XFOIL Version 6.94 Calculated polar for: PSU 94-097 (AIAA 2001-2478) 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.450 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.4860 0.00685 0.00259 -0.1065 0.7424 1.0000 0.500 0.5455 0.00686 0.00249 -0.1073 0.7312 1.0000 1.000 0.6042 0.00694 0.00242 -0.1078 0.7179 1.0000 1.500 0.6624 0.00720 0.00251 -0.1084 0.6997 1.0000 2.000 0.7207 0.00723 0.00254 -0.1089 0.6898 1.0000 2.500 0.7784 0.00732 0.00258 -0.1093 0.6732 1.0000 3.000 0.8353 0.00756 0.00273 -0.1095 0.6525 1.0000 3.500 0.8927 0.00763 0.00286 -0.1099 0.6352 1.0000 4.000 0.9483 0.00789 0.00303 -0.1098 0.6059 1.0000 4.500 1.0038 0.00812 0.00324 -0.1098 0.5718 1.0000 5.000 1.0561 0.00865 0.00360 -0.1093 0.5142 1.0000 5.500 1.1069 0.00937 0.00410 -0.1086 0.4464 1.0000 6.000 1.1536 0.01050 0.00485 -0.1074 0.3630 1.0000 6.500 1.1992 0.01171 0.00572 -0.1062 0.2912 1.0000 7.000 1.2448 0.01286 0.00667 -0.1050 0.2351 1.0000 7.500 1.2882 0.01412 0.00769 -0.1035 0.1810 1.0000 8.000 1.3298 0.01544 0.00882 -0.1017 0.1384 1.0000 8.500 1.3684 0.01691 0.01027 -0.0994 0.0975 1.0000 9.000 1.4025 0.01859 0.01183 -0.0965 0.0625 1.0000 9.500 1.4215 0.02115 0.01424 -0.0912 0.0312 1.0000 10.000 1.4366 0.02356 0.01673 -0.0855 0.0202 1.0000 10.500 1.4545 0.02595 0.01936 -0.0811 0.0162 1.0000 11.000 1.4775 0.02807 0.02163 -0.0779 0.0124 1.0000 11.500 1.4592 0.03408 0.02801 -0.0713 0.0072 1.0000 12.000 1.4656 0.03806 0.03227 -0.0678 0.0060 1.0000 12.500 1.4580 0.04390 0.03847 -0.0641 0.0053 1.0000 13.000 1.4470 0.05048 0.04543 -0.0611 0.0048 1.0000 13.500 1.4332 0.05756 0.05287 -0.0591 0.0044 1.0000 14.000 1.4200 0.06487 0.06050 -0.0583 0.0040 1.0000 14.500 1.4031 0.07374 0.06971 -0.0591 0.0037 1.0000 15.000 1.3842 0.08380 0.08017 -0.0617 0.0035 1.0000 15.500 1.3568 0.09602 0.09276 -0.0660 0.0034 1.0000 16.000 1.3280 0.10934 0.10642 -0.0722 0.0034 1.0000 16.500 1.2885 0.12566 0.12312 -0.0809 0.0035 1.0000 17.000 1.2551 0.14118 0.13887 -0.0906 0.0036 1.0000 17.500 1.2054 0.16354 0.16155 -0.1038 0.0040 1.0000 18.000 1.1277 0.20109 0.19932 -0.1220 0.0054 1.0000 18.500 1.0920 0.22947 0.22763 -0.1318 0.0059 1.0000 19.000 1.0813 0.24825 0.24636 -0.1376 0.0062 1.0000 19.500 1.0761 0.26443 0.26251 -0.1421 0.0064 1.0000 20.000 1.0740 0.27866 0.27673 -0.1457 0.0063 1.0000 20.500 1.0728 0.29190 0.28997 -0.1488 0.0059 1.0000 21.000 1.0683 0.30511 0.30317 -0.1512 0.0059 1.0000 21.500 1.0591 0.31765 0.31571 -0.1527 0.0064 1.0000 22.500 0.9360 0.31514 0.31328 -0.1362 0.0074 1.0000 23.000 0.9125 0.31589 0.31405 -0.1339 0.0074 1.0000 23.500 0.8957 0.31764 0.31582 -0.1328 0.0074 1.0000 24.000 0.8829 0.31984 0.31803 -0.1323 0.0074 1.0000 24.500 0.8729 0.32231 0.32053 -0.1322 0.0074 1.0000 25.000 0.8645 0.32492 0.32316 -0.1324 0.0073 1.0000 25.500 0.8576 0.32775 0.32600 -0.1329 0.0073 1.0000 26.000 0.8518 0.33056 0.32883 -0.1335 0.0073 1.0000 26.500 0.8470 0.33355 0.33184 -0.1343 0.0072 1.0000 27.000 0.8429 0.33658 0.33489 -0.1353 0.0072 1.0000 27.500 0.8395 0.33963 0.33800 -0.1363 0.0071 1.0000 28.000 0.8368 0.34288 0.34127 -0.1377 0.0070 1.0000 28.500 0.8350 0.34628 0.34469 -0.1392 0.0068 1.0000 29.000 0.8347 0.35009 0.34852 -0.1408 0.0061 1.0000 29.500 0.8332 0.35351 0.35197 -0.1422 0.0054 1.0000 30.000 0.8311 0.35662 0.35509 -0.1434 0.0047 1.0000 30.500 0.8291 0.35977 0.35826 -0.1448 0.0042 1.0000 31.000 0.8272 0.36281 0.36133 -0.1462 0.0038 1.0000 31.500 0.8254 0.36590 0.36444 -0.1476 0.0034 1.0000 32.000 0.8236 0.36895 0.36751 -0.1491 0.0032 1.0000 32.500 0.8217 0.37189 0.37047 -0.1506 0.0029 1.0000 33.000 0.8200 0.37489 0.37350 -0.1521 0.0027 1.0000 33.500 0.8182 0.37778 0.37645 -0.1537 0.0025 1.0000 34.000 0.8164 0.38060 0.37930 -0.1553 0.0024 1.0000 34.500 0.8144 0.38333 0.38204 -0.1569 0.0022 1.0000 35.000 0.8124 0.38596 0.38470 -0.1585 0.0021 1.0000 35.500 0.8100 0.38841 0.38718 -0.1599 0.0019 1.0000 37.000 0.7988 0.39825 0.39706 -0.1636 0.0016 1.0000 37.500 0.7965 0.40141 0.40023 -0.1654 0.0016 1.0000 38.000 0.7943 0.40469 0.40354 -0.1672 0.0016 1.0000 38.500 0.7919 0.40793 0.40682 -0.1690 0.0016 1.0000 39.000 0.7893 0.41095 0.40986 -0.1708 0.0016 1.0000 39.500 0.7868 0.41411 0.41304 -0.1727 0.0016 1.0000 40.000 0.7841 0.41720 0.41616 -0.1746 0.0016 1.0000 40.500 0.7813 0.42033 0.41931 -0.1764 0.0016 1.0000 41.000 0.7784 0.42333 0.42234 -0.1783 0.0016 1.0000 41.500 0.7754 0.42633 0.42535 -0.1802 0.0016 1.0000 42.000 0.7723 0.42936 0.42840 -0.1821 0.0016 1.0000 42.500 0.7690 0.43237 0.43144 -0.1841 0.0016 1.0000 43.000 0.7656 0.43536 0.43447 -0.1860 0.0016 1.0000 43.500 0.7622 0.43840 0.43753 -0.1880 0.0016 1.0000 44.000 0.7587 0.44142 0.44058 -0.1900 0.0015 1.0000 44.500 0.7550 0.44441 0.44358 -0.1919 0.0015 1.0000 45.000 0.7512 0.44742 0.44662 -0.1939 0.0015 1.0000 45.500 0.7472 0.45023 0.44945 -0.1959 0.0015 1.0000 46.000 0.7432 0.45321 0.45244 -0.1979 0.0015 1.0000 46.500 0.7390 0.45613 0.45539 -0.1999 0.0015 1.0000 47.000 0.7347 0.45898 0.45826 -0.2018 0.0015 1.0000 47.500 0.7303 0.46183 0.46115 -0.2038 0.0015 1.0000 48.000 0.7256 0.46445 0.46379 -0.2058 0.0015 1.0000 48.500 0.7210 0.46723 0.46658 -0.2078 0.0015 1.0000 49.000 0.7162 0.47003 0.46941 -0.2098 0.0015 1.0000 49.500 0.7114 0.47280 0.47220 -0.2118 0.0014 1.0000 50.000 0.7064 0.47549 0.47491 -0.2137 0.0014 1.0000 50.500 0.7013 0.47828 0.47772 -0.2157 0.0014 1.0000 51.000 0.6962 0.48106 0.48052 -0.2176 0.0014 1.0000 51.500 0.6909 0.48375 0.48322 -0.2195 0.0013 1.0000 52.000 0.6854 0.48642 0.48593 -0.2215 0.0013 1.0000 52.500 0.6796 0.48884 0.48837 -0.2234 0.0013 1.0000 53.000 0.6738 0.49127 0.49082 -0.2254 0.0012 1.0000 53.500 0.6676 0.49337 0.49294 -0.2273 0.0012 1.0000 54.000 0.6614 0.49577 0.49536 -0.2293 0.0012 1.0000 54.500 0.6551 0.49816 0.49776 -0.2313 0.0011 1.0000 55.000 0.6487 0.50040 0.50002 -0.2333 0.0011 1.0000 55.500 0.6419 0.50232 0.50196 -0.2352 0.0011 1.0000 56.000 0.6351 0.50433 0.50400 -0.2372 0.0010 1.0000 56.500 0.6283 0.50656 0.50625 -0.2392 0.0010 1.0000 57.000 0.6212 0.50845 0.50817 -0.2412 0.0010 1.0000 57.500 0.6141 0.51037 0.51010 -0.2432 0.0010 1.0000 58.000 0.6068 0.51230 0.51205 -0.2452 0.0009 1.0000 58.500 0.5995 0.51425 0.51402 -0.2472 0.0008 1.0000 59.000 0.5920 0.51611 0.51589 -0.2492 0.0008 1.0000 59.500 0.5845 0.51799 0.51780 -0.2512 0.0007 1.0000 60.000 0.5768 0.51969 0.51952 -0.2531 0.0005 1.0000