Airfoil: S822 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 #: 101200 Number of angles of attack: 49 alpha / Cl / Cm -6.33 -0.583 -0.0700 -4.81 -0.382 -0.0700 -3.96 -0.322 -0.0700 -2.76 -0.195 -0.0700 -1.89 -0.128 -0.0700 -0.83 -0.040 -0.0700 0.21 0.032 -0.0700 1.26 0.090 -0.0700 2.31 0.194 -0.0700 3.24 0.555 -0.0700 4.28 0.599 -0.0700 5.33 0.610 -0.0700 6.42 0.698 -0.0700 7.30 0.761 -0.0700 8.34 0.828 -0.0700 9.39 0.888 -0.0700 10.39 0.943 -0.0700 11.39 0.991 -0.0700 12.37 1.043 -0.0700 13.37 1.096 -0.0700 14.35 1.129 -0.0700 15.47 0.822 -0.0700 16.38 0.749 -0.0700 17.46 0.766 -0.0700 18.41 0.805 -0.0700 16.94 0.751 -0.0700 16.05 0.852 -0.0700 14.97 0.819 -0.0700 14.08 0.931 -0.0700 12.95 1.074 -0.0700 12.13 1.026 -0.0700 11.01 0.968 -0.0700 10.02 0.917 -0.0700 9.02 0.859 -0.0700 8.02 0.801 -0.0700 7.00 0.730 -0.0700 5.92 0.649 -0.0700 4.89 0.587 -0.0700 3.88 0.583 -0.0700 2.87 0.479 -0.0700 1.77 0.123 -0.0700 0.84 0.052 -0.0700 -0.24 -0.001 -0.0700 -1.20 -0.075 -0.0700 -2.31 -0.155 -0.0700 -3.27 -0.228 -0.0700 -4.27 -0.343 -0.0700 -5.37 -0.451 -0.0700 -6.42 -0.565 -0.0700 Tabulated from data in file PG00826.DAT & reduced using program Q02.00L Average Reynolds #: 201900 Number of angles of attack: 49 alpha / Cl / Cm -6.43 -0.360 -0.0700 -4.73 -0.206 -0.0700 -3.67 -0.115 -0.0700 -2.91 -0.046 -0.0700 -1.61 0.113 -0.0700 -0.67 0.213 -0.0700 0.38 0.297 -0.0700 1.35 0.369 -0.0700 2.30 0.447 -0.0700 3.28 0.526 -0.0700 4.52 0.607 -0.0700 5.23 0.639 -0.0700 6.37 0.702 -0.0700 7.28 0.775 -0.0700 8.40 0.848 -0.0700 9.52 0.912 -0.0700 10.38 0.956 -0.0700 11.43 1.006 -0.0700 12.48 1.051 -0.0700 13.56 1.090 -0.0700 14.52 1.123 -0.0700 15.48 1.143 -0.0700 16.48 1.166 -0.0700 17.13 0.777 -0.0700 18.47 0.830 -0.0700 16.91 0.908 -0.0700 15.96 0.869 -0.0700 14.90 0.909 -0.0700 14.10 1.107 -0.0700 13.01 1.070 -0.0700 12.11 1.030 -0.0700 11.06 0.983 -0.0700 9.99 0.932 -0.0700 8.88 0.870 -0.0700 7.99 0.816 -0.0700 6.85 0.736 -0.0700 5.92 0.665 -0.0700 4.94 0.627 -0.0700 3.93 0.572 -0.0700 2.90 0.493 -0.0700 1.87 0.407 -0.0700 0.82 0.329 -0.0700 -0.28 0.246 -0.0700 -1.39 0.136 -0.0700 -2.28 0.011 -0.0700 -3.47 -0.100 -0.0700 -4.30 -0.168 -0.0700 -5.49 -0.275 -0.0700 -6.43 -0.361 -0.0700 Tabulated from data in file PG00828.DAT & reduced using program Q02.00L Average Reynolds #: 302900 Number of angles of attack: 49 alpha / Cl / Cm -6.33 -0.306 -0.0700 -4.91 -0.183 -0.0700 -3.73 -0.079 -0.0700 -2.73 0.001 -0.0700 -1.76 0.082 -0.0700 -0.81 0.169 -0.0700 0.25 0.256 -0.0700 1.35 0.351 -0.0700 2.43 0.451 -0.0700 3.45 0.540 -0.0700 4.43 0.621 -0.0700 5.44 0.696 -0.0700 6.42 0.754 -0.0700 7.36 0.789 -0.0700 8.45 0.847 -0.0700 9.34 0.899 -0.0700 10.32 0.949 -0.0700 11.40 1.001 -0.0700 12.54 1.051 -0.0700 13.53 1.092 -0.0700 14.35 1.120 -0.0700 15.51 1.163 -0.0700 16.41 1.176 -0.0700 17.40 1.173 -0.0700 18.02 0.805 -0.0700 16.84 0.864 -0.0700 15.89 0.904 -0.0700 15.23 1.150 -0.0700 13.99 1.109 -0.0700 13.01 1.073 -0.0700 11.98 1.029 -0.0700 10.99 0.983 -0.0700 9.93 0.931 -0.0700 8.84 0.870 -0.0700 7.97 0.817 -0.0700 7.01 0.776 -0.0700 5.90 0.726 -0.0700 4.77 0.646 -0.0700 3.84 0.572 -0.0700 2.87 0.488 -0.0700 1.64 0.375 -0.0700 0.68 0.291 -0.0700 -0.41 0.201 -0.0700 -1.48 0.105 -0.0700 -2.54 0.015 -0.0700 -3.32 -0.044 -0.0700 -4.31 -0.130 -0.0700 -5.58 -0.241 -0.0700 -6.45 -0.315 -0.0700 Tabulated from data in file PG00830.DAT & reduced using program Q02.00L Average Reynolds #: 403900 Number of angles of attack: 33 alpha / Cl / Cm -2.29 0.025 -0.0700 -0.80 0.159 -0.0700 0.27 0.254 -0.0700 1.14 0.335 -0.0700 2.32 0.442 -0.0700 3.32 0.527 -0.0700 4.52 0.625 -0.0700 5.37 0.689 -0.0700 6.41 0.759 -0.0700 7.56 0.827 -0.0700 8.38 0.869 -0.0700 9.55 0.916 -0.0700 10.45 0.962 -0.0700 11.50 1.016 -0.0700 12.42 1.058 -0.0700 13.40 1.102 -0.0700 14.41 1.138 -0.0700 13.05 1.085 -0.0700 11.91 1.034 -0.0700 10.96 0.988 -0.0700 9.94 0.934 -0.0700 8.81 0.883 -0.0700 7.78 0.837 -0.0700 6.82 0.782 -0.0700 5.60 0.702 -0.0700 4.87 0.650 -0.0700 3.72 0.558 -0.0700 2.55 0.456 -0.0700 1.73 0.383 -0.0700 0.66 0.282 -0.0700 -0.40 0.188 -0.0700 -1.31 0.109 -0.0700 -2.56 -0.003 -0.0700 Tabulated from data in file PG00853.DAT & reduced using program Q02.00L File s822t1.lft created on 09-12-1997 at 13:46:18 using program FORMAT