Airfoil: E387 (A) Builder: B. Champine Comment: clean Number of Reynolds #'s: 8 Average Reynolds #: 30100 Number of angles of attack: 97 alpha / Cl / Cm -6.79 -0.351 -0.0850 -6.45 -0.328 -0.0850 -5.81 -0.275 -0.0850 -5.43 -0.243 -0.0850 -4.85 -0.200 -0.0850 -4.46 -0.178 -0.0850 -3.91 -0.140 -0.0850 -3.44 -0.110 -0.0850 -2.73 -0.058 -0.0850 -2.43 -0.032 -0.0850 -1.75 0.026 -0.0850 -1.36 0.065 -0.0850 -0.78 0.114 -0.0850 -0.38 0.152 -0.0850 0.20 0.215 -0.0850 0.71 0.269 -0.0850 1.31 0.325 -0.0850 1.64 0.363 -0.0850 2.33 0.428 -0.0850 2.72 0.461 -0.0850 3.30 0.512 -0.0850 3.74 0.551 -0.0850 4.27 0.570 -0.0850 4.76 0.615 -0.0850 5.43 0.646 -0.0850 5.78 0.662 -0.0850 6.44 0.728 -0.0850 6.76 0.717 -0.0850 7.33 0.714 -0.0850 7.81 0.766 -0.0850 8.35 0.808 -0.0850 8.80 0.794 -0.0850 9.44 0.830 -0.0850 9.81 0.867 -0.0850 10.33 0.889 -0.0850 10.90 1.141 -0.0850 11.56 1.239 -0.0850 11.94 1.234 -0.0850 12.49 1.248 -0.0850 12.92 1.204 -0.0850 13.37 1.230 -0.0850 13.94 1.269 -0.0850 14.35 1.268 -0.0850 14.87 1.051 -0.0850 15.49 1.081 -0.0850 15.88 1.056 -0.0850 16.48 1.069 -0.0850 16.88 1.039 -0.0850 17.52 1.062 -0.0850 17.08 1.046 -0.0850 16.50 1.067 -0.0850 15.95 1.078 -0.0850 15.47 1.088 -0.0850 14.95 1.062 -0.0850 14.57 1.060 -0.0850 14.08 1.091 -0.0850 13.63 1.160 -0.0850 13.06 1.232 -0.0850 12.62 1.228 -0.0850 12.06 1.218 -0.0850 11.63 1.210 -0.0850 11.06 1.222 -0.0850 10.59 1.204 -0.0850 10.05 1.182 -0.0850 9.57 1.023 -0.0850 8.94 0.813 -0.0850 8.56 0.793 -0.0850 7.97 0.770 -0.0850 7.52 0.770 -0.0850 6.94 0.747 -0.0850 6.51 0.741 -0.0850 5.96 0.688 -0.0850 5.28 0.664 -0.0850 4.85 0.638 -0.0850 4.40 0.619 -0.0850 3.82 0.579 -0.0850 3.48 0.552 -0.0850 2.99 0.505 -0.0850 2.35 0.460 -0.0850 1.88 0.395 -0.0850 1.43 0.373 -0.0850 0.89 0.307 -0.0850 0.34 0.257 -0.0850 -0.27 0.199 -0.0850 -0.66 0.167 -0.0850 -1.20 0.111 -0.0850 -1.66 0.068 -0.0850 -2.23 0.018 -0.0850 -2.72 -0.019 -0.0850 -3.20 -0.052 -0.0850 -3.71 -0.083 -0.0850 -4.21 -0.121 -0.0850 -4.72 -0.155 -0.0850 -5.21 -0.194 -0.0850 -5.80 -0.247 -0.0850 -6.40 -0.304 -0.0850 -6.79 -0.330 -0.0850 Tabulated from data in file MS00296.DAT & reduced using program Q01.00L Average Reynolds #: 40500 Number of angles of attack: 97 alpha / Cl / Cm -7.15 -0.381 -0.0850 -6.62 -0.348 -0.0850 -5.86 -0.288 -0.0850 -5.49 -0.256 -0.0850 -4.76 -0.198 -0.0850 -4.39 -0.170 -0.0850 -3.82 -0.125 -0.0850 -3.40 -0.090 -0.0850 -2.74 -0.036 -0.0850 -2.41 -0.010 -0.0850 -1.78 0.045 -0.0850 -1.38 0.084 -0.0850 -0.76 0.142 -0.0850 -0.37 0.184 -0.0850 0.24 0.260 -0.0850 0.66 0.314 -0.0850 1.29 0.387 -0.0850 1.72 0.451 -0.0850 2.35 0.510 -0.0850 2.75 0.539 -0.0850 3.40 0.579 -0.0850 3.72 0.583 -0.0850 4.29 0.587 -0.0850 4.77 0.611 -0.0850 5.28 0.649 -0.0850 5.83 0.670 -0.0850 6.36 0.701 -0.0850 6.75 0.727 -0.0850 7.48 0.732 -0.0850 7.76 0.742 -0.0850 8.30 1.067 -0.0850 8.93 1.139 -0.0850 9.42 1.163 -0.0850 9.88 1.181 -0.0850 10.44 1.189 -0.0850 10.94 1.192 -0.0850 11.45 1.191 -0.0850 11.91 1.186 -0.0850 12.42 1.177 -0.0850 12.89 1.191 -0.0850 13.54 1.098 -0.0850 13.89 1.101 -0.0850 14.48 1.104 -0.0850 14.89 1.115 -0.0850 15.57 1.073 -0.0850 15.83 1.055 -0.0850 16.40 1.014 -0.0850 16.87 1.039 -0.0850 17.50 1.041 -0.0850 16.96 1.008 -0.0850 16.43 1.029 -0.0850 15.96 1.029 -0.0850 15.54 1.062 -0.0850 14.99 1.070 -0.0850 14.57 1.059 -0.0850 13.98 1.095 -0.0850 13.60 1.216 -0.0850 13.07 1.205 -0.0850 12.64 1.206 -0.0850 12.03 1.195 -0.0850 11.63 1.196 -0.0850 11.02 1.192 -0.0850 10.63 1.200 -0.0850 10.10 1.189 -0.0850 9.61 1.174 -0.0850 9.06 1.153 -0.0850 8.63 1.132 -0.0850 8.06 1.075 -0.0850 7.59 0.863 -0.0850 6.95 0.724 -0.0850 6.54 0.702 -0.0850 5.95 0.681 -0.0850 5.42 0.649 -0.0850 4.87 0.625 -0.0850 4.51 0.608 -0.0850 3.86 0.609 -0.0850 3.47 0.582 -0.0850 2.81 0.541 -0.0850 2.42 0.529 -0.0850 1.94 0.478 -0.0850 1.41 0.418 -0.0850 0.92 0.360 -0.0850 0.40 0.302 -0.0850 -0.15 0.225 -0.0850 -0.69 0.167 -0.0850 -1.18 0.112 -0.0850 -1.70 0.065 -0.0850 -2.29 0.015 -0.0850 -2.66 -0.011 -0.0850 -3.31 -0.062 -0.0850 -3.68 -0.093 -0.0850 -4.22 -0.139 -0.0850 -4.73 -0.178 -0.0850 -5.32 -0.223 -0.0850 -5.75 -0.259 -0.0850 -6.27 -0.300 -0.0850 -6.81 -0.341 -0.0850 Tabulated from data in file MS00294.DAT & reduced using program Q01.00L Average Reynolds #: 50800 Number of angles of attack: 97 alpha / Cl / Cm -7.05 -0.367 -0.0850 -6.50 -0.335 -0.0850 -5.90 -0.288 -0.0850 -5.50 -0.254 -0.0850 -4.91 -0.206 -0.0850 -4.44 -0.177 -0.0850 -3.86 -0.140 -0.0850 -3.46 -0.107 -0.0850 -2.77 -0.041 -0.0850 -2.37 0.002 -0.0850 -1.81 0.047 -0.0850 -1.35 0.099 -0.0850 -0.77 0.179 -0.0850 -0.36 0.233 -0.0850 0.19 0.301 -0.0850 0.62 0.361 -0.0850 1.20 0.423 -0.0850 1.65 0.463 -0.0850 2.26 0.515 -0.0850 2.78 0.555 -0.0850 3.40 0.604 -0.0850 3.78 0.628 -0.0850 4.34 0.685 -0.0850 4.79 0.753 -0.0850 5.47 0.832 -0.0850 5.83 0.869 -0.0850 6.44 0.934 -0.0850 6.87 0.977 -0.0850 7.48 1.035 -0.0850 7.84 1.071 -0.0850 8.51 1.128 -0.0850 8.88 1.145 -0.0850 9.43 1.169 -0.0850 9.92 1.179 -0.0850 10.54 1.190 -0.0850 10.88 1.198 -0.0850 11.42 1.205 -0.0850 11.89 1.209 -0.0850 12.44 1.206 -0.0850 12.89 1.201 -0.0850 13.50 1.187 -0.0850 13.91 1.193 -0.0850 14.54 1.216 -0.0850 14.89 1.178 -0.0850 15.43 1.205 -0.0850 15.89 1.146 -0.0850 16.40 1.138 -0.0850 16.87 1.061 -0.0850 17.47 1.084 -0.0850 16.99 1.120 -0.0850 16.47 1.139 -0.0850 15.98 1.096 -0.0850 15.53 1.151 -0.0850 15.05 1.100 -0.0850 14.57 1.090 -0.0850 14.07 1.178 -0.0850 13.63 1.191 -0.0850 13.06 1.191 -0.0850 12.59 1.201 -0.0850 12.09 1.198 -0.0850 11.57 1.201 -0.0850 11.05 1.188 -0.0850 10.58 1.186 -0.0850 10.04 1.175 -0.0850 9.64 1.169 -0.0850 9.05 1.141 -0.0850 8.63 1.120 -0.0850 8.02 1.075 -0.0850 7.58 1.027 -0.0850 7.03 0.976 -0.0850 6.53 0.924 -0.0850 5.93 0.863 -0.0850 5.46 0.819 -0.0850 4.91 0.762 -0.0850 4.46 0.689 -0.0850 3.88 0.628 -0.0850 3.41 0.594 -0.0850 2.95 0.566 -0.0850 2.35 0.521 -0.0850 1.84 0.486 -0.0850 1.40 0.435 -0.0850 0.80 0.378 -0.0850 0.40 0.335 -0.0850 -0.23 0.239 -0.0850 -0.64 0.190 -0.0850 -1.25 0.115 -0.0850 -1.65 0.075 -0.0850 -2.21 0.021 -0.0850 -2.72 -0.030 -0.0850 -3.35 -0.088 -0.0850 -3.74 -0.116 -0.0850 -4.37 -0.161 -0.0850 -4.73 -0.192 -0.0850 -5.28 -0.227 -0.0850 -5.82 -0.267 -0.0850 -6.43 -0.330 -0.0850 -6.81 -0.351 -0.0850 Tabulated from data in file MS00295.DAT & reduced using program Q01.00L Average Reynolds #: 61300 Number of angles of attack: 33 alpha / Cl / Cm -7.00 -0.383 -0.0850 -5.32 -0.240 -0.0850 -3.76 -0.125 -0.0850 -2.08 0.053 -0.0850 -0.64 0.251 -0.0850 0.85 0.409 -0.0850 2.55 0.578 -0.0850 4.10 0.739 -0.0850 5.47 0.870 -0.0850 6.96 1.011 -0.0850 8.79 1.171 -0.0850 10.11 1.213 -0.0850 11.69 1.241 -0.0850 13.03 1.246 -0.0850 14.51 1.179 -0.0850 16.16 1.156 -0.0850 17.59 1.117 -0.0850 15.85 1.146 -0.0850 14.43 1.237 -0.0850 12.97 1.247 -0.0850 11.26 1.230 -0.0850 9.90 1.203 -0.0850 8.35 1.136 -0.0850 6.83 0.992 -0.0850 5.27 0.840 -0.0850 3.79 0.698 -0.0850 2.27 0.543 -0.0850 0.68 0.389 -0.0850 -1.00 0.174 -0.0850 -2.45 0.003 -0.0850 -3.93 -0.144 -0.0850 -5.50 -0.255 -0.0850 -7.10 -0.394 -0.0850 Tabulated from data in file AB00208.DAT & reduced using program Q01.00L Average Reynolds #: 101900 Number of angles of attack: 33 alpha / Cl / Cm -6.91 -0.398 -0.0850 -5.33 -0.269 -0.0850 -3.68 -0.067 -0.0850 -2.00 0.154 -0.0850 -0.51 0.306 -0.0850 0.78 0.428 -0.0850 2.49 0.589 -0.0850 3.91 0.723 -0.0850 5.56 0.877 -0.0850 6.91 1.009 -0.0850 8.65 1.149 -0.0850 10.07 1.178 -0.0850 11.69 1.202 -0.0850 13.05 1.202 -0.0850 14.68 1.178 -0.0850 15.96 1.060 -0.0850 17.66 1.036 -0.0850 15.81 1.079 -0.0850 14.25 1.193 -0.0850 12.99 1.186 -0.0850 11.44 1.189 -0.0850 9.96 1.161 -0.0850 8.29 1.111 -0.0850 6.84 0.982 -0.0850 5.20 0.825 -0.0850 3.73 0.683 -0.0850 2.03 0.519 -0.0850 0.58 0.381 -0.0850 -0.92 0.238 -0.0850 -2.47 0.074 -0.0850 -4.14 -0.155 -0.0850 -5.56 -0.310 -0.0850 -7.10 -0.420 -0.0850 Tabulated from data in file AB00210.DAT & reduced using program Q01.00L Average Reynolds #: 152600 Number of angles of attack: 33 alpha / Cl / Cm -7.07 -0.441 -0.0850 -5.32 -0.275 -0.0850 -3.53 -0.021 -0.0850 -2.08 0.116 -0.0850 -0.60 0.253 -0.0850 0.85 0.403 -0.0850 2.50 0.572 -0.0850 4.04 0.728 -0.0850 5.61 0.880 -0.0850 7.03 1.015 -0.0850 8.61 1.130 -0.0850 10.01 1.172 -0.0850 11.54 1.191 -0.0850 13.00 1.194 -0.0850 14.53 1.208 -0.0850 16.09 1.124 -0.0850 17.55 1.072 -0.0850 15.84 1.113 -0.0850 14.38 1.210 -0.0850 12.98 1.191 -0.0850 11.45 1.189 -0.0850 9.94 1.161 -0.0850 8.43 1.112 -0.0850 6.81 0.985 -0.0850 5.29 0.837 -0.0850 3.80 0.690 -0.0850 2.08 0.513 -0.0850 0.69 0.371 -0.0850 -0.93 0.203 -0.0850 -2.61 0.051 -0.0850 -4.05 -0.102 -0.0850 -5.62 -0.328 -0.0850 -7.26 -0.453 -0.0850 Tabulated from data in file JG00554.DAT & reduced using program Q01.00L Average Reynolds #: 203100 Number of angles of attack: 33 alpha / Cl / Cm -7.02 -0.429 -0.0850 -4.62 -0.122 -0.0850 -3.39 -0.001 -0.0850 -2.05 0.121 -0.0850 -0.39 0.282 -0.0850 1.18 0.443 -0.0850 2.71 0.601 -0.0850 4.30 0.767 -0.0850 5.65 0.900 -0.0850 7.21 1.045 -0.0850 8.76 1.136 -0.0850 10.20 1.180 -0.0850 11.53 1.192 -0.0850 13.06 1.198 -0.0850 14.59 1.225 -0.0850 16.50 1.092 -0.0850 17.67 1.057 -0.0850 15.68 1.145 -0.0850 14.13 1.222 -0.0850 12.89 1.196 -0.0850 11.29 1.186 -0.0850 9.79 1.166 -0.0850 8.19 1.103 -0.0850 6.68 0.992 -0.0850 4.98 0.825 -0.0850 3.56 0.682 -0.0850 1.74 0.493 -0.0850 0.42 0.356 -0.0850 -1.21 0.187 -0.0850 -2.73 0.048 -0.0850 -4.61 -0.135 -0.0850 -5.86 -0.315 -0.0850 -7.57 -0.470 -0.0850 Tabulated from data in file JG00212.DAT & reduced using program Q01.00L Average Reynolds #: 304400 Number of angles of attack: 33 alpha / Cl / Cm -6.95 -0.427 -0.0850 -5.49 -0.229 -0.0850 -3.97 -0.075 -0.0850 -2.28 0.085 -0.0850 -0.45 0.264 -0.0850 1.01 0.423 -0.0850 2.46 0.579 -0.0850 4.03 0.743 -0.0850 5.54 0.897 -0.0850 6.93 1.023 -0.0850 8.49 1.123 -0.0850 9.96 1.184 -0.0850 11.48 1.202 -0.0850 12.94 1.209 -0.0850 14.37 1.260 -0.0850 15.98 1.150 -0.0850 17.76 1.063 -0.0850 15.83 1.151 -0.0850 14.45 1.263 -0.0850 12.92 1.209 -0.0850 11.42 1.196 -0.0850 9.90 1.174 -0.0850 8.39 1.107 -0.0850 6.88 1.005 -0.0850 5.31 0.861 -0.0850 3.78 0.703 -0.0850 2.06 0.522 -0.0850 0.41 0.348 -0.0850 -1.41 0.157 -0.0850 -2.77 0.028 -0.0850 -4.21 -0.107 -0.0850 -5.50 -0.242 -0.0850 -7.09 -0.442 -0.0850 Tabulated from data in file JG00214.DAT & reduced using program Q01.00L File e387a.lft created on 12-05-1997 at 15:25:49 using program FORMAT