Airfoil: FX 63-137 (C) Builder: Y. Tinel Comment: clean Number of Reynolds #'s: 5 Average Reynolds #: 100019 Number of angles of attack: 61 alpha / Cl / Cm -10.08 -0.223 -0.0207 -9.04 -0.260 -0.0079 -8.07 -0.317 0.0005 -7.08 -0.328 -0.0120 -6.10 -0.304 -0.0281 -5.11 0.013 -0.1463 -4.14 0.134 -0.1707 -3.12 0.263 -0.1764 -2.04 0.391 -0.1885 -1.05 0.466 -0.1694 -0.07 0.530 -0.1616 1.02 0.630 -0.1703 2.00 0.655 -0.1568 3.08 0.698 -0.1653 4.06 0.864 -0.1704 5.11 1.152 -0.1632 6.16 1.304 -0.1706 7.16 1.417 -0.1551 8.18 1.520 -0.1672 9.31 1.611 -0.1574 10.26 1.677 -0.1448 11.31 1.722 -0.1460 12.29 1.739 -0.1430 13.30 1.735 -0.1358 14.31 1.731 -0.1302 15.37 1.739 -0.1291 16.28 1.733 -0.1309 17.33 1.734 -0.1281 17.99 1.193 -0.2612 19.03 1.211 -0.2783 20.03 1.244 -0.2839 19.51 1.232 -0.2913 18.54 1.175 -0.2749 17.52 1.174 -0.2621 16.56 1.159 -0.2469 15.56 1.219 -0.2443 14.54 1.214 -0.2313 13.63 1.196 -0.2190 12.86 1.734 -0.1363 11.80 1.740 -0.1391 10.74 1.698 -0.1583 9.79 1.649 -0.1656 8.72 1.565 -0.1545 7.66 1.476 -0.1623 6.70 1.371 -0.1589 5.65 1.235 -0.1593 4.54 0.883 -0.1620 3.51 0.773 -0.1693 2.52 0.692 -0.1652 1.53 0.649 -0.1586 0.48 0.587 -0.1638 -0.53 0.520 -0.1691 -1.54 0.453 -0.1731 -2.61 0.358 -0.1728 -3.65 0.216 -0.1659 -4.64 0.096 -0.1569 -5.64 -0.227 -0.0739 -6.60 -0.318 -0.0198 -7.61 -0.287 -0.0082 -8.56 -0.266 -0.0064 -9.55 -0.236 -0.0104 Tabulated from data in file bm04996.dat & reduced using program C10.20 Average Reynolds #: 150054 Number of angles of attack: 61 alpha / Cl / Cm -10.02 -0.224 -0.0149 -9.02 -0.253 -0.0118 -8.04 -0.241 -0.0309 -7.11 -0.194 -0.0582 -6.16 0.016 -0.1689 -5.15 0.172 -0.1825 -4.14 0.316 -0.1984 -3.06 0.451 -0.2001 -2.05 0.559 -0.1996 -1.04 0.657 -0.1971 0.02 0.749 -0.1933 1.06 0.833 -0.1867 2.02 0.925 -0.1795 3.09 1.028 -0.1799 4.10 1.121 -0.1724 5.14 1.224 -0.1715 6.15 1.331 -0.1747 7.18 1.430 -0.1723 8.21 1.516 -0.1679 9.27 1.597 -0.1608 10.26 1.662 -0.1555 11.31 1.704 -0.1474 12.30 1.708 -0.1360 13.30 1.708 -0.1269 14.28 1.709 -0.1210 15.28 1.720 -0.1178 16.33 1.714 -0.1162 17.35 1.708 -0.1193 18.25 1.686 -0.1308 18.98 1.158 -0.2588 20.01 1.176 -0.2662 19.49 1.221 -0.2823 18.50 1.165 -0.2659 17.52 1.156 -0.2592 16.56 1.177 -0.2537 15.54 1.201 -0.2471 14.56 1.206 -0.2329 13.83 1.709 -0.1286 12.76 1.706 -0.1347 11.76 1.706 -0.1458 10.75 1.686 -0.1560 9.73 1.621 -0.1624 8.74 1.560 -0.1669 7.68 1.476 -0.1733 6.67 1.387 -0.1747 5.64 1.281 -0.1752 4.59 1.169 -0.1753 3.58 1.079 -0.1770 2.57 0.981 -0.1796 1.54 0.888 -0.1833 0.49 0.795 -0.1880 -0.52 0.701 -0.1956 -1.57 0.607 -0.1975 -2.57 0.512 -0.2011 -3.57 0.395 -0.1999 -4.61 0.258 -0.1943 -5.64 0.109 -0.1819 -6.66 -0.129 -0.0916 -7.59 -0.209 -0.0380 -8.58 -0.254 -0.0161 -9.56 -0.230 -0.0110 Tabulated from data in file bm04998.dat & reduced using program C10.20 Average Reynolds #: 199952 Number of angles of attack: 61 alpha / Cl / Cm -10.07 -0.227 -0.0112 -9.06 -0.244 -0.0195 -8.05 -0.188 -0.0437 -7.14 -0.102 -0.0862 -6.18 0.093 -0.1836 -5.13 0.225 -0.1906 -4.06 0.340 -0.1955 -3.07 0.452 -0.2006 -2.10 0.559 -0.1988 -1.08 0.660 -0.1984 0.04 0.767 -0.1951 1.03 0.863 -0.1920 2.01 0.964 -0.1898 3.08 1.070 -0.1869 4.14 1.171 -0.1848 5.15 1.257 -0.1801 6.17 1.356 -0.1784 7.16 1.452 -0.1756 8.19 1.538 -0.1710 9.23 1.621 -0.1656 10.25 1.679 -0.1573 11.34 1.715 -0.1470 12.28 1.717 -0.1363 13.28 1.722 -0.1290 14.35 1.727 -0.1232 15.36 1.735 -0.1207 16.34 1.741 -0.1204 17.35 1.746 -0.1225 18.27 1.734 -0.1254 19.31 1.736 -0.1368 20.27 1.685 -0.1430 19.79 1.692 -0.1398 18.81 1.728 -0.1336 17.79 1.741 -0.1279 16.78 1.745 -0.1237 15.80 1.735 -0.1235 14.83 1.731 -0.1241 13.77 1.720 -0.1278 12.81 1.713 -0.1341 11.78 1.719 -0.1448 10.78 1.697 -0.1554 9.76 1.650 -0.1643 8.71 1.582 -0.1715 7.71 1.503 -0.1761 6.68 1.410 -0.1801 5.67 1.310 -0.1809 4.56 1.219 -0.1857 3.55 1.122 -0.1888 2.56 1.023 -0.1908 1.55 0.921 -0.1928 0.54 0.822 -0.1964 -0.52 0.721 -0.1982 -1.55 0.620 -0.2003 -2.59 0.514 -0.2025 -3.61 0.397 -0.1987 -4.61 0.292 -0.1986 -5.65 0.167 -0.1891 -6.65 0.002 -0.1539 -7.60 -0.143 -0.0576 -8.58 -0.213 -0.0321 -9.55 -0.226 -0.0205 Tabulated from data in file bm05000.dat & reduced using program C10.20 Average Reynolds #: 349860 Number of angles of attack: 61 alpha / Cl / Cm -10.05 -0.215 -0.0199 -9.08 -0.194 -0.0370 -8.15 -0.133 -0.0691 -7.14 -0.036 -0.1323 -6.12 0.129 -0.1869 -5.09 0.251 -0.1940 -4.15 0.352 -0.1956 -3.07 0.483 -0.2009 -2.08 0.598 -0.2045 -1.05 0.704 -0.2027 0.01 0.819 -0.2019 1.04 0.922 -0.2004 1.99 1.023 -0.1995 3.09 1.129 -0.1964 4.15 1.240 -0.1941 5.13 1.327 -0.1903 6.18 1.425 -0.1861 7.19 1.509 -0.1804 8.24 1.593 -0.1747 9.26 1.647 -0.1662 10.31 1.692 -0.1554 11.28 1.717 -0.1453 12.27 1.728 -0.1365 13.28 1.741 -0.1298 14.33 1.749 -0.1264 15.29 1.762 -0.1253 16.32 1.759 -0.1249 17.30 1.765 -0.1280 18.25 1.756 -0.1304 19.28 1.741 -0.1347 20.30 1.724 -0.1406 19.77 1.726 -0.1389 18.80 1.763 -0.1365 17.80 1.754 -0.1294 16.81 1.758 -0.1270 15.80 1.763 -0.1257 14.80 1.753 -0.1265 13.81 1.738 -0.1286 12.76 1.733 -0.1347 11.74 1.723 -0.1433 10.85 1.705 -0.1517 9.74 1.669 -0.1622 8.72 1.621 -0.1719 7.68 1.547 -0.1786 6.62 1.467 -0.1847 5.65 1.385 -0.1905 4.61 1.283 -0.1943 3.63 1.188 -0.1966 2.55 1.080 -0.1989 1.57 0.969 -0.1995 0.46 0.859 -0.2016 -0.49 0.764 -0.2036 -1.53 0.648 -0.2045 -2.56 0.536 -0.2043 -3.61 0.411 -0.1986 -4.67 0.295 -0.1956 -5.65 0.181 -0.1903 -6.69 0.067 -0.1812 -7.57 -0.089 -0.0967 -8.63 -0.171 -0.0500 -9.62 -0.209 -0.0262 Tabulated from data in file bm05002.dat & reduced using program C10.20 Average Reynolds #: 499848 Number of angles of attack: 61 alpha / Cl / Cm -10.20 -0.235 -0.0254 -9.10 -0.193 -0.0476 -8.32 -0.152 -0.0757 -7.31 -0.042 -0.1319 -6.11 0.137 -0.1860 -5.04 0.257 -0.1901 -4.13 0.361 -0.1931 -3.04 0.493 -0.1978 -2.02 0.616 -0.2013 -0.97 0.720 -0.2003 -0.02 0.819 -0.1986 1.00 0.928 -0.1980 2.08 1.031 -0.1964 3.15 1.143 -0.1936 4.17 1.243 -0.1910 5.19 1.345 -0.1874 6.17 1.444 -0.1833 7.17 1.525 -0.1770 8.23 1.599 -0.1678 9.27 1.656 -0.1579 10.28 1.687 -0.1468 11.37 1.714 -0.1363 12.32 1.723 -0.1302 13.30 1.739 -0.1254 14.28 1.749 -0.1246 15.35 1.747 -0.1232 16.34 1.760 -0.1255 17.34 1.746 -0.1271 18.35 1.729 -0.1308 19.31 1.737 -0.1377 20.29 1.715 -0.1455 19.77 1.720 -0.1436 18.77 1.730 -0.1348 17.82 1.732 -0.1298 16.74 1.753 -0.1277 15.82 1.763 -0.1267 14.86 1.745 -0.1248 13.75 1.744 -0.1263 12.74 1.736 -0.1293 11.79 1.727 -0.1348 10.74 1.711 -0.1433 9.71 1.681 -0.1547 8.68 1.622 -0.1645 7.74 1.572 -0.1738 6.68 1.485 -0.1805 5.62 1.395 -0.1866 4.62 1.300 -0.1908 3.63 1.189 -0.1928 2.52 1.081 -0.1952 1.49 0.984 -0.1981 0.50 0.873 -0.1989 -0.54 0.770 -0.2005 -1.52 0.666 -0.2012 -2.57 0.546 -0.1993 -3.63 0.422 -0.1948 -4.64 0.302 -0.1924 -5.64 0.188 -0.1873 -6.69 0.072 -0.1807 -7.62 -0.085 -0.1116 -8.57 -0.155 -0.0608 -9.55 -0.208 -0.0354 Tabulated from data in file bm05004.dat & reduced using program C10.20 File fx63137_c.lft created using program C10.20 on Thu May 22 17:01:21 2003