Airfoil: BE50 Builder: R. Cooney Comment: clean Number of Reynolds #'s: 6 Average Reynolds #: 30600 Number of angles of attack: 49 alpha / Cl / Cm -5.03 -0.294 -0.1140 -3.92 -0.184 -0.1140 -2.96 -0.096 -0.1140 -1.81 -0.005 -0.1140 -0.86 0.087 -0.1140 0.27 0.190 -0.1140 1.20 0.282 -0.1140 2.35 0.418 -0.1140 3.30 0.588 -0.1140 4.43 0.730 -0.1140 5.38 0.801 -0.1140 6.31 0.853 -0.1140 7.47 0.909 -0.1140 8.44 0.947 -0.1140 9.37 0.936 -0.1140 10.26 0.924 -0.1140 11.36 0.955 -0.1140 12.46 0.903 -0.1140 13.37 0.963 -0.1140 14.47 0.911 -0.1140 15.38 0.901 -0.1140 16.29 0.924 -0.1140 17.45 1.016 -0.1140 18.41 1.046 -0.1140 19.36 1.100 -0.1140 18.01 0.976 -0.1140 17.10 0.986 -0.1140 16.09 0.899 -0.1140 14.92 0.887 -0.1140 14.04 0.848 -0.1140 12.90 0.861 -0.1140 11.97 0.874 -0.1140 10.82 0.877 -0.1140 9.95 0.915 -0.1140 9.05 0.855 -0.1140 7.96 0.914 -0.1140 7.12 0.855 -0.1140 6.02 0.832 -0.1140 4.95 0.775 -0.1140 3.91 0.664 -0.1140 2.94 0.528 -0.1140 1.87 0.381 -0.1140 0.75 0.257 -0.1140 -0.12 0.176 -0.1140 -1.23 0.074 -0.1140 -2.36 -0.030 -0.1140 -3.22 -0.106 -0.1140 -4.28 -0.209 -0.1140 -5.20 -0.301 -0.1140 Tabulated from data in file JG00567.DAT & reduced using program Q01.00L Average Reynolds #: 40100 Number of angles of attack: 49 alpha / Cl / Cm -5.02 -0.278 -0.1140 -3.78 -0.144 -0.1140 -2.79 -0.055 -0.1140 -1.78 0.034 -0.1140 -0.83 0.125 -0.1140 0.28 0.231 -0.1140 1.22 0.312 -0.1140 2.36 0.522 -0.1140 3.30 0.663 -0.1140 4.44 0.752 -0.1140 5.38 0.815 -0.1140 6.32 0.895 -0.1140 7.46 0.984 -0.1140 8.42 1.032 -0.1140 9.33 1.059 -0.1140 10.46 1.048 -0.1140 11.33 1.008 -0.1140 12.44 0.978 -0.1140 13.27 0.943 -0.1140 14.37 0.978 -0.1140 15.45 0.977 -0.1140 16.34 0.996 -0.1140 17.45 0.967 -0.1140 18.37 0.978 -0.1140 19.56 1.009 -0.1140 18.03 1.008 -0.1140 17.14 0.999 -0.1140 15.97 0.973 -0.1140 15.11 0.940 -0.1140 13.94 0.909 -0.1140 12.88 0.957 -0.1140 12.10 0.984 -0.1140 10.96 1.032 -0.1140 10.17 1.147 -0.1140 9.00 1.078 -0.1140 8.01 1.003 -0.1140 6.99 0.929 -0.1140 6.01 0.863 -0.1140 5.04 0.793 -0.1140 4.03 0.713 -0.1140 3.03 0.617 -0.1140 2.03 0.470 -0.1140 0.98 0.291 -0.1140 -0.26 0.184 -0.1140 -1.22 0.091 -0.1140 -2.17 0.014 -0.1140 -3.18 -0.069 -0.1140 -4.20 -0.168 -0.1140 -5.28 -0.272 -0.1140 Tabulated from data in file JG00568.DAT & reduced using program Q01.00L Average Reynolds #: 62200 Number of angles of attack: 33 alpha / Cl / Cm -4.98 -0.243 -0.1140 -3.40 -0.084 -0.1140 -1.73 0.057 -0.1140 -0.21 0.193 -0.1140 1.40 0.445 -0.1140 2.94 0.600 -0.1140 4.47 0.738 -0.1140 5.74 0.848 -0.1140 7.42 0.982 -0.1140 8.97 1.090 -0.1140 10.57 1.195 -0.1140 12.02 1.223 -0.1140 13.46 1.112 -0.1140 14.82 1.125 -0.1140 16.40 1.119 -0.1140 17.95 1.047 -0.1140 19.54 1.023 -0.1140 17.50 1.078 -0.1140 15.94 1.083 -0.1140 14.55 1.142 -0.1140 12.96 1.118 -0.1140 11.64 1.186 -0.1140 9.94 1.155 -0.1140 8.53 1.045 -0.1140 7.06 0.934 -0.1140 5.54 0.808 -0.1140 3.96 0.675 -0.1140 2.49 0.546 -0.1140 0.82 0.332 -0.1140 -0.73 0.103 -0.1140 -2.34 -0.040 -0.1140 -3.71 -0.143 -0.1140 -5.24 -0.310 -0.1140 Tabulated from data in file JG00569.DAT & reduced using program Q01.00L Average Reynolds #: 101700 Number of angles of attack: 33 alpha / Cl / Cm -5.06 -0.303 -0.1140 -3.44 -0.117 -0.1140 -1.72 0.026 -0.1140 -0.34 0.230 -0.1140 1.38 0.453 -0.1140 2.97 0.600 -0.1140 4.27 0.715 -0.1140 6.03 0.870 -0.1140 7.28 0.973 -0.1140 9.10 1.118 -0.1140 10.42 1.183 -0.1140 12.06 1.202 -0.1140 13.50 1.187 -0.1140 14.77 1.080 -0.1140 16.34 1.042 -0.1140 17.87 1.015 -0.1140 19.51 0.990 -0.1140 17.33 1.012 -0.1140 16.00 1.047 -0.1140 14.55 1.112 -0.1140 13.10 1.181 -0.1140 11.57 1.188 -0.1140 10.02 1.161 -0.1140 8.61 1.063 -0.1140 6.97 0.929 -0.1140 5.40 0.797 -0.1140 4.00 0.673 -0.1140 2.50 0.539 -0.1140 0.81 0.371 -0.1140 -0.69 0.166 -0.1140 -2.19 -0.016 -0.1140 -3.71 -0.141 -0.1140 -5.29 -0.329 -0.1140 Tabulated from data in file JG00571.DAT & reduced using program Q01.00L Average Reynolds #: 202800 Number of angles of attack: 33 alpha / Cl / Cm -5.37 -0.351 -0.1140 -3.31 -0.097 -0.1140 -1.77 0.105 -0.1140 -0.32 0.265 -0.1140 1.27 0.431 -0.1140 2.73 0.579 -0.1140 4.41 0.742 -0.1140 5.77 0.870 -0.1140 7.55 1.023 -0.1140 8.79 1.117 -0.1140 10.35 1.197 -0.1140 11.90 1.217 -0.1140 13.40 1.186 -0.1140 14.80 1.196 -0.1140 16.23 1.083 -0.1140 17.81 1.030 -0.1140 19.21 0.989 -0.1140 17.17 1.049 -0.1140 15.85 1.105 -0.1140 14.52 1.154 -0.1140 13.13 1.192 -0.1140 11.65 1.216 -0.1140 9.92 1.175 -0.1140 8.57 1.096 -0.1140 6.95 0.960 -0.1140 5.34 0.816 -0.1140 4.02 0.690 -0.1140 2.19 0.508 -0.1140 0.59 0.347 -0.1140 -0.97 0.182 -0.1140 -2.39 0.013 -0.1140 -3.83 -0.156 -0.1140 -5.27 -0.348 -0.1140 Tabulated from data in file JG00573.DAT & reduced using program Q01.00L Average Reynolds #: 303900 Number of angles of attack: 33 alpha / Cl / Cm -5.04 -0.301 -0.1140 -3.50 -0.087 -0.1140 -2.11 0.082 -0.1140 -0.35 0.260 -0.1140 1.20 0.421 -0.1140 2.95 0.597 -0.1140 4.42 0.739 -0.1140 6.17 0.907 -0.1140 7.67 1.043 -0.1140 9.27 1.155 -0.1140 10.55 1.219 -0.1140 11.88 1.233 -0.1140 13.45 1.193 -0.1140 14.90 1.170 -0.1140 16.04 1.150 -0.1140 17.64 1.049 -0.1140 19.11 0.984 -0.1140 17.63 1.059 -0.1140 16.14 1.124 -0.1140 14.84 1.161 -0.1140 12.84 1.207 -0.1140 11.63 1.231 -0.1140 9.96 1.189 -0.1140 8.49 1.099 -0.1140 7.01 0.979 -0.1140 5.30 0.820 -0.1140 3.63 0.654 -0.1140 2.00 0.491 -0.1140 0.56 0.336 -0.1140 -0.83 0.201 -0.1140 -2.33 0.045 -0.1140 -3.82 -0.137 -0.1140 -5.43 -0.363 -0.1140 Tabulated from data in file JG00575.DAT & reduced using program Q01.00L File be50.lft created on 12-05-1997 at 15:25:49 using program FORMAT