Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-cp-160-050-gn-200000 Airfoil,cp-160-050-gn Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,39.0811 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-cp-160-050-gn-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -5.500,-0.0180,0.12906,0.12536,-0.0871,0.7910,0.0308 -5.250,-0.0172,0.12733,0.12363,-0.0858,0.7877,0.0310 -5.000,-0.0096,0.12519,0.12148,-0.0862,0.7857,0.0312 -4.750,0.0025,0.12280,0.11908,-0.0877,0.7844,0.0316 -4.500,-0.0296,0.12480,0.12116,-0.0798,0.7755,0.0316 -4.250,-0.0259,0.12317,0.11953,-0.0796,0.7720,0.0319 -4.000,-0.0124,0.12066,0.11699,-0.0814,0.7699,0.0323 -3.750,0.0044,0.11792,0.11422,-0.0839,0.7685,0.0328 -3.500,-0.0009,0.11750,0.11383,-0.0819,0.7636,0.0331 -3.250,0.0467,0.11270,0.10893,-0.0912,0.7662,0.0336 -2.500,0.0608,0.10976,0.10601,-0.0926,0.7516,0.0339 -2.250,0.0300,0.11193,0.10826,-0.0858,0.7416,0.0339 -2.000,0.0407,0.10888,0.10519,-0.0859,0.7391,0.0340 -1.750,0.0620,0.10592,0.10221,-0.0887,0.7374,0.0343 -1.500,0.0896,0.10298,0.09923,-0.0929,0.7362,0.0348 -1.250,0.1226,0.09992,0.09613,-0.0982,0.7353,0.0354 -1.000,0.0943,0.10205,0.09834,-0.0922,0.7249,0.0355 -0.750,0.1228,0.09963,0.09587,-0.0967,0.7227,0.0361 -0.500,0.1647,0.09698,0.09315,-0.1041,0.7212,0.0370 -0.250,0.2358,0.09472,0.09077,-0.1189,0.7202,0.0374 0.000,0.2543,0.09094,0.08697,-0.1196,0.7193,0.0377 0.250,0.2366,0.09264,0.08875,-0.1156,0.7095,0.0377 0.500,0.2631,0.09060,0.08669,-0.1190,0.7071,0.0381 0.750,0.3020,0.08832,0.08436,-0.1248,0.7055,0.0389 1.000,0.3489,0.08594,0.08191,-0.1322,0.7043,0.0401 1.250,0.4507,0.08497,0.08075,-0.1522,0.7037,0.0415 1.500,0.4708,0.08139,0.07718,-0.1527,0.7029,0.0417 1.750,0.5093,0.07892,0.07467,-0.1573,0.7022,0.0424 2.000,0.5585,0.07693,0.07263,-0.1643,0.7017,0.0437 2.250,0.6596,0.07732,0.07282,-0.1829,0.7009,0.0461 2.500,0.6353,0.08031,0.07589,-0.1777,0.6882,0.0461 2.750,0.6559,0.07707,0.07268,-0.1780,0.6872,0.0465 3.000,0.6953,0.07514,0.07074,-0.1822,0.6865,0.0474 3.250,0.7451,0.07376,0.06930,-0.1885,0.6859,0.0492 3.500,0.8209,0.07320,0.06861,-0.2001,0.6855,0.0517 3.750,0.8548,0.07129,0.06672,-0.2028,0.6850,0.0527 4.000,0.8282,0.07509,0.07060,-0.1975,0.6713,0.0528 4.250,0.8732,0.07403,0.06951,-0.2023,0.6704,0.0547 4.500,0.9463,0.07412,0.06944,-0.2123,0.6698,0.0578 4.750,0.9760,0.07231,0.06768,-0.2140,0.6692,0.0589 5.000,1.0178,0.07140,0.06675,-0.2176,0.6687,0.0622 5.250,1.0856,0.06920,0.06444,-0.2249,0.6678,0.0659 5.500,1.2722,0.05030,0.04523,-0.2439,0.6706,0.0764 5.750,1.3907,0.04016,0.03486,-0.2556,0.6641,0.0882 6.000,1.4394,0.03748,0.03187,-0.2579,0.6328,0.0969 6.250,1.4503,0.03711,0.03123,-0.2550,0.5842,0.0995 6.500,1.4438,0.03872,0.03227,-0.2496,0.5053,0.1022 6.750,1.4187,0.04229,0.03537,-0.2422,0.4339,0.1031 7.000,1.3847,0.04706,0.03967,-0.2343,0.3518,0.1027 7.250,1.3567,0.05182,0.04397,-0.2279,0.2622,0.1031 7.500,1.3265,0.05715,0.04877,-0.2217,0.1375,0.1031 7.750,1.3232,0.06109,0.05231,-0.2188,0.0599,0.1095 8.000,1.3337,0.06235,0.05364,-0.2176,0.0534,0.1120 8.250,1.3502,0.06405,0.05530,-0.2168,0.0510,0.1236 8.500,1.3594,0.06548,0.05686,-0.2154,0.0490,0.1283 8.750,1.3717,0.06742,0.05881,-0.2143,0.0476,0.1396 9.000,1.3798,0.06938,0.06088,-0.2128,0.0464,0.1465 9.250,1.3911,0.07127,0.06282,-0.2117,0.0455,0.1572 9.500,1.4009,0.07334,0.06494,-0.2104,0.0444,0.1708 9.750,1.4085,0.07564,0.06730,-0.2090,0.0438,0.1856 10.000,1.4146,0.07810,0.06982,-0.2075,0.0433,0.2011 10.250,1.4202,0.08059,0.07239,-0.2059,0.0429,0.2178 10.500,1.4256,0.08310,0.07497,-0.2044,0.0426,0.2365 10.750,1.4315,0.08550,0.07742,-0.2029,0.0423,0.2672 11.000,1.4527,0.08777,0.07936,-0.2026,0.0420,0.1551 11.250,1.4555,0.09006,0.08181,-0.2007,0.0419,0.2114 11.500,1.4618,0.09188,0.08379,-0.1992,0.0418,0.2849 11.750,1.4945,0.09369,0.08483,-0.1995,0.0416,0.0933 12.000,1.5088,0.09501,0.08610,-0.1982,0.0416,0.0928 12.250,1.5258,0.09583,0.08689,-0.1967,0.0418,0.0934 12.500,1.5456,0.09620,0.08723,-0.1953,0.0419,0.0955 12.750,1.5685,0.09624,0.08727,-0.1942,0.0416,0.1031 13.000,1.5958,0.09578,0.08676,-0.1933,0.0411,0.1197 13.250,1.6301,0.09414,0.08569,-0.1925,0.0421,1.0000 13.500,1.6964,0.08997,0.08138,-0.1929,0.0446,1.0000 15.000,2.0478,0.10803,0.10133,-0.1999,0.0670,1.0000 15.250,2.0075,0.10967,0.10329,-0.1921,0.0669,1.0000 15.500,1.9558,0.11076,0.10476,-0.1836,0.0669,1.0000 15.750,1.9113,0.11243,0.10677,-0.1768,0.0668,1.0000 16.000,1.8653,0.11414,0.10881,-0.1706,0.0666,1.0000 16.250,1.8227,0.11635,0.11133,-0.1655,0.0665,1.0000