Airfoil: GM15 Builder: G. Morris Comment: clean Number of Reynolds #'s: 5 Average Reynolds #: 30600 Number of angles of attack: 49 alpha / Cl / Cm -3.44 -0.043 -0.1540 -2.36 0.087 -0.1540 -1.30 0.190 -0.1540 -0.33 0.275 -0.1540 0.76 0.386 -0.1540 1.75 0.476 -0.1540 2.77 0.561 -0.1540 3.66 0.682 -0.1540 4.84 0.853 -0.1540 5.82 0.948 -0.1540 6.90 1.084 -0.1540 7.95 1.129 -0.1540 8.87 1.210 -0.1540 9.92 1.257 -0.1540 10.93 1.323 -0.1540 11.84 1.364 -0.1540 12.86 1.391 -0.1540 14.04 1.419 -0.1540 14.96 1.437 -0.1540 16.02 1.418 -0.1540 16.99 1.397 -0.1540 17.84 1.284 -0.1540 18.89 1.317 -0.1540 19.98 1.306 -0.1540 20.89 1.314 -0.1540 19.96 1.258 -0.1540 18.90 1.281 -0.1540 17.94 1.266 -0.1540 16.91 1.247 -0.1540 15.97 1.269 -0.1540 14.96 1.326 -0.1540 13.97 1.408 -0.1540 12.96 1.366 -0.1540 12.03 1.369 -0.1540 10.95 1.378 -0.1540 9.96 1.302 -0.1540 8.95 1.255 -0.1540 7.93 1.209 -0.1540 6.92 1.119 -0.1540 5.85 1.004 -0.1540 4.80 0.872 -0.1540 3.75 0.675 -0.1540 2.79 0.588 -0.1540 1.75 0.502 -0.1540 0.71 0.398 -0.1540 -0.29 0.282 -0.1540 -1.34 0.184 -0.1540 -2.41 0.070 -0.1540 -3.39 -0.023 -0.1540 Tabulated from data in file JG00403.DAT & reduced using program Q01.00L Average Reynolds #: 40200 Number of angles of attack: 49 alpha / Cl / Cm -3.55 -0.055 -0.1540 -2.44 0.079 -0.1540 -1.44 0.177 -0.1540 -0.48 0.264 -0.1540 0.71 0.371 -0.1540 1.56 0.453 -0.1540 2.65 0.578 -0.1540 3.75 0.752 -0.1540 4.67 0.880 -0.1540 5.76 0.991 -0.1540 6.88 1.087 -0.1540 7.84 1.155 -0.1540 8.84 1.231 -0.1540 9.90 1.290 -0.1540 10.87 1.270 -0.1540 11.82 1.275 -0.1540 12.87 1.311 -0.1540 13.83 1.317 -0.1540 14.88 1.323 -0.1540 16.00 1.322 -0.1540 16.94 1.221 -0.1540 17.88 1.160 -0.1540 18.99 1.171 -0.1540 19.87 1.242 -0.1540 20.81 1.232 -0.1540 19.90 1.178 -0.1540 18.92 1.201 -0.1540 17.90 1.183 -0.1540 16.95 1.302 -0.1540 16.00 1.349 -0.1540 14.94 1.303 -0.1540 14.05 1.315 -0.1540 12.98 1.302 -0.1540 12.02 1.306 -0.1540 10.92 1.276 -0.1540 9.94 1.270 -0.1540 8.91 1.222 -0.1540 7.93 1.165 -0.1540 6.82 1.076 -0.1540 5.87 1.010 -0.1540 4.83 0.903 -0.1540 3.84 0.759 -0.1540 2.74 0.600 -0.1540 1.75 0.488 -0.1540 0.71 0.371 -0.1540 -0.26 0.278 -0.1540 -1.36 0.179 -0.1540 -2.40 0.078 -0.1540 -3.43 -0.041 -0.1540 Tabulated from data in file JG00402.DAT & reduced using program Q01.00L Average Reynolds #: 60900 Number of angles of attack: 33 alpha / Cl / Cm -3.53 0.000 -0.1540 -1.94 0.173 -0.1540 -0.41 0.317 -0.1540 1.12 0.482 -0.1540 2.69 0.727 -0.1540 4.25 0.911 -0.1540 5.78 1.042 -0.1540 7.30 1.170 -0.1540 8.92 1.251 -0.1540 10.34 1.304 -0.1540 11.93 1.339 -0.1540 13.32 1.324 -0.1540 14.93 1.286 -0.1540 16.31 1.282 -0.1540 17.87 1.179 -0.1540 19.27 1.166 -0.1540 20.88 1.224 -0.1540 19.35 1.166 -0.1540 17.86 1.196 -0.1540 16.38 1.270 -0.1540 14.87 1.300 -0.1540 13.38 1.317 -0.1540 11.94 1.326 -0.1540 10.38 1.292 -0.1540 8.92 1.234 -0.1540 7.40 1.163 -0.1540 5.84 1.027 -0.1540 4.27 0.891 -0.1540 2.71 0.698 -0.1540 1.16 0.463 -0.1540 -0.39 0.299 -0.1540 -1.91 0.159 -0.1540 -3.51 -0.006 -0.1540 Tabulated from data in file JG00400.DAT & reduced using program Q01.00L Average Reynolds #: 101200 Number of angles of attack: 33 alpha / Cl / Cm -3.39 0.025 -0.1540 -1.43 0.240 -0.1540 0.01 0.419 -0.1540 1.55 0.635 -0.1540 3.10 0.812 -0.1540 4.59 0.946 -0.1540 6.12 1.077 -0.1540 7.52 1.180 -0.1540 9.08 1.244 -0.1540 10.55 1.301 -0.1540 12.41 1.326 -0.1540 13.94 1.261 -0.1540 15.35 1.240 -0.1540 16.84 1.216 -0.1540 18.29 1.121 -0.1540 19.84 1.135 -0.1540 21.36 1.189 -0.1540 18.15 1.112 -0.1540 17.61 1.143 -0.1540 15.98 1.224 -0.1540 14.63 1.264 -0.1540 13.13 1.334 -0.1540 11.55 1.313 -0.1540 10.17 1.279 -0.1540 8.46 1.206 -0.1540 6.94 1.130 -0.1540 5.63 1.021 -0.1540 4.17 0.886 -0.1540 2.20 0.695 -0.1540 0.91 0.521 -0.1540 -0.77 0.289 -0.1540 -2.15 0.141 -0.1540 -3.94 -0.097 -0.1540 Tabulated from data in file MS00394.DAT & reduced using program Q01.00L Average Reynolds #: 201800 Number of angles of attack: 33 alpha / Cl / Cm -3.34 0.133 -0.1540 -1.65 0.339 -0.1540 -0.33 0.503 -0.1540 1.47 0.676 -0.1540 2.96 0.822 -0.1540 4.66 0.987 -0.1540 5.94 1.098 -0.1540 7.58 1.196 -0.1540 9.02 1.268 -0.1540 10.67 1.317 -0.1540 12.14 1.373 -0.1540 13.58 1.343 -0.1540 14.85 1.333 -0.1540 16.31 1.304 -0.1540 17.85 1.101 -0.1540 19.31 1.135 -0.1540 20.83 1.176 -0.1540 19.17 1.133 -0.1540 17.55 1.099 -0.1540 16.12 1.283 -0.1540 14.59 1.298 -0.1540 13.24 1.360 -0.1540 11.76 1.362 -0.1540 10.22 1.304 -0.1540 8.71 1.251 -0.1540 6.97 1.162 -0.1540 5.50 1.056 -0.1540 3.89 0.904 -0.1540 2.34 0.751 -0.1540 0.64 0.587 -0.1540 -0.65 0.454 -0.1540 -2.25 0.249 -0.1540 -3.71 0.068 -0.1540 Tabulated from data in file JG00398.DAT & reduced using program Q01.00L File gm15.lft created on 12-05-1997 at 15:25:49 using program FORMAT