XFOIL Version 6.94 Calculated polar for: GOE 701 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 0.5174 0.00981 0.00295 -0.1060 0.6929 0.1842 0.500 0.5655 0.00964 0.00286 -0.1041 0.6746 0.2097 1.000 0.6145 0.00952 0.00283 -0.1024 0.6588 0.2488 1.500 0.6606 0.00929 0.00287 -0.1003 0.6410 0.3557 2.000 0.8163 0.00835 0.00342 -0.1217 0.6170 0.9961 2.500 0.8761 0.00856 0.00350 -0.1225 0.5946 1.0000 3.000 0.9148 0.00880 0.00363 -0.1188 0.5708 1.0000 3.500 0.9347 0.00936 0.00380 -0.1112 0.5026 1.0000 4.000 0.9621 0.00988 0.00409 -0.1054 0.4574 1.0000 4.500 0.9653 0.01104 0.00464 -0.0949 0.3538 1.0000 5.000 0.9768 0.01189 0.00516 -0.0861 0.2976 1.0000 5.500 0.9962 0.01275 0.00576 -0.0792 0.2540 1.0000 6.000 1.0171 0.01375 0.00648 -0.0729 0.2119 1.0000 6.500 1.0425 0.01471 0.00722 -0.0677 0.1774 1.0000 7.000 1.0645 0.01593 0.00816 -0.0623 0.1337 1.0000 7.500 1.0700 0.01814 0.00991 -0.0548 0.0617 1.0000 8.000 1.0815 0.02030 0.01183 -0.0488 0.0045 1.0000 8.500 1.1114 0.02152 0.01309 -0.0455 0.0032 1.0000 9.000 1.1407 0.02284 0.01449 -0.0423 0.0030 1.0000 9.500 1.1687 0.02432 0.01607 -0.0393 0.0029 1.0000 10.000 1.1949 0.02602 0.01788 -0.0363 0.0028 1.0000 10.500 1.2190 0.02796 0.01995 -0.0333 0.0029 1.0000 11.000 1.2407 0.03017 0.02230 -0.0305 0.0029 1.0000 11.500 1.2598 0.03270 0.02498 -0.0278 0.0029 1.0000 12.000 1.2763 0.03558 0.02801 -0.0254 0.0030 1.0000 12.500 1.2902 0.03884 0.03143 -0.0231 0.0031 1.0000 13.000 1.3005 0.04262 0.03538 -0.0211 0.0031 1.0000 13.500 1.3074 0.04696 0.03991 -0.0195 0.0032 1.0000 14.000 1.3095 0.05207 0.04523 -0.0183 0.0034 1.0000 14.500 1.3063 0.05814 0.05151 -0.0177 0.0035 1.0000 15.000 1.2989 0.06504 0.05863 -0.0178 0.0035 1.0000 15.500 1.2848 0.07327 0.06710 -0.0188 0.0036 1.0000 16.000 1.2673 0.08236 0.07642 -0.0204 0.0037 1.0000 16.500 1.2482 0.09213 0.08642 -0.0228 0.0037 1.0000 17.000 1.2237 0.10305 0.09756 -0.0260 0.0038 1.0000 17.500 1.2032 0.11365 0.10838 -0.0294 0.0038 1.0000 18.000 1.1841 0.12415 0.11904 -0.0331 0.0039 1.0000 18.500 1.1726 0.13347 0.12850 -0.0367 0.0039 1.0000 19.000 1.1666 0.14156 0.13668 -0.0398 0.0040 1.0000 19.500 1.1695 0.14771 0.14287 -0.0420 0.0041 1.0000 20.000 1.1723 0.15494 0.15024 -0.0454 0.0043 1.0000 20.500 1.1778 0.16145 0.15693 -0.0485 0.0046 1.0000 21.000 1.1860 0.16697 0.16258 -0.0510 0.0048 1.0000 21.500 1.1958 0.17182 0.16755 -0.0531 0.0052 1.0000 22.000 1.2155 0.17383 0.16959 -0.0531 0.0057 1.0000 22.500 1.2136 0.18244 0.17844 -0.0586 0.0059 1.0000 23.000 1.2031 0.19307 0.18951 -0.0651 0.0066 1.0000 23.500 1.1934 0.20338 0.20007 -0.0717 0.0071 1.0000 24.000 1.1858 0.21413 0.21108 -0.0788 0.0077 1.0000 24.500 1.1319 0.24149 0.23892 -0.0967 0.0079 1.0000 25.500 0.8450 0.31131 0.30949 -0.1268 0.0135 1.0000 26.000 0.8515 0.31990 0.31810 -0.1303 0.0123 1.0000 26.500 0.8607 0.32597 0.32420 -0.1331 0.0118 1.0000 27.000 0.8623 0.33872 0.33696 -0.1376 0.0106 1.0000 27.500 0.8685 0.34692 0.34518 -0.1409 0.0099 1.0000 28.000 0.8761 0.35333 0.35162 -0.1437 0.0095 1.0000 28.500 0.8783 0.36586 0.36416 -0.1479 0.0088 1.0000 29.000 0.8832 0.37482 0.37314 -0.1512 0.0080 1.0000 29.500 0.8885 0.38243 0.38078 -0.1544 0.0076 1.0000 30.000 0.8946 0.38908 0.38746 -0.1571 0.0074 1.0000 30.500 0.8964 0.40097 0.39936 -0.1609 0.0072 1.0000 31.000 0.8998 0.41125 0.40966 -0.1643 0.0068 1.0000 31.500 0.9033 0.42034 0.41878 -0.1675 0.0064 1.0000 32.000 0.9065 0.42888 0.42734 -0.1707 0.0061 1.0000 32.500 0.9094 0.43718 0.43567 -0.1738 0.0059 1.0000 33.000 0.9122 0.44464 0.44315 -0.1767 0.0057 1.0000 34.000 0.9166 0.46119 0.45975 -0.1825 0.0056 1.0000 34.500 0.9176 0.47051 0.46909 -0.1857 0.0056 1.0000 35.000 0.9184 0.47990 0.47851 -0.1888 0.0055 1.0000 35.500 0.9193 0.48778 0.48642 -0.1917 0.0056 1.0000 36.000 0.9197 0.49711 0.49577 -0.1947 0.0055 1.0000 36.500 0.9199 0.50541 0.50410 -0.1976 0.0055 1.0000 37.000 0.9199 0.51359 0.51231 -0.2005 0.0055 1.0000 37.500 0.9194 0.52142 0.52017 -0.2033 0.0054 1.0000 38.000 0.9187 0.52912 0.52790 -0.2061 0.0054 1.0000 38.500 0.9176 0.53680 0.53560 -0.2088 0.0054 1.0000 39.000 0.9162 0.54416 0.54299 -0.2115 0.0054 1.0000 39.500 0.9146 0.55166 0.55052 -0.2142 0.0053 1.0000 40.000 0.9125 0.55867 0.55756 -0.2168 0.0053 1.0000 40.500 0.9101 0.56546 0.56438 -0.2194 0.0053 1.0000 41.000 0.9075 0.57242 0.57137 -0.2219 0.0052 1.0000 41.500 0.9047 0.57910 0.57808 -0.2244 0.0050 1.0000 42.000 0.9015 0.58557 0.58459 -0.2269 0.0047 1.0000 42.500 0.8979 0.59160 0.59065 -0.2293 0.0045 1.0000 43.000 0.8940 0.59723 0.59630 -0.2317 0.0043 1.0000 43.500 0.8896 0.60210 0.60120 -0.2340 0.0042 1.0000 44.500 0.8804 0.61474 0.61389 -0.2385 0.0041 1.0000 45.000 0.8761 0.62245 0.62163 -0.2405 0.0039 1.0000 45.500 0.8713 0.62853 0.62774 -0.2426 0.0036 1.0000 46.000 0.8659 0.63355 0.63278 -0.2447 0.0033 1.0000 46.500 0.8602 0.63795 0.63721 -0.2467 0.0031 1.0000 47.000 0.8539 0.64119 0.64047 -0.2488 0.0029 1.0000 47.500 0.8472 0.64376 0.64307 -0.2508 0.0028 1.0000 48.500 0.8349 0.65563 0.65498 -0.2543 0.0027 1.0000 49.000 0.8287 0.66083 0.66020 -0.2559 0.0025 1.0000 49.500 0.8218 0.66445 0.66385 -0.2576 0.0022 1.0000 50.000 0.8144 0.66695 0.66637 -0.2593 0.0020 1.0000 50.500 0.8067 0.66874 0.66819 -0.2610 0.0018 1.0000 51.000 0.7985 0.66945 0.66892 -0.2627 0.0017 1.0000 52.000 0.7824 0.67468 0.67419 -0.2656 0.0017 1.0000 52.500 0.7747 0.67783 0.67736 -0.2669 0.0016 1.0000 53.000 0.7666 0.68001 0.67956 -0.2681 0.0016 1.0000 53.500 0.7583 0.68148 0.68105 -0.2693 0.0015 1.0000 54.000 0.7496 0.68221 0.68180 -0.2705 0.0013 1.0000 54.500 0.7406 0.68210 0.68171 -0.2717 0.0011 1.0000 55.000 0.7314 0.68146 0.68109 -0.2729 0.0010 1.0000 55.500 0.7219 0.68006 0.67971 -0.2740 0.0009 1.0000 56.000 0.7121 0.67788 0.67755 -0.2752 0.0008 1.0000 56.500 0.7018 0.67482 0.67451 -0.2763 0.0008 1.0000 57.000 0.6925 0.67578 0.67548 -0.2770 0.0007 1.0000 57.500 0.6834 0.67518 0.67489 -0.2777 0.0007 1.0000 58.000 0.6736 0.67314 0.67287 -0.2784 0.0006 1.0000 58.500 0.6634 0.67006 0.66981 -0.2792 0.0005 1.0000 59.000 0.6530 0.66625 0.66602 -0.2799 0.0004 1.0000