XFOIL Version 6.96 Calculated polar for: WORTMANN FX 75-193 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 ------ -------- --------- --------- -------- -------- -------- -13.750 -0.1346 0.09450 0.08825 -0.1472 0.8663 0.0230 -13.500 -0.1610 0.08396 0.07769 -0.1529 0.8655 0.0226 -13.250 -0.1902 0.07486 0.06849 -0.1586 0.8645 0.0221 -13.000 -0.2204 0.06758 0.06105 -0.1627 0.8633 0.0219 -12.750 -0.2455 0.06221 0.05549 -0.1650 0.8619 0.0217 -12.500 -0.2657 0.05804 0.05112 -0.1659 0.8602 0.0215 -12.250 -0.2815 0.05464 0.04749 -0.1659 0.8583 0.0214 -12.000 -0.2948 0.05159 0.04421 -0.1654 0.8566 0.0215 -11.500 -0.3121 0.04693 0.03913 -0.1625 0.8537 0.0216 -11.250 -0.3175 0.04503 0.03703 -0.1604 0.8520 0.0217 -11.000 -0.3191 0.04333 0.03513 -0.1583 0.8500 0.0219 -10.750 -0.3161 0.04182 0.03343 -0.1563 0.8477 0.0221 -10.500 -0.3094 0.04034 0.03173 -0.1545 0.8456 0.0225 -10.250 -0.2977 0.03901 0.03018 -0.1531 0.8440 0.0230 -10.000 -0.2860 0.03809 0.02918 -0.1517 0.8422 0.0233 -9.750 -0.2736 0.03725 0.02826 -0.1504 0.8403 0.0239 -9.500 -0.2589 0.03642 0.02732 -0.1493 0.8385 0.0248 -9.250 -0.2423 0.03563 0.02639 -0.1481 0.8368 0.0257 -9.000 -0.2366 0.03515 0.02585 -0.1453 0.8342 0.0268 -8.750 -0.2339 0.03482 0.02553 -0.1423 0.8310 0.0276 -8.500 -0.2284 0.03449 0.02515 -0.1396 0.8280 0.0295 -8.250 -0.2215 0.03410 0.02472 -0.1371 0.8252 0.0324 -8.000 -0.2121 0.03361 0.02417 -0.1349 0.8226 0.0351 -7.750 -0.2031 0.03308 0.02358 -0.1327 0.8204 0.0388 -7.500 -0.1950 0.03258 0.02306 -0.1304 0.8186 0.0434 -7.250 -0.2251 0.03324 0.02378 -0.1217 0.8123 0.0438 -7.000 -0.2364 0.03326 0.02381 -0.1161 0.8075 0.0464 -6.750 -0.2312 0.03290 0.02342 -0.1132 0.8045 0.0525 -6.500 -0.2191 0.03249 0.02300 -0.1114 0.8024 0.0629 -6.250 -0.2352 0.03282 0.02336 -0.1051 0.7972 0.0668 -6.000 -0.2525 0.03309 0.02363 -0.0984 0.7902 0.0708 -5.750 -0.2401 0.03270 0.02329 -0.0966 0.7873 0.0839 -5.500 -0.2220 0.03226 0.02290 -0.0956 0.7854 0.1018 -5.250 -0.2486 0.03273 0.02340 -0.0874 0.7775 0.1040 -5.000 -0.2457 0.03248 0.02326 -0.0841 0.7725 0.1215 -4.750 -0.2301 0.03177 0.02284 -0.0830 0.7699 0.1690 -4.250 -0.2335 0.03050 0.02255 -0.0765 0.7596 0.3423 -4.000 -0.2293 0.03102 0.02406 -0.0707 0.7555 0.4975 -3.750 -0.2077 0.03235 0.02550 -0.0673 0.7533 0.5623 -3.250 -0.1853 0.03381 0.02673 -0.0623 0.7435 0.6105 -3.000 -0.1628 0.03465 0.02742 -0.0611 0.7401 0.6353 -2.500 -0.1117 0.03655 0.02904 -0.0584 0.7364 0.6801 -2.250 -0.1219 0.03751 0.02998 -0.0530 0.7276 0.6915 -2.000 -0.1047 0.03815 0.03056 -0.0496 0.7247 0.7011 -1.500 -0.0766 0.03871 0.03092 -0.0459 0.7164 0.7153 -1.250 -0.0583 0.03880 0.03091 -0.0448 0.7124 0.7196 -1.000 -0.0295 0.03862 0.03059 -0.0458 0.7100 0.7243 -0.750 0.0021 0.03840 0.03021 -0.0472 0.7083 0.7288 -0.500 0.0028 0.03890 0.03069 -0.0436 0.7008 0.7320 -0.250 0.0244 0.03890 0.03061 -0.0431 0.6970 0.7351 0.000 0.0532 0.03874 0.03034 -0.0439 0.6947 0.7377 0.250 0.0852 0.03854 0.03003 -0.0453 0.6930 0.7404 0.750 0.1151 0.03913 0.03049 -0.0438 0.6814 0.7467 1.000 0.1419 0.03902 0.03032 -0.0439 0.6790 0.7486 1.250 0.1715 0.03888 0.03012 -0.0446 0.6773 0.7504 1.750 0.1988 0.03973 0.03090 -0.0425 0.6654 0.7549 2.000 0.2289 0.03962 0.03073 -0.0434 0.6630 0.7570 2.250 0.2612 0.03947 0.03053 -0.0447 0.6612 0.7594 2.750 0.2910 0.04043 0.03146 -0.0432 0.6489 0.7641 3.000 0.3193 0.04029 0.03131 -0.0435 0.6465 0.7657 3.250 0.3503 0.04006 0.03106 -0.0443 0.6447 0.7672 3.750 0.3777 0.04115 0.03218 -0.0421 0.6317 0.7715 4.000 0.4076 0.04105 0.03207 -0.0428 0.6295 0.7735 4.250 0.4399 0.04086 0.03188 -0.0439 0.6279 0.7752 4.750 0.4699 0.04221 0.03327 -0.0427 0.6141 0.7786 5.000 0.5019 0.04206 0.03313 -0.0438 0.6121 0.7804 5.250 0.5329 0.04172 0.03283 -0.0443 0.6105 0.7818 5.750 0.5588 0.04307 0.03427 -0.0421 0.5957 0.7847 6.000 0.5904 0.04274 0.03400 -0.0429 0.5938 0.7859 6.250 0.6235 0.04229 0.03360 -0.0437 0.5924 0.7871 6.750 0.6478 0.04400 0.03543 -0.0417 0.5768 0.7900 7.000 0.6799 0.04360 0.03511 -0.0424 0.5752 0.7917 7.500 0.7071 0.04530 0.03695 -0.0409 0.5596 0.7946 7.750 0.7407 0.04472 0.03645 -0.0417 0.5577 0.7956 8.000 0.7755 0.04407 0.03588 -0.0426 0.5561 0.7966 8.500 0.8022 0.04578 0.03777 -0.0411 0.5400 0.7990 8.750 0.8355 0.04512 0.03724 -0.0416 0.5384 0.8002 9.250 0.8635 0.04665 0.03898 -0.0400 0.5220 0.8024 9.500 0.9013 0.04554 0.03801 -0.0409 0.5201 0.8034 10.500 0.9639 0.04836 0.04132 -0.0385 0.4866 0.8081 11.000 1.0243 0.04647 0.03963 -0.0383 0.4654 0.8102 11.250 1.0393 0.04687 0.04009 -0.0374 0.4479 0.8110 11.500 1.0632 0.04643 0.03965 -0.0368 0.4272 0.8121 11.750 1.0674 0.04798 0.04124 -0.0355 0.4041 0.8132 12.000 1.0818 0.04849 0.04162 -0.0345 0.3724 0.8143 12.250 1.0880 0.04989 0.04287 -0.0332 0.3359 0.8152 12.500 1.0899 0.05176 0.04450 -0.0318 0.2928 0.8159 12.750 1.0866 0.05429 0.04675 -0.0305 0.2497 0.8164 13.000 1.0803 0.05731 0.04953 -0.0293 0.2076 0.8169 13.250 1.0705 0.06088 0.05281 -0.0283 0.1632 0.8173 13.500 1.0614 0.06459 0.05624 -0.0276 0.1241 0.8177 13.750 1.0558 0.06808 0.05954 -0.0272 0.0967 0.8182 14.000 1.0532 0.07136 0.06270 -0.0270 0.0764 0.8188 14.250 1.0533 0.07445 0.06576 -0.0270 0.0636 0.8193 14.500 1.0540 0.07755 0.06889 -0.0271 0.0536 0.8199 14.750 1.0549 0.08069 0.07206 -0.0274 0.0473 0.8205 15.000 1.0553 0.08396 0.07538 -0.0277 0.0427 0.8212 15.250 1.0556 0.08731 0.07879 -0.0281 0.0391 0.8218 15.500 1.0564 0.09063 0.08218 -0.0287 0.0364 0.8225 15.750 1.0587 0.09378 0.08546 -0.0292 0.0337 0.8234 16.000 1.0609 0.09694 0.08868 -0.0299 0.0321 0.8244 16.250 1.0655 0.09982 0.09169 -0.0305 0.0300 0.8255 16.500 1.0697 0.10274 0.09469 -0.0313 0.0287 0.8266 16.750 1.0754 0.10546 0.09751 -0.0320 0.0272 0.8277 17.000 1.0816 0.10810 0.10024 -0.0328 0.0261 0.8288 17.250 1.0870 0.11085 0.10305 -0.0338 0.0251 0.8297