Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64012a-il-100000-n5 Airfoil,n64012a-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,35.5344 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-n64012a-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.7268,0.10113,0.09592,-0.0123,1.0000,0.0288 -12.250,-0.7458,0.09231,0.08705,-0.0181,1.0000,0.0285 -12.000,-0.7676,0.08429,0.07894,-0.0235,1.0000,0.0283 -11.750,-0.7898,0.07741,0.07193,-0.0277,1.0000,0.0281 -11.500,-0.8112,0.07158,0.06595,-0.0306,1.0000,0.0280 -11.250,-0.8315,0.06663,0.06080,-0.0320,1.0000,0.0279 -11.000,-0.8500,0.06239,0.05635,-0.0321,1.0000,0.0279 -10.750,-0.8668,0.05869,0.05241,-0.0309,1.0000,0.0279 -10.500,-0.8813,0.05541,0.04885,-0.0285,1.0000,0.0281 -10.250,-0.8906,0.05215,0.04521,-0.0261,1.0000,0.0285 -9.750,-0.8905,0.04606,0.03850,-0.0222,1.0000,0.0297 -9.500,-0.8817,0.04367,0.03592,-0.0208,1.0000,0.0304 -9.250,-0.8714,0.04122,0.03320,-0.0193,1.0000,0.0309 -9.000,-0.8587,0.03882,0.03048,-0.0179,1.0000,0.0314 -8.750,-0.8436,0.03660,0.02797,-0.0165,1.0000,0.0320 -8.500,-0.8263,0.03453,0.02564,-0.0154,1.0000,0.0328 -8.250,-0.8071,0.03261,0.02348,-0.0143,1.0000,0.0337 -8.000,-0.7868,0.03091,0.02156,-0.0133,1.0000,0.0350 -7.750,-0.7660,0.02953,0.01993,-0.0123,1.0000,0.0369 -7.500,-0.7449,0.02794,0.01821,-0.0114,1.0000,0.0386 -7.250,-0.7249,0.02657,0.01685,-0.0105,1.0000,0.0402 -7.000,-0.7054,0.02540,0.01565,-0.0093,1.0000,0.0420 -6.750,-0.6868,0.02432,0.01452,-0.0079,1.0000,0.0441 -6.500,-0.6690,0.02340,0.01350,-0.0063,1.0000,0.0471 -6.250,-0.6541,0.02240,0.01252,-0.0044,1.0000,0.0507 -6.000,-0.6389,0.02161,0.01172,-0.0025,1.0000,0.0552 -5.750,-0.6238,0.02087,0.01090,-0.0003,1.0000,0.0598 -5.500,-0.6105,0.02005,0.01014,0.0018,1.0000,0.0673 -5.250,-0.5969,0.01932,0.00944,0.0040,1.0000,0.0776 -5.000,-0.5837,0.01859,0.00877,0.0062,1.0000,0.0941 -4.500,-0.5468,0.01602,0.00727,0.0073,0.9920,0.2739 -4.250,-0.5220,0.01469,0.00707,0.0070,0.9826,0.4919 -4.000,-0.4888,0.01451,0.00707,0.0060,0.9743,0.5736 -3.750,-0.4561,0.01449,0.00709,0.0052,0.9650,0.6206 -3.500,-0.4238,0.01458,0.00721,0.0047,0.9563,0.6624 -3.250,-0.3912,0.01479,0.00744,0.0045,0.9482,0.6989 -3.000,-0.3610,0.01483,0.00741,0.0043,0.9379,0.7205 -2.750,-0.3271,0.01481,0.00731,0.0033,0.9298,0.7322 -2.500,-0.2949,0.01475,0.00715,0.0025,0.9203,0.7419 -2.250,-0.2643,0.01466,0.00696,0.0019,0.9103,0.7518 -2.000,-0.2309,0.01458,0.00682,0.0009,0.9024,0.7594 -1.750,-0.2025,0.01450,0.00665,0.0008,0.8915,0.7681 -1.500,-0.1725,0.01444,0.00654,0.0005,0.8821,0.7761 -1.250,-0.1422,0.01437,0.00641,0.0001,0.8733,0.7842 -1.000,-0.1142,0.01433,0.00633,0.0001,0.8630,0.7928 -0.750,-0.0847,0.01429,0.00626,-0.0001,0.8545,0.8008 -0.500,-0.0570,0.01425,0.00619,0.0000,0.8449,0.8101 -0.250,-0.0283,0.01425,0.00619,0.0000,0.8357,0.8179 0.000,0.0000,0.01422,0.00613,0.0000,0.8275,0.8275 0.250,0.0283,0.01425,0.00619,0.0000,0.8179,0.8357 0.500,0.0570,0.01425,0.00619,0.0000,0.8101,0.8448 0.750,0.0847,0.01429,0.00626,0.0001,0.8008,0.8545 1.000,0.1143,0.01433,0.00633,-0.0001,0.7928,0.8630 1.250,0.1422,0.01437,0.00641,-0.0001,0.7842,0.8733 1.500,0.1725,0.01444,0.00654,-0.0005,0.7761,0.8821 1.750,0.2025,0.01450,0.00665,-0.0008,0.7681,0.8915 2.000,0.2309,0.01458,0.00682,-0.0009,0.7594,0.9024 2.250,0.2643,0.01466,0.00696,-0.0019,0.7518,0.9103 2.500,0.2949,0.01475,0.00715,-0.0025,0.7419,0.9203 2.750,0.3271,0.01481,0.00731,-0.0033,0.7322,0.9298 3.000,0.3610,0.01483,0.00741,-0.0043,0.7205,0.9379 3.250,0.3912,0.01479,0.00744,-0.0045,0.6989,0.9482 3.500,0.4238,0.01458,0.00721,-0.0047,0.6624,0.9563 3.750,0.4561,0.01449,0.00709,-0.0052,0.6205,0.9650 4.000,0.4888,0.01451,0.00707,-0.0060,0.5737,0.9743 4.250,0.5220,0.01469,0.00707,-0.0070,0.4920,0.9826 4.500,0.5468,0.01602,0.00727,-0.0073,0.2740,0.9920 5.000,0.5837,0.01859,0.00877,-0.0062,0.0941,1.0000 5.250,0.5969,0.01932,0.00944,-0.0040,0.0776,1.0000 5.500,0.6105,0.02005,0.01014,-0.0018,0.0673,1.0000 5.750,0.6238,0.02086,0.01089,0.0003,0.0598,1.0000 6.000,0.6389,0.02160,0.01172,0.0025,0.0552,1.0000 6.250,0.6541,0.02240,0.01252,0.0044,0.0507,1.0000 6.500,0.6690,0.02340,0.01350,0.0063,0.0471,1.0000 6.750,0.6868,0.02431,0.01452,0.0079,0.0441,1.0000 7.000,0.7054,0.02540,0.01565,0.0093,0.0420,1.0000 7.250,0.7249,0.02657,0.01685,0.0105,0.0402,1.0000 7.500,0.7449,0.02794,0.01821,0.0114,0.0386,1.0000 7.750,0.7660,0.02953,0.01993,0.0123,0.0369,1.0000 8.000,0.7869,0.03091,0.02156,0.0133,0.0350,1.0000 8.250,0.8072,0.03261,0.02348,0.0143,0.0337,1.0000 8.500,0.8264,0.03453,0.02565,0.0153,0.0328,1.0000 8.750,0.8437,0.03660,0.02798,0.0165,0.0320,1.0000 9.000,0.8588,0.03883,0.03049,0.0178,0.0314,1.0000 9.250,0.8715,0.04123,0.03320,0.0193,0.0309,1.0000 9.500,0.8819,0.04368,0.03592,0.0208,0.0304,1.0000 9.750,0.8907,0.04606,0.03850,0.0222,0.0297,1.0000 10.250,0.8908,0.05217,0.04523,0.0260,0.0285,1.0000 10.500,0.8815,0.05543,0.04887,0.0284,0.0281,1.0000 10.750,0.8670,0.05872,0.05245,0.0308,0.0279,1.0000 11.000,0.8503,0.06243,0.05639,0.0320,0.0279,1.0000 11.250,0.8318,0.06669,0.06087,0.0319,0.0279,1.0000 11.500,0.8116,0.07166,0.06602,0.0304,0.0280,1.0000 11.750,0.7903,0.07749,0.07202,0.0275,0.0281,1.0000 12.000,0.7681,0.08440,0.07905,0.0233,0.0283,1.0000 12.250,0.7463,0.09246,0.08720,0.0178,0.0285,1.0000 12.500,0.7273,0.10136,0.09615,0.0120,0.0288,1.0000