Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa35a-il-50000-n5 Airfoil,usa35a-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,20.3922 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-usa35a-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,0.0132,0.11608,0.10894,-0.0828,0.9114,0.1490 -9.000,0.0084,0.11434,0.10722,-0.0865,0.9001,0.1537 -8.750,0.0031,0.11224,0.10516,-0.0894,0.8879,0.1546 -7.750,0.0342,0.09264,0.08534,-0.0989,0.8489,0.0970 -7.500,0.0452,0.08951,0.08219,-0.1001,0.8399,0.0957 -7.250,0.0445,0.08683,0.07952,-0.1004,0.8277,0.0949 -7.000,0.0454,0.08357,0.07624,-0.1019,0.8180,0.0943 -6.750,0.0399,0.08076,0.07343,-0.1028,0.8053,0.0937 -6.500,0.0421,0.07667,0.06928,-0.1061,0.7966,0.0930 -6.250,0.0352,0.07294,0.06549,-0.1081,0.7845,0.0918 -6.000,0.0222,0.06530,0.05746,-0.1144,0.7754,0.0892 -5.750,0.0257,0.06216,0.05415,-0.1150,0.7657,0.0889 -5.500,0.0322,0.05860,0.05034,-0.1160,0.7566,0.0889 -5.250,0.0517,0.05498,0.04641,-0.1181,0.7513,0.0899 -5.000,0.0581,0.05399,0.04538,-0.1163,0.7398,0.0911 -4.750,0.0786,0.05157,0.04271,-0.1172,0.7332,0.0930 -4.500,0.1050,0.04832,0.03899,-0.1192,0.7290,0.0948 -4.250,0.1100,0.04696,0.03734,-0.1174,0.7177,0.0956 -4.000,0.1349,0.04422,0.03393,-0.1183,0.7121,0.0978 -3.750,0.1673,0.04294,0.03265,-0.1193,0.7081,0.1006 -3.500,0.1760,0.04262,0.03218,-0.1172,0.6977,0.1028 -3.250,0.2031,0.04108,0.03021,-0.1175,0.6919,0.1058 -3.000,0.2363,0.03970,0.02860,-0.1183,0.6880,0.1094 -2.750,0.2497,0.03965,0.02850,-0.1167,0.6794,0.1124 -2.500,0.2738,0.03892,0.02746,-0.1162,0.6728,0.1165 -2.250,0.3063,0.03797,0.02643,-0.1167,0.6685,0.1211 -2.000,0.3326,0.03747,0.02575,-0.1164,0.6629,0.1266 -1.750,0.3454,0.03766,0.02590,-0.1145,0.6541,0.1304 -1.500,0.3768,0.03701,0.02518,-0.1147,0.6492,0.1372 -1.250,0.4143,0.03608,0.02413,-0.1156,0.6456,0.1452 -1.000,0.4178,0.03697,0.02505,-0.1125,0.6352,0.1502 -0.750,0.4480,0.03651,0.02452,-0.1125,0.6297,0.1596 -0.500,0.4860,0.03571,0.02362,-0.1134,0.6259,0.1734 -0.250,0.4917,0.03664,0.02457,-0.1107,0.6164,0.1827 0.000,0.5182,0.03643,0.02436,-0.1103,0.6104,0.2014 0.250,0.5547,0.03558,0.02363,-0.1112,0.6065,0.2351 0.500,0.5669,0.03609,0.02437,-0.1094,0.5987,0.2734 0.750,0.5838,0.03616,0.02493,-0.1083,0.5916,0.3587 1.000,0.6094,0.03498,0.02470,-0.1069,0.5875,0.5891 1.250,0.6517,0.03374,0.02383,-0.1070,0.5842,1.0000 1.500,0.6377,0.03602,0.02611,-0.1024,0.5728,1.0000 1.750,0.6680,0.03613,0.02593,-0.1025,0.5679,1.0000 2.000,0.7078,0.03581,0.02529,-0.1036,0.5645,1.0000 2.250,0.6902,0.03833,0.02785,-0.0987,0.5532,1.0000 2.500,0.7160,0.03868,0.02800,-0.0983,0.5478,1.0000 2.750,0.7557,0.03839,0.02745,-0.0994,0.5444,1.0000 3.250,0.7554,0.04199,0.03096,-0.0937,0.5271,1.0000 3.500,0.7926,0.04166,0.03043,-0.0943,0.5237,1.0000 3.750,0.8371,0.04105,0.02959,-0.0957,0.5213,1.0000 4.000,0.7854,0.04644,0.03518,-0.0893,0.5056,1.0000 4.250,0.8208,0.04608,0.03466,-0.0895,0.5026,1.0000 4.500,0.8626,0.04536,0.03375,-0.0903,0.5004,1.0000 5.000,0.8422,0.05160,0.04004,-0.0853,0.4810,1.0000 5.250,0.8803,0.05095,0.03925,-0.0855,0.4792,1.0000 5.750,0.8573,0.05839,0.04676,-0.0819,0.4600,1.0000 6.750,0.8239,0.07477,0.06324,-0.0789,0.4248,1.0000 7.000,0.8512,0.07481,0.06320,-0.0783,0.4226,1.0000 7.500,0.8340,0.08349,0.07196,-0.0776,0.4067,1.0000 7.750,0.8623,0.08340,0.07179,-0.0770,0.4047,1.0000 8.000,0.8252,0.09116,0.07967,-0.0771,0.3922,1.0000 8.250,0.8495,0.09149,0.07995,-0.0766,0.3892,1.0000 8.750,0.8480,0.09801,0.08651,-0.0761,0.3744,1.0000 9.000,0.8758,0.09772,0.08616,-0.0753,0.3715,1.0000 9.500,0.8745,0.10423,0.09272,-0.0750,0.3563,1.0000 9.750,0.9026,0.10384,0.09228,-0.0742,0.3538,1.0000 10.000,0.8767,0.11051,0.09904,-0.0750,0.3421,1.0000 10.250,0.8976,0.11105,0.09957,-0.0744,0.3385,1.0000 10.500,0.9250,0.11068,0.09917,-0.0736,0.3362,1.0000 10.750,0.8970,0.11787,0.10646,-0.0748,0.3239,1.0000 11.000,0.9186,0.11827,0.10684,-0.0742,0.3207,1.0000