Airfoil: SH3055 Builder: Y. Tinel Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' Number of Reynolds #'s: 4 Average Reynolds #: 99926 Number of angles of attack: 61 alpha / Cl / Cm -10.09 -0.204 0.0033 -9.00 -0.198 0.0032 -7.95 -0.207 0.0033 -6.98 -0.224 0.0036 -5.95 -0.172 0.0027 -4.91 -0.081 0.0013 -3.99 0.116 -0.0019 -2.98 0.259 -0.0042 -2.03 0.403 -0.0065 -0.90 0.571 -0.0092 0.17 0.705 -0.0114 1.25 0.752 -0.0121 2.22 0.826 -0.0133 3.20 0.940 -0.0152 4.26 1.057 -0.0170 5.21 1.161 -0.0187 6.32 1.276 -0.0205 7.40 1.386 -0.0223 8.50 1.484 -0.0239 9.50 1.562 -0.0251 10.50 1.634 -0.0263 11.37 1.686 -0.0271 12.51 1.733 -0.0279 13.35 1.736 -0.0279 14.44 1.692 -0.0272 15.32 1.648 -0.0265 16.51 1.622 -0.0261 17.40 1.645 -0.0265 18.29 1.654 -0.0266 19.54 1.678 -0.0270 20.40 1.677 -0.0270 19.83 1.676 -0.0270 18.94 1.667 -0.0268 17.92 1.650 -0.0265 16.85 1.638 -0.0264 16.00 1.649 -0.0265 14.90 1.663 -0.0268 13.83 1.713 -0.0276 12.94 1.739 -0.0280 11.81 1.714 -0.0276 10.83 1.650 -0.0265 9.85 1.587 -0.0255 8.82 1.504 -0.0242 7.71 1.410 -0.0227 6.86 1.333 -0.0215 5.81 1.223 -0.0197 4.69 1.105 -0.0178 3.83 1.010 -0.0163 2.76 0.886 -0.0143 1.61 0.770 -0.0124 0.69 0.723 -0.0117 -0.42 0.641 -0.0103 -1.38 0.523 -0.0084 -2.38 0.357 -0.0058 -3.39 0.204 -0.0033 -4.44 0.082 -0.0014 -5.57 -0.069 0.0011 -6.46 -0.190 0.0030 -7.66 -0.345 0.0055 -8.59 -0.209 0.0033 -9.57 -0.189 0.0030 Tabulated from data in file bm05117.dat & reduced using program C10.20 Average Reynolds #: 200101 Number of angles of attack: 61 alpha / Cl / Cm -10.06 -0.266 -0.0074 -9.09 -0.286 -0.0131 -8.13 -0.297 -0.0656 -7.21 -0.237 -0.1513 -6.21 -0.027 -0.1858 -5.12 0.173 -0.2108 -4.14 0.341 -0.2274 -3.11 0.471 -0.2360 -2.09 0.588 -0.2383 -1.07 0.696 -0.2378 -0.06 0.802 -0.2356 0.96 0.904 -0.2316 2.06 0.992 -0.2264 3.02 1.064 -0.2185 4.06 1.144 -0.2110 5.13 1.229 -0.2052 6.12 1.298 -0.1973 7.16 1.361 -0.1899 8.20 1.422 -0.1823 9.18 1.471 -0.1753 10.24 1.504 -0.1677 11.22 1.527 -0.1659 12.17 1.539 -0.1638 13.22 1.537 -0.1645 14.19 1.519 -0.1671 15.23 1.527 -0.1703 16.22 1.524 -0.1732 17.21 1.520 -0.1771 18.18 1.543 -0.1827 19.21 1.561 -0.1871 20.17 1.600 -0.1957 19.67 1.587 -0.1920 18.71 1.532 -0.1852 17.69 1.539 -0.1828 16.67 1.528 -0.1772 15.72 1.531 -0.1744 14.69 1.534 -0.1685 13.70 1.539 -0.1668 12.70 1.530 -0.1650 11.71 1.533 -0.1653 10.75 1.518 -0.1671 9.68 1.487 -0.1725 8.68 1.446 -0.1802 7.70 1.390 -0.1878 6.62 1.335 -0.1964 5.63 1.262 -0.2020 4.61 1.188 -0.2103 3.58 1.105 -0.2153 2.51 1.026 -0.2235 1.53 0.949 -0.2311 0.46 0.850 -0.2345 -0.52 0.746 -0.2356 -1.58 0.642 -0.2361 -2.62 0.532 -0.2389 -3.61 0.405 -0.2328 -4.62 0.254 -0.2225 -5.68 0.061 -0.1991 -6.73 -0.140 -0.1685 -7.70 -0.333 -0.1338 -8.72 -0.495 -0.1068 -9.76 -0.604 -0.0995 Tabulated from data in file bm05066.dat & reduced using program C10.20 Average Reynolds #: 349945 Number of angles of attack: 61 alpha / Cl / Cm -10.08 -0.268 -0.0218 -9.27 -0.344 -0.0716 -8.21 -0.238 -0.1171 -7.14 -0.087 -0.1804 -6.20 0.098 -0.2101 -5.23 0.240 -0.2226 -4.16 0.374 -0.2307 -3.08 0.494 -0.2342 -2.11 0.597 -0.2341 -1.06 0.694 -0.2310 -0.07 0.787 -0.2281 1.03 0.894 -0.2276 2.01 0.990 -0.2249 2.98 1.077 -0.2220 4.06 1.167 -0.2171 5.11 1.263 -0.2129 6.14 1.334 -0.2051 7.14 1.400 -0.1972 8.17 1.460 -0.1881 9.26 1.509 -0.1796 10.24 1.533 -0.1735 11.21 1.556 -0.1724 12.19 1.561 -0.1724 13.23 1.565 -0.1713 14.23 1.562 -0.1728 15.22 1.570 -0.1741 16.15 1.547 -0.1770 17.19 1.558 -0.1831 18.23 1.563 -0.1876 19.20 1.568 -0.1922 20.14 1.566 -0.2021 19.67 1.578 -0.1986 18.68 1.563 -0.1915 17.69 1.568 -0.1859 16.72 1.558 -0.1825 15.72 1.561 -0.1792 14.66 1.571 -0.1768 13.69 1.566 -0.1734 12.68 1.562 -0.1730 11.69 1.553 -0.1717 10.70 1.549 -0.1732 9.69 1.521 -0.1767 8.67 1.486 -0.1851 7.64 1.432 -0.1935 6.62 1.372 -0.2027 5.65 1.304 -0.2094 4.56 1.222 -0.2168 3.55 1.133 -0.2211 2.54 1.044 -0.2254 1.53 0.953 -0.2282 0.43 0.843 -0.2304 -0.51 0.749 -0.2320 -1.58 0.650 -0.2338 -2.58 0.552 -0.2366 -3.63 0.435 -0.2339 -4.66 0.321 -0.2304 -5.68 0.175 -0.2191 -6.64 0.014 -0.1976 -7.68 -0.183 -0.1636 -8.70 -0.362 -0.1291 -9.74 -0.490 -0.1050 Tabulated from data in file bm05068.dat & reduced using program C10.20 Average Reynolds #: 500080 Number of angles of attack: 61 alpha / Cl / Cm -10.23 -0.276 -0.0358 -9.11 -0.312 -0.1029 -8.21 -0.217 -0.1604 -7.23 -0.045 -0.1902 -6.20 0.108 -0.2105 -5.13 0.255 -0.2248 -4.11 0.369 -0.2296 -3.06 0.486 -0.2301 -2.08 0.598 -0.2316 -1.06 0.695 -0.2303 0.02 0.796 -0.2284 1.00 0.889 -0.2256 2.00 0.983 -0.2225 3.05 1.079 -0.2186 4.10 1.172 -0.2141 5.14 1.253 -0.2081 6.07 1.333 -0.2037 7.15 1.404 -0.1948 8.15 1.449 -0.1853 9.19 1.495 -0.1776 10.24 1.520 -0.1741 11.20 1.529 -0.1736 12.23 1.539 -0.1755 13.20 1.534 -0.1746 14.20 1.527 -0.1765 15.20 1.516 -0.1793 16.21 1.530 -0.1817 17.26 1.528 -0.1850 18.19 1.531 -0.1888 19.15 1.531 -0.2033 20.17 1.491 -0.2118 19.67 1.513 -0.2083 18.60 1.528 -0.1974 17.71 1.539 -0.1877 16.70 1.548 -0.1859 15.73 1.531 -0.1823 14.65 1.524 -0.1786 13.69 1.538 -0.1764 12.65 1.538 -0.1758 11.65 1.530 -0.1744 10.70 1.522 -0.1737 9.67 1.509 -0.1748 8.70 1.473 -0.1801 7.64 1.431 -0.1895 6.66 1.372 -0.1977 5.56 1.295 -0.2053 4.56 1.217 -0.2117 3.58 1.127 -0.2159 2.51 1.022 -0.2187 1.48 0.937 -0.2237 0.44 0.843 -0.2274 -0.54 0.748 -0.2298 -1.58 0.644 -0.2294 -2.66 0.532 -0.2303 -3.67 0.425 -0.2295 -4.67 0.306 -0.2268 -5.72 0.182 -0.2187 -6.67 0.037 -0.2021 -7.69 -0.123 -0.1764 -8.70 -0.297 -0.1410 -9.70 -0.450 -0.1055 Tabulated from data in file bm05070.dat & reduced using program C10.20 File sh3055_tf.lft created using program C10.20 on Thu May 22 17:01:23 2003