Name = AG14 Mach = 0; Re = 25000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. S.U. S.L. L/D A.C. C.P. [¡] [-] [-] [-] [-] [-] [-] [-] [-] [-] [-] -15.0 -0.223 0.39686 0.011 1.000 0.002 1.000 0.004 -0.561 0.050 0.301 -14.5 -0.232 0.34925 0.009 1.000 0.002 1.000 0.004 -0.666 0.048 0.290 -14.0 -0.242 0.33952 0.007 1.000 0.002 1.000 0.004 -0.714 0.042 0.280 -13.5 -0.252 0.28949 0.005 1.000 0.002 1.000 0.004 -0.870 0.032 0.271 -13.0 -0.261 0.28028 0.003 1.000 0.002 1.000 0.004 -0.930 0.014 0.262 -12.5 -0.269 0.25149 0.001 1.000 0.002 1.000 0.004 -1.069 -0.016 0.254 -12.0 -0.276 0.23359 -0.001 1.000 0.002 1.000 0.004 -1.181 -0.070 0.247 -11.5 -0.282 0.20317 -0.003 1.000 0.002 1.000 0.003 -1.387 -0.180 0.240 -11.0 -0.286 0.18015 -0.005 1.000 0.002 1.000 0.003 -1.585 -0.498 0.233 -10.5 -0.287 0.26560 -0.007 1.000 0.002 1.000 0.003 -1.081 -4.499 0.226 -10.0 -0.286 0.21600 -0.009 1.000 0.002 1.000 0.003 -1.326 1.155 0.218 -9.5 -0.283 0.20467 -0.011 1.000 0.002 1.000 0.003 -1.381 0.644 0.211 -9.0 -0.276 0.17034 -0.013 1.000 0.002 1.000 0.003 -1.619 0.493 0.202 -8.5 -0.265 0.15968 -0.015 1.000 0.002 1.000 0.003 -1.662 0.424 0.192 -8.0 -0.252 0.13996 -0.017 1.000 0.001 1.000 0.002 -1.798 0.386 0.181 -7.5 -0.234 0.11893 -0.020 1.000 0.001 1.000 0.002 -1.970 0.361 0.166 -7.0 -0.213 0.10370 -0.022 1.000 0.001 1.000 0.002 -2.058 0.344 0.148 -6.5 -0.189 0.08975 -0.024 1.000 0.001 1.000 0.002 -2.107 0.332 0.124 -6.0 -0.161 0.07586 -0.026 1.000 0.002 1.000 0.002 -2.126 0.324 0.089 -5.5 -0.131 0.06385 -0.028 1.000 0.002 1.000 0.002 -2.058 0.319 0.036 -5.0 -0.099 0.05697 -0.030 1.000 0.002 1.000 0.003 -1.740 0.315 -0.055 -4.5 -0.065 0.04935 -0.032 1.000 0.002 1.000 0.003 -1.325 0.313 -0.246 -4.0 -0.030 0.04234 -0.035 1.000 0.002 1.000 0.003 -0.719 0.201 -0.887 -3.5 -0.154 0.03622 -0.037 1.000 0.002 1.000 0.003 -4.247 0.181 0.011 -3.0 -0.094 0.03177 -0.039 1.000 0.002 1.000 0.003 -2.956 0.286 -0.165 -2.5 -0.034 0.02807 -0.041 1.000 0.003 1.000 0.003 -1.215 0.287 -0.956 -2.0 0.025 0.02486 -0.043 1.000 0.003 1.000 0.005 1.015 0.344 1.966 -1.5 0.082 0.03601 -0.052 0.967 0.183 1.000 0.996 2.271 0.327 0.886 -1.0 0.139 0.02603 -0.052 0.940 0.995 1.000 0.995 5.351 0.251 0.624 -0.5 0.197 0.02666 -0.052 0.867 0.995 1.000 0.995 7.380 0.251 0.515 0.0 0.254 0.02790 -0.052 0.774 0.995 1.000 0.995 9.108 0.251 0.455 0.5 0.311 0.02892 -0.052 0.692 0.995 1.000 0.995 10.771 0.251 0.418 1.0 0.369 0.03018 -0.052 0.595 0.995 1.000 0.995 12.218 0.251 0.392 1.5 0.426 0.03184 -0.052 0.471 0.995 1.000 0.995 13.380 0.251 0.373 2.0 0.483 0.03372 -0.052 0.371 0.995 1.000 0.995 14.328 0.251 0.358 2.5 0.540 0.03434 -0.052 0.298 0.995 1.000 0.995 15.731 0.251 0.347 3.0 0.597 0.03512 -0.052 0.230 0.995 1.000 0.995 17.000 0.251 0.338 3.5 0.654 0.03539 -0.053 0.171 0.995 1.000 0.996 18.472 0.251 0.330 4.0 0.710 0.03570 -0.053 0.110 0.995 1.000 0.996 19.887 0.251 0.324 4.5 0.765 0.03507 -0.053 0.065 0.996 1.000 0.996 21.815 0.267 0.319 5.0 0.808 0.02999 -0.054 0.038 0.996 0.977 0.996 26.956 0.101 0.317 5.5 0.596 0.04647 -0.078 0.020 0.996 0.051 0.996 12.828 0.073 0.381 6.0 0.668 0.04397 -0.079 0.001 0.995 0.003 0.995 15.183 0.284 0.369 6.5 0.699 0.04982 -0.081 0.001 0.995 0.002 0.995 14.030 0.327 0.367 7.0 0.726 0.05650 -0.084 0.001 0.995 0.001 0.995 12.850 0.344 0.365 7.5 0.747 0.06434 -0.086 0.001 0.995 0.001 0.995 11.616 0.370 0.365 8.0 0.764 0.07600 -0.088 0.001 0.995 0.001 0.995 10.053 0.410 0.366 8.5 0.776 0.08615 -0.091 0.001 0.995 0.001 0.995 9.005 0.493 0.367 9.0 0.783 0.09758 -0.093 0.001 0.996 0.001 0.996 8.023 0.802 0.369 9.5 0.784 0.11089 -0.095 0.001 0.996 0.001 0.996 7.072 -1.387 0.371 10.0 0.780 0.12480 -0.097 0.001 0.996 0.001 0.996 6.251 -0.089 0.375 10.5 0.771 0.14846 -0.100 0.001 0.996 0.001 0.996 5.190 0.053 0.379 11.0 0.757 0.15923 -0.102 0.001 0.995 0.001 0.995 4.752 0.105 0.385 11.5 0.739 0.18506 -0.104 0.000 0.995 0.001 0.995 3.992 0.136 0.391 12.0 0.716 0.20725 -0.107 0.001 0.995 0.001 0.995 3.456 0.153 0.399 12.5 0.691 0.19416 -0.109 0.001 0.995 0.002 0.995 3.558 0.162 0.408 13.0 0.663 0.20465 -0.111 0.001 0.995 0.002 0.995 3.242 0.168 0.418 13.5 0.635 0.23659 -0.114 0.001 0.995 0.001 0.995 2.682 0.172 0.429 14.0 0.604 0.26694 -0.116 0.001 0.995 0.002 0.995 2.263 0.174 0.442 14.5 0.573 0.27596 -0.118 0.001 0.996 0.002 0.996 2.078 0.175 0.456 15.0 0.543 0.31073 -0.120 0.001 0.996 0.002 0.996 1.746 0.175 0.472 Name = AG14 Mach = 0; Re = 50000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. S.U. S.L. L/D A.C. C.P. [¡] [-] [-] [-] [-] [-] [-] [-] [-] [-] [-] -15.0 -0.223 0.29983 0.011 1.000 0.002 1.000 0.004 -0.742 0.050 0.301 -14.5 -0.232 0.28272 0.009 1.000 0.002 1.000 0.004 -0.822 0.048 0.290 -14.0 -0.242 0.25475 0.007 1.000 0.002 1.000 0.004 -0.951 0.042 0.280 -13.5 -0.252 0.22040 0.005 1.000 0.002 1.000 0.004 -1.142 0.032 0.271 -13.0 -0.261 0.21482 0.003 1.000 0.002 1.000 0.004 -1.213 0.014 0.263 -12.5 -0.269 0.19362 0.001 1.000 0.002 1.000 0.004 -1.388 -0.016 0.255 -12.0 -0.276 0.16866 -0.001 1.000 0.002 1.000 0.004 -1.636 -0.070 0.247 -11.5 -0.282 0.16202 -0.003 1.000 0.002 1.000 0.004 -1.738 -0.183 0.240 -11.0 -0.285 0.14253 -0.005 1.000 0.002 1.000 0.004 -2.003 -0.488 0.233 -10.5 -0.287 0.18813 -0.007 1.000 0.002 1.000 0.003 -1.527 -4.627 0.226 -10.0 -0.286 0.12256 -0.009 1.000 0.002 1.000 0.003 -2.336 1.155 0.218 -9.5 -0.283 0.14834 -0.011 1.000 0.002 1.000 0.003 -1.905 0.645 0.211 -9.0 -0.276 0.13073 -0.013 1.000 0.002 1.000 0.003 -2.109 0.493 0.202 -8.5 -0.265 0.11778 -0.015 1.000 0.002 1.000 0.003 -2.253 0.425 0.192 -8.0 -0.252 0.10317 -0.017 1.000 0.001 1.000 0.002 -2.439 0.386 0.181 -7.5 -0.234 0.08976 -0.020 1.000 0.001 1.000 0.002 -2.611 0.361 0.166 -7.0 -0.213 0.08019 -0.022 1.000 0.001 1.000 0.002 -2.659 0.344 0.148 -6.5 -0.189 0.07040 -0.024 1.000 0.001 1.000 0.002 -2.683 0.332 0.124 -6.0 -0.161 0.05918 -0.026 1.000 0.002 1.000 0.002 -2.725 0.324 0.089 -5.5 -0.131 0.05232 -0.028 1.000 0.002 1.000 0.003 -2.508 0.319 0.036 -5.0 -0.099 0.04538 -0.030 1.000 0.002 1.000 0.003 -2.185 0.316 -0.055 -4.5 -0.065 0.03964 -0.032 1.000 0.002 1.000 0.003 -1.649 0.313 -0.246 -4.0 -0.030 0.03429 -0.035 1.000 0.002 1.000 0.003 -0.887 0.201 -0.887 -3.5 -0.154 0.02955 -0.037 1.000 0.002 1.000 0.003 -5.205 0.181 0.011 -3.0 -0.094 0.02595 -0.039 1.000 0.002 1.000 0.003 -3.619 0.286 -0.165 -2.5 -0.034 0.02287 -0.041 1.000 0.003 1.000 0.003 -1.491 0.287 -0.956 -2.0 0.025 0.02027 -0.043 1.000 0.003 1.000 0.005 1.245 0.344 1.966 -1.5 0.082 0.03067 -0.052 0.967 0.183 1.000 0.997 2.666 0.327 0.886 -1.0 0.139 0.01899 -0.052 0.940 0.995 1.000 0.995 7.333 0.251 0.624 -0.5 0.197 0.01994 -0.052 0.867 0.995 1.000 0.995 9.868 0.251 0.515 0.0 0.254 0.02125 -0.052 0.774 0.995 1.000 0.995 11.960 0.251 0.455 0.5 0.311 0.02268 -0.052 0.692 0.995 1.000 0.995 13.734 0.251 0.418 1.0 0.369 0.02431 -0.052 0.595 0.995 1.000 0.995 15.168 0.251 0.392 1.5 0.426 0.02638 -0.052 0.471 0.995 1.000 0.995 16.146 0.251 0.373 2.0 0.483 0.02806 -0.052 0.371 0.995 1.000 0.995 17.218 0.251 0.358 2.5 0.540 0.02916 -0.052 0.298 0.995 1.000 0.995 18.527 0.251 0.347 3.0 0.597 0.03015 -0.052 0.230 0.995 1.000 0.995 19.803 0.251 0.338 3.5 0.654 0.03065 -0.053 0.171 0.995 1.000 0.996 21.330 0.251 0.330 4.0 0.710 0.03128 -0.053 0.110 0.995 1.000 0.996 22.695 0.251 0.324 4.5 0.765 0.03224 -0.053 0.065 0.996 1.000 0.996 23.735 0.252 0.319 5.0 0.819 0.03174 -0.053 0.038 0.996 1.000 0.996 25.795 0.252 0.314 5.5 0.870 0.03079 -0.053 0.020 0.996 1.000 0.996 28.262 0.078 0.311 6.0 0.665 0.03827 -0.079 0.001 0.995 0.004 0.995 17.374 0.084 0.369 6.5 0.699 0.04258 -0.081 0.001 0.995 0.002 0.995 16.405 0.324 0.367 7.0 0.726 0.04819 -0.084 0.001 0.995 0.001 0.995 15.058 0.344 0.365 7.5 0.747 0.05482 -0.086 0.001 0.995 0.001 0.995 13.625 0.369 0.365 8.0 0.764 0.06146 -0.088 0.001 0.995 0.001 0.995 12.430 0.409 0.366 8.5 0.776 0.06877 -0.091 0.001 0.995 0.001 0.995 11.281 0.496 0.367 9.0 0.783 0.07973 -0.093 0.001 0.996 0.001 0.996 9.816 0.820 0.369 9.5 0.784 0.08974 -0.095 0.001 0.996 0.001 0.996 8.735 -1.392 0.371 10.0 0.780 0.09959 -0.097 0.001 0.996 0.001 0.996 7.830 -0.096 0.375 10.5 0.771 0.11232 -0.100 0.001 0.996 0.001 0.996 6.861 0.053 0.379 11.0 0.756 0.12915 -0.102 0.001 0.995 0.001 0.995 5.856 0.107 0.385 11.5 0.738 0.14900 -0.104 0.000 0.995 0.001 0.995 4.955 0.136 0.391 12.0 0.716 0.13790 -0.107 0.001 0.995 0.002 0.995 5.191 0.153 0.399 12.5 0.691 0.14304 -0.109 0.001 0.995 0.002 0.995 4.830 0.162 0.408 13.0 0.663 0.16236 -0.111 0.001 0.995 0.002 0.995 4.085 0.168 0.418 13.5 0.634 0.18745 -0.114 0.001 0.995 0.002 0.995 3.384 0.172 0.429 14.0 0.604 0.20756 -0.116 0.001 0.995 0.002 0.995 2.910 0.174 0.442 14.5 0.573 0.21413 -0.118 0.001 0.996 0.002 0.996 2.677 0.175 0.456 15.0 0.542 0.23647 -0.121 0.001 0.996 0.002 0.996 2.294 0.175 0.472 Name = AG14 Mach = 0; Re = 75000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. S.U. S.L. L/D A.C. C.P. [¡] [-] [-] [-] [-] [-] [-] [-] [-] [-] [-] -15.0 -0.222 0.25787 0.011 1.000 0.002 1.000 0.004 -0.863 0.050 0.301 -14.5 -0.232 0.23854 0.009 1.000 0.002 1.000 0.005 -0.974 0.048 0.290 -14.0 -0.242 0.21829 0.007 1.000 0.002 1.000 0.004 -1.109 0.041 0.280 -13.5 -0.252 0.19067 0.005 1.000 0.002 1.000 0.004 -1.320 0.031 0.271 -13.0 -0.261 0.17374 0.003 1.000 0.002 1.000 0.004 -1.500 0.013 0.263 -12.5 -0.269 0.15714 0.001 1.000 0.002 1.000 0.004 -1.711 -0.017 0.255 -12.0 -0.276 0.15006 -0.001 1.000 0.002 1.000 0.004 -1.839 -0.070 0.247 -11.5 -0.282 0.13505 -0.003 1.000 0.002 1.000 0.004 -2.085 -0.184 0.240 -11.0 -0.285 0.12696 -0.005 1.000 0.002 1.000 0.004 -2.248 -0.501 0.233 -10.5 -0.287 0.11320 -0.007 1.000 0.002 1.000 0.004 -2.536 -4.140 0.226 -10.0 -0.286 0.10346 -0.009 1.000 0.002 1.000 0.003 -2.767 1.180 0.218 -9.5 -0.283 0.12401 -0.011 1.000 0.002 1.000 0.003 -2.279 0.640 0.211 -9.0 -0.276 0.11361 -0.013 1.000 0.002 1.000 0.003 -2.426 0.489 0.202 -8.5 -0.265 0.10678 -0.015 1.000 0.002 1.000 0.003 -2.483 0.424 0.192 -8.0 -0.251 0.09379 -0.017 1.000 0.001 1.000 0.003 -2.680 0.386 0.181 -7.5 -0.234 0.08243 -0.020 1.000 0.001 1.000 0.002 -2.839 0.360 0.166 -7.0 -0.213 0.07394 -0.022 1.000 0.001 1.000 0.002 -2.880 0.344 0.148 -6.5 -0.189 0.06101 -0.024 1.000 0.001 1.000 0.002 -3.096 0.332 0.124 -6.0 -0.161 0.05346 -0.026 1.000 0.002 1.000 0.003 -3.013 0.324 0.089 -5.5 -0.131 0.04606 -0.028 1.000 0.002 1.000 0.003 -2.848 0.319 0.036 -5.0 -0.099 0.04028 -0.030 1.000 0.002 1.000 0.003 -2.462 0.316 -0.055 -4.5 -0.065 0.03535 -0.032 1.000 0.002 1.000 0.003 -1.849 0.313 -0.246 -4.0 -0.030 0.03074 -0.035 1.000 0.002 1.000 0.003 -0.990 0.201 -0.887 -3.5 -0.154 0.02661 -0.037 1.000 0.002 1.000 0.003 -5.781 0.181 0.011 -3.0 -0.094 0.02338 -0.039 1.000 0.002 1.000 0.003 -4.017 0.286 -0.165 -2.5 -0.034 0.02057 -0.041 1.000 0.003 1.000 0.003 -1.658 0.287 -0.956 -2.0 0.025 0.01826 -0.043 1.000 0.003 1.000 0.005 1.382 0.344 1.965 -1.5 0.082 0.02841 -0.052 0.967 0.183 1.000 0.997 2.878 0.327 0.886 -1.0 0.139 0.01567 -0.052 0.940 0.995 1.000 0.995 8.886 0.251 0.624 -0.5 0.197 0.01693 -0.052 0.867 0.995 1.000 0.995 11.623 0.251 0.515 0.0 0.254 0.01840 -0.052 0.774 0.995 1.000 0.995 13.814 0.251 0.455 0.5 0.311 0.02009 -0.052 0.692 0.995 1.000 0.995 15.505 0.251 0.418 1.0 0.369 0.02147 -0.052 0.595 0.995 1.000 0.995 17.173 0.251 0.392 1.5 0.426 0.02360 -0.052 0.471 0.995 1.000 0.995 18.051 0.251 0.373 2.0 0.483 0.02540 -0.052 0.371 0.995 1.000 0.995 19.018 0.251 0.358 2.5 0.540 0.02627 -0.052 0.298 0.995 1.000 0.995 20.559 0.251 0.347 3.0 0.597 0.02736 -0.052 0.230 0.995 1.000 0.995 21.823 0.251 0.338 3.5 0.654 0.02846 -0.053 0.171 0.995 1.000 0.996 22.965 0.251 0.330 4.0 0.710 0.02927 -0.053 0.110 0.995 1.000 0.996 24.258 0.251 0.324 4.5 0.765 0.02972 -0.053 0.065 0.996 1.000 0.996 25.744 0.252 0.319 5.0 0.819 0.02982 -0.053 0.038 0.996 1.000 0.996 27.455 0.252 0.314 5.5 0.870 0.02975 -0.053 0.020 0.996 1.000 0.996 29.251 0.083 0.311 6.0 0.660 0.03602 -0.079 0.001 0.995 0.007 0.995 18.329 0.084 0.370 6.5 0.699 0.03889 -0.081 0.001 0.995 0.002 0.995 17.961 0.318 0.367 7.0 0.726 0.04379 -0.084 0.001 0.995 0.001 0.995 16.572 0.344 0.365 7.5 0.747 0.04943 -0.086 0.001 0.995 0.001 0.995 15.111 0.369 0.365 8.0 0.764 0.05508 -0.088 0.001 0.995 0.001 0.995 13.871 0.410 0.366 8.5 0.776 0.06289 -0.091 0.001 0.995 0.001 0.995 12.332 0.496 0.367 9.0 0.783 0.07002 -0.093 0.001 0.996 0.001 0.996 11.177 0.800 0.369 9.5 0.784 0.07822 -0.095 0.001 0.996 0.001 0.996 10.021 -1.259 0.371 10.0 0.780 0.08877 -0.097 0.001 0.996 0.001 0.996 8.781 -0.086 0.375 10.5 0.770 0.10323 -0.100 0.001 0.996 0.001 0.996 7.461 0.051 0.380 11.0 0.756 0.10934 -0.102 0.001 0.995 0.001 0.995 6.918 0.107 0.385 11.5 0.738 0.11277 -0.104 0.000 0.995 0.002 0.995 6.544 0.136 0.391 12.0 0.716 0.11655 -0.107 0.001 0.995 0.002 0.995 6.143 0.152 0.399 12.5 0.691 0.12859 -0.109 0.001 0.995 0.002 0.995 5.371 0.163 0.408 13.0 0.663 0.14491 -0.111 0.001 0.995 0.002 0.995 4.575 0.168 0.418 13.5 0.634 0.15585 -0.114 0.001 0.995 0.002 0.995 4.070 0.172 0.429 14.0 0.604 0.17008 -0.116 0.001 0.995 0.002 0.995 3.551 0.174 0.442 14.5 0.573 0.18784 -0.118 0.001 0.996 0.002 0.996 3.051 0.175 0.456 15.0 0.542 0.20461 -0.121 0.001 0.996 0.002 0.996 2.650 0.175 0.472 Name = AG14 Mach = 0; Re = 100000; T.U. = 1.0; T.L. = 1.0 Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0 ? Cl Cd Cm 0.25 T.U. T.L. S.U. S.L. L/D A.C. C.P. [¡] [-] [-] [-] [-] [-] [-] [-] [-] [-] [-] -15.0 -0.222 0.23287 0.011 1.000 0.002 1.000 0.005 -0.955 0.050 0.301 -14.5 -0.232 0.21233 0.009 1.000 0.002 1.000 0.005 -1.094 0.047 0.290 -14.0 -0.242 0.19671 0.007 1.000 0.002 1.000 0.005 -1.231 0.041 0.280 -13.5 -0.252 0.17313 0.005 1.000 0.002 1.000 0.005 -1.453 0.031 0.271 -13.0 -0.261 0.15940 0.003 1.000 0.002 1.000 0.004 -1.635 0.013 0.263 -12.5 -0.269 0.14462 0.001 1.000 0.002 1.000 0.004 -1.859 -0.017 0.255 -12.0 -0.276 0.13965 -0.001 1.000 0.002 1.000 0.004 -1.975 -0.071 0.247 -11.5 -0.282 0.12672 -0.003 1.000 0.002 1.000 0.004 -2.222 -0.185 0.240 -11.0 -0.285 0.11834 -0.005 1.000 0.002 1.000 0.004 -2.410 -0.492 0.233 -10.5 -0.287 0.10028 -0.007 1.000 0.002 1.000 0.004 -2.863 -4.248 0.226 -10.0 -0.286 0.09805 -0.009 1.000 0.002 1.000 0.004 -2.919 1.151 0.218 -9.5 -0.282 0.08884 -0.011 1.000 0.002 1.000 0.003 -3.180 0.639 0.211 -9.0 -0.275 0.08180 -0.013 1.000 0.002 1.000 0.003 -3.367 0.492 0.202 -8.5 -0.265 0.09415 -0.015 1.000 0.002 1.000 0.003 -2.816 0.425 0.192 -8.0 -0.251 0.08271 -0.017 1.000 0.001 1.000 0.003 -3.039 0.386 0.181 -7.5 -0.234 0.07353 -0.020 1.000 0.001 1.000 0.002 -3.183 0.360 0.166 -7.0 -0.213 0.06593 -0.022 1.000 0.001 1.000 0.002 -3.230 0.343 0.148 -6.5 -0.189 0.05888 -0.024 1.000 0.001 1.000 0.002 -3.203 0.332 0.124 -6.0 -0.161 0.04877 -0.026 1.000 0.002 1.000 0.003 -3.303 0.324 0.089 -5.5 -0.131 0.04351 -0.028 1.000 0.002 1.000 0.003 -3.011 0.319 0.036 -5.0 -0.099 0.03725 -0.030 1.000 0.002 1.000 0.003 -2.662 0.316 -0.055 -4.5 -0.065 0.03281 -0.032 1.000 0.002 1.000 0.003 -1.992 0.313 -0.246 -4.0 -0.030 0.02863 -0.035 1.000 0.002 1.000 0.003 -1.063 0.201 -0.887 -3.5 -0.154 0.02486 -0.037 1.000 0.002 1.000 0.003 -6.189 0.181 0.011 -3.0 -0.094 0.02206 -0.039 1.000 0.002 1.000 0.003 -4.257 0.286 -0.165 -2.5 -0.034 0.01935 -0.041 1.000 0.003 1.000 0.004 -1.763 0.287 -0.956 -2.0 0.025 0.01698 -0.043 1.000 0.003 1.000 0.005 1.486 0.344 1.965 -1.5 0.082 0.02746 -0.052 0.967 0.183 1.000 0.997 2.977 0.327 0.886 -1.0 0.139 0.01393 -0.052 0.940 0.995 1.000 0.995 9.999 0.251 0.624 -0.5 0.197 0.01499 -0.052 0.867 0.995 1.000 0.995 13.121 0.251 0.515 0.0 0.254 0.01691 -0.052 0.774 0.995 1.000 0.995 15.026 0.251 0.455 0.5 0.311 0.01838 -0.052 0.692 0.995 1.000 0.995 16.946 0.251 0.418 1.0 0.369 0.01984 -0.052 0.595 0.995 1.000 0.995 18.591 0.251 0.392 1.5 0.426 0.02201 -0.052 0.471 0.995 1.000 0.995 19.352 0.251 0.373 2.0 0.483 0.02388 -0.052 0.371 0.995 1.000 0.995 20.234 0.251 0.358 2.5 0.540 0.02490 -0.052 0.298 0.995 1.000 0.995 21.696 0.251 0.347 3.0 0.597 0.02563 -0.052 0.230 0.995 1.000 0.995 23.296 0.251 0.338 3.5 0.654 0.02682 -0.053 0.171 0.995 1.000 0.996 24.377 0.251 0.330 4.0 0.710 0.02770 -0.053 0.110 0.995 1.000 0.996 25.628 0.251 0.324 4.5 0.765 0.02817 -0.053 0.065 0.996 1.000 0.996 27.157 0.252 0.319 5.0 0.819 0.02883 -0.053 0.038 0.996 1.000 0.996 28.399 0.252 0.314 5.5 0.870 0.02878 -0.053 0.020 0.996 1.000 0.996 30.241 0.252 0.311 6.0 0.920 0.02867 -0.053 0.001 0.995 1.000 0.995 32.074 0.084 0.308 6.5 0.698 0.03711 -0.081 0.001 0.995 0.002 0.995 18.808 0.092 0.367 7.0 0.726 0.04118 -0.084 0.001 0.995 0.001 0.995 17.621 0.342 0.365 7.5 0.747 0.04624 -0.086 0.001 0.995 0.001 0.995 16.154 0.370 0.365 8.0 0.764 0.05265 -0.088 0.001 0.995 0.001 0.995 14.506 0.410 0.366 8.5 0.776 0.05799 -0.091 0.001 0.995 0.001 0.995 13.373 0.495 0.367 9.0 0.782 0.06595 -0.093 0.001 0.996 0.001 0.996 11.863 0.819 0.369 9.5 0.784 0.07336 -0.095 0.001 0.996 0.001 0.996 10.682 -1.282 0.371 10.0 0.779 0.08249 -0.097 0.001 0.996 0.001 0.996 9.448 -0.092 0.375 10.5 0.770 0.09225 -0.100 0.001 0.996 0.001 0.996 8.349 0.053 0.380 11.0 0.756 0.09021 -0.102 0.001 0.995 0.002 0.995 8.381 0.107 0.385 11.5 0.738 0.09986 -0.104 0.000 0.995 0.002 0.995 7.390 0.136 0.391 12.0 0.716 0.11034 -0.107 0.001 0.995 0.002 0.995 6.486 0.153 0.399 12.5 0.690 0.12067 -0.109 0.001 0.995 0.002 0.995 5.721 0.162 0.408 13.0 0.663 0.12662 -0.111 0.001 0.995 0.002 0.995 5.236 0.168 0.418 13.5 0.634 0.14553 -0.114 0.001 0.995 0.002 0.995 4.357 0.172 0.429 14.0 0.604 0.15720 -0.116 0.001 0.995 0.002 0.995 3.840 0.174 0.442 14.5 0.573 0.17259 -0.118 0.001 0.996 0.002 0.996 3.319 0.175 0.456 15.0 0.542 0.18585 -0.121 0.001 0.996 0.002 0.996 2.916 0.175 0.472