XFOIL Version 6.96 Calculated polar for: TRAINER60 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -17.250 -1.3016 0.09205 0.08697 0.0186 1.0000 0.0363 -17.000 -1.3081 0.08759 0.08247 0.0170 1.0000 0.0367 -16.750 -1.3139 0.08322 0.07804 0.0155 1.0000 0.0372 -16.500 -1.3191 0.07895 0.07370 0.0141 1.0000 0.0377 -16.250 -1.3247 0.07467 0.06935 0.0127 1.0000 0.0382 -16.000 -1.3295 0.07054 0.06513 0.0114 1.0000 0.0388 -15.750 -1.3336 0.06660 0.06109 0.0102 1.0000 0.0393 -15.500 -1.3369 0.06284 0.05724 0.0091 1.0000 0.0399 -15.250 -1.3433 0.05882 0.05313 0.0081 1.0000 0.0405 -15.000 -1.3543 0.05434 0.04858 0.0070 1.0000 0.0411 -14.750 -1.3613 0.05037 0.04454 0.0061 1.0000 0.0418 -14.500 -1.3649 0.04680 0.04090 0.0053 1.0000 0.0425 -14.250 -1.3652 0.04362 0.03764 0.0046 1.0000 0.0434 -14.000 -1.3630 0.04071 0.03464 0.0040 1.0000 0.0445 -13.750 -1.3603 0.03789 0.03173 0.0034 1.0000 0.0455 -13.500 -1.3620 0.03465 0.02843 0.0028 1.0000 0.0467 -13.250 -1.3583 0.03211 0.02584 0.0026 1.0000 0.0481 -13.000 -1.3509 0.03006 0.02372 0.0026 1.0000 0.0500 -12.750 -1.3463 0.02792 0.02152 0.0029 1.0000 0.0519 -12.500 -1.3408 0.02606 0.01962 0.0037 1.0000 0.0542 -12.250 -1.3322 0.02463 0.01814 0.0048 1.0000 0.0571 -12.000 -1.3276 0.02321 0.01671 0.0069 1.0000 0.0605 -11.750 -1.3205 0.02207 0.01555 0.0093 1.0000 0.0652 -11.500 -1.3080 0.02088 0.01440 0.0109 1.0000 0.0726 -11.250 -1.2944 0.01967 0.01327 0.0123 1.0000 0.0849 -11.000 -1.2798 0.01852 0.01226 0.0137 1.0000 0.1041 -10.750 -1.2613 0.01763 0.01152 0.0146 1.0000 0.1241 -10.500 -1.2381 0.01709 0.01102 0.0150 1.0000 0.1377 -10.250 -1.2142 0.01659 0.01058 0.0154 1.0000 0.1486 -10.000 -1.1948 0.01597 0.01000 0.0168 0.9856 0.1559 -9.750 -1.1473 0.01567 0.00965 0.0125 0.9694 0.1647 -9.500 -1.0965 0.01511 0.00912 0.0072 0.9638 0.1736 -9.250 -1.0410 0.01479 0.00872 0.0011 0.9568 0.1806 -9.000 -0.9874 0.01427 0.00823 -0.0050 0.9490 0.1888 -8.750 -0.9380 0.01404 0.00792 -0.0098 0.9399 0.1950 -8.500 -0.9008 0.01372 0.00758 -0.0121 0.9295 0.2013 -8.250 -0.8722 0.01351 0.00735 -0.0124 0.9182 0.2068 -8.000 -0.8463 0.01338 0.00716 -0.0119 0.9072 0.2118 -7.750 -0.8247 0.01312 0.00690 -0.0106 0.8956 0.2172 -7.500 -0.8044 0.01284 0.00663 -0.0090 0.8827 0.2240 -7.000 -0.7639 0.01224 0.00606 -0.0056 0.8492 0.2411 -6.750 -0.7421 0.01199 0.00578 -0.0041 0.8267 0.2501 -6.500 -0.7207 0.01169 0.00546 -0.0026 0.8021 0.2601 -6.250 -0.6964 0.01147 0.00517 -0.0017 0.7794 0.2707 -6.000 -0.6711 0.01126 0.00493 -0.0011 0.7615 0.2846 -5.500 -0.6196 0.01085 0.00454 0.0000 0.7334 0.3181 -5.250 -0.5930 0.01072 0.00439 0.0004 0.7216 0.3338 -5.000 -0.5660 0.01060 0.00427 0.0007 0.7107 0.3482 -4.750 -0.5388 0.01053 0.00415 0.0011 0.7000 0.3613 -4.500 -0.5118 0.01040 0.00404 0.0014 0.6905 0.3723 -4.250 -0.4841 0.01035 0.00394 0.0017 0.6811 0.3825 -4.000 -0.4567 0.01027 0.00385 0.0020 0.6726 0.3917 -3.750 -0.4291 0.01018 0.00377 0.0023 0.6638 0.4012 -3.500 -0.4013 0.01014 0.00367 0.0026 0.6550 0.4100 -3.250 -0.3738 0.01005 0.00361 0.0029 0.6466 0.4191 -3.000 -0.3456 0.01002 0.00353 0.0031 0.6371 0.4270 -2.750 -0.3182 0.00997 0.00346 0.0034 0.6279 0.4355 -2.500 -0.2901 0.00989 0.00341 0.0036 0.6195 0.4439 -2.250 -0.2620 0.00985 0.00334 0.0038 0.6103 0.4516 -2.000 -0.2342 0.00981 0.00330 0.0041 0.6016 0.4605 -1.750 -0.2058 0.00977 0.00326 0.0042 0.5920 0.4694 -1.500 -0.1782 0.00974 0.00322 0.0045 0.5823 0.4782 -1.250 -0.1498 0.00970 0.00320 0.0047 0.5723 0.4873 -1.000 -0.1218 0.00970 0.00315 0.0050 0.5607 0.4956 -0.750 -0.0936 0.00967 0.00315 0.0052 0.5492 0.5047 -0.500 -0.0657 0.00972 0.00311 0.0054 0.5371 0.5136 -0.250 -0.0374 0.00969 0.00313 0.0056 0.5266 0.5226 0.000 -0.0095 0.00974 0.00313 0.0059 0.5151 0.5317 0.250 0.0190 0.00975 0.00315 0.0060 0.5050 0.5407 0.500 0.0468 0.00980 0.00319 0.0063 0.4953 0.5506 1.000 0.1036 0.00987 0.00328 0.0065 0.4787 0.5692 1.250 0.1314 0.00997 0.00332 0.0068 0.4702 0.5781 1.500 0.1605 0.00999 0.00336 0.0068 0.4628 0.5856 1.750 0.1897 0.01000 0.00340 0.0067 0.4550 0.5933 2.000 0.2180 0.01011 0.00346 0.0069 0.4473 0.6006 2.250 0.2472 0.01014 0.00351 0.0068 0.4408 0.6067 2.500 0.2775 0.01014 0.00355 0.0065 0.4327 0.6141 2.750 0.3064 0.01023 0.00362 0.0064 0.4248 0.6216 3.000 0.3359 0.01026 0.00368 0.0063 0.4178 0.6286 3.250 0.3665 0.01029 0.00374 0.0059 0.4099 0.6364 3.500 0.3964 0.01036 0.00383 0.0056 0.4021 0.6441 3.750 0.4265 0.01041 0.00391 0.0054 0.3936 0.6516 4.000 0.4568 0.01050 0.00399 0.0049 0.3839 0.6595 4.250 0.4881 0.01052 0.00410 0.0044 0.3746 0.6688 4.500 0.5179 0.01064 0.00419 0.0041 0.3637 0.6783 4.750 0.5501 0.01068 0.00432 0.0033 0.3522 0.6897 5.250 0.6119 0.01097 0.00461 0.0021 0.3216 0.7152 5.500 0.6431 0.01115 0.00479 0.0014 0.3015 0.7303 5.750 0.6738 0.01139 0.00502 0.0007 0.2807 0.7485 6.000 0.7050 0.01167 0.00529 -0.0001 0.2613 0.7693 6.250 0.7362 0.01199 0.00560 -0.0009 0.2454 0.7914 6.500 0.7647 0.01225 0.00592 -0.0011 0.2345 0.8140 6.750 0.7862 0.01255 0.00626 0.0004 0.2261 0.8360 7.000 0.8018 0.01282 0.00658 0.0032 0.2194 0.8564 7.250 0.8149 0.01318 0.00692 0.0064 0.2134 0.8737 7.500 0.8291 0.01345 0.00720 0.0095 0.2086 0.8885 7.750 0.8435 0.01368 0.00745 0.0125 0.2037 0.9015 8.000 0.8595 0.01396 0.00771 0.0150 0.1980 0.9139 8.250 0.8830 0.01420 0.00796 0.0158 0.1928 0.9254 8.500 0.9182 0.01435 0.00816 0.0141 0.1875 0.9347 8.750 0.9603 0.01467 0.00847 0.0106 0.1811 0.9419 9.000 1.0099 0.01495 0.00880 0.0055 0.1748 0.9475 9.250 1.0617 0.01530 0.00916 0.0000 0.1674 0.9522 9.500 1.1108 0.01569 0.00959 -0.0050 0.1602 0.9570 9.750 1.1579 0.01610 0.01000 -0.0096 0.1515 0.9620 10.000 1.2044 0.01647 0.01039 -0.0139 0.1410 0.9699 10.250 1.2249 0.01719 0.01106 -0.0128 0.1307 0.9993 10.500 1.2519 0.01793 0.01166 -0.0134 0.1102 1.0000 10.750 1.2678 0.01922 0.01271 -0.0125 0.0819 1.0000 11.000 1.2827 0.02055 0.01392 -0.0114 0.0678 1.0000 11.250 1.2985 0.02174 0.01507 -0.0104 0.0613 1.0000 11.500 1.3139 0.02285 0.01619 -0.0094 0.0575 1.0000 11.750 1.3243 0.02407 0.01743 -0.0077 0.0548 1.0000 12.000 1.3316 0.02525 0.01868 -0.0058 0.0530 1.0000 12.250 1.3363 0.02691 0.02037 -0.0045 0.0513 1.0000 12.500 1.3377 0.02912 0.02263 -0.0037 0.0498 1.0000 12.750 1.3473 0.03085 0.02444 -0.0035 0.0486 1.0000 13.000 1.3539 0.03301 0.02667 -0.0036 0.0474 1.0000 13.250 1.3584 0.03550 0.02923 -0.0039 0.0465 1.0000 13.500 1.3593 0.03847 0.03226 -0.0044 0.0456 1.0000 13.750 1.3558 0.04194 0.03579 -0.0051 0.0449 1.0000 14.000 1.3549 0.04517 0.03911 -0.0057 0.0442 1.0000 14.250 1.3565 0.04814 0.04217 -0.0063 0.0436 1.0000 14.500 1.3560 0.05137 0.04549 -0.0070 0.0430 1.0000 14.750 1.3540 0.05482 0.04902 -0.0078 0.0424 1.0000 15.000 1.3507 0.05843 0.05272 -0.0087 0.0419 1.0000 15.250 1.3463 0.06223 0.05659 -0.0097 0.0414 1.0000 15.500 1.3416 0.06614 0.06057 -0.0108 0.0410 1.0000 15.750 1.3356 0.07031 0.06480 -0.0121 0.0405 1.0000 16.000 1.3284 0.07466 0.06920 -0.0133 0.0401 1.0000 16.500 1.3212 0.08250 0.07718 -0.0157 0.0392 1.0000 16.750 1.3199 0.08627 0.08102 -0.0169 0.0389 1.0000