Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sg6041-il-100000-n5 Airfoil,sg6041-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,49.7673 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-sg6041-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4378,0.09073,0.08561,-0.0389,1.0000,0.0261 -9.000,-0.4428,0.08668,0.08163,-0.0400,1.0000,0.0255 -8.750,-0.4511,0.08230,0.07734,-0.0415,1.0000,0.0249 -8.500,-0.4628,0.07783,0.07296,-0.0434,1.0000,0.0243 -8.250,-0.4846,0.07325,0.06847,-0.0449,1.0000,0.0238 -7.750,-0.5397,0.06147,0.05645,-0.0437,1.0000,0.0218 -7.500,-0.5484,0.05854,0.05344,-0.0414,1.0000,0.0216 -7.250,-0.5555,0.05531,0.05009,-0.0392,1.0000,0.0215 -7.000,-0.5591,0.05209,0.04669,-0.0371,1.0000,0.0214 -6.750,-0.5601,0.04868,0.04306,-0.0350,1.0000,0.0212 -6.500,-0.5580,0.04516,0.03924,-0.0331,1.0000,0.0211 -6.250,-0.5473,0.04100,0.03464,-0.0324,0.9984,0.0211 -6.000,-0.5237,0.03673,0.02978,-0.0337,0.9944,0.0211 -5.750,-0.4997,0.03304,0.02548,-0.0342,0.9904,0.0213 -5.500,-0.4725,0.02985,0.02161,-0.0346,0.9869,0.0219 -5.250,-0.4432,0.02810,0.01966,-0.0358,0.9839,0.0231 -5.000,-0.4161,0.02687,0.01822,-0.0362,0.9796,0.0257 -4.750,-0.3861,0.02510,0.01602,-0.0365,0.9761,0.0276 -4.500,-0.3554,0.02350,0.01428,-0.0373,0.9731,0.0294 -4.250,-0.3261,0.02246,0.01314,-0.0378,0.9694,0.0327 -4.000,-0.2985,0.02149,0.01206,-0.0379,0.9648,0.0376 -3.750,-0.2678,0.02066,0.01117,-0.0386,0.9609,0.0444 -3.500,-0.2353,0.01983,0.01033,-0.0398,0.9578,0.0553 -3.250,-0.2106,0.01918,0.00964,-0.0394,0.9519,0.0697 -3.000,-0.1807,0.01851,0.00907,-0.0401,0.9473,0.0939 -2.750,-0.1477,0.01783,0.00858,-0.0415,0.9439,0.1358 -2.500,-0.1248,0.01699,0.00819,-0.0410,0.9374,0.2316 -2.250,-0.1023,0.01552,0.00808,-0.0405,0.9327,0.5345 -2.000,-0.0744,0.01524,0.00830,-0.0395,0.9290,0.7142 -1.750,-0.0543,0.01524,0.00834,-0.0372,0.9213,0.7759 -1.500,-0.0245,0.01523,0.00832,-0.0367,0.9166,0.8244 -1.250,0.0050,0.01528,0.00839,-0.0357,0.9120,0.8776 -1.000,0.0514,0.01548,0.00856,-0.0380,0.9090,0.9344 -0.750,0.1028,0.01553,0.00847,-0.0424,0.9057,0.9538 -0.250,0.1993,0.01535,0.00804,-0.0507,0.8985,0.9685 0.000,0.2395,0.01527,0.00790,-0.0535,0.8906,0.9766 0.250,0.2854,0.01509,0.00764,-0.0571,0.8856,0.9825 0.500,0.3255,0.01496,0.00747,-0.0597,0.8768,0.9904 0.750,0.3702,0.01471,0.00719,-0.0630,0.8702,0.9958 1.000,0.3994,0.01457,0.00703,-0.0634,0.8583,1.0000 1.250,0.4219,0.01441,0.00685,-0.0623,0.8457,1.0000 1.500,0.4453,0.01426,0.00668,-0.0613,0.8327,1.0000 1.750,0.4686,0.01411,0.00653,-0.0602,0.8188,1.0000 2.000,0.4911,0.01399,0.00639,-0.0589,0.8033,1.0000 2.250,0.5135,0.01388,0.00627,-0.0576,0.7862,1.0000 2.500,0.5379,0.01377,0.00613,-0.0565,0.7677,1.0000 2.750,0.5616,0.01369,0.00605,-0.0553,0.7468,1.0000 3.000,0.5869,0.01362,0.00594,-0.0544,0.7236,1.0000 3.250,0.6117,0.01359,0.00587,-0.0534,0.6965,1.0000 3.500,0.6372,0.01361,0.00583,-0.0525,0.6648,1.0000 3.750,0.6617,0.01371,0.00581,-0.0514,0.6278,1.0000 4.000,0.6851,0.01391,0.00584,-0.0502,0.5862,1.0000 4.250,0.7068,0.01421,0.00595,-0.0488,0.5413,1.0000 4.500,0.7271,0.01461,0.00616,-0.0472,0.4949,1.0000 4.750,0.7465,0.01508,0.00642,-0.0455,0.4490,1.0000 5.000,0.7651,0.01561,0.00674,-0.0439,0.4033,1.0000 5.250,0.7835,0.01620,0.00713,-0.0422,0.3604,1.0000 5.500,0.8017,0.01681,0.00756,-0.0406,0.3203,1.0000 5.750,0.8205,0.01743,0.00802,-0.0392,0.2848,1.0000 6.000,0.8394,0.01807,0.00853,-0.0378,0.2539,1.0000 6.250,0.8584,0.01872,0.00909,-0.0365,0.2275,1.0000 6.500,0.8775,0.01938,0.00967,-0.0352,0.2044,1.0000 6.750,0.8965,0.02006,0.01029,-0.0339,0.1850,1.0000 7.000,0.9157,0.02075,0.01096,-0.0327,0.1686,1.0000 7.250,0.9346,0.02146,0.01168,-0.0314,0.1538,1.0000 7.500,0.9531,0.02221,0.01241,-0.0301,0.1412,1.0000 7.750,0.9709,0.02302,0.01321,-0.0288,0.1306,1.0000 8.000,0.9898,0.02378,0.01405,-0.0275,0.1204,1.0000 8.250,1.0076,0.02462,0.01493,-0.0262,0.1115,1.0000 8.500,1.0241,0.02552,0.01584,-0.0247,0.1038,1.0000 8.750,1.0423,0.02639,0.01684,-0.0234,0.0960,1.0000 9.000,1.0574,0.02736,0.01778,-0.0219,0.0895,1.0000 9.250,1.0749,0.02826,0.01887,-0.0206,0.0828,1.0000 9.500,1.0881,0.02930,0.01992,-0.0188,0.0777,1.0000 9.750,1.1042,0.03038,0.02120,-0.0173,0.0725,1.0000 10.000,1.1172,0.03142,0.02232,-0.0155,0.0679,1.0000 10.250,1.1295,0.03269,0.02366,-0.0138,0.0641,1.0000 10.500,1.1430,0.03399,0.02518,-0.0121,0.0599,1.0000 10.750,1.1544,0.03532,0.02661,-0.0104,0.0568,1.0000 11.000,1.1641,0.03688,0.02820,-0.0087,0.0542,1.0000 11.250,1.1748,0.03851,0.03015,-0.0070,0.0513,1.0000 11.500,1.1827,0.04013,0.03198,-0.0051,0.0485,1.0000 11.750,1.1897,0.04184,0.03384,-0.0034,0.0466,1.0000 12.000,1.1957,0.04364,0.03572,-0.0018,0.0450,1.0000 12.250,1.2005,0.04590,0.03810,-0.0003,0.0435,1.0000 12.500,1.1997,0.04840,0.04098,0.0015,0.0420,1.0000 12.750,1.1968,0.05107,0.04395,0.0030,0.0405,1.0000 13.000,1.1924,0.05389,0.04703,0.0042,0.0392,1.0000 13.250,1.1868,0.05692,0.05028,0.0051,0.0382,1.0000 13.500,1.1797,0.06024,0.05380,0.0055,0.0375,1.0000 13.750,1.1710,0.06393,0.05771,0.0054,0.0369,1.0000 14.000,1.1609,0.06796,0.06192,0.0048,0.0364,1.0000 14.250,1.1507,0.07224,0.06634,0.0038,0.0358,1.0000 14.500,1.1362,0.07742,0.07170,0.0019,0.0355,1.0000 14.750,1.1184,0.08353,0.07800,-0.0009,0.0353,1.0000 15.000,1.0855,0.09300,0.08777,-0.0067,0.0356,1.0000