Name = AG03 (flat aft bottom) 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 -0.192 0.34032 0.032 1.000 0.003 1.000 0.004 -0.565 0.038 0.417 -14.5 -0.202 0.31986 0.030 1.000 0.002 1.000 0.004 -0.632 0.040 0.398 -14.0 -0.212 0.29083 0.028 1.000 0.002 1.000 0.004 -0.729 0.041 0.382 -13.5 -0.222 0.28104 0.026 1.000 0.002 1.000 0.004 -0.790 0.040 0.366 -13.0 -0.232 0.24726 0.024 1.000 0.002 1.000 0.004 -0.939 0.035 0.352 -12.5 -0.242 0.22153 0.022 1.000 0.002 1.000 0.004 -1.092 0.025 0.339 -12.0 -0.251 0.20134 0.019 1.000 0.002 1.000 0.004 -1.247 0.008 0.327 -11.5 -0.260 0.19400 0.017 1.000 0.002 1.000 0.004 -1.338 -0.022 0.317 -11.0 -0.267 0.17358 0.015 1.000 0.002 1.000 0.003 -1.538 -0.076 0.307 -10.5 -0.273 0.15750 0.013 1.000 0.002 1.000 0.003 -1.732 -0.186 0.297 -10.0 -0.277 0.14045 0.011 1.000 0.002 1.000 0.003 -1.972 -0.489 0.289 -9.5 -0.279 0.17696 0.009 1.000 0.002 1.000 0.003 -1.576 -4.715 0.281 -9.0 -0.278 0.15617 0.006 1.000 0.002 1.000 0.003 -1.779 1.136 0.273 -8.5 -0.274 0.13941 0.004 1.000 0.002 1.000 0.003 -1.964 0.648 0.265 -8.0 -0.267 0.12234 0.002 1.000 0.002 1.000 0.003 -2.179 0.496 0.257 -7.5 -0.255 0.10600 -0.000 1.000 0.002 1.000 0.003 -2.410 0.423 0.248 -7.0 -0.241 0.09765 -0.003 1.000 0.002 1.000 0.003 -2.463 0.386 0.239 -6.5 -0.222 0.08488 -0.005 1.000 0.002 1.000 0.002 -2.616 0.363 0.228 -6.0 -0.200 0.07354 -0.007 1.000 0.001 1.000 0.002 -2.721 0.346 0.214 -5.5 -0.174 0.06512 -0.010 1.000 0.001 1.000 0.002 -2.678 0.335 0.195 -5.0 -0.146 0.05549 -0.012 1.000 0.001 1.000 0.002 -2.630 0.327 0.169 -4.5 -0.115 0.04855 -0.014 1.000 0.001 1.000 0.002 -2.359 0.322 0.127 -4.0 -0.081 0.04217 -0.016 1.000 0.001 1.000 0.002 -1.930 0.319 0.048 -3.5 -0.047 0.03769 -0.019 0.917 0.001 1.000 0.002 -1.236 0.316 -0.154 -3.0 -0.011 0.03332 -0.021 0.892 0.001 1.000 0.002 -0.318 0.131 -1.745 -2.5 -0.086 0.02982 -0.024 0.867 0.001 1.000 0.002 -2.887 -0.051 -0.023 -2.0 -0.026 0.02665 -0.026 0.840 0.001 1.000 0.001 -0.986 0.290 -0.734 -1.5 0.033 0.02396 -0.028 0.806 0.002 1.000 0.003 1.383 0.328 1.102 -1.0 0.090 0.02630 -0.035 0.753 0.995 1.000 0.996 3.432 0.310 0.637 -0.5 0.148 0.02695 -0.035 0.688 0.995 1.000 0.996 5.503 0.254 0.487 0.0 0.206 0.02739 -0.035 0.636 0.996 1.000 0.996 7.530 0.254 0.422 0.5 0.264 0.02789 -0.036 0.584 0.996 1.000 0.996 9.469 0.254 0.385 1.0 0.322 0.02827 -0.036 0.539 0.996 1.000 0.996 11.387 0.254 0.362 1.5 0.380 0.02898 -0.036 0.488 0.996 1.000 0.996 13.102 0.254 0.345 2.0 0.437 0.02951 -0.036 0.422 0.996 1.000 0.996 14.823 0.255 0.333 2.5 0.495 0.03024 -0.037 0.340 0.996 1.000 0.996 16.368 0.255 0.324 3.0 0.552 0.03122 -0.037 0.270 0.996 1.000 0.996 17.693 0.255 0.317 3.5 0.610 0.03102 -0.037 0.210 0.995 1.000 0.996 19.649 0.255 0.311 4.0 0.667 0.03106 -0.038 0.158 0.995 1.000 0.996 21.461 0.255 0.306 4.5 0.723 0.03076 -0.038 0.115 0.995 1.000 0.996 23.512 0.267 0.302 5.0 0.771 0.02951 -0.039 0.075 0.995 0.981 0.996 26.125 0.411 0.301 5.5 0.778 0.02979 -0.047 0.035 0.996 0.876 0.996 26.106 0.106 0.310 6.0 0.584 0.04940 -0.066 0.024 0.996 0.059 0.996 11.820 0.103 0.363 6.5 0.631 0.05160 -0.068 0.014 0.995 0.029 0.996 12.238 0.294 0.358 7.0 0.676 0.05412 -0.070 0.006 0.995 0.013 0.996 12.488 0.298 0.354 7.5 0.721 0.05653 -0.072 0.001 0.995 0.002 0.996 12.756 0.314 0.351 8.0 0.748 0.06348 -0.075 0.000 0.995 0.001 0.996 11.790 0.355 0.350 8.5 0.769 0.07310 -0.077 0.000 0.995 0.001 0.996 10.514 0.393 0.351 9.0 0.784 0.08457 -0.080 0.000 0.996 0.000 0.997 9.265 0.457 0.352 9.5 0.793 0.09267 -0.083 0.000 0.996 0.000 0.997 8.557 0.651 0.354 10.0 0.796 0.10709 -0.085 0.000 0.996 0.000 0.997 7.435 8.752 0.357 10.5 0.794 0.12076 -0.088 0.000 0.996 0.001 0.997 6.571 -0.275 0.360 11.0 0.787 0.13127 -0.090 0.000 0.996 0.001 0.997 5.992 -0.010 0.365 11.5 0.774 0.15451 -0.093 0.000 0.995 0.001 0.996 5.009 0.074 0.370 12.0 0.758 0.17196 -0.095 0.000 0.995 0.001 0.996 4.406 0.115 0.376 12.5 0.736 0.19345 -0.098 0.000 0.995 0.001 0.996 3.805 0.138 0.383 13.0 0.712 0.21036 -0.100 0.000 0.995 0.001 0.996 3.384 0.150 0.391 13.5 0.685 0.24075 -0.103 0.000 0.996 0.001 0.997 2.845 0.159 0.400 14.0 0.656 0.26993 -0.105 0.000 0.996 0.001 0.997 2.430 0.164 0.411 14.5 0.626 0.29464 -0.108 0.000 0.996 0.001 0.997 2.123 0.170 0.423 15.0 0.592 0.34486 -0.111 0.000 0.996 0.001 0.997 1.716 0.174 0.437 Name = AG03 (flat aft bottom) 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 -0.192 0.26694 0.032 1.000 0.003 1.000 0.005 -0.720 0.037 0.417 -14.5 -0.202 0.23770 0.030 1.000 0.002 1.000 0.004 -0.850 0.039 0.398 -14.0 -0.212 0.21958 0.028 1.000 0.002 1.000 0.004 -0.966 0.041 0.382 -13.5 -0.222 0.21310 0.026 1.000 0.002 1.000 0.004 -1.042 0.040 0.366 -13.0 -0.232 0.18871 0.024 1.000 0.002 1.000 0.004 -1.230 0.035 0.352 -12.5 -0.242 0.17172 0.022 1.000 0.002 1.000 0.004 -1.408 0.025 0.339 -12.0 -0.251 0.15562 0.019 1.000 0.002 1.000 0.004 -1.613 0.008 0.327 -11.5 -0.260 0.14200 0.017 1.000 0.002 1.000 0.004 -1.828 -0.022 0.317 -11.0 -0.267 0.13691 0.015 1.000 0.002 1.000 0.004 -1.949 -0.077 0.307 -10.5 -0.273 0.12391 0.013 1.000 0.002 1.000 0.004 -2.201 -0.187 0.298 -10.0 -0.277 0.11213 0.011 1.000 0.002 1.000 0.003 -2.469 -0.491 0.289 -9.5 -0.279 0.10187 0.009 1.000 0.002 1.000 0.003 -2.736 -4.826 0.281 -9.0 -0.278 0.09201 0.006 1.000 0.002 1.000 0.003 -3.019 1.155 0.273 -8.5 -0.274 0.10363 0.004 1.000 0.002 1.000 0.003 -2.642 0.652 0.265 -8.0 -0.267 0.09255 0.002 1.000 0.002 1.000 0.003 -2.881 0.493 0.257 -7.5 -0.255 0.08627 -0.000 1.000 0.002 1.000 0.003 -2.959 0.423 0.249 -7.0 -0.241 0.07474 -0.003 1.000 0.002 1.000 0.003 -3.218 0.387 0.239 -6.5 -0.222 0.06599 -0.005 1.000 0.002 1.000 0.002 -3.365 0.363 0.228 -6.0 -0.200 0.05804 -0.007 1.000 0.001 1.000 0.002 -3.448 0.346 0.214 -5.5 -0.174 0.05146 -0.010 1.000 0.001 1.000 0.002 -3.390 0.334 0.195 -5.0 -0.146 0.04632 -0.012 1.000 0.001 1.000 0.002 -3.146 0.327 0.169 -4.5 -0.114 0.03947 -0.014 1.000 0.001 1.000 0.002 -2.899 0.322 0.127 -4.0 -0.081 0.03489 -0.016 1.000 0.001 1.000 0.002 -2.329 0.319 0.047 -3.5 -0.046 0.03144 -0.019 0.917 0.001 1.000 0.002 -1.477 0.316 -0.155 -3.0 -0.010 0.02800 -0.021 0.892 0.001 1.000 0.002 -0.373 0.131 -1.773 -2.5 -0.086 0.02500 -0.024 0.867 0.001 1.000 0.002 -3.443 -0.049 -0.023 -2.0 -0.026 0.02212 -0.026 0.840 0.001 1.000 0.001 -1.188 0.290 -0.734 -1.5 0.033 0.02018 -0.028 0.806 0.002 1.000 0.003 1.643 0.328 1.102 -1.0 0.090 0.02031 -0.035 0.753 0.995 1.000 0.996 4.446 0.310 0.637 -0.5 0.148 0.02148 -0.035 0.688 0.995 1.000 0.996 6.905 0.254 0.487 0.0 0.206 0.02230 -0.035 0.636 0.996 1.000 0.996 9.249 0.254 0.422 0.5 0.264 0.02269 -0.036 0.584 0.996 1.000 0.996 11.641 0.254 0.385 1.0 0.322 0.02314 -0.036 0.539 0.996 1.000 0.996 13.914 0.254 0.362 1.5 0.380 0.02387 -0.036 0.488 0.996 1.000 0.996 15.907 0.254 0.345 2.0 0.437 0.02493 -0.036 0.422 0.996 1.000 0.996 17.546 0.255 0.333 2.5 0.495 0.02598 -0.037 0.340 0.996 1.000 0.996 19.053 0.255 0.324 3.0 0.552 0.02660 -0.037 0.270 0.996 1.000 0.996 20.768 0.255 0.317 3.5 0.610 0.02726 -0.037 0.210 0.995 1.000 0.996 22.363 0.255 0.311 4.0 0.667 0.02745 -0.038 0.158 0.995 1.000 0.996 24.285 0.255 0.306 4.5 0.723 0.02809 -0.038 0.115 0.995 1.000 0.996 25.746 0.255 0.302 5.0 0.779 0.02833 -0.038 0.075 0.995 1.000 0.996 27.503 0.256 0.299 5.5 0.834 0.02790 -0.038 0.035 0.996 1.000 0.996 29.907 0.256 0.296 6.0 0.888 0.02662 -0.039 0.024 0.996 1.000 0.996 33.351 0.111 0.294 6.5 0.611 0.04620 -0.069 0.014 0.995 0.091 0.996 13.217 0.106 0.364 7.0 0.668 0.04747 -0.071 0.006 0.995 0.021 0.996 14.068 0.278 0.356 7.5 0.719 0.04859 -0.072 0.001 0.995 0.003 0.996 14.799 0.305 0.351 8.0 0.748 0.05367 -0.075 0.000 0.995 0.001 0.996 13.936 0.350 0.350 8.5 0.769 0.05981 -0.077 0.000 0.995 0.001 0.996 12.851 0.391 0.351 9.0 0.784 0.06832 -0.080 0.000 0.996 0.000 0.997 11.469 0.461 0.352 9.5 0.793 0.07836 -0.083 0.000 0.996 0.000 0.997 10.114 0.666 0.354 10.0 0.796 0.08700 -0.085 0.000 0.996 0.001 0.997 9.146 5.244 0.357 10.5 0.794 0.09435 -0.088 0.000 0.996 0.001 0.997 8.411 -0.277 0.360 11.0 0.786 0.10839 -0.090 0.000 0.996 0.001 0.997 7.252 -0.010 0.365 11.5 0.774 0.11730 -0.093 0.000 0.995 0.001 0.996 6.598 0.074 0.370 12.0 0.757 0.13811 -0.095 0.000 0.995 0.001 0.996 5.483 0.116 0.376 12.5 0.736 0.15221 -0.098 0.000 0.995 0.001 0.996 4.834 0.138 0.383 13.0 0.712 0.16410 -0.100 0.000 0.995 0.001 0.996 4.336 0.150 0.391 13.5 0.685 0.17676 -0.103 0.000 0.996 0.001 0.997 3.873 0.159 0.400 14.0 0.656 0.20975 -0.105 0.000 0.996 0.001 0.997 3.126 0.164 0.411 14.5 0.625 0.22719 -0.108 0.000 0.996 0.001 0.997 2.752 0.170 0.423 15.0 0.591 0.23220 -0.111 0.000 0.996 0.001 0.997 2.547 0.174 0.437 Name = AG03 (flat aft bottom) 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 -0.192 0.22402 0.032 1.000 0.003 1.000 0.005 -0.858 0.038 0.417 -14.5 -0.202 0.21273 0.030 1.000 0.002 1.000 0.005 -0.949 0.039 0.399 -14.0 -0.212 0.19887 0.028 1.000 0.002 1.000 0.005 -1.066 0.041 0.382 -13.5 -0.222 0.18383 0.026 1.000 0.002 1.000 0.004 -1.208 0.040 0.366 -13.0 -0.232 0.16348 0.024 1.000 0.002 1.000 0.004 -1.419 0.035 0.352 -12.5 -0.242 0.15034 0.022 1.000 0.002 1.000 0.004 -1.608 0.025 0.339 -12.0 -0.251 0.13597 0.019 1.000 0.002 1.000 0.004 -1.846 0.008 0.328 -11.5 -0.259 0.12530 0.017 1.000 0.002 1.000 0.004 -2.071 -0.022 0.317 -11.0 -0.267 0.11516 0.015 1.000 0.002 1.000 0.004 -2.318 -0.077 0.307 -10.5 -0.273 0.10976 0.013 1.000 0.002 1.000 0.004 -2.485 -0.190 0.298 -10.0 -0.277 0.10032 0.011 1.000 0.002 1.000 0.004 -2.759 -0.484 0.289 -9.5 -0.279 0.08756 0.009 1.000 0.002 1.000 0.003 -3.183 -4.941 0.281 -9.0 -0.278 0.08297 0.006 1.000 0.002 1.000 0.003 -3.346 1.133 0.273 -8.5 -0.274 0.07489 0.004 1.000 0.002 1.000 0.003 -3.655 0.650 0.265 -8.0 -0.266 0.08323 0.002 1.000 0.002 1.000 0.003 -3.201 0.495 0.257 -7.5 -0.255 0.07400 -0.000 1.000 0.002 1.000 0.003 -3.450 0.423 0.249 -7.0 -0.240 0.06790 -0.003 1.000 0.002 1.000 0.003 -3.540 0.387 0.239 -6.5 -0.222 0.05771 -0.005 1.000 0.002 1.000 0.002 -3.847 0.363 0.228 -6.0 -0.200 0.05340 -0.007 1.000 0.001 1.000 0.002 -3.743 0.346 0.214 -5.5 -0.174 0.04737 -0.010 1.000 0.001 1.000 0.002 -3.677 0.335 0.195 -5.0 -0.146 0.04093 -0.012 1.000 0.001 1.000 0.002 -3.560 0.327 0.169 -4.5 -0.114 0.03521 -0.014 1.000 0.001 1.000 0.002 -3.250 0.322 0.127 -4.0 -0.081 0.03123 -0.016 1.000 0.001 1.000 0.002 -2.602 0.319 0.047 -3.5 -0.046 0.02844 -0.019 0.917 0.001 1.000 0.002 -1.633 0.316 -0.155 -3.0 -0.010 0.02555 -0.021 0.892 0.001 1.000 0.002 -0.409 0.131 -1.773 -2.5 -0.086 0.02265 -0.024 0.867 0.001 1.000 0.002 -3.801 -0.049 -0.023 -2.0 -0.026 0.02034 -0.026 0.840 0.001 1.000 0.001 -1.292 0.290 -0.734 -1.5 0.033 0.01841 -0.028 0.806 0.002 1.000 0.003 1.801 0.328 1.102 -1.0 0.090 0.01773 -0.035 0.753 0.995 1.000 0.996 5.092 0.310 0.637 -0.5 0.148 0.01892 -0.035 0.688 0.995 1.000 0.996 7.837 0.254 0.487 0.0 0.206 0.01956 -0.035 0.636 0.996 1.000 0.996 10.543 0.254 0.422 0.5 0.264 0.02063 -0.036 0.584 0.996 1.000 0.996 12.804 0.254 0.385 1.0 0.322 0.02116 -0.036 0.539 0.996 1.000 0.996 15.215 0.254 0.362 1.5 0.380 0.02144 -0.036 0.488 0.996 1.000 0.996 17.711 0.254 0.345 2.0 0.437 0.02250 -0.036 0.422 0.996 1.000 0.996 19.438 0.255 0.333 2.5 0.495 0.02371 -0.037 0.340 0.996 1.000 0.996 20.875 0.255 0.324 3.0 0.552 0.02448 -0.037 0.270 0.996 1.000 0.996 22.565 0.255 0.317 3.5 0.610 0.02525 -0.037 0.210 0.995 1.000 0.996 24.142 0.255 0.311 4.0 0.667 0.02554 -0.038 0.158 0.995 1.000 0.996 26.098 0.255 0.306 4.5 0.723 0.02635 -0.038 0.115 0.995 1.000 0.996 27.447 0.255 0.302 5.0 0.779 0.02599 -0.038 0.075 0.995 1.000 0.996 29.980 0.256 0.299 5.5 0.834 0.02642 -0.038 0.035 0.996 1.000 0.996 31.586 0.256 0.296 6.0 0.888 0.02617 -0.039 0.024 0.996 1.000 0.996 33.923 0.256 0.294 6.5 0.938 0.02486 -0.039 0.014 0.995 1.000 0.996 37.743 0.113 0.292 7.0 0.648 0.04603 -0.072 0.006 0.995 0.062 0.996 14.078 0.100 0.360 7.5 0.715 0.04545 -0.073 0.001 0.995 0.005 0.996 15.741 0.284 0.351 8.0 0.748 0.04919 -0.075 0.000 0.995 0.001 0.996 15.198 0.343 0.350 8.5 0.768 0.05536 -0.077 0.000 0.995 0.001 0.996 13.873 0.390 0.351 9.0 0.784 0.06120 -0.080 0.000 0.996 0.000 0.997 12.803 0.456 0.352 9.5 0.793 0.06951 -0.083 0.000 0.996 0.000 0.997 11.403 0.666 0.354 10.0 0.796 0.07638 -0.085 0.000 0.996 0.001 0.997 10.419 5.244 0.357 10.5 0.794 0.08283 -0.088 0.000 0.996 0.001 0.997 9.581 -0.277 0.360 11.0 0.786 0.09372 -0.090 0.000 0.996 0.001 0.997 8.388 -0.005 0.365 11.5 0.774 0.10670 -0.093 0.000 0.995 0.001 0.996 7.250 0.074 0.370 12.0 0.757 0.11711 -0.095 0.000 0.995 0.001 0.996 6.466 0.115 0.376 12.5 0.736 0.12729 -0.098 0.000 0.995 0.001 0.996 5.780 0.139 0.383 13.0 0.711 0.13603 -0.100 0.000 0.995 0.001 0.996 5.229 0.150 0.391 13.5 0.685 0.14798 -0.103 0.000 0.996 0.001 0.997 4.626 0.158 0.400 14.0 0.656 0.17379 -0.105 0.000 0.996 0.001 0.997 3.772 0.164 0.411 14.5 0.625 0.18179 -0.108 0.000 0.996 0.001 0.997 3.439 0.170 0.423 15.0 0.591 0.19906 -0.111 0.000 0.996 0.001 0.997 2.970 0.174 0.437 Name = AG03 (flat aft bottom) 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 -0.192 0.19857 0.032 1.000 0.003 1.000 0.005 -0.968 0.038 0.417 -14.5 -0.202 0.18913 0.030 1.000 0.002 1.000 0.005 -1.068 0.039 0.399 -14.0 -0.212 0.17847 0.028 1.000 0.002 1.000 0.005 -1.187 0.041 0.382 -13.5 -0.222 0.15867 0.026 1.000 0.002 1.000 0.004 -1.399 0.040 0.366 -13.0 -0.232 0.14860 0.024 1.000 0.002 1.000 0.005 -1.561 0.035 0.352 -12.5 -0.242 0.13784 0.022 1.000 0.002 1.000 0.004 -1.754 0.025 0.339 -12.0 -0.251 0.12446 0.019 1.000 0.002 1.000 0.004 -2.016 0.008 0.328 -11.5 -0.259 0.11560 0.017 1.000 0.002 1.000 0.004 -2.244 -0.022 0.317 -11.0 -0.267 0.10707 0.015 1.000 0.002 1.000 0.004 -2.492 -0.077 0.307 -10.5 -0.273 0.09681 0.013 1.000 0.002 1.000 0.004 -2.817 -0.188 0.298 -10.0 -0.277 0.08921 0.011 1.000 0.002 1.000 0.004 -3.103 -0.494 0.289 -9.5 -0.279 0.08239 0.009 1.000 0.002 1.000 0.003 -3.382 -4.941 0.281 -9.0 -0.278 0.07444 0.006 1.000 0.002 1.000 0.003 -3.730 1.151 0.273 -8.5 -0.274 0.06777 0.004 1.000 0.002 1.000 0.003 -4.039 0.650 0.265 -8.0 -0.266 0.07465 0.002 1.000 0.002 1.000 0.003 -3.569 0.495 0.257 -7.5 -0.255 0.06682 -0.000 1.000 0.002 1.000 0.003 -3.821 0.423 0.249 -7.0 -0.240 0.06123 -0.003 1.000 0.002 1.000 0.003 -3.926 0.386 0.239 -6.5 -0.222 0.05491 -0.005 1.000 0.002 1.000 0.003 -4.040 0.363 0.228 -6.0 -0.200 0.04886 -0.007 1.000 0.001 1.000 0.002 -4.091 0.346 0.214 -5.5 -0.174 0.04337 -0.010 1.000 0.001 1.000 0.002 -4.016 0.335 0.195 -5.0 -0.146 0.03774 -0.012 1.000 0.001 1.000 0.002 -3.860 0.327 0.169 -4.5 -0.114 0.03370 -0.014 1.000 0.001 1.000 0.002 -3.387 0.322 0.126 -4.0 -0.081 0.02905 -0.016 1.000 0.001 1.000 0.002 -2.797 0.319 0.047 -3.5 -0.046 0.02656 -0.019 0.917 0.001 1.000 0.002 -1.748 0.316 -0.155 -3.0 -0.010 0.02394 -0.021 0.892 0.001 1.000 0.002 -0.437 0.131 -1.773 -2.5 -0.086 0.02149 -0.024 0.867 0.001 1.000 0.002 -4.007 -0.048 -0.023 -2.0 -0.026 0.01936 -0.026 0.840 0.001 1.000 0.002 -1.357 0.290 -0.734 -1.5 0.033 0.01753 -0.028 0.806 0.002 1.000 0.004 1.891 0.328 1.102 -1.0 0.090 0.01606 -0.035 0.753 0.995 1.000 0.996 5.622 0.310 0.637 -0.5 0.148 0.01726 -0.035 0.688 0.995 1.000 0.996 8.592 0.254 0.487 0.0 0.206 0.01802 -0.035 0.636 0.996 1.000 0.996 11.444 0.254 0.422 0.5 0.264 0.01906 -0.036 0.584 0.996 1.000 0.996 13.857 0.254 0.385 1.0 0.322 0.01963 -0.036 0.539 0.996 1.000 0.996 16.399 0.254 0.362 1.5 0.380 0.01996 -0.036 0.488 0.996 1.000 0.996 19.018 0.254 0.345 2.0 0.437 0.02104 -0.036 0.422 0.996 1.000 0.996 20.790 0.255 0.333 2.5 0.495 0.02235 -0.037 0.340 0.996 1.000 0.996 22.147 0.255 0.324 3.0 0.552 0.02321 -0.037 0.270 0.996 1.000 0.996 23.800 0.255 0.317 3.5 0.610 0.02345 -0.037 0.210 0.995 1.000 0.996 26.000 0.255 0.311 4.0 0.667 0.02440 -0.038 0.158 0.995 1.000 0.996 27.318 0.255 0.306 4.5 0.723 0.02464 -0.038 0.115 0.995 1.000 0.996 29.347 0.255 0.302 5.0 0.779 0.02501 -0.038 0.075 0.995 1.000 0.996 31.151 0.256 0.299 5.5 0.834 0.02555 -0.038 0.035 0.996 1.000 0.996 32.657 0.256 0.296 6.0 0.888 0.02525 -0.039 0.024 0.996 1.000 0.996 35.153 0.256 0.294 6.5 0.938 0.02443 -0.039 0.014 0.995 1.000 0.996 38.415 0.284 0.292 7.0 0.973 0.02247 -0.042 0.006 0.995 0.975 0.996 43.300 0.104 0.293 7.5 0.708 0.04424 -0.073 0.001 0.995 0.009 0.996 16.005 0.103 0.353 8.0 0.747 0.04701 -0.075 0.000 0.995 0.001 0.996 15.886 0.330 0.350 8.5 0.768 0.05159 -0.077 0.000 0.995 0.001 0.996 14.888 0.386 0.351 9.0 0.784 0.05700 -0.080 0.000 0.996 0.000 0.997 13.748 0.456 0.352 9.5 0.793 0.06428 -0.083 0.000 0.996 0.000 0.997 12.330 0.666 0.354 10.0 0.796 0.07014 -0.085 0.000 0.996 0.001 0.997 11.345 8.750 0.357 10.5 0.793 0.07942 -0.088 0.000 0.996 0.001 0.997 9.987 -0.277 0.360 11.0 0.786 0.08515 -0.090 0.000 0.996 0.001 0.997 9.232 -0.011 0.365 11.5 0.774 0.09579 -0.093 0.000 0.995 0.001 0.996 8.076 0.076 0.370 12.0 0.757 0.11002 -0.095 0.000 0.995 0.001 0.996 6.880 0.116 0.376 12.5 0.735 0.11278 -0.098 0.000 0.995 0.001 0.996 6.521 0.138 0.383 13.0 0.711 0.12551 -0.100 0.000 0.995 0.001 0.996 5.665 0.150 0.391 13.5 0.684 0.13733 -0.103 0.000 0.996 0.001 0.997 4.983 0.158 0.400 14.0 0.655 0.14884 -0.105 0.000 0.996 0.001 0.997 4.403 0.164 0.411 14.5 0.625 0.16666 -0.108 0.000 0.996 0.001 0.997 3.749 0.170 0.423 15.0 0.591 0.17943 -0.111 0.000 0.996 0.001 0.997 3.294 0.174 0.437