XFOIL Version 6.96 Calculated polar for: WORTMANN FX 75-141 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -11.250 -0.3944 0.09460 0.08963 -0.0668 0.9763 0.0360 -11.000 -0.4032 0.08508 0.08010 -0.0739 0.9660 0.0359 -10.750 -0.4254 0.07195 0.06689 -0.0858 0.9566 0.0355 -10.500 -0.4524 0.06025 0.05491 -0.0995 0.9465 0.0351 -10.250 -0.4702 0.05245 0.04671 -0.1093 0.9367 0.0352 -10.000 -0.4809 0.04723 0.04104 -0.1144 0.9264 0.0354 -9.750 -0.4843 0.04294 0.03621 -0.1168 0.9186 0.0358 -9.500 -0.4776 0.03973 0.03257 -0.1178 0.9127 0.0363 -9.250 -0.4592 0.03764 0.03031 -0.1190 0.9092 0.0372 -9.000 -0.4423 0.03611 0.02861 -0.1193 0.9051 0.0384 -8.750 -0.4266 0.03463 0.02689 -0.1191 0.9003 0.0402 -8.500 -0.4078 0.03271 0.02456 -0.1194 0.8963 0.0422 -8.250 -0.3853 0.03075 0.02221 -0.1198 0.8933 0.0438 -8.000 -0.3615 0.02944 0.02084 -0.1203 0.8907 0.0454 -7.750 -0.3433 0.02861 0.01992 -0.1194 0.8865 0.0476 -7.500 -0.3215 0.02761 0.01870 -0.1191 0.8828 0.0507 -7.250 -0.2974 0.02649 0.01742 -0.1190 0.8799 0.0534 -7.000 -0.2717 0.02560 0.01652 -0.1194 0.8773 0.0563 -6.750 -0.2462 0.02487 0.01564 -0.1195 0.8746 0.0608 -6.500 -0.2289 0.02422 0.01495 -0.1180 0.8702 0.0643 -6.250 -0.2075 0.02362 0.01436 -0.1174 0.8665 0.0685 -6.000 -0.1824 0.02305 0.01368 -0.1173 0.8633 0.0748 -5.750 -0.1568 0.02239 0.01306 -0.1175 0.8607 0.0816 -5.500 -0.1349 0.02193 0.01256 -0.1169 0.8572 0.0900 -5.250 -0.1164 0.02159 0.01221 -0.1156 0.8527 0.0994 -5.000 -0.0934 0.02112 0.01178 -0.1153 0.8490 0.1131 -4.750 -0.0671 0.02061 0.01131 -0.1155 0.8459 0.1328 -4.500 -0.0392 0.02004 0.01087 -0.1161 0.8434 0.1650 -4.250 -0.0226 0.01970 0.01073 -0.1147 0.8383 0.2068 -4.000 -0.0011 0.01918 0.01050 -0.1143 0.8341 0.2748 -3.750 0.0233 0.01857 0.01038 -0.1143 0.8307 0.3813 -3.500 0.0505 0.01835 0.01046 -0.1141 0.8280 0.4775 -3.250 0.0694 0.01852 0.01075 -0.1123 0.8232 0.5284 -3.000 0.0904 0.01876 0.01105 -0.1107 0.8184 0.5670 -2.750 0.1162 0.01900 0.01129 -0.1098 0.8149 0.5982 -2.500 0.1449 0.01922 0.01145 -0.1094 0.8122 0.6231 -2.250 0.1641 0.01961 0.01179 -0.1076 0.8070 0.6424 -2.000 0.1858 0.01993 0.01206 -0.1062 0.8019 0.6606 -1.750 0.2127 0.02015 0.01220 -0.1056 0.7984 0.6767 -1.500 0.2421 0.02028 0.01225 -0.1055 0.7958 0.6904 -1.250 0.2570 0.02065 0.01261 -0.1031 0.7889 0.7031 -1.000 0.2814 0.02082 0.01272 -0.1023 0.7844 0.7165 -0.750 0.3093 0.02086 0.01272 -0.1019 0.7812 0.7261 -0.500 0.3310 0.02102 0.01283 -0.1009 0.7759 0.7345 -0.250 0.3511 0.02117 0.01297 -0.0995 0.7698 0.7420 0.000 0.3805 0.02114 0.01287 -0.0998 0.7662 0.7496 0.250 0.4114 0.02105 0.01274 -0.1001 0.7636 0.7560 0.500 0.4239 0.02141 0.01312 -0.0978 0.7548 0.7639 0.750 0.4507 0.02137 0.01307 -0.0974 0.7507 0.7698 1.000 0.4834 0.02126 0.01291 -0.0982 0.7480 0.7769 1.250 0.4937 0.02161 0.01332 -0.0954 0.7389 0.7830 1.500 0.5216 0.02156 0.01326 -0.0953 0.7347 0.7896 1.750 0.5541 0.02140 0.01309 -0.0960 0.7319 0.7958 2.000 0.5634 0.02179 0.01355 -0.0930 0.7221 0.8022 2.250 0.5938 0.02169 0.01345 -0.0934 0.7183 0.8089 2.750 0.6344 0.02193 0.01377 -0.0909 0.7050 0.8212 3.000 0.6665 0.02172 0.01360 -0.0915 0.7017 0.8271 3.250 0.6783 0.02209 0.01404 -0.0890 0.6923 0.8337 3.500 0.7084 0.02194 0.01393 -0.0893 0.6879 0.8402 3.750 0.7269 0.02208 0.01414 -0.0877 0.6806 0.8464 4.000 0.7512 0.02205 0.01418 -0.0871 0.6742 0.8532 4.250 0.7856 0.02166 0.01385 -0.0878 0.6707 0.8593 4.500 0.7972 0.02198 0.01426 -0.0852 0.6601 0.8673 4.750 0.8333 0.02144 0.01379 -0.0861 0.6557 0.8739 5.000 0.8485 0.02149 0.01393 -0.0839 0.6440 0.8829 5.250 0.8719 0.02119 0.01371 -0.0827 0.6329 0.8918 5.500 0.9050 0.02060 0.01319 -0.0829 0.6232 0.9013 5.750 0.9293 0.02044 0.01313 -0.0821 0.6120 0.9135 6.000 0.9555 0.02038 0.01319 -0.0818 0.6005 0.9303 6.250 0.9877 0.02013 0.01304 -0.0824 0.5890 1.0000 6.500 1.0204 0.02002 0.01297 -0.0832 0.5767 1.0000 6.750 1.0488 0.02004 0.01303 -0.0832 0.5622 1.0000 7.000 1.0720 0.02023 0.01324 -0.0826 0.5455 1.0000 7.250 1.0907 0.02052 0.01356 -0.0812 0.5255 1.0000 7.500 1.1102 0.02077 0.01376 -0.0798 0.5006 1.0000 7.750 1.1232 0.02126 0.01418 -0.0775 0.4714 1.0000 8.000 1.1350 0.02185 0.01466 -0.0752 0.4385 1.0000 8.250 1.1440 0.02264 0.01531 -0.0727 0.4018 1.0000 8.500 1.1502 0.02364 0.01611 -0.0701 0.3617 1.0000 8.750 1.1539 0.02489 0.01712 -0.0674 0.3224 1.0000 9.000 1.1565 0.02633 0.01833 -0.0648 0.2866 1.0000 9.250 1.1594 0.02787 0.01968 -0.0625 0.2550 1.0000 9.500 1.1631 0.02944 0.02111 -0.0604 0.2277 1.0000 9.750 1.1668 0.03109 0.02264 -0.0585 0.2035 1.0000 10.000 1.1721 0.03269 0.02415 -0.0568 0.1813 1.0000 10.250 1.1771 0.03436 0.02575 -0.0551 0.1614 1.0000 10.500 1.1815 0.03613 0.02744 -0.0536 0.1429 1.0000 10.750 1.1873 0.03785 0.02912 -0.0522 0.1258 1.0000 11.000 1.1923 0.03967 0.03090 -0.0508 0.1115 1.0000 11.250 1.1966 0.04160 0.03280 -0.0495 0.0996 1.0000 11.500 1.2010 0.04358 0.03476 -0.0483 0.0900 1.0000 11.750 1.2065 0.04551 0.03673 -0.0472 0.0823 1.0000 12.000 1.2091 0.04772 0.03891 -0.0461 0.0768 1.0000 12.250 1.2156 0.04966 0.04095 -0.0452 0.0714 1.0000 12.500 1.2193 0.05189 0.04321 -0.0443 0.0669 1.0000 12.750 1.2235 0.05415 0.04553 -0.0435 0.0633 1.0000 13.000 1.2299 0.05625 0.04775 -0.0428 0.0598 1.0000 13.250 1.2343 0.05858 0.05014 -0.0422 0.0568 1.0000 13.500 1.2377 0.06107 0.05262 -0.0417 0.0543 1.0000 13.750 1.2452 0.06323 0.05496 -0.0412 0.0518 1.0000 14.000 1.2508 0.06562 0.05746 -0.0408 0.0492 1.0000 14.250 1.2554 0.06813 0.06004 -0.0406 0.0473 1.0000 14.500 1.2600 0.07067 0.06257 -0.0403 0.0455 1.0000 14.750 1.2665 0.07316 0.06529 -0.0400 0.0438 1.0000 15.000 1.2718 0.07582 0.06813 -0.0399 0.0421 1.0000 15.250 1.2758 0.07863 0.07108 -0.0400 0.0406 1.0000 15.500 1.2787 0.08158 0.07410 -0.0402 0.0392 1.0000 15.750 1.2825 0.08439 0.07693 -0.0405 0.0379 1.0000 16.000 1.2839 0.08774 0.08047 -0.0409 0.0368 1.0000 16.250 1.2827 0.09157 0.08457 -0.0415 0.0358 1.0000 16.500 1.2803 0.09560 0.08885 -0.0425 0.0349 1.0000 16.750 1.2763 0.09992 0.09338 -0.0437 0.0340 1.0000 17.000 1.2715 0.10438 0.09803 -0.0453 0.0332 1.0000 17.250 1.2668 0.10885 0.10265 -0.0470 0.0325 1.0000 17.500 1.2628 0.11326 0.10718 -0.0489 0.0318 1.0000 17.750 1.2609 0.11731 0.11130 -0.0506 0.0311 1.0000 18.000 1.2538 0.12249 0.11661 -0.0531 0.0306 1.0000 18.250 1.2365 0.12991 0.12431 -0.0573 0.0304 1.0000 18.500 1.2171 0.13813 0.13281 -0.0623 0.0302 1.0000 18.750 1.1944 0.14757 0.14250 -0.0684 0.0301 1.0000 19.000 1.1663 0.15903 0.15420 -0.0762 0.0302 1.0000 19.250 1.1265 0.17497 0.17033 -0.0871 0.0305 1.0000