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 = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -11.750 -0.4293 0.08608 0.08257 -0.0634 1.0000 0.0163 -11.500 -0.4810 0.06696 0.06333 -0.0766 0.9923 0.0158 -11.250 -0.5049 0.05636 0.05238 -0.0880 0.9406 0.0155 -11.000 -0.5168 0.04799 0.04346 -0.0971 0.9061 0.0154 -10.750 -0.5206 0.04269 0.03761 -0.1009 0.8714 0.0154 -10.500 -0.5266 0.03926 0.03371 -0.1003 0.8441 0.0154 -10.250 -0.5309 0.03678 0.03084 -0.0979 0.8225 0.0154 -10.000 -0.5338 0.03473 0.02842 -0.0947 0.8054 0.0155 -9.750 -0.5313 0.03282 0.02614 -0.0920 0.7914 0.0156 -9.500 -0.5242 0.03098 0.02394 -0.0896 0.7796 0.0158 -9.000 -0.4985 0.02787 0.02018 -0.0861 0.7594 0.0162 -8.750 -0.4816 0.02655 0.01856 -0.0848 0.7513 0.0165 -8.500 -0.4627 0.02539 0.01717 -0.0837 0.7434 0.0166 -8.000 -0.4234 0.02340 0.01495 -0.0819 0.7299 0.0177 -7.750 -0.4030 0.02268 0.01413 -0.0810 0.7237 0.0183 -7.500 -0.3821 0.02196 0.01328 -0.0802 0.7183 0.0191 -7.250 -0.3610 0.02118 0.01239 -0.0793 0.7126 0.0197 -7.000 -0.3403 0.02045 0.01153 -0.0783 0.7074 0.0201 -6.750 -0.3199 0.01980 0.01076 -0.0772 0.7028 0.0207 -6.500 -0.3010 0.01910 0.01004 -0.0760 0.6976 0.0213 -6.250 -0.2811 0.01855 0.00942 -0.0749 0.6931 0.0220 -6.000 -0.2605 0.01807 0.00885 -0.0738 0.6893 0.0231 -5.750 -0.2394 0.01762 0.00832 -0.0728 0.6856 0.0244 -5.500 -0.2182 0.01717 0.00782 -0.0719 0.6816 0.0263 -5.250 -0.1963 0.01679 0.00739 -0.0710 0.6780 0.0295 -5.000 -0.1747 0.01637 0.00695 -0.0701 0.6748 0.0345 -4.500 -0.1324 0.01547 0.00617 -0.0682 0.6688 0.0712 -4.250 -0.1111 0.01507 0.00589 -0.0673 0.6654 0.1047 -4.000 -0.0905 0.01463 0.00563 -0.0664 0.6621 0.1492 -3.750 -0.0725 0.01399 0.00536 -0.0651 0.6593 0.2296 -3.500 -0.0585 0.01315 0.00505 -0.0632 0.6569 0.3581 -3.250 -0.0467 0.01225 0.00487 -0.0606 0.6545 0.5163 -3.000 -0.0286 0.01203 0.00526 -0.0581 0.6518 0.6470 -2.750 -0.0037 0.01225 0.00554 -0.0571 0.6492 0.7034 -2.500 0.0218 0.01242 0.00563 -0.0564 0.6468 0.7308 -2.250 0.0477 0.01259 0.00571 -0.0558 0.6446 0.7489 -2.000 0.0739 0.01275 0.00578 -0.0553 0.6425 0.7629 -1.750 0.1002 0.01293 0.00585 -0.0549 0.6405 0.7758 -1.500 0.1250 0.01313 0.00600 -0.0541 0.6381 0.7895 -1.250 0.1501 0.01343 0.00630 -0.0529 0.6356 0.8015 -1.000 0.1752 0.01365 0.00650 -0.0520 0.6334 0.8114 -0.750 0.2007 0.01377 0.00657 -0.0515 0.6313 0.8193 -0.500 0.2270 0.01384 0.00658 -0.0513 0.6294 0.8242 -0.250 0.2540 0.01392 0.00661 -0.0511 0.6276 0.8279 0.000 0.2809 0.01398 0.00661 -0.0510 0.6259 0.8320 0.250 0.3081 0.01401 0.00655 -0.0511 0.6242 0.8364 0.500 0.3337 0.01406 0.00660 -0.0509 0.6219 0.8395 0.750 0.3596 0.01412 0.00667 -0.0506 0.6197 0.8421 1.000 0.3859 0.01419 0.00674 -0.0505 0.6177 0.8449 1.250 0.4123 0.01424 0.00678 -0.0505 0.6157 0.8479 1.500 0.4390 0.01428 0.00680 -0.0505 0.6136 0.8511 1.750 0.4663 0.01432 0.00680 -0.0508 0.6117 0.8540 2.000 0.4937 0.01439 0.00686 -0.0509 0.6100 0.8558 2.250 0.5216 0.01447 0.00691 -0.0511 0.6084 0.8577 2.500 0.5465 0.01456 0.00706 -0.0508 0.6060 0.8599 2.750 0.5716 0.01465 0.00720 -0.0505 0.6034 0.8624 3.000 0.5974 0.01473 0.00732 -0.0505 0.6008 0.8650 3.250 0.6241 0.01480 0.00741 -0.0506 0.5984 0.8672 3.500 0.6517 0.01487 0.00748 -0.0509 0.5960 0.8696 3.750 0.6793 0.01493 0.00754 -0.0510 0.5938 0.8714 4.000 0.7054 0.01502 0.00769 -0.0509 0.5912 0.8734 4.250 0.7284 0.01513 0.00790 -0.0503 0.5876 0.8756 4.500 0.7533 0.01522 0.00805 -0.0500 0.5841 0.8779 4.750 0.7799 0.01526 0.00812 -0.0500 0.5807 0.8801 5.000 0.8084 0.01529 0.00816 -0.0504 0.5777 0.8826 5.250 0.8316 0.01538 0.00835 -0.0498 0.5734 0.8855 5.500 0.8541 0.01544 0.00851 -0.0490 0.5684 0.8879 5.750 0.8802 0.01541 0.00853 -0.0488 0.5638 0.8901 6.000 0.9047 0.01543 0.00860 -0.0483 0.5588 0.8927 6.250 0.9257 0.01546 0.00875 -0.0473 0.5520 0.8958 6.500 0.9524 0.01538 0.00868 -0.0472 0.5461 0.8987 6.750 0.9705 0.01544 0.00890 -0.0456 0.5380 0.9023 7.000 0.9939 0.01535 0.00885 -0.0448 0.5307 0.9056 7.250 1.0111 0.01543 0.00908 -0.0431 0.5211 0.9100 7.500 1.0315 0.01543 0.00917 -0.0419 0.5115 0.9144 7.750 1.0501 0.01543 0.00924 -0.0403 0.5001 0.9187 8.000 1.0653 0.01550 0.00941 -0.0382 0.4858 0.9243 8.250 1.0793 0.01560 0.00959 -0.0358 0.4673 0.9312 8.500 1.0896 0.01570 0.00968 -0.0328 0.4421 0.9400 8.750 1.0980 0.01607 0.00993 -0.0298 0.4082 0.9531 9.000 1.1068 0.01691 0.01057 -0.0277 0.3688 0.9740 9.250 1.1074 0.01799 0.01148 -0.0247 0.3355 1.0000 9.500 1.1041 0.01928 0.01263 -0.0213 0.3066 1.0000 9.750 1.1016 0.02073 0.01397 -0.0184 0.2801 1.0000 10.000 1.0993 0.02234 0.01547 -0.0158 0.2564 1.0000 10.250 1.0958 0.02417 0.01719 -0.0134 0.2321 1.0000 10.500 1.0947 0.02598 0.01892 -0.0115 0.2109 1.0000 10.750 1.0940 0.02787 0.02073 -0.0098 0.1907 1.0000 11.000 1.0943 0.02977 0.02256 -0.0083 0.1734 1.0000 11.250 1.0952 0.03168 0.02442 -0.0069 0.1569 1.0000 11.500 1.0977 0.03353 0.02623 -0.0058 0.1430 1.0000 11.750 1.1003 0.03540 0.02807 -0.0047 0.1295 1.0000 12.000 1.1034 0.03728 0.02992 -0.0037 0.1170 1.0000 12.250 1.1076 0.03912 0.03175 -0.0029 0.1057 1.0000 12.500 1.1116 0.04103 0.03365 -0.0021 0.0952 1.0000 12.750 1.1153 0.04301 0.03560 -0.0014 0.0850 1.0000 13.000 1.1192 0.04502 0.03760 -0.0008 0.0764 1.0000 13.250 1.1240 0.04702 0.03959 -0.0003 0.0686 1.0000 13.500 1.1298 0.04894 0.04154 0.0001 0.0620 1.0000 13.750 1.1334 0.05113 0.04372 0.0004 0.0563 1.0000 14.000 1.1404 0.05303 0.04569 0.0007 0.0515 1.0000 14.250 1.1442 0.05531 0.04798 0.0009 0.0474 1.0000 14.500 1.1505 0.05735 0.05010 0.0010 0.0432 1.0000 14.750 1.1538 0.05976 0.05255 0.0011 0.0395 1.0000 15.000 1.1589 0.06202 0.05490 0.0011 0.0364 1.0000 15.250 1.1621 0.06455 0.05748 0.0010 0.0333 1.0000 15.500 1.1650 0.06716 0.06016 0.0009 0.0309 1.0000 15.750 1.1680 0.06980 0.06289 0.0007 0.0282 1.0000 16.000 1.1682 0.07285 0.06598 0.0003 0.0263 1.0000 16.250 1.1706 0.07570 0.06894 -0.0001 0.0244 1.0000 16.500 1.1718 0.07875 0.07207 -0.0007 0.0227 1.0000 16.750 1.1701 0.08224 0.07564 -0.0014 0.0214 1.0000 17.000 1.1707 0.08548 0.07900 -0.0021 0.0200 1.0000 17.250 1.1701 0.08898 0.08260 -0.0030 0.0189 1.0000 17.500 1.1690 0.09259 0.08632 -0.0041 0.0183 1.0000 17.750 1.1655 0.09665 0.09046 -0.0054 0.0175 1.0000 18.000 1.1621 0.10074 0.09465 -0.0067 0.0170 1.0000