Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-kc135winglet-il-200000 Airfoil,kc135winglet-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,85.6 Max Cl/Cd alpha,3.25 Url,http://airfoiltools.com/polar/csv?polar=xf-kc135winglet-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.4314,0.09966,0.09605,-0.0367,1.0000,0.0287 -8.750,-0.4344,0.09664,0.09309,-0.0377,1.0000,0.0288 -8.500,-0.4380,0.09090,0.08742,-0.0361,1.0000,0.0295 -8.250,-0.4305,0.08803,0.08456,-0.0331,1.0000,0.0307 -8.000,-0.4336,0.08567,0.08225,-0.0318,1.0000,0.0314 -7.750,-0.4398,0.08333,0.07998,-0.0306,1.0000,0.0321 -7.500,-0.4440,0.08061,0.07732,-0.0307,1.0000,0.0328 -7.250,-0.4483,0.07758,0.07433,-0.0318,1.0000,0.0336 -7.000,-0.4508,0.07392,0.07072,-0.0346,1.0000,0.0342 -6.750,-0.4500,0.07002,0.06680,-0.0377,1.0000,0.0350 -6.500,-0.4450,0.06599,0.06272,-0.0409,1.0000,0.0361 -6.250,-0.4331,0.06171,0.05831,-0.0451,1.0000,0.0377 -6.000,-0.4067,0.05904,0.05512,-0.0512,1.0000,0.0396 -5.750,-0.3916,0.05230,0.04819,-0.0550,1.0000,0.0406 -5.500,-0.3790,0.04824,0.04424,-0.0555,1.0000,0.0419 -5.250,-0.3611,0.04536,0.04132,-0.0566,1.0000,0.0437 -5.000,-0.3363,0.04239,0.03819,-0.0589,0.9999,0.0466 -3.000,-0.0008,0.02102,0.01378,-0.0868,0.9880,0.0409 -2.750,0.0383,0.01901,0.01166,-0.0887,0.9876,0.0341 -2.500,0.0782,0.01774,0.01020,-0.0905,0.9866,0.0308 -2.250,0.1181,0.01689,0.00940,-0.0932,0.9855,0.0345 -2.000,0.1602,0.01609,0.00861,-0.0962,0.9845,0.0359 -1.750,0.1998,0.01548,0.00796,-0.0989,0.9813,0.0374 -1.500,0.2412,0.01503,0.00739,-0.1019,0.9782,0.0418 -1.250,0.2912,0.01322,0.00792,-0.1069,0.9809,0.7536 -1.000,0.3119,0.01362,0.00845,-0.1039,0.9751,0.8147 -0.750,0.3370,0.01377,0.00863,-0.1023,0.9712,0.8474 -0.500,0.3542,0.01382,0.00872,-0.0994,0.9640,0.8725 -0.250,0.3917,0.01381,0.00865,-0.1016,0.9606,0.8809 0.000,0.4235,0.01374,0.00857,-0.1025,0.9550,0.8876 0.250,0.4624,0.01355,0.00836,-0.1047,0.9481,0.8945 0.500,0.5037,0.01309,0.00790,-0.1069,0.9404,0.9000 0.750,0.5520,0.01234,0.00717,-0.1101,0.9314,0.9049 1.000,0.5898,0.01162,0.00646,-0.1110,0.9178,0.9102 1.250,0.6204,0.01109,0.00595,-0.1105,0.9040,0.9164 1.500,0.6483,0.01079,0.00569,-0.1099,0.8913,0.9235 1.750,0.6742,0.01053,0.00549,-0.1089,0.8787,0.9315 2.000,0.6996,0.01024,0.00523,-0.1077,0.8635,0.9400 2.250,0.7246,0.00992,0.00493,-0.1063,0.8446,0.9504 2.500,0.7471,0.00967,0.00471,-0.1045,0.8206,0.9663 2.750,0.7759,0.00946,0.00451,-0.1041,0.7908,1.0000 3.000,0.8066,0.00950,0.00447,-0.1044,0.7472,1.0000 3.250,0.8346,0.00975,0.00441,-0.1039,0.6563,1.0000 3.500,0.8513,0.01122,0.00470,-0.1017,0.4431,1.0000 3.750,0.8690,0.01306,0.00555,-0.1008,0.2632,1.0000 4.000,0.8923,0.01440,0.00633,-0.1008,0.1785,1.0000 4.250,0.9182,0.01537,0.00709,-0.1009,0.1485,1.0000 4.500,0.9446,0.01622,0.00786,-0.1010,0.1323,1.0000 4.750,0.9706,0.01709,0.00867,-0.1010,0.1208,1.0000 5.000,0.9961,0.01797,0.00945,-0.1010,0.1100,1.0000 5.250,1.0233,0.01850,0.01008,-0.1011,0.1017,1.0000 5.500,1.0482,0.01947,0.01101,-0.1009,0.0947,1.0000 5.750,1.0743,0.02009,0.01171,-0.1008,0.0876,1.0000 6.000,1.0988,0.02110,0.01273,-0.1005,0.0807,1.0000 6.250,1.1240,0.02176,0.01347,-0.1002,0.0733,1.0000 6.500,1.1480,0.02303,0.01484,-0.0997,0.0660,1.0000 6.750,1.1719,0.02407,0.01588,-0.0992,0.0596,1.0000 7.000,1.1963,0.02592,0.01789,-0.0986,0.0551,1.0000 7.250,1.2210,0.02738,0.01954,-0.0980,0.0518,1.0000 7.500,1.2445,0.02865,0.02090,-0.0974,0.0490,1.0000 7.750,1.2669,0.03188,0.02429,-0.0970,0.0462,1.0000 8.000,1.2885,0.03367,0.02644,-0.0959,0.0453,1.0000 8.250,1.3080,0.03613,0.02932,-0.0945,0.0442,1.0000 8.500,1.3240,0.03925,0.03289,-0.0927,0.0434,1.0000 8.750,1.3364,0.04248,0.03660,-0.0905,0.0422,1.0000 9.000,1.3474,0.04527,0.03975,-0.0883,0.0406,1.0000 9.250,1.3569,0.04800,0.04277,-0.0862,0.0393,1.0000 9.500,1.3733,0.04878,0.04351,-0.0853,0.0373,1.0000 10.000,1.3560,0.05788,0.05347,-0.0780,0.0352,1.0000 10.250,1.3410,0.06188,0.05789,-0.0737,0.0346,1.0000 10.500,1.3178,0.06587,0.06218,-0.0689,0.0345,1.0000 10.750,1.2924,0.07025,0.06682,-0.0653,0.0345,1.0000 11.000,1.2657,0.07534,0.07212,-0.0633,0.0347,1.0000 11.250,1.2390,0.08114,0.07811,-0.0631,0.0350,1.0000 11.500,1.2121,0.08787,0.08496,-0.0646,0.0354,1.0000 11.750,1.1865,0.09580,0.09297,-0.0674,0.0359,1.0000