Airfoil: SG6043 Builder: M. Allen Comment: clean Number of Reynolds #'s: 6 Average Reynolds #: 99911 Number of angles of attack: 59 alpha / Cl / Cm -8.82 -0.313 0.0157 -7.96 -0.334 0.0187 -6.90 -0.383 0.0207 -5.82 -0.372 0.0173 -4.94 -0.359 -0.0022 -4.07 -0.247 -0.0451 -3.02 0.067 -0.1285 -1.95 0.196 -0.1427 -0.90 0.299 -0.1476 0.10 0.387 -0.1498 1.11 0.478 -0.1513 2.39 0.646 -0.1595 3.14 0.763 -0.1641 4.22 0.988 -0.1724 5.19 1.125 -0.1707 6.29 1.230 -0.1639 7.27 1.305 -0.1576 8.40 1.391 -0.1510 9.36 1.436 -0.1438 10.34 1.448 -0.1304 11.43 1.464 -0.1224 12.33 1.478 -0.1180 13.30 1.501 -0.1130 14.45 1.511 -0.1060 15.45 1.519 -0.1053 16.12 1.137 -0.2010 17.37 1.182 -0.2151 18.27 1.211 -0.2191 19.28 1.202 -0.2290 20.27 1.273 -0.2240 19.37 1.197 -0.2323 18.46 1.223 -0.2384 17.45 1.198 -0.2298 16.48 1.158 -0.2153 15.49 1.161 -0.2130 14.42 1.164 -0.2045 13.57 1.509 -0.1198 12.72 1.488 -0.1222 11.66 1.460 -0.1313 10.71 1.449 -0.1376 9.58 1.434 -0.1443 8.42 1.399 -0.1556 7.38 1.329 -0.1614 6.58 1.269 -0.1666 5.61 1.185 -0.1731 4.49 1.039 -0.1746 3.21 0.798 -0.1672 2.47 0.676 -0.1616 1.40 0.551 -0.1549 0.33 0.430 -0.1487 -0.64 0.374 -0.1551 -1.63 0.255 -0.1456 -2.64 0.144 -0.1362 -3.74 -0.111 -0.0863 -4.69 -0.342 -0.0154 -5.64 -0.359 0.0022 -6.63 -0.376 0.0160 -7.62 -0.366 0.0211 -8.80 -0.291 0.0116 Tabulated from data in file pg02384.dat & reduced using program C06.01 Average Reynolds #: 149958 Number of angles of attack: 59 alpha / Cl / Cm -8.99 -0.300 0.0203 -7.84 -0.357 0.0263 -7.00 -0.358 0.0244 -5.92 -0.357 0.0097 -4.95 -0.297 -0.0227 -3.92 -0.028 -0.1143 -2.90 0.172 -0.1454 -1.73 0.328 -0.1566 -0.72 0.471 -0.1673 0.32 0.594 -0.1696 1.31 0.744 -0.1756 2.23 0.866 -0.1791 3.41 1.003 -0.1773 4.32 1.092 -0.1732 5.35 1.191 -0.1682 6.37 1.278 -0.1622 7.60 1.374 -0.1533 8.42 1.426 -0.1463 9.47 1.467 -0.1342 10.50 1.483 -0.1214 11.48 1.517 -0.1121 12.51 1.535 -0.1033 13.39 1.548 -0.0964 14.44 1.555 -0.0915 15.40 1.551 -0.0923 16.39 1.535 -0.0977 17.13 1.147 -0.2201 18.63 1.131 -0.2267 19.35 1.142 -0.2230 20.31 1.186 -0.2259 18.98 1.177 -0.2296 18.14 1.149 -0.2331 17.15 1.128 -0.2242 16.17 1.145 -0.2210 15.24 1.167 -0.2143 14.50 1.559 -0.0949 13.69 1.554 -0.0975 12.71 1.546 -0.1041 11.68 1.522 -0.1124 10.55 1.491 -0.1224 9.58 1.467 -0.1334 8.40 1.423 -0.1467 7.55 1.373 -0.1533 6.44 1.291 -0.1611 5.22 1.182 -0.1677 4.39 1.104 -0.1716 3.43 1.008 -0.1755 2.26 0.872 -0.1784 1.25 0.738 -0.1739 0.18 0.577 -0.1687 -0.70 0.467 -0.1655 -1.78 0.329 -0.1550 -2.81 0.193 -0.1459 -3.86 -0.016 -0.1147 -4.71 -0.254 -0.0425 -5.66 -0.342 -0.0075 -6.63 -0.349 0.0120 -7.63 -0.342 0.0193 -8.66 -0.269 0.0115 Tabulated from data in file pg02501.dat & reduced using program C06.01 Average Reynolds #: 199819 Number of angles of attack: 59 alpha / Cl / Cm -8.74 -0.334 0.0100 -8.02 -0.333 0.0094 -7.00 -0.339 -0.0037 -5.95 -0.281 -0.0274 -4.92 -0.134 -0.0850 -4.00 0.131 -0.1566 -3.08 0.277 -0.1698 -1.76 0.464 -0.1809 -0.98 0.567 -0.1868 0.14 0.679 -0.1825 1.58 0.839 -0.1819 2.27 0.915 -0.1812 3.30 1.019 -0.1776 4.50 1.137 -0.1725 5.37 1.224 -0.1694 6.34 1.304 -0.1639 7.52 1.389 -0.1550 8.33 1.430 -0.1472 9.43 1.475 -0.1347 10.40 1.498 -0.1226 11.37 1.531 -0.1136 12.37 1.555 -0.1061 13.39 1.575 -0.0980 14.39 1.583 -0.1062 15.47 1.592 -0.0997 16.47 1.584 -0.0962 17.39 1.582 -0.0990 17.82 1.208 -0.2259 19.07 1.192 -0.2267 20.18 1.255 -0.2302 19.37 1.244 -0.2348 18.41 1.194 -0.2277 17.40 1.210 -0.2223 16.44 1.162 -0.2169 15.41 1.465 -0.1045 14.66 1.594 -0.1085 13.27 1.573 -0.1047 12.52 1.563 -0.1061 11.57 1.535 -0.1119 10.54 1.510 -0.1215 9.45 1.481 -0.1344 8.36 1.438 -0.1470 7.37 1.382 -0.1557 6.22 1.297 -0.1636 5.20 1.207 -0.1691 4.31 1.126 -0.1725 3.38 1.034 -0.1762 2.39 0.931 -0.1790 1.37 0.814 -0.1804 0.18 0.682 -0.1807 -0.64 0.613 -0.1857 -1.70 0.468 -0.1796 -2.78 0.318 -0.1721 -3.92 0.142 -0.1593 -4.69 -0.081 -0.1085 -5.70 -0.245 -0.0388 -6.63 -0.330 -0.0115 -7.65 -0.332 0.0039 -8.69 -0.309 0.0059 Tabulated from data in file pg02386.dat & reduced using program C06.01 Average Reynolds #: 299800 Number of angles of attack: 59 alpha / Cl / Cm -8.68 -0.291 -0.0013 -7.97 -0.292 -0.0158 -6.97 -0.217 -0.0408 -6.17 -0.134 -0.0765 -5.19 0.053 -0.1430 -4.13 0.270 -0.1860 -3.10 0.392 -0.1881 -2.06 0.511 -0.1900 -0.99 0.629 -0.1920 -0.01 0.727 -0.1892 1.06 0.834 -0.1846 2.07 0.941 -0.1835 3.10 1.042 -0.1811 4.25 1.159 -0.1784 5.07 1.232 -0.1745 6.23 1.328 -0.1671 7.25 1.399 -0.1586 8.33 1.456 -0.1478 9.39 1.504 -0.1368 10.33 1.530 -0.1264 11.45 1.570 -0.1160 12.51 1.596 -0.1073 13.60 1.621 -0.1013 14.61 1.642 -0.1002 15.74 1.653 -0.1019 16.66 1.646 -0.1044 17.47 1.649 -0.1071 18.56 1.625 -0.1168 19.32 1.603 -0.1195 19.91 1.288 -0.2544 19.60 1.215 -0.2419 18.60 1.203 -0.2361 17.57 1.173 -0.2237 16.50 1.225 -0.2217 16.24 1.654 -0.0957 14.64 1.643 -0.0944 13.61 1.619 -0.0976 12.52 1.600 -0.1024 11.32 1.569 -0.1121 10.32 1.534 -0.1225 9.69 1.512 -0.1288 8.57 1.471 -0.1416 7.64 1.426 -0.1513 6.54 1.352 -0.1605 5.53 1.270 -0.1671 4.57 1.183 -0.1723 3.57 1.085 -0.1758 2.52 0.979 -0.1784 1.48 0.873 -0.1798 0.47 0.767 -0.1825 -0.59 0.676 -0.1888 -1.69 0.554 -0.1889 -2.62 0.448 -0.1877 -3.66 0.330 -0.1860 -4.68 0.163 -0.1705 -5.66 -0.042 -0.1146 -6.69 -0.197 -0.0521 -7.67 -0.277 -0.0208 -8.84 -0.315 -0.0007 Tabulated from data in file pg02389.dat & reduced using program C06.01 Average Reynolds #: 399815 Number of angles of attack: 59 alpha / Cl / Cm -8.33 -0.297 -0.0141 -8.08 -0.275 -0.0216 -7.37 -0.210 -0.0464 -6.46 -0.100 -0.0918 -5.28 0.107 -0.1616 -4.14 0.301 -0.1875 -3.14 0.409 -0.1880 -2.07 0.528 -0.1887 -1.01 0.643 -0.1881 -0.07 0.740 -0.1877 0.94 0.836 -0.1814 1.99 0.947 -0.1803 3.08 1.057 -0.1773 4.09 1.153 -0.1729 5.16 1.248 -0.1671 6.16 1.332 -0.1606 7.28 1.408 -0.1508 8.23 1.461 -0.1413 9.39 1.512 -0.1295 10.40 1.550 -0.1192 11.41 1.582 -0.1115 12.51 1.613 -0.1043 13.37 1.633 -0.0995 14.63 1.663 -0.0955 15.51 1.665 -0.0959 16.34 1.677 -0.0986 17.31 1.658 -0.1036 18.34 1.627 -0.1082 19.29 1.615 -0.1165 20.31 1.587 -0.1266 19.57 1.611 -0.1279 18.54 1.638 -0.1153 17.44 1.655 -0.1064 16.40 1.682 -0.0998 15.36 1.672 -0.0935 14.36 1.651 -0.0931 13.13 1.633 -0.0988 12.38 1.613 -0.1029 11.56 1.593 -0.1086 10.50 1.549 -0.1170 9.54 1.515 -0.1265 8.45 1.469 -0.1382 7.51 1.419 -0.1476 6.55 1.361 -0.1564 5.61 1.291 -0.1636 4.51 1.195 -0.1705 3.40 1.089 -0.1751 2.25 0.976 -0.1785 1.44 0.891 -0.1805 0.46 0.790 -0.1838 -0.62 0.688 -0.1869 -1.69 0.565 -0.1862 -2.61 0.467 -0.1864 -3.60 0.356 -0.1854 -4.63 0.219 -0.1805 -5.66 0.028 -0.1348 -6.59 -0.114 -0.0835 -7.65 -0.229 -0.0365 -8.32 -0.298 -0.0117 Tabulated from data in file pg02392.dat & reduced using program C06.01 Average Reynolds #: 499253 Number of angles of attack: 53 alpha / Cl / Cm -6.39 -0.050 -0.1087 -5.22 0.145 -0.1710 -4.17 0.315 -0.1911 -3.16 0.429 -0.1920 -2.10 0.550 -0.1926 -1.08 0.659 -0.1930 -0.04 0.768 -0.1918 0.98 0.872 -0.1875 2.08 0.983 -0.1852 3.03 1.076 -0.1814 4.18 1.181 -0.1764 5.19 1.267 -0.1704 6.16 1.341 -0.1633 7.16 1.405 -0.1543 8.19 1.468 -0.1439 9.34 1.520 -0.1326 10.37 1.557 -0.1226 11.31 1.592 -0.1149 12.39 1.627 -0.1075 13.42 1.651 -0.1010 14.44 1.675 -0.0992 15.42 1.690 -0.1016 16.37 1.678 -0.1051 17.32 1.658 -0.1106 18.35 1.632 -0.1175 19.42 1.616 -0.1273 20.50 1.589 -0.1383 19.64 1.615 -0.1303 18.55 1.617 -0.1206 17.63 1.649 -0.1129 16.46 1.677 -0.1055 15.38 1.699 -0.0974 14.37 1.676 -0.0971 12.99 1.642 -0.1025 12.45 1.633 -0.1061 11.64 1.600 -0.1110 10.65 1.571 -0.1181 9.63 1.531 -0.1269 8.58 1.484 -0.1372 7.64 1.436 -0.1465 6.58 1.373 -0.1561 5.59 1.304 -0.1636 4.60 1.223 -0.1708 3.55 1.131 -0.1766 2.50 1.031 -0.1803 1.50 0.926 -0.1821 0.44 0.824 -0.1874 -0.59 0.725 -0.1904 -1.65 0.605 -0.1904 -2.61 0.500 -0.1903 -3.72 0.375 -0.1902 -4.68 0.252 -0.1877 -5.65 0.063 -0.1497 Tabulated from data in file pg02396.dat & reduced using program C06.01 File sg6043.lft created using program C06.01 on Mon Feb 02 15:11:35 1998