XFOIL Version 6.94 Calculated polar for: GOE 501 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 0.7670 0.00917 0.00305 -0.1728 0.6929 0.3320 0.500 0.8197 0.00920 0.00306 -0.1718 0.6721 0.3670 1.000 0.8704 0.00923 0.00310 -0.1705 0.6440 0.3998 1.500 0.9177 0.00938 0.00315 -0.1686 0.6050 0.4334 2.000 0.9619 0.00969 0.00337 -0.1662 0.5654 0.4787 2.500 1.0074 0.01001 0.00375 -0.1642 0.5384 0.5570 3.000 1.0521 0.01022 0.00417 -0.1620 0.5170 0.6832 3.500 1.0911 0.01024 0.00450 -0.1584 0.4809 1.0000 4.000 1.1329 0.01076 0.00484 -0.1557 0.4535 1.0000 4.500 1.1595 0.01155 0.00528 -0.1501 0.4019 1.0000 5.000 1.1941 0.01218 0.00576 -0.1462 0.3704 1.0000 5.500 1.2175 0.01330 0.00653 -0.1405 0.3127 1.0000 6.000 1.2089 0.01626 0.00857 -0.1304 0.1675 1.0000 6.500 1.2401 0.01738 0.00960 -0.1267 0.1491 1.0000 7.000 1.2685 0.01869 0.01078 -0.1228 0.1216 1.0000 7.500 1.2612 0.02220 0.01367 -0.1146 0.0226 1.0000 8.000 1.2823 0.02419 0.01564 -0.1104 0.0030 1.0000 8.500 1.3101 0.02583 0.01734 -0.1073 0.0028 1.0000 9.000 1.3363 0.02768 0.01928 -0.1042 0.0027 1.0000 9.500 1.3602 0.02979 0.02149 -0.1012 0.0027 1.0000 10.000 1.3819 0.03218 0.02401 -0.0982 0.0027 1.0000 10.500 1.4014 0.03489 0.02686 -0.0954 0.0027 1.0000 11.000 1.4190 0.03793 0.03003 -0.0927 0.0028 1.0000 11.500 1.4345 0.04134 0.03360 -0.0903 0.0029 1.0000 12.000 1.4479 0.04514 0.03756 -0.0882 0.0030 1.0000 12.500 1.4587 0.04944 0.04204 -0.0863 0.0031 1.0000 13.000 1.4668 0.05430 0.04710 -0.0848 0.0032 1.0000 13.500 1.4719 0.05981 0.05281 -0.0838 0.0033 1.0000 14.000 1.4739 0.06609 0.05931 -0.0834 0.0034 1.0000 14.500 1.4718 0.07331 0.06674 -0.0837 0.0035 1.0000 15.000 1.4645 0.08173 0.07539 -0.0848 0.0036 1.0000 15.500 1.4530 0.09117 0.08504 -0.0867 0.0037 1.0000 16.000 1.4458 0.10024 0.09430 -0.0890 0.0038 1.0000 16.500 1.4468 0.10808 0.10232 -0.0912 0.0039 1.0000 17.000 1.4472 0.11613 0.11058 -0.0937 0.0041 1.0000 17.500 1.4433 0.12500 0.11964 -0.0969 0.0043 1.0000 18.000 1.4387 0.13398 0.12879 -0.1005 0.0045 1.0000 18.500 1.4357 0.14254 0.13750 -0.1041 0.0047 1.0000 19.000 1.4385 0.14950 0.14451 -0.1068 0.0050 1.0000 19.500 1.4474 0.15555 0.15064 -0.1095 0.0052 1.0000 20.000 1.4535 0.16270 0.15804 -0.1132 0.0056 1.0000 20.500 1.4666 0.16735 0.16283 -0.1150 0.0063 1.0000 21.000 1.4859 0.17062 0.16615 -0.1160 0.0069 1.0000 21.500 1.4885 0.17814 0.17406 -0.1201 0.0079 1.0000 22.000 1.5051 0.18203 0.17812 -0.1217 0.0090 1.0000 22.500 1.5087 0.18867 0.18519 -0.1250 0.0109 1.0000 23.000 1.4688 0.20656 0.20365 -0.1378 0.0115 1.0000 23.500 1.4296 0.22525 0.22276 -0.1515 0.0116 1.0000 24.000 1.3988 0.24282 0.24058 -0.1643 0.0114 1.0000 24.500 1.0275 0.36084 0.35941 -0.1962 0.0160 1.0000 25.000 1.0284 0.37497 0.37354 -0.2003 0.0142 1.0000 25.500 1.0342 0.38314 0.38174 -0.2028 0.0133 1.0000 26.000 1.0358 0.39683 0.39543 -0.2065 0.0118 1.0000 26.500 1.0406 0.40568 0.40430 -0.2092 0.0109 1.0000 27.500 1.0460 0.42924 0.42788 -0.2154 0.0091 1.0000 28.000 1.0509 0.43654 0.43521 -0.2175 0.0086 1.0000 28.500 1.0513 0.45131 0.44998 -0.2211 0.0082 1.0000 29.000 1.0536 0.46278 0.46147 -0.2240 0.0073 1.0000 29.500 1.0562 0.47217 0.47088 -0.2265 0.0069 1.0000 30.000 1.0599 0.47902 0.47775 -0.2283 0.0067 1.0000 30.500 1.0590 0.49503 0.49377 -0.2320 0.0065 1.0000 31.000 1.0603 0.50712 0.50589 -0.2347 0.0061 1.0000 31.500 1.0612 0.51779 0.51658 -0.2373 0.0057 1.0000 32.000 1.0620 0.52794 0.52675 -0.2398 0.0055 1.0000 32.500 1.0623 0.53770 0.53653 -0.2423 0.0053 1.0000 33.000 1.0627 0.54572 0.54458 -0.2444 0.0051 1.0000 33.500 1.0628 0.55509 0.55397 -0.2466 0.0051 1.0000 34.000 1.0616 0.56707 0.56598 -0.2493 0.0051 1.0000 34.500 1.0604 0.57752 0.57645 -0.2517 0.0050 1.0000 35.000 1.0590 0.58872 0.58767 -0.2542 0.0050 1.0000 35.500 1.0574 0.59937 0.59834 -0.2566 0.0050 1.0000 36.000 1.0556 0.61028 0.60928 -0.2590 0.0049 1.0000 36.500 1.0535 0.62001 0.61904 -0.2612 0.0049 1.0000 37.000 1.0510 0.62940 0.62845 -0.2634 0.0049 1.0000 37.500 1.0483 0.63888 0.63796 -0.2656 0.0049 1.0000 38.000 1.0451 0.64799 0.64709 -0.2677 0.0048 1.0000 38.500 1.0417 0.65660 0.65574 -0.2698 0.0048 1.0000 39.000 1.0381 0.66560 0.66476 -0.2719 0.0047 1.0000 39.500 1.0340 0.67388 0.67307 -0.2739 0.0047 1.0000 40.000 1.0297 0.68206 0.68128 -0.2759 0.0047 1.0000 40.500 1.0252 0.69007 0.68932 -0.2778 0.0045 1.0000 41.000 1.0203 0.69781 0.69709 -0.2797 0.0044 1.0000 41.500 1.0151 0.70523 0.70453 -0.2815 0.0042 1.0000 42.000 1.0096 0.71221 0.71154 -0.2833 0.0040 1.0000 42.500 1.0038 0.71842 0.71777 -0.2851 0.0038 1.0000 43.000 0.9974 0.72379 0.72318 -0.2869 0.0038 1.0000 44.000 0.9849 0.74007 0.73949 -0.2901 0.0036 1.0000 44.500 0.9791 0.74902 0.74847 -0.2916 0.0034 1.0000 45.000 0.9724 0.75551 0.75498 -0.2931 0.0031 1.0000 45.500 0.9652 0.76105 0.76054 -0.2946 0.0029 1.0000 46.000 0.9576 0.76566 0.76518 -0.2960 0.0027 1.0000 46.500 0.9494 0.76889 0.76843 -0.2975 0.0026 1.0000 47.000 0.9408 0.77176 0.77132 -0.2988 0.0025 1.0000 47.500 0.9336 0.78067 0.78024 -0.3001 0.0025 1.0000 48.000 0.9263 0.78781 0.78740 -0.3012 0.0024 1.0000 48.500 0.9182 0.79246 0.79207 -0.3023 0.0022 1.0000 49.000 0.9095 0.79597 0.79561 -0.3035 0.0020 1.0000 49.500 0.9006 0.79868 0.79834 -0.3046 0.0018 1.0000 50.000 0.8912 0.80024 0.79992 -0.3058 0.0016 1.0000 50.500 0.8813 0.80061 0.80031 -0.3070 0.0015 1.0000 52.000 0.8530 0.80935 0.80910 -0.3096 0.0015 1.0000 52.500 0.8438 0.81223 0.81199 -0.3102 0.0014 1.0000 53.000 0.8340 0.81345 0.81323 -0.3110 0.0014 1.0000 53.500 0.8240 0.81395 0.81375 -0.3116 0.0012 1.0000 54.000 0.8136 0.81369 0.81351 -0.3123 0.0011 1.0000 54.500 0.8031 0.81273 0.81257 -0.3129 0.0010 1.0000 55.000 0.7922 0.81088 0.81073 -0.3136 0.0009 1.0000 55.500 0.7812 0.80829 0.80817 -0.3142 0.0008 1.0000 56.000 0.7698 0.80486 0.80475 -0.3149 0.0007 1.0000 57.500 0.7369 0.79943 0.79936 -0.3159 0.0006 1.0000 58.000 0.7259 0.79681 0.79675 -0.3161 0.0005 1.0000 58.500 0.7144 0.79247 0.79243 -0.3164 0.0005 1.0000 59.000 0.7027 0.78751 0.78748 -0.3166 0.0004 1.0000 59.500 0.6907 0.78150 0.78149 -0.3169 0.0003 1.0000