Name = AG16 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 -0.322 0.29594 0.014 1.000 0.002 1.000 0.003 -1.087 0.045 0.293 -14.5 -0.332 0.39046 0.012 1.000 0.002 1.000 0.003 -0.851 0.036 0.285 -14.0 -0.342 0.25109 0.010 1.000 0.002 1.000 0.003 -1.362 0.014 0.278 -13.5 -0.351 0.31008 0.007 1.000 0.002 1.000 0.003 -1.131 -0.022 0.271 -13.0 -0.358 0.22181 0.005 1.000 0.002 1.000 0.003 -1.614 -0.086 0.265 -12.5 -0.364 0.25966 0.003 1.000 0.002 1.000 0.003 -1.401 -0.211 0.258 -12.0 -0.368 0.22597 0.001 1.000 0.002 1.000 0.003 -1.627 -0.655 0.252 -11.5 -0.369 0.20613 -0.001 1.000 0.002 1.000 0.003 -1.789 12.778 0.246 -11.0 -0.367 0.19537 -0.004 1.000 0.002 1.000 0.003 -1.880 1.066 0.240 -10.5 -0.363 0.16932 -0.006 1.000 0.002 1.000 0.003 -2.145 0.648 0.234 -10.0 -0.356 0.14575 -0.008 1.000 0.002 1.000 0.002 -2.443 0.500 0.227 -9.5 -0.345 0.13470 -0.010 1.000 0.002 1.000 0.002 -2.563 0.430 0.220 -9.0 -0.331 0.11909 -0.013 1.000 0.002 1.000 0.002 -2.780 0.395 0.212 -8.5 -0.314 0.10529 -0.015 1.000 0.001 1.000 0.002 -2.982 0.371 0.202 -8.0 -0.293 0.09454 -0.017 1.000 0.001 1.000 0.002 -3.103 0.352 0.191 -7.5 -0.269 0.08241 -0.020 1.000 0.001 1.000 0.002 -3.268 0.341 0.178 -7.0 -0.243 0.07321 -0.022 1.000 0.001 1.000 0.002 -3.321 0.332 0.160 -6.5 -0.214 0.06379 -0.024 1.000 0.001 1.000 0.002 -3.349 0.325 0.137 -6.0 -0.182 0.05770 -0.026 1.000 0.001 1.000 0.002 -3.155 0.321 0.105 -5.5 -0.149 0.05035 -0.029 1.000 0.001 1.000 0.002 -2.960 0.317 0.057 -5.0 -0.114 0.04458 -0.031 1.000 0.002 1.000 0.002 -2.553 0.315 -0.022 -4.5 -0.078 0.03960 -0.033 1.000 0.002 1.000 0.003 -1.961 0.313 -0.179 -4.0 -0.041 0.03516 -0.036 1.000 0.002 1.000 0.003 -1.158 0.311 -0.625 -3.5 -0.002 0.03208 -0.038 0.952 0.003 1.000 0.004 -0.074 0.179 -15.778 -3.0 -0.105 0.02974 -0.040 0.913 0.005 1.000 0.008 -3.530 -0.163 -0.133 -2.5 -0.040 0.03487 -0.053 0.879 0.160 1.000 0.996 -1.142 0.361 -1.091 -2.0 0.016 0.03461 -0.054 0.844 0.224 1.000 0.996 0.457 0.253 3.642 -1.5 0.074 0.03478 -0.054 0.801 0.281 1.000 0.996 2.123 0.253 0.978 -1.0 0.132 0.03498 -0.054 0.743 0.374 1.000 0.996 3.770 0.253 0.659 -0.5 0.190 0.03431 -0.054 0.677 0.479 1.000 0.996 5.535 0.253 0.535 0.0 0.248 0.02846 -0.054 0.621 0.995 1.000 0.995 8.709 0.253 0.469 0.5 0.306 0.02933 -0.055 0.566 0.995 1.000 0.995 10.426 0.253 0.428 1.0 0.364 0.03005 -0.055 0.514 0.995 1.000 0.995 12.103 0.253 0.400 1.5 0.422 0.03053 -0.055 0.458 0.995 1.000 0.995 13.809 0.253 0.380 2.0 0.479 0.03095 -0.055 0.403 0.995 1.000 0.995 15.488 0.253 0.365 2.5 0.537 0.03192 -0.055 0.347 0.995 1.000 0.995 16.824 0.253 0.353 3.0 0.595 0.03204 -0.055 0.292 0.995 1.000 0.995 18.557 0.253 0.343 3.5 0.652 0.03269 -0.056 0.227 0.995 1.000 0.995 19.941 0.253 0.335 4.0 0.709 0.03314 -0.056 0.167 0.995 1.000 0.995 21.383 0.253 0.329 4.5 0.764 0.03292 -0.056 0.113 0.995 1.000 0.995 23.210 0.254 0.323 5.0 0.818 0.03256 -0.056 0.061 0.996 1.000 0.996 25.132 3.348 0.319 5.5 0.769 0.03151 -0.070 0.016 0.996 0.776 0.996 24.397 0.073 0.341 6.0 0.668 0.04329 -0.083 0.001 0.996 0.003 0.996 15.427 0.026 0.374 6.5 0.701 0.04792 -0.085 0.001 0.995 0.001 0.995 14.636 0.326 0.371 7.0 0.730 0.05537 -0.087 0.001 0.995 0.001 0.995 13.178 0.340 0.370 7.5 0.754 0.06163 -0.090 0.001 0.995 0.001 0.995 12.231 0.359 0.369 8.0 0.773 0.07224 -0.092 0.001 0.995 0.001 0.995 10.704 0.388 0.369 8.5 0.788 0.08535 -0.095 0.001 0.995 0.001 0.995 9.235 0.436 0.370 9.0 0.799 0.09581 -0.097 0.001 0.995 0.001 0.995 8.338 0.547 0.371 9.5 0.804 0.10900 -0.099 0.000 0.995 0.001 0.995 7.378 1.133 0.374 10.0 0.804 0.12858 -0.102 0.000 0.995 0.001 0.995 6.255 -0.774 0.376 10.5 0.800 0.14259 -0.104 0.001 0.995 0.001 0.995 5.607 -0.077 0.380 11.0 0.790 0.14069 -0.106 0.001 0.995 0.001 0.995 5.613 0.050 0.385 11.5 0.776 0.14812 -0.109 0.001 0.995 0.001 0.995 5.237 0.102 0.390 12.0 0.758 0.16972 -0.111 0.001 0.995 0.001 0.995 4.464 0.130 0.397 12.5 0.736 0.19205 -0.114 0.001 0.995 0.001 0.995 3.833 0.147 0.404 13.0 0.712 0.19883 -0.116 0.001 0.995 0.001 0.995 3.581 0.157 0.413 13.5 0.685 0.22581 -0.118 0.001 0.995 0.002 0.995 3.034 0.164 0.423 14.0 0.657 0.25906 -0.121 0.001 0.995 0.002 0.995 2.536 0.168 0.434 14.5 0.628 0.26866 -0.123 0.001 0.995 0.002 0.995 2.338 0.170 0.446 15.0 0.598 0.30707 -0.125 0.001 0.996 0.002 0.996 1.948 0.171 0.460 Name = AG16 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 0.22725 0.014 1.000 0.002 1.000 0.004 -1.415 0.045 0.294 -14.5 -0.332 0.20430 0.012 1.000 0.002 1.000 0.003 -1.626 0.036 0.286 -14.0 -0.342 0.18238 0.010 1.000 0.002 1.000 0.003 -1.875 0.013 0.278 -13.5 -0.351 0.17626 0.007 1.000 0.002 1.000 0.003 -1.989 -0.024 0.271 -13.0 -0.358 0.17307 0.005 1.000 0.002 1.000 0.003 -2.068 -0.087 0.265 -12.5 -0.364 0.15495 0.003 1.000 0.002 1.000 0.003 -2.347 -0.216 0.258 -12.0 -0.367 0.17877 0.001 1.000 0.002 1.000 0.003 -2.056 -0.660 0.252 -11.5 -0.369 0.12685 -0.001 1.000 0.002 1.000 0.003 -2.906 34.962 0.246 -11.0 -0.367 0.14277 -0.004 1.000 0.002 1.000 0.003 -2.573 1.052 0.240 -10.5 -0.363 0.13685 -0.006 1.000 0.002 1.000 0.003 -2.653 0.638 0.234 -10.0 -0.356 0.11951 -0.008 1.000 0.002 1.000 0.003 -2.977 0.502 0.227 -9.5 -0.345 0.10630 -0.010 1.000 0.002 1.000 0.003 -3.246 0.433 0.220 -9.0 -0.331 0.09132 -0.013 1.000 0.002 1.000 0.002 -3.625 0.395 0.212 -8.5 -0.314 0.08286 -0.015 1.000 0.001 1.000 0.002 -3.787 0.370 0.202 -8.0 -0.293 0.07660 -0.017 1.000 0.001 1.000 0.002 -3.827 0.352 0.191 -7.5 -0.269 0.06546 -0.020 1.000 0.001 1.000 0.002 -4.114 0.341 0.178 -7.0 -0.243 0.06039 -0.022 1.000 0.001 1.000 0.002 -4.023 0.332 0.160 -6.5 -0.213 0.05319 -0.024 1.000 0.001 1.000 0.002 -4.012 0.325 0.137 -6.0 -0.182 0.04682 -0.026 1.000 0.001 1.000 0.002 -3.888 0.321 0.105 -5.5 -0.149 0.04244 -0.029 1.000 0.001 1.000 0.002 -3.507 0.317 0.057 -5.0 -0.114 0.03688 -0.031 1.000 0.002 1.000 0.002 -3.086 0.315 -0.022 -4.5 -0.078 0.03294 -0.033 1.000 0.002 1.000 0.003 -2.358 0.313 -0.179 -4.0 -0.040 0.02968 -0.036 1.000 0.002 1.000 0.003 -1.364 0.311 -0.630 -3.5 -0.002 0.02689 -0.038 0.952 0.003 1.000 0.004 -0.075 0.179 -18.541 -3.0 -0.105 0.02551 -0.040 0.913 0.005 1.000 0.011 -4.115 -0.160 -0.133 -2.5 -0.040 0.03017 -0.053 0.879 0.160 1.000 0.996 -1.321 0.361 -1.091 -2.0 0.016 0.02984 -0.054 0.844 0.224 1.000 0.996 0.529 0.253 3.642 -1.5 0.074 0.02988 -0.054 0.801 0.281 1.000 0.996 2.471 0.253 0.978 -1.0 0.132 0.02967 -0.054 0.743 0.374 1.000 0.996 4.445 0.253 0.659 -0.5 0.190 0.02966 -0.054 0.677 0.479 1.000 0.996 6.403 0.253 0.535 0.0 0.248 0.02292 -0.054 0.621 0.995 1.000 0.995 10.817 0.253 0.469 0.5 0.306 0.02379 -0.055 0.566 0.995 1.000 0.995 12.856 0.253 0.428 1.0 0.364 0.02487 -0.055 0.514 0.995 1.000 0.995 14.626 0.253 0.400 1.5 0.422 0.02550 -0.055 0.458 0.995 1.000 0.995 16.534 0.253 0.380 2.0 0.479 0.02643 -0.055 0.403 0.995 1.000 0.995 18.137 0.253 0.365 2.5 0.537 0.02711 -0.055 0.347 0.995 1.000 0.995 19.813 0.253 0.353 3.0 0.595 0.02783 -0.055 0.292 0.995 1.000 0.995 21.367 0.253 0.343 3.5 0.652 0.02876 -0.056 0.227 0.995 1.000 0.995 22.666 0.253 0.335 4.0 0.709 0.02945 -0.056 0.167 0.995 1.000 0.995 24.066 0.253 0.329 4.5 0.764 0.02983 -0.056 0.113 0.995 1.000 0.995 25.614 0.254 0.323 5.0 0.818 0.03017 -0.056 0.061 0.996 1.000 0.996 27.124 0.254 0.319 5.5 0.871 0.03037 -0.056 0.016 0.996 1.000 0.996 28.660 0.076 0.315 6.0 0.665 0.03782 -0.083 0.001 0.996 0.004 0.996 17.579 0.081 0.375 6.5 0.701 0.04143 -0.085 0.001 0.995 0.002 0.995 16.913 0.322 0.371 7.0 0.730 0.04639 -0.087 0.001 0.995 0.001 0.995 15.730 0.339 0.370 7.5 0.754 0.05126 -0.090 0.001 0.995 0.001 0.995 14.703 0.359 0.369 8.0 0.773 0.05890 -0.092 0.001 0.995 0.001 0.995 13.130 0.388 0.369 8.5 0.788 0.06810 -0.095 0.001 0.995 0.001 0.995 11.575 0.438 0.370 9.0 0.799 0.07909 -0.097 0.001 0.995 0.001 0.995 10.096 0.553 0.371 9.5 0.804 0.08858 -0.099 0.000 0.995 0.001 0.995 9.075 1.084 0.374 10.0 0.804 0.09843 -0.102 0.000 0.995 0.001 0.995 8.170 -0.788 0.376 10.5 0.799 0.11357 -0.104 0.001 0.995 0.001 0.995 7.038 -0.077 0.380 11.0 0.790 0.10738 -0.106 0.001 0.995 0.001 0.995 7.354 0.051 0.385 11.5 0.775 0.12113 -0.109 0.001 0.995 0.001 0.995 6.402 0.102 0.390 12.0 0.758 0.12785 -0.111 0.001 0.995 0.001 0.995 5.926 0.130 0.397 12.5 0.736 0.14313 -0.114 0.001 0.995 0.001 0.995 5.143 0.147 0.404 13.0 0.712 0.15934 -0.116 0.001 0.995 0.002 0.995 4.466 0.157 0.413 13.5 0.685 0.17776 -0.118 0.001 0.995 0.002 0.995 3.853 0.164 0.423 14.0 0.657 0.18435 -0.121 0.001 0.995 0.002 0.995 3.563 0.168 0.434 14.5 0.628 0.21174 -0.123 0.001 0.995 0.002 0.995 2.965 0.170 0.446 15.0 0.598 0.23602 -0.125 0.001 0.996 0.002 0.996 2.534 0.171 0.460 Name = AG16 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 0.19796 0.014 1.000 0.002 1.000 0.004 -1.623 0.044 0.294 -14.5 -0.332 0.18015 0.012 1.000 0.002 1.000 0.004 -1.843 0.036 0.286 -14.0 -0.342 0.16230 0.010 1.000 0.002 1.000 0.004 -2.106 0.014 0.278 -13.5 -0.351 0.14757 0.007 1.000 0.002 1.000 0.003 -2.376 -0.023 0.271 -13.0 -0.358 0.14203 0.005 1.000 0.002 1.000 0.003 -2.520 -0.090 0.265 -12.5 -0.364 0.13851 0.003 1.000 0.002 1.000 0.003 -2.625 -0.222 0.258 -12.0 -0.367 0.12597 0.001 1.000 0.002 1.000 0.003 -2.916 -0.665 0.252 -11.5 -0.368 0.11473 -0.001 1.000 0.002 1.000 0.003 -3.211 29.040 0.246 -11.0 -0.367 0.12806 -0.004 1.000 0.002 1.000 0.003 -2.867 1.079 0.240 -10.5 -0.363 0.11486 -0.006 1.000 0.002 1.000 0.003 -3.160 0.645 0.234 -10.0 -0.356 0.10194 -0.008 1.000 0.002 1.000 0.003 -3.490 0.502 0.227 -9.5 -0.345 0.09107 -0.010 1.000 0.002 1.000 0.003 -3.789 0.430 0.220 -9.0 -0.331 0.08399 -0.013 1.000 0.002 1.000 0.003 -3.937 0.393 0.212 -8.5 -0.313 0.07679 -0.015 1.000 0.001 1.000 0.002 -4.083 0.371 0.202 -8.0 -0.293 0.06788 -0.017 1.000 0.001 1.000 0.002 -4.317 0.353 0.191 -7.5 -0.269 0.05881 -0.020 1.000 0.001 1.000 0.002 -4.576 0.341 0.178 -7.0 -0.243 0.05346 -0.022 1.000 0.001 1.000 0.002 -4.544 0.332 0.160 -6.5 -0.213 0.04740 -0.024 1.000 0.001 1.000 0.002 -4.502 0.325 0.137 -6.0 -0.182 0.04206 -0.026 1.000 0.001 1.000 0.002 -4.328 0.321 0.105 -5.5 -0.149 0.03819 -0.029 1.000 0.001 1.000 0.002 -3.897 0.317 0.057 -5.0 -0.114 0.03349 -0.031 1.000 0.002 1.000 0.002 -3.398 0.315 -0.022 -4.5 -0.078 0.03000 -0.033 1.000 0.002 1.000 0.003 -2.589 0.313 -0.179 -4.0 -0.040 0.02704 -0.036 1.000 0.002 1.000 0.003 -1.497 0.311 -0.630 -3.5 -0.002 0.02484 -0.038 0.952 0.003 1.000 0.004 -0.067 -0.059 -22.456 -3.0 -0.097 0.02823 -0.053 0.913 0.005 1.000 0.996 -3.453 -0.156 -0.296 -2.5 -0.040 0.02765 -0.053 0.879 0.160 1.000 0.996 -1.441 0.253 -1.090 -2.0 0.016 0.02759 -0.054 0.844 0.224 1.000 0.996 0.573 0.253 3.642 -1.5 0.074 0.02769 -0.054 0.801 0.281 1.000 0.996 2.667 0.253 0.978 -1.0 0.132 0.02732 -0.054 0.743 0.374 1.000 0.996 4.827 0.253 0.659 -0.5 0.190 0.02738 -0.054 0.677 0.479 1.000 0.996 6.935 0.253 0.535 0.0 0.248 0.02036 -0.054 0.621 0.995 1.000 0.995 12.173 0.253 0.469 0.5 0.306 0.02127 -0.055 0.566 0.995 1.000 0.995 14.379 0.253 0.428 1.0 0.364 0.02238 -0.055 0.514 0.995 1.000 0.995 16.255 0.253 0.400 1.5 0.422 0.02311 -0.055 0.458 0.995 1.000 0.995 18.243 0.253 0.380 2.0 0.479 0.02373 -0.055 0.403 0.995 1.000 0.995 20.203 0.253 0.365 2.5 0.537 0.02488 -0.055 0.347 0.995 1.000 0.995 21.589 0.253 0.353 3.0 0.595 0.02570 -0.055 0.292 0.995 1.000 0.995 23.139 0.253 0.343 3.5 0.652 0.02633 -0.056 0.227 0.995 1.000 0.995 24.754 0.253 0.335 4.0 0.709 0.02714 -0.056 0.167 0.995 1.000 0.995 26.114 0.253 0.329 4.5 0.764 0.02763 -0.056 0.113 0.995 1.000 0.995 27.653 0.254 0.323 5.0 0.818 0.02814 -0.056 0.061 0.996 1.000 0.996 29.075 0.254 0.319 5.5 0.871 0.02867 -0.056 0.016 0.996 1.000 0.996 30.368 0.080 0.315 6.0 0.661 0.03548 -0.083 0.001 0.996 0.006 0.996 18.640 0.081 0.375 6.5 0.701 0.03804 -0.085 0.001 0.995 0.002 0.995 18.422 0.318 0.371 7.0 0.730 0.04243 -0.087 0.001 0.995 0.001 0.995 17.198 0.340 0.370 7.5 0.753 0.04769 -0.090 0.001 0.995 0.001 0.995 15.794 0.360 0.369 8.0 0.773 0.05333 -0.092 0.001 0.995 0.001 0.995 14.490 0.385 0.369 8.5 0.788 0.06057 -0.095 0.001 0.995 0.001 0.995 13.014 0.434 0.370 9.0 0.799 0.06955 -0.097 0.001 0.995 0.001 0.995 11.481 0.559 0.371 9.5 0.804 0.08002 -0.099 0.000 0.995 0.001 0.995 10.043 1.159 0.374 10.0 0.804 0.09136 -0.102 0.000 0.995 0.001 0.995 8.798 -0.851 0.377 10.5 0.799 0.09740 -0.104 0.001 0.995 0.001 0.995 8.206 -0.078 0.380 11.0 0.789 0.09896 -0.106 0.001 0.995 0.001 0.995 7.976 0.051 0.385 11.5 0.775 0.10330 -0.109 0.001 0.995 0.001 0.995 7.506 0.102 0.390 12.0 0.757 0.11712 -0.111 0.001 0.995 0.001 0.995 6.466 0.130 0.397 12.5 0.736 0.13020 -0.114 0.001 0.995 0.002 0.995 5.652 0.146 0.404 13.0 0.712 0.13391 -0.116 0.001 0.995 0.002 0.995 5.314 0.157 0.413 13.5 0.685 0.14709 -0.118 0.001 0.995 0.002 0.995 4.656 0.164 0.423 14.0 0.657 0.16241 -0.121 0.001 0.995 0.002 0.995 4.043 0.168 0.434 14.5 0.628 0.17545 -0.123 0.001 0.995 0.002 0.995 3.578 0.170 0.446 15.0 0.598 0.20578 -0.125 0.001 0.996 0.002 0.996 2.905 0.171 0.460 Name = AG16 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 -0.321 0.18086 0.014 1.000 0.002 1.000 0.004 -1.777 0.044 0.294 -14.5 -0.332 0.16623 0.012 1.000 0.002 1.000 0.004 -1.997 0.036 0.286 -14.0 -0.342 0.15091 0.010 1.000 0.002 1.000 0.004 -2.264 0.013 0.278 -13.5 -0.350 0.13830 0.007 1.000 0.002 1.000 0.004 -2.534 -0.023 0.271 -13.0 -0.358 0.13171 0.005 1.000 0.002 1.000 0.004 -2.717 -0.088 0.265 -12.5 -0.364 0.12096 0.003 1.000 0.002 1.000 0.003 -3.006 -0.217 0.258 -12.0 -0.367 0.11130 0.001 1.000 0.002 1.000 0.003 -3.300 -0.665 0.252 -11.5 -0.368 0.10138 -0.001 1.000 0.002 1.000 0.003 -3.634 29.040 0.246 -11.0 -0.367 0.11265 -0.004 1.000 0.002 1.000 0.003 -3.259 1.079 0.240 -10.5 -0.363 0.10213 -0.006 1.000 0.002 1.000 0.003 -3.554 0.634 0.234 -10.0 -0.355 0.09731 -0.008 1.000 0.002 1.000 0.003 -3.653 0.499 0.227 -9.5 -0.345 0.08439 -0.010 1.000 0.002 1.000 0.003 -4.087 0.432 0.220 -9.0 -0.331 0.07564 -0.013 1.000 0.002 1.000 0.003 -4.372 0.394 0.212 -8.5 -0.313 0.06920 -0.015 1.000 0.001 1.000 0.002 -4.530 0.371 0.202 -8.0 -0.293 0.06186 -0.017 1.000 0.001 1.000 0.002 -4.736 0.353 0.191 -7.5 -0.269 0.05423 -0.020 1.000 0.001 1.000 0.002 -4.962 0.341 0.178 -7.0 -0.243 0.04996 -0.022 1.000 0.001 1.000 0.002 -4.859 0.332 0.160 -6.5 -0.213 0.04506 -0.024 1.000 0.001 1.000 0.002 -4.731 0.325 0.137 -6.0 -0.182 0.04008 -0.026 1.000 0.001 1.000 0.002 -4.536 0.322 0.105 -5.5 -0.149 0.03568 -0.029 1.000 0.001 1.000 0.002 -4.171 0.318 0.057 -5.0 -0.114 0.03147 -0.031 1.000 0.002 1.000 0.002 -3.616 0.315 -0.022 -4.5 -0.078 0.02826 -0.033 1.000 0.002 1.000 0.003 -2.749 0.313 -0.179 -4.0 -0.040 0.02548 -0.036 1.000 0.002 1.000 0.003 -1.589 0.310 -0.630 -3.5 -0.001 0.02367 -0.038 0.952 0.003 1.000 0.004 -0.056 -0.059 -28.433 -3.0 -0.097 0.02712 -0.053 0.913 0.005 1.000 0.996 -3.594 -0.152 -0.296 -2.5 -0.040 0.02642 -0.053 0.879 0.160 1.000 0.996 -1.508 0.253 -1.090 -2.0 0.016 0.02637 -0.054 0.844 0.224 1.000 0.997 0.599 0.253 3.643 -1.5 0.074 0.02630 -0.054 0.801 0.281 1.000 0.996 2.807 0.253 0.978 -1.0 0.132 0.02617 -0.054 0.743 0.374 1.000 0.996 5.039 0.253 0.659 -0.5 0.190 0.02574 -0.054 0.677 0.479 1.000 0.996 7.376 0.253 0.535 0.0 0.248 0.01870 -0.054 0.621 0.995 1.000 0.995 13.258 0.253 0.469 0.5 0.306 0.01963 -0.055 0.566 0.995 1.000 0.995 15.578 0.253 0.428 1.0 0.364 0.02075 -0.055 0.514 0.995 1.000 0.995 17.527 0.253 0.400 1.5 0.422 0.02155 -0.055 0.458 0.995 1.000 0.995 19.563 0.253 0.380 2.0 0.479 0.02222 -0.055 0.403 0.995 1.000 0.995 21.574 0.253 0.365 2.5 0.537 0.02302 -0.055 0.347 0.995 1.000 0.995 23.329 0.253 0.353 3.0 0.595 0.02388 -0.055 0.292 0.995 1.000 0.995 24.900 0.253 0.343 3.5 0.652 0.02501 -0.056 0.227 0.995 1.000 0.995 26.058 0.253 0.335 4.0 0.709 0.02589 -0.056 0.167 0.995 1.000 0.995 27.367 0.253 0.329 4.5 0.764 0.02646 -0.056 0.113 0.995 1.000 0.995 28.881 0.254 0.323 5.0 0.818 0.02707 -0.056 0.061 0.996 1.000 0.996 30.225 0.254 0.319 5.5 0.871 0.02731 -0.056 0.016 0.996 1.000 0.996 31.874 0.254 0.315 6.0 0.921 0.02707 -0.057 0.001 0.996 1.000 0.996 34.003 0.081 0.311 6.5 0.700 0.03649 -0.085 0.001 0.995 0.002 0.995 19.185 0.088 0.372 7.0 0.730 0.04008 -0.087 0.001 0.995 0.001 0.995 18.207 0.339 0.370 7.5 0.753 0.04474 -0.090 0.001 0.995 0.001 0.995 16.835 0.360 0.369 8.0 0.773 0.04969 -0.092 0.001 0.995 0.001 0.995 15.552 0.386 0.369 8.5 0.788 0.05764 -0.095 0.001 0.995 0.001 0.995 13.671 0.434 0.370 9.0 0.799 0.06394 -0.097 0.001 0.995 0.001 0.995 12.489 0.553 0.371 9.5 0.804 0.07261 -0.099 0.000 0.995 0.001 0.995 11.068 1.159 0.374 10.0 0.804 0.08209 -0.102 0.000 0.995 0.001 0.995 9.791 -0.748 0.377 10.5 0.799 0.08219 -0.104 0.001 0.995 0.001 0.995 9.720 -0.078 0.380 11.0 0.789 0.08889 -0.106 0.001 0.995 0.001 0.995 8.879 0.051 0.385 11.5 0.775 0.09811 -0.109 0.001 0.995 0.001 0.995 7.900 0.102 0.390 12.0 0.757 0.10447 -0.111 0.001 0.995 0.001 0.995 7.248 0.129 0.397 12.5 0.736 0.11553 -0.114 0.001 0.995 0.002 0.995 6.369 0.147 0.404 13.0 0.711 0.12578 -0.116 0.001 0.995 0.002 0.995 5.655 0.157 0.413 13.5 0.685 0.13691 -0.118 0.001 0.995 0.002 0.995 5.000 0.164 0.423 14.0 0.656 0.14973 -0.121 0.001 0.995 0.002 0.995 4.383 0.168 0.434 14.5 0.628 0.16327 -0.123 0.001 0.995 0.002 0.995 3.843 0.170 0.446 15.0 0.598 0.17640 -0.125 0.001 0.996 0.002 0.996 3.389 0.171 0.460