Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa46-il-200000-n5 Airfoil,usa46-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,63.6059 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-usa46-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.5155,0.08659,0.08310,-0.0136,1.0000,0.0118 -8.500,-0.5185,0.08200,0.07856,-0.0157,1.0000,0.0117 -8.250,-0.5232,0.07755,0.07417,-0.0178,1.0000,0.0116 -8.000,-0.5298,0.07270,0.06940,-0.0205,1.0000,0.0116 -7.750,-0.5322,0.06620,0.06295,-0.0267,1.0000,0.0116 -7.500,-0.5312,0.05741,0.05415,-0.0364,1.0000,0.0114 -7.250,-0.5326,0.04071,0.03714,-0.0500,1.0000,0.0109 -7.000,-0.5229,0.03022,0.02576,-0.0555,1.0000,0.0109 -6.750,-0.5045,0.02550,0.02035,-0.0566,1.0000,0.0113 -6.500,-0.4833,0.02239,0.01663,-0.0567,1.0000,0.0119 -6.250,-0.4601,0.02078,0.01465,-0.0563,1.0000,0.0128 -6.000,-0.4382,0.01792,0.01134,-0.0560,1.0000,0.0149 -5.750,-0.4145,0.01657,0.00976,-0.0554,1.0000,0.0167 -5.500,-0.3903,0.01553,0.00853,-0.0548,1.0000,0.0193 -5.250,-0.3659,0.01477,0.00758,-0.0541,1.0000,0.0234 -5.000,-0.3415,0.01405,0.00681,-0.0536,1.0000,0.0310 -4.750,-0.3171,0.01361,0.00628,-0.0530,1.0000,0.0406 -4.500,-0.2928,0.01321,0.00582,-0.0524,1.0000,0.0494 -4.250,-0.2687,0.01292,0.00546,-0.0517,1.0000,0.0589 -4.000,-0.2447,0.01257,0.00505,-0.0511,1.0000,0.0660 -3.750,-0.2207,0.01221,0.00459,-0.0504,1.0000,0.0707 -3.500,-0.1932,0.01183,0.00419,-0.0505,0.9985,0.0796 -3.250,-0.1581,0.01147,0.00382,-0.0522,0.9933,0.0902 -3.000,-0.1231,0.01118,0.00356,-0.0538,0.9877,0.1062 -2.750,-0.0889,0.01097,0.00334,-0.0552,0.9813,0.1265 -2.500,-0.0541,0.01080,0.00316,-0.0567,0.9750,0.1448 -2.250,-0.0201,0.01062,0.00299,-0.0580,0.9676,0.1624 -2.000,0.0132,0.01044,0.00280,-0.0592,0.9596,0.1781 -1.750,0.0486,0.01024,0.00264,-0.0608,0.9519,0.1951 -1.500,0.0834,0.01000,0.00247,-0.0622,0.9405,0.2147 -1.250,0.1192,0.00971,0.00229,-0.0638,0.9272,0.2466 -1.000,0.1543,0.00926,0.00215,-0.0654,0.9123,0.3281 -0.750,0.1859,0.00867,0.00210,-0.0662,0.8955,0.4929 -0.500,0.2139,0.00825,0.00212,-0.0659,0.8758,0.6314 -0.250,0.2411,0.00805,0.00212,-0.0651,0.8548,0.7296 0.000,0.2672,0.00797,0.00207,-0.0643,0.8305,0.7835 0.250,0.2935,0.00786,0.00200,-0.0634,0.8073,0.8257 0.500,0.3292,0.00765,0.00191,-0.0645,0.7850,0.9069 0.750,0.3622,0.00771,0.00188,-0.0654,0.7602,1.0000 1.000,0.3887,0.00784,0.00189,-0.0648,0.7349,1.0000 1.250,0.4149,0.00798,0.00192,-0.0643,0.7090,1.0000 1.500,0.4411,0.00814,0.00197,-0.0637,0.6837,1.0000 1.750,0.4672,0.00832,0.00206,-0.0631,0.6575,1.0000 2.000,0.4932,0.00851,0.00215,-0.0626,0.6302,1.0000 2.250,0.5189,0.00873,0.00226,-0.0620,0.6015,1.0000 2.500,0.5446,0.00897,0.00242,-0.0614,0.5735,1.0000 2.750,0.5704,0.00921,0.00259,-0.0608,0.5466,1.0000 3.000,0.5959,0.00948,0.00278,-0.0603,0.5170,1.0000 3.250,0.6212,0.00978,0.00301,-0.0597,0.4818,1.0000 3.500,0.6456,0.01015,0.00322,-0.0589,0.4274,1.0000 3.750,0.6672,0.01087,0.00347,-0.0579,0.3368,1.0000 4.000,0.6912,0.01142,0.00383,-0.0573,0.2896,1.0000 4.250,0.7150,0.01202,0.00422,-0.0567,0.2292,1.0000 4.500,0.7340,0.01351,0.00491,-0.0558,0.0769,1.0000 4.750,0.7559,0.01465,0.00575,-0.0549,0.0263,1.0000 5.000,0.7801,0.01541,0.00658,-0.0541,0.0202,1.0000 5.250,0.8045,0.01607,0.00739,-0.0534,0.0171,1.0000 5.500,0.8279,0.01692,0.00839,-0.0526,0.0152,1.0000 5.750,0.8500,0.01796,0.00960,-0.0516,0.0140,1.0000 6.000,0.8702,0.01939,0.01115,-0.0503,0.0127,1.0000 6.250,0.8891,0.02134,0.01322,-0.0489,0.0113,1.0000 6.500,0.9116,0.02263,0.01464,-0.0479,0.0107,1.0000 6.750,0.9336,0.02427,0.01646,-0.0468,0.0103,1.0000 7.000,0.9554,0.02618,0.01859,-0.0456,0.0099,1.0000 7.250,0.9766,0.02833,0.02101,-0.0445,0.0097,1.0000 7.500,0.9963,0.03078,0.02379,-0.0432,0.0095,1.0000 7.750,1.0144,0.03330,0.02672,-0.0418,0.0091,1.0000 8.000,1.0312,0.03553,0.02926,-0.0405,0.0086,1.0000 8.250,1.0472,0.03727,0.03117,-0.0395,0.0079,1.0000 8.500,1.0598,0.03957,0.03371,-0.0383,0.0075,1.0000 8.750,1.0678,0.04281,0.03726,-0.0367,0.0073,1.0000 9.000,1.0717,0.04638,0.04119,-0.0349,0.0072,1.0000 9.250,1.0710,0.05011,0.04526,-0.0330,0.0072,1.0000 9.500,1.0654,0.05387,0.04934,-0.0311,0.0072,1.0000 9.750,1.0537,0.05733,0.05305,-0.0288,0.0072,1.0000 10.000,1.0390,0.06073,0.05667,-0.0271,0.0073,1.0000 10.250,1.0210,0.06505,0.06119,-0.0274,0.0073,1.0000 10.500,1.0033,0.07033,0.06666,-0.0298,0.0074,1.0000 10.750,0.9819,0.07784,0.07438,-0.0351,0.0075,1.0000 11.000,0.9491,0.09127,0.08806,-0.0456,0.0079,1.0000