Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca1412-il-50000-n5 Airfoil,naca1412-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,31.1514 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-naca1412-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.6491,0.09164,0.08382,-0.0263,1.0000,0.0810 -10.750,-0.7098,0.07546,0.06759,-0.0390,1.0000,0.0789 -10.500,-0.7844,0.06482,0.05664,-0.0434,1.0000,0.0766 -10.250,-0.7911,0.06154,0.05324,-0.0426,1.0000,0.0777 -9.750,-0.8008,0.05474,0.04598,-0.0403,1.0000,0.0799 -9.500,-0.8019,0.05135,0.04227,-0.0388,1.0000,0.0811 -9.250,-0.7994,0.04821,0.03879,-0.0372,1.0000,0.0829 -9.000,-0.7949,0.04525,0.03537,-0.0355,1.0000,0.0854 -8.750,-0.7860,0.04263,0.03235,-0.0339,1.0000,0.0880 -8.500,-0.7699,0.04091,0.03062,-0.0327,1.0000,0.0906 -8.250,-0.7543,0.03902,0.02854,-0.0314,1.0000,0.0933 -8.000,-0.7383,0.03709,0.02631,-0.0299,1.0000,0.0966 -7.750,-0.7217,0.03528,0.02415,-0.0285,1.0000,0.1010 -7.500,-0.7033,0.03402,0.02296,-0.0273,1.0000,0.1054 -7.250,-0.6846,0.03262,0.02140,-0.0259,1.0000,0.1108 -7.000,-0.6650,0.03120,0.01981,-0.0246,1.0000,0.1161 -6.750,-0.6463,0.03011,0.01873,-0.0233,1.0000,0.1233 -6.500,-0.6271,0.02900,0.01756,-0.0220,1.0000,0.1322 -6.250,-0.6076,0.02799,0.01644,-0.0206,1.0000,0.1431 -6.000,-0.5890,0.02704,0.01557,-0.0192,1.0000,0.1557 -5.750,-0.5700,0.02615,0.01469,-0.0179,1.0000,0.1712 -5.500,-0.5510,0.02533,0.01391,-0.0166,1.0000,0.1905 -5.250,-0.5325,0.02455,0.01326,-0.0152,1.0000,0.2122 -5.000,-0.5133,0.02384,0.01261,-0.0140,1.0000,0.2388 -4.750,-0.4939,0.02318,0.01204,-0.0127,1.0000,0.2688 -4.500,-0.4745,0.02256,0.01156,-0.0115,1.0000,0.3015 -4.250,-0.4549,0.02199,0.01114,-0.0102,1.0000,0.3362 -4.000,-0.4357,0.02148,0.01078,-0.0089,1.0000,0.3737 -3.750,-0.4167,0.02104,0.01048,-0.0074,1.0000,0.4147 -3.500,-0.3978,0.02064,0.01028,-0.0059,1.0000,0.4578 -3.250,-0.3789,0.02030,0.01012,-0.0042,1.0000,0.5039 -3.000,-0.3600,0.02002,0.01003,-0.0025,1.0000,0.5524 -2.750,-0.3411,0.01981,0.01001,-0.0006,1.0000,0.6023 -2.500,-0.3222,0.01967,0.01005,0.0014,1.0000,0.6532 -2.250,-0.3033,0.01961,0.01015,0.0036,1.0000,0.7046 -2.000,-0.2839,0.01963,0.01030,0.0057,1.0000,0.7569 -1.750,-0.2554,0.01977,0.01052,0.0061,0.9967,0.8124 -1.500,-0.2068,0.02006,0.01079,0.0028,0.9880,0.8674 -1.250,-0.1493,0.02038,0.01100,-0.0027,0.9802,0.9144 -1.000,-0.0843,0.02064,0.01113,-0.0100,0.9730,0.9517 -0.750,-0.0159,0.02077,0.01113,-0.0183,0.9651,0.9798 -0.500,0.0536,0.02078,0.01103,-0.0272,0.9574,1.0000 -0.250,0.0954,0.02070,0.01086,-0.0308,0.9421,1.0000 0.000,0.1386,0.02062,0.01072,-0.0345,0.9274,1.0000 0.250,0.1777,0.02052,0.01057,-0.0371,0.9112,1.0000 0.500,0.2129,0.02043,0.01045,-0.0388,0.8937,1.0000 0.750,0.2458,0.02035,0.01035,-0.0399,0.8754,1.0000 1.000,0.2772,0.02028,0.01026,-0.0405,0.8568,1.0000 1.250,0.3076,0.02021,0.01018,-0.0408,0.8380,1.0000 1.500,0.3371,0.02014,0.01009,-0.0408,0.8191,1.0000 1.750,0.3659,0.02008,0.01001,-0.0405,0.8001,1.0000 2.000,0.3912,0.02009,0.01001,-0.0396,0.7794,1.0000 2.250,0.4157,0.02013,0.01003,-0.0386,0.7582,1.0000 2.500,0.4408,0.02016,0.01005,-0.0375,0.7377,1.0000 2.750,0.4662,0.02020,0.01005,-0.0364,0.7175,1.0000 3.000,0.4884,0.02035,0.01019,-0.0350,0.6951,1.0000 3.250,0.5122,0.02049,0.01031,-0.0337,0.6730,1.0000 3.500,0.5363,0.02062,0.01040,-0.0324,0.6511,1.0000 3.750,0.5583,0.02084,0.01062,-0.0309,0.6269,1.0000 4.000,0.5817,0.02103,0.01076,-0.0295,0.6038,1.0000 4.250,0.6033,0.02130,0.01103,-0.0280,0.5785,1.0000 4.500,0.6261,0.02155,0.01122,-0.0265,0.5543,1.0000 4.750,0.6470,0.02188,0.01157,-0.0250,0.5275,1.0000 5.000,0.6683,0.02221,0.01186,-0.0234,0.5006,1.0000 5.250,0.6891,0.02257,0.01215,-0.0217,0.4728,1.0000 5.500,0.7088,0.02299,0.01255,-0.0201,0.4425,1.0000 5.750,0.7280,0.02345,0.01298,-0.0184,0.4115,1.0000 6.000,0.7467,0.02397,0.01344,-0.0166,0.3797,1.0000 6.250,0.7646,0.02456,0.01395,-0.0149,0.3470,1.0000 6.500,0.7816,0.02524,0.01453,-0.0131,0.3136,1.0000 6.750,0.7977,0.02604,0.01518,-0.0113,0.2804,1.0000 7.000,0.8132,0.02696,0.01597,-0.0096,0.2478,1.0000 7.250,0.8281,0.02800,0.01686,-0.0078,0.2185,1.0000 7.750,0.8578,0.03033,0.01899,-0.0047,0.1720,1.0000 8.000,0.8732,0.03160,0.02023,-0.0032,0.1542,1.0000 8.250,0.8884,0.03292,0.02151,-0.0017,0.1404,1.0000 8.500,0.9038,0.03427,0.02284,-0.0003,0.1292,1.0000 8.750,0.9214,0.03570,0.02441,0.0010,0.1198,1.0000 9.000,0.9379,0.03715,0.02582,0.0022,0.1127,1.0000 9.250,0.9550,0.03866,0.02751,0.0034,0.1056,1.0000 9.500,0.9725,0.04019,0.02895,0.0044,0.1007,1.0000 9.750,0.9911,0.04210,0.03117,0.0055,0.0965,1.0000 10.000,1.0071,0.04397,0.03325,0.0066,0.0925,1.0000 10.250,1.0230,0.04567,0.03497,0.0076,0.0890,1.0000 10.500,1.0356,0.04784,0.03733,0.0088,0.0859,1.0000 10.750,1.0426,0.05034,0.04020,0.0104,0.0832,1.0000 11.000,1.0483,0.05299,0.04314,0.0120,0.0813,1.0000 11.250,1.0502,0.05558,0.04597,0.0138,0.0797,1.0000 11.500,1.0515,0.05811,0.04869,0.0155,0.0780,1.0000 11.750,1.0560,0.06049,0.05114,0.0167,0.0763,1.0000 12.000,1.0505,0.06367,0.05447,0.0179,0.0750,1.0000 12.250,1.0301,0.06792,0.05907,0.0188,0.0745,1.0000 12.500,1.0061,0.07302,0.06447,0.0182,0.0741,1.0000 12.750,0.9779,0.07931,0.07101,0.0160,0.0741,1.0000 13.000,0.9449,0.08725,0.07917,0.0119,0.0743,1.0000 13.250,0.9069,0.09739,0.08944,0.0057,0.0748,1.0000 13.500,0.8669,0.10976,0.10191,-0.0021,0.0752,1.0000