Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-cp-080-050-gn-100000-n5 Airfoil,cp-080-050-gn Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,29.2986 Max Cl/Cd alpha,9 Url,http://airfoiltools.com/polar/csv?polar=xf-cp-080-050-gn-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.000,-0.2526,0.12087,0.11499,-0.0490,0.9799,0.0668 -6.750,-0.2476,0.11886,0.11299,-0.0520,0.9755,0.0673 -6.500,-0.2353,0.11573,0.10988,-0.0541,0.9727,0.0677 -6.250,-0.2185,0.11238,0.10653,-0.0558,0.9706,0.0682 -6.000,-0.2090,0.10984,0.10401,-0.0565,0.9665,0.0689 -5.750,-0.1992,0.10737,0.10156,-0.0577,0.9622,0.0697 -5.500,-0.1870,0.10480,0.09899,-0.0599,0.9589,0.0707 -5.250,-0.1744,0.10223,0.09643,-0.0629,0.9558,0.0720 -5.000,-0.1788,0.10097,0.09520,-0.0633,0.9476,0.0729 -4.750,-0.1756,0.09918,0.09342,-0.0675,0.9422,0.0734 -4.500,-0.1642,0.09617,0.09044,-0.0658,0.9383,0.0739 -4.250,-0.1574,0.09393,0.08824,-0.0652,0.9325,0.0746 -4.000,-0.1427,0.09126,0.08559,-0.0671,0.9286,0.0756 -3.750,-0.1242,0.08839,0.08272,-0.0706,0.9256,0.0770 -3.500,-0.1277,0.08690,0.08127,-0.0692,0.9163,0.0778 -3.250,-0.1090,0.08419,0.07851,-0.0755,0.9111,0.0794 -2.750,-0.0915,0.07953,0.07388,-0.0764,0.8992,0.0807 -2.500,-0.0737,0.07699,0.07137,-0.0772,0.8956,0.0820 -2.250,-0.0500,0.07434,0.06870,-0.0805,0.8928,0.0840 -2.000,-0.0442,0.07273,0.06708,-0.0807,0.8846,0.0857 -1.750,-0.0128,0.07014,0.06432,-0.0889,0.8788,0.0873 -1.500,0.0054,0.06725,0.06150,-0.0885,0.8762,0.0879 -1.250,0.0288,0.06474,0.05901,-0.0896,0.8742,0.0894 -1.000,0.0301,0.06361,0.05791,-0.0870,0.8650,0.0911 -0.750,0.0733,0.06140,0.05545,-0.0954,0.8606,0.0956 -0.500,0.0928,0.05868,0.05281,-0.0951,0.8581,0.0964 -0.250,0.1195,0.05639,0.05055,-0.0965,0.8561,0.0980 0.000,0.1237,0.05540,0.04957,-0.0939,0.8469,0.0995 0.500,0.1896,0.05120,0.04520,-0.1001,0.8402,0.1061 1.000,0.2569,0.04734,0.04110,-0.1042,0.8243,0.1157 1.250,0.2928,0.04382,0.03764,-0.1053,0.8127,0.1176 1.500,0.3355,0.04093,0.03471,-0.1075,0.8025,0.1221 1.750,0.3648,0.03934,0.03292,-0.1079,0.7890,0.1281 2.000,0.3922,0.03707,0.03072,-0.1075,0.7754,0.1313 2.250,0.4241,0.03557,0.02904,-0.1078,0.7569,0.1414 2.500,0.4477,0.03361,0.02709,-0.1065,0.7292,0.1440 2.750,0.4968,0.03119,0.02419,-0.1087,0.6436,0.1493 3.000,0.4922,0.03357,0.02386,-0.1028,0.1640,0.1563 3.250,0.5060,0.03346,0.02332,-0.1007,0.0979,0.1572 3.750,0.5653,0.02981,0.01869,-0.0994,0.0867,0.0917 4.000,0.5869,0.02929,0.01803,-0.0979,0.0832,0.0907 4.250,0.6080,0.02889,0.01748,-0.0963,0.0808,0.0901 4.500,0.6273,0.02876,0.01723,-0.0945,0.0788,0.0908 4.750,0.6471,0.02867,0.01705,-0.0928,0.0773,0.0919 5.000,0.6666,0.02862,0.01691,-0.0909,0.0758,0.0927 5.250,0.6855,0.02863,0.01683,-0.0890,0.0741,0.0926 5.500,0.7034,0.02875,0.01684,-0.0870,0.0724,0.0926 5.750,0.7205,0.02899,0.01696,-0.0849,0.0711,0.0928 6.000,0.7368,0.02934,0.01719,-0.0827,0.0699,0.0932 6.250,0.7555,0.02962,0.01741,-0.0808,0.0690,0.0942 6.500,0.7751,0.02998,0.01769,-0.0790,0.0682,0.0958 6.750,0.7963,0.03035,0.01805,-0.0777,0.0675,0.0969 7.000,0.8189,0.03076,0.01842,-0.0764,0.0668,0.0976 7.250,0.8439,0.03120,0.01881,-0.0756,0.0661,0.0984 7.500,0.8719,0.03170,0.01925,-0.0752,0.0655,0.0994 7.750,0.9039,0.03229,0.01975,-0.0754,0.0647,0.1008 8.000,0.9364,0.03295,0.02032,-0.0758,0.0638,0.1026 8.250,0.9728,0.03382,0.02105,-0.0770,0.0626,0.1059 8.500,1.0053,0.03463,0.02192,-0.0774,0.0618,0.1097 8.750,1.0386,0.03555,0.02288,-0.0779,0.0611,0.1131 9.000,1.0735,0.03664,0.02404,-0.0788,0.0606,0.1171 9.250,1.1080,0.03789,0.02538,-0.0796,0.0602,0.1234 9.500,1.1397,0.03922,0.02684,-0.0801,0.0598,0.1358 9.750,1.1681,0.04051,0.02840,-0.0800,0.0593,0.1798 10.250,1.2230,0.04250,0.03163,-0.0799,0.0579,1.0000 10.500,1.2445,0.04396,0.03311,-0.0788,0.0571,1.0000 10.750,1.2661,0.04556,0.03473,-0.0778,0.0566,1.0000 11.000,1.2868,0.04733,0.03656,-0.0766,0.0562,1.0000 11.250,1.3067,0.04924,0.03854,-0.0754,0.0559,1.0000 11.500,1.3256,0.05131,0.04071,-0.0742,0.0557,1.0000 11.750,1.3406,0.05349,0.04302,-0.0724,0.0556,1.0000 12.000,1.3485,0.05560,0.04537,-0.0694,0.0554,1.0000 12.250,1.3530,0.05779,0.04784,-0.0661,0.0554,1.0000 12.500,1.3531,0.06001,0.05033,-0.0623,0.0552,1.0000 12.750,1.3470,0.06221,0.05284,-0.0578,0.0551,1.0000 13.000,1.3371,0.06448,0.05540,-0.0529,0.0548,1.0000 13.250,1.3247,0.06690,0.05810,-0.0482,0.0546,1.0000 13.500,1.3108,0.06955,0.06102,-0.0439,0.0544,1.0000 13.750,1.2954,0.07243,0.06415,-0.0401,0.0543,1.0000 14.000,1.2784,0.07561,0.06758,-0.0367,0.0542,1.0000 14.250,1.2599,0.07912,0.07131,-0.0338,0.0542,1.0000 14.500,1.2402,0.08298,0.07540,-0.0316,0.0543,1.0000 14.750,1.2185,0.08728,0.07992,-0.0300,0.0544,1.0000 15.000,1.1949,0.09208,0.08493,-0.0293,0.0546,1.0000 15.250,1.1704,0.09742,0.09046,-0.0295,0.0548,1.0000 15.500,1.1454,0.10334,0.09656,-0.0308,0.0550,1.0000 15.750,1.1218,0.10973,0.10312,-0.0330,0.0552,1.0000 16.000,1.1036,0.11606,0.10956,-0.0356,0.0554,1.0000