XFOIL Version 6.94 Calculated polar for: GOE 723 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 0.4768 0.00897 0.00254 -0.1049 0.6433 0.3912 0.500 0.5289 0.00884 0.00260 -0.1039 0.6310 0.4572 1.000 0.5811 0.00883 0.00270 -0.1028 0.6190 0.5254 1.500 0.6313 0.00864 0.00280 -0.1014 0.6070 0.6189 2.000 0.7540 0.00802 0.00293 -0.1160 0.5908 1.0000 2.500 0.8051 0.00825 0.00301 -0.1148 0.5741 1.0000 3.000 0.8557 0.00842 0.00312 -0.1134 0.5565 1.0000 3.500 0.9030 0.00865 0.00321 -0.1113 0.5254 1.0000 4.000 0.9479 0.00901 0.00336 -0.1088 0.4820 1.0000 4.500 0.9878 0.00966 0.00365 -0.1055 0.4110 1.0000 5.000 1.0214 0.01079 0.00427 -0.1013 0.3237 1.0000 5.500 1.0537 0.01206 0.00507 -0.0971 0.2395 1.0000 6.000 1.0668 0.01442 0.00662 -0.0899 0.0928 1.0000 6.500 1.0947 0.01577 0.00767 -0.0851 0.0482 1.0000 7.000 1.1284 0.01656 0.00845 -0.0811 0.0401 1.0000 7.500 1.1604 0.01736 0.00923 -0.0769 0.0336 1.0000 8.000 1.1893 0.01837 0.01019 -0.0725 0.0234 1.0000 8.500 1.2062 0.02012 0.01186 -0.0667 0.0038 1.0000 9.000 1.2330 0.02149 0.01331 -0.0628 0.0034 1.0000 9.500 1.2576 0.02311 0.01505 -0.0592 0.0032 1.0000 10.000 1.2802 0.02503 0.01711 -0.0557 0.0031 1.0000 10.500 1.3001 0.02734 0.01957 -0.0525 0.0030 1.0000 11.000 1.3164 0.03014 0.02254 -0.0496 0.0030 1.0000 11.500 1.3314 0.03325 0.02583 -0.0471 0.0030 1.0000 12.000 1.3439 0.03675 0.02951 -0.0449 0.0030 1.0000 12.500 1.3541 0.04064 0.03359 -0.0429 0.0030 1.0000 13.000 1.3625 0.04483 0.03797 -0.0412 0.0030 1.0000 13.500 1.3693 0.04938 0.04272 -0.0399 0.0030 1.0000 14.000 1.3727 0.05450 0.04805 -0.0389 0.0030 1.0000 14.500 1.3750 0.06004 0.05378 -0.0384 0.0031 1.0000 15.000 1.3743 0.06616 0.06011 -0.0383 0.0031 1.0000 15.500 1.3714 0.07286 0.06701 -0.0388 0.0031 1.0000 16.000 1.3652 0.08025 0.07461 -0.0398 0.0031 1.0000 16.500 1.3562 0.08839 0.08296 -0.0413 0.0032 1.0000 17.000 1.3455 0.09701 0.09179 -0.0434 0.0032 1.0000 17.500 1.3316 0.10647 0.10148 -0.0462 0.0032 1.0000 18.000 1.3175 0.11622 0.11144 -0.0495 0.0033 1.0000 18.500 1.3018 0.12657 0.12201 -0.0535 0.0033 1.0000 19.000 1.2869 0.13706 0.13272 -0.0580 0.0034 1.0000 19.500 1.2708 0.14811 0.14398 -0.0633 0.0034 1.0000 20.000 1.2556 0.15939 0.15546 -0.0692 0.0034 1.0000 20.500 1.2413 0.17094 0.16721 -0.0757 0.0035 1.0000 21.000 1.2283 0.18263 0.17909 -0.0826 0.0035 1.0000 21.500 1.2179 0.19421 0.19084 -0.0897 0.0036 1.0000 22.000 1.2113 0.20511 0.20189 -0.0965 0.0037 1.0000 22.500 1.2056 0.21613 0.21305 -0.1036 0.0037 1.0000 23.000 1.2021 0.22681 0.22387 -0.1107 0.0038 1.0000 23.500 1.1984 0.23793 0.23513 -0.1181 0.0040 1.0000 24.000 1.1926 0.25048 0.24782 -0.1263 0.0041 1.0000 24.500 1.1764 0.26923 0.26676 -0.1377 0.0043 1.0000 25.000 0.8938 0.32432 0.32253 -0.1466 0.0123 1.0000 25.500 0.9025 0.33126 0.32950 -0.1492 0.0120 1.0000 26.000 0.9050 0.34381 0.34206 -0.1538 0.0115 1.0000 26.500 0.9108 0.35317 0.35144 -0.1572 0.0106 1.0000 27.000 0.9169 0.36154 0.35983 -0.1604 0.0100 1.0000 27.500 0.9232 0.36929 0.36761 -0.1633 0.0098 1.0000 28.000 0.9273 0.37974 0.37808 -0.1668 0.0096 1.0000 28.500 0.9314 0.39052 0.38888 -0.1704 0.0090 1.0000 29.000 0.9360 0.39970 0.39809 -0.1736 0.0085 1.0000 29.500 0.9402 0.40864 0.40705 -0.1767 0.0082 1.0000 30.000 0.9443 0.41719 0.41563 -0.1798 0.0079 1.0000 30.500 0.9480 0.42548 0.42395 -0.1827 0.0078 1.0000 31.000 0.9521 0.43368 0.43217 -0.1853 0.0076 1.0000 31.500 0.9543 0.44344 0.44196 -0.1886 0.0076 1.0000 32.000 0.9561 0.45389 0.45244 -0.1919 0.0076 1.0000 32.500 0.9583 0.46373 0.46230 -0.1950 0.0075 1.0000 33.000 0.9602 0.47297 0.47157 -0.1980 0.0074 1.0000 33.500 0.9618 0.48217 0.48080 -0.2009 0.0072 1.0000 34.000 0.9631 0.49106 0.48972 -0.2038 0.0072 1.0000 34.500 0.9640 0.49994 0.49863 -0.2066 0.0070 1.0000 35.000 0.9646 0.50874 0.50746 -0.2095 0.0069 1.0000 35.500 0.9648 0.51746 0.51621 -0.2122 0.0067 1.0000 36.000 0.9648 0.52581 0.52459 -0.2150 0.0064 1.0000 36.500 0.9643 0.53409 0.53291 -0.2177 0.0062 1.0000 37.000 0.9635 0.54179 0.54064 -0.2204 0.0060 1.0000 38.000 0.9609 0.56018 0.55908 -0.2256 0.0058 1.0000 38.500 0.9598 0.57038 0.56931 -0.2281 0.0052 1.0000 39.000 0.9579 0.57870 0.57766 -0.2306 0.0048 1.0000 39.500 0.9553 0.58545 0.58444 -0.2331 0.0044 1.0000 40.500 0.9504 0.60524 0.60427 -0.2378 0.0041 1.0000 41.000 0.9476 0.61399 0.61305 -0.2400 0.0035 1.0000 41.500 0.9440 0.62096 0.62005 -0.2423 0.0032 1.0000 42.000 0.9397 0.62697 0.62609 -0.2447 0.0030 1.0000 42.500 0.9358 0.63632 0.63545 -0.2468 0.0029 1.0000 43.000 0.9325 0.64660 0.64576 -0.2488 0.0028 1.0000 43.500 0.9283 0.65452 0.65370 -0.2508 0.0023 1.0000 44.000 0.9234 0.66085 0.66005 -0.2529 0.0020 1.0000 44.500 0.9178 0.66613 0.66536 -0.2550 0.0019 1.0000 45.000 0.9116 0.67102 0.67028 -0.2570 0.0018 1.0000 45.500 0.9066 0.68007 0.67934 -0.2589 0.0018 1.0000 46.000 0.9016 0.68850 0.68780 -0.2606 0.0017 1.0000 46.500 0.8963 0.69611 0.69543 -0.2622 0.0016 1.0000 47.000 0.8901 0.70193 0.70127 -0.2639 0.0013 1.0000 47.500 0.8834 0.70705 0.70641 -0.2657 0.0011 1.0000 48.000 0.8764 0.71126 0.71065 -0.2673 0.0010 1.0000 48.500 0.8689 0.71467 0.71409 -0.2691 0.0009 1.0000 49.500 0.8547 0.72561 0.72506 -0.2720 0.0008 1.0000 50.000 0.8474 0.73002 0.72949 -0.2733 0.0006 1.0000 50.500 0.8394 0.73311 0.73261 -0.2747 0.0005 1.0000 51.000 0.8307 0.73459 0.73410 -0.2762 0.0004 1.0000 52.000 0.8143 0.74136 0.74091 -0.2786 0.0004 1.0000 52.500 0.8058 0.74392 0.74349 -0.2798 0.0003 1.0000 53.000 0.7969 0.74531 0.74490 -0.2809 0.0002 1.0000 53.500 0.7877 0.74584 0.74545 -0.2821 0.0000 1.0000 55.000 0.7591 0.74664 0.74630 -0.2851 0.0000 1.0000 55.500 0.7495 0.74651 0.74619 -0.2860 0.0000 1.0000 56.000 0.7396 0.74590 0.74560 -0.2868 0.0000 1.0000 56.500 0.7295 0.74451 0.74423 -0.2876 0.0000 1.0000 57.000 0.7193 0.74271 0.74244 -0.2883 0.0000 1.0000 57.500 0.7088 0.74027 0.74002 -0.2890 0.0001 1.0000 58.000 0.6983 0.73741 0.73718 -0.2897 0.0003 1.0000 58.500 0.6874 0.73375 0.73353 -0.2904 0.0005 1.0000 59.000 0.6765 0.72958 0.72939 -0.2910 0.0007 1.0000 59.500 0.6653 0.72474 0.72456 -0.2916 0.0009 1.0000 60.000 0.6536 0.71897 0.71880 -0.2923 0.0010 1.0000