Airfoil: S823 Builder: M. Allen Comment: Zig-Zag trip type "C" @ x/c = 2% u.s. & 5% l.s. (h/c = 0.19%) Number of Reynolds #'s: 4 Average Reynolds #: 101300 Number of angles of attack: 49 alpha / Cl / Cm -5.95 -0.129 -0.1500 -4.58 -0.186 -0.1500 -3.52 -0.117 -0.1500 -2.42 0.027 -0.1500 -1.59 -0.034 -0.1500 -0.34 0.087 -0.1500 0.49 0.207 -0.1500 1.58 0.356 -0.1500 2.67 0.486 -0.1500 3.78 0.603 -0.1500 4.68 0.686 -0.1500 5.78 0.763 -0.1500 6.67 0.808 -0.1500 7.75 0.865 -0.1500 8.78 0.918 -0.1500 9.81 0.960 -0.1500 10.80 0.988 -0.1500 11.76 1.012 -0.1500 12.73 1.043 -0.1500 13.69 1.075 -0.1500 14.89 1.115 -0.1500 15.88 1.137 -0.1500 16.87 1.152 -0.1500 17.69 0.826 -0.1500 18.78 0.846 -0.1500 17.17 0.807 -0.1500 16.34 0.838 -0.1500 15.20 1.143 -0.1500 14.26 1.116 -0.1500 13.40 1.084 -0.1500 12.30 1.045 -0.1500 11.19 1.014 -0.1500 10.35 0.992 -0.1500 9.22 0.948 -0.1500 8.32 0.910 -0.1500 7.10 0.847 -0.1500 6.17 0.797 -0.1500 5.20 0.735 -0.1500 4.22 0.657 -0.1500 3.22 0.556 -0.1500 2.24 0.445 -0.1500 1.03 0.286 -0.1500 0.09 0.162 -0.1500 -0.90 0.028 -0.1500 -2.12 -0.105 -0.1500 -3.03 -0.195 -0.1500 -3.97 -0.264 -0.1500 -5.11 -0.408 -0.1500 -6.05 -0.494 -0.1500 Tabulated from data in file CL00729.DAT & reduced using program Q02.00L Average Reynolds #: 202600 Number of angles of attack: 49 alpha / Cl / Cm -5.91 -0.253 -0.1500 -4.43 -0.138 -0.1500 -3.44 -0.078 -0.1500 -2.44 0.000 -0.1500 -1.38 0.098 -0.1500 -0.32 0.202 -0.1500 0.72 0.301 -0.1500 1.71 0.387 -0.1500 2.63 0.462 -0.1500 3.64 0.547 -0.1500 4.83 0.648 -0.1500 5.78 0.721 -0.1500 6.83 0.796 -0.1500 7.87 0.862 -0.1500 8.91 0.921 -0.1500 9.92 0.957 -0.1500 10.67 0.985 -0.1500 11.89 1.026 -0.1500 12.74 1.046 -0.1500 13.85 1.076 -0.1500 14.82 1.094 -0.1500 15.84 1.121 -0.1500 16.86 1.145 -0.1500 17.85 1.142 -0.1500 18.52 0.793 -0.1500 17.35 1.156 -0.1500 16.33 1.142 -0.1500 15.29 1.110 -0.1500 14.17 1.087 -0.1500 13.34 1.059 -0.1500 12.36 1.036 -0.1500 11.30 1.003 -0.1500 10.23 0.966 -0.1500 9.15 0.924 -0.1500 8.30 0.882 -0.1500 7.08 0.806 -0.1500 6.15 0.743 -0.1500 5.20 0.671 -0.1500 4.23 0.592 -0.1500 2.99 0.487 -0.1500 2.07 0.408 -0.1500 1.11 0.332 -0.1500 -0.15 0.211 -0.1500 -1.06 0.120 -0.1500 -1.88 0.040 -0.1500 -3.09 -0.064 -0.1500 -4.01 -0.126 -0.1500 -4.98 -0.181 -0.1500 -6.16 -0.292 -0.1500 Tabulated from data in file PG00833.DAT & reduced using program Q02.00L Average Reynolds #: 303800 Number of angles of attack: 49 alpha / Cl / Cm -6.03 -0.265 -0.1500 -4.50 -0.171 -0.1500 -3.65 -0.114 -0.1500 -2.62 -0.037 -0.1500 -1.50 0.064 -0.1500 -0.41 0.174 -0.1500 0.60 0.266 -0.1500 1.50 0.346 -0.1500 2.64 0.450 -0.1500 3.53 0.533 -0.1500 4.72 0.637 -0.1500 5.69 0.714 -0.1500 6.68 0.784 -0.1500 7.70 0.847 -0.1500 8.73 0.899 -0.1500 9.93 0.948 -0.1500 10.72 0.980 -0.1500 11.73 1.016 -0.1500 12.72 1.046 -0.1500 13.73 1.073 -0.1500 14.73 1.115 -0.1500 15.69 1.131 -0.1500 16.92 1.141 -0.1500 17.69 1.140 -0.1500 18.83 1.137 -0.1500 17.17 1.130 -0.1500 16.27 1.134 -0.1500 15.22 1.122 -0.1500 14.26 1.099 -0.1500 13.12 1.066 -0.1500 12.17 1.033 -0.1500 11.23 0.998 -0.1500 10.26 0.964 -0.1500 9.26 0.923 -0.1500 8.17 0.868 -0.1500 7.04 0.803 -0.1500 6.21 0.746 -0.1500 5.09 0.661 -0.1500 4.15 0.582 -0.1500 3.09 0.487 -0.1500 1.94 0.378 -0.1500 1.07 0.305 -0.1500 -0.19 0.193 -0.1500 -1.15 0.098 -0.1500 -2.09 0.008 -0.1500 -3.04 -0.070 -0.1500 -4.17 -0.152 -0.1500 -5.02 -0.196 -0.1500 -6.15 -0.278 -0.1500 Tabulated from data in file PG00835.DAT & reduced using program Q02.00L Average Reynolds #: 404600 Number of angles of attack: 37 alpha / Cl / Cm -2.85 -0.065 -0.1500 -1.75 0.036 -0.1500 -0.76 0.128 -0.1500 0.26 0.222 -0.1500 1.28 0.333 -0.1500 2.38 0.445 -0.1500 3.44 0.550 -0.1500 4.46 0.639 -0.1500 5.54 0.716 -0.1500 6.62 0.792 -0.1500 7.53 0.846 -0.1500 8.59 0.899 -0.1500 9.64 0.947 -0.1500 10.69 0.981 -0.1500 11.65 1.015 -0.1500 12.65 1.048 -0.1500 13.63 1.062 -0.1500 14.60 1.079 -0.1500 15.69 1.085 -0.1500 14.13 1.071 -0.1500 13.15 1.049 -0.1500 12.22 1.032 -0.1500 11.30 1.004 -0.1500 10.10 0.965 -0.1500 9.28 0.935 -0.1500 8.25 0.887 -0.1500 7.19 0.828 -0.1500 6.28 0.773 -0.1500 5.18 0.698 -0.1500 4.17 0.618 -0.1500 3.23 0.528 -0.1500 2.25 0.438 -0.1500 1.10 0.316 -0.1500 0.16 0.214 -0.1500 -0.84 0.118 -0.1500 -1.93 0.018 -0.1500 -2.88 -0.073 -0.1500 Tabulated from data in file PG00734.DAT & reduced using program Q02.00L File s823t.lft created on 09-12-1997 at 13:46:18 using program FORMAT