XFOIL Version 6.94 Calculated polar for: GOE 497 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 0.6524 0.00882 0.00271 -0.1493 0.6961 0.3722 0.500 0.7066 0.00885 0.00277 -0.1487 0.6793 0.4025 1.000 0.7604 0.00891 0.00286 -0.1480 0.6623 0.4387 1.500 0.8135 0.00902 0.00298 -0.1472 0.6437 0.4784 2.000 0.8656 0.00911 0.00313 -0.1462 0.6235 0.5178 2.500 0.9166 0.00917 0.00330 -0.1450 0.6013 0.5691 3.000 0.9554 0.00924 0.00349 -0.1414 0.5347 0.6966 3.500 0.9957 0.00935 0.00376 -0.1380 0.4765 1.0000 4.000 1.0311 0.01033 0.00427 -0.1341 0.4115 1.0000 4.500 1.0768 0.01085 0.00466 -0.1321 0.3863 1.0000 5.000 1.1054 0.01205 0.00531 -0.1272 0.2916 1.0000 5.500 1.1255 0.01351 0.00626 -0.1209 0.2160 1.0000 6.000 1.1495 0.01484 0.00723 -0.1155 0.1533 1.0000 6.500 1.1559 0.01714 0.00893 -0.1077 0.0584 1.0000 7.000 1.1698 0.01919 0.01071 -0.1015 0.0036 1.0000 7.500 1.2027 0.02026 0.01182 -0.0982 0.0033 1.0000 8.000 1.2336 0.02147 0.01311 -0.0948 0.0032 1.0000 8.500 1.2627 0.02287 0.01459 -0.0913 0.0032 1.0000 9.000 1.2896 0.02446 0.01629 -0.0879 0.0032 1.0000 9.500 1.3146 0.02629 0.01824 -0.0845 0.0033 1.0000 10.000 1.3372 0.02838 0.02046 -0.0812 0.0034 1.0000 10.500 1.3572 0.03080 0.02303 -0.0780 0.0035 1.0000 11.000 1.3742 0.03360 0.02599 -0.0749 0.0036 1.0000 11.500 1.3880 0.03687 0.02944 -0.0720 0.0038 1.0000 12.000 1.3986 0.04066 0.03342 -0.0695 0.0039 1.0000 12.500 1.4035 0.04533 0.03828 -0.0673 0.0040 1.0000 13.000 1.4017 0.05110 0.04426 -0.0657 0.0041 1.0000 13.500 1.3972 0.05766 0.05101 -0.0649 0.0042 1.0000 14.000 1.4037 0.06329 0.05681 -0.0647 0.0044 1.0000 14.500 1.4076 0.06958 0.06329 -0.0651 0.0046 1.0000 15.000 1.4023 0.07756 0.07148 -0.0664 0.0048 1.0000 15.500 1.3938 0.08649 0.08064 -0.0685 0.0051 1.0000 16.000 1.3842 0.09598 0.09032 -0.0712 0.0053 1.0000 16.500 1.3755 0.10542 0.09992 -0.0742 0.0055 1.0000 17.000 1.3744 0.11326 0.10781 -0.0764 0.0057 1.0000 17.500 1.3793 0.12109 0.11589 -0.0798 0.0060 1.0000 18.000 1.3853 0.12817 0.12318 -0.0823 0.0066 1.0000 18.500 1.4123 0.12973 0.12465 -0.0805 0.0074 1.0000 19.000 1.4099 0.13925 0.13454 -0.0857 0.0080 1.0000 19.500 1.4413 0.14034 0.13572 -0.0838 0.0094 1.0000 20.000 1.4542 0.14602 0.14184 -0.0852 0.0117 1.0000 20.500 1.2001 0.17774 0.17489 -0.1146 0.0095 1.0000 21.000 1.1677 0.19356 0.19113 -0.1245 0.0099 1.0000 21.500 1.1367 0.21000 0.20789 -0.1343 0.0098 1.0000 22.000 1.0824 0.23675 0.23503 -0.1487 0.0098 1.0000 23.000 0.9725 0.32623 0.32470 -0.1773 0.0175 1.0000 23.500 0.9817 0.33346 0.33195 -0.1796 0.0167 1.0000 24.000 0.9829 0.34708 0.34556 -0.1841 0.0146 1.0000 24.500 0.9916 0.35404 0.35255 -0.1863 0.0140 1.0000 25.000 0.9928 0.36813 0.36664 -0.1907 0.0122 1.0000 25.500 0.9998 0.37557 0.37410 -0.1932 0.0115 1.0000 26.000 1.0019 0.38949 0.38802 -0.1971 0.0103 1.0000 26.500 1.0072 0.39838 0.39693 -0.1999 0.0095 1.0000 27.000 1.0144 0.40522 0.40380 -0.2019 0.0093 1.0000 27.500 1.0145 0.42144 0.42002 -0.2063 0.0082 1.0000 28.000 1.0185 0.43120 0.42980 -0.2092 0.0078 1.0000 28.500 1.0227 0.43954 0.43816 -0.2117 0.0074 1.0000 29.000 1.0257 0.45049 0.44912 -0.2145 0.0073 1.0000 29.500 1.0276 0.46384 0.46249 -0.2179 0.0069 1.0000 30.000 1.0302 0.47475 0.47342 -0.2207 0.0064 1.0000 30.500 1.0324 0.48494 0.48363 -0.2235 0.0062 1.0000 31.000 1.0345 0.49463 0.49334 -0.2261 0.0059 1.0000 31.500 1.0362 0.50420 0.50293 -0.2288 0.0058 1.0000 32.000 1.0380 0.51244 0.51120 -0.2311 0.0057 1.0000 32.500 1.0390 0.52281 0.52159 -0.2336 0.0056 1.0000 33.000 1.0391 0.53429 0.53308 -0.2364 0.0056 1.0000 33.500 1.0392 0.54444 0.54326 -0.2391 0.0056 1.0000 34.000 1.0390 0.55572 0.55456 -0.2418 0.0056 1.0000 34.500 1.0387 0.56628 0.56514 -0.2443 0.0055 1.0000 35.000 1.0381 0.57624 0.57513 -0.2468 0.0055 1.0000 35.500 1.0371 0.58625 0.58516 -0.2493 0.0055 1.0000 36.000 1.0359 0.59579 0.59473 -0.2517 0.0054 1.0000 36.500 1.0342 0.60484 0.60380 -0.2540 0.0054 1.0000 37.000 1.0323 0.61403 0.61303 -0.2564 0.0054 1.0000 37.500 1.0301 0.62339 0.62241 -0.2586 0.0054 1.0000 38.000 1.0274 0.63181 0.63086 -0.2609 0.0054 1.0000 38.500 1.0246 0.64073 0.63980 -0.2631 0.0053 1.0000 39.000 1.0214 0.64919 0.64829 -0.2653 0.0053 1.0000 39.500 1.0180 0.65763 0.65676 -0.2674 0.0051 1.0000 40.000 1.0141 0.66568 0.66484 -0.2695 0.0050 1.0000 40.500 1.0100 0.67359 0.67277 -0.2715 0.0048 1.0000 41.000 1.0056 0.68108 0.68029 -0.2736 0.0046 1.0000 41.500 1.0008 0.68801 0.68725 -0.2755 0.0044 1.0000 42.000 0.9955 0.69414 0.69340 -0.2775 0.0042 1.0000 43.000 0.9847 0.71013 0.70944 -0.2812 0.0041 1.0000 43.500 0.9797 0.71952 0.71886 -0.2828 0.0040 1.0000 44.000 0.9740 0.72696 0.72631 -0.2845 0.0037 1.0000 44.500 0.9678 0.73332 0.73270 -0.2862 0.0034 1.0000 45.000 0.9612 0.73886 0.73827 -0.2879 0.0032 1.0000 45.500 0.9540 0.74299 0.74242 -0.2895 0.0030 1.0000 46.000 0.9462 0.74630 0.74576 -0.2911 0.0029 1.0000 46.500 0.9393 0.75413 0.75360 -0.2926 0.0029 1.0000 47.000 0.9328 0.76224 0.76173 -0.2940 0.0028 1.0000 47.500 0.9256 0.76829 0.76780 -0.2952 0.0026 1.0000 48.000 0.9179 0.77314 0.77267 -0.2965 0.0023 1.0000 48.500 0.9097 0.77656 0.77611 -0.2979 0.0021 1.0000 49.000 0.9011 0.77913 0.77870 -0.2992 0.0019 1.0000 49.500 0.8921 0.78076 0.78035 -0.3005 0.0018 1.0000 50.000 0.8825 0.78189 0.78151 -0.3018 0.0018 1.0000 51.000 0.8658 0.79198 0.79162 -0.3037 0.0017 1.0000 51.500 0.8570 0.79508 0.79474 -0.3047 0.0017 1.0000 52.000 0.8478 0.79704 0.79672 -0.3056 0.0016 1.0000 52.500 0.8384 0.79892 0.79862 -0.3065 0.0015 1.0000 53.000 0.8286 0.79945 0.79917 -0.3073 0.0013 1.0000 53.500 0.8187 0.79960 0.79933 -0.3082 0.0011 1.0000 54.000 0.8084 0.79899 0.79874 -0.3090 0.0010 1.0000 54.500 0.7979 0.79741 0.79718 -0.3098 0.0009 1.0000 55.000 0.7869 0.79463 0.79442 -0.3106 0.0009 1.0000 55.500 0.7754 0.79139 0.79120 -0.3114 0.0008 1.0000 56.500 0.7555 0.79248 0.79231 -0.3122 0.0007 1.0000 57.000 0.7450 0.79056 0.79040 -0.3126 0.0006 1.0000 57.500 0.7339 0.78728 0.78714 -0.3131 0.0006 1.0000 58.000 0.7226 0.78329 0.78317 -0.3135 0.0005 1.0000 58.500 0.7110 0.77841 0.77830 -0.3140 0.0004 1.0000 60.000 0.6772 0.76661 0.76654 -0.3146 0.0004 1.0000