Airfoil: FX 63-137 (C) Builder: Y. Tinel Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' Number of Reynolds #'s: 5 Average Reynolds #: 99985 Number of angles of attack: 61 alpha / Cl / Cm -10.08 -0.218 -0.0337 -9.07 -0.270 -0.0203 -8.09 -0.288 -0.0167 -7.12 -0.340 -0.0133 -6.08 -0.312 -0.0326 -5.13 -0.012 -0.1532 -4.14 0.116 -0.1651 -3.12 0.244 -0.1727 -2.09 0.368 -0.1807 -1.05 0.456 -0.1646 -0.01 0.527 -0.1677 0.98 0.598 -0.1693 2.03 0.656 -0.1654 3.11 0.880 -0.1560 4.11 1.016 -0.1454 5.13 1.140 -0.1502 6.19 1.237 -0.1543 7.21 1.336 -0.1510 8.23 1.410 -0.1436 9.26 1.485 -0.1295 10.26 1.528 -0.1328 11.29 1.532 -0.1219 12.24 1.514 -0.1242 13.27 1.503 -0.1234 14.24 1.491 -0.1279 15.27 1.495 -0.1273 16.24 1.508 -0.1309 17.26 1.545 -0.1337 18.26 1.566 -0.1376 19.05 1.109 -0.2642 20.03 1.191 -0.2861 19.48 1.134 -0.2838 18.47 1.102 -0.2707 17.50 1.066 -0.2508 16.50 1.107 -0.2425 15.57 1.199 -0.2268 14.80 1.506 -0.1251 13.74 1.511 -0.1276 12.74 1.520 -0.1220 11.80 1.534 -0.1200 10.69 1.540 -0.1271 9.76 1.515 -0.1385 8.71 1.461 -0.1383 7.68 1.390 -0.1429 6.68 1.299 -0.1466 5.61 1.205 -0.1560 4.59 1.079 -0.1497 3.60 0.963 -0.1604 2.48 0.699 -0.1640 1.45 0.620 -0.1616 0.50 0.568 -0.1676 -0.56 0.501 -0.1723 -1.59 0.432 -0.1879 -2.59 0.316 -0.1707 -3.60 0.181 -0.1614 -4.57 0.073 -0.1585 -5.60 -0.244 -0.0700 -6.59 -0.307 -0.0244 -7.59 -0.319 -0.0181 -8.62 -0.277 -0.0266 -9.56 -0.251 -0.0335 Tabulated from data in file bm05006.dat & reduced using program C10.20 Average Reynolds #: 149980 Number of angles of attack: 61 alpha / Cl / Cm -10.13 -0.239 -0.0144 -9.09 -0.261 -0.0177 -8.07 -0.267 -0.0268 -7.11 -0.197 -0.0566 -6.16 -0.023 -0.1541 -5.14 0.159 -0.1856 -4.12 0.302 -0.1925 -3.06 0.422 -0.1982 -2.06 0.535 -0.1980 -1.03 0.643 -0.1927 0.05 0.742 -0.1908 1.03 0.832 -0.1868 2.09 0.933 -0.1789 3.07 1.024 -0.1751 4.10 1.097 -0.1650 5.12 1.168 -0.1579 6.18 1.244 -0.1557 7.18 1.306 -0.1494 8.21 1.352 -0.1418 9.23 1.384 -0.1324 10.19 1.420 -0.1296 11.25 1.442 -0.1274 12.24 1.463 -0.1252 13.25 1.474 -0.1269 14.24 1.483 -0.1300 15.26 1.485 -0.1329 16.24 1.489 -0.1407 17.21 1.470 -0.1416 18.24 1.460 -0.1474 19.26 1.491 -0.1509 20.00 1.190 -0.2624 19.56 1.181 -0.2647 18.54 1.271 -0.2632 17.54 1.285 -0.2448 16.60 1.322 -0.2299 15.62 1.296 -0.2128 14.76 1.489 -0.1368 13.74 1.486 -0.1321 12.72 1.470 -0.1291 11.75 1.454 -0.1287 10.71 1.432 -0.1293 9.72 1.407 -0.1326 8.73 1.372 -0.1383 7.65 1.327 -0.1455 6.64 1.269 -0.1518 5.61 1.207 -0.1596 4.62 1.129 -0.1618 3.57 1.059 -0.1697 2.56 0.977 -0.1760 1.52 0.881 -0.1807 0.54 0.790 -0.1858 -0.51 0.698 -0.1916 -1.57 0.595 -0.1934 -2.61 0.483 -0.1931 -3.60 0.365 -0.1962 -4.64 0.233 -0.1856 -5.68 0.077 -0.1715 -6.63 -0.147 -0.0765 -7.61 -0.216 -0.0403 -8.62 -0.275 -0.0177 -9.58 -0.244 -0.0171 Tabulated from data in file bm05008.dat & reduced using program C10.20 Average Reynolds #: 200005 Number of angles of attack: 61 alpha / Cl / Cm -10.11 -0.212 -0.0155 -9.09 -0.246 -0.0197 -8.08 -0.185 -0.0436 -7.09 -0.110 -0.0857 -6.17 0.085 -0.1815 -5.15 0.207 -0.1908 -4.11 0.321 -0.1936 -3.10 0.431 -0.1959 -2.07 0.538 -0.1944 -1.01 0.640 -0.1919 0.01 0.752 -0.1912 1.01 0.849 -0.1879 2.03 0.937 -0.1812 3.07 1.006 -0.1735 4.09 1.084 -0.1673 5.17 1.162 -0.1608 6.16 1.225 -0.1550 7.15 1.296 -0.1501 8.22 1.346 -0.1430 9.25 1.392 -0.1366 10.26 1.426 -0.1327 11.27 1.453 -0.1311 12.25 1.478 -0.1309 13.23 1.492 -0.1309 14.22 1.500 -0.1334 15.26 1.495 -0.1367 16.25 1.489 -0.1415 17.24 1.509 -0.1481 18.21 1.482 -0.1509 19.25 1.494 -0.1600 20.17 1.496 -0.1632 19.70 1.493 -0.1649 18.70 1.506 -0.1608 17.70 1.492 -0.1520 16.71 1.512 -0.1479 15.73 1.506 -0.1420 14.71 1.508 -0.1378 13.71 1.501 -0.1349 12.72 1.491 -0.1334 11.67 1.471 -0.1329 10.72 1.444 -0.1340 9.77 1.411 -0.1369 8.71 1.379 -0.1427 7.67 1.326 -0.1487 6.64 1.257 -0.1543 5.62 1.199 -0.1610 4.60 1.131 -0.1671 3.59 1.052 -0.1734 2.54 0.981 -0.1806 1.51 0.892 -0.1862 0.55 0.805 -0.1905 -0.53 0.695 -0.1934 -1.56 0.595 -0.1961 -2.59 0.487 -0.1965 -3.64 0.377 -0.1942 -4.62 0.269 -0.1912 -5.66 0.150 -0.1866 -6.61 -0.014 -0.1435 -7.59 -0.156 -0.0625 -8.59 -0.225 -0.0313 -9.61 -0.233 -0.0180 Tabulated from data in file bm05010.dat & reduced using program C10.20 Average Reynolds #: 349891 Number of angles of attack: 61 alpha / Cl / Cm -10.15 -0.252 -0.0298 -9.08 -0.213 -0.0451 -8.12 -0.143 -0.0780 -7.17 -0.044 -0.1271 -6.13 0.126 -0.1858 -5.09 0.241 -0.1898 -4.08 0.362 -0.1943 -3.05 0.468 -0.1943 -2.02 0.568 -0.1919 -1.00 0.658 -0.1885 -0.01 0.746 -0.1843 1.00 0.839 -0.1819 2.01 0.927 -0.1789 3.08 1.027 -0.1761 4.10 1.109 -0.1717 5.10 1.195 -0.1675 6.19 1.276 -0.1629 7.15 1.337 -0.1564 8.20 1.383 -0.1480 9.25 1.419 -0.1420 10.21 1.455 -0.1384 11.23 1.492 -0.1368 12.23 1.509 -0.1363 13.21 1.527 -0.1370 14.25 1.538 -0.1393 15.24 1.519 -0.1428 16.22 1.508 -0.1456 17.16 1.521 -0.1523 18.20 1.516 -0.1576 19.20 1.518 -0.1651 20.19 1.500 -0.1710 19.69 1.514 -0.1698 18.67 1.521 -0.1624 17.72 1.513 -0.1545 16.72 1.527 -0.1501 15.72 1.526 -0.1448 14.70 1.532 -0.1403 13.68 1.534 -0.1389 12.71 1.512 -0.1344 11.74 1.492 -0.1352 10.69 1.469 -0.1371 9.73 1.433 -0.1393 8.67 1.398 -0.1446 7.66 1.361 -0.1524 6.65 1.309 -0.1599 5.64 1.233 -0.1652 4.61 1.155 -0.1697 3.64 1.068 -0.1732 2.59 0.976 -0.1772 1.52 0.884 -0.1807 0.49 0.790 -0.1833 -0.50 0.696 -0.1864 -1.57 0.607 -0.1907 -2.60 0.511 -0.1952 -3.58 0.409 -0.1952 -4.63 0.297 -0.1922 -5.67 0.172 -0.1877 -6.64 0.060 -0.1813 -7.56 -0.099 -0.1000 -8.63 -0.181 -0.0509 -9.62 -0.223 -0.0267 Tabulated from data in file bm05012.dat & reduced using program C10.20 Average Reynolds #: 499970 Number of angles of attack: 61 alpha / Cl / Cm -10.10 -0.218 -0.0234 -9.16 -0.191 -0.0438 -8.14 -0.129 -0.0760 -7.12 -0.025 -0.1402 -6.16 0.132 -0.1850 -5.08 0.259 -0.1912 -4.08 0.358 -0.1907 -3.05 0.460 -0.1899 -2.03 0.566 -0.1886 -1.04 0.654 -0.1857 0.02 0.752 -0.1833 1.06 0.841 -0.1807 2.08 0.939 -0.1778 3.10 1.028 -0.1737 4.15 1.118 -0.1705 5.13 1.195 -0.1662 6.17 1.267 -0.1597 7.15 1.336 -0.1532 8.18 1.390 -0.1468 9.20 1.431 -0.1420 10.19 1.475 -0.1389 11.24 1.497 -0.1380 12.24 1.508 -0.1383 13.22 1.519 -0.1419 14.22 1.525 -0.1449 15.28 1.519 -0.1472 16.28 1.519 -0.1518 17.26 1.506 -0.1552 18.20 1.509 -0.1627 19.22 1.496 -0.1666 20.20 1.516 -0.1770 19.71 1.495 -0.1708 18.73 1.507 -0.1652 17.65 1.511 -0.1586 16.71 1.520 -0.1540 15.71 1.511 -0.1494 14.72 1.531 -0.1466 13.67 1.530 -0.1423 12.72 1.520 -0.1389 11.72 1.512 -0.1378 10.72 1.476 -0.1375 9.75 1.452 -0.1399 8.67 1.414 -0.1440 7.69 1.364 -0.1492 6.64 1.308 -0.1567 5.64 1.236 -0.1626 4.60 1.161 -0.1684 3.56 1.065 -0.1722 2.50 0.973 -0.1753 1.49 0.883 -0.1787 0.47 0.787 -0.1820 -0.51 0.693 -0.1834 -1.54 0.611 -0.1869 -2.61 0.503 -0.1879 -3.54 0.412 -0.1901 -4.61 0.296 -0.1902 -5.60 0.190 -0.1871 -6.69 0.066 -0.1818 -7.57 -0.081 -0.1042 -8.53 -0.150 -0.0627 -9.43 -0.198 -0.0381 Tabulated from data in file bm05014.dat & reduced using program C10.20 File fx63137_tf.lft created using program C10.20 on Thu May 22 17:01:21 2003