Airfoil: S823 Builder: M. Allen Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 102500 Number of angles of attack: 39 alpha / Cl / Cm -7.86 0.013 -0.1500 -6.20 -0.007 -0.1500 -4.63 -0.030 -0.1500 -3.21 0.032 -0.1500 -1.68 -0.047 -0.1500 -0.10 0.110 -0.1500 1.48 0.281 -0.1500 3.02 0.452 -0.1500 4.39 0.587 -0.1500 6.02 0.763 -0.1500 7.62 0.916 -0.1500 9.20 1.064 -0.1500 10.55 1.157 -0.1500 12.21 1.166 -0.1500 13.68 1.137 -0.1500 15.13 1.124 -0.1500 16.68 1.127 -0.1500 18.05 0.835 -0.1500 19.61 0.830 -0.1500 21.16 0.879 -0.1500 19.34 0.795 -0.1500 17.96 0.841 -0.1500 16.53 1.139 -0.1500 15.06 1.132 -0.1500 13.52 1.146 -0.1500 11.98 1.174 -0.1500 10.55 1.159 -0.1500 9.01 1.040 -0.1500 7.56 0.916 -0.1500 5.94 0.758 -0.1500 4.45 0.603 -0.1500 2.79 0.398 -0.1500 1.34 0.245 -0.1500 -0.19 0.099 -0.1500 -1.70 0.093 -0.1500 -3.24 0.043 -0.1500 -4.79 -0.055 -0.1500 -6.23 0.002 -0.1500 -7.76 0.010 -0.1500 Tabulated from data in file JG00453.DAT & reduced using program Q01.00L Average Reynolds #: 204800 Number of angles of attack: 39 alpha / Cl / Cm -7.50 0.012 -0.1500 -6.19 0.017 -0.1500 -4.59 0.049 -0.1500 -3.16 0.023 -0.1500 -1.64 0.066 -0.1500 0.24 0.268 -0.1500 1.61 0.418 -0.1500 3.00 0.569 -0.1500 4.63 0.740 -0.1500 6.08 0.882 -0.1500 7.62 1.020 -0.1500 9.27 1.147 -0.1500 10.62 1.184 -0.1500 12.24 1.167 -0.1500 13.64 1.159 -0.1500 15.14 1.155 -0.1500 16.81 1.152 -0.1500 18.12 1.151 -0.1500 19.52 0.825 -0.1500 21.02 0.886 -0.1500 19.33 0.837 -0.1500 18.07 1.162 -0.1500 16.53 1.168 -0.1500 14.84 1.153 -0.1500 13.35 1.159 -0.1500 11.94 1.171 -0.1500 10.40 1.184 -0.1500 8.94 1.120 -0.1500 7.34 0.987 -0.1500 5.71 0.838 -0.1500 4.35 0.701 -0.1500 2.65 0.521 -0.1500 0.92 0.330 -0.1500 -0.52 0.175 -0.1500 -2.25 -0.008 -0.1500 -3.54 -0.126 -0.1500 -5.16 -0.255 -0.1500 -4.21 0.072 -0.1500 -8.68 -0.025 -0.1500 Tabulated from data in file JG00456.DAT & reduced using program Q01.00L Average Reynolds #: 306700 Number of angles of attack: 39 alpha / Cl / Cm -7.83 -0.522 -0.1500 -6.40 -0.373 -0.1500 -4.89 -0.243 -0.1500 -3.31 -0.106 -0.1500 -1.82 0.048 -0.1500 -0.23 0.219 -0.1500 1.28 0.389 -0.1500 2.82 0.561 -0.1500 4.41 0.733 -0.1500 5.94 0.889 -0.1500 7.49 1.028 -0.1500 9.17 1.145 -0.1500 10.69 1.176 -0.1500 12.36 1.174 -0.1500 13.83 1.174 -0.1500 15.19 1.173 -0.1500 16.54 1.169 -0.1500 18.15 1.159 -0.1500 19.35 0.895 -0.1500 20.87 0.878 -0.1500 19.46 0.882 -0.1500 18.25 1.158 -0.1500 16.15 1.166 -0.1500 14.84 1.170 -0.1500 13.27 1.173 -0.1500 11.80 1.172 -0.1500 10.17 1.168 -0.1500 8.75 1.119 -0.1500 7.26 1.006 -0.1500 5.83 0.874 -0.1500 4.32 0.722 -0.1500 2.87 0.563 -0.1500 1.25 0.380 -0.1500 -0.18 0.220 -0.1500 -1.74 0.054 -0.1500 -3.28 -0.109 -0.1500 -4.89 -0.259 -0.1500 -6.36 -0.385 -0.1500 -7.96 -0.544 -0.1500 Tabulated from data in file AB00460.DAT & reduced using program Q01.00L Average Reynolds #: 409200 Number of angles of attack: 31 alpha / Cl / Cm -7.84 -0.531 -0.1500 -6.39 -0.390 -0.1500 -4.79 -0.250 -0.1500 -3.29 -0.111 -0.1500 -1.73 0.055 -0.1500 -0.23 0.221 -0.1500 1.36 0.400 -0.1500 2.86 0.569 -0.1500 4.46 0.744 -0.1500 6.00 0.897 -0.1500 7.53 1.032 -0.1500 9.04 1.124 -0.1500 10.61 1.156 -0.1500 12.02 1.160 -0.1500 13.54 1.166 -0.1500 15.04 1.163 -0.1500 13.24 1.165 -0.1500 11.59 1.153 -0.1500 10.00 1.144 -0.1500 8.84 1.113 -0.1500 7.35 1.015 -0.1500 5.81 0.875 -0.1500 4.37 0.730 -0.1500 2.82 0.559 -0.1500 1.27 0.383 -0.1500 -0.23 0.213 -0.1500 -1.82 0.037 -0.1500 -3.33 -0.128 -0.1500 -4.88 -0.269 -0.1500 -6.38 -0.406 -0.1500 -7.95 -0.553 -0.1500 Tabulated from data in file JG00463.DAT & reduced using program Q01.00L File s823.lft created on 12-05-1997 at 15:25:50 using program FORMAT