XFOIL Version 6.96 Calculated polar for: RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -12.750 -0.3404 0.13005 0.12642 -0.0474 1.0000 0.0521 -12.500 -0.3586 0.12468 0.12113 -0.0535 1.0000 0.0541 -12.250 -0.3725 0.11931 0.11583 -0.0582 1.0000 0.0544 -12.000 -0.3537 0.11633 0.11285 -0.0542 1.0000 0.0557 -11.750 -0.2261 0.10786 0.10482 -0.0591 0.9820 0.0617 -11.500 -0.2487 0.10080 0.09779 -0.0670 0.9697 0.0648 -11.250 -0.2688 0.09249 0.08950 -0.0755 0.9589 0.0652 -11.000 -0.2225 0.08901 0.08594 -0.0748 0.9415 0.0672 -10.750 -0.1985 0.08452 0.08137 -0.0791 0.9258 0.0692 -10.500 -0.1872 0.07883 0.07561 -0.0843 0.9103 0.0718 -10.250 -0.4261 0.07906 0.07567 -0.0870 0.9519 0.0652 -10.000 -0.3515 0.07687 0.07376 -0.0820 0.9494 0.0679 -9.750 -0.3313 0.07062 0.06739 -0.0914 0.9310 0.0699 -9.500 -0.3311 0.06263 0.05913 -0.1031 0.9043 0.0728 -9.250 -0.3542 0.05800 0.05410 -0.1062 0.8715 0.0754 -8.500 -0.4354 0.03988 0.03404 -0.0926 0.8240 0.0462 -8.250 -0.4288 0.03426 0.02775 -0.0894 0.8156 0.0363 -8.000 -0.4170 0.03150 0.02468 -0.0874 0.8063 0.0353 -7.750 -0.4014 0.02911 0.02190 -0.0857 0.7989 0.0344 -7.500 -0.3830 0.02704 0.01946 -0.0843 0.7909 0.0341 -7.250 -0.3608 0.02549 0.01760 -0.0834 0.7849 0.0345 -7.000 -0.3384 0.02429 0.01619 -0.0825 0.7777 0.0354 -6.750 -0.3140 0.02327 0.01491 -0.0819 0.7721 0.0366 -6.500 -0.2876 0.02219 0.01365 -0.0815 0.7672 0.0370 -6.250 -0.2609 0.02087 0.01228 -0.0814 0.7617 0.0378 -6.000 -0.2366 0.01980 0.01122 -0.0810 0.7570 0.0392 -5.750 -0.2136 0.01911 0.01049 -0.0803 0.7531 0.0413 -5.500 -0.1932 0.01851 0.00987 -0.0791 0.7483 0.0437 -5.250 -0.1747 0.01783 0.00918 -0.0776 0.7436 0.0473 -5.000 -0.1537 0.01738 0.00868 -0.0765 0.7397 0.0543 -4.750 -0.1378 0.01650 0.00792 -0.0746 0.7363 0.0781 -4.500 -0.1268 0.01547 0.00744 -0.0721 0.7323 0.1642 -4.250 -0.1131 0.01471 0.00714 -0.0702 0.7285 0.2616 -4.000 -0.1039 0.01374 0.00686 -0.0675 0.7252 0.4107 -3.750 -0.0952 0.01297 0.00710 -0.0635 0.7225 0.6192 -3.500 -0.0726 0.01365 0.00797 -0.0611 0.7200 0.7282 -3.250 -0.0508 0.01433 0.00864 -0.0589 0.7167 0.7623 -3.000 -0.0264 0.01492 0.00918 -0.0573 0.7133 0.7814 -2.750 -0.0009 0.01543 0.00960 -0.0559 0.7103 0.7961 -2.500 0.0248 0.01589 0.00996 -0.0547 0.7078 0.8096 -2.250 0.0499 0.01627 0.01022 -0.0535 0.7057 0.8226 -2.000 0.0814 0.01681 0.01068 -0.0531 0.7036 0.8308 -1.750 0.1048 0.01715 0.01101 -0.0518 0.7009 0.8416 -1.500 0.1273 0.01751 0.01133 -0.0503 0.6982 0.8542 -1.250 0.1716 0.01809 0.01185 -0.0521 0.6957 0.8630 -1.000 0.2037 0.01832 0.01200 -0.0525 0.6932 0.8728 -0.750 0.2445 0.01852 0.01211 -0.0548 0.6912 0.8789 -0.500 0.2667 0.01858 0.01210 -0.0539 0.6894 0.8869 -0.250 0.3082 0.01872 0.01217 -0.0567 0.6876 0.8900 0.000 0.3332 0.01884 0.01232 -0.0565 0.6849 0.8957 0.250 0.3478 0.01889 0.01238 -0.0544 0.6819 0.9024 0.500 0.3873 0.01898 0.01243 -0.0571 0.6796 0.9050 0.750 0.4201 0.01905 0.01247 -0.0585 0.6774 0.9086 1.000 0.4215 0.01907 0.01248 -0.0537 0.6751 0.9163 1.250 0.4637 0.01909 0.01245 -0.0569 0.6732 0.9178 1.500 0.4998 0.01922 0.01257 -0.0591 0.6712 0.9200 1.750 0.5217 0.01945 0.01287 -0.0587 0.6678 0.9238 2.000 0.5155 0.01962 0.01310 -0.0526 0.6646 0.9311 2.250 0.5531 0.01969 0.01317 -0.0550 0.6620 0.9326 2.500 0.5886 0.01972 0.01319 -0.0570 0.6596 0.9343 2.750 0.6224 0.01975 0.01320 -0.0586 0.6575 0.9364 3.000 0.6467 0.01994 0.01342 -0.0584 0.6549 0.9394 3.250 0.6378 0.02032 0.01392 -0.0521 0.6503 0.9459 3.500 0.6695 0.02045 0.01409 -0.0535 0.6469 0.9475 3.750 0.7047 0.02044 0.01409 -0.0554 0.6441 0.9491 4.000 0.7396 0.02038 0.01403 -0.0570 0.6416 0.9508 4.250 0.7592 0.02065 0.01436 -0.0561 0.6378 0.9537 4.500 0.7590 0.02100 0.01482 -0.0515 0.6324 0.9595 4.750 0.7955 0.02090 0.01473 -0.0534 0.6288 0.9607 5.000 0.8336 0.02066 0.01450 -0.0555 0.6258 0.9617 5.250 0.8576 0.02089 0.01482 -0.0555 0.6206 0.9641 5.500 0.8836 0.02091 0.01491 -0.0556 0.6148 0.9669 5.750 0.9195 0.02050 0.01452 -0.0570 0.6108 0.9688 6.000 0.9398 0.02042 0.01449 -0.0558 0.6055 0.9722 6.250 0.9708 0.02023 0.01438 -0.0568 0.5982 0.9740 6.500 1.0143 0.01956 0.01368 -0.0594 0.5933 0.9747 6.750 1.0363 0.01958 0.01384 -0.0589 0.5846 0.9781 7.000 1.0752 0.01897 0.01323 -0.0607 0.5784 0.9798 7.250 1.0958 0.01889 0.01329 -0.0598 0.5700 0.9841 7.500 1.1353 0.01825 0.01264 -0.0618 0.5622 0.9854 7.750 1.1607 0.01809 0.01265 -0.0618 0.5517 0.9888 8.000 1.1902 0.01769 0.01231 -0.0623 0.5415 0.9921 8.250 1.2200 0.01725 0.01192 -0.0628 0.5296 0.9954 8.500 1.2459 0.01703 0.01184 -0.0629 0.5147 1.0000 8.750 1.2357 0.01705 0.01198 -0.0561 0.5028 1.0000 9.000 1.2194 0.01700 0.01200 -0.0483 0.4917 1.0000 9.250 1.2055 0.01690 0.01193 -0.0410 0.4786 1.0000 9.500 1.2066 0.01692 0.01192 -0.0365 0.4569 1.0000 9.750 1.2090 0.01721 0.01209 -0.0325 0.4259 1.0000 10.000 1.2063 0.01797 0.01263 -0.0282 0.3896 1.0000 10.250 1.1982 0.01924 0.01367 -0.0238 0.3546 1.0000 10.500 1.1882 0.02088 0.01512 -0.0197 0.3223 1.0000 10.750 1.1779 0.02281 0.01688 -0.0161 0.2922 1.0000 11.000 1.1675 0.02499 0.01891 -0.0131 0.2632 1.0000 11.250 1.1581 0.02733 0.02111 -0.0105 0.2360 1.0000 11.500 1.1497 0.02976 0.02340 -0.0083 0.2119 1.0000 11.750 1.1422 0.03225 0.02576 -0.0064 0.1891 1.0000 12.000 1.1365 0.03470 0.02810 -0.0048 0.1690 1.0000 12.250 1.1331 0.03707 0.03038 -0.0034 0.1508 1.0000 12.500 1.1306 0.03944 0.03266 -0.0022 0.1350 1.0000 12.750 1.1296 0.04177 0.03492 -0.0012 0.1211 1.0000 13.000 1.1303 0.04403 0.03715 -0.0004 0.1093 1.0000 13.250 1.1312 0.04632 0.03940 0.0003 0.0995 1.0000 13.500 1.1316 0.04872 0.04173 0.0009 0.0908 1.0000 13.750 1.1368 0.05076 0.04383 0.0014 0.0826 1.0000 14.000 1.1385 0.05314 0.04619 0.0018 0.0760 1.0000 14.250 1.1424 0.05540 0.04848 0.0021 0.0696 1.0000 14.500 1.1450 0.05779 0.05090 0.0025 0.0637 1.0000 14.750 1.1473 0.06031 0.05344 0.0026 0.0582 1.0000 15.000 1.1499 0.06282 0.05600 0.0028 0.0530 1.0000 15.250 1.1507 0.06560 0.05878 0.0028 0.0483 1.0000 15.500 1.1534 0.06818 0.06144 0.0030 0.0440 1.0000 15.750 1.1550 0.07098 0.06425 0.0028 0.0405 1.0000 16.000 1.1580 0.07358 0.06689 0.0029 0.0374 1.0000 16.250 1.1621 0.07616 0.06956 0.0028 0.0349 1.0000 16.500 1.1656 0.07878 0.07217 0.0025 0.0330 1.0000 16.750 1.1727 0.08089 0.07433 0.0028 0.0312 1.0000 17.000 1.1774 0.08353 0.07714 0.0026 0.0298 1.0000 17.250 1.1827 0.08608 0.07979 0.0024 0.0286 1.0000 17.500 1.1891 0.08847 0.08224 0.0021 0.0277 1.0000 17.750 1.1990 0.09029 0.08404 0.0022 0.0266 1.0000 18.000 1.2045 0.09296 0.08685 0.0022 0.0259 1.0000 18.250 1.2030 0.09666 0.09077 0.0012 0.0255 1.0000 18.500 1.1995 0.10074 0.09506 0.0000 0.0250 1.0000 18.750 1.1948 0.10502 0.09955 -0.0015 0.0244 1.0000 19.000 1.1898 0.10945 0.10417 -0.0032 0.0239 1.0000 19.250 1.1840 0.11403 0.10893 -0.0051 0.0236 1.0000