Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rc1064c-il-100000-n5 Airfoil,rc1064c-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,41.9041 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-rc1064c-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.5948,0.09214,0.08684,-0.0261,1.0000,0.0355 -10.000,-0.6057,0.08515,0.07990,-0.0308,1.0000,0.0350 -9.750,-0.6259,0.07658,0.07133,-0.0376,1.0000,0.0343 -9.500,-0.6514,0.07012,0.06481,-0.0396,1.0000,0.0337 -9.250,-0.6748,0.06480,0.05937,-0.0385,1.0000,0.0333 -9.000,-0.6937,0.05929,0.05364,-0.0368,1.0000,0.0330 -8.750,-0.7078,0.05434,0.04842,-0.0343,1.0000,0.0328 -8.500,-0.7163,0.04999,0.04374,-0.0313,1.0000,0.0328 -8.250,-0.7194,0.04620,0.03961,-0.0283,1.0000,0.0330 -8.000,-0.7183,0.04285,0.03590,-0.0253,1.0000,0.0332 -7.750,-0.7137,0.03985,0.03253,-0.0224,1.0000,0.0336 -7.500,-0.7057,0.03731,0.02964,-0.0198,1.0000,0.0344 -7.250,-0.6949,0.03519,0.02717,-0.0173,1.0000,0.0358 -7.000,-0.6827,0.03302,0.02458,-0.0149,1.0000,0.0373 -6.750,-0.6681,0.03092,0.02203,-0.0127,1.0000,0.0382 -6.500,-0.6512,0.02904,0.01977,-0.0108,1.0000,0.0389 -6.250,-0.6329,0.02725,0.01774,-0.0092,1.0000,0.0397 -6.000,-0.6141,0.02581,0.01622,-0.0078,1.0000,0.0409 -5.750,-0.5947,0.02470,0.01501,-0.0064,1.0000,0.0424 -5.500,-0.5749,0.02376,0.01398,-0.0050,1.0000,0.0445 -5.250,-0.5547,0.02293,0.01298,-0.0037,1.0000,0.0478 -5.000,-0.5344,0.02198,0.01193,-0.0024,1.0000,0.0505 -4.750,-0.5150,0.02112,0.01108,-0.0010,1.0000,0.0534 -4.500,-0.4951,0.02040,0.01033,0.0003,1.0000,0.0574 -4.250,-0.4752,0.01974,0.00956,0.0017,1.0000,0.0626 -4.000,-0.4555,0.01915,0.00902,0.0030,1.0000,0.0713 -3.750,-0.4304,0.01854,0.00846,0.0031,0.9984,0.0835 -3.500,-0.3969,0.01798,0.00793,0.0015,0.9942,0.1054 -3.250,-0.3647,0.01739,0.00754,0.0001,0.9890,0.1372 -3.000,-0.3293,0.01718,0.00736,-0.0017,0.9839,0.1841 -2.750,-0.2995,0.01641,0.00677,-0.0027,0.9780,0.2182 -2.500,-0.2698,0.01532,0.00647,-0.0039,0.9733,0.3624 -2.250,-0.2454,0.01406,0.00653,-0.0030,0.9692,0.6610 -2.000,-0.2116,0.01403,0.00686,-0.0030,0.9653,0.7942 -1.750,-0.1702,0.01433,0.00721,-0.0045,0.9628,0.8727 -1.500,-0.1231,0.01472,0.00752,-0.0075,0.9614,0.9216 -1.250,-0.0696,0.01505,0.00774,-0.0122,0.9607,0.9496 -1.000,-0.0151,0.01518,0.00775,-0.0177,0.9596,0.9634 -0.750,0.0305,0.01518,0.00766,-0.0216,0.9554,0.9712 -0.500,0.0804,0.01509,0.00750,-0.0264,0.9517,0.9747 -0.250,0.1298,0.01499,0.00734,-0.0311,0.9479,0.9783 0.000,0.1752,0.01493,0.00726,-0.0350,0.9429,0.9832 0.250,0.2244,0.01483,0.00714,-0.0397,0.9393,0.9862 0.500,0.2688,0.01479,0.00711,-0.0434,0.9331,0.9900 0.750,0.3101,0.01480,0.00716,-0.0464,0.9254,0.9937 1.000,0.3439,0.01486,0.00727,-0.0479,0.9116,0.9983 1.250,0.3492,0.01494,0.00741,-0.0438,0.8840,1.0000 1.500,0.3782,0.01470,0.00721,-0.0438,0.8699,1.0000 1.750,0.4100,0.01437,0.00692,-0.0440,0.8568,1.0000 2.000,0.4395,0.01410,0.00665,-0.0437,0.8386,1.0000 2.250,0.4651,0.01393,0.00648,-0.0427,0.8148,1.0000 2.500,0.4875,0.01383,0.00642,-0.0412,0.7870,1.0000 2.750,0.5106,0.01374,0.00631,-0.0397,0.7568,1.0000 3.000,0.5332,0.01371,0.00623,-0.0381,0.7228,1.0000 3.250,0.5548,0.01375,0.00621,-0.0364,0.6827,1.0000 3.500,0.5758,0.01386,0.00616,-0.0345,0.6263,1.0000 3.750,0.5942,0.01418,0.00613,-0.0321,0.5442,1.0000 4.000,0.6095,0.01478,0.00623,-0.0295,0.4426,1.0000 4.250,0.6226,0.01564,0.00652,-0.0268,0.3340,1.0000 4.500,0.6363,0.01657,0.00696,-0.0245,0.2434,1.0000 4.750,0.6511,0.01745,0.00750,-0.0224,0.1779,1.0000 5.000,0.6668,0.01827,0.00806,-0.0204,0.1358,1.0000 5.250,0.6833,0.01900,0.00867,-0.0185,0.1113,1.0000 5.500,0.6999,0.01972,0.00932,-0.0166,0.0968,1.0000 5.750,0.7166,0.02043,0.01002,-0.0146,0.0866,1.0000 6.000,0.7322,0.02124,0.01078,-0.0126,0.0789,1.0000 6.250,0.7495,0.02193,0.01156,-0.0107,0.0732,1.0000 6.500,0.7661,0.02273,0.01239,-0.0088,0.0691,1.0000 6.750,0.7820,0.02374,0.01336,-0.0069,0.0658,1.0000 7.000,0.8009,0.02455,0.01430,-0.0053,0.0622,1.0000 7.250,0.8195,0.02541,0.01525,-0.0038,0.0586,1.0000 7.500,0.8382,0.02642,0.01628,-0.0024,0.0561,1.0000 7.750,0.8575,0.02780,0.01765,-0.0013,0.0540,1.0000 8.000,0.8784,0.02913,0.01914,-0.0002,0.0523,1.0000 8.250,0.8985,0.03038,0.02061,0.0010,0.0500,1.0000 8.500,0.9174,0.03163,0.02207,0.0022,0.0475,1.0000 8.750,0.9360,0.03306,0.02366,0.0035,0.0458,1.0000 9.000,0.9538,0.03466,0.02540,0.0047,0.0445,1.0000 9.250,0.9708,0.03656,0.02743,0.0059,0.0434,1.0000 9.500,0.9850,0.03903,0.03013,0.0073,0.0422,1.0000 9.750,0.9945,0.04108,0.03263,0.0097,0.0410,1.0000 10.000,1.0012,0.04337,0.03537,0.0121,0.0395,1.0000 10.250,1.0050,0.04594,0.03832,0.0146,0.0384,1.0000 10.500,1.0049,0.04878,0.04151,0.0173,0.0377,1.0000 10.750,1.0006,0.05174,0.04479,0.0202,0.0371,1.0000 11.000,0.9908,0.05470,0.04804,0.0234,0.0367,1.0000 11.250,0.9767,0.05776,0.05134,0.0265,0.0364,1.0000 11.500,0.9602,0.06116,0.05498,0.0287,0.0361,1.0000 11.750,0.9394,0.06529,0.05933,0.0297,0.0359,1.0000 12.000,0.9112,0.07087,0.06515,0.0289,0.0361,1.0000 12.250,0.8695,0.07974,0.07428,0.0244,0.0367,1.0000 12.500,0.8141,0.09524,0.08993,0.0131,0.0379,1.0000