Airfoil: E374 (B) Builder: M. Bame Comment: clean Number of Reynolds #'s: 5 Average Reynolds #: 61300 Number of angles of attack: 49 alpha / Cl / Cm -6.58 -0.407 -0.0420 -5.25 -0.348 -0.0420 -4.17 -0.282 -0.0420 -3.14 -0.209 -0.0420 -2.29 -0.120 -0.0420 -1.25 0.014 -0.0420 -0.22 0.150 -0.0420 1.00 0.284 -0.0420 1.82 0.347 -0.0420 2.86 0.427 -0.0420 3.89 0.544 -0.0420 4.92 0.697 -0.0420 5.97 0.793 -0.0420 7.01 0.881 -0.0420 8.06 0.960 -0.0420 9.10 0.983 -0.0420 10.08 1.036 -0.0420 11.14 1.056 -0.0420 12.04 1.062 -0.0420 13.10 1.057 -0.0420 14.02 1.079 -0.0420 15.13 1.041 -0.0420 16.14 0.946 -0.0420 17.13 0.909 -0.0420 18.16 0.925 -0.0420 16.93 0.887 -0.0420 15.90 0.982 -0.0420 14.97 1.026 -0.0420 14.00 1.067 -0.0420 12.97 1.054 -0.0420 11.90 1.071 -0.0420 10.94 1.048 -0.0420 9.90 1.008 -0.0420 8.91 0.976 -0.0420 7.91 0.951 -0.0420 6.92 0.875 -0.0420 5.86 0.783 -0.0420 4.88 0.686 -0.0420 3.82 0.551 -0.0420 2.81 0.432 -0.0420 1.76 0.354 -0.0420 0.71 0.254 -0.0420 -0.26 0.142 -0.0420 -1.30 -0.006 -0.0420 -2.33 -0.122 -0.0420 -3.34 -0.216 -0.0420 -4.36 -0.290 -0.0420 -5.38 -0.349 -0.0420 -6.45 -0.402 -0.0420 Tabulated from data in file JG00361.DAT & reduced using program Q01.00L Average Reynolds #: 102100 Number of angles of attack: 49 alpha / Cl / Cm -6.36 -0.418 -0.0420 -5.21 -0.362 -0.0420 -4.20 -0.251 -0.0420 -3.17 -0.128 -0.0420 -2.24 0.022 -0.0420 -1.23 0.156 -0.0420 -0.14 0.261 -0.0420 0.85 0.332 -0.0420 1.85 0.411 -0.0420 2.84 0.501 -0.0420 3.89 0.602 -0.0420 5.01 0.710 -0.0420 6.02 0.805 -0.0420 7.01 0.895 -0.0420 8.03 0.939 -0.0420 9.13 0.975 -0.0420 10.03 1.010 -0.0420 11.00 1.037 -0.0420 12.07 1.052 -0.0420 12.98 1.031 -0.0420 14.08 1.011 -0.0420 15.03 0.914 -0.0420 16.12 0.889 -0.0420 17.12 0.868 -0.0420 18.10 0.864 -0.0420 16.92 0.871 -0.0420 15.85 0.887 -0.0420 14.94 0.915 -0.0420 13.98 1.028 -0.0420 12.95 1.044 -0.0420 11.90 1.036 -0.0420 10.91 1.024 -0.0420 9.96 0.994 -0.0420 8.89 0.953 -0.0420 7.95 0.925 -0.0420 6.91 0.875 -0.0420 5.91 0.784 -0.0420 4.86 0.681 -0.0420 3.88 0.586 -0.0420 2.80 0.481 -0.0420 1.80 0.395 -0.0420 0.81 0.313 -0.0420 -0.26 0.235 -0.0420 -1.26 0.139 -0.0420 -2.34 -0.007 -0.0420 -3.39 -0.154 -0.0420 -4.38 -0.278 -0.0420 -5.47 -0.382 -0.0420 -6.44 -0.425 -0.0420 Tabulated from data in file JG00363.DAT & reduced using program Q01.00L Average Reynolds #: 152900 Number of angles of attack: 53 alpha / Cl / Cm -6.53 -0.461 -0.0420 -5.31 -0.370 -0.0420 -4.32 -0.225 -0.0420 -3.14 -0.090 -0.0420 -2.19 -0.024 -0.0420 -1.12 0.084 -0.0420 -0.22 0.236 -0.0420 0.82 0.327 -0.0420 1.85 0.418 -0.0420 2.89 0.514 -0.0420 3.98 0.619 -0.0420 4.92 0.713 -0.0420 5.95 0.809 -0.0420 7.05 0.902 -0.0420 8.00 0.938 -0.0420 9.00 0.976 -0.0420 10.02 1.009 -0.0420 10.98 1.036 -0.0420 12.00 1.049 -0.0420 13.03 1.072 -0.0420 14.11 1.038 -0.0420 15.05 0.932 -0.0420 15.98 0.895 -0.0420 17.00 0.887 -0.0420 18.04 0.879 -0.0420 19.10 0.874 -0.0420 20.13 0.897 -0.0420 18.84 0.876 -0.0420 17.84 0.864 -0.0420 16.91 0.886 -0.0420 15.89 0.918 -0.0420 14.92 0.931 -0.0420 13.94 1.034 -0.0420 12.97 1.082 -0.0420 11.94 1.050 -0.0420 10.91 1.033 -0.0420 9.98 1.007 -0.0420 8.91 0.967 -0.0420 7.92 0.930 -0.0420 6.95 0.887 -0.0420 5.87 0.790 -0.0420 4.82 0.692 -0.0420 3.76 0.587 -0.0420 2.82 0.495 -0.0420 1.77 0.399 -0.0420 0.71 0.308 -0.0420 -0.28 0.221 -0.0420 -1.37 0.040 -0.0420 -2.32 -0.043 -0.0420 -3.45 -0.130 -0.0420 -4.35 -0.241 -0.0420 -5.50 -0.397 -0.0420 -6.47 -0.462 -0.0420 Tabulated from data in file AB00501.DAT & reduced using program Q01.00L Average Reynolds #: 203500 Number of angles of attack: 49 alpha / Cl / Cm -6.15 -0.385 -0.0420 -5.30 -0.268 -0.0420 -3.99 -0.135 -0.0420 -3.06 -0.066 -0.0420 -2.14 0.002 -0.0420 -1.12 0.097 -0.0420 -0.22 0.248 -0.0420 0.89 0.349 -0.0420 1.99 0.448 -0.0420 2.89 0.533 -0.0420 3.94 0.634 -0.0420 4.98 0.735 -0.0420 5.99 0.827 -0.0420 6.95 0.898 -0.0420 8.02 0.940 -0.0420 9.06 0.983 -0.0420 9.99 1.017 -0.0420 11.06 1.041 -0.0420 11.99 1.058 -0.0420 13.05 1.084 -0.0420 14.13 1.033 -0.0420 15.12 0.938 -0.0420 15.99 0.917 -0.0420 17.06 0.891 -0.0420 18.29 0.850 -0.0420 16.76 0.907 -0.0420 15.73 0.915 -0.0420 14.82 0.984 -0.0420 13.92 1.067 -0.0420 12.88 1.083 -0.0420 11.95 1.052 -0.0420 10.96 1.033 -0.0420 9.91 1.008 -0.0420 8.89 0.969 -0.0420 7.90 0.927 -0.0420 6.86 0.885 -0.0420 5.86 0.807 -0.0420 4.86 0.714 -0.0420 3.86 0.617 -0.0420 2.83 0.519 -0.0420 1.80 0.420 -0.0420 0.71 0.321 -0.0420 -0.30 0.216 -0.0420 -1.29 0.073 -0.0420 -2.38 -0.028 -0.0420 -3.44 -0.103 -0.0420 -4.42 -0.180 -0.0420 -5.60 -0.326 -0.0420 -6.53 -0.439 -0.0420 Tabulated from data in file JG00359.DAT & reduced using program Q01.00L Average Reynolds #: 305000 Number of angles of attack: 49 alpha / Cl / Cm -6.37 -0.361 -0.0420 -5.24 -0.244 -0.0420 -4.08 -0.154 -0.0420 -3.09 -0.075 -0.0420 -2.13 0.002 -0.0420 -1.02 0.093 -0.0420 -0.00 0.215 -0.0420 1.00 0.356 -0.0420 2.06 0.454 -0.0420 2.97 0.540 -0.0420 3.96 0.635 -0.0420 5.16 0.752 -0.0420 6.09 0.831 -0.0420 6.96 0.881 -0.0420 8.01 0.932 -0.0420 9.10 0.982 -0.0420 10.06 1.017 -0.0420 11.07 1.041 -0.0420 12.03 1.117 -0.0420 13.02 1.104 -0.0420 14.07 1.092 -0.0420 15.00 1.004 -0.0420 16.02 0.934 -0.0420 17.06 0.904 -0.0420 18.08 0.892 -0.0420 16.82 0.909 -0.0420 15.73 0.942 -0.0420 14.85 1.015 -0.0420 13.75 1.110 -0.0420 12.94 1.094 -0.0420 11.90 1.097 -0.0420 10.91 1.032 -0.0420 9.91 1.006 -0.0420 8.86 0.965 -0.0420 7.82 0.915 -0.0420 6.78 0.867 -0.0420 5.78 0.794 -0.0420 4.79 0.701 -0.0420 3.75 0.601 -0.0420 2.70 0.498 -0.0420 1.61 0.396 -0.0420 0.60 0.299 -0.0420 -0.41 0.138 -0.0420 -1.48 0.044 -0.0420 -2.53 -0.041 -0.0420 -3.45 -0.117 -0.0420 -4.66 -0.212 -0.0420 -5.60 -0.293 -0.0420 -6.78 -0.429 -0.0420 Tabulated from data in file JG00062.DAT & reduced using program Q01.00L File e374b.lft created on 12-05-1997 at 15:25:49 using program FORMAT