Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe746-il-100000-n5 Airfoil,goe746-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,49.1395 Max Cl/Cd alpha,8.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe746-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.3801,0.10460,0.09973,0.0119,0.6640,0.0406 -8.000,-0.3838,0.10261,0.09780,0.0074,0.6582,0.0413 -7.750,-0.3857,0.10028,0.09547,0.0038,0.6532,0.0415 -7.500,-0.3805,0.09731,0.09243,0.0002,0.6490,0.0417 -7.250,-0.3724,0.09250,0.08764,-0.0010,0.6433,0.0421 -7.000,-0.3607,0.08779,0.08291,0.0020,0.6378,0.0434 -6.750,-0.3512,0.08451,0.07957,0.0016,0.6335,0.0447 -6.500,-0.3410,0.08131,0.07636,-0.0002,0.6281,0.0463 -6.250,-0.3300,0.07817,0.07315,-0.0027,0.6235,0.0494 -6.000,-0.3096,0.07588,0.07053,-0.0119,0.6202,0.0529 -5.750,-0.3018,0.07086,0.06560,-0.0102,0.6159,0.0543 -5.500,-0.2884,0.06770,0.06241,-0.0099,0.6109,0.0563 -5.250,-0.2719,0.06465,0.05925,-0.0111,0.6067,0.0591 -5.000,-0.2406,0.06261,0.05657,-0.0170,0.6036,0.0650 -4.750,-0.2293,0.05763,0.05178,-0.0164,0.5989,0.0665 -4.500,-0.2136,0.05503,0.04918,-0.0158,0.5945,0.0705 -4.250,-0.1855,0.05234,0.04596,-0.0185,0.5911,0.0788 -4.000,-0.1691,0.04900,0.04261,-0.0180,0.5880,0.0806 -3.750,-0.1477,0.04642,0.03993,-0.0182,0.5832,0.0834 -3.250,-0.0932,0.03938,0.03199,-0.0185,0.5760,0.0629 -3.000,-0.0662,0.03559,0.02753,-0.0176,0.5734,0.0521 -2.750,-0.0418,0.03333,0.02505,-0.0174,0.5695,0.0510 -2.500,-0.0153,0.03150,0.02275,-0.0168,0.5654,0.0520 -2.250,0.0108,0.02987,0.02071,-0.0162,0.5617,0.0523 -2.000,0.0366,0.02822,0.01875,-0.0157,0.5586,0.0517 -1.750,0.0636,0.02685,0.01709,-0.0154,0.5549,0.0513 -1.500,0.0912,0.02569,0.01566,-0.0151,0.5509,0.0512 -1.250,0.1189,0.02467,0.01436,-0.0148,0.5473,0.0512 -1.000,0.1467,0.02399,0.01336,-0.0143,0.5441,0.0525 -0.750,0.1743,0.02311,0.01231,-0.0141,0.5409,0.0540 -0.500,0.2027,0.02244,0.01156,-0.0142,0.5365,0.0542 -0.250,0.2307,0.02184,0.01088,-0.0141,0.5329,0.0544 0.000,0.2582,0.02130,0.01026,-0.0138,0.5297,0.0549 0.250,0.2854,0.02082,0.00970,-0.0135,0.5270,0.0556 0.500,0.3128,0.02054,0.00948,-0.0135,0.5225,0.0566 0.750,0.3400,0.02030,0.00924,-0.0134,0.5186,0.0579 1.000,0.3681,0.02011,0.00898,-0.0133,0.5153,0.0599 1.250,0.3964,0.02000,0.00874,-0.0131,0.5124,0.0644 1.500,0.4249,0.01996,0.00871,-0.0134,0.5083,0.0693 1.750,0.4528,0.02000,0.00873,-0.0135,0.5040,0.0743 2.000,0.4798,0.01995,0.00866,-0.0133,0.5004,0.0845 2.500,0.6059,0.01824,0.00891,-0.0279,0.4911,1.0000 2.750,0.6311,0.01848,0.00908,-0.0275,0.4868,1.0000 3.000,0.6561,0.01863,0.00913,-0.0269,0.4833,1.0000 3.250,0.6811,0.01882,0.00924,-0.0263,0.4797,1.0000 3.500,0.7060,0.01918,0.00966,-0.0262,0.4738,1.0000 3.750,0.7309,0.01933,0.00976,-0.0256,0.4694,1.0000 4.000,0.7556,0.01938,0.00970,-0.0249,0.4660,1.0000 4.250,0.7802,0.01982,0.01026,-0.0248,0.4595,1.0000 4.500,0.8048,0.02000,0.01045,-0.0243,0.4548,1.0000 4.750,0.8296,0.02006,0.01044,-0.0235,0.4514,1.0000 5.000,0.8535,0.02053,0.01105,-0.0234,0.4451,1.0000 5.250,0.8778,0.02074,0.01129,-0.0229,0.4401,1.0000 5.500,0.9026,0.02079,0.01132,-0.0222,0.4365,1.0000 5.750,0.9259,0.02131,0.01201,-0.0220,0.4298,1.0000 6.000,0.9500,0.02150,0.01226,-0.0215,0.4248,1.0000 6.250,0.9746,0.02155,0.01231,-0.0208,0.4209,1.0000 6.500,0.9969,0.02214,0.01311,-0.0206,0.4134,1.0000 6.750,1.0211,0.02224,0.01325,-0.0199,0.4085,1.0000 7.000,1.0437,0.02267,0.01383,-0.0195,0.4022,1.0000 7.250,1.0665,0.02300,0.01430,-0.0190,0.3960,1.0000 7.500,1.0907,0.02308,0.01442,-0.0183,0.3914,1.0000 7.750,1.1112,0.02373,0.01530,-0.0179,0.3832,1.0000 8.000,1.1348,0.02372,0.01536,-0.0171,0.3762,1.0000 8.250,1.1560,0.02387,0.01564,-0.0164,0.3642,1.0000 8.500,1.1764,0.02394,0.01576,-0.0156,0.3481,1.0000 8.750,1.1937,0.02446,0.01639,-0.0149,0.3295,1.0000 9.000,1.2105,0.02505,0.01707,-0.0141,0.3132,1.0000 9.250,1.2236,0.02582,0.01783,-0.0131,0.2915,1.0000 9.500,1.2305,0.02716,0.01913,-0.0121,0.2661,1.0000 9.750,1.2323,0.02889,0.02082,-0.0110,0.2460,1.0000 10.000,1.2252,0.03130,0.02322,-0.0099,0.2302,1.0000 10.250,1.2125,0.03428,0.02614,-0.0089,0.2131,1.0000 10.500,1.2018,0.03747,0.02929,-0.0085,0.1957,1.0000 10.750,1.1896,0.04105,0.03279,-0.0083,0.1756,1.0000 11.250,1.1574,0.04943,0.04084,-0.0086,0.1103,1.0000 11.500,1.1363,0.05438,0.04553,-0.0091,0.0846,1.0000 11.750,1.1141,0.05963,0.05054,-0.0097,0.0487,1.0000 12.000,1.0990,0.06435,0.05515,-0.0104,0.0390,1.0000 12.250,1.0900,0.06859,0.05940,-0.0111,0.0349,1.0000 12.500,1.0828,0.07274,0.06363,-0.0119,0.0320,1.0000 12.750,1.0776,0.07675,0.06777,-0.0127,0.0306,1.0000 13.000,1.0714,0.08105,0.07221,-0.0137,0.0293,1.0000 13.250,1.0664,0.08525,0.07654,-0.0148,0.0287,1.0000 13.500,1.0584,0.09005,0.08148,-0.0161,0.0277,1.0000 13.750,1.0506,0.09491,0.08648,-0.0176,0.0269,1.0000