,-0.1330,0.02116,0.01463,-0.0482,0.9186,0.7586 -2.000,-0.1227,0.02202,0.01552,-0.0421,0.9130,0.8079 -1.750,-0.1224,0.02262,0.01612,-0.0351,0.9063,0.8436 -1.500,-0.1226,0.02309,0.01660,-0.0273,0.8999,0.8802 -1.250,-0.1010,0.02364,0.01708,-0.0227,0.8964,0.9258 -1.000,-0.0720,0.02383,0.01713,-0.0232,0.8910,0.9464 -0.750,-0.0241,0.02398,0.01710,-0.0280,0.8869,0.9526 -0.500,0.0221,0.02410,0.01706,-0.0324,0.8833,0.9599 -0.250,0.0814,0.02428,0.01710,-0.0393,0.8813,0.9638 0.000,0.1123,0.02450,0.01726,-0.0416,0.8748,0.9727 0.250,0.1657,0.02467,0.01734,-0.0476,0.8711,0.9775 0.500,0.2180,0.02480,0.01741,-0.0533,0.8681,0.9832 0.750,0.2713,0.02495,0.01752,-0.0592,0.8651,0.9881 1.000,0.3053,0.02529,0.01786,-0.0623,0.8586,0.9980 1.250,0.3351,0.02544,0.01801,-0.0639,0.8537,1.0000 1.500,0.3140,0.02584,0.01840,-0.0571,0.8439,1.0000 1.750,0.3315,0.02601,0.01856,-0.0563,0.8384,1.0000 2.000,0.3191,0.02644,0.01897,-0.0511,0.8291,1.0000 2.250,0.3504,0.02672,0.01926,-0.0527,0.8240,1.0000 2.500,0.3707,0.02724,0.01978,-0.0527,0.8170,1.0000 2.750,0.3996,0.02764,0.02022,-0.0539,0.8104,1.0000 3.000,0.4452,0.02779,0.02042,-0.0572,0.8068,1.0000 3.250,0.4548,0.02861,0.02126,-0.0557,0.7965,1.0000 3.500,0.4992,0.02872,0.02147,-0.0586,0.7925,1.0000 3.750,0.5118,0.02957,0.02235,-0.0575,0.7821,1.0000 4.000,0.5605,0.02941,0.02232,-0.0605,0.7775,1.0000 4.250,0.5802,0.02989,0.02289,-0.0598,0.7657,1.0000 4.500,0.6110,0.03003,0.02317,-0.0603,0.7558,1.0000 4.750,0.6605,0.02940,0.02274,-0.0628,0.7493,1.0000 5.000,0.7603,0.02391,0.01760,-0.0667,0.7304,1.0000 5.250,0.8277,0.01875,0.01252,-0.0657,0.6899,1.0000 5.500,0.8562,0.01748,0.01137,-0.0636,0.6553,1.0000 5.750,0.8720,0.01646,0.01029,-0.0592,0.5776,1.0000 6.000,0.8524,0.01827,0.01015,-0.0502,0.2672,1.0000 6.250,0.8386,0.02126,0.01188,-0.0446,0.1258,1.0000 6.500,0.8446,0.02284,0.01324,-0.0415,0.1022,1.0000 6.750,0.8531,0.02430,0.01460,-0.0388,0.0915,1.0000 7.000,0.8680,0.02559,0.01585,-0.0370,0.0825,1.0000 7.250,0.8902,0.02718,0.01740,-0.0363,0.0760,1.0000 7.500,0.9240,0.02890,0.01910,-0.0371,0.0711,1.0000 7.750,0.9717,0.03191,0.02194,-0.0402,0.0664,1.0000 8.000,1.0008,0.03352,0.02385,-0.0402,0.0635,1.0000 8.250,1.0343,0.03603,0.02662,-0.0408,0.0623,1.0000 8.500,1.0632,0.03889,0.02983,-0.0408,0.0621,1.0000 8.750,1.0875,0.04212,0.03345,-0.0401,0.0629,1.0000 9.000,1.1065,0.04551,0.03724,-0.0389,0.0635,1.0000 9.250,1.1200,0.04883,0.04099,-0.0372,0.0636,1.0000 9.500,1.1305,0.05251,0.04504,-0.0354,0.0642,1.0000 9.750,1.1533,0.05894,0.05156,-0.0358,0.0672,1.0000 10.000,1.0904,0.05766,0.05151,-0.0267,0.0799,1.0000 12.000,0.8292,0.13212,0.12757,-0.0484,0.1680,1.0000 12.250,0.6746,0.13382,0.12968,-0.0425,0.1670,1.0000 12.500,0.6939,0.13715,0.13304,-0.0416,0.1636,1.0000