Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca0012h-sa-100000-n5 Airfoil,naca0012h-sa Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,33.5342 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca0012h-sa-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.750,-1.0473,0.06564,0.05889,-0.0331,1.0000,0.0703 -13.500,-1.0644,0.06051,0.05361,-0.0356,1.0000,0.0709 -13.250,-1.0768,0.05651,0.04944,-0.0368,1.0000,0.0717 -13.000,-1.0876,0.05308,0.04585,-0.0370,1.0000,0.0726 -12.750,-1.0971,0.05007,0.04265,-0.0364,1.0000,0.0736 -12.500,-1.1057,0.04736,0.03972,-0.0349,1.0000,0.0748 -12.250,-1.1132,0.04488,0.03697,-0.0326,1.0000,0.0762 -12.000,-1.1178,0.04247,0.03421,-0.0301,1.0000,0.0777 -11.750,-1.1102,0.04074,0.03232,-0.0285,1.0000,0.0792 -11.500,-1.0962,0.03968,0.03128,-0.0273,1.0000,0.0807 -11.250,-1.0834,0.03851,0.03004,-0.0259,1.0000,0.0826 -11.000,-1.0715,0.03712,0.02847,-0.0244,1.0000,0.0848 -10.750,-1.0595,0.03554,0.02659,-0.0229,1.0000,0.0873 -10.500,-1.0445,0.03416,0.02506,-0.0216,1.0000,0.0895 -10.250,-1.0264,0.03329,0.02421,-0.0205,1.0000,0.0916 -10.000,-1.0087,0.03235,0.02320,-0.0193,1.0000,0.0943 -9.750,-0.9911,0.03125,0.02190,-0.0181,1.0000,0.0974 -9.500,-0.9728,0.03010,0.02054,-0.0170,1.0000,0.1004 -9.250,-0.9530,0.02932,0.01981,-0.0160,1.0000,0.1030 -9.000,-0.9331,0.02855,0.01899,-0.0149,1.0000,0.1063 -8.750,-0.9130,0.02767,0.01793,-0.0138,1.0000,0.1102 -8.500,-0.8925,0.02681,0.01700,-0.0128,1.0000,0.1136 -8.250,-0.8718,0.02616,0.01638,-0.0117,1.0000,0.1171 -8.000,-0.8507,0.02547,0.01560,-0.0107,1.0000,0.1215 -7.750,-0.8293,0.02473,0.01471,-0.0096,1.0000,0.1259 -7.500,-0.8084,0.02412,0.01417,-0.0085,1.0000,0.1298 -7.250,-0.7870,0.02354,0.01355,-0.0074,1.0000,0.1347 -7.000,-0.7652,0.02292,0.01282,-0.0064,1.0000,0.1399 -6.750,-0.7442,0.02238,0.01235,-0.0052,1.0000,0.1444 -6.500,-0.7226,0.02188,0.01181,-0.0041,1.0000,0.1502 -6.250,-0.7011,0.02135,0.01124,-0.0029,1.0000,0.1558 -6.000,-0.6799,0.02089,0.01083,-0.0017,1.0000,0.1615 -5.750,-0.6579,0.02046,0.01033,-0.0006,1.0000,0.1685 -5.500,-0.6368,0.02000,0.00995,0.0006,1.0000,0.1744 -5.250,-0.6151,0.01961,0.00956,0.0018,1.0000,0.1818 -5.000,-0.5937,0.01921,0.00920,0.0030,1.0000,0.1889 -4.750,-0.5722,0.01886,0.00887,0.0041,1.0000,0.1969 -4.500,-0.5508,0.01850,0.00855,0.0053,1.0000,0.2048 -4.250,-0.5294,0.01819,0.00828,0.0065,1.0000,0.2136 -4.000,-0.5080,0.01788,0.00802,0.0077,1.0000,0.2224 -3.750,-0.4865,0.01761,0.00777,0.0088,1.0000,0.2323 -3.500,-0.4653,0.01733,0.00758,0.0100,1.0000,0.2421 -3.250,-0.4436,0.01711,0.00739,0.0110,1.0000,0.2533 -3.000,-0.4223,0.01686,0.00723,0.0121,1.0000,0.2646 -2.750,-0.4009,0.01663,0.00708,0.0131,1.0000,0.2770 -2.500,-0.3598,0.01635,0.00691,0.0103,0.9924,0.2950 -2.250,-0.3179,0.01600,0.00670,0.0073,0.9827,0.3162 -2.000,-0.2771,0.01558,0.00651,0.0046,0.9716,0.3425 -1.750,-0.2378,0.01510,0.00636,0.0023,0.9598,0.3876 -1.500,-0.2006,0.01454,0.00627,0.0005,0.9478,0.4657 -1.250,-0.1658,0.01405,0.00624,-0.0004,0.9339,0.5601 -1.000,-0.1321,0.01369,0.00623,-0.0007,0.9168,0.6383 -0.750,-0.0993,0.01346,0.00625,-0.0007,0.8973,0.7005 -0.500,-0.0659,0.01331,0.00625,-0.0005,0.8745,0.7500 -0.250,-0.0321,0.01323,0.00625,-0.0004,0.8506,0.7902 0.000,0.0000,0.01321,0.00627,0.0000,0.8227,0.8227 0.250,0.0321,0.01323,0.00625,0.0004,0.7902,0.8506 0.500,0.0659,0.01331,0.00625,0.0005,0.7500,0.8745 0.750,0.0993,0.01346,0.00625,0.0006,0.7005,0.8973 1.000,0.1321,0.01369,0.00623,0.0007,0.6383,0.9168 1.250,0.1657,0.01405,0.00624,0.0004,0.5601,0.9339 1.500,0.2006,0.01454,0.00627,-0.0005,0.4657,0.9478 1.750,0.2378,0.01510,0.00636,-0.0023,0.3876,0.9598 2.000,0.2771,0.01558,0.00651,-0.0046,0.3425,0.9716 2.250,0.3179,0.01600,0.00670,-0.0073,0.3162,0.9827 2.500,0.3598,0.01635,0.00690,-0.0103,0.2950,0.9924 2.750,0.4008,0.01663,0.00708,-0.0131,0.2771,1.0000 3.000,0.4222,0.01686,0.00722,-0.0121,0.2646,1.0000 3.250,0.4435,0.01711,0.00738,-0.0110,0.2533,1.0000 3.500,0.4652,0.01733,0.00758,-0.0099,0.2421,1.0000 3.750,0.4864,0.01761,0.00777,-0.0088,0.2324,1.0000 4.000,0.5079,0.01788,0.00802,-0.0077,0.2224,1.0000 4.250,0.5293,0.01819,0.00827,-0.0065,0.2137,1.0000 4.500,0.5507,0.01850,0.00854,-0.0053,0.2048,1.0000 4.750,0.5722,0.01886,0.00887,-0.0041,0.1969,1.0000 5.000,0.5936,0.01921,0.00919,-0.0029,0.1889,1.0000 5.250,0.6150,0.01961,0.00955,-0.0018,0.1818,1.0000 5.500,0.6367,0.02000,0.00995,-0.0006,0.1745,1.0000 5.750,0.6579,0.02046,0.01033,0.0006,0.1685,1.0000 6.000,0.6798,0.02089,0.01083,0.0017,0.1615,1.0000 6.250,0.7010,0.02134,0.01124,0.0029,0.1558,1.0000 6.500,0.7226,0.02188,0.01181,0.0041,0.1502,1.0000 6.750,0.7441,0.02238,0.01234,0.0052,0.1444,1.0000 7.000,0.7652,0.02292,0.01282,0.0064,0.1399,1.0000 7.250,0.7869,0.02354,0.01355,0.0074,0.1347,1.0000 7.500,0.8084,0.02412,0.01417,0.0085,0.1298,1.0000 7.750,0.8293,0.02473,0.01471,0.0096,0.1259,1.0000 8.000,0.8507,0.02547,0.01560,0.0107,0.1215,1.0000 8.250,0.8718,0.02616,0.01637,0.0117,0.1171,1.0000 8.500,0.8926,0.02681,0.01700,0.0127,0.1136,1.0000 8.750,0.9131,0.02767,0.01793,0.0138,0.1102,1.0000 9.000,0.9332,0.02855,0.01899,0.0149,0.1063,1.0000 9.250,0.9531,0.02932,0.01981,0.0159,0.1030,1.0000 9.500,0.9730,0.03010,0.02054,0.0169,0.1004,1.0000 9.750,0.9912,0.03125,0.02190,0.0181,0.0974,1.0000 10.000,1.0089,0.03236,0.02320,0.0193,0.0943,1.0000 10.250,1.0266,0.03329,0.02421,0.0205,0.0916,1.0000 10.500,1.0447,0.03417,0.02506,0.0215,0.0895,1.0000 10.750,1.0597,0.03554,0.02660,0.0228,0.0873,1.0000 11.000,1.0718,0.03712,0.02848,0.0243,0.0848,1.0000 11.250,1.0838,0.03851,0.03004,0.0258,0.0826,1.0000 11.500,1.0966,0.03968,0.03128,0.0272,0.0807,1.0000 11.750,1.1107,0.04074,0.03232,0.0284,0.0791,1.0000 12.000,1.1182,0.04249,0.03423,0.0300,0.0777,1.0000 12.250,1.1137,0.04490,0.03699,0.0325,0.0762,1.0000 12.500,1.1064,0.04738,0.03973,0.0347,0.0748,1.0000 12.750,1.0980,0.05007,0.04265,0.0362,0.0736,1.0000 13.000,1.0886,0.05307,0.04584,0.0369,0.0726,1.0000 13.250,1.0782,0.05647,0.04941,0.0367,0.0716,1.0000 13.500,1.0664,0.06041,0.05349,0.0355,0.0709,1.0000 13.750,1.0519,0.06517,0.05839,0.0333,0.0702,1.0000