Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca641112-il-100000 Airfoil,naca641112-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,44.1299 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-naca641112-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5899,0.09785,0.09297,-0.0138,1.0000,0.1656 -9.750,-0.5751,0.09497,0.09005,-0.0127,1.0000,0.1719 -9.500,-0.5922,0.08974,0.08492,-0.0163,1.0000,0.1807 -9.250,-0.6029,0.08560,0.08085,-0.0190,1.0000,0.1908 -9.000,-0.5898,0.08219,0.07746,-0.0176,1.0000,0.1978 -8.250,-0.7417,0.04964,0.04333,-0.0324,1.0000,0.0939 -8.000,-0.7345,0.04413,0.03695,-0.0299,1.0000,0.0762 -7.750,-0.7210,0.04019,0.03278,-0.0288,1.0000,0.0739 -7.500,-0.7074,0.03692,0.02914,-0.0272,1.0000,0.0720 -7.250,-0.6926,0.03425,0.02611,-0.0254,1.0000,0.0716 -7.000,-0.6776,0.03227,0.02383,-0.0235,1.0000,0.0733 -6.750,-0.6623,0.03041,0.02167,-0.0214,1.0000,0.0746 -6.500,-0.6463,0.02864,0.01964,-0.0194,1.0000,0.0752 -6.250,-0.6303,0.02714,0.01789,-0.0172,1.0000,0.0764 -6.000,-0.6140,0.02571,0.01630,-0.0152,1.0000,0.0783 -5.750,-0.5981,0.02414,0.01486,-0.0136,1.0000,0.0825 -5.500,-0.5829,0.02318,0.01387,-0.0116,1.0000,0.0873 -5.250,-0.5671,0.02233,0.01290,-0.0096,1.0000,0.0911 -5.000,-0.5536,0.02109,0.01186,-0.0076,1.0000,0.0976 -4.750,-0.5399,0.02030,0.01109,-0.0056,1.0000,0.1068 -4.500,-0.5263,0.01948,0.01034,-0.0038,1.0000,0.1191 -4.250,-0.5135,0.01842,0.00951,-0.0021,1.0000,0.1432 -4.000,-0.5022,0.01529,0.00886,-0.0008,0.9959,0.5510 -3.750,-0.4678,0.01613,0.00983,-0.0007,0.9864,0.6501 -3.500,-0.4329,0.01687,0.01051,-0.0011,0.9773,0.6897 -3.250,-0.3977,0.01779,0.01141,-0.0009,0.9691,0.7228 -3.000,-0.3707,0.01892,0.01256,0.0018,0.9598,0.7565 -2.750,-0.3440,0.01992,0.01354,0.0045,0.9512,0.7843 -2.500,-0.3075,0.02039,0.01392,0.0040,0.9442,0.8014 -2.250,-0.2756,0.02037,0.01375,0.0029,0.9353,0.8122 -2.000,-0.2330,0.02039,0.01365,0.0000,0.9293,0.8209 -1.750,-0.2013,0.02037,0.01354,-0.0010,0.9205,0.8294 -1.500,-0.1599,0.02029,0.01334,-0.0040,0.9143,0.8391 -1.250,-0.1293,0.02032,0.01332,-0.0045,0.9058,0.8461 -1.000,-0.0928,0.02019,0.01311,-0.0067,0.8994,0.8552 -0.750,-0.0627,0.02023,0.01311,-0.0073,0.8909,0.8621 -0.500,-0.0276,0.02011,0.01294,-0.0090,0.8844,0.8708 -0.250,0.0014,0.02017,0.01298,-0.0095,0.8760,0.8783 0.000,0.0352,0.02011,0.01290,-0.0108,0.8697,0.8871 0.250,0.0645,0.02017,0.01296,-0.0115,0.8617,0.8958 0.500,0.1005,0.02014,0.01293,-0.0132,0.8552,0.9036 0.750,0.1267,0.02022,0.01302,-0.0134,0.8477,0.9145 1.000,0.1707,0.02026,0.01310,-0.0167,0.8415,0.9209 1.250,0.2091,0.02019,0.01305,-0.0188,0.8367,0.9299 1.500,0.2482,0.02038,0.01332,-0.0218,0.8280,0.9375 1.750,0.2919,0.02028,0.01327,-0.0248,0.8228,0.9454 2.000,0.3359,0.02040,0.01350,-0.0287,0.8140,0.9530 2.250,0.3819,0.02024,0.01342,-0.0321,0.8079,0.9601 2.500,0.4231,0.02036,0.01369,-0.0356,0.7988,0.9690 2.750,0.4708,0.02013,0.01358,-0.0393,0.7922,0.9760 3.000,0.5120,0.02009,0.01369,-0.0423,0.7808,0.9852 3.250,0.5542,0.01924,0.01295,-0.0436,0.7638,0.9934 3.500,0.5863,0.01801,0.01174,-0.0423,0.7373,1.0000 3.750,0.5992,0.01707,0.01074,-0.0378,0.7138,1.0000 4.000,0.6111,0.01653,0.01023,-0.0342,0.6890,1.0000 4.250,0.6250,0.01606,0.00977,-0.0309,0.6665,1.0000 4.500,0.6384,0.01565,0.00940,-0.0277,0.6408,1.0000 4.750,0.6503,0.01527,0.00903,-0.0241,0.6064,1.0000 5.000,0.6593,0.01494,0.00864,-0.0200,0.5477,1.0000 5.250,0.6481,0.01597,0.00833,-0.0128,0.2919,1.0000 5.500,0.6394,0.01866,0.00976,-0.0081,0.1476,1.0000 5.750,0.6499,0.02014,0.01095,-0.0057,0.1199,1.0000 6.000,0.6662,0.02139,0.01207,-0.0041,0.1043,1.0000 6.250,0.6860,0.02270,0.01323,-0.0030,0.0945,1.0000 6.500,0.7099,0.02406,0.01459,-0.0022,0.0868,1.0000 6.750,0.7357,0.02589,0.01623,-0.0021,0.0799,1.0000 7.000,0.7637,0.02758,0.01808,-0.0018,0.0768,1.0000 7.250,0.7907,0.02935,0.02003,-0.0014,0.0734,1.0000 7.500,0.8157,0.03110,0.02185,-0.0012,0.0695,1.0000 7.750,0.8413,0.03382,0.02466,-0.0011,0.0674,1.0000 8.000,0.8645,0.03710,0.02822,-0.0006,0.0669,1.0000 8.250,0.8851,0.03982,0.03130,0.0004,0.0671,1.0000 8.500,0.9031,0.04228,0.03423,0.0018,0.0681,1.0000 8.750,0.9120,0.04565,0.03829,0.0040,0.0696,1.0000 9.000,0.9150,0.05007,0.04335,0.0063,0.0724,1.0000 9.250,0.9168,0.05480,0.04849,0.0080,0.0756,1.0000 9.500,0.8416,0.05152,0.04627,0.0139,0.0858,1.0000