Name = AG08 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 -0.321 0.43708 0.026 1.000 0.002 1.000 0.003 -0.734 0.087 0.332 -14.5 -0.334 0.39012 0.024 1.000 0.002 1.000 0.003 -0.855 0.083 0.323 -14.0 -0.346 0.36044 0.022 1.000 0.002 1.000 0.003 -0.959 0.072 0.314 -13.5 -0.357 0.31903 0.020 1.000 0.002 1.000 0.003 -1.119 0.045 0.306 -13.0 -0.366 0.28240 0.018 1.000 0.002 1.000 0.003 -1.297 -0.007 0.299 -12.5 -0.373 0.26674 0.016 1.000 0.002 1.000 0.003 -1.400 -0.078 0.293 -12.0 -0.379 0.23556 0.014 1.000 0.002 1.000 0.003 -1.609 -0.220 0.286 -11.5 -0.382 0.22172 0.012 1.000 0.002 1.000 0.003 -1.725 -0.680 0.281 -11.0 -0.384 0.19510 0.010 1.000 0.001 1.000 0.003 -1.967 9.380 0.275 -10.5 -0.382 0.17251 0.007 1.000 0.001 1.000 0.002 -2.215 0.909 0.269 -10.0 -0.377 0.16081 0.005 1.000 0.001 1.000 0.002 -2.345 0.578 0.264 -9.5 -0.369 0.14465 0.003 1.000 0.002 1.000 0.003 -2.550 0.474 0.258 -9.0 -0.358 0.13679 0.001 1.000 0.001 1.000 0.002 -2.615 0.420 0.252 -8.5 -0.343 0.11938 -0.001 1.000 0.001 1.000 0.002 -2.874 0.382 0.246 -8.0 -0.325 0.10193 -0.004 1.000 0.001 1.000 0.002 -3.185 0.361 0.239 -7.5 -0.303 0.09275 -0.006 1.000 0.001 1.000 0.002 -3.272 0.347 0.231 -7.0 -0.279 0.08199 -0.008 1.000 0.001 1.000 0.002 -3.403 0.336 0.222 -6.5 -0.252 0.07313 -0.010 1.000 0.001 1.000 0.002 -3.444 0.328 0.210 -6.0 -0.222 0.06156 -0.012 1.000 0.002 1.000 0.002 -3.613 0.322 0.194 -5.5 -0.190 0.05451 -0.015 1.000 0.002 1.000 0.002 -3.492 0.317 0.173 -5.0 -0.156 0.04848 -0.017 1.000 0.002 1.000 0.003 -3.225 0.314 0.142 -4.5 -0.121 0.04295 -0.019 1.000 0.002 1.000 0.004 -2.812 0.312 0.092 -4.0 -0.084 0.03781 -0.021 1.000 0.003 1.000 0.004 -2.229 0.310 -0.003 -3.5 -0.046 0.03420 -0.024 1.000 0.004 1.000 0.006 -1.350 0.307 -0.260 -3.0 -0.006 0.03160 -0.026 0.961 0.006 1.000 0.009 -0.201 0.160 -3.801 -2.5 -0.095 0.02992 -0.028 0.941 0.014 1.000 0.024 -3.166 -0.315 -0.045 -2.0 -0.030 0.03508 -0.039 0.921 0.037 1.000 0.998 -0.853 0.345 -1.056 -1.5 0.024 0.03668 -0.039 0.896 0.092 1.000 0.998 0.660 0.252 1.869 -1.0 0.082 0.02615 -0.039 0.863 0.996 1.000 0.997 3.132 0.252 0.730 -0.5 0.140 0.02630 -0.039 0.820 0.996 1.000 0.997 5.308 0.252 0.532 0.0 0.197 0.02721 -0.040 0.767 0.996 1.000 0.997 7.252 0.252 0.450 0.5 0.255 0.02779 -0.040 0.700 0.996 1.000 0.997 9.176 0.252 0.406 1.0 0.313 0.02854 -0.040 0.632 0.996 1.000 0.996 10.950 0.252 0.377 1.5 0.370 0.03011 -0.040 0.547 0.996 1.000 0.996 12.293 0.252 0.358 2.0 0.428 0.03225 -0.040 0.399 0.996 1.000 0.996 13.260 0.252 0.344 2.5 0.485 0.03319 -0.040 0.292 0.996 1.000 0.996 14.613 0.252 0.333 3.0 0.542 0.03365 -0.040 0.234 0.997 1.000 0.997 16.114 0.253 0.324 3.5 0.599 0.03445 -0.040 0.178 0.996 1.000 0.996 17.395 0.253 0.318 4.0 0.655 0.03404 -0.041 0.136 0.996 1.000 0.996 19.252 0.253 0.312 4.5 0.711 0.03369 -0.041 0.088 0.997 1.000 0.997 21.094 0.253 0.307 5.0 0.765 0.03316 -0.041 0.032 0.997 1.000 0.997 23.060 0.062 0.304 5.5 0.581 0.04094 -0.065 0.002 0.997 0.005 0.997 14.180 0.072 0.362 6.0 0.615 0.04526 -0.068 0.002 0.996 0.003 0.997 13.595 0.320 0.360 6.5 0.647 0.05034 -0.070 0.001 0.997 0.002 0.997 12.848 0.328 0.358 7.0 0.675 0.05726 -0.072 0.001 0.997 0.002 0.997 11.788 0.338 0.357 7.5 0.700 0.06587 -0.075 0.001 0.996 0.002 0.997 10.627 0.350 0.356 8.0 0.722 0.07343 -0.077 0.001 0.996 0.001 0.996 9.830 0.370 0.356 8.5 0.739 0.08545 -0.079 0.001 0.996 0.001 0.996 8.651 0.402 0.357 9.0 0.753 0.09677 -0.082 0.001 0.997 0.001 0.997 7.779 0.451 0.358 9.5 0.763 0.10950 -0.084 0.001 0.997 0.001 0.997 6.965 0.563 0.360 10.0 0.768 0.12400 -0.086 0.001 0.997 0.001 0.997 6.192 1.388 0.362 10.5 0.767 0.13490 -0.089 0.001 0.997 0.001 0.997 5.684 -0.429 0.366 11.0 0.761 0.15973 -0.091 0.001 0.997 0.001 0.997 4.764 -0.053 0.370 11.5 0.751 0.17783 -0.093 0.001 0.997 0.001 0.997 4.225 0.051 0.374 12.0 0.737 0.19586 -0.096 0.001 0.997 0.001 0.997 3.764 0.102 0.380 12.5 0.719 0.20186 -0.098 0.001 0.997 0.002 0.997 3.563 0.126 0.386 13.0 0.699 0.25399 -0.100 0.001 0.996 0.001 0.996 2.752 0.141 0.394 13.5 0.676 0.27887 -0.103 0.001 0.996 0.001 0.996 2.424 0.151 0.402 14.0 0.651 0.30814 -0.105 0.001 0.996 0.001 0.996 2.113 0.158 0.411 14.5 0.625 0.29199 -0.108 0.001 0.996 0.002 0.996 2.139 0.162 0.422 15.0 0.598 0.32561 -0.110 0.001 0.996 0.002 0.996 1.836 0.163 0.434 Name = AG08 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 -0.321 0.27187 0.026 1.000 0.002 1.000 0.004 -1.179 0.086 0.333 -14.5 -0.333 0.30069 0.024 1.000 0.002 1.000 0.003 -1.109 0.082 0.323 -14.0 -0.346 0.26310 0.022 1.000 0.002 1.000 0.003 -1.313 0.072 0.314 -13.5 -0.357 0.24949 0.020 1.000 0.002 1.000 0.003 -1.430 0.044 0.307 -13.0 -0.366 0.22431 0.018 1.000 0.002 1.000 0.003 -1.632 -0.006 0.299 -12.5 -0.373 0.19848 0.016 1.000 0.002 1.000 0.003 -1.881 -0.077 0.293 -12.0 -0.379 0.17820 0.014 1.000 0.002 1.000 0.003 -2.127 -0.222 0.286 -11.5 -0.382 0.16856 0.012 1.000 0.002 1.000 0.003 -2.268 -0.685 0.281 -11.0 -0.384 0.15056 0.010 1.000 0.001 1.000 0.003 -2.548 8.990 0.275 -10.5 -0.382 0.13505 0.007 1.000 0.001 1.000 0.003 -2.827 0.925 0.269 -10.0 -0.377 0.12038 0.005 1.000 0.001 1.000 0.002 -3.133 0.583 0.264 -9.5 -0.369 0.10828 0.003 1.000 0.002 1.000 0.003 -3.407 0.472 0.258 -9.0 -0.358 0.09964 0.001 1.000 0.001 1.000 0.002 -3.589 0.418 0.252 -8.5 -0.343 0.09584 -0.001 1.000 0.001 1.000 0.002 -3.578 0.383 0.246 -8.0 -0.325 0.07907 -0.004 1.000 0.001 1.000 0.002 -4.106 0.362 0.239 -7.5 -0.303 0.07272 -0.006 1.000 0.001 1.000 0.002 -4.173 0.347 0.231 -7.0 -0.279 0.06451 -0.008 1.000 0.001 1.000 0.002 -4.325 0.336 0.222 -6.5 -0.252 0.05821 -0.010 1.000 0.001 1.000 0.002 -4.328 0.328 0.210 -6.0 -0.222 0.05178 -0.012 1.000 0.002 1.000 0.002 -4.290 0.322 0.194 -5.5 -0.190 0.04559 -0.015 1.000 0.002 1.000 0.003 -4.170 0.317 0.173 -5.0 -0.156 0.04054 -0.017 1.000 0.002 1.000 0.003 -3.850 0.314 0.142 -4.5 -0.121 0.03538 -0.019 1.000 0.002 1.000 0.004 -3.413 0.312 0.092 -4.0 -0.084 0.03198 -0.021 1.000 0.003 1.000 0.005 -2.620 0.310 -0.004 -3.5 -0.046 0.02868 -0.024 1.000 0.004 1.000 0.006 -1.596 0.307 -0.264 -3.0 -0.005 0.02673 -0.026 0.961 0.006 1.000 0.010 -0.200 0.164 -4.558 -2.5 -0.095 0.02563 -0.028 0.941 0.014 1.000 0.042 -3.692 -0.289 -0.043 -2.0 -0.030 0.03219 -0.039 0.921 0.037 1.000 0.998 -0.935 0.347 -1.048 -1.5 0.024 0.03177 -0.039 0.896 0.092 1.000 0.998 0.762 0.252 1.870 -1.0 0.082 0.01966 -0.039 0.863 0.996 1.000 0.997 4.165 0.252 0.730 -0.5 0.140 0.02035 -0.039 0.820 0.996 1.000 0.997 6.860 0.252 0.532 0.0 0.197 0.02121 -0.040 0.767 0.996 1.000 0.997 9.302 0.252 0.450 0.5 0.255 0.02211 -0.040 0.700 0.996 1.000 0.997 11.529 0.252 0.406 1.0 0.313 0.02314 -0.040 0.632 0.996 1.000 0.996 13.509 0.252 0.377 1.5 0.370 0.02470 -0.040 0.547 0.996 1.000 0.996 14.984 0.252 0.358 2.0 0.428 0.02673 -0.040 0.399 0.996 1.000 0.996 16.001 0.252 0.344 2.5 0.485 0.02863 -0.040 0.292 0.996 1.000 0.996 16.939 0.252 0.333 3.0 0.542 0.02929 -0.040 0.234 0.997 1.000 0.997 18.516 0.253 0.324 3.5 0.599 0.02959 -0.040 0.178 0.996 1.000 0.996 20.252 0.253 0.318 4.0 0.655 0.03047 -0.041 0.136 0.996 1.000 0.996 21.507 0.253 0.312 4.5 0.711 0.03087 -0.041 0.088 0.997 1.000 0.997 23.022 0.253 0.307 5.0 0.765 0.03070 -0.041 0.032 0.997 1.000 0.997 24.905 0.064 0.304 5.5 0.579 0.03549 -0.065 0.002 0.997 0.005 0.997 16.326 0.073 0.363 6.0 0.615 0.03903 -0.068 0.002 0.996 0.003 0.997 15.749 0.319 0.360 6.5 0.646 0.04306 -0.070 0.001 0.997 0.002 0.997 15.015 0.327 0.358 7.0 0.675 0.04776 -0.072 0.001 0.997 0.002 0.997 14.135 0.337 0.357 7.5 0.700 0.05425 -0.075 0.001 0.996 0.002 0.997 12.903 0.350 0.356 8.0 0.722 0.06017 -0.077 0.001 0.996 0.001 0.996 11.996 0.370 0.356 8.5 0.739 0.06861 -0.079 0.001 0.996 0.001 0.996 10.774 0.402 0.357 9.0 0.753 0.07645 -0.082 0.001 0.997 0.001 0.997 9.847 0.451 0.358 9.5 0.763 0.08607 -0.084 0.001 0.997 0.001 0.997 8.861 0.563 0.360 10.0 0.768 0.09650 -0.086 0.001 0.997 0.001 0.997 7.957 1.479 0.362 10.5 0.767 0.11008 -0.089 0.001 0.997 0.001 0.997 6.963 -0.429 0.366 11.0 0.761 0.12088 -0.091 0.001 0.997 0.001 0.997 6.295 -0.054 0.370 11.5 0.751 0.14158 -0.093 0.001 0.997 0.001 0.997 5.304 0.052 0.374 12.0 0.737 0.15460 -0.096 0.001 0.997 0.001 0.997 4.768 0.102 0.380 12.5 0.719 0.15698 -0.098 0.001 0.997 0.002 0.997 4.581 0.126 0.386 13.0 0.699 0.17476 -0.100 0.001 0.996 0.002 0.996 3.999 0.141 0.394 13.5 0.676 0.18870 -0.103 0.001 0.996 0.002 0.996 3.582 0.151 0.402 14.0 0.651 0.20510 -0.105 0.001 0.996 0.002 0.996 3.174 0.158 0.412 14.5 0.624 0.21861 -0.108 0.001 0.996 0.002 0.996 2.856 0.162 0.422 15.0 0.598 0.24447 -0.110 0.001 0.996 0.002 0.996 2.444 0.163 0.434 Name = AG08 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 -0.321 0.22756 0.026 1.000 0.002 1.000 0.004 -1.409 0.086 0.333 -14.5 -0.333 0.20936 0.024 1.000 0.002 1.000 0.004 -1.592 0.082 0.323 -14.0 -0.345 0.19865 0.022 1.000 0.002 1.000 0.004 -1.739 0.071 0.315 -13.5 -0.357 0.21008 0.020 1.000 0.002 1.000 0.003 -1.698 0.044 0.307 -13.0 -0.366 0.19117 0.018 1.000 0.002 1.000 0.003 -1.914 -0.006 0.299 -12.5 -0.373 0.16898 0.016 1.000 0.002 1.000 0.003 -2.209 -0.080 0.293 -12.0 -0.379 0.16086 0.014 1.000 0.002 1.000 0.003 -2.354 -0.223 0.287 -11.5 -0.382 0.14572 0.012 1.000 0.002 1.000 0.003 -2.623 -0.666 0.281 -11.0 -0.383 0.13143 0.010 1.000 0.001 1.000 0.003 -2.917 8.632 0.275 -10.5 -0.382 0.11905 0.007 1.000 0.001 1.000 0.003 -3.206 0.923 0.269 -10.0 -0.377 0.10707 0.005 1.000 0.001 1.000 0.003 -3.521 0.582 0.264 -9.5 -0.369 0.09632 0.003 1.000 0.002 1.000 0.003 -3.828 0.472 0.258 -9.0 -0.357 0.08910 0.001 1.000 0.001 1.000 0.003 -4.011 0.418 0.252 -8.5 -0.343 0.08069 -0.001 1.000 0.001 1.000 0.002 -4.247 0.383 0.246 -8.0 -0.324 0.07178 -0.004 1.000 0.001 1.000 0.002 -4.520 0.361 0.239 -7.5 -0.303 0.06462 -0.006 1.000 0.001 1.000 0.002 -4.692 0.347 0.231 -7.0 -0.279 0.05806 -0.008 1.000 0.001 1.000 0.002 -4.802 0.336 0.222 -6.5 -0.252 0.05165 -0.010 1.000 0.001 1.000 0.002 -4.877 0.328 0.210 -6.0 -0.222 0.04620 -0.012 1.000 0.002 1.000 0.002 -4.808 0.322 0.194 -5.5 -0.190 0.04082 -0.015 1.000 0.002 1.000 0.003 -4.657 0.317 0.173 -5.0 -0.156 0.03645 -0.017 1.000 0.002 1.000 0.003 -4.283 0.314 0.142 -4.5 -0.121 0.03244 -0.019 1.000 0.002 1.000 0.004 -3.717 0.312 0.092 -4.0 -0.084 0.02900 -0.021 1.000 0.003 1.000 0.005 -2.890 0.310 -0.004 -3.5 -0.046 0.02614 -0.024 1.000 0.004 1.000 0.006 -1.743 0.306 -0.266 -3.0 -0.004 0.02444 -0.026 0.961 0.006 1.000 0.012 -0.176 -0.119 -5.730 -2.5 -0.087 0.02943 -0.039 0.941 0.014 1.000 0.998 -2.971 -0.266 -0.196 -2.0 -0.030 0.03014 -0.039 0.921 0.037 1.000 0.998 -1.002 0.252 -1.044 -1.5 0.024 0.03030 -0.039 0.896 0.092 1.000 0.998 0.799 0.252 1.870 -1.0 0.082 0.01682 -0.039 0.863 0.996 1.000 0.997 4.871 0.252 0.730 -0.5 0.140 0.01749 -0.039 0.820 0.996 1.000 0.997 7.982 0.252 0.532 0.0 0.197 0.01846 -0.040 0.767 0.996 1.000 0.997 10.686 0.252 0.450 0.5 0.255 0.01934 -0.040 0.700 0.996 1.000 0.997 13.184 0.252 0.406 1.0 0.313 0.02067 -0.040 0.632 0.996 1.000 0.996 15.119 0.252 0.377 1.5 0.370 0.02230 -0.040 0.547 0.996 1.000 0.996 16.600 0.252 0.358 2.0 0.428 0.02463 -0.040 0.399 0.996 1.000 0.996 17.363 0.252 0.344 2.5 0.485 0.02567 -0.040 0.292 0.996 1.000 0.996 18.896 0.252 0.333 3.0 0.542 0.02640 -0.040 0.234 0.997 1.000 0.997 20.542 0.253 0.324 3.5 0.599 0.02735 -0.040 0.178 0.996 1.000 0.996 21.904 0.253 0.318 4.0 0.655 0.02768 -0.041 0.136 0.996 1.000 0.996 23.677 0.253 0.312 4.5 0.711 0.02880 -0.041 0.088 0.997 1.000 0.997 24.680 0.253 0.307 5.0 0.765 0.02891 -0.041 0.032 0.997 1.000 0.997 26.453 0.068 0.304 5.5 0.576 0.03345 -0.065 0.002 0.997 0.007 0.997 17.222 0.073 0.363 6.0 0.614 0.03607 -0.068 0.002 0.996 0.004 0.997 17.031 0.315 0.360 6.5 0.646 0.03978 -0.070 0.001 0.997 0.003 0.997 16.242 0.327 0.358 7.0 0.675 0.04444 -0.072 0.001 0.997 0.002 0.997 15.181 0.337 0.357 7.5 0.700 0.04915 -0.075 0.001 0.996 0.002 0.997 14.244 0.349 0.356 8.0 0.722 0.05432 -0.077 0.001 0.996 0.001 0.996 13.288 0.370 0.356 8.5 0.739 0.06123 -0.079 0.001 0.996 0.001 0.996 12.074 0.404 0.357 9.0 0.752 0.07055 -0.082 0.001 0.997 0.001 0.997 10.666 0.454 0.358 9.5 0.762 0.07922 -0.084 0.001 0.997 0.001 0.997 9.622 0.563 0.360 10.0 0.768 0.08836 -0.086 0.001 0.997 0.001 0.997 8.686 1.370 0.362 10.5 0.767 0.09508 -0.089 0.001 0.997 0.001 0.997 8.062 -0.437 0.366 11.0 0.761 0.10139 -0.091 0.001 0.997 0.002 0.997 7.502 -0.054 0.370 11.5 0.751 0.11977 -0.093 0.001 0.997 0.001 0.997 6.270 0.052 0.374 12.0 0.737 0.12602 -0.096 0.001 0.997 0.002 0.997 5.847 0.102 0.380 12.5 0.719 0.13098 -0.098 0.001 0.997 0.002 0.997 5.490 0.126 0.386 13.0 0.699 0.14581 -0.100 0.001 0.996 0.002 0.996 4.793 0.141 0.394 13.5 0.676 0.16497 -0.103 0.001 0.996 0.002 0.996 4.096 0.152 0.402 14.0 0.651 0.17838 -0.105 0.001 0.996 0.002 0.996 3.649 0.158 0.412 14.5 0.624 0.19666 -0.108 0.001 0.996 0.002 0.996 3.173 0.162 0.422 15.0 0.597 0.20915 -0.110 0.001 0.996 0.002 0.996 2.856 0.163 0.434 Name = AG08 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 -0.320 0.21033 0.026 1.000 0.002 1.000 0.004 -1.524 0.086 0.333 -14.5 -0.333 0.19516 0.024 1.000 0.002 1.000 0.004 -1.707 0.082 0.323 -14.0 -0.345 0.17688 0.022 1.000 0.002 1.000 0.004 -1.952 0.071 0.315 -13.5 -0.357 0.16292 0.020 1.000 0.002 1.000 0.004 -2.189 0.044 0.307 -13.0 -0.366 0.15088 0.018 1.000 0.002 1.000 0.004 -2.424 -0.008 0.299 -12.5 -0.373 0.13871 0.016 1.000 0.002 1.000 0.004 -2.689 -0.080 0.293 -12.0 -0.379 0.14475 0.014 1.000 0.002 1.000 0.004 -2.616 -0.222 0.287 -11.5 -0.382 0.13232 0.012 1.000 0.002 1.000 0.003 -2.888 -0.676 0.281 -11.0 -0.383 0.12024 0.010 1.000 0.001 1.000 0.003 -3.188 8.303 0.275 -10.5 -0.382 0.10977 0.007 1.000 0.001 1.000 0.003 -3.476 0.921 0.269 -10.0 -0.377 0.09945 0.005 1.000 0.001 1.000 0.003 -3.789 0.582 0.264 -9.5 -0.369 0.08945 0.003 1.000 0.002 1.000 0.003 -4.120 0.474 0.258 -9.0 -0.357 0.07979 0.001 1.000 0.001 1.000 0.003 -4.479 0.420 0.252 -8.5 -0.343 0.07279 -0.001 1.000 0.001 1.000 0.002 -4.708 0.383 0.246 -8.0 -0.324 0.06523 -0.004 1.000 0.001 1.000 0.002 -4.974 0.361 0.239 -7.5 -0.303 0.05912 -0.006 1.000 0.001 1.000 0.002 -5.129 0.347 0.231 -7.0 -0.279 0.05319 -0.008 1.000 0.001 1.000 0.002 -5.242 0.336 0.222 -6.5 -0.252 0.04777 -0.010 1.000 0.001 1.000 0.002 -5.273 0.328 0.210 -6.0 -0.222 0.04289 -0.012 1.000 0.002 1.000 0.002 -5.179 0.322 0.194 -5.5 -0.190 0.03879 -0.015 1.000 0.002 1.000 0.003 -4.894 0.317 0.173 -5.0 -0.156 0.03457 -0.017 1.000 0.002 1.000 0.003 -4.507 0.314 0.142 -4.5 -0.120 0.03068 -0.019 1.000 0.002 1.000 0.004 -3.922 0.312 0.092 -4.0 -0.084 0.02741 -0.021 1.000 0.003 1.000 0.005 -3.049 0.310 -0.005 -3.5 -0.045 0.02473 -0.024 1.000 0.004 1.000 0.007 -1.826 0.304 -0.271 -3.0 -0.003 0.02338 -0.026 0.961 0.006 1.000 0.015 -0.108 -0.115 -9.941 -2.5 -0.088 0.02899 -0.039 0.941 0.014 1.000 0.998 -3.020 -0.233 -0.195 -2.0 -0.030 0.02953 -0.039 0.921 0.037 1.000 0.998 -1.026 0.252 -1.040 -1.5 0.024 0.02961 -0.039 0.896 0.092 1.000 0.998 0.817 0.252 1.870 -1.0 0.082 0.01506 -0.039 0.863 0.996 1.000 0.997 5.439 0.252 0.730 -0.5 0.140 0.01592 -0.039 0.820 0.996 1.000 0.997 8.771 0.252 0.532 0.0 0.197 0.01675 -0.040 0.767 0.996 1.000 0.997 11.781 0.252 0.450 0.5 0.255 0.01794 -0.040 0.700 0.996 1.000 0.997 14.210 0.252 0.406 1.0 0.313 0.01927 -0.040 0.632 0.996 1.000 0.996 16.222 0.252 0.377 1.5 0.370 0.02055 -0.040 0.547 0.996 1.000 0.996 18.012 0.252 0.358 2.0 0.428 0.02304 -0.040 0.399 0.996 1.000 0.996 18.562 0.252 0.344 2.5 0.485 0.02417 -0.040 0.292 0.996 1.000 0.996 20.069 0.252 0.333 3.0 0.542 0.02497 -0.040 0.234 0.997 1.000 0.997 21.719 0.253 0.324 3.5 0.599 0.02600 -0.040 0.178 0.996 1.000 0.996 23.041 0.253 0.318 4.0 0.655 0.02636 -0.041 0.136 0.996 1.000 0.996 24.863 0.253 0.312 4.5 0.711 0.02693 -0.041 0.088 0.997 1.000 0.997 26.391 0.253 0.307 5.0 0.765 0.02781 -0.041 0.032 0.997 1.000 0.997 27.495 0.253 0.304 5.5 0.817 0.02779 -0.041 0.002 0.997 1.000 0.997 29.399 0.074 0.300 6.0 0.614 0.03451 -0.068 0.002 0.996 0.004 0.997 17.786 0.082 0.360 6.5 0.646 0.03784 -0.070 0.001 0.997 0.003 0.997 17.067 0.326 0.358 7.0 0.675 0.04177 -0.072 0.001 0.997 0.002 0.997 16.152 0.336 0.357 7.5 0.700 0.04612 -0.075 0.001 0.996 0.002 0.997 15.178 0.350 0.356 8.0 0.721 0.05245 -0.077 0.001 0.996 0.001 0.996 13.753 0.370 0.357 8.5 0.739 0.05686 -0.079 0.001 0.996 0.001 0.996 13.000 0.402 0.357 9.0 0.752 0.06460 -0.082 0.001 0.997 0.001 0.997 11.648 0.454 0.358 9.5 0.762 0.07233 -0.084 0.001 0.997 0.001 0.997 10.539 0.563 0.360 10.0 0.768 0.08030 -0.086 0.001 0.997 0.001 0.997 9.559 1.456 0.362 10.5 0.766 0.08503 -0.089 0.001 0.997 0.002 0.997 9.011 -0.437 0.366 11.0 0.761 0.09145 -0.091 0.001 0.997 0.002 0.997 8.318 -0.054 0.370 11.5 0.751 0.10440 -0.093 0.001 0.997 0.002 0.997 7.191 0.052 0.374 12.0 0.737 0.11197 -0.096 0.001 0.997 0.002 0.997 6.580 0.101 0.380 12.5 0.719 0.12087 -0.098 0.001 0.997 0.002 0.997 5.947 0.126 0.386 13.0 0.699 0.13457 -0.100 0.001 0.996 0.002 0.996 5.192 0.141 0.394 13.5 0.675 0.15107 -0.103 0.001 0.996 0.002 0.996 4.471 0.152 0.402 14.0 0.651 0.16261 -0.105 0.001 0.996 0.002 0.996 4.001 0.158 0.412 14.5 0.624 0.17570 -0.108 0.001 0.996 0.002 0.996 3.551 0.162 0.422 15.0 0.597 0.19719 -0.110 0.001 0.996 0.002 0.996 3.028 0.163 0.434