Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-us1000root-il-50000-n5 Airfoil,us1000root-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,24.6949 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-us1000root-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.750,-0.6170,0.08981,0.08113,-0.0230,1.0000,0.2551 -11.250,-0.6549,0.07789,0.06919,-0.0264,1.0000,0.2687 -10.750,-0.6958,0.06647,0.05776,-0.0289,1.0000,0.2839 -10.500,-0.6709,0.06662,0.05780,-0.0276,1.0000,0.2872 -10.250,-0.7841,0.05332,0.04462,-0.0284,1.0000,0.2992 -10.000,-0.7771,0.05191,0.04314,-0.0270,1.0000,0.3039 -9.750,-0.8587,0.04630,0.03751,-0.0190,1.0000,0.3098 -9.500,-0.8487,0.04535,0.03649,-0.0169,1.0000,0.3143 -9.250,-0.8407,0.04432,0.03538,-0.0147,1.0000,0.3190 -9.000,-0.8686,0.04178,0.03269,-0.0089,1.0000,0.3245 -8.750,-0.8543,0.04107,0.03193,-0.0071,1.0000,0.3291 -8.500,-0.8456,0.04023,0.03103,-0.0046,1.0000,0.3342 -8.250,-0.8630,0.03839,0.02900,0.0007,1.0000,0.3400 -8.000,-0.8439,0.03800,0.02863,0.0021,1.0000,0.3443 -7.750,-0.8384,0.03724,0.02780,0.0051,1.0000,0.3495 -7.500,-0.8514,0.03588,0.02624,0.0104,1.0000,0.3551 -7.250,-0.8350,0.03562,0.02597,0.0122,1.0000,0.3594 -7.000,-0.8315,0.03496,0.02524,0.0156,1.0000,0.3644 -6.750,-0.8375,0.03396,0.02403,0.0200,1.0000,0.3700 -6.500,-0.8237,0.03369,0.02378,0.0221,1.0000,0.3744 -6.250,-0.8183,0.03312,0.02312,0.0251,1.0000,0.3798 -6.000,-0.7937,0.03242,0.02225,0.0243,0.9931,0.3865 -5.750,-0.7541,0.03196,0.02171,0.0214,0.9816,0.3939 -5.500,-0.7190,0.03128,0.02085,0.0190,0.9687,0.4016 -5.250,-0.6795,0.03080,0.02028,0.0161,0.9570,0.4093 -5.000,-0.6423,0.03022,0.01959,0.0137,0.9448,0.4172 -4.750,-0.6048,0.02972,0.01899,0.0113,0.9326,0.4256 -4.500,-0.5646,0.02927,0.01847,0.0087,0.9211,0.4339 -4.250,-0.5255,0.02869,0.01775,0.0060,0.9100,0.4439 -4.000,-0.4778,0.02830,0.01737,0.0023,0.9003,0.4530 -3.750,-0.4376,0.02789,0.01690,-0.0003,0.8878,0.4628 -3.500,-0.4012,0.02746,0.01640,-0.0021,0.8746,0.4737 -3.250,-0.3623,0.02717,0.01612,-0.0041,0.8611,0.4834 -3.000,-0.3270,0.02687,0.01580,-0.0054,0.8467,0.4940 -2.750,-0.2954,0.02658,0.01548,-0.0060,0.8315,0.5053 -2.500,-0.2663,0.02630,0.01515,-0.0062,0.8157,0.5173 -2.250,-0.2350,0.02612,0.01500,-0.0065,0.7998,0.5282 -2.000,-0.2061,0.02591,0.01480,-0.0063,0.7837,0.5402 -1.750,-0.1791,0.02571,0.01459,-0.0058,0.7673,0.5525 -1.500,-0.1558,0.02555,0.01444,-0.0047,0.7498,0.5652 -1.250,-0.1313,0.02539,0.01429,-0.0038,0.7328,0.5787 -1.000,-0.1058,0.02525,0.01415,-0.0029,0.7161,0.5927 -0.750,-0.0800,0.02512,0.01403,-0.0021,0.6997,0.6070 -0.500,-0.0537,0.02504,0.01394,-0.0014,0.6837,0.6218 -0.250,-0.0273,0.02498,0.01389,-0.0006,0.6678,0.6370 0.000,-0.0007,0.02496,0.01388,0.0001,0.6523,0.6523 0.250,0.0259,0.02498,0.01389,0.0009,0.6369,0.6678 0.500,0.0523,0.02504,0.01395,0.0017,0.6219,0.6837 0.750,0.0785,0.02512,0.01403,0.0024,0.6071,0.6997 1.000,0.1044,0.02525,0.01416,0.0032,0.5927,0.7162 1.250,0.1298,0.02539,0.01429,0.0040,0.5787,0.7328 1.500,0.1544,0.02554,0.01443,0.0050,0.5651,0.7498 1.750,0.1776,0.02570,0.01460,0.0061,0.5525,0.7675 2.000,0.2049,0.02591,0.01481,0.0066,0.5402,0.7838 2.250,0.2338,0.02611,0.01500,0.0067,0.5284,0.7999 2.500,0.2650,0.02630,0.01516,0.0064,0.5172,0.8158 2.750,0.2942,0.02657,0.01548,0.0063,0.5053,0.8316 3.000,0.3260,0.02687,0.01581,0.0056,0.4941,0.8468 3.250,0.3615,0.02716,0.01613,0.0043,0.4835,0.8612 3.500,0.4004,0.02746,0.01641,0.0023,0.4737,0.8747 3.750,0.4371,0.02788,0.01692,0.0004,0.4628,0.8879 4.000,0.4772,0.02829,0.01739,-0.0021,0.4530,0.9003 4.250,0.5247,0.02867,0.01776,-0.0058,0.4438,0.9102 4.500,0.5640,0.02926,0.01849,-0.0085,0.4339,0.9212 4.750,0.6041,0.02970,0.01901,-0.0112,0.4256,0.9327 5.000,0.6418,0.03021,0.01962,-0.0136,0.4171,0.9449 5.250,0.6788,0.03078,0.02030,-0.0160,0.4092,0.9572 5.500,0.7183,0.03127,0.02088,-0.0188,0.4015,0.9689 5.750,0.7535,0.03194,0.02175,-0.0212,0.3936,0.9818 6.000,0.7930,0.03241,0.02230,-0.0242,0.3865,0.9932 6.250,0.8174,0.03310,0.02316,-0.0248,0.3797,1.0000 6.500,0.8229,0.03368,0.02384,-0.0218,0.3744,1.0000 6.750,0.8366,0.03396,0.02410,-0.0198,0.3700,1.0000 7.000,0.8310,0.03494,0.02528,-0.0154,0.3644,1.0000 7.250,0.8345,0.03560,0.02602,-0.0120,0.3593,1.0000 7.500,0.8503,0.03590,0.02634,-0.0101,0.3552,1.0000 7.750,0.8383,0.03721,0.02785,-0.0050,0.3494,1.0000 8.000,0.8439,0.03799,0.02869,-0.0020,0.3443,1.0000 8.250,0.8636,0.03836,0.02905,-0.0006,0.3400,1.0000 8.500,0.8460,0.04023,0.03112,0.0047,0.3343,1.0000 8.750,0.8543,0.04109,0.03205,0.0072,0.3291,1.0000 9.000,0.8706,0.04172,0.03273,0.0089,0.3246,1.0000 9.250,0.8415,0.04432,0.03550,0.0147,0.3191,1.0000 9.500,0.8486,0.04541,0.03666,0.0171,0.3143,1.0000 9.750,0.8654,0.04612,0.03744,0.0185,0.3101,1.0000 10.000,0.7788,0.05190,0.04325,0.0270,0.3040,1.0000