Airfoil: SH3055 Builder: Y. Tinel Comment: 'clean' Number of Reynolds #'s: 4 Average Reynolds #: 99991 Number of angles of attack: 61 alpha / Cl / Cm -10.15 -0.226 -0.0345 -9.08 -0.213 -0.0308 -8.08 -0.279 -0.0155 -7.05 -0.287 -0.0199 -6.11 -0.273 -0.0254 -5.06 -0.210 -0.0389 -4.05 -0.120 -0.0658 -3.09 0.003 -0.0976 -2.08 0.184 -0.1314 -1.05 0.344 -0.1484 -0.02 0.504 -0.1622 1.00 0.628 -0.1695 2.01 0.740 -0.1603 3.05 0.864 -0.1810 4.12 0.990 -0.1845 5.11 1.093 -0.1801 6.13 1.215 -0.1874 7.13 1.324 -0.1793 8.20 1.436 -0.1763 9.16 1.543 -0.1852 10.22 1.627 -0.1661 11.26 1.718 -0.1694 12.26 1.771 -0.1604 13.28 1.823 -0.1624 14.35 1.846 -0.1547 15.30 1.868 -0.1615 16.33 1.885 -0.1615 17.25 1.824 -0.1647 18.33 1.751 -0.1698 19.26 1.702 -0.1770 20.24 1.645 -0.1905 19.72 1.648 -0.1904 18.73 1.726 -0.1790 17.81 1.785 -0.1709 16.79 1.866 -0.1709 15.87 1.894 -0.1700 14.80 1.855 -0.1549 13.78 1.844 -0.1666 12.71 1.801 -0.1786 11.78 1.750 -0.1782 10.73 1.662 -0.1699 9.70 1.586 -0.1774 8.71 1.481 -0.1746 7.65 1.370 -0.1758 6.67 1.268 -0.1938 5.63 1.146 -0.1902 4.60 1.039 -0.1822 3.54 0.923 -0.1782 2.50 0.804 -0.1723 1.46 0.674 -0.1586 0.48 0.553 -0.1591 -0.53 0.452 -0.1556 -1.56 0.288 -0.1437 -2.59 0.071 -0.1064 -3.61 -0.080 -0.0799 -4.60 -0.178 -0.0516 -5.63 -0.244 -0.0301 -6.61 -0.247 -0.0259 -7.61 -0.278 -0.0149 -8.55 -0.237 -0.0196 -9.61 -0.238 -0.0272 Tabulated from data in file bm05056.dat & reduced using program C10.20 Average Reynolds #: 200055 Number of angles of attack: 61 alpha / Cl / Cm -10.10 -0.255 -0.0072 -9.01 -0.236 -0.0112 -8.02 -0.238 -0.0166 -7.10 -0.183 -0.0319 -6.16 -0.026 -0.1297 -5.16 0.220 -0.2281 -4.17 0.376 -0.2374 -3.11 0.498 -0.2388 -2.10 0.606 -0.2391 -1.07 0.705 -0.2352 -0.10 0.802 -0.2344 0.94 0.901 -0.2308 2.06 1.008 -0.2283 3.06 1.110 -0.2252 4.10 1.206 -0.2216 5.10 1.303 -0.2183 6.17 1.402 -0.2143 7.18 1.492 -0.2097 8.18 1.581 -0.2057 9.17 1.662 -0.2006 10.27 1.742 -0.1945 11.29 1.809 -0.1875 12.29 1.874 -0.1806 13.35 1.908 -0.1699 14.32 1.891 -0.1572 15.30 1.875 -0.1528 16.30 1.829 -0.1534 17.26 1.786 -0.1588 18.25 1.731 -0.1674 19.22 1.683 -0.1775 20.19 1.643 -0.1902 19.70 1.662 -0.1824 18.75 1.714 -0.1755 17.73 1.760 -0.1656 16.75 1.816 -0.1583 15.80 1.851 -0.1550 14.80 1.883 -0.1556 13.80 1.905 -0.1650 12.75 1.888 -0.1771 11.83 1.847 -0.1855 10.74 1.775 -0.1928 9.72 1.705 -0.1987 8.71 1.623 -0.2044 7.70 1.539 -0.2092 6.62 1.445 -0.2138 5.65 1.361 -0.2182 4.60 1.252 -0.2207 3.59 1.153 -0.2242 2.52 1.054 -0.2274 1.51 0.959 -0.2306 0.46 0.853 -0.2325 -0.60 0.756 -0.2376 -1.57 0.668 -0.2407 -2.60 0.559 -0.2410 -3.64 0.446 -0.2407 -4.65 0.311 -0.2341 -5.70 0.133 -0.2193 -6.71 -0.050 -0.1988 -7.72 -0.217 -0.1836 -8.78 -0.390 -0.1605 -9.79 -0.558 -0.1271 Tabulated from data in file bm05058.dat & reduced using program C10.20 Average Reynolds #: 349917 Number of angles of attack: 61 alpha / Cl / Cm -10.07 -0.277 -0.0091 -9.04 -0.244 -0.0213 -8.09 -0.180 -0.0514 -7.17 0.011 -0.2258 -6.17 0.166 -0.2402 -5.13 0.296 -0.2442 -4.13 0.409 -0.2469 -3.13 0.521 -0.2475 -2.09 0.631 -0.2476 -1.08 0.737 -0.2474 -0.07 0.843 -0.2455 1.01 0.960 -0.2446 2.02 1.057 -0.2421 3.07 1.165 -0.2393 4.09 1.269 -0.2369 5.08 1.366 -0.2327 6.14 1.466 -0.2280 7.17 1.559 -0.2230 8.22 1.645 -0.2161 9.26 1.731 -0.2099 10.26 1.783 -0.2013 11.24 1.838 -0.1907 12.30 1.868 -0.1777 13.28 1.871 -0.1664 14.29 1.842 -0.1625 15.31 1.798 -0.1651 16.31 1.753 -0.1667 17.27 1.720 -0.1689 18.26 1.706 -0.1722 19.23 1.676 -0.1770 20.17 1.649 -0.1930 19.70 1.659 -0.1863 18.78 1.694 -0.1767 17.74 1.713 -0.1698 16.77 1.757 -0.1664 15.75 1.784 -0.1637 14.82 1.822 -0.1596 13.87 1.858 -0.1628 12.76 1.874 -0.1729 11.78 1.866 -0.1847 10.71 1.826 -0.1972 9.73 1.767 -0.2056 8.70 1.695 -0.2140 7.68 1.612 -0.2205 6.62 1.520 -0.2265 5.59 1.417 -0.2303 4.56 1.322 -0.2355 3.58 1.223 -0.2385 2.55 1.117 -0.2412 1.56 1.011 -0.2431 0.44 0.900 -0.2451 -0.58 0.797 -0.2474 -1.61 0.683 -0.2470 -2.63 0.574 -0.2478 -3.66 0.466 -0.2481 -4.68 0.348 -0.2467 -5.69 0.229 -0.2422 -6.68 0.100 -0.2350 -7.75 -0.095 -0.2135 -8.77 -0.281 -0.1896 -9.76 -0.477 -0.1580 Tabulated from data in file bm05060.dat & reduced using program C10.20 Average Reynolds #: 500174 Number of angles of attack: 61 alpha / Cl / Cm -10.16 -0.267 -0.0211 -9.17 -0.226 -0.0472 -8.22 -0.099 -0.2220 -7.24 0.054 -0.2349 -6.20 0.188 -0.2412 -5.23 0.304 -0.2459 -4.11 0.436 -0.2472 -3.12 0.547 -0.2487 -2.12 0.654 -0.2480 -1.04 0.767 -0.2474 -0.02 0.877 -0.2473 0.97 0.976 -0.2448 2.06 1.092 -0.2440 3.05 1.190 -0.2404 4.09 1.283 -0.2354 5.16 1.395 -0.2327 6.17 1.492 -0.2275 7.17 1.584 -0.2217 8.29 1.680 -0.2151 9.30 1.764 -0.2077 10.27 1.822 -0.1969 11.30 1.859 -0.1840 12.27 1.862 -0.1702 13.27 1.846 -0.1608 14.30 1.830 -0.1601 15.33 1.784 -0.1594 16.32 1.731 -0.1614 17.27 1.712 -0.1683 18.26 1.668 -0.1760 19.23 1.635 -0.1851 20.16 1.600 -0.1972 19.69 1.602 -0.1916 18.70 1.653 -0.1811 17.70 1.701 -0.1732 16.73 1.727 -0.1659 15.75 1.771 -0.1626 14.73 1.811 -0.1591 13.81 1.840 -0.1603 12.77 1.852 -0.1641 11.74 1.859 -0.1755 10.71 1.838 -0.1894 9.69 1.786 -0.2010 8.70 1.720 -0.2109 7.67 1.643 -0.2196 6.62 1.549 -0.2260 5.65 1.459 -0.2310 4.58 1.350 -0.2357 3.54 1.240 -0.2383 2.56 1.143 -0.2405 1.48 1.027 -0.2428 0.52 0.929 -0.2465 -0.51 0.827 -0.2473 -1.57 0.712 -0.2481 -2.61 0.597 -0.2482 -3.61 0.492 -0.2488 -4.63 0.373 -0.2474 -5.69 0.244 -0.2430 -6.71 0.120 -0.2384 -7.80 -0.023 -0.2263 -8.75 -0.183 -0.2108 -9.76 -0.396 -0.1729 Tabulated from data in file bm05062.dat & reduced using program C10.20 File sh3055_c.lft created using program C10.20 on Thu May 22 17:01:22 2003