Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe673-il-200000-n5 Airfoil,goe673-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,73.3625 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe673-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.3273,0.08623,0.08303,-0.0433,1.0000,0.0141 -9.500,-0.3351,0.08174,0.07859,-0.0438,1.0000,0.0136 -9.250,-0.3452,0.07708,0.07399,-0.0441,1.0000,0.0131 -9.000,-0.3582,0.07233,0.06929,-0.0442,1.0000,0.0127 -8.750,-0.3749,0.06738,0.06441,-0.0441,1.0000,0.0123 -8.250,-0.4182,0.04576,0.04273,-0.0589,0.9937,0.0108 -8.000,-0.4960,0.05674,0.05346,-0.0587,0.9945,0.0108 -7.750,-0.4805,0.05117,0.04749,-0.0644,0.9884,0.0105 -7.250,-0.4446,0.04139,0.03697,-0.0717,0.9783,0.0101 -7.000,-0.4260,0.03658,0.03168,-0.0739,0.9725,0.0100 -6.500,-0.3725,0.02927,0.02333,-0.0777,0.9654,0.0101 -6.250,-0.3480,0.02659,0.02019,-0.0781,0.9598,0.0103 -6.000,-0.3211,0.02309,0.01627,-0.0793,0.9564,0.0116 -5.750,-0.2891,0.02150,0.01444,-0.0807,0.9538,0.0127 -5.500,-0.2629,0.01998,0.01270,-0.0805,0.9482,0.0132 -5.250,-0.2330,0.01858,0.01108,-0.0810,0.9440,0.0139 -5.000,-0.2017,0.01733,0.00969,-0.0819,0.9408,0.0149 -4.750,-0.1740,0.01651,0.00876,-0.0820,0.9354,0.0168 -4.500,-0.1450,0.01579,0.00793,-0.0823,0.9303,0.0184 -4.250,-0.1145,0.01466,0.00664,-0.0831,0.9266,0.0208 -4.000,-0.0878,0.01410,0.00594,-0.0830,0.9198,0.0257 -3.750,-0.0578,0.01352,0.00524,-0.0835,0.9148,0.0339 -3.500,-0.0313,0.01234,0.00466,-0.0839,0.9089,0.1643 -3.250,-0.0044,0.01165,0.00438,-0.0842,0.9024,0.2747 -3.000,0.0229,0.01096,0.00421,-0.0846,0.8969,0.4123 -2.750,0.0495,0.01069,0.00405,-0.0844,0.8891,0.4705 -2.500,0.0782,0.01047,0.00384,-0.0845,0.8830,0.5064 -2.250,0.1050,0.01027,0.00368,-0.0843,0.8747,0.5421 -2.000,0.1324,0.01007,0.00356,-0.0841,0.8673,0.5822 -1.750,0.1594,0.00991,0.00345,-0.0838,0.8591,0.6243 -1.500,0.1860,0.00978,0.00337,-0.0834,0.8502,0.6651 -1.250,0.2131,0.00964,0.00326,-0.0830,0.8422,0.7035 -1.000,0.2388,0.00952,0.00321,-0.0823,0.8325,0.7428 -0.750,0.2639,0.00939,0.00315,-0.0815,0.8229,0.7828 -0.500,0.2884,0.00926,0.00309,-0.0804,0.8135,0.8251 -0.250,0.3131,0.00916,0.00306,-0.0792,0.8032,0.8733 0.000,0.3426,0.00910,0.00301,-0.0792,0.7924,0.9242 0.250,0.3776,0.00907,0.00293,-0.0806,0.7815,0.9621 0.500,0.4154,0.00904,0.00284,-0.0829,0.7700,0.9956 0.750,0.4433,0.00908,0.00279,-0.0830,0.7577,1.0000 1.000,0.4700,0.00914,0.00278,-0.0828,0.7447,1.0000 1.250,0.4967,0.00921,0.00278,-0.0827,0.7312,1.0000 1.500,0.5234,0.00930,0.00282,-0.0825,0.7173,1.0000 1.750,0.5502,0.00940,0.00286,-0.0824,0.7030,1.0000 2.000,0.5769,0.00952,0.00292,-0.0822,0.6884,1.0000 2.250,0.6035,0.00965,0.00301,-0.0820,0.6737,1.0000 2.500,0.6301,0.00979,0.00311,-0.0818,0.6584,1.0000 2.750,0.6565,0.00995,0.00324,-0.0816,0.6427,1.0000 3.000,0.6828,0.01013,0.00341,-0.0814,0.6268,1.0000 3.250,0.7090,0.01031,0.00358,-0.0812,0.6113,1.0000 3.500,0.7353,0.01050,0.00377,-0.0810,0.5964,1.0000 3.750,0.7615,0.01071,0.00399,-0.0808,0.5818,1.0000 4.000,0.7876,0.01092,0.00426,-0.0805,0.5673,1.0000 4.250,0.8137,0.01114,0.00453,-0.0803,0.5530,1.0000 4.500,0.8378,0.01142,0.00478,-0.0796,0.5250,1.0000 4.750,0.8569,0.01195,0.00502,-0.0780,0.4614,1.0000 5.000,0.8736,0.01273,0.00543,-0.0761,0.3802,1.0000 5.250,0.8837,0.01420,0.00612,-0.0735,0.2432,1.0000 5.500,0.8846,0.01688,0.00760,-0.0699,0.0403,1.0000 5.750,0.9035,0.01781,0.00848,-0.0686,0.0231,1.0000 6.000,0.9244,0.01851,0.00934,-0.0674,0.0192,1.0000 6.250,0.9433,0.01936,0.01033,-0.0660,0.0166,1.0000 6.500,0.9554,0.02076,0.01190,-0.0635,0.0138,1.0000 6.750,0.9715,0.02173,0.01302,-0.0618,0.0130,1.0000 7.000,0.9853,0.02290,0.01431,-0.0596,0.0123,1.0000 7.250,0.9982,0.02419,0.01570,-0.0573,0.0117,1.0000 7.500,1.0114,0.02556,0.01717,-0.0551,0.0112,1.0000 7.750,1.0258,0.02677,0.01847,-0.0532,0.0103,1.0000 8.000,1.0402,0.02789,0.01966,-0.0514,0.0093,1.0000 8.250,1.0546,0.02940,0.02124,-0.0497,0.0087,1.0000 8.500,1.0736,0.03174,0.02368,-0.0486,0.0083,1.0000 8.750,1.0991,0.03503,0.02717,-0.0486,0.0080,1.0000 9.000,1.1172,0.03720,0.02960,-0.0473,0.0079,1.0000 9.250,1.1325,0.03966,0.03235,-0.0457,0.0078,1.0000 9.500,1.1438,0.04236,0.03544,-0.0436,0.0077,1.0000 9.750,1.1498,0.04516,0.03855,-0.0409,0.0077,1.0000 10.000,1.1508,0.04792,0.04162,-0.0378,0.0076,1.0000 10.250,1.1484,0.05053,0.04452,-0.0345,0.0075,1.0000 10.500,1.1438,0.05321,0.04749,-0.0313,0.0073,1.0000 10.750,1.1369,0.05612,0.05067,-0.0284,0.0071,1.0000 11.000,1.1273,0.05934,0.05415,-0.0260,0.0069,1.0000 11.250,1.1161,0.06279,0.05785,-0.0241,0.0067,1.0000 11.500,1.1026,0.06671,0.06200,-0.0228,0.0067,1.0000 11.750,1.0874,0.07102,0.06653,-0.0222,0.0066,1.0000 12.000,1.0709,0.07579,0.07151,-0.0225,0.0066,1.0000 12.250,1.0533,0.08111,0.07703,-0.0236,0.0066,1.0000 12.500,1.0347,0.08702,0.08313,-0.0257,0.0066,1.0000 12.750,1.0155,0.09358,0.08986,-0.0287,0.0067,1.0000 13.000,0.9962,0.10079,0.09722,-0.0326,0.0068,1.0000