XFOIL Version 6.94 Calculated polar for: GOE 534 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.5432 0.01194 0.00425 -0.0938 0.4805 0.3032 0.500 0.5973 0.01213 0.00446 -0.0927 0.4636 0.3465 1.500 0.7045 0.01255 0.00488 -0.0904 0.4303 0.4121 2.000 0.7575 0.01282 0.00510 -0.0891 0.4133 0.4431 2.500 0.8093 0.01311 0.00534 -0.0878 0.3960 0.4720 3.000 0.8610 0.01326 0.00554 -0.0864 0.3781 0.5028 3.500 0.9118 0.01347 0.00581 -0.0849 0.3600 0.5380 4.000 0.9608 0.01367 0.00613 -0.0832 0.3418 0.5864 5.000 1.0797 0.01401 0.00693 -0.0843 0.3054 1.0000 5.500 1.1280 0.01459 0.00741 -0.0826 0.2906 1.0000 6.000 1.1756 0.01522 0.00799 -0.0808 0.2776 1.0000 6.500 1.2200 0.01589 0.00854 -0.0787 0.2619 1.0000 7.000 1.2622 0.01651 0.00904 -0.0762 0.2423 1.0000 7.500 1.3024 0.01720 0.00962 -0.0735 0.2227 1.0000 8.000 1.3397 0.01808 0.01040 -0.0705 0.2097 1.0000 8.500 1.3786 0.01878 0.01115 -0.0676 0.1996 1.0000 9.000 1.4060 0.01972 0.01200 -0.0631 0.1817 1.0000 9.500 1.4337 0.02076 0.01304 -0.0588 0.1715 1.0000 10.000 1.4580 0.02204 0.01430 -0.0546 0.1589 1.0000 10.500 1.4766 0.02377 0.01595 -0.0505 0.1396 1.0000 11.000 1.4909 0.02602 0.01816 -0.0467 0.1247 1.0000 11.500 1.5028 0.02878 0.02093 -0.0436 0.1123 1.0000 12.000 1.5085 0.03242 0.02457 -0.0411 0.0975 1.0000 12.500 1.5071 0.03714 0.02929 -0.0394 0.0836 1.0000 13.000 1.5007 0.04278 0.03497 -0.0386 0.0702 1.0000 13.500 1.4884 0.04957 0.04185 -0.0386 0.0596 1.0000 14.000 1.4760 0.05691 0.04932 -0.0395 0.0527 1.0000 14.500 1.4408 0.06770 0.06019 -0.0420 0.0383 1.0000 15.000 1.3961 0.08060 0.07321 -0.0458 0.0230 1.0000 15.500 1.3622 0.09269 0.08548 -0.0498 0.0143 1.0000 16.000 1.3289 0.10539 0.09839 -0.0546 0.0063 1.0000 16.500 1.3041 0.11723 0.11045 -0.0593 0.0032 1.0000 17.000 1.2884 0.12777 0.12120 -0.0638 0.0027 1.0000 17.500 1.2764 0.13788 0.13152 -0.0684 0.0026 1.0000 18.000 1.2662 0.14780 0.14163 -0.0732 0.0025 1.0000 18.500 1.2574 0.15756 0.15157 -0.0782 0.0025 1.0000 19.000 1.2506 0.16705 0.16124 -0.0833 0.0024 1.0000 19.500 1.2448 0.17641 0.17078 -0.0886 0.0024 1.0000 20.000 1.2396 0.18568 0.18022 -0.0940 0.0024 1.0000 20.500 1.2351 0.19491 0.18961 -0.0995 0.0023 1.0000 21.000 1.2311 0.20412 0.19899 -0.1052 0.0023 1.0000 21.500 1.2276 0.21331 0.20834 -0.1109 0.0023 1.0000 22.000 1.2253 0.22229 0.21747 -0.1167 0.0023 1.0000 22.500 1.2240 0.23108 0.22640 -0.1223 0.0023 1.0000 23.000 1.2230 0.23988 0.23534 -0.1281 0.0023 1.0000 23.500 1.2234 0.24835 0.24395 -0.1337 0.0023 1.0000 24.000 1.2249 0.25658 0.25230 -0.1393 0.0023 1.0000 24.500 1.2276 0.26452 0.26036 -0.1447 0.0024 1.0000 25.000 1.2314 0.27215 0.26808 -0.1499 0.0024 1.0000 25.500 1.2369 0.27924 0.27525 -0.1550 0.0024 1.0000 26.000 1.2437 0.28580 0.28188 -0.1598 0.0024 1.0000 26.500 1.2520 0.29172 0.28786 -0.1643 0.0024 1.0000 27.000 1.2618 0.29687 0.29305 -0.1686 0.0024 1.0000 27.500 1.2731 0.30126 0.29747 -0.1725 0.0024 1.0000 28.000 1.2856 0.30487 0.30110 -0.1762 0.0025 1.0000 28.500 1.2999 0.30754 0.30378 -0.1794 0.0025 1.0000 29.000 1.3150 0.30966 0.30592 -0.1825 0.0025 1.0000 29.500 1.3313 0.31113 0.30739 -0.1853 0.0025 1.0000 30.000 1.3470 0.31267 0.30893 -0.1881 0.0025 1.0000 30.500 1.3618 0.31444 0.31071 -0.1912 0.0026 1.0000 31.000 1.3761 0.31620 0.31250 -0.1942 0.0026 1.0000 31.500 1.3890 0.31831 0.31465 -0.1976 0.0026 1.0000 32.000 1.4006 0.32072 0.31710 -0.2011 0.0026 1.0000 32.500 1.4138 0.32226 0.31868 -0.2043 0.0027 1.0000 33.000 1.4222 0.32576 0.32227 -0.2086 0.0027 1.0000 33.500 1.4245 0.33172 0.32838 -0.2143 0.0028 1.0000 34.000 1.4214 0.34027 0.33718 -0.2213 0.0029 1.0000 34.500 1.3903 0.36645 0.36388 -0.2364 0.0036 1.0000 35.000 1.0025 0.53240 0.53090 -0.2247 0.0097 1.0000 35.500 1.0035 0.53943 0.53797 -0.2269 0.0095 1.0000 36.000 1.0007 0.55442 0.55298 -0.2301 0.0090 1.0000 36.500 0.9998 0.56417 0.56275 -0.2326 0.0085 1.0000 37.000 0.9986 0.57270 0.57132 -0.2351 0.0081 1.0000 37.500 0.9977 0.57956 0.57822 -0.2375 0.0078 1.0000 38.000 0.9961 0.58817 0.58685 -0.2399 0.0077 1.0000 38.500 0.9929 0.60026 0.59897 -0.2425 0.0075 1.0000 39.000 0.9904 0.61066 0.60940 -0.2449 0.0070 1.0000 39.500 0.9875 0.61893 0.61770 -0.2472 0.0068 1.0000 40.000 0.9845 0.62692 0.62573 -0.2495 0.0066 1.0000 40.500 0.9812 0.63418 0.63302 -0.2518 0.0064 1.0000 41.000 0.9776 0.64063 0.63950 -0.2539 0.0063 1.0000 42.000 0.9691 0.65645 0.65539 -0.2583 0.0061 1.0000 42.500 0.9644 0.66607 0.66504 -0.2604 0.0060 1.0000 43.000 0.9597 0.67421 0.67320 -0.2624 0.0057 1.0000 43.500 0.9546 0.68100 0.68003 -0.2644 0.0054 1.0000 44.000 0.9492 0.68653 0.68559 -0.2664 0.0050 1.0000 44.500 0.9435 0.69093 0.69003 -0.2683 0.0049 1.0000 45.000 0.9375 0.69847 0.69759 -0.2701 0.0048 1.0000 45.500 0.9317 0.70826 0.70741 -0.2719 0.0045 1.0000 46.000 0.9255 0.71429 0.71347 -0.2737 0.0042 1.0000 46.500 0.9188 0.71867 0.71788 -0.2754 0.0039 1.0000 47.000 0.9117 0.72153 0.72078 -0.2771 0.0037 1.0000 47.500 0.9047 0.72965 0.72892 -0.2787 0.0036 1.0000 48.000 0.8977 0.73646 0.73576 -0.2801 0.0034 1.0000 48.500 0.8902 0.74100 0.74032 -0.2816 0.0031 1.0000 49.000 0.8823 0.74362 0.74298 -0.2832 0.0028 1.0000 49.500 0.8740 0.74498 0.74436 -0.2847 0.0027 1.0000 50.000 0.8661 0.75190 0.75130 -0.2860 0.0027 1.0000 50.500 0.8582 0.75738 0.75681 -0.2871 0.0025 1.0000 51.000 0.8497 0.76028 0.75974 -0.2884 0.0022 1.0000 51.500 0.8408 0.76166 0.76114 -0.2897 0.0020 1.0000 52.000 0.8315 0.76159 0.76110 -0.2910 0.0019 1.0000 53.000 0.8135 0.76799 0.76753 -0.2930 0.0018 1.0000 53.500 0.8043 0.77007 0.76964 -0.2940 0.0017 1.0000 54.000 0.7947 0.77087 0.77046 -0.2949 0.0015 1.0000 54.500 0.7849 0.77048 0.77010 -0.2959 0.0014 1.0000 55.000 0.7746 0.76882 0.76846 -0.2968 0.0013 1.0000 55.500 0.7641 0.76615 0.76581 -0.2978 0.0012 1.0000 56.500 0.7437 0.76619 0.76588 -0.2992 0.0012 1.0000 57.000 0.7335 0.76551 0.76523 -0.2998 0.0012 1.0000 57.500 0.7231 0.76397 0.76370 -0.3003 0.0011 1.0000 58.000 0.7124 0.76164 0.76140 -0.3009 0.0010 1.0000 58.500 0.7015 0.75834 0.75812 -0.3014 0.0009 1.0000 59.000 0.6904 0.75425 0.75405 -0.3019 0.0008 1.0000 59.500 0.6792 0.74940 0.74921 -0.3024 0.0008 1.0000 60.000 0.6678 0.74405 0.74388 -0.3029 0.0007 1.0000