Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag35-il-100000 Airfoil,ag35-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,50.4762 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-ag35-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.3782,0.10375,0.09911,-0.0110,1.0000,0.0941 -10.750,-0.3839,0.10043,0.09583,-0.0132,1.0000,0.0977 -10.500,-0.4920,0.10628,0.10143,-0.0040,1.0000,0.0894 -10.250,-0.4848,0.10288,0.09805,-0.0045,1.0000,0.0927 -10.000,-0.4846,0.09948,0.09471,-0.0073,1.0000,0.0967 -9.750,-0.5013,0.09646,0.09182,-0.0165,1.0000,0.0992 -9.500,-0.4991,0.09125,0.08666,-0.0193,1.0000,0.1008 -9.250,-0.4790,0.08816,0.08355,-0.0129,1.0000,0.1047 -9.000,-0.4756,0.08460,0.08001,-0.0157,1.0000,0.1093 -8.750,-0.4836,0.07848,0.07386,-0.0314,1.0000,0.1145 -8.500,-0.4663,0.07602,0.07150,-0.0231,1.0000,0.1186 -8.250,-0.4670,0.07092,0.06616,-0.0362,1.0000,0.1285 -8.000,-0.4502,0.06825,0.06372,-0.0282,1.0000,0.1334 -7.750,-0.4436,0.06365,0.05900,-0.0338,1.0000,0.1443 -7.500,-0.4311,0.06088,0.05616,-0.0347,1.0000,0.1557 -7.250,-0.4206,0.05714,0.05248,-0.0334,1.0000,0.1610 -7.000,-0.4099,0.05383,0.04907,-0.0344,1.0000,0.1740 -6.750,-0.3981,0.05092,0.04608,-0.0345,1.0000,0.1881 -6.500,-0.3673,0.03654,0.03023,-0.0412,1.0000,0.0898 -6.250,-0.3435,0.03169,0.02410,-0.0400,1.0000,0.0724 -6.000,-0.3244,0.02830,0.02041,-0.0392,1.0000,0.0736 -5.750,-0.3028,0.02596,0.01773,-0.0382,1.0000,0.0741 -5.500,-0.2797,0.02389,0.01530,-0.0371,1.0000,0.0744 -5.250,-0.2564,0.02221,0.01341,-0.0362,1.0000,0.0765 -5.000,-0.2330,0.02111,0.01215,-0.0353,1.0000,0.0826 -4.750,-0.2081,0.01971,0.01057,-0.0345,1.0000,0.0878 -4.500,-0.1837,0.01865,0.00952,-0.0339,1.0000,0.0961 -4.250,-0.1590,0.01770,0.00861,-0.0334,1.0000,0.1105 -4.000,-0.1336,0.01670,0.00777,-0.0331,1.0000,0.1335 -3.750,-0.1062,0.01542,0.00702,-0.0333,1.0000,0.2121 -3.500,-0.0803,0.01326,0.00681,-0.0331,1.0000,0.6051 -3.250,-0.0568,0.01253,0.00682,-0.0307,1.0000,1.0000 -3.000,-0.0351,0.01276,0.00678,-0.0303,1.0000,1.0000 -2.750,-0.0025,0.01305,0.00680,-0.0320,0.9963,1.0000 -2.500,0.0538,0.01330,0.00676,-0.0381,0.9844,1.0000 -2.250,0.1092,0.01346,0.00671,-0.0439,0.9711,1.0000 -2.000,0.1644,0.01353,0.00661,-0.0495,0.9571,1.0000 -1.750,0.2189,0.01350,0.00646,-0.0548,0.9426,1.0000 -1.500,0.2687,0.01341,0.00628,-0.0588,0.9269,1.0000 -1.250,0.3085,0.01334,0.00613,-0.0607,0.9067,1.0000 -1.000,0.3442,0.01326,0.00597,-0.0615,0.8863,1.0000 -0.750,0.3751,0.01320,0.00583,-0.0613,0.8658,1.0000 -0.500,0.4012,0.01321,0.00577,-0.0602,0.8429,1.0000 -0.250,0.4269,0.01322,0.00569,-0.0590,0.8223,1.0000 0.000,0.4515,0.01330,0.00569,-0.0577,0.8007,1.0000 0.250,0.4765,0.01338,0.00567,-0.0564,0.7814,1.0000 0.500,0.5010,0.01354,0.00575,-0.0553,0.7601,1.0000 0.750,0.5260,0.01368,0.00582,-0.0542,0.7403,1.0000 1.000,0.5512,0.01383,0.00588,-0.0532,0.7218,1.0000 1.250,0.5763,0.01403,0.00606,-0.0524,0.7012,1.0000 1.500,0.6017,0.01420,0.00618,-0.0516,0.6818,1.0000 1.750,0.6273,0.01435,0.00627,-0.0507,0.6631,1.0000 2.000,0.6526,0.01452,0.00643,-0.0500,0.6424,1.0000 2.250,0.6782,0.01472,0.00656,-0.0491,0.6234,1.0000 2.500,0.7036,0.01505,0.00682,-0.0484,0.6029,1.0000 2.750,0.7288,0.01544,0.00715,-0.0477,0.5815,1.0000 3.000,0.7540,0.01588,0.00755,-0.0470,0.5599,1.0000 3.250,0.7788,0.01629,0.00795,-0.0463,0.5368,1.0000 3.500,0.8034,0.01668,0.00834,-0.0456,0.5129,1.0000 3.750,0.8280,0.01702,0.00863,-0.0448,0.4889,1.0000 4.000,0.8519,0.01729,0.00898,-0.0439,0.4615,1.0000 4.250,0.8758,0.01754,0.00924,-0.0431,0.4332,1.0000 4.500,0.8992,0.01784,0.00951,-0.0422,0.4038,1.0000 4.750,0.9222,0.01827,0.00985,-0.0414,0.3736,1.0000 5.000,0.9447,0.01881,0.01039,-0.0405,0.3420,1.0000 5.250,0.9668,0.01947,0.01098,-0.0397,0.3112,1.0000 5.500,0.9884,0.02025,0.01169,-0.0388,0.2816,1.0000 5.750,1.0093,0.02111,0.01248,-0.0380,0.2527,1.0000 6.000,1.0297,0.02207,0.01337,-0.0371,0.2248,1.0000 6.250,1.0492,0.02312,0.01439,-0.0361,0.1979,1.0000 6.500,1.0679,0.02426,0.01545,-0.0351,0.1721,1.0000 6.750,1.0854,0.02548,0.01657,-0.0340,0.1474,1.0000 7.000,1.1021,0.02677,0.01792,-0.0327,0.1235,1.0000 7.250,1.1179,0.02843,0.01955,-0.0314,0.1034,1.0000 7.500,1.1336,0.03021,0.02139,-0.0300,0.0872,1.0000 7.750,1.1494,0.03217,0.02339,-0.0287,0.0750,1.0000 8.000,1.1668,0.03465,0.02587,-0.0276,0.0669,1.0000 8.250,1.1825,0.03651,0.02787,-0.0263,0.0600,1.0000 8.500,1.1987,0.03959,0.03115,-0.0252,0.0556,1.0000 8.750,1.2121,0.04253,0.03450,-0.0236,0.0527,1.0000 9.000,1.2234,0.04520,0.03743,-0.0222,0.0499,1.0000 9.250,1.2350,0.04872,0.04099,-0.0214,0.0471,1.0000 9.500,1.2332,0.05228,0.04502,-0.0191,0.0459,1.0000 9.750,1.2271,0.05570,0.04890,-0.0166,0.0453,1.0000 10.000,1.2154,0.05935,0.05291,-0.0140,0.0451,1.0000 10.250,1.1991,0.06309,0.05696,-0.0118,0.0451,1.0000 10.500,1.1805,0.06728,0.06143,-0.0107,0.0451,1.0000 10.750,1.1603,0.07205,0.06643,-0.0109,0.0453,1.0000 11.000,1.1389,0.07747,0.07207,-0.0123,0.0455,1.0000 11.250,1.1167,0.08363,0.07842,-0.0148,0.0458,1.0000 11.500,1.0943,0.09058,0.08552,-0.0184,0.0462,1.0000 11.750,1.0724,0.09820,0.09326,-0.0225,0.0465,1.0000 12.000,0.9687,0.12811,0.12344,-0.0444,0.0567,1.0000 12.250,0.9591,0.13593,0.13123,-0.0473,0.0574,1.0000