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 = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.7632 0.01097 0.00434 -0.1730 0.7230 0.3667 0.500 0.8142 0.01090 0.00433 -0.1716 0.7038 0.4048 1.000 0.8653 0.01082 0.00432 -0.1704 0.6810 0.4442 1.500 0.9152 0.01076 0.00431 -0.1689 0.6540 0.4909 2.000 0.9626 0.01077 0.00442 -0.1669 0.6222 0.5563 2.500 1.0074 0.01080 0.00461 -0.1645 0.5899 0.6699 3.000 1.0518 0.01071 0.00478 -0.1618 0.5625 1.0000 3.500 1.0994 0.01129 0.00513 -0.1602 0.5402 1.0000 4.000 1.1398 0.01191 0.00554 -0.1572 0.5076 1.0000 4.500 1.1780 0.01253 0.00597 -0.1538 0.4773 1.0000 5.000 1.2059 0.01321 0.00641 -0.1484 0.4371 1.0000 5.500 1.2407 0.01380 0.00693 -0.1445 0.4154 1.0000 6.000 1.2638 0.01471 0.00761 -0.1387 0.3725 1.0000 6.500 1.2859 0.01588 0.00853 -0.1331 0.3234 1.0000 7.000 1.2858 0.01834 0.01036 -0.1248 0.2176 1.0000 7.500 1.2948 0.02080 0.01246 -0.1186 0.1642 1.0000 8.000 1.3159 0.02270 0.01424 -0.1142 0.1398 1.0000 8.500 1.3335 0.02493 0.01624 -0.1098 0.0907 1.0000 9.000 1.3343 0.02849 0.01954 -0.1042 0.0465 1.0000 9.500 1.3340 0.03253 0.02337 -0.0992 0.0047 1.0000 10.000 1.3547 0.03514 0.02609 -0.0964 0.0039 1.0000 10.500 1.3740 0.03800 0.02909 -0.0938 0.0037 1.0000 11.000 1.3913 0.04121 0.03246 -0.0914 0.0036 1.0000 11.500 1.4059 0.04484 0.03629 -0.0892 0.0035 1.0000 12.000 1.4179 0.04895 0.04059 -0.0873 0.0035 1.0000 12.500 1.4275 0.05357 0.04541 -0.0857 0.0035 1.0000 13.000 1.4349 0.05870 0.05077 -0.0846 0.0036 1.0000 13.500 1.4403 0.06439 0.05668 -0.0839 0.0036 1.0000 14.000 1.4431 0.07074 0.06327 -0.0838 0.0036 1.0000 14.500 1.4443 0.07766 0.07044 -0.0842 0.0036 1.0000 15.000 1.4427 0.08528 0.07831 -0.0852 0.0037 1.0000 15.500 1.4378 0.09370 0.08699 -0.0869 0.0037 1.0000 16.000 1.4338 0.10222 0.09576 -0.0891 0.0037 1.0000 16.500 1.4293 0.11099 0.10476 -0.0917 0.0038 1.0000 17.000 1.4244 0.11999 0.11399 -0.0948 0.0038 1.0000 17.500 1.4191 0.12918 0.12340 -0.0984 0.0039 1.0000 18.000 1.4138 0.13844 0.13288 -0.1025 0.0040 1.0000 18.500 1.4082 0.14782 0.14246 -0.1069 0.0041 1.0000 19.000 1.4037 0.15699 0.15181 -0.1115 0.0042 1.0000 19.500 1.4013 0.16565 0.16064 -0.1161 0.0043 1.0000 20.000 1.4018 0.17360 0.16872 -0.1205 0.0044 1.0000 20.500 1.4054 0.18072 0.17595 -0.1245 0.0046 1.0000 21.000 1.4132 0.18664 0.18197 -0.1279 0.0047 1.0000 21.500 1.4239 0.19165 0.18705 -0.1307 0.0049 1.0000 22.000 1.4503 0.19192 0.18726 -0.1299 0.0051 1.0000 22.500 1.4478 0.20097 0.19655 -0.1362 0.0052 1.0000 23.000 1.4434 0.21049 0.20636 -0.1430 0.0054 1.0000 23.500 1.4370 0.22049 0.21669 -0.1501 0.0056 1.0000 24.000 1.4275 0.23132 0.22784 -0.1580 0.0059 1.0000 24.500 1.4137 0.24360 0.24042 -0.1670 0.0061 1.0000 25.000 1.3953 0.25796 0.25506 -0.1773 0.0062 1.0000 25.500 1.3418 0.28879 0.28626 -0.1962 0.0065 1.0000 26.000 1.0301 0.39601 0.39431 -0.2046 0.0170 1.0000 26.500 1.0351 0.40525 0.40356 -0.2071 0.0160 1.0000 27.000 1.0427 0.41314 0.41148 -0.2087 0.0157 1.0000 27.500 1.0405 0.42904 0.42739 -0.2135 0.0141 1.0000 28.000 1.0448 0.43819 0.43657 -0.2160 0.0132 1.0000 28.500 1.0498 0.44664 0.44504 -0.2179 0.0130 1.0000 29.000 1.0488 0.46202 0.46043 -0.2221 0.0118 1.0000 29.500 1.0514 0.47218 0.47062 -0.2247 0.0111 1.0000 30.500 1.0550 0.49377 0.49226 -0.2301 0.0104 1.0000 31.000 1.0562 0.50571 0.50422 -0.2329 0.0097 1.0000 31.500 1.0573 0.51611 0.51465 -0.2355 0.0092 1.0000 32.000 1.0583 0.52579 0.52436 -0.2380 0.0088 1.0000 32.500 1.0593 0.53427 0.53287 -0.2401 0.0085 1.0000 33.000 1.0589 0.54621 0.54483 -0.2428 0.0084 1.0000 33.500 1.0584 0.55789 0.55654 -0.2455 0.0083 1.0000 34.000 1.0579 0.56914 0.56781 -0.2481 0.0080 1.0000 34.500 1.0571 0.57919 0.57789 -0.2505 0.0078 1.0000 35.000 1.0561 0.58937 0.58811 -0.2528 0.0076 1.0000 35.500 1.0546 0.59903 0.59779 -0.2552 0.0073 1.0000 36.000 1.0528 0.60854 0.60734 -0.2574 0.0071 1.0000 36.500 1.0507 0.61768 0.61651 -0.2597 0.0070 1.0000 37.000 1.0482 0.62654 0.62540 -0.2619 0.0069 1.0000 37.500 1.0455 0.63507 0.63397 -0.2640 0.0068 1.0000 38.000 1.0424 0.64268 0.64162 -0.2658 0.0067 1.0000 39.500 1.0311 0.66970 0.66872 -0.2722 0.0066 1.0000 40.000 1.0268 0.67825 0.67730 -0.2743 0.0066 1.0000 40.500 1.0223 0.68687 0.68595 -0.2763 0.0066 1.0000 41.000 1.0176 0.69534 0.69446 -0.2783 0.0065 1.0000 41.500 1.0128 0.70358 0.70273 -0.2801 0.0063 1.0000 42.000 1.0075 0.71132 0.71050 -0.2819 0.0061 1.0000 42.500 1.0020 0.71871 0.71792 -0.2837 0.0057 1.0000 43.000 0.9961 0.72529 0.72454 -0.2855 0.0054 1.0000 43.500 0.9897 0.73100 0.73028 -0.2871 0.0052 1.0000 44.000 0.9828 0.73596 0.73527 -0.2886 0.0051 1.0000 44.500 0.9765 0.74506 0.74439 -0.2904 0.0050 1.0000 45.000 0.9704 0.75326 0.75262 -0.2918 0.0048 1.0000 45.500 0.9635 0.75956 0.75894 -0.2933 0.0045 1.0000 46.000 0.9562 0.76504 0.76446 -0.2947 0.0042 1.0000 46.500 0.9484 0.76945 0.76889 -0.2962 0.0039 1.0000 47.000 0.9402 0.77296 0.77243 -0.2976 0.0038 1.0000 48.000 0.9247 0.78533 0.78484 -0.3001 0.0036 1.0000 48.500 0.9166 0.79008 0.78962 -0.3012 0.0034 1.0000 49.000 0.9081 0.79377 0.79333 -0.3024 0.0032 1.0000 49.500 0.8992 0.79687 0.79646 -0.3035 0.0029 1.0000 50.000 0.8900 0.79879 0.79840 -0.3046 0.0027 1.0000 50.500 0.8801 0.79948 0.79912 -0.3058 0.0025 1.0000 51.500 0.8617 0.80596 0.80564 -0.3076 0.0025 1.0000 52.000 0.8524 0.80846 0.80816 -0.3084 0.0024 1.0000 52.500 0.8430 0.81049 0.81021 -0.3091 0.0022 1.0000 53.000 0.8330 0.81110 0.81084 -0.3099 0.0020 1.0000 53.500 0.8227 0.81080 0.81056 -0.3107 0.0018 1.0000 54.000 0.8122 0.80978 0.80957 -0.3114 0.0017 1.0000 54.500 0.8013 0.80798 0.80778 -0.3122 0.0016 1.0000 55.000 0.7898 0.80495 0.80478 -0.3129 0.0015 1.0000 56.500 0.7583 0.80328 0.80315 -0.3142 0.0015 1.0000 57.000 0.7473 0.80075 0.80065 -0.3146 0.0014 1.0000 57.500 0.7363 0.79806 0.79797 -0.3148 0.0014 1.0000 58.000 0.7251 0.79491 0.79484 -0.3151 0.0013 1.0000 58.500 0.7137 0.79069 0.79063 -0.3154 0.0012 1.0000 59.000 0.7021 0.78628 0.78624 -0.3156 0.0010 1.0000 59.500 0.6904 0.78095 0.78093 -0.3158 0.0010 1.0000 60.000 0.6786 0.77541 0.77541 -0.3160 0.0008 1.0000