Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa35-il-50000-n5 Airfoil,usa35-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,20.6215 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-usa35-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,0.0123,0.11600,0.10886,-0.0826,0.9109,0.1490 -9.000,0.0136,0.11390,0.10677,-0.0861,0.9008,0.1546 -8.750,0.0017,0.11243,0.10533,-0.0894,0.8878,0.1560 -8.500,0.0349,0.10739,0.10028,-0.0900,0.8817,0.1580 -8.250,0.0500,0.10429,0.09718,-0.0907,0.8715,0.1597 -7.750,0.0273,0.09251,0.08522,-0.0993,0.8480,0.0989 -7.500,0.0447,0.08932,0.08199,-0.1004,0.8403,0.0968 -7.250,0.0439,0.08680,0.07948,-0.1003,0.8274,0.0957 -7.000,0.0462,0.08336,0.07601,-0.1022,0.8187,0.0950 -6.750,0.0393,0.08069,0.07336,-0.1028,0.8053,0.0944 -6.500,0.0430,0.07650,0.06908,-0.1064,0.7975,0.0938 -6.250,0.0352,0.07314,0.06568,-0.1078,0.7846,0.0929 -6.000,0.0343,0.06741,0.05973,-0.1125,0.7768,0.0915 -5.750,0.0221,0.06215,0.05412,-0.1147,0.7648,0.0899 -5.500,0.0329,0.05830,0.04999,-0.1164,0.7572,0.0898 -5.250,0.0475,0.05501,0.04641,-0.1176,0.7503,0.0905 -5.000,0.0578,0.05390,0.04527,-0.1163,0.7398,0.0918 -4.750,0.0808,0.05144,0.04255,-0.1175,0.7343,0.0937 -4.500,0.0947,0.04929,0.04008,-0.1174,0.7262,0.0952 -4.250,0.1103,0.04710,0.03750,-0.1172,0.7180,0.0964 -4.000,0.1380,0.04426,0.03401,-0.1186,0.7131,0.0983 -3.750,0.1580,0.04340,0.03310,-0.1179,0.7058,0.1004 -3.500,0.1756,0.04271,0.03228,-0.1170,0.6977,0.1029 -3.250,0.2058,0.04108,0.03025,-0.1177,0.6929,0.1059 -3.000,0.2409,0.03948,0.02829,-0.1188,0.6894,0.1093 -2.750,0.2466,0.03984,0.02869,-0.1161,0.6787,0.1116 -2.500,0.2762,0.03890,0.02749,-0.1164,0.6735,0.1159 -2.250,0.3114,0.03774,0.02610,-0.1172,0.6699,0.1203 -2.000,0.3206,0.03815,0.02653,-0.1149,0.6606,0.1236 -1.750,0.3474,0.03762,0.02578,-0.1146,0.6546,0.1290 -1.500,0.3820,0.03676,0.02489,-0.1152,0.6505,0.1349 -1.250,0.3975,0.03700,0.02504,-0.1135,0.6426,0.1406 -1.000,0.4185,0.03692,0.02496,-0.1125,0.6354,0.1466 -0.750,0.4536,0.03623,0.02412,-0.1129,0.6310,0.1569 -0.500,0.4772,0.03617,0.02406,-0.1123,0.6248,0.1667 -0.250,0.4904,0.03664,0.02458,-0.1104,0.6162,0.1767 0.000,0.5238,0.03605,0.02398,-0.1108,0.6116,0.1967 0.250,0.5633,0.03508,0.02310,-0.1120,0.6082,0.2345 0.500,0.5595,0.03651,0.02476,-0.1085,0.5975,0.2600 0.750,0.5890,0.03579,0.02454,-0.1086,0.5926,0.3667 1.000,0.6156,0.03429,0.02415,-0.1069,0.5892,0.6416 1.250,0.6188,0.03527,0.02562,-0.1034,0.5796,1.0000 1.500,0.6420,0.03575,0.02581,-0.1027,0.5735,1.0000 1.750,0.6790,0.03555,0.02527,-0.1035,0.5697,1.0000 2.000,0.6833,0.03701,0.02663,-0.1009,0.5614,1.0000 2.250,0.6932,0.03812,0.02761,-0.0988,0.5537,1.0000 2.500,0.7296,0.03797,0.02721,-0.0996,0.5498,1.0000 2.750,0.7731,0.03749,0.02645,-0.1011,0.5469,1.0000 3.000,0.7355,0.04118,0.03028,-0.0944,0.5332,1.0000 3.250,0.7693,0.04107,0.02997,-0.0947,0.5293,1.0000 3.500,0.8117,0.04056,0.02924,-0.0960,0.5266,1.0000 4.000,0.8015,0.04514,0.03381,-0.0901,0.5082,1.0000 4.250,0.8418,0.04453,0.03301,-0.0908,0.5057,1.0000 4.750,0.8246,0.05047,0.03898,-0.0859,0.4867,1.0000 5.000,0.8623,0.04986,0.03822,-0.0861,0.4846,1.0000 5.500,0.8432,0.05679,0.04521,-0.0824,0.4654,1.0000 6.500,0.8139,0.07251,0.06101,-0.0791,0.4302,1.0000 6.750,0.8400,0.07272,0.06114,-0.0786,0.4278,1.0000 7.250,0.8246,0.08112,0.06960,-0.0778,0.4119,1.0000 7.500,0.8519,0.08117,0.06958,-0.0772,0.4097,1.0000 7.750,0.8162,0.08877,0.07729,-0.0772,0.3978,1.0000 8.000,0.8380,0.08944,0.07791,-0.0767,0.3944,1.0000 8.250,0.8671,0.08918,0.07759,-0.0760,0.3923,1.0000 8.750,0.8616,0.09617,0.08462,-0.0755,0.3768,1.0000 9.250,0.8626,0.10236,0.09084,-0.0751,0.3620,1.0000 9.500,0.8900,0.10207,0.09051,-0.0743,0.3592,1.0000 9.750,0.8678,0.10819,0.09672,-0.0749,0.3482,1.0000 10.000,0.8869,0.10897,0.09747,-0.0744,0.3441,1.0000 10.250,0.9142,0.10864,0.09711,-0.0736,0.3417,1.0000 10.500,0.8883,0.11548,0.10404,-0.0746,0.3299,1.0000 10.750,0.9090,0.11602,0.10457,-0.0740,0.3264,1.0000 11.000,0.9356,0.11570,0.10423,-0.0732,0.3241,1.0000 11.250,0.9077,0.12307,0.11169,-0.0747,0.3118,1.0000 11.500,0.9290,0.12350,0.11211,-0.0742,0.3087,1.0000