Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n63412-il-100000 Airfoil,n63412-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,56.6417 Max Cl/Cd alpha,6.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-n63412-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.4645,0.09508,0.09024,-0.0421,1.0000,0.1434 -9.250,-0.4258,0.09255,0.08760,-0.0366,1.0000,0.1486 -9.000,-0.4586,0.08890,0.08412,-0.0421,1.0000,0.1568 -8.750,-0.4385,0.08534,0.08055,-0.0393,1.0000,0.1611 -8.500,-0.4366,0.08262,0.07788,-0.0390,1.0000,0.1683 -8.250,-0.5188,0.07808,0.07362,-0.0468,1.0000,0.1722 -8.000,-0.4524,0.07664,0.07211,-0.0383,1.0000,0.1827 -7.750,-0.5190,0.07267,0.06836,-0.0423,1.0000,0.1865 -7.500,-0.4863,0.07128,0.06703,-0.0359,1.0000,0.1947 -6.750,-0.5919,0.04422,0.03794,-0.0449,1.0000,0.0835 -6.500,-0.5809,0.04042,0.03396,-0.0440,1.0000,0.0803 -6.250,-0.5672,0.03727,0.03041,-0.0434,1.0000,0.0793 -6.000,-0.5501,0.03439,0.02709,-0.0428,1.0000,0.0783 -5.750,-0.5300,0.03160,0.02377,-0.0423,1.0000,0.0765 -5.500,-0.5084,0.02948,0.02124,-0.0417,1.0000,0.0764 -5.250,-0.4687,0.02769,0.01912,-0.0445,0.9951,0.0801 -5.000,-0.4289,0.02617,0.01719,-0.0468,0.9893,0.0838 -4.750,-0.3894,0.02434,0.01526,-0.0492,0.9844,0.0875 -4.500,-0.3531,0.02332,0.01423,-0.0512,0.9780,0.0959 -4.250,-0.3148,0.02209,0.01310,-0.0534,0.9724,0.1048 -4.000,-0.2796,0.02114,0.01225,-0.0553,0.9658,0.1207 -3.750,-0.2422,0.01996,0.01128,-0.0577,0.9594,0.1573 -3.500,-0.2109,0.01769,0.01123,-0.0594,0.9543,0.5682 -3.250,-0.1834,0.01819,0.01177,-0.0584,0.9453,0.6331 -3.000,-0.1516,0.01877,0.01229,-0.0582,0.9379,0.6752 -2.750,-0.1258,0.01933,0.01286,-0.0566,0.9292,0.7085 -2.500,-0.1030,0.01994,0.01348,-0.0540,0.9211,0.7399 -2.250,-0.0788,0.02040,0.01390,-0.0518,0.9132,0.7683 -2.000,-0.0585,0.02071,0.01418,-0.0492,0.9047,0.7889 -1.750,-0.0282,0.02079,0.01419,-0.0490,0.8978,0.8063 -1.500,-0.0028,0.02084,0.01414,-0.0484,0.8897,0.8205 -1.250,0.0294,0.02079,0.01401,-0.0490,0.8829,0.8342 -1.000,0.0574,0.02076,0.01391,-0.0490,0.8753,0.8474 -0.750,0.0864,0.02069,0.01377,-0.0491,0.8679,0.8606 -0.500,0.1149,0.02062,0.01364,-0.0491,0.8608,0.8741 -0.250,0.1406,0.02054,0.01352,-0.0487,0.8527,0.8878 0.000,0.1715,0.02042,0.01335,-0.0491,0.8466,0.9015 0.250,0.1953,0.02038,0.01329,-0.0485,0.8378,0.9162 0.500,0.2383,0.02011,0.01299,-0.0508,0.8339,0.9288 0.750,0.2647,0.02023,0.01312,-0.0512,0.8237,0.9449 1.000,0.3188,0.01999,0.01286,-0.0559,0.8198,0.9557 1.250,0.3655,0.02010,0.01299,-0.0602,0.8116,0.9680 1.500,0.4240,0.01990,0.01280,-0.0662,0.8064,0.9769 1.750,0.4820,0.01969,0.01262,-0.0720,0.8013,0.9859 2.000,0.5319,0.01974,0.01272,-0.0772,0.7925,0.9989 2.250,0.5439,0.01996,0.01295,-0.0752,0.7833,1.0000 2.500,0.5566,0.02010,0.01310,-0.0731,0.7746,1.0000 2.750,0.5649,0.02058,0.01362,-0.0708,0.7637,1.0000 3.000,0.5983,0.02044,0.01349,-0.0716,0.7579,1.0000 3.250,0.6188,0.02093,0.01403,-0.0713,0.7467,1.0000 3.500,0.6514,0.02092,0.01405,-0.0720,0.7395,1.0000 3.750,0.6796,0.02109,0.01430,-0.0722,0.7296,1.0000 4.000,0.7066,0.02131,0.01459,-0.0722,0.7189,1.0000 4.250,0.7443,0.02079,0.01412,-0.0728,0.7114,1.0000 4.500,0.7712,0.02080,0.01422,-0.0723,0.6983,1.0000 4.750,0.8004,0.02054,0.01403,-0.0718,0.6845,1.0000 5.000,0.8311,0.02002,0.01358,-0.0711,0.6693,1.0000 5.250,0.8632,0.01923,0.01282,-0.0703,0.6518,1.0000 5.500,0.8893,0.01864,0.01228,-0.0687,0.6278,1.0000 5.750,0.9169,0.01797,0.01160,-0.0673,0.6019,1.0000 6.000,0.9420,0.01758,0.01125,-0.0658,0.5737,1.0000 6.250,0.9639,0.01740,0.01114,-0.0641,0.5387,1.0000 6.500,0.9833,0.01736,0.01106,-0.0619,0.4889,1.0000 6.750,0.9923,0.01791,0.01113,-0.0582,0.3732,1.0000 7.000,0.9792,0.02086,0.01259,-0.0527,0.1912,1.0000 7.250,0.9772,0.02342,0.01448,-0.0490,0.1325,1.0000 7.500,0.9860,0.02514,0.01604,-0.0465,0.1096,1.0000 7.750,0.9983,0.02674,0.01752,-0.0445,0.0960,1.0000 8.000,1.0160,0.02846,0.01916,-0.0432,0.0867,1.0000 8.250,1.0403,0.03050,0.02098,-0.0429,0.0784,1.0000 8.500,1.0656,0.03205,0.02272,-0.0425,0.0725,1.0000 8.750,1.0980,0.03436,0.02493,-0.0432,0.0681,1.0000 9.000,1.1293,0.03714,0.02788,-0.0436,0.0650,1.0000 9.250,1.1513,0.03920,0.03026,-0.0428,0.0620,1.0000 9.500,1.1735,0.04176,0.03310,-0.0422,0.0601,1.0000 9.750,1.1928,0.04474,0.03643,-0.0412,0.0593,1.0000 10.000,1.2068,0.04805,0.04015,-0.0397,0.0591,1.0000 10.250,1.2141,0.05176,0.04432,-0.0377,0.0596,1.0000 10.500,1.2159,0.05558,0.04859,-0.0353,0.0600,1.0000 10.750,1.2124,0.05932,0.05273,-0.0328,0.0602,1.0000 11.000,1.2026,0.06310,0.05686,-0.0300,0.0606,1.0000 11.250,1.1867,0.06674,0.06080,-0.0270,0.0611,1.0000 11.500,1.1676,0.07071,0.06504,-0.0246,0.0618,1.0000 11.750,1.1465,0.07507,0.06963,-0.0233,0.0626,1.0000 12.000,1.1248,0.07994,0.07471,-0.0229,0.0634,1.0000 12.250,1.1032,0.08535,0.08030,-0.0236,0.0642,1.0000 12.500,1.0857,0.09127,0.08634,-0.0250,0.0652,1.0000 12.750,0.9692,0.09557,0.09108,-0.0209,0.0669,1.0000