Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n63012a-il-100000-n5 Airfoil,n63012a-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,38.2796 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-n63012a-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.7603,0.09822,0.09295,-0.0120,1.0000,0.0279 -12.500,-0.7822,0.08943,0.08408,-0.0179,1.0000,0.0277 -12.250,-0.8050,0.08166,0.07619,-0.0231,1.0000,0.0275 -12.000,-0.8271,0.07502,0.06940,-0.0271,1.0000,0.0274 -11.750,-0.8480,0.06938,0.06356,-0.0297,1.0000,0.0273 -11.500,-0.8675,0.06454,0.05852,-0.0311,1.0000,0.0273 -11.250,-0.8850,0.06039,0.05413,-0.0312,1.0000,0.0273 -11.000,-0.9004,0.05677,0.05025,-0.0300,1.0000,0.0273 -10.750,-0.9134,0.05360,0.04677,-0.0278,1.0000,0.0275 -10.500,-0.9216,0.05059,0.04337,-0.0254,1.0000,0.0279 -10.250,-0.9217,0.04751,0.04004,-0.0237,1.0000,0.0285 -10.000,-0.9145,0.04514,0.03752,-0.0224,1.0000,0.0292 -9.750,-0.9054,0.04296,0.03514,-0.0211,1.0000,0.0300 -9.500,-0.8946,0.04062,0.03253,-0.0197,1.0000,0.0306 -9.250,-0.8814,0.03827,0.02989,-0.0183,1.0000,0.0311 -9.000,-0.8656,0.03609,0.02743,-0.0171,1.0000,0.0318 -8.750,-0.8477,0.03406,0.02515,-0.0160,1.0000,0.0327 -8.500,-0.8281,0.03219,0.02302,-0.0150,1.0000,0.0336 -8.250,-0.8076,0.03054,0.02115,-0.0141,1.0000,0.0349 -8.000,-0.7870,0.02912,0.01954,-0.0131,1.0000,0.0366 -7.750,-0.7681,0.02767,0.01813,-0.0122,1.0000,0.0387 -7.500,-0.7486,0.02648,0.01691,-0.0112,1.0000,0.0407 -7.250,-0.7295,0.02531,0.01564,-0.0099,1.0000,0.0429 -7.000,-0.7112,0.02424,0.01446,-0.0085,1.0000,0.0453 -6.750,-0.6953,0.02313,0.01335,-0.0068,1.0000,0.0484 -6.500,-0.6785,0.02227,0.01249,-0.0052,1.0000,0.0533 -6.250,-0.6625,0.02139,0.01156,-0.0034,1.0000,0.0589 -6.000,-0.6469,0.02055,0.01071,-0.0016,1.0000,0.0666 -5.750,-0.6318,0.01972,0.00993,0.0004,1.0000,0.0782 -5.500,-0.6168,0.01890,0.00920,0.0023,1.0000,0.0967 -5.250,-0.6033,0.01794,0.00850,0.0043,1.0000,0.1319 -5.000,-0.5916,0.01683,0.00781,0.0064,1.0000,0.2034 -4.750,-0.5818,0.01562,0.00728,0.0088,1.0000,0.3197 -4.500,-0.5695,0.01488,0.00710,0.0112,1.0000,0.4328 -4.250,-0.5360,0.01454,0.00704,0.0098,0.9911,0.5208 -4.000,-0.5013,0.01444,0.00702,0.0084,0.9824,0.5747 -3.750,-0.4658,0.01443,0.00704,0.0070,0.9740,0.6165 -3.500,-0.4320,0.01446,0.00709,0.0060,0.9646,0.6494 -3.250,-0.3981,0.01449,0.00706,0.0050,0.9555,0.6755 -3.000,-0.3624,0.01451,0.00702,0.0037,0.9474,0.6947 -2.750,-0.3307,0.01447,0.00693,0.0030,0.9367,0.7098 -2.500,-0.2976,0.01441,0.00678,0.0020,0.9271,0.7225 -2.250,-0.2642,0.01433,0.00661,0.0010,0.9179,0.7344 -2.000,-0.2336,0.01428,0.00652,0.0006,0.9070,0.7441 -1.750,-0.2026,0.01422,0.00640,0.0001,0.8970,0.7544 -1.500,-0.1718,0.01414,0.00626,-0.0004,0.8874,0.7654 -1.250,-0.1431,0.01411,0.00621,-0.0003,0.8763,0.7750 -1.000,-0.1138,0.01407,0.00614,-0.0004,0.8660,0.7850 -0.750,-0.0846,0.01402,0.00604,-0.0005,0.8567,0.7959 -0.500,-0.0565,0.01401,0.00604,-0.0003,0.8455,0.8052 -0.250,-0.0283,0.01400,0.00602,-0.0001,0.8354,0.8152 0.000,0.0000,0.01398,0.00596,0.0000,0.8261,0.8261 0.250,0.0283,0.01400,0.00602,0.0001,0.8152,0.8354 0.500,0.0565,0.01402,0.00604,0.0003,0.8052,0.8455 0.750,0.0846,0.01402,0.00604,0.0005,0.7959,0.8567 1.000,0.1139,0.01407,0.00614,0.0004,0.7850,0.8660 1.250,0.1431,0.01411,0.00621,0.0003,0.7750,0.8763 1.500,0.1718,0.01414,0.00626,0.0004,0.7654,0.8874 1.750,0.2026,0.01422,0.00640,-0.0001,0.7544,0.8970 2.000,0.2336,0.01428,0.00652,-0.0006,0.7441,0.9070 2.250,0.2642,0.01433,0.00661,-0.0010,0.7344,0.9179 2.500,0.2976,0.01441,0.00678,-0.0021,0.7225,0.9271 2.750,0.3307,0.01447,0.00693,-0.0030,0.7098,0.9367 3.000,0.3625,0.01451,0.00702,-0.0037,0.6947,0.9474 3.250,0.3981,0.01449,0.00706,-0.0050,0.6755,0.9554 3.500,0.4320,0.01447,0.00709,-0.0060,0.6494,0.9646 3.750,0.4658,0.01443,0.00704,-0.0070,0.6165,0.9740 4.000,0.5013,0.01444,0.00702,-0.0084,0.5747,0.9824 4.250,0.5361,0.01454,0.00704,-0.0098,0.5208,0.9911 4.500,0.5696,0.01488,0.00710,-0.0112,0.4327,1.0000 4.750,0.5819,0.01562,0.00728,-0.0088,0.3196,1.0000 5.000,0.5917,0.01683,0.00782,-0.0065,0.2033,1.0000 5.250,0.6034,0.01794,0.00850,-0.0043,0.1317,1.0000 5.500,0.6168,0.01890,0.00920,-0.0023,0.0967,1.0000 5.750,0.6319,0.01972,0.00993,-0.0004,0.0781,1.0000 6.000,0.6470,0.02055,0.01071,0.0015,0.0666,1.0000 6.250,0.6625,0.02139,0.01157,0.0034,0.0589,1.0000 6.500,0.6786,0.02227,0.01249,0.0052,0.0533,1.0000 6.750,0.6953,0.02313,0.01335,0.0068,0.0484,1.0000 7.000,0.7112,0.02424,0.01446,0.0085,0.0453,1.0000 7.250,0.7295,0.02531,0.01564,0.0099,0.0429,1.0000 7.500,0.7486,0.02648,0.01691,0.0112,0.0407,1.0000 7.750,0.7681,0.02767,0.01813,0.0122,0.0387,1.0000 8.000,0.7870,0.02912,0.01954,0.0131,0.0366,1.0000 8.250,0.8076,0.03054,0.02115,0.0141,0.0349,1.0000 8.500,0.8282,0.03219,0.02302,0.0150,0.0336,1.0000 8.750,0.8477,0.03406,0.02515,0.0160,0.0327,1.0000 9.000,0.8656,0.03609,0.02743,0.0171,0.0318,1.0000 9.250,0.8814,0.03827,0.02989,0.0183,0.0311,1.0000 9.500,0.8946,0.04062,0.03253,0.0196,0.0306,1.0000 9.750,0.9055,0.04296,0.03514,0.0211,0.0300,1.0000 10.000,0.9147,0.04513,0.03751,0.0224,0.0292,1.0000 10.250,0.9219,0.04751,0.04004,0.0237,0.0284,1.0000 10.500,0.9217,0.05060,0.04338,0.0254,0.0279,1.0000 10.750,0.9136,0.05361,0.04679,0.0278,0.0275,1.0000 11.000,0.9006,0.05679,0.05027,0.0300,0.0273,1.0000 11.250,0.8853,0.06042,0.05416,0.0311,0.0273,1.0000 11.500,0.8678,0.06458,0.05856,0.0310,0.0273,1.0000 11.750,0.8484,0.06942,0.06362,0.0296,0.0273,1.0000 12.000,0.8275,0.07509,0.06947,0.0269,0.0274,1.0000 12.250,0.8054,0.08174,0.07628,0.0229,0.0275,1.0000 12.500,0.7827,0.08953,0.08419,0.0176,0.0277,1.0000 12.750,0.7607,0.09840,0.09313,0.0117,0.0279,1.0000