Name = AG25 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 -0.293 0.32092 0.001 1.000 0.002 1.000 0.004 -0.912 -0.018 0.252 -14.5 -0.301 0.28041 -0.002 1.000 0.002 1.000 0.003 -1.074 -0.034 0.245 -14.0 -0.309 0.28001 -0.004 1.000 0.002 1.000 0.003 -1.102 -0.078 0.237 -13.5 -0.315 0.35811 -0.006 1.000 0.002 1.000 0.003 -0.879 -0.154 0.231 -13.0 -0.320 0.31072 -0.008 1.000 0.002 1.000 0.003 -1.029 -0.331 0.224 -12.5 -0.323 0.29935 -0.011 1.000 0.002 1.000 0.003 -1.078 -0.929 0.217 -12.0 -0.324 0.25414 -0.013 1.000 0.002 1.000 0.003 -1.274 14.799 0.210 -11.5 -0.322 0.22096 -0.015 1.000 0.002 1.000 0.003 -1.459 1.158 0.203 -11.0 -0.319 0.21493 -0.018 1.000 0.002 1.000 0.003 -1.482 0.668 0.195 -10.5 -0.311 0.19264 -0.020 1.000 0.002 1.000 0.003 -1.616 0.520 0.186 -10.0 -0.301 0.16933 -0.022 1.000 0.002 1.000 0.003 -1.780 0.454 0.176 -9.5 -0.288 0.14322 -0.025 1.000 0.002 1.000 0.002 -2.014 0.409 0.165 -9.0 -0.272 0.12839 -0.027 1.000 0.002 1.000 0.002 -2.117 0.380 0.151 -8.5 -0.252 0.11488 -0.029 1.000 0.002 1.000 0.002 -2.195 0.361 0.134 -8.0 -0.229 0.10293 -0.032 1.000 0.001 1.000 0.002 -2.228 0.349 0.112 -7.5 -0.204 0.09017 -0.034 1.000 0.001 1.000 0.002 -2.266 0.338 0.083 -7.0 -0.175 0.07900 -0.036 0.960 0.002 1.000 0.002 -2.218 0.329 0.042 -6.5 -0.144 0.07168 -0.039 0.948 0.001 1.000 0.002 -2.016 0.325 -0.018 -6.0 -0.112 0.06141 -0.041 0.936 0.002 1.000 0.002 -1.820 0.321 -0.118 -5.5 -0.077 0.05344 -0.044 0.922 0.002 1.000 0.002 -1.449 0.319 -0.313 -5.0 -0.042 0.04601 -0.046 0.905 0.002 1.000 0.002 -0.909 0.316 -0.849 -4.5 -0.004 0.04153 -0.048 0.884 0.002 1.000 0.003 -0.103 0.205 -11.007 -4.0 -0.149 0.03669 -0.051 0.856 0.002 1.000 0.003 -4.069 0.192 -0.090 -3.5 -0.088 0.03364 -0.053 0.832 0.003 1.000 0.004 -2.603 0.289 -0.358 -3.0 -0.026 0.03073 -0.056 0.805 0.004 1.000 0.005 -0.852 0.289 -1.875 -2.5 0.035 0.02880 -0.058 0.778 0.008 1.000 0.015 1.201 0.365 1.926 -2.0 0.091 0.03362 -0.069 0.750 0.270 1.000 0.996 2.720 0.350 1.007 -1.5 0.150 0.03348 -0.069 0.719 0.372 1.000 0.996 4.475 0.255 0.714 -1.0 0.208 0.03225 -0.070 0.689 0.515 1.000 0.996 6.455 0.255 0.585 -0.5 0.266 0.02676 -0.070 0.660 0.995 1.000 0.995 9.954 0.255 0.513 0.0 0.325 0.02658 -0.070 0.627 0.995 1.000 0.995 12.212 0.255 0.467 0.5 0.383 0.02729 -0.071 0.589 0.995 1.000 0.995 14.028 0.255 0.435 1.0 0.441 0.02771 -0.071 0.546 0.995 1.000 0.995 15.911 0.255 0.411 1.5 0.499 0.02809 -0.071 0.496 0.995 1.000 0.995 17.765 0.255 0.393 2.0 0.557 0.02882 -0.072 0.443 0.995 1.000 0.995 19.327 0.255 0.379 2.5 0.615 0.02919 -0.072 0.386 0.995 1.000 0.995 21.059 0.255 0.367 3.0 0.673 0.03002 -0.072 0.329 0.995 1.000 0.995 22.402 0.255 0.357 3.5 0.730 0.03031 -0.072 0.277 0.995 1.000 0.995 24.088 0.255 0.349 4.0 0.787 0.03044 -0.073 0.225 0.995 1.000 0.996 25.861 0.268 0.342 4.5 0.833 0.03036 -0.074 0.172 0.995 0.978 0.996 27.450 0.287 0.339 5.0 0.877 0.03031 -0.076 0.121 0.995 0.958 0.996 28.940 0.301 0.337 5.5 0.915 0.03165 -0.079 0.072 0.995 0.930 0.995 28.908 0.073 0.336 6.0 0.740 0.04279 -0.100 0.002 0.995 0.007 0.995 17.296 0.068 0.386 6.5 0.782 0.04555 -0.103 0.001 0.995 0.002 0.995 17.163 0.319 0.382 7.0 0.811 0.05173 -0.105 0.001 0.995 0.002 0.995 15.684 0.339 0.380 7.5 0.838 0.05710 -0.108 0.001 0.995 0.001 0.995 14.676 0.354 0.379 8.0 0.859 0.06626 -0.110 0.001 0.996 0.001 0.996 12.969 0.382 0.378 8.5 0.876 0.07545 -0.113 0.000 0.996 0.001 0.996 11.611 0.424 0.379 9.0 0.888 0.08629 -0.115 0.000 0.996 0.001 0.996 10.293 0.508 0.380 9.5 0.895 0.09609 -0.118 0.000 0.996 0.001 0.996 9.320 0.743 0.382 10.0 0.898 0.11174 -0.120 0.000 0.996 0.001 0.996 8.040 -17.899 0.384 10.5 0.895 0.13098 -0.123 0.000 0.996 0.001 0.996 6.835 -0.217 0.387 11.0 0.888 0.14149 -0.125 0.000 0.996 0.001 0.996 6.274 0.008 0.391 11.5 0.874 0.16583 -0.128 0.000 0.996 0.001 0.996 5.273 0.085 0.396 12.0 0.857 0.18760 -0.130 0.000 0.996 0.001 0.996 4.569 0.119 0.402 12.5 0.836 0.19694 -0.133 0.000 0.996 0.001 0.996 4.246 0.140 0.409 13.0 0.811 0.22865 -0.135 0.000 0.996 0.001 0.996 3.549 0.154 0.417 13.5 0.784 0.21051 -0.138 0.001 0.996 0.001 0.996 3.724 0.162 0.426 14.0 0.755 0.22701 -0.140 0.001 0.996 0.001 0.996 3.325 0.167 0.436 14.5 0.724 0.26074 -0.143 0.001 0.996 0.001 0.996 2.775 0.171 0.447 15.0 0.692 0.28546 -0.145 0.001 0.996 0.002 0.996 2.423 0.172 0.460 Name = AG25 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 -0.293 0.22793 0.001 1.000 0.002 1.000 0.004 -1.284 -0.019 0.252 -14.5 -0.301 0.22140 -0.002 1.000 0.002 1.000 0.004 -1.360 -0.034 0.245 -14.0 -0.309 0.19846 -0.004 1.000 0.002 1.000 0.003 -1.555 -0.079 0.237 -13.5 -0.315 0.19506 -0.006 1.000 0.002 1.000 0.003 -1.614 -0.157 0.231 -13.0 -0.320 0.24097 -0.008 1.000 0.002 1.000 0.003 -1.327 -0.333 0.224 -12.5 -0.323 0.16778 -0.011 1.000 0.002 1.000 0.003 -1.923 -0.939 0.217 -12.0 -0.324 0.14902 -0.013 1.000 0.002 1.000 0.003 -2.171 14.056 0.210 -11.5 -0.322 0.17496 -0.015 1.000 0.002 1.000 0.003 -1.842 1.190 0.203 -11.0 -0.319 0.15706 -0.018 1.000 0.002 1.000 0.003 -2.028 0.675 0.195 -10.5 -0.311 0.14110 -0.020 1.000 0.002 1.000 0.003 -2.207 0.517 0.186 -10.0 -0.301 0.13054 -0.022 1.000 0.002 1.000 0.003 -2.308 0.452 0.176 -9.5 -0.288 0.11287 -0.025 1.000 0.002 1.000 0.003 -2.554 0.409 0.165 -9.0 -0.272 0.09927 -0.027 1.000 0.002 1.000 0.003 -2.737 0.380 0.151 -8.5 -0.252 0.09192 -0.029 1.000 0.002 1.000 0.002 -2.742 0.361 0.134 -8.0 -0.229 0.07909 -0.032 1.000 0.001 1.000 0.002 -2.899 0.349 0.112 -7.5 -0.204 0.07337 -0.034 1.000 0.001 1.000 0.002 -2.782 0.338 0.083 -7.0 -0.175 0.06270 -0.036 0.960 0.002 1.000 0.002 -2.795 0.330 0.042 -6.5 -0.144 0.05696 -0.039 0.948 0.001 1.000 0.002 -2.537 0.325 -0.018 -6.0 -0.112 0.04966 -0.041 0.936 0.002 1.000 0.002 -2.250 0.321 -0.118 -5.5 -0.077 0.04395 -0.044 0.922 0.002 1.000 0.002 -1.761 0.318 -0.313 -5.0 -0.042 0.03953 -0.046 0.905 0.002 1.000 0.002 -1.052 0.316 -0.856 -4.5 -0.004 0.03490 -0.048 0.884 0.002 1.000 0.003 -0.123 0.205 -11.007 -4.0 -0.149 0.03124 -0.051 0.856 0.002 1.000 0.003 -4.779 0.192 -0.090 -3.5 -0.088 0.02852 -0.053 0.832 0.003 1.000 0.004 -3.070 0.289 -0.358 -3.0 -0.026 0.02648 -0.056 0.805 0.004 1.000 0.006 -0.989 0.380 -1.875 -2.5 0.033 0.03065 -0.069 0.778 0.008 1.000 0.996 1.082 0.365 2.328 -2.0 0.091 0.02934 -0.069 0.750 0.270 1.000 0.996 3.117 0.255 1.007 -1.5 0.150 0.02858 -0.069 0.719 0.372 1.000 0.996 5.241 0.255 0.714 -1.0 0.208 0.02711 -0.070 0.689 0.515 1.000 0.996 7.676 0.255 0.585 -0.5 0.266 0.02123 -0.070 0.660 0.995 1.000 0.995 12.551 0.255 0.513 0.0 0.325 0.02147 -0.070 0.627 0.995 1.000 0.995 15.119 0.255 0.467 0.5 0.383 0.02226 -0.071 0.589 0.995 1.000 0.995 17.193 0.255 0.435 1.0 0.441 0.02273 -0.071 0.546 0.995 1.000 0.995 19.396 0.255 0.411 1.5 0.499 0.02384 -0.071 0.496 0.995 1.000 0.995 20.926 0.255 0.393 2.0 0.557 0.02438 -0.072 0.443 0.995 1.000 0.995 22.843 0.255 0.379 2.5 0.615 0.02530 -0.072 0.386 0.995 1.000 0.995 24.296 0.255 0.367 3.0 0.673 0.02592 -0.072 0.329 0.995 1.000 0.995 25.949 0.255 0.357 3.5 0.730 0.02675 -0.072 0.277 0.995 1.000 0.995 27.287 0.255 0.349 4.0 0.787 0.02710 -0.073 0.225 0.995 1.000 0.996 29.051 0.256 0.342 4.5 0.844 0.02777 -0.073 0.172 0.995 1.000 0.996 30.391 0.256 0.337 5.0 0.899 0.02803 -0.073 0.121 0.995 1.000 0.996 32.061 0.256 0.332 5.5 0.952 0.02829 -0.074 0.072 0.995 1.000 0.995 33.655 0.256 0.328 6.0 1.003 0.02856 -0.074 0.002 0.995 1.000 0.995 35.129 0.081 0.324 6.5 0.781 0.03973 -0.103 0.001 0.995 0.002 0.995 19.647 0.088 0.382 7.0 0.811 0.04449 -0.105 0.001 0.995 0.002 0.995 18.224 0.338 0.380 7.5 0.837 0.04939 -0.108 0.001 0.995 0.001 0.995 16.954 0.353 0.379 8.0 0.859 0.05487 -0.110 0.001 0.996 0.001 0.996 15.662 0.379 0.378 8.5 0.876 0.06156 -0.113 0.000 0.996 0.001 0.996 14.230 0.424 0.379 9.0 0.888 0.06948 -0.115 0.000 0.996 0.001 0.996 12.784 0.512 0.380 9.5 0.895 0.07765 -0.118 0.000 0.996 0.001 0.996 11.529 0.758 0.382 10.0 0.898 0.09097 -0.120 0.000 0.996 0.001 0.996 9.872 -679.817 0.384 10.5 0.895 0.10045 -0.123 0.000 0.996 0.001 0.996 8.912 -0.218 0.387 11.0 0.887 0.11297 -0.125 0.000 0.996 0.001 0.996 7.855 0.011 0.391 11.5 0.874 0.12954 -0.128 0.000 0.996 0.001 0.996 6.748 0.084 0.396 12.0 0.857 0.13988 -0.130 0.000 0.996 0.001 0.996 6.128 0.119 0.402 12.5 0.836 0.15816 -0.133 0.000 0.996 0.001 0.996 5.285 0.141 0.409 13.0 0.811 0.15217 -0.135 0.000 0.996 0.001 0.996 5.330 0.153 0.417 13.5 0.784 0.15711 -0.138 0.001 0.996 0.001 0.996 4.990 0.162 0.426 14.0 0.754 0.18210 -0.140 0.001 0.996 0.001 0.996 4.143 0.167 0.436 14.5 0.723 0.20552 -0.143 0.001 0.996 0.002 0.996 3.520 0.171 0.448 15.0 0.692 0.20296 -0.145 0.001 0.996 0.002 0.996 3.407 0.172 0.460 Name = AG25 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 -0.293 0.20128 0.001 1.000 0.002 1.000 0.004 -1.454 -0.019 0.252 -14.5 -0.301 0.19714 -0.002 1.000 0.002 1.000 0.004 -1.527 -0.035 0.245 -14.0 -0.308 0.17549 -0.004 1.000 0.002 1.000 0.004 -1.758 -0.078 0.238 -13.5 -0.315 0.16052 -0.006 1.000 0.002 1.000 0.003 -1.961 -0.158 0.231 -13.0 -0.320 0.15615 -0.008 1.000 0.002 1.000 0.003 -2.047 -0.333 0.224 -12.5 -0.323 0.13765 -0.011 1.000 0.002 1.000 0.003 -2.343 -0.904 0.217 -12.0 -0.324 0.12433 -0.013 1.000 0.002 1.000 0.003 -2.602 9.381 0.210 -11.5 -0.322 0.12150 -0.015 1.000 0.002 1.000 0.003 -2.651 1.142 0.203 -11.0 -0.318 0.14176 -0.018 1.000 0.002 1.000 0.003 -2.246 0.674 0.195 -10.5 -0.311 0.12868 -0.020 1.000 0.002 1.000 0.003 -2.418 0.522 0.186 -10.0 -0.301 0.10934 -0.022 1.000 0.002 1.000 0.003 -2.755 0.453 0.176 -9.5 -0.288 0.09990 -0.025 1.000 0.002 1.000 0.003 -2.884 0.406 0.165 -9.0 -0.271 0.09170 -0.027 1.000 0.002 1.000 0.003 -2.959 0.381 0.151 -8.5 -0.252 0.07905 -0.029 1.000 0.002 1.000 0.002 -3.188 0.362 0.134 -8.0 -0.229 0.07108 -0.032 1.000 0.001 1.000 0.002 -3.223 0.349 0.112 -7.5 -0.204 0.06404 -0.034 1.000 0.001 1.000 0.002 -3.187 0.338 0.083 -7.0 -0.175 0.05736 -0.036 0.960 0.002 1.000 0.002 -3.051 0.330 0.042 -6.5 -0.144 0.05057 -0.039 0.948 0.001 1.000 0.002 -2.857 0.325 -0.018 -6.0 -0.112 0.04580 -0.041 0.936 0.002 1.000 0.002 -2.435 0.321 -0.119 -5.5 -0.077 0.04090 -0.044 0.922 0.002 1.000 0.002 -1.888 0.319 -0.314 -5.0 -0.042 0.03580 -0.046 0.905 0.002 1.000 0.002 -1.161 0.316 -0.856 -4.5 -0.004 0.03195 -0.048 0.884 0.002 1.000 0.003 -0.135 0.205 -11.007 -4.0 -0.149 0.02920 -0.051 0.856 0.002 1.000 0.003 -5.114 0.192 -0.090 -3.5 -0.088 0.02667 -0.053 0.832 0.003 1.000 0.004 -3.283 0.289 -0.358 -3.0 -0.026 0.02463 -0.056 0.805 0.004 1.000 0.006 -1.063 0.380 -1.875 -2.5 0.033 0.02875 -0.069 0.778 0.008 1.000 0.996 1.154 0.366 2.328 -2.0 0.091 0.02713 -0.069 0.750 0.270 1.000 0.996 3.370 0.255 1.007 -1.5 0.150 0.02653 -0.070 0.719 0.372 1.000 0.996 5.646 0.255 0.714 -1.0 0.208 0.02530 -0.070 0.689 0.515 1.000 0.996 8.226 0.255 0.585 -0.5 0.266 0.01901 -0.070 0.660 0.995 1.000 0.995 14.017 0.255 0.513 0.0 0.325 0.01929 -0.070 0.627 0.995 1.000 0.995 16.824 0.255 0.467 0.5 0.383 0.02011 -0.071 0.589 0.995 1.000 0.995 19.039 0.255 0.435 1.0 0.441 0.02063 -0.071 0.546 0.995 1.000 0.995 21.367 0.255 0.411 1.5 0.499 0.02145 -0.071 0.496 0.995 1.000 0.995 23.256 0.255 0.393 2.0 0.557 0.02210 -0.072 0.443 0.995 1.000 0.995 25.200 0.255 0.379 2.5 0.615 0.02311 -0.072 0.386 0.995 1.000 0.995 26.602 0.255 0.367 3.0 0.673 0.02384 -0.072 0.329 0.995 1.000 0.995 28.213 0.255 0.357 3.5 0.730 0.02475 -0.072 0.277 0.995 1.000 0.995 29.495 0.255 0.349 4.0 0.787 0.02522 -0.073 0.225 0.995 1.000 0.996 31.220 0.256 0.342 4.5 0.844 0.02554 -0.073 0.172 0.995 1.000 0.996 33.044 0.256 0.337 5.0 0.899 0.02636 -0.073 0.121 0.995 1.000 0.996 34.091 0.256 0.332 5.5 0.952 0.02662 -0.074 0.072 0.995 1.000 0.995 35.758 0.256 0.328 6.0 1.003 0.02689 -0.074 0.002 0.995 1.000 0.995 37.314 0.083 0.324 6.5 0.779 0.03722 -0.103 0.001 0.995 0.003 0.995 20.919 0.088 0.382 7.0 0.811 0.04068 -0.105 0.001 0.995 0.002 0.995 19.929 0.334 0.380 7.5 0.837 0.04507 -0.108 0.001 0.995 0.001 0.995 18.581 0.353 0.379 8.0 0.859 0.04986 -0.110 0.001 0.996 0.001 0.996 17.237 0.379 0.378 8.5 0.876 0.05547 -0.113 0.000 0.996 0.001 0.996 15.792 0.426 0.379 9.0 0.888 0.06377 -0.115 0.000 0.996 0.001 0.996 13.923 0.519 0.380 9.5 0.895 0.07273 -0.118 0.000 0.996 0.001 0.996 12.302 0.744 0.382 10.0 0.898 0.07949 -0.120 0.000 0.996 0.001 0.996 11.298 -63.964 0.384 10.5 0.895 0.09332 -0.123 0.000 0.996 0.001 0.996 9.587 -0.207 0.387 11.0 0.887 0.10076 -0.125 0.000 0.996 0.001 0.996 8.804 0.010 0.391 11.5 0.874 0.10474 -0.128 0.000 0.996 0.001 0.996 8.342 0.084 0.396 12.0 0.857 0.12770 -0.130 0.000 0.996 0.001 0.996 6.709 0.119 0.402 12.5 0.835 0.12342 -0.133 0.000 0.996 0.001 0.996 6.769 0.140 0.409 13.0 0.811 0.12745 -0.135 0.000 0.996 0.001 0.996 6.364 0.153 0.417 13.5 0.784 0.14274 -0.138 0.001 0.996 0.001 0.996 5.490 0.162 0.426 14.0 0.754 0.15258 -0.140 0.001 0.996 0.001 0.996 4.945 0.167 0.436 14.5 0.723 0.16915 -0.143 0.001 0.996 0.002 0.996 4.276 0.171 0.448 15.0 0.691 0.17878 -0.145 0.001 0.996 0.002 0.996 3.867 0.172 0.460 Name = AG25 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 -0.293 0.18593 0.001 1.000 0.002 1.000 0.004 -1.573 -0.019 0.252 -14.5 -0.301 0.17015 -0.002 1.000 0.002 1.000 0.004 -1.769 -0.035 0.245 -14.0 -0.308 0.16237 -0.004 1.000 0.002 1.000 0.004 -1.899 -0.079 0.238 -13.5 -0.315 0.14997 -0.006 1.000 0.002 1.000 0.004 -2.098 -0.156 0.231 -13.0 -0.320 0.13654 -0.008 1.000 0.002 1.000 0.003 -2.340 -0.335 0.224 -12.5 -0.322 0.12873 -0.011 1.000 0.002 1.000 0.004 -2.505 -0.947 0.217 -12.0 -0.323 0.11747 -0.013 1.000 0.002 1.000 0.004 -2.753 13.025 0.210 -11.5 -0.322 0.10722 -0.015 1.000 0.002 1.000 0.003 -3.004 1.172 0.203 -11.0 -0.318 0.12435 -0.018 1.000 0.002 1.000 0.003 -2.560 0.674 0.195 -10.5 -0.311 0.11289 -0.020 1.000 0.002 1.000 0.003 -2.756 0.520 0.186 -10.0 -0.301 0.10031 -0.022 1.000 0.002 1.000 0.003 -3.002 0.451 0.176 -9.5 -0.288 0.09239 -0.025 1.000 0.002 1.000 0.003 -3.116 0.407 0.165 -9.0 -0.271 0.08166 -0.027 1.000 0.002 1.000 0.003 -3.322 0.380 0.151 -8.5 -0.252 0.07388 -0.029 1.000 0.002 1.000 0.003 -3.409 0.361 0.134 -8.0 -0.229 0.06653 -0.032 1.000 0.001 1.000 0.003 -3.441 0.349 0.112 -7.5 -0.204 0.05940 -0.034 1.000 0.001 1.000 0.002 -3.433 0.338 0.083 -7.0 -0.175 0.05264 -0.036 0.960 0.002 1.000 0.002 -3.325 0.330 0.042 -6.5 -0.144 0.04809 -0.039 0.948 0.001 1.000 0.002 -3.000 0.325 -0.019 -6.0 -0.112 0.04251 -0.041 0.936 0.002 1.000 0.002 -2.624 0.321 -0.119 -5.5 -0.077 0.03816 -0.044 0.922 0.002 1.000 0.002 -2.023 0.319 -0.314 -5.0 -0.042 0.03377 -0.046 0.905 0.002 1.000 0.002 -1.231 0.316 -0.856 -4.5 -0.004 0.03026 -0.048 0.884 0.002 1.000 0.003 -0.142 0.205 -11.007 -4.0 -0.149 0.02766 -0.051 0.856 0.002 1.000 0.003 -5.398 0.192 -0.090 -3.5 -0.088 0.02535 -0.053 0.832 0.003 1.000 0.004 -3.455 0.289 -0.358 -3.0 -0.026 0.02354 -0.056 0.805 0.004 1.000 0.007 -1.112 0.380 -1.874 -2.5 0.033 0.02762 -0.069 0.778 0.008 1.000 0.996 1.201 0.366 2.328 -2.0 0.091 0.02591 -0.069 0.750 0.270 1.000 0.996 3.529 0.255 1.007 -1.5 0.150 0.02520 -0.070 0.719 0.372 1.000 0.996 5.944 0.255 0.714 -1.0 0.208 0.02362 -0.070 0.689 0.515 1.000 0.996 8.813 0.255 0.585 -0.5 0.266 0.01752 -0.070 0.660 0.995 1.000 0.995 15.205 0.255 0.513 0.0 0.325 0.01784 -0.070 0.627 0.995 1.000 0.995 18.195 0.255 0.467 0.5 0.383 0.01849 -0.071 0.589 0.995 1.000 0.995 20.702 0.255 0.435 1.0 0.441 0.01936 -0.071 0.546 0.995 1.000 0.995 22.771 0.255 0.411 1.5 0.499 0.02023 -0.071 0.496 0.995 1.000 0.995 24.663 0.255 0.393 2.0 0.557 0.02097 -0.072 0.443 0.995 1.000 0.995 26.564 0.255 0.379 2.5 0.615 0.02168 -0.072 0.386 0.995 1.000 0.995 28.363 0.255 0.367 3.0 0.673 0.02247 -0.072 0.329 0.995 1.000 0.995 29.925 0.255 0.357 3.5 0.730 0.02302 -0.072 0.277 0.995 1.000 0.995 31.713 0.255 0.349 4.0 0.787 0.02397 -0.073 0.225 0.995 1.000 0.996 32.851 0.256 0.342 4.5 0.844 0.02434 -0.073 0.172 0.995 1.000 0.996 34.666 0.256 0.337 5.0 0.899 0.02480 -0.073 0.121 0.995 1.000 0.996 36.240 0.256 0.332 5.5 0.952 0.02551 -0.074 0.072 0.995 1.000 0.995 37.324 0.256 0.328 6.0 1.003 0.02580 -0.074 0.002 0.995 1.000 0.995 38.891 0.086 0.324 6.5 0.775 0.03596 -0.103 0.001 0.995 0.005 0.995 21.550 0.088 0.383 7.0 0.810 0.03895 -0.105 0.001 0.995 0.002 0.995 20.799 0.329 0.380 7.5 0.837 0.04251 -0.108 0.001 0.995 0.001 0.995 19.698 0.352 0.379 8.0 0.859 0.04789 -0.110 0.001 0.996 0.001 0.996 17.940 0.381 0.378 8.5 0.876 0.05294 -0.113 0.000 0.996 0.001 0.996 16.542 0.424 0.379 9.0 0.888 0.05904 -0.115 0.000 0.996 0.001 0.996 15.040 0.515 0.380 9.5 0.895 0.06649 -0.118 0.000 0.996 0.001 0.996 13.457 0.758 0.382 10.0 0.898 0.07479 -0.120 0.000 0.996 0.001 0.996 12.004 -63.964 0.384 10.5 0.895 0.08393 -0.123 0.000 0.996 0.001 0.996 10.660 -0.208 0.387 11.0 0.887 0.09369 -0.125 0.000 0.996 0.001 0.996 9.465 0.010 0.391 11.5 0.874 0.09370 -0.128 0.000 0.996 0.001 0.996 9.325 0.083 0.396 12.0 0.857 0.11325 -0.130 0.000 0.996 0.001 0.996 7.565 0.119 0.402 12.5 0.835 0.10938 -0.133 0.000 0.996 0.001 0.996 7.638 0.141 0.409 13.0 0.811 0.11968 -0.135 0.000 0.996 0.001 0.996 6.775 0.153 0.417 13.5 0.784 0.12674 -0.138 0.001 0.996 0.001 0.996 6.184 0.162 0.426 14.0 0.754 0.14348 -0.140 0.001 0.996 0.002 0.996 5.256 0.167 0.436 14.5 0.723 0.15768 -0.143 0.001 0.996 0.002 0.996 4.586 0.171 0.448 15.0 0.691 0.16474 -0.145 0.001 0.996 0.002 0.996 4.195 0.172 0.460