XFOIL Version 6.96 Calculated polar for: GOE 460 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -1.1869 0.07772 0.07323 -0.0559 1.0000 0.0443 -19.500 -1.1887 0.07458 0.07001 -0.0567 1.0000 0.0448 -19.250 -1.1966 0.07074 0.06610 -0.0577 1.0000 0.0454 -19.000 -1.2069 0.06669 0.06198 -0.0586 1.0000 0.0461 -18.750 -1.2141 0.06310 0.05833 -0.0593 1.0000 0.0467 -18.500 -1.2189 0.05986 0.05503 -0.0598 1.0000 0.0475 -18.250 -1.2222 0.05683 0.05194 -0.0601 1.0000 0.0483 -18.000 -1.2221 0.05423 0.04928 -0.0603 1.0000 0.0491 -17.750 -1.2219 0.05171 0.04669 -0.0604 1.0000 0.0497 -17.500 -1.2198 0.04943 0.04433 -0.0604 1.0000 0.0502 -17.250 -1.2241 0.04657 0.04143 -0.0603 1.0000 0.0514 -17.000 -1.2264 0.04399 0.03880 -0.0600 1.0000 0.0525 -16.750 -1.2267 0.04169 0.03646 -0.0595 1.0000 0.0535 -16.500 -1.2252 0.03963 0.03434 -0.0589 1.0000 0.0546 -16.250 -1.2218 0.03779 0.03245 -0.0583 1.0000 0.0557 -16.000 -1.2206 0.03584 0.03046 -0.0574 1.0000 0.0572 -15.750 -1.2211 0.03387 0.02846 -0.0562 1.0000 0.0589 -15.500 -1.2196 0.03215 0.02670 -0.0549 1.0000 0.0607 -15.250 -1.2166 0.03063 0.02515 -0.0535 1.0000 0.0627 -15.000 -1.2166 0.02899 0.02351 -0.0517 1.0000 0.0660 -14.750 -1.2152 0.02756 0.02209 -0.0498 1.0000 0.0700 -14.500 -1.2147 0.02621 0.02077 -0.0475 1.0000 0.0757 -14.250 -1.2134 0.02501 0.01960 -0.0451 1.0000 0.0824 -14.000 -1.2103 0.02403 0.01863 -0.0426 1.0000 0.0875 -13.750 -1.2057 0.02323 0.01783 -0.0401 1.0000 0.0926 -13.500 -1.2022 0.02247 0.01705 -0.0373 1.0000 0.0956 -13.250 -1.2013 0.02167 0.01625 -0.0340 1.0000 0.0985 -13.000 -1.1988 0.02104 0.01560 -0.0308 1.0000 0.1012 -12.750 -1.1743 0.02045 0.01498 -0.0315 0.9991 0.1043 -12.500 -1.1498 0.01957 0.01411 -0.0326 0.9975 0.1082 -12.250 -1.1221 0.01887 0.01340 -0.0340 0.9955 0.1116 -12.000 -1.0915 0.01834 0.01284 -0.0357 0.9936 0.1143 -11.750 -1.0644 0.01759 0.01210 -0.0370 0.9916 0.1184 -11.500 -1.0418 0.01688 0.01139 -0.0373 0.9882 0.1219 -11.250 -1.0147 0.01631 0.01082 -0.0382 0.9854 0.1253 -11.000 -0.9877 0.01562 0.01016 -0.0393 0.9829 0.1315 -10.750 -0.9589 0.01500 0.00957 -0.0406 0.9809 0.1387 -10.500 -0.9317 0.01427 0.00894 -0.0417 0.9792 0.1531 -10.250 -0.9106 0.01368 0.00844 -0.0413 0.9746 0.1679 -10.000 -0.8825 0.01328 0.00807 -0.0420 0.9711 0.1784 -9.750 -0.8532 0.01283 0.00767 -0.0430 0.9682 0.1882 -9.500 -0.8184 0.01257 0.00739 -0.0449 0.9661 0.1931 -9.250 -0.7829 0.01214 0.00699 -0.0471 0.9641 0.1998 -9.000 -0.7568 0.01185 0.00671 -0.0472 0.9572 0.2044 -8.750 -0.7183 0.01164 0.00647 -0.0498 0.9537 0.2088 -8.500 -0.6792 0.01126 0.00611 -0.0527 0.9502 0.2147 -8.250 -0.6471 0.01097 0.00582 -0.0541 0.9431 0.2190 -8.000 -0.6119 0.01073 0.00556 -0.0560 0.9352 0.2227 -7.750 -0.5790 0.01055 0.00534 -0.0574 0.9262 0.2259 -7.500 -0.5510 0.01026 0.00504 -0.0578 0.9151 0.2311 -7.250 -0.5291 0.01003 0.00480 -0.0569 0.9021 0.2363 -7.000 -0.5047 0.00986 0.00459 -0.0565 0.8901 0.2406 -6.750 -0.4825 0.00970 0.00438 -0.0555 0.8777 0.2455 -6.500 -0.4649 0.00951 0.00418 -0.0536 0.8654 0.2510 -6.250 -0.4456 0.00936 0.00399 -0.0520 0.8544 0.2571 -6.000 -0.4277 0.00920 0.00382 -0.0502 0.8436 0.2642 -5.750 -0.4109 0.00901 0.00364 -0.0481 0.8338 0.2747 -5.500 -0.3953 0.00881 0.00347 -0.0457 0.8235 0.2869 -5.250 -0.3795 0.00862 0.00330 -0.0434 0.8141 0.3024 -5.000 -0.3646 0.00842 0.00315 -0.0408 0.8030 0.3205 -4.750 -0.3495 0.00824 0.00300 -0.0383 0.7923 0.3388 -4.500 -0.3336 0.00809 0.00288 -0.0358 0.7804 0.3557 -4.250 -0.3160 0.00796 0.00277 -0.0337 0.7700 0.3707 -4.000 -0.2993 0.00786 0.00267 -0.0314 0.7582 0.3843 -3.750 -0.2823 0.00774 0.00258 -0.0291 0.7460 0.3963 -3.500 -0.2642 0.00769 0.00250 -0.0271 0.7328 0.4074 -3.250 -0.2490 0.00763 0.00244 -0.0244 0.7163 0.4190 -2.750 -0.2178 0.00762 0.00235 -0.0191 0.6813 0.4379 -2.500 -0.2010 0.00762 0.00232 -0.0167 0.6647 0.4472 -2.250 -0.1830 0.00760 0.00228 -0.0146 0.6503 0.4580 -2.000 -0.1643 0.00760 0.00226 -0.0127 0.6373 0.4678 -1.750 -0.1447 0.00760 0.00224 -0.0109 0.6246 0.4781 -1.500 -0.1246 0.00758 0.00222 -0.0092 0.6133 0.4878 -1.250 -0.1045 0.00759 0.00221 -0.0076 0.6026 0.4989 -1.000 -0.0841 0.00755 0.00219 -0.0059 0.5921 0.5102 -0.500 -0.0428 0.00753 0.00218 -0.0028 0.5712 0.5324 -0.250 -0.0218 0.00756 0.00218 -0.0013 0.5611 0.5425 0.000 0.0000 0.00753 0.00218 0.0000 0.5525 0.5525 0.250 0.0217 0.00756 0.00218 0.0013 0.5425 0.5612 0.500 0.0429 0.00753 0.00218 0.0028 0.5332 0.5712 1.000 0.0843 0.00755 0.00219 0.0059 0.5106 0.5920 1.250 0.1045 0.00759 0.00221 0.0076 0.4988 0.6025 1.500 0.1246 0.00758 0.00222 0.0092 0.4880 0.6133 1.750 0.1449 0.00760 0.00224 0.0108 0.4782 0.6239 2.000 0.1642 0.00761 0.00226 0.0127 0.4674 0.6372 2.250 0.1829 0.00760 0.00228 0.0146 0.4577 0.6504 2.500 0.2010 0.00762 0.00232 0.0167 0.4471 0.6645 2.750 0.2181 0.00762 0.00235 0.0191 0.4380 0.6809 3.000 0.2330 0.00763 0.00239 0.0218 0.4282 0.6986 3.250 0.2490 0.00764 0.00244 0.0244 0.4190 0.7163 3.500 0.2644 0.00769 0.00250 0.0270 0.4075 0.7323 3.750 0.2824 0.00774 0.00258 0.0291 0.3964 0.7460 4.000 0.2994 0.00786 0.00267 0.0314 0.3843 0.7581 4.250 0.3161 0.00796 0.00277 0.0337 0.3705 0.7698 4.500 0.3334 0.00810 0.00288 0.0359 0.3551 0.7806 4.750 0.3495 0.00824 0.00300 0.0383 0.3389 0.7924 5.000 0.3644 0.00841 0.00315 0.0408 0.3207 0.8041 5.250 0.3794 0.00862 0.00330 0.0434 0.3022 0.8145 5.500 0.3953 0.00881 0.00347 0.0457 0.2870 0.8240 5.750 0.4109 0.00901 0.00364 0.0481 0.2743 0.8338 6.000 0.4276 0.00920 0.00382 0.0501 0.2639 0.8436 6.250 0.4457 0.00936 0.00399 0.0520 0.2569 0.8542 6.500 0.4650 0.00951 0.00418 0.0536 0.2510 0.8656 6.750 0.4825 0.00970 0.00438 0.0555 0.2451 0.8778 7.000 0.5049 0.00986 0.00459 0.0564 0.2410 0.8900 7.250 0.5295 0.01003 0.00480 0.0569 0.2369 0.9020 7.500 0.5515 0.01025 0.00503 0.0577 0.2318 0.9151 7.750 0.5791 0.01055 0.00534 0.0573 0.2259 0.9263 8.000 0.6119 0.01073 0.00556 0.0560 0.2231 0.9352 8.250 0.6474 0.01096 0.00582 0.0540 0.2190 0.9429 8.500 0.6798 0.01126 0.00610 0.0526 0.2147 0.9503 8.750 0.7187 0.01164 0.00647 0.0497 0.2089 0.9537 9.000 0.7572 0.01185 0.00671 0.0472 0.2049 0.9571 9.250 0.7835 0.01214 0.00699 0.0470 0.1997 0.9641 9.500 0.8190 0.01256 0.00738 0.0448 0.1930 0.9660 9.750 0.8538 0.01283 0.00767 0.0429 0.1878 0.9682 10.000 0.8831 0.01329 0.00807 0.0419 0.1781 0.9711 10.250 0.9111 0.01368 0.00843 0.0412 0.1675 0.9746 10.500 0.9323 0.01427 0.00894 0.0416 0.1524 0.9792 10.750 0.9596 0.01500 0.00956 0.0404 0.1382 0.9809 11.000 0.9884 0.01562 0.01015 0.0391 0.1312 0.9829 11.250 1.0156 0.01630 0.01081 0.0380 0.1254 0.9855 11.500 1.0427 0.01686 0.01138 0.0371 0.1219 0.9883 11.750 1.0650 0.01760 0.01210 0.0369 0.1180 0.9917 12.000 1.0930 0.01831 0.01281 0.0355 0.1140 0.9937 12.250 1.1234 0.01885 0.01338 0.0338 0.1114 0.9957 12.500 1.1511 0.01955 0.01408 0.0324 0.1082 0.9976 12.750 1.1755 0.02045 0.01497 0.0312 0.1040 0.9992 13.000 1.1990 0.02101 0.01556 0.0308 0.1014 1.0000 13.250 1.2020 0.02163 0.01620 0.0340 0.0988 1.0000 13.500 1.2023 0.02244 0.01702 0.0373 0.0956 1.0000 13.750 1.2062 0.02318 0.01778 0.0401 0.0924 1.0000 14.000 1.2113 0.02396 0.01857 0.0425 0.0881 1.0000 14.250 1.2143 0.02496 0.01955 0.0450 0.0830 1.0000 14.500 1.2154 0.02617 0.02072 0.0475 0.0754 1.0000 14.750 1.2161 0.02752 0.02204 0.0497 0.0697 1.0000 15.000 1.2178 0.02893 0.02345 0.0516 0.0658 1.0000 15.250 1.2179 0.03056 0.02508 0.0534 0.0626 1.0000 15.500 1.2207 0.03210 0.02665 0.0548 0.0604 1.0000 15.750 1.2224 0.03381 0.02839 0.0560 0.0587 1.0000 16.000 1.2221 0.03578 0.03039 0.0572 0.0571 1.0000 16.250 1.2239 0.03769 0.03234 0.0581 0.0557 1.0000 16.500 1.2275 0.03951 0.03422 0.0587 0.0546 1.0000 16.750 1.2292 0.04157 0.03633 0.0593 0.0534 1.0000 17.000 1.2293 0.04383 0.03864 0.0597 0.0524 1.0000 17.250 1.2267 0.04645 0.04129 0.0600 0.0513 1.0000 17.500 1.2225 0.04931 0.04421 0.0601 0.0503 1.0000 17.750 1.2247 0.05158 0.04655 0.0601 0.0497 1.0000 18.000 1.2252 0.05410 0.04914 0.0600 0.0489 1.0000 18.250 1.2254 0.05668 0.05179 0.0598 0.0482 1.0000 18.500 1.2230 0.05961 0.05477 0.0595 0.0475 1.0000 18.750 1.2178 0.06291 0.05813 0.0589 0.0466 1.0000 19.000 1.2101 0.06658 0.06186 0.0582 0.0460 1.0000 19.250 1.1995 0.07067 0.06602 0.0573 0.0452 1.0000