Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e329-il-200000-n5 Airfoil,e329-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,66.6372 Max Cl/Cd alpha,9.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e329-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.3324,0.08994,0.08661,-0.0353,1.0000,0.0240 -8.750,-0.3361,0.08607,0.08280,-0.0370,1.0000,0.0241 -8.500,-0.3428,0.08200,0.07879,-0.0391,1.0000,0.0243 -8.250,-0.3542,0.07787,0.07472,-0.0413,1.0000,0.0242 -8.000,-0.3608,0.07356,0.07041,-0.0442,0.9898,0.0242 -7.750,-0.3594,0.06871,0.06548,-0.0481,0.9473,0.0245 -7.500,-0.3366,0.06232,0.05886,-0.0561,0.9091,0.0249 -7.000,-0.3110,0.04704,0.04263,-0.0622,0.8413,0.0138 -6.750,-0.2973,0.04438,0.03969,-0.0620,0.8108,0.0135 -6.500,-0.2863,0.04173,0.03676,-0.0607,0.7854,0.0131 -6.250,-0.2762,0.03871,0.03339,-0.0587,0.7643,0.0127 -5.750,-0.2558,0.02951,0.02297,-0.0523,0.7315,0.0109 -5.500,-0.2386,0.02737,0.02045,-0.0505,0.7155,0.0109 -5.250,-0.2195,0.02527,0.01793,-0.0488,0.7005,0.0108 -5.000,-0.1983,0.02316,0.01535,-0.0472,0.6866,0.0109 -4.750,-0.1750,0.02168,0.01351,-0.0461,0.6727,0.0109 -4.500,-0.1507,0.02029,0.01182,-0.0451,0.6592,0.0111 -4.250,-0.1262,0.01931,0.01066,-0.0444,0.6466,0.0114 -4.000,-0.1016,0.01850,0.00970,-0.0437,0.6347,0.0119 -3.500,-0.0529,0.01702,0.00792,-0.0420,0.6116,0.0132 -3.250,-0.0292,0.01649,0.00729,-0.0411,0.6009,0.0145 -3.000,-0.0055,0.01613,0.00684,-0.0403,0.5908,0.0166 -2.750,0.0174,0.01561,0.00625,-0.0393,0.5809,0.0183 -2.500,0.0403,0.01520,0.00576,-0.0382,0.5717,0.0201 -2.250,0.0633,0.01481,0.00530,-0.0373,0.5622,0.0229 -2.000,0.0867,0.01451,0.00496,-0.0364,0.5534,0.0300 -1.750,0.1096,0.01416,0.00460,-0.0354,0.5448,0.0445 -1.500,0.1320,0.01377,0.00433,-0.0344,0.5370,0.0856 -1.250,0.1401,0.01217,0.00399,-0.0315,0.5300,0.4190 -1.000,0.1423,0.01163,0.00484,-0.0247,0.5241,0.8132 -0.750,0.1630,0.01210,0.00525,-0.0220,0.5161,0.8502 -0.250,0.2082,0.01286,0.00581,-0.0176,0.5023,0.8891 0.000,0.2366,0.01321,0.00603,-0.0167,0.4955,0.9032 0.250,0.2611,0.01327,0.00597,-0.0159,0.4889,0.9092 0.500,0.2882,0.01328,0.00587,-0.0158,0.4822,0.9108 0.750,0.3146,0.01332,0.00577,-0.0156,0.4766,0.9127 1.000,0.3406,0.01332,0.00571,-0.0154,0.4703,0.9147 1.250,0.3653,0.01334,0.00563,-0.0149,0.4645,0.9170 1.500,0.3889,0.01337,0.00556,-0.0142,0.4592,0.9196 1.750,0.4118,0.01337,0.00552,-0.0134,0.4535,0.9220 2.000,0.4380,0.01342,0.00549,-0.0132,0.4484,0.9235 2.250,0.4652,0.01349,0.00549,-0.0132,0.4436,0.9251 2.500,0.4921,0.01354,0.00551,-0.0132,0.4380,0.9267 2.750,0.5182,0.01361,0.00553,-0.0130,0.4329,0.9283 3.000,0.5439,0.01370,0.00555,-0.0128,0.4285,0.9301 3.250,0.5693,0.01376,0.00562,-0.0125,0.4233,0.9322 3.500,0.5936,0.01383,0.00567,-0.0120,0.4184,0.9348 4.000,0.6443,0.01403,0.00582,-0.0115,0.4097,0.9388 4.250,0.6714,0.01413,0.00593,-0.0116,0.4047,0.9404 4.500,0.6979,0.01425,0.00602,-0.0116,0.4004,0.9422 4.750,0.7242,0.01439,0.00617,-0.0116,0.3963,0.9442 5.000,0.7497,0.01450,0.00632,-0.0114,0.3913,0.9465 5.250,0.7742,0.01462,0.00645,-0.0110,0.3868,0.9495 5.500,0.7995,0.01479,0.00659,-0.0108,0.3829,0.9520 5.750,0.8274,0.01493,0.00681,-0.0112,0.3778,0.9539 6.000,0.8547,0.01508,0.00701,-0.0114,0.3730,0.9561 6.250,0.8814,0.01526,0.00719,-0.0116,0.3686,0.9585 6.500,0.9074,0.01544,0.00742,-0.0116,0.3639,0.9613 6.750,0.9329,0.01560,0.00766,-0.0115,0.3587,0.9643 7.000,0.9614,0.01581,0.00789,-0.0121,0.3538,0.9664 7.250,0.9896,0.01603,0.00818,-0.0127,0.3488,0.9689 7.500,1.0171,0.01623,0.00847,-0.0131,0.3431,0.9721 7.750,1.0442,0.01646,0.00874,-0.0135,0.3379,0.9756 8.000,1.0742,0.01671,0.00910,-0.0145,0.3316,0.9781 8.250,1.1030,0.01696,0.00942,-0.0153,0.3254,0.9811 8.500,1.1306,0.01724,0.00977,-0.0159,0.3191,0.9849 8.750,1.1594,0.01751,0.01015,-0.0168,0.3116,0.9887 9.250,1.2048,0.01808,0.01088,-0.0162,0.2973,1.0000 9.500,1.2169,0.01835,0.01118,-0.0138,0.2911,1.0000 9.750,1.2328,0.01865,0.01157,-0.0122,0.2834,1.0000 10.000,1.2484,0.01901,0.01197,-0.0106,0.2761,1.0000 10.250,1.2645,0.01939,0.01245,-0.0092,0.2674,1.0000 10.500,1.2782,0.01982,0.01293,-0.0073,0.2590,1.0000 10.750,1.2894,0.02032,0.01346,-0.0052,0.2501,1.0000 11.000,1.3016,0.02086,0.01408,-0.0033,0.2405,1.0000 11.250,1.3116,0.02152,0.01479,-0.0013,0.2310,1.0000 11.500,1.3190,0.02233,0.01561,0.0009,0.2208,1.0000 11.750,1.3265,0.02322,0.01655,0.0029,0.2099,1.0000 12.000,1.3321,0.02427,0.01765,0.0048,0.1992,1.0000 12.250,1.3355,0.02555,0.01896,0.0067,0.1891,1.0000 12.500,1.3361,0.02711,0.02054,0.0083,0.1789,1.0000 12.750,1.3363,0.02889,0.02236,0.0097,0.1685,1.0000 13.000,1.3365,0.03083,0.02437,0.0107,0.1592,1.0000 13.250,1.3335,0.03317,0.02674,0.0115,0.1504,1.0000 13.500,1.3291,0.03581,0.02942,0.0120,0.1418,1.0000 13.750,1.3260,0.03850,0.03217,0.0122,0.1337,1.0000 14.000,1.3191,0.04166,0.03536,0.0122,0.1268,1.0000 14.250,1.3136,0.04480,0.03858,0.0120,0.1194,1.0000 14.500,1.3058,0.04829,0.04212,0.0116,0.1136,1.0000 14.750,1.2991,0.05176,0.04567,0.0112,0.1073,1.0000 15.000,1.2896,0.05565,0.04961,0.0104,0.1021,1.0000 15.250,1.2833,0.05931,0.05337,0.0097,0.0965,1.0000 15.500,1.2729,0.06359,0.05767,0.0086,0.0919,1.0000 15.750,1.2678,0.06731,0.06150,0.0076,0.0869,1.0000 16.000,1.2588,0.07165,0.06589,0.0063,0.0823,1.0000 16.250,1.2519,0.07580,0.07011,0.0050,0.0783,1.0000 16.500,1.2455,0.07996,0.07435,0.0036,0.0740,1.0000 16.750,1.2363,0.08461,0.07905,0.0019,0.0704,1.0000 17.000,1.2318,0.08868,0.08321,0.0005,0.0668,1.0000