Airfoil: RG15 (C) Builder: B. Champine / J. Robertson Comment: covering over obechi: flap = 0 degs Number of Reynolds #'s: 4 Average Reynolds #: 60500 Number of angles of attack: 49 alpha / Cl / Cm -6.72 -0.349 -0.0580 -5.11 -0.236 -0.0580 -4.23 -0.174 -0.0580 -3.08 -0.095 -0.0580 -2.22 -0.037 -0.0580 -1.10 0.068 -0.0580 0.04 0.181 -0.0580 0.90 0.272 -0.0580 2.07 0.488 -0.0580 2.94 0.592 -0.0580 4.10 0.691 -0.0580 4.99 0.762 -0.0580 6.19 0.853 -0.0580 7.09 0.917 -0.0580 7.99 0.971 -0.0580 9.20 1.020 -0.0580 10.20 1.060 -0.0580 11.05 1.065 -0.0580 12.17 1.056 -0.0580 13.02 1.004 -0.0580 14.14 0.968 -0.0580 15.00 0.967 -0.0580 16.26 0.967 -0.0580 16.95 0.978 -0.0580 18.17 0.932 -0.0580 16.56 0.983 -0.0580 15.59 0.992 -0.0580 14.63 0.992 -0.0580 13.68 0.971 -0.0580 12.56 1.055 -0.0580 11.64 1.077 -0.0580 10.71 1.074 -0.0580 9.60 1.046 -0.0580 8.62 1.004 -0.0580 7.65 0.959 -0.0580 6.67 0.899 -0.0580 5.46 0.812 -0.0580 4.65 0.747 -0.0580 3.49 0.655 -0.0580 2.51 0.566 -0.0580 1.57 0.413 -0.0580 0.43 0.238 -0.0580 -0.66 0.124 -0.0580 -1.61 0.028 -0.0580 -2.73 -0.068 -0.0580 -3.69 -0.124 -0.0580 -4.63 -0.188 -0.0580 -5.77 -0.269 -0.0580 -6.71 -0.338 -0.0580 Tabulated from data in file FS00928.DAT & reduced using program Q02.00L Average Reynolds #: 100400 Number of angles of attack: 49 alpha / Cl / Cm -6.69 -0.394 -0.0580 -5.12 -0.267 -0.0580 -4.18 -0.196 -0.0580 -3.24 -0.116 -0.0580 -2.03 -0.034 -0.0580 -1.12 0.064 -0.0580 -0.16 0.221 -0.0580 1.07 0.410 -0.0580 2.00 0.506 -0.0580 2.93 0.589 -0.0580 4.18 0.700 -0.0580 5.12 0.785 -0.0580 6.21 0.875 -0.0580 7.19 0.946 -0.0580 8.16 0.986 -0.0580 9.12 1.032 -0.0580 10.34 1.076 -0.0580 11.20 1.082 -0.0580 12.23 1.092 -0.0580 13.15 0.984 -0.0580 14.06 0.964 -0.0580 15.12 0.938 -0.0580 16.08 0.918 -0.0580 17.16 0.900 -0.0580 18.15 0.912 -0.0580 16.56 0.912 -0.0580 15.50 0.920 -0.0580 14.46 0.954 -0.0580 13.62 0.979 -0.0580 12.64 1.060 -0.0580 11.69 1.073 -0.0580 10.58 1.091 -0.0580 9.54 1.042 -0.0580 8.70 1.005 -0.0580 7.62 0.956 -0.0580 6.57 0.893 -0.0580 5.52 0.806 -0.0580 4.44 0.717 -0.0580 3.38 0.621 -0.0580 2.57 0.548 -0.0580 1.38 0.434 -0.0580 0.35 0.294 -0.0580 -0.57 0.131 -0.0580 -1.64 -0.002 -0.0580 -2.73 -0.087 -0.0580 -3.63 -0.152 -0.0580 -4.85 -0.247 -0.0580 -5.76 -0.311 -0.0580 -6.87 -0.395 -0.0580 Tabulated from data in file FS00930.DAT & reduced using program Q02.00L Average Reynolds #: 201100 Number of angles of attack: 49 alpha / Cl / Cm -6.66 -0.388 -0.0580 -5.10 -0.259 -0.0580 -4.08 -0.175 -0.0580 -3.16 -0.075 -0.0580 -2.16 0.049 -0.0580 -0.94 0.189 -0.0580 0.08 0.297 -0.0580 1.14 0.399 -0.0580 2.14 0.499 -0.0580 3.13 0.599 -0.0580 4.11 0.699 -0.0580 5.00 0.796 -0.0580 6.14 0.894 -0.0580 7.25 0.970 -0.0580 8.23 1.027 -0.0580 9.04 1.067 -0.0580 10.21 1.102 -0.0580 11.06 1.126 -0.0580 12.11 1.098 -0.0580 13.14 1.048 -0.0580 14.19 0.970 -0.0580 15.00 0.969 -0.0580 16.18 0.915 -0.0580 17.01 0.914 -0.0580 18.23 0.919 -0.0580 16.33 0.918 -0.0580 15.55 0.938 -0.0580 14.30 0.977 -0.0580 13.64 1.026 -0.0580 12.54 1.066 -0.0580 11.69 1.109 -0.0580 10.73 1.106 -0.0580 9.62 1.082 -0.0580 8.67 1.044 -0.0580 7.50 0.977 -0.0580 6.69 0.924 -0.0580 5.44 0.824 -0.0580 4.47 0.736 -0.0580 3.46 0.625 -0.0580 2.47 0.524 -0.0580 1.35 0.411 -0.0580 0.32 0.306 -0.0580 -0.73 0.207 -0.0580 -1.65 0.102 -0.0580 -2.78 -0.031 -0.0580 -3.67 -0.141 -0.0580 -4.78 -0.244 -0.0580 -5.80 -0.324 -0.0580 -6.96 -0.418 -0.0580 Tabulated from data in file FS00932.DAT & reduced using program Q02.00L Average Reynolds #: 301500 Number of angles of attack: 49 alpha / Cl / Cm -6.17 -0.342 -0.0580 -5.18 -0.254 -0.0580 -4.05 -0.128 -0.0580 -2.94 -0.003 -0.0580 -1.94 0.096 -0.0580 -1.00 0.167 -0.0580 0.02 0.275 -0.0580 1.19 0.429 -0.0580 1.91 0.506 -0.0580 2.96 0.617 -0.0580 4.22 0.740 -0.0580 5.19 0.827 -0.0580 6.04 0.897 -0.0580 7.04 0.972 -0.0580 8.30 1.049 -0.0580 9.18 1.089 -0.0580 10.33 1.124 -0.0580 11.12 1.145 -0.0580 12.30 1.127 -0.0580 12.65 1.115 -0.0580 14.02 1.013 -0.0580 15.22 0.974 -0.0580 15.99 0.934 -0.0580 17.11 0.924 -0.0580 18.13 0.959 -0.0580 16.29 0.930 -0.0580 15.46 0.947 -0.0580 14.51 0.992 -0.0580 13.55 1.046 -0.0580 12.60 1.122 -0.0580 11.30 1.139 -0.0580 10.91 1.148 -0.0580 9.59 1.099 -0.0580 8.64 1.061 -0.0580 7.59 1.003 -0.0580 6.57 0.933 -0.0580 5.47 0.845 -0.0580 4.34 0.745 -0.0580 3.50 0.665 -0.0580 2.25 0.538 -0.0580 1.33 0.438 -0.0580 0.43 0.338 -0.0580 -0.82 0.182 -0.0580 -1.79 0.108 -0.0580 -2.77 0.012 -0.0580 -3.83 -0.107 -0.0580 -4.87 -0.224 -0.0580 -5.81 -0.314 -0.0580 -7.07 -0.426 -0.0580 Tabulated from data in file FS00934.DAT & reduced using program Q02.00L File rg15cf0.lft created on 09-12-1997 at 13:46:18 using program FORMAT