XFOIL Version 6.94 Calculated polar for: GOE 567 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 0.6308 0.00957 0.00316 -0.1441 0.6149 0.4368 0.500 0.6854 0.00968 0.00322 -0.1436 0.6019 0.4616 1.000 0.7399 0.00976 0.00334 -0.1432 0.5889 0.4845 1.500 0.7939 0.00995 0.00347 -0.1427 0.5761 0.5086 2.000 0.8477 0.01003 0.00365 -0.1421 0.5639 0.5313 2.500 0.9005 0.01021 0.00383 -0.1414 0.5506 0.5534 3.000 0.9433 0.01041 0.00385 -0.1387 0.5062 0.5761 3.500 0.9853 0.01079 0.00406 -0.1359 0.4556 0.6009 4.000 1.0276 0.01125 0.00440 -0.1334 0.4144 0.6308 4.500 1.0565 0.01220 0.00504 -0.1286 0.3334 0.6720 5.000 1.0274 0.01462 0.00696 -0.1137 0.1394 0.8655 5.500 1.0557 0.01591 0.00804 -0.1095 0.1003 1.0000 6.000 1.0783 0.01725 0.00915 -0.1045 0.0541 1.0000 6.500 1.0946 0.01897 0.01069 -0.0988 0.0164 1.0000 7.000 1.1196 0.02041 0.01212 -0.0948 0.0039 1.0000 7.500 1.1477 0.02178 0.01354 -0.0914 0.0036 1.0000 8.000 1.1738 0.02338 0.01521 -0.0881 0.0035 1.0000 8.500 1.1978 0.02526 0.01718 -0.0850 0.0035 1.0000 9.000 1.2195 0.02744 0.01946 -0.0819 0.0036 1.0000 9.500 1.2392 0.02994 0.02207 -0.0791 0.0036 1.0000 10.000 1.2569 0.03277 0.02502 -0.0765 0.0038 1.0000 10.500 1.2722 0.03597 0.02836 -0.0741 0.0039 1.0000 11.000 1.2852 0.03956 0.03210 -0.0719 0.0040 1.0000 11.500 1.2959 0.04358 0.03628 -0.0701 0.0042 1.0000 12.000 1.3040 0.04811 0.04098 -0.0685 0.0044 1.0000 12.500 1.3088 0.05328 0.04631 -0.0673 0.0045 1.0000 13.000 1.3073 0.05951 0.05272 -0.0666 0.0046 1.0000 13.500 1.3133 0.06518 0.05852 -0.0665 0.0047 1.0000 14.000 1.3263 0.07019 0.06368 -0.0665 0.0051 1.0000 14.500 1.3280 0.07689 0.07055 -0.0671 0.0053 1.0000 15.000 1.3262 0.08438 0.07821 -0.0682 0.0057 1.0000 15.500 1.3221 0.09238 0.08636 -0.0697 0.0060 1.0000 16.000 1.3193 0.10021 0.09427 -0.0712 0.0062 1.0000 16.500 1.3300 0.10636 0.10057 -0.0728 0.0065 1.0000 17.000 1.3419 0.11220 0.10660 -0.0741 0.0073 1.0000 17.500 1.3633 0.11534 0.10967 -0.0734 0.0081 1.0000 18.000 1.3722 0.12227 0.11694 -0.0759 0.0090 1.0000 18.500 1.4032 0.12408 0.11881 -0.0748 0.0105 1.0000 19.000 1.2345 0.14041 0.13641 -0.0889 0.0102 1.0000 19.500 1.2408 0.14579 0.14224 -0.0909 0.0128 1.0000 20.000 1.2078 0.15891 0.15610 -0.0979 0.0158 1.0000 20.500 1.1632 0.17554 0.17317 -0.1084 0.0158 1.0000 21.000 1.1068 0.19730 0.19536 -0.1219 0.0158 1.0000 21.500 1.0688 0.21658 0.21486 -0.1330 0.0154 1.0000 22.500 0.9423 0.30240 0.30086 -0.1644 0.0213 1.0000 23.000 0.9436 0.31506 0.31351 -0.1690 0.0188 1.0000 23.500 0.9542 0.32153 0.32000 -0.1711 0.0180 1.0000 24.000 0.9547 0.33467 0.33315 -0.1758 0.0156 1.0000 24.500 0.9590 0.34591 0.34439 -0.1794 0.0142 1.0000 25.000 0.9652 0.35486 0.35335 -0.1825 0.0129 1.0000 26.000 0.9743 0.37614 0.37466 -0.1891 0.0107 1.0000 26.500 0.9816 0.38306 0.38160 -0.1915 0.0102 1.0000 27.000 0.9830 0.39761 0.39615 -0.1955 0.0093 1.0000 27.500 0.9877 0.40711 0.40566 -0.1985 0.0085 1.0000 28.000 0.9929 0.41511 0.41368 -0.2011 0.0082 1.0000 28.500 0.9967 0.42542 0.42400 -0.2039 0.0080 1.0000 29.000 0.9985 0.43936 0.43796 -0.2076 0.0074 1.0000 29.500 1.0017 0.44960 0.44822 -0.2105 0.0069 1.0000 30.000 1.0048 0.45953 0.45817 -0.2133 0.0067 1.0000 30.500 1.0079 0.46784 0.46650 -0.2159 0.0064 1.0000 31.000 1.0111 0.47634 0.47502 -0.2183 0.0063 1.0000 31.500 1.0127 0.48717 0.48587 -0.2211 0.0062 1.0000 32.000 1.0136 0.49867 0.49738 -0.2241 0.0062 1.0000 32.500 1.0146 0.51016 0.50890 -0.2270 0.0061 1.0000 33.000 1.0157 0.52090 0.51965 -0.2298 0.0060 1.0000 33.500 1.0165 0.53048 0.52926 -0.2324 0.0060 1.0000 34.000 1.0170 0.54126 0.54006 -0.2350 0.0057 1.0000 34.500 1.0171 0.55087 0.54969 -0.2376 0.0057 1.0000 35.000 1.0170 0.56046 0.55931 -0.2401 0.0056 1.0000 35.500 1.0164 0.56972 0.56859 -0.2426 0.0056 1.0000 36.000 1.0156 0.57907 0.57796 -0.2450 0.0055 1.0000 36.500 1.0144 0.58825 0.58717 -0.2475 0.0055 1.0000 37.000 1.0129 0.59697 0.59591 -0.2499 0.0055 1.0000 37.500 1.0111 0.60589 0.60486 -0.2522 0.0054 1.0000 38.000 1.0088 0.61409 0.61309 -0.2545 0.0055 1.0000 38.500 1.0064 0.62255 0.62157 -0.2568 0.0054 1.0000 39.000 1.0036 0.63069 0.62974 -0.2590 0.0054 1.0000 39.500 1.0005 0.63856 0.63763 -0.2612 0.0054 1.0000 40.000 0.9971 0.64625 0.64535 -0.2634 0.0054 1.0000 40.500 0.9934 0.65365 0.65278 -0.2656 0.0053 1.0000 41.000 0.9894 0.66102 0.66018 -0.2677 0.0052 1.0000 41.500 0.9851 0.66789 0.66707 -0.2697 0.0051 1.0000 42.000 0.9804 0.67417 0.67338 -0.2717 0.0049 1.0000 42.500 0.9754 0.68024 0.67948 -0.2737 0.0048 1.0000 43.000 0.9700 0.68552 0.68478 -0.2756 0.0047 1.0000 44.000 0.9588 0.70041 0.69972 -0.2792 0.0046 1.0000 44.500 0.9536 0.70904 0.70837 -0.2810 0.0044 1.0000 45.000 0.9478 0.71580 0.71516 -0.2826 0.0041 1.0000 45.500 0.9414 0.72131 0.72069 -0.2843 0.0038 1.0000 46.000 0.9347 0.72623 0.72563 -0.2859 0.0036 1.0000 46.500 0.9277 0.73014 0.72957 -0.2876 0.0034 1.0000 47.000 0.9201 0.73303 0.73248 -0.2892 0.0033 1.0000 48.000 0.9053 0.74419 0.74368 -0.2920 0.0032 1.0000 48.500 0.8982 0.75024 0.74974 -0.2933 0.0031 1.0000 49.000 0.8907 0.75499 0.75452 -0.2946 0.0028 1.0000 49.500 0.8825 0.75820 0.75775 -0.2958 0.0025 1.0000 50.000 0.8740 0.76045 0.76002 -0.2971 0.0023 1.0000 50.500 0.8651 0.76159 0.76118 -0.2984 0.0021 1.0000 51.000 0.8559 0.76208 0.76170 -0.2997 0.0020 1.0000 52.000 0.8377 0.76693 0.76657 -0.3018 0.0019 1.0000 52.500 0.8289 0.77004 0.76971 -0.3026 0.0019 1.0000 53.000 0.8199 0.77203 0.77171 -0.3035 0.0019 1.0000 53.500 0.8106 0.77322 0.77292 -0.3043 0.0018 1.0000 54.000 0.8009 0.77335 0.77306 -0.3051 0.0016 1.0000 54.500 0.7911 0.77309 0.77283 -0.3059 0.0014 1.0000 55.000 0.7809 0.77194 0.77169 -0.3067 0.0013 1.0000 55.500 0.7706 0.77002 0.76979 -0.3074 0.0011 1.0000 56.000 0.7599 0.76718 0.76697 -0.3082 0.0010 1.0000 56.500 0.7490 0.76371 0.76351 -0.3089 0.0010 1.0000 57.500 0.7281 0.76156 0.76138 -0.3098 0.0009 1.0000 58.000 0.7176 0.75870 0.75854 -0.3101 0.0008 1.0000 58.500 0.7068 0.75561 0.75546 -0.3105 0.0007 1.0000 59.000 0.6957 0.75123 0.75110 -0.3109 0.0006 1.0000 59.500 0.6843 0.74593 0.74581 -0.3112 0.0005 1.0000