Name = AG26 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 -0.264 0.33032 -0.001 1.000 0.002 1.000 0.004 -0.800 -0.006 0.247 -14.5 -0.273 0.29183 -0.003 1.000 0.002 1.000 0.004 -0.935 -0.018 0.240 -14.0 -0.280 0.28400 -0.005 1.000 0.002 1.000 0.004 -0.987 -0.049 0.232 -13.5 -0.287 0.38264 -0.007 1.000 0.002 1.000 0.003 -0.751 -0.103 0.225 -13.0 -0.293 0.36766 -0.009 1.000 0.002 1.000 0.003 -0.796 -0.204 0.218 -12.5 -0.297 0.31727 -0.012 1.000 0.002 1.000 0.003 -0.935 -0.446 0.211 -12.0 -0.299 0.27680 -0.014 1.000 0.002 1.000 0.003 -1.080 -1.707 0.204 -11.5 -0.299 0.26608 -0.016 1.000 0.002 1.000 0.003 -1.124 2.334 0.197 -11.0 -0.297 0.23045 -0.018 1.000 0.002 1.000 0.003 -1.288 0.882 0.189 -10.5 -0.292 0.19716 -0.020 1.000 0.002 1.000 0.003 -1.481 0.587 0.180 -10.0 -0.284 0.19028 -0.023 1.000 0.002 1.000 0.003 -1.491 0.481 0.170 -9.5 -0.273 0.16281 -0.025 1.000 0.002 1.000 0.003 -1.675 0.426 0.159 -9.0 -0.258 0.14701 -0.027 1.000 0.001 1.000 0.003 -1.757 0.391 0.145 -8.5 -0.241 0.12586 -0.029 1.000 0.001 1.000 0.002 -1.913 0.368 0.128 -8.0 -0.220 0.11318 -0.032 1.000 0.001 1.000 0.002 -1.942 0.350 0.106 -7.5 -0.196 0.09745 -0.034 1.000 0.002 1.000 0.002 -2.008 0.340 0.077 -7.0 -0.169 0.08530 -0.036 1.000 0.002 1.000 0.002 -1.981 0.332 0.036 -6.5 -0.140 0.07406 -0.038 1.000 0.001 1.000 0.002 -1.885 0.325 -0.025 -6.0 -0.108 0.06491 -0.041 0.965 0.002 1.000 0.002 -1.661 0.320 -0.128 -5.5 -0.074 0.05702 -0.043 0.958 0.002 1.000 0.002 -1.301 0.317 -0.330 -5.0 -0.039 0.05003 -0.045 0.949 0.002 1.000 0.002 -0.787 0.315 -0.901 -4.5 -0.003 0.04433 -0.048 0.918 0.002 1.000 0.002 -0.076 0.207 -13.949 -4.0 -0.147 0.03914 -0.050 0.884 0.002 1.000 0.003 -3.752 0.193 -0.090 -3.5 -0.086 0.03455 -0.052 0.856 0.002 1.000 0.003 -2.482 0.288 -0.360 -3.0 -0.025 0.03144 -0.055 0.826 0.003 1.000 0.004 -0.791 0.288 -1.948 -2.5 0.036 0.02896 -0.057 0.794 0.004 1.000 0.006 1.227 0.364 1.853 -2.0 0.092 0.03625 -0.068 0.760 0.082 1.000 0.996 2.539 0.348 0.989 -1.5 0.150 0.03538 -0.068 0.726 0.318 1.000 0.996 4.244 0.253 0.704 -1.0 0.208 0.02722 -0.068 0.689 0.995 1.000 0.995 7.651 0.254 0.578 -0.5 0.266 0.02773 -0.069 0.657 0.995 1.000 0.995 9.604 0.254 0.508 0.0 0.324 0.02786 -0.069 0.623 0.995 1.000 0.995 11.637 0.254 0.462 0.5 0.382 0.02786 -0.069 0.579 0.995 1.000 0.995 13.716 0.254 0.431 1.0 0.440 0.02845 -0.069 0.539 0.995 1.000 0.995 15.465 0.254 0.407 1.5 0.498 0.02859 -0.069 0.507 0.995 1.000 0.995 17.410 0.254 0.390 2.0 0.556 0.02923 -0.070 0.466 0.995 1.000 0.995 19.007 0.254 0.375 2.5 0.613 0.02966 -0.070 0.412 0.995 1.000 0.995 20.670 0.254 0.364 3.0 0.671 0.03056 -0.070 0.348 0.995 1.000 0.995 21.944 0.254 0.355 3.5 0.728 0.03186 -0.070 0.258 0.995 1.000 0.995 22.842 0.254 0.347 4.0 0.785 0.03225 -0.071 0.195 0.995 1.000 0.995 24.332 0.254 0.340 4.5 0.841 0.03231 -0.071 0.149 0.995 1.000 0.995 26.035 0.254 0.334 5.0 0.896 0.03229 -0.071 0.081 0.995 1.000 0.995 27.762 0.305 0.329 5.5 0.921 0.03113 -0.075 0.047 0.996 0.944 0.996 29.575 0.112 0.332 6.0 0.682 0.05019 -0.101 0.026 0.996 0.189 0.996 13.578 0.079 0.398 6.5 0.774 0.04665 -0.100 0.002 0.996 0.004 0.996 16.591 0.265 0.380 7.0 0.808 0.05124 -0.103 0.001 0.996 0.002 0.996 15.761 0.330 0.377 7.5 0.834 0.05751 -0.105 0.001 0.996 0.001 0.996 14.497 0.351 0.376 8.0 0.856 0.06463 -0.108 0.001 0.996 0.001 0.996 13.239 0.375 0.376 8.5 0.873 0.07430 -0.110 0.001 0.995 0.001 0.995 11.749 0.416 0.376 9.0 0.885 0.08675 -0.112 0.000 0.996 0.001 0.996 10.203 0.501 0.377 9.5 0.892 0.09556 -0.115 0.000 0.996 0.001 0.996 9.338 0.785 0.379 10.0 0.894 0.11346 -0.117 0.000 0.996 0.001 0.996 7.881 -3.043 0.381 10.5 0.891 0.12265 -0.120 0.000 0.996 0.001 0.996 7.264 -0.149 0.384 11.0 0.882 0.14357 -0.122 0.000 0.996 0.001 0.996 6.143 0.029 0.389 11.5 0.869 0.16344 -0.125 0.000 0.996 0.001 0.996 5.315 0.093 0.394 12.0 0.851 0.18175 -0.127 0.000 0.996 0.001 0.996 4.680 0.128 0.399 12.5 0.828 0.17468 -0.130 0.001 0.996 0.001 0.996 4.743 0.146 0.406 13.0 0.803 0.19451 -0.132 0.001 0.996 0.001 0.996 4.129 0.158 0.414 13.5 0.775 0.21305 -0.135 0.001 0.995 0.001 0.995 3.639 0.165 0.424 14.0 0.745 0.23067 -0.137 0.001 0.995 0.001 0.995 3.231 0.170 0.434 14.5 0.714 0.24866 -0.139 0.001 0.995 0.001 0.995 2.872 0.173 0.445 15.0 0.682 0.27774 -0.142 0.001 0.995 0.001 0.995 2.455 0.174 0.458 Name = AG26 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 -0.264 0.25485 -0.001 1.000 0.002 1.000 0.004 -1.037 -0.006 0.247 -14.5 -0.273 0.22369 -0.003 1.000 0.002 1.000 0.004 -1.219 -0.018 0.240 -14.0 -0.280 0.21916 -0.005 1.000 0.002 1.000 0.004 -1.279 -0.050 0.232 -13.5 -0.287 0.19771 -0.007 1.000 0.002 1.000 0.004 -1.452 -0.102 0.225 -13.0 -0.293 0.25637 -0.009 1.000 0.002 1.000 0.003 -1.142 -0.205 0.218 -12.5 -0.297 0.17816 -0.012 1.000 0.002 1.000 0.003 -1.665 -0.458 0.211 -12.0 -0.299 0.15732 -0.014 1.000 0.002 1.000 0.003 -1.899 -1.620 0.204 -11.5 -0.299 0.18872 -0.016 1.000 0.002 1.000 0.003 -1.584 2.247 0.197 -11.0 -0.297 0.18260 -0.018 1.000 0.002 1.000 0.003 -1.624 0.860 0.189 -10.5 -0.292 0.15875 -0.020 1.000 0.002 1.000 0.003 -1.838 0.594 0.180 -10.0 -0.284 0.13758 -0.023 1.000 0.002 1.000 0.003 -2.062 0.485 0.170 -9.5 -0.273 0.12080 -0.025 1.000 0.002 1.000 0.003 -2.258 0.426 0.159 -9.0 -0.258 0.10893 -0.027 1.000 0.001 1.000 0.003 -2.371 0.391 0.145 -8.5 -0.241 0.09554 -0.029 1.000 0.001 1.000 0.002 -2.520 0.368 0.128 -8.0 -0.220 0.08594 -0.032 1.000 0.001 1.000 0.002 -2.557 0.350 0.106 -7.5 -0.195 0.07844 -0.034 1.000 0.002 1.000 0.002 -2.492 0.339 0.077 -7.0 -0.169 0.06952 -0.036 1.000 0.002 1.000 0.002 -2.428 0.332 0.036 -6.5 -0.139 0.06045 -0.038 1.000 0.001 1.000 0.002 -2.307 0.325 -0.026 -6.0 -0.108 0.05358 -0.041 0.965 0.002 1.000 0.002 -2.009 0.320 -0.128 -5.5 -0.074 0.04740 -0.043 0.958 0.002 1.000 0.003 -1.561 0.318 -0.331 -5.0 -0.039 0.04090 -0.045 0.949 0.002 1.000 0.002 -0.962 0.316 -0.901 -4.5 -0.003 0.03665 -0.048 0.918 0.002 1.000 0.002 -0.092 0.207 -13.949 -4.0 -0.147 0.03260 -0.050 0.884 0.002 1.000 0.003 -4.505 0.194 -0.090 -3.5 -0.086 0.02965 -0.052 0.856 0.002 1.000 0.003 -2.892 0.288 -0.360 -3.0 -0.025 0.02694 -0.055 0.826 0.003 1.000 0.004 -0.923 0.288 -1.948 -2.5 0.036 0.02475 -0.057 0.794 0.004 1.000 0.007 1.435 0.364 1.853 -2.0 0.092 0.03198 -0.068 0.760 0.082 1.000 0.996 2.878 0.348 0.989 -1.5 0.150 0.03017 -0.068 0.726 0.318 1.000 0.996 4.977 0.253 0.704 -1.0 0.208 0.02137 -0.068 0.689 0.995 1.000 0.995 9.747 0.254 0.578 -0.5 0.266 0.02207 -0.069 0.657 0.995 1.000 0.995 12.069 0.254 0.508 0.0 0.324 0.02226 -0.069 0.623 0.995 1.000 0.995 14.563 0.254 0.462 0.5 0.382 0.02301 -0.069 0.579 0.995 1.000 0.995 16.606 0.254 0.431 1.0 0.440 0.02345 -0.069 0.539 0.995 1.000 0.995 18.762 0.254 0.407 1.5 0.498 0.02395 -0.069 0.507 0.995 1.000 0.995 20.787 0.254 0.390 2.0 0.556 0.02463 -0.070 0.466 0.995 1.000 0.995 22.555 0.254 0.375 2.5 0.613 0.02535 -0.070 0.412 0.995 1.000 0.995 24.183 0.254 0.364 3.0 0.671 0.02644 -0.070 0.348 0.995 1.000 0.995 25.357 0.254 0.355 3.5 0.728 0.02782 -0.070 0.258 0.995 1.000 0.995 26.165 0.254 0.347 4.0 0.785 0.02847 -0.071 0.195 0.995 1.000 0.995 27.566 0.254 0.340 4.5 0.841 0.02863 -0.071 0.149 0.995 1.000 0.995 29.387 0.254 0.334 5.0 0.896 0.02956 -0.071 0.081 0.995 1.000 0.995 30.324 0.255 0.329 5.5 0.950 0.02927 -0.071 0.047 0.996 1.000 0.996 32.445 0.255 0.325 6.0 1.001 0.02870 -0.072 0.026 0.996 1.000 0.996 34.878 0.090 0.322 6.5 0.768 0.04111 -0.100 0.002 0.996 0.007 0.996 18.685 0.090 0.381 7.0 0.807 0.04398 -0.103 0.001 0.996 0.002 0.996 18.352 0.323 0.377 7.5 0.833 0.04923 -0.105 0.001 0.996 0.001 0.996 16.924 0.350 0.376 8.0 0.856 0.05380 -0.108 0.001 0.996 0.001 0.996 15.904 0.373 0.376 8.5 0.873 0.06100 -0.110 0.001 0.995 0.001 0.995 14.310 0.416 0.376 9.0 0.885 0.06991 -0.112 0.000 0.996 0.001 0.996 12.660 0.505 0.377 9.5 0.892 0.07879 -0.115 0.000 0.996 0.001 0.996 11.322 0.785 0.379 10.0 0.894 0.08688 -0.117 0.000 0.996 0.001 0.996 10.292 -2.555 0.381 10.5 0.890 0.10338 -0.120 0.000 0.996 0.001 0.996 8.612 -0.149 0.385 11.0 0.882 0.10943 -0.122 0.000 0.996 0.001 0.996 8.059 0.026 0.389 11.5 0.868 0.12869 -0.125 0.000 0.996 0.001 0.996 6.748 0.094 0.394 12.0 0.850 0.14104 -0.127 0.000 0.996 0.001 0.996 6.030 0.127 0.400 12.5 0.828 0.13202 -0.130 0.001 0.996 0.001 0.996 6.275 0.146 0.406 13.0 0.803 0.14505 -0.132 0.001 0.996 0.001 0.996 5.537 0.158 0.414 13.5 0.775 0.17037 -0.135 0.001 0.995 0.001 0.995 4.549 0.165 0.424 14.0 0.745 0.18435 -0.137 0.001 0.995 0.001 0.995 4.042 0.170 0.434 14.5 0.714 0.19784 -0.139 0.001 0.995 0.001 0.995 3.608 0.173 0.445 15.0 0.681 0.21640 -0.142 0.001 0.995 0.001 0.995 3.149 0.174 0.458 Name = AG26 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 -0.264 0.20583 -0.001 1.000 0.002 1.000 0.004 -1.284 -0.006 0.247 -14.5 -0.273 0.19451 -0.003 1.000 0.002 1.000 0.004 -1.402 -0.018 0.240 -14.0 -0.280 0.19196 -0.005 1.000 0.002 1.000 0.004 -1.460 -0.050 0.232 -13.5 -0.287 0.17556 -0.007 1.000 0.002 1.000 0.004 -1.635 -0.103 0.225 -13.0 -0.293 0.15809 -0.009 1.000 0.002 1.000 0.004 -1.851 -0.203 0.218 -12.5 -0.297 0.14805 -0.012 1.000 0.002 1.000 0.003 -2.004 -0.461 0.211 -12.0 -0.299 0.14109 -0.014 1.000 0.002 1.000 0.004 -2.117 -1.729 0.204 -11.5 -0.299 0.12715 -0.016 1.000 0.002 1.000 0.003 -2.350 2.374 0.197 -11.0 -0.297 0.15005 -0.018 1.000 0.002 1.000 0.003 -1.977 0.874 0.189 -10.5 -0.292 0.13277 -0.020 1.000 0.002 1.000 0.003 -2.197 0.586 0.180 -10.0 -0.283 0.12368 -0.023 1.000 0.002 1.000 0.003 -2.291 0.481 0.170 -9.5 -0.272 0.10981 -0.025 1.000 0.002 1.000 0.003 -2.481 0.426 0.159 -9.0 -0.258 0.09923 -0.027 1.000 0.001 1.000 0.003 -2.599 0.391 0.145 -8.5 -0.240 0.08785 -0.029 1.000 0.001 1.000 0.003 -2.737 0.368 0.128 -8.0 -0.219 0.07922 -0.032 1.000 0.001 1.000 0.003 -2.770 0.351 0.106 -7.5 -0.195 0.06778 -0.034 1.000 0.002 1.000 0.002 -2.884 0.340 0.077 -7.0 -0.169 0.06061 -0.036 1.000 0.002 1.000 0.002 -2.784 0.331 0.036 -6.5 -0.139 0.05474 -0.038 1.000 0.001 1.000 0.002 -2.544 0.325 -0.026 -6.0 -0.108 0.04758 -0.041 0.965 0.002 1.000 0.002 -2.262 0.320 -0.128 -5.5 -0.074 0.04237 -0.043 0.958 0.002 1.000 0.003 -1.746 0.317 -0.331 -5.0 -0.039 0.03784 -0.045 0.949 0.002 1.000 0.002 -1.034 0.316 -0.908 -4.5 -0.003 0.03354 -0.048 0.918 0.002 1.000 0.002 -0.097 0.207 -14.446 -4.0 -0.147 0.02999 -0.050 0.884 0.002 1.000 0.003 -4.898 0.194 -0.090 -3.5 -0.086 0.02723 -0.052 0.856 0.002 1.000 0.003 -3.149 0.288 -0.360 -3.0 -0.025 0.02493 -0.055 0.826 0.003 1.000 0.004 -0.997 0.288 -1.948 -2.5 0.036 0.02303 -0.057 0.794 0.004 1.000 0.007 1.543 0.365 1.853 -2.0 0.092 0.03037 -0.068 0.760 0.082 1.000 0.997 3.031 0.348 0.989 -1.5 0.150 0.02813 -0.068 0.726 0.318 1.000 0.997 5.337 0.253 0.704 -1.0 0.208 0.01912 -0.068 0.689 0.995 1.000 0.995 10.893 0.254 0.578 -0.5 0.266 0.01947 -0.069 0.657 0.995 1.000 0.995 13.675 0.254 0.508 0.0 0.324 0.02007 -0.069 0.623 0.995 1.000 0.995 16.155 0.254 0.462 0.5 0.382 0.02054 -0.069 0.579 0.995 1.000 0.995 18.604 0.254 0.431 1.0 0.440 0.02136 -0.069 0.539 0.995 1.000 0.995 20.600 0.254 0.407 1.5 0.498 0.02187 -0.069 0.507 0.995 1.000 0.995 22.759 0.254 0.390 2.0 0.556 0.02225 -0.070 0.466 0.995 1.000 0.995 24.963 0.254 0.375 2.5 0.613 0.02333 -0.070 0.412 0.995 1.000 0.995 26.278 0.254 0.364 3.0 0.671 0.02416 -0.070 0.348 0.995 1.000 0.995 27.749 0.254 0.355 3.5 0.728 0.02535 -0.070 0.258 0.995 1.000 0.995 28.709 0.254 0.347 4.0 0.785 0.02613 -0.071 0.195 0.995 1.000 0.995 30.034 0.254 0.340 4.5 0.841 0.02680 -0.071 0.149 0.995 1.000 0.995 31.384 0.254 0.334 5.0 0.896 0.02752 -0.071 0.081 0.995 1.000 0.995 32.572 0.255 0.329 5.5 0.950 0.02790 -0.071 0.047 0.996 1.000 0.996 34.041 0.255 0.325 6.0 1.001 0.02779 -0.072 0.026 0.996 1.000 0.996 36.026 0.255 0.322 6.5 1.050 0.02715 -0.072 0.002 0.996 1.000 0.996 38.682 0.090 0.318 7.0 0.806 0.04080 -0.103 0.001 0.996 0.002 0.996 19.765 0.097 0.377 7.5 0.833 0.04480 -0.105 0.001 0.996 0.001 0.996 18.599 0.350 0.376 8.0 0.855 0.05010 -0.108 0.001 0.996 0.001 0.996 17.066 0.373 0.376 8.5 0.873 0.05514 -0.110 0.001 0.995 0.001 0.995 15.829 0.413 0.376 9.0 0.885 0.06252 -0.112 0.000 0.996 0.001 0.996 14.156 0.510 0.377 9.5 0.892 0.07063 -0.115 0.000 0.996 0.001 0.996 12.626 0.823 0.379 10.0 0.894 0.08129 -0.117 0.000 0.996 0.001 0.996 10.992 -3.147 0.381 10.5 0.890 0.08933 -0.120 0.000 0.996 0.001 0.996 9.966 -0.150 0.385 11.0 0.881 0.10107 -0.122 0.000 0.996 0.001 0.996 8.720 0.026 0.389 11.5 0.868 0.10962 -0.125 0.000 0.996 0.001 0.996 7.922 0.092 0.394 12.0 0.850 0.12349 -0.127 0.000 0.996 0.001 0.996 6.885 0.128 0.400 12.5 0.828 0.12091 -0.130 0.001 0.996 0.001 0.996 6.848 0.146 0.407 13.0 0.803 0.13271 -0.132 0.001 0.996 0.001 0.996 6.049 0.157 0.415 13.5 0.775 0.14167 -0.135 0.001 0.995 0.001 0.995 5.470 0.165 0.424 14.0 0.745 0.15332 -0.137 0.001 0.995 0.001 0.995 4.860 0.170 0.434 14.5 0.713 0.17702 -0.139 0.001 0.995 0.002 0.995 4.030 0.173 0.445 15.0 0.681 0.19056 -0.142 0.001 0.995 0.002 0.995 3.575 0.174 0.458 Name = AG26 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 -0.264 0.18946 -0.001 1.000 0.002 1.000 0.005 -1.395 -0.007 0.247 -14.5 -0.273 0.17738 -0.003 1.000 0.002 1.000 0.005 -1.536 -0.018 0.240 -14.0 -0.280 0.16334 -0.005 1.000 0.002 1.000 0.004 -1.716 -0.050 0.232 -13.5 -0.287 0.15137 -0.007 1.000 0.002 1.000 0.004 -1.896 -0.104 0.225 -13.0 -0.292 0.14837 -0.009 1.000 0.002 1.000 0.004 -1.971 -0.206 0.218 -12.5 -0.297 0.13993 -0.011 1.000 0.002 1.000 0.004 -2.119 -0.452 0.211 -12.0 -0.299 0.12266 -0.014 1.000 0.002 1.000 0.004 -2.435 -1.640 0.204 -11.5 -0.299 0.11202 -0.016 1.000 0.002 1.000 0.003 -2.668 2.225 0.197 -11.0 -0.296 0.10963 -0.018 1.000 0.002 1.000 0.003 -2.704 0.852 0.189 -10.5 -0.291 0.12561 -0.020 1.000 0.002 1.000 0.003 -2.321 0.591 0.180 -10.0 -0.283 0.10809 -0.023 1.000 0.002 1.000 0.003 -2.622 0.485 0.170 -9.5 -0.272 0.09714 -0.025 1.000 0.002 1.000 0.003 -2.804 0.426 0.159 -9.0 -0.258 0.08777 -0.027 1.000 0.001 1.000 0.003 -2.939 0.391 0.145 -8.5 -0.240 0.07862 -0.029 1.000 0.001 1.000 0.003 -3.059 0.368 0.128 -8.0 -0.219 0.07092 -0.032 1.000 0.001 1.000 0.003 -3.095 0.350 0.106 -7.5 -0.195 0.06354 -0.034 1.000 0.002 1.000 0.003 -3.073 0.340 0.077 -7.0 -0.169 0.05538 -0.036 1.000 0.002 1.000 0.002 -3.047 0.332 0.036 -6.5 -0.139 0.05000 -0.038 1.000 0.001 1.000 0.002 -2.785 0.325 -0.026 -6.0 -0.107 0.04507 -0.041 0.965 0.002 1.000 0.003 -2.384 0.320 -0.129 -5.5 -0.074 0.03925 -0.043 0.958 0.002 1.000 0.003 -1.885 0.318 -0.331 -5.0 -0.039 0.03530 -0.045 0.949 0.002 1.000 0.002 -1.109 0.316 -0.908 -4.5 -0.003 0.03158 -0.048 0.918 0.002 1.000 0.002 -0.103 0.207 -14.446 -4.0 -0.147 0.02820 -0.050 0.884 0.002 1.000 0.003 -5.208 0.194 -0.090 -3.5 -0.086 0.02565 -0.052 0.856 0.002 1.000 0.003 -3.343 0.288 -0.360 -3.0 -0.025 0.02371 -0.055 0.826 0.003 1.000 0.004 -1.048 0.288 -1.948 -2.5 0.036 0.02201 -0.057 0.794 0.004 1.000 0.008 1.614 0.365 1.853 -2.0 0.092 0.02942 -0.068 0.760 0.082 1.000 0.997 3.129 0.348 0.989 -1.5 0.150 0.02686 -0.068 0.726 0.318 1.000 0.997 5.591 0.253 0.704 -1.0 0.208 0.01746 -0.068 0.689 0.995 1.000 0.995 11.928 0.254 0.578 -0.5 0.266 0.01797 -0.069 0.657 0.995 1.000 0.995 14.815 0.254 0.508 0.0 0.324 0.01860 -0.069 0.623 0.995 1.000 0.995 17.428 0.254 0.462 0.5 0.382 0.01923 -0.069 0.579 0.995 1.000 0.995 19.872 0.254 0.431 1.0 0.440 0.01977 -0.069 0.539 0.995 1.000 0.995 22.257 0.254 0.407 1.5 0.498 0.02029 -0.069 0.507 0.995 1.000 0.995 24.534 0.254 0.390 2.0 0.556 0.02106 -0.070 0.466 0.995 1.000 0.995 26.377 0.254 0.375 2.5 0.613 0.02177 -0.070 0.412 0.995 1.000 0.995 28.158 0.254 0.364 3.0 0.671 0.02268 -0.070 0.348 0.995 1.000 0.995 29.567 0.254 0.355 3.5 0.728 0.02400 -0.070 0.258 0.995 1.000 0.995 30.321 0.254 0.347 4.0 0.785 0.02486 -0.071 0.195 0.995 1.000 0.995 31.572 0.254 0.340 4.5 0.841 0.02558 -0.071 0.149 0.995 1.000 0.995 32.882 0.254 0.334 5.0 0.896 0.02643 -0.071 0.081 0.995 1.000 0.995 33.917 0.255 0.329 5.5 0.950 0.02647 -0.071 0.047 0.996 1.000 0.996 35.879 0.255 0.325 6.0 1.001 0.02640 -0.072 0.026 0.996 1.000 0.996 37.926 0.255 0.322 6.5 1.050 0.02657 -0.072 0.002 0.996 1.000 0.996 39.514 0.091 0.318 7.0 0.806 0.03892 -0.103 0.001 0.996 0.002 0.996 20.707 0.097 0.377 7.5 0.833 0.04282 -0.105 0.001 0.996 0.002 0.996 19.444 0.349 0.376 8.0 0.855 0.04703 -0.108 0.001 0.996 0.001 0.996 18.181 0.372 0.376 8.5 0.873 0.05302 -0.110 0.001 0.995 0.001 0.995 16.458 0.415 0.376 9.0 0.885 0.05965 -0.112 0.000 0.996 0.001 0.996 14.831 0.505 0.377 9.5 0.892 0.06498 -0.115 0.000 0.996 0.001 0.996 13.724 0.802 0.379 10.0 0.894 0.07392 -0.117 0.000 0.996 0.001 0.996 12.088 -3.147 0.381 10.5 0.890 0.08113 -0.120 0.000 0.996 0.001 0.996 10.973 -0.150 0.385 11.0 0.881 0.09065 -0.122 0.000 0.996 0.001 0.996 9.722 0.029 0.389 11.5 0.868 0.10155 -0.125 0.000 0.996 0.001 0.996 8.549 0.094 0.394 12.0 0.850 0.10434 -0.127 0.000 0.996 0.001 0.996 8.145 0.127 0.400 12.5 0.828 0.10805 -0.130 0.001 0.996 0.001 0.996 7.663 0.145 0.407 13.0 0.803 0.11771 -0.132 0.001 0.996 0.001 0.996 6.820 0.158 0.415 13.5 0.775 0.13318 -0.135 0.001 0.995 0.002 0.995 5.817 0.165 0.424 14.0 0.745 0.14406 -0.137 0.001 0.995 0.002 0.995 5.170 0.170 0.434 14.5 0.713 0.15420 -0.139 0.001 0.995 0.002 0.995 4.627 0.173 0.445 15.0 0.681 0.17574 -0.142 0.001 0.995 0.002 0.995 3.875 0.174 0.458