XFOIL Version 6.94 Calculated polar for: GOE 265 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.450 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.6754 0.01026 0.00284 -0.1192 0.5441 0.0491 0.500 0.7317 0.01026 0.00282 -0.1189 0.5278 0.0626 1.000 0.7873 0.01046 0.00298 -0.1185 0.5093 0.0800 1.500 0.8426 0.01076 0.00321 -0.1181 0.4912 0.0954 2.000 0.8974 0.01107 0.00349 -0.1177 0.4713 0.1127 2.500 0.9522 0.01110 0.00347 -0.1173 0.4491 0.1234 3.000 1.0067 0.01120 0.00354 -0.1170 0.4265 0.1355 3.500 1.0607 0.01138 0.00367 -0.1166 0.4041 0.1502 4.000 1.1143 0.01160 0.00389 -0.1163 0.3842 0.1724 4.500 1.1678 0.01169 0.00429 -0.1161 0.3650 0.3525 5.000 1.2134 0.01168 0.00475 -0.1146 0.2894 1.0000 5.500 1.2620 0.01262 0.00532 -0.1137 0.2384 1.0000 6.000 1.3017 0.01461 0.00660 -0.1119 0.1309 1.0000 6.500 1.3443 0.01612 0.00784 -0.1102 0.0885 1.0000 7.000 1.3768 0.01862 0.00990 -0.1072 0.0035 1.0000 7.500 1.4217 0.01954 0.01089 -0.1057 0.0036 1.0000 8.000 1.4644 0.02058 0.01204 -0.1039 0.0040 1.0000 8.500 1.5045 0.02172 0.01330 -0.1017 0.0046 1.0000 9.000 1.5402 0.02306 0.01481 -0.0990 0.0053 1.0000 9.500 1.5683 0.02457 0.01649 -0.0952 0.0061 1.0000 10.000 1.5893 0.02658 0.01870 -0.0910 0.0068 1.0000 10.500 1.6049 0.02935 0.02170 -0.0874 0.0073 1.0000 11.000 1.6109 0.03352 0.02614 -0.0845 0.0078 1.0000 11.500 1.6067 0.03946 0.03235 -0.0827 0.0081 1.0000 12.000 1.6094 0.04512 0.03824 -0.0819 0.0086 1.0000 12.500 1.5965 0.05295 0.04635 -0.0817 0.0092 1.0000 13.000 1.5738 0.06233 0.05599 -0.0821 0.0096 1.0000 13.500 1.5453 0.07289 0.06679 -0.0833 0.0098 1.0000 14.000 1.5342 0.08154 0.07567 -0.0844 0.0105 1.0000 14.500 1.5168 0.09120 0.08556 -0.0857 0.0113 1.0000 15.000 1.4995 0.10041 0.09486 -0.0866 0.0120 1.0000 15.500 1.5005 0.10714 0.10175 -0.0870 0.0126 1.0000 16.000 1.5126 0.11091 0.10564 -0.0849 0.0134 1.0000 16.500 1.5382 0.11150 0.10628 -0.0799 0.0138 1.0000 17.000 1.5491 0.11587 0.11086 -0.0784 0.0135 1.0000 17.500 1.5738 0.11683 0.11179 -0.0732 0.0120 1.0000 18.000 1.5549 0.12778 0.12314 -0.0785 0.0118 1.0000 18.500 1.5369 0.13905 0.13478 -0.0845 0.0116 1.0000 19.000 1.5183 0.15094 0.14704 -0.0914 0.0114 1.0000 19.500 1.4984 0.16365 0.16010 -0.0995 0.0113 1.0000 20.000 1.4801 0.17659 0.17336 -0.1081 0.0115 1.0000 20.500 1.4612 0.19035 0.18741 -0.1177 0.0117 1.0000 21.000 1.4460 0.20357 0.20086 -0.1270 0.0120 1.0000 21.500 0.9157 0.24802 0.24618 -0.1145 0.0364 1.0000 22.000 0.9220 0.25487 0.25304 -0.1154 0.0359 1.0000 22.500 0.9131 0.26493 0.26309 -0.1199 0.0320 1.0000 23.000 0.9078 0.27503 0.27319 -0.1237 0.0285 1.0000 23.500 0.9074 0.28347 0.28163 -0.1264 0.0255 1.0000 24.000 0.9091 0.29111 0.28927 -0.1287 0.0224 1.0000 24.500 0.9115 0.29829 0.29646 -0.1309 0.0198 1.0000 25.500 0.9181 0.31126 0.30948 -0.1349 0.0148 1.0000 26.000 0.9176 0.32033 0.31855 -0.1377 0.0126 1.0000 26.500 0.9184 0.32896 0.32720 -0.1402 0.0108 1.0000 27.000 0.9222 0.33447 0.33272 -0.1419 0.0099 1.0000 27.500 0.9225 0.34322 0.34148 -0.1446 0.0083 1.0000 28.000 0.9229 0.35227 0.35054 -0.1470 0.0074 1.0000 28.500 0.9251 0.35866 0.35696 -0.1491 0.0065 1.0000 29.000 0.9257 0.36753 0.36585 -0.1514 0.0061 1.0000 29.500 0.9269 0.37555 0.37388 -0.1537 0.0053 1.0000 30.000 0.9287 0.38107 0.37944 -0.1556 0.0049 1.0000 30.500 0.9287 0.39011 0.38848 -0.1579 0.0048 1.0000 31.000 0.9293 0.39914 0.39753 -0.1602 0.0043 1.0000 31.500 0.9298 0.40645 0.40486 -0.1624 0.0039 1.0000 32.000 0.9302 0.41291 0.41135 -0.1645 0.0037 1.0000 32.500 0.9310 0.41832 0.41680 -0.1662 0.0036 1.0000 33.000 0.9299 0.42737 0.42587 -0.1686 0.0035 1.0000 33.500 0.9295 0.43615 0.43467 -0.1709 0.0034 1.0000 34.000 0.9291 0.44395 0.44249 -0.1730 0.0033 1.0000 34.500 0.9284 0.45129 0.44986 -0.1751 0.0031 1.0000 35.000 0.9276 0.45850 0.45710 -0.1773 0.0030 1.0000 35.500 0.9263 0.46544 0.46406 -0.1794 0.0029 1.0000 36.000 0.9249 0.47222 0.47088 -0.1815 0.0028 1.0000 36.500 0.9232 0.47890 0.47759 -0.1835 0.0028 1.0000 37.000 0.9212 0.48546 0.48417 -0.1856 0.0027 1.0000 37.500 0.9189 0.49183 0.49057 -0.1877 0.0027 1.0000 38.000 0.9165 0.49807 0.49685 -0.1898 0.0027 1.0000 38.500 0.9138 0.50432 0.50313 -0.1918 0.0026 1.0000 39.000 0.9108 0.51030 0.50914 -0.1939 0.0026 1.0000 39.500 0.9077 0.51624 0.51512 -0.1959 0.0026 1.0000 40.000 0.9043 0.52206 0.52096 -0.1980 0.0026 1.0000 40.500 0.9006 0.52768 0.52662 -0.2000 0.0026 1.0000 41.000 0.8967 0.53317 0.53214 -0.2020 0.0026 1.0000 41.500 0.8926 0.53851 0.53752 -0.2040 0.0027 1.0000 42.000 0.8882 0.54371 0.54275 -0.2060 0.0027 1.0000 42.500 0.8837 0.54875 0.54781 -0.2080 0.0027 1.0000 43.000 0.8788 0.55356 0.55267 -0.2099 0.0027 1.0000 43.500 0.8738 0.55824 0.55738 -0.2119 0.0027 1.0000 44.000 0.8685 0.56260 0.56177 -0.2138 0.0027 1.0000 44.500 0.8630 0.56669 0.56589 -0.2157 0.0026 1.0000 45.000 0.8570 0.57043 0.56966 -0.2176 0.0026 1.0000 45.500 0.8508 0.57382 0.57309 -0.2196 0.0025 1.0000 46.500 0.8384 0.58267 0.58199 -0.2231 0.0024 1.0000 47.000 0.8327 0.58778 0.58712 -0.2249 0.0024 1.0000 47.500 0.8268 0.59242 0.59179 -0.2265 0.0024 1.0000 48.000 0.8205 0.59655 0.59594 -0.2281 0.0022 1.0000 48.500 0.8137 0.59998 0.59940 -0.2297 0.0020 1.0000 49.000 0.8066 0.60304 0.60248 -0.2314 0.0018 1.0000 49.500 0.7993 0.60563 0.60511 -0.2331 0.0017 1.0000 50.000 0.7915 0.60761 0.60711 -0.2348 0.0016 1.0000 50.500 0.7832 0.60899 0.60853 -0.2366 0.0015 1.0000 52.000 0.7599 0.61740 0.61700 -0.2411 0.0015 1.0000 52.500 0.7523 0.62004 0.61966 -0.2425 0.0015 1.0000 53.000 0.7444 0.62218 0.62182 -0.2439 0.0014 1.0000 53.500 0.7363 0.62397 0.62363 -0.2452 0.0014 1.0000 54.000 0.7278 0.62511 0.62480 -0.2466 0.0012 1.0000 54.500 0.7191 0.62612 0.62583 -0.2480 0.0011 1.0000 55.000 0.7102 0.62654 0.62628 -0.2494 0.0010 1.0000 55.500 0.7011 0.62672 0.62648 -0.2508 0.0009 1.0000 56.000 0.6917 0.62631 0.62609 -0.2522 0.0008 1.0000 56.500 0.6819 0.62529 0.62510 -0.2536 0.0007 1.0000 57.000 0.6717 0.62374 0.62357 -0.2551 0.0007 1.0000 58.000 0.6531 0.62448 0.62435 -0.2574 0.0007 1.0000 58.500 0.6442 0.62456 0.62445 -0.2584 0.0006 1.0000 59.000 0.6348 0.62376 0.62367 -0.2595 0.0006 1.0000 59.500 0.6249 0.62240 0.62232 -0.2606 0.0005 1.0000 60.000 0.6148 0.62034 0.62028 -0.2618 0.0005 1.0000