XFOIL Version 6.94 Calculated polar for: FX 83-W-160 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.4572 0.01329 0.00746 -0.1270 0.7929 0.6059 0.500 0.5152 0.01331 0.00752 -0.1271 0.7861 0.6216 1.000 0.5866 0.01317 0.00726 -0.1302 0.7802 0.6287 1.500 0.6223 0.01330 0.00753 -0.1259 0.7702 0.6436 2.000 0.6754 0.01318 0.00744 -0.1250 0.7603 0.6535 2.500 0.7535 0.01284 0.00699 -0.1291 0.7498 0.6618 3.000 0.7829 0.01264 0.00693 -0.1234 0.7356 0.6719 3.500 0.8522 0.01226 0.00649 -0.1254 0.7206 0.6857 4.000 0.8806 0.01223 0.00657 -0.1196 0.7058 0.6944 4.500 0.9392 0.01201 0.00642 -0.1197 0.6901 0.7056 5.000 0.9633 0.01201 0.00654 -0.1128 0.6717 0.7158 5.500 1.0018 0.01200 0.00656 -0.1090 0.6505 0.7270 6.000 1.0347 0.01211 0.00673 -0.1039 0.6206 0.7448 6.500 1.0694 0.01238 0.00710 -0.0998 0.5872 0.7646 7.000 1.0760 0.01351 0.00781 -0.0906 0.4839 0.7926 7.500 1.0763 0.01582 0.00961 -0.0826 0.3687 0.8529 8.000 1.1008 0.01815 0.01162 -0.0799 0.2867 1.0000 8.500 1.1179 0.02039 0.01352 -0.0754 0.2302 1.0000 9.000 1.1284 0.02317 0.01583 -0.0705 0.1701 1.0000 9.500 1.1583 0.02491 0.01743 -0.0681 0.1521 1.0000 10.000 1.1865 0.02684 0.01956 -0.0653 0.1447 1.0000 10.500 1.2123 0.02895 0.02163 -0.0626 0.1238 1.0000 11.000 1.2394 0.03100 0.02358 -0.0603 0.1076 1.0000 11.500 1.2661 0.03313 0.02583 -0.0582 0.0995 1.0000 12.000 1.2871 0.03584 0.02874 -0.0553 0.0986 1.0000 12.500 1.3037 0.03900 0.03189 -0.0526 0.0809 1.0000 13.000 1.3349 0.04100 0.03372 -0.0518 0.0668 1.0000 13.500 1.3538 0.04402 0.03668 -0.0500 0.0515 1.0000 14.000 1.3619 0.04810 0.04118 -0.0469 0.0580 1.0000 14.500 1.3774 0.05175 0.04477 -0.0453 0.0494 1.0000 15.000 1.3765 0.05699 0.05031 -0.0423 0.0497 1.0000 15.500 1.4049 0.05983 0.05301 -0.0431 0.0391 1.0000 16.000 1.4201 0.06385 0.05724 -0.0424 0.0345 1.0000 16.500 1.4049 0.07094 0.06469 -0.0401 0.0398 1.0000 17.000 1.4142 0.07582 0.06973 -0.0402 0.0372 1.0000 17.500 1.4056 0.08221 0.07647 -0.0384 0.0373 1.0000 18.000 1.4080 0.08860 0.08306 -0.0401 0.0344 1.0000 18.500 1.4022 0.09598 0.09069 -0.0418 0.0323 1.0000 19.000 1.3902 0.10364 0.09879 -0.0421 0.0343 1.0000 19.500 1.3920 0.11106 0.10625 -0.0466 0.0309 1.0000 20.000 1.3642 0.12239 0.11770 -0.0519 0.0262 1.0000 20.500 1.3407 0.13299 0.12870 -0.0566 0.0265 1.0000 21.000 1.3327 0.14273 0.13866 -0.0631 0.0248 1.0000 21.500 1.2852 0.15777 0.15416 -0.0723 0.0269 1.0000 22.000 1.2593 0.17281 0.16940 -0.0834 0.0219 1.0000 22.500 1.2151 0.19234 0.18917 -0.0960 0.0203 1.0000 24.500 1.0366 0.31624 0.31345 -0.1428 0.0270 1.0000 25.000 1.0347 0.33273 0.32991 -0.1468 0.0265 1.0000 25.500 1.0411 0.34343 0.34066 -0.1502 0.0265 1.0000 26.000 1.0458 0.35409 0.35135 -0.1542 0.0264 1.0000 26.500 1.0493 0.36452 0.36181 -0.1577 0.0263 1.0000 27.000 1.0510 0.37537 0.37269 -0.1613 0.0261 1.0000 27.500 1.0486 0.38680 0.38412 -0.1664 0.0253 1.0000 28.000 1.0454 0.39718 0.39452 -0.1672 0.0258 1.0000 28.500 1.0412 0.40666 0.40405 -0.1708 0.0202 1.0000 29.500 0.8448 0.36561 0.36331 -0.1379 0.0170 1.0000 30.000 0.8337 0.36634 0.36410 -0.1391 0.0169 1.0000 30.500 0.8254 0.36754 0.36536 -0.1410 0.0168 1.0000 31.000 0.8186 0.36902 0.36691 -0.1434 0.0167 1.0000 31.500 0.8139 0.37180 0.36975 -0.1463 0.0164 1.0000 32.000 0.8123 0.37519 0.37318 -0.1493 0.0156 1.0000 32.500 0.8105 0.37756 0.37561 -0.1519 0.0134 1.0000 33.000 0.8090 0.37915 0.37725 -0.1544 0.0119 1.0000 33.500 0.8084 0.38000 0.37815 -0.1568 0.0107 1.0000 34.000 0.8077 0.38046 0.37868 -0.1591 0.0102 1.0000 34.500 0.8014 0.38104 0.37931 -0.1606 0.0095 1.0000 35.000 0.8019 0.38276 0.38108 -0.1628 0.0096 1.0000 35.500 0.7972 0.38681 0.38517 -0.1659 0.0094 1.0000 36.000 0.7964 0.38932 0.38772 -0.1684 0.0094 1.0000 36.500 0.7945 0.39327 0.39169 -0.1711 0.0092 1.0000 37.000 0.7944 0.39831 0.39677 -0.1736 0.0074 1.0000 37.500 0.7934 0.40090 0.39938 -0.1760 0.0059 1.0000 38.000 0.7921 0.40355 0.40208 -0.1783 0.0058 1.0000 38.500 0.7907 0.40628 0.40485 -0.1806 0.0063 1.0000 39.000 0.7891 0.40917 0.40778 -0.1828 0.0071 1.0000 39.500 0.7875 0.41154 0.41019 -0.1851 0.0056 1.0000 40.000 0.7859 0.41437 0.41305 -0.1872 0.0054 1.0000 40.500 0.7838 0.41632 0.41502 -0.1893 0.0048 1.0000 41.000 0.7819 0.41814 0.41688 -0.1916 0.0047 1.0000 41.500 0.7795 0.42134 0.42011 -0.1937 0.0047 1.0000 42.500 0.7719 0.42491 0.42373 -0.1968 0.0042 1.0000 43.000 0.7688 0.42886 0.42771 -0.1990 0.0042 1.0000 43.500 0.7661 0.43066 0.42955 -0.2011 0.0042 1.0000 44.000 0.7629 0.43470 0.43360 -0.2032 0.0042 1.0000 44.500 0.7600 0.43798 0.43692 -0.2055 0.0042 1.0000 45.000 0.7578 0.44414 0.44311 -0.2078 0.0040 1.0000 45.500 0.7555 0.44935 0.44833 -0.2098 0.0038 1.0000 46.000 0.7522 0.45257 0.45157 -0.2117 0.0035 1.0000 46.500 0.7487 0.45578 0.45482 -0.2139 0.0037 1.0000