Airfoil: LD-79 Builder: L. DeWitt Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 59900 Number of angles of attack: 49 alpha / Cl / Cm -7.85 -0.509 -0.0900 -6.12 -0.441 -0.0900 -5.39 -0.373 -0.0900 -4.08 -0.193 -0.0900 -3.27 -0.079 -0.0900 -2.19 0.067 -0.0900 -1.11 0.206 -0.0900 -0.20 0.323 -0.0900 0.84 0.466 -0.0900 1.87 0.562 -0.0900 2.91 0.662 -0.0900 3.96 0.760 -0.0900 5.03 0.854 -0.0900 6.07 0.941 -0.0900 7.13 1.032 -0.0900 8.19 1.103 -0.0900 9.21 1.160 -0.0900 10.19 1.202 -0.0900 11.15 1.233 -0.0900 12.12 1.237 -0.0900 13.09 1.217 -0.0900 14.07 1.269 -0.0900 15.22 1.299 -0.0900 16.23 1.229 -0.0900 16.95 1.152 -0.0900 15.36 1.288 -0.0900 14.50 1.287 -0.0900 13.36 1.218 -0.0900 12.49 1.231 -0.0900 11.50 1.244 -0.0900 10.61 1.221 -0.0900 9.42 1.173 -0.0900 8.55 1.129 -0.0900 7.37 1.054 -0.0900 6.44 0.977 -0.0900 5.49 0.893 -0.0900 4.23 0.794 -0.0900 3.52 0.727 -0.0900 2.32 0.604 -0.0900 1.38 0.515 -0.0900 0.19 0.382 -0.0900 -0.75 0.237 -0.0900 -1.73 0.124 -0.0900 -2.96 -0.027 -0.0900 -3.91 -0.161 -0.0900 -4.91 -0.305 -0.0900 -5.76 -0.394 -0.0900 -6.94 -0.477 -0.0900 -8.08 -0.503 -0.0900 Tabulated from data in file FS00944.DAT & reduced using program Q02.00L Average Reynolds #: 100200 Number of angles of attack: 49 alpha / Cl / Cm -7.80 -0.520 -0.0900 -6.11 -0.441 -0.0900 -5.44 -0.380 -0.0900 -4.11 -0.173 -0.0900 -3.12 -0.026 -0.0900 -1.96 0.115 -0.0900 -1.19 0.214 -0.0900 -0.10 0.364 -0.0900 0.95 0.474 -0.0900 1.91 0.567 -0.0900 3.01 0.674 -0.0900 3.95 0.765 -0.0900 4.95 0.859 -0.0900 6.05 0.950 -0.0900 7.16 1.035 -0.0900 8.26 1.113 -0.0900 9.16 1.166 -0.0900 10.08 1.208 -0.0900 11.23 1.228 -0.0900 12.22 1.210 -0.0900 13.21 1.180 -0.0900 14.10 1.272 -0.0900 15.29 1.274 -0.0900 16.04 1.210 -0.0900 17.18 1.118 -0.0900 15.44 1.198 -0.0900 14.57 1.311 -0.0900 13.44 1.202 -0.0900 12.43 1.187 -0.0900 11.55 1.201 -0.0900 10.36 1.187 -0.0900 9.48 1.155 -0.0900 8.56 1.104 -0.0900 7.29 1.018 -0.0900 6.34 0.945 -0.0900 5.36 0.863 -0.0900 4.34 0.772 -0.0900 3.34 0.677 -0.0900 2.35 0.571 -0.0900 1.21 0.457 -0.0900 0.24 0.357 -0.0900 -0.65 0.250 -0.0900 -1.88 0.082 -0.0900 -2.77 -0.035 -0.0900 -3.75 -0.183 -0.0900 -5.11 -0.360 -0.0900 -6.02 -0.445 -0.0900 -6.88 -0.502 -0.0900 -7.98 -0.535 -0.0900 Tabulated from data in file FS00946.DAT & reduced using program Q02.00L Average Reynolds #: 150400 Number of angles of attack: 49 alpha / Cl / Cm -7.81 -0.516 -0.0900 -6.21 -0.435 -0.0900 -5.24 -0.341 -0.0900 -4.25 -0.184 -0.0900 -3.22 -0.030 -0.0900 -1.91 0.132 -0.0900 -1.22 0.231 -0.0900 -0.03 0.370 -0.0900 1.10 0.487 -0.0900 1.89 0.569 -0.0900 2.99 0.689 -0.0900 4.22 0.834 -0.0900 4.88 0.888 -0.0900 6.05 0.983 -0.0900 7.19 1.069 -0.0900 8.14 1.130 -0.0900 9.27 1.187 -0.0900 10.04 1.209 -0.0900 11.07 1.207 -0.0900 12.06 1.204 -0.0900 13.03 1.261 -0.0900 13.99 1.295 -0.0900 15.33 1.206 -0.0900 16.10 1.164 -0.0900 17.07 1.122 -0.0900 15.04 1.249 -0.0900 14.47 1.265 -0.0900 13.52 1.299 -0.0900 12.51 1.185 -0.0900 11.52 1.201 -0.0900 10.53 1.203 -0.0900 9.34 1.177 -0.0900 8.32 1.128 -0.0900 7.30 1.062 -0.0900 6.22 0.980 -0.0900 5.41 0.916 -0.0900 4.37 0.831 -0.0900 3.16 0.715 -0.0900 2.35 0.609 -0.0900 1.10 0.470 -0.0900 0.31 0.388 -0.0900 -0.72 0.274 -0.0900 -1.76 0.135 -0.0900 -2.96 -0.034 -0.0900 -4.14 -0.178 -0.0900 -4.85 -0.287 -0.0900 -5.87 -0.408 -0.0900 -6.94 -0.485 -0.0900 -7.93 -0.515 -0.0900 Tabulated from data in file FS00950.DAT & reduced using program Q02.00L Average Reynolds #: 200500 Number of angles of attack: 49 alpha / Cl / Cm -7.41 -0.523 -0.0900 -6.44 -0.484 -0.0900 -5.16 -0.347 -0.0900 -4.41 -0.228 -0.0900 -3.18 -0.031 -0.0900 -2.00 0.116 -0.0900 -1.20 0.221 -0.0900 -0.04 0.350 -0.0900 0.92 0.489 -0.0900 1.96 0.600 -0.0900 3.01 0.706 -0.0900 4.06 0.807 -0.0900 5.12 0.893 -0.0900 6.02 0.966 -0.0900 6.98 1.038 -0.0900 8.26 1.125 -0.0900 9.22 1.173 -0.0900 10.22 1.203 -0.0900 11.01 1.204 -0.0900 12.15 1.200 -0.0900 13.28 1.309 -0.0900 14.21 1.272 -0.0900 14.87 1.237 -0.0900 16.16 1.198 -0.0900 16.87 1.101 -0.0900 15.29 1.230 -0.0900 14.72 1.256 -0.0900 13.91 1.299 -0.0900 12.30 1.188 -0.0900 11.41 1.199 -0.0900 10.52 1.199 -0.0900 9.50 1.173 -0.0900 8.30 1.113 -0.0900 7.21 1.042 -0.0900 6.41 0.983 -0.0900 5.23 0.888 -0.0900 4.15 0.797 -0.0900 3.42 0.728 -0.0900 2.40 0.627 -0.0900 1.10 0.488 -0.0900 0.09 0.379 -0.0900 -0.94 0.229 -0.0900 -1.75 0.131 -0.0900 -3.08 -0.048 -0.0900 -3.84 -0.142 -0.0900 -4.90 -0.311 -0.0900 -5.98 -0.442 -0.0900 -6.77 -0.505 -0.0900 -7.83 -0.543 -0.0900 Tabulated from data in file FS00948.DAT & reduced using program Q02.00L File ld79.lft created on 09-12-1997 at 13:46:17 using program FORMAT