Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64212ma-il-50000-n5 Airfoil,n64212ma-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,28.1256 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-n64212ma-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.3909,0.10180,0.09477,-0.0298,1.0000,0.1588 -8.750,-0.3691,0.09836,0.09133,-0.0277,1.0000,0.1647 -8.500,-0.3986,0.09658,0.08974,-0.0318,1.0000,0.1743 -8.250,-0.3812,0.09235,0.08557,-0.0300,1.0000,0.1792 -8.000,-0.3710,0.08948,0.08275,-0.0290,1.0000,0.1853 -7.500,-0.3854,0.08410,0.07766,-0.0282,1.0000,0.2027 -7.250,-0.3996,0.08192,0.07563,-0.0271,1.0000,0.2089 -7.000,-0.4164,0.07968,0.07357,-0.0251,1.0000,0.2224 -6.500,-0.4918,0.06707,0.05991,-0.0321,1.0000,0.0886 -6.000,-0.4632,0.05946,0.05190,-0.0341,0.9899,0.0785 -5.750,-0.4373,0.05588,0.04806,-0.0369,0.9814,0.0779 -5.500,-0.4122,0.05264,0.04453,-0.0391,0.9726,0.0773 -5.250,-0.3833,0.04942,0.04099,-0.0415,0.9653,0.0756 -5.000,-0.3569,0.04650,0.03764,-0.0429,0.9565,0.0734 -4.750,-0.3247,0.04379,0.03424,-0.0447,0.9496,0.0712 -4.500,-0.2975,0.04167,0.03181,-0.0455,0.9412,0.0708 -4.250,-0.2639,0.03959,0.02948,-0.0474,0.9355,0.0718 -4.000,-0.2377,0.03802,0.02779,-0.0479,0.9274,0.0733 -3.750,-0.2053,0.03644,0.02597,-0.0490,0.9208,0.0745 -3.500,-0.1674,0.03483,0.02407,-0.0509,0.9162,0.0746 -3.250,-0.1433,0.03371,0.02275,-0.0503,0.9076,0.0749 -3.000,-0.1096,0.03253,0.02138,-0.0512,0.9017,0.0755 -2.750,-0.0720,0.03148,0.02015,-0.0526,0.8972,0.0776 -2.500,-0.0479,0.03086,0.01939,-0.0516,0.8888,0.0797 -2.250,-0.0178,0.03004,0.01868,-0.0518,0.8826,0.0820 -2.000,0.0163,0.02935,0.01799,-0.0523,0.8780,0.0839 -1.750,0.0418,0.02890,0.01750,-0.0515,0.8708,0.0859 -1.500,0.0677,0.02852,0.01703,-0.0508,0.8624,0.0888 -1.250,0.1014,0.02782,0.01642,-0.0517,0.8560,0.0941 -1.000,0.1216,0.02756,0.01610,-0.0504,0.8460,0.0985 -0.750,0.1502,0.02702,0.01557,-0.0504,0.8373,0.1037 -0.500,0.1811,0.02652,0.01505,-0.0508,0.8294,0.1135 -0.250,0.2027,0.02622,0.01479,-0.0499,0.8185,0.1264 0.250,0.2343,0.02389,0.01496,-0.0440,0.7999,0.7152 0.500,0.2485,0.02385,0.01515,-0.0378,0.7897,0.8283 0.750,0.2697,0.02382,0.01517,-0.0334,0.7757,0.9020 1.000,0.3859,0.02273,0.01383,-0.0445,0.7524,0.9719 1.250,0.4240,0.02223,0.01319,-0.0457,0.7340,0.9811 1.500,0.4622,0.02173,0.01256,-0.0469,0.7134,0.9910 1.750,0.4921,0.02137,0.01211,-0.0470,0.6923,1.0000 2.000,0.5047,0.02117,0.01182,-0.0441,0.6734,1.0000 2.250,0.5155,0.02107,0.01167,-0.0410,0.6538,1.0000 2.500,0.5265,0.02100,0.01153,-0.0379,0.6320,1.0000 2.750,0.5372,0.02098,0.01145,-0.0348,0.6050,1.0000 3.000,0.5518,0.02096,0.01133,-0.0323,0.5727,1.0000 3.250,0.5688,0.02100,0.01123,-0.0301,0.5315,1.0000 3.500,0.5880,0.02107,0.01104,-0.0282,0.4665,1.0000 3.750,0.6047,0.02150,0.01070,-0.0257,0.3758,1.0000 4.000,0.6184,0.02241,0.01107,-0.0238,0.3227,1.0000 4.250,0.6332,0.02338,0.01165,-0.0222,0.2903,1.0000 4.500,0.6497,0.02431,0.01229,-0.0209,0.2696,1.0000 4.750,0.6684,0.02514,0.01296,-0.0199,0.2541,1.0000 5.000,0.6883,0.02597,0.01365,-0.0190,0.2423,1.0000 5.250,0.7095,0.02677,0.01433,-0.0183,0.2329,1.0000 5.500,0.7327,0.02754,0.01501,-0.0177,0.2257,1.0000 5.750,0.7576,0.02828,0.01572,-0.0174,0.2194,1.0000 6.000,0.7838,0.02905,0.01642,-0.0173,0.2146,1.0000 6.250,0.8123,0.02982,0.01714,-0.0174,0.2107,1.0000 6.500,0.8412,0.03059,0.01798,-0.0176,0.2070,1.0000 6.750,0.8700,0.03142,0.01883,-0.0177,0.2038,1.0000 7.000,0.8986,0.03228,0.01974,-0.0179,0.2009,1.0000 7.250,0.9271,0.03319,0.02062,-0.0182,0.1982,1.0000 7.500,0.9555,0.03418,0.02157,-0.0184,0.1956,1.0000 7.750,0.9800,0.03521,0.02282,-0.0182,0.1926,1.0000 8.000,1.0042,0.03629,0.02406,-0.0180,0.1896,1.0000 8.250,1.0281,0.03739,0.02528,-0.0179,0.1869,1.0000 8.500,1.0521,0.03849,0.02645,-0.0177,0.1840,1.0000 8.750,1.0777,0.03957,0.02749,-0.0177,0.1810,1.0000 9.000,1.0935,0.04092,0.02918,-0.0167,0.1774,1.0000 9.250,1.1100,0.04212,0.03059,-0.0159,0.1730,1.0000 9.500,1.1311,0.04296,0.03139,-0.0154,0.1683,1.0000 9.750,1.1424,0.04435,0.03308,-0.0141,0.1636,1.0000 10.000,1.1551,0.04548,0.03438,-0.0129,0.1586,1.0000 10.250,1.1706,0.04644,0.03538,-0.0120,0.1539,1.0000 10.500,1.1751,0.04801,0.03727,-0.0102,0.1490,1.0000 10.750,1.1896,0.04868,0.03792,-0.0091,0.1441,1.0000 11.000,1.1857,0.05056,0.04015,-0.0068,0.1393,1.0000 11.250,1.1972,0.05124,0.04078,-0.0055,0.1350,1.0000 11.500,1.1873,0.05375,0.04365,-0.0032,0.1310,1.0000 11.750,1.1956,0.05482,0.04473,-0.0021,0.1271,1.0000 12.000,1.1830,0.05792,0.04814,-0.0007,0.1235,1.0000 12.250,1.1885,0.05939,0.04965,0.0001,0.1195,1.0000 12.500,1.1718,0.06335,0.05389,0.0005,0.1164,1.0000 12.750,1.1726,0.06565,0.05625,0.0008,0.1129,1.0000 13.000,1.1522,0.07063,0.06147,0.0001,0.1103,1.0000 13.250,1.1220,0.07738,0.06848,-0.0020,0.1082,1.0000 13.500,1.1246,0.08011,0.07121,-0.0025,0.1051,1.0000 13.750,1.0414,0.09693,0.08841,-0.0118,0.1048,1.0000 14.000,0.9317,0.12592,0.11752,-0.0296,0.1002,1.0000