Name = AG13 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 -0.250 0.34162 0.014 1.000 0.002 1.000 0.004 -0.733 0.057 0.305 -14.5 -0.261 0.33016 0.012 1.000 0.002 1.000 0.004 -0.790 0.054 0.295 -14.0 -0.271 0.29736 0.010 1.000 0.002 1.000 0.004 -0.912 0.046 0.285 -13.5 -0.281 0.25963 0.008 1.000 0.002 1.000 0.004 -1.083 0.033 0.277 -13.0 -0.290 0.24830 0.005 1.000 0.002 1.000 0.004 -1.169 0.010 0.269 -12.5 -0.298 0.23849 0.003 1.000 0.002 1.000 0.004 -1.251 -0.029 0.261 -12.0 -0.305 0.21234 0.001 1.000 0.002 1.000 0.004 -1.437 -0.100 0.254 -11.5 -0.310 0.18814 -0.001 1.000 0.002 1.000 0.003 -1.649 -0.261 0.248 -11.0 -0.313 0.18220 -0.003 1.000 0.002 1.000 0.003 -1.719 -0.816 0.241 -10.5 -0.314 0.23516 -0.005 1.000 0.002 1.000 0.003 -1.336 3.721 0.234 -10.0 -0.312 0.20490 -0.007 1.000 0.002 1.000 0.003 -1.523 0.803 0.227 -9.5 -0.307 0.18755 -0.009 1.000 0.002 1.000 0.003 -1.635 0.557 0.220 -9.0 -0.298 0.14949 -0.011 1.000 0.002 1.000 0.003 -1.995 0.459 0.212 -8.5 -0.286 0.14019 -0.013 1.000 0.002 1.000 0.003 -2.041 0.406 0.203 -8.0 -0.271 0.11905 -0.016 1.000 0.002 1.000 0.002 -2.274 0.377 0.192 -7.5 -0.252 0.10903 -0.018 1.000 0.001 1.000 0.002 -2.312 0.356 0.179 -7.0 -0.230 0.09153 -0.020 1.000 0.001 1.000 0.002 -2.511 0.340 0.163 -6.5 -0.204 0.08029 -0.022 1.000 0.002 1.000 0.002 -2.539 0.329 0.141 -6.0 -0.175 0.06937 -0.024 1.000 0.002 1.000 0.002 -2.528 0.324 0.111 -5.5 -0.145 0.05966 -0.026 1.000 0.002 1.000 0.002 -2.426 0.319 0.067 -5.0 -0.112 0.05209 -0.029 1.000 0.002 1.000 0.002 -2.148 0.315 -0.006 -4.5 -0.078 0.04455 -0.031 1.000 0.002 1.000 0.002 -1.740 0.313 -0.148 -4.0 -0.042 0.03918 -0.033 1.000 0.002 1.000 0.003 -1.070 0.311 -0.538 -3.5 -0.005 0.03437 -0.035 1.000 0.002 1.000 0.003 -0.153 0.181 -6.452 -3.0 -0.106 0.03033 -0.037 1.000 0.003 1.000 0.003 -3.502 0.142 -0.103 -2.5 -0.046 0.02716 -0.040 1.000 0.003 1.000 0.005 -1.694 0.287 -0.612 -2.0 0.014 0.02493 -0.042 1.000 0.005 1.000 0.009 0.547 0.344 3.321 -1.5 0.071 0.03468 -0.051 0.934 0.319 1.000 0.996 2.039 0.327 0.966 -1.0 0.128 0.02628 -0.051 0.889 0.995 1.000 0.995 4.884 0.251 0.645 -0.5 0.186 0.02711 -0.051 0.825 0.995 1.000 0.995 6.857 0.252 0.523 0.0 0.243 0.02808 -0.051 0.725 0.995 1.000 0.995 8.671 0.251 0.459 0.5 0.301 0.02950 -0.051 0.631 0.995 1.000 0.995 10.203 0.251 0.419 1.0 0.358 0.03089 -0.051 0.539 0.995 1.000 0.995 11.601 0.251 0.392 1.5 0.416 0.03183 -0.051 0.463 0.995 1.000 0.995 13.063 0.251 0.373 2.0 0.473 0.03277 -0.051 0.392 0.995 1.000 0.995 14.435 0.251 0.358 2.5 0.530 0.03325 -0.051 0.325 0.995 1.000 0.995 15.947 0.252 0.347 3.0 0.587 0.03432 -0.051 0.247 0.995 1.000 0.995 17.113 0.252 0.337 3.5 0.644 0.03478 -0.051 0.182 0.995 1.000 0.996 18.519 0.252 0.330 4.0 0.701 0.03506 -0.052 0.120 0.995 1.000 0.996 19.979 0.252 0.324 4.5 0.756 0.03510 -0.052 0.068 0.995 1.000 0.995 21.537 0.252 0.318 5.0 0.810 0.03237 -0.052 0.038 0.995 1.000 0.995 25.006 0.098 0.314 5.5 0.591 0.04559 -0.077 0.013 0.996 0.040 0.996 12.974 0.073 0.380 6.0 0.660 0.04392 -0.078 0.001 0.996 0.002 0.996 15.024 0.288 0.369 6.5 0.691 0.04997 -0.080 0.001 0.996 0.002 0.996 13.832 0.328 0.366 7.0 0.719 0.05584 -0.083 0.001 0.996 0.001 0.996 12.870 0.342 0.365 7.5 0.741 0.06447 -0.085 0.001 0.996 0.001 0.996 11.491 0.366 0.365 8.0 0.758 0.07246 -0.087 0.001 0.996 0.001 0.996 10.466 0.398 0.365 8.5 0.772 0.08442 -0.090 0.001 0.996 0.001 0.996 9.143 0.461 0.366 9.0 0.780 0.09725 -0.092 0.000 0.996 0.001 0.996 8.023 0.670 0.368 9.5 0.783 0.10965 -0.094 0.001 0.996 0.001 0.996 7.139 11.771 0.370 10.0 0.781 0.13129 -0.097 0.000 0.996 0.001 0.996 5.946 -0.198 0.374 10.5 0.772 0.14516 -0.099 0.001 0.996 0.001 0.996 5.322 0.024 0.378 11.0 0.760 0.14292 -0.101 0.001 0.996 0.001 0.996 5.319 0.091 0.383 11.5 0.743 0.15736 -0.104 0.001 0.996 0.001 0.996 4.724 0.125 0.389 12.0 0.723 0.17534 -0.106 0.001 0.996 0.001 0.996 4.124 0.145 0.396 12.5 0.699 0.20084 -0.108 0.001 0.996 0.002 0.996 3.481 0.157 0.405 13.0 0.673 0.27864 -0.110 0.001 0.996 0.001 0.996 2.417 0.165 0.414 13.5 0.645 0.23766 -0.113 0.001 0.996 0.002 0.996 2.714 0.169 0.425 14.0 0.616 0.24921 -0.115 0.001 0.996 0.002 0.996 2.471 0.172 0.437 14.5 0.586 0.27499 -0.117 0.001 0.996 0.002 0.996 2.131 0.173 0.450 15.0 0.556 0.31263 -0.120 0.001 0.996 0.002 0.996 1.777 0.173 0.466 Name = AG13 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 -0.250 0.25632 0.014 1.000 0.002 1.000 0.004 -0.976 0.057 0.305 -14.5 -0.261 0.24898 0.012 1.000 0.002 1.000 0.004 -1.047 0.054 0.295 -14.0 -0.271 0.22881 0.010 1.000 0.002 1.000 0.004 -1.185 0.046 0.286 -13.5 -0.281 0.20320 0.008 1.000 0.002 1.000 0.004 -1.383 0.032 0.277 -13.0 -0.290 0.19372 0.006 1.000 0.002 1.000 0.004 -1.498 0.010 0.269 -12.5 -0.298 0.17306 0.003 1.000 0.002 1.000 0.004 -1.724 -0.030 0.261 -12.0 -0.305 0.16570 0.001 1.000 0.002 1.000 0.004 -1.840 -0.102 0.254 -11.5 -0.310 0.14942 -0.001 1.000 0.002 1.000 0.004 -2.076 -0.257 0.248 -11.0 -0.313 0.13434 -0.003 1.000 0.002 1.000 0.003 -2.332 -0.842 0.241 -10.5 -0.314 0.18468 -0.005 1.000 0.002 1.000 0.003 -1.700 3.187 0.234 -10.0 -0.312 0.15973 -0.007 1.000 0.002 1.000 0.003 -1.952 0.819 0.227 -9.5 -0.307 0.13583 -0.009 1.000 0.002 1.000 0.003 -2.257 0.556 0.220 -9.0 -0.298 0.12044 -0.011 1.000 0.002 1.000 0.003 -2.474 0.459 0.212 -8.5 -0.286 0.10451 -0.013 1.000 0.002 1.000 0.003 -2.738 0.406 0.203 -8.0 -0.270 0.09692 -0.016 1.000 0.002 1.000 0.003 -2.790 0.376 0.192 -7.5 -0.252 0.08486 -0.018 1.000 0.001 1.000 0.002 -2.969 0.356 0.179 -7.0 -0.230 0.07484 -0.020 1.000 0.001 1.000 0.002 -3.068 0.340 0.163 -6.5 -0.204 0.06296 -0.022 1.000 0.002 1.000 0.002 -3.238 0.330 0.141 -6.0 -0.175 0.05496 -0.024 1.000 0.002 1.000 0.002 -3.190 0.323 0.111 -5.5 -0.145 0.04930 -0.026 1.000 0.002 1.000 0.002 -2.932 0.319 0.067 -5.0 -0.112 0.04208 -0.029 1.000 0.002 1.000 0.002 -2.658 0.315 -0.006 -4.5 -0.077 0.03731 -0.031 1.000 0.002 1.000 0.003 -2.072 0.313 -0.149 -4.0 -0.042 0.03219 -0.033 1.000 0.002 1.000 0.003 -1.303 0.311 -0.538 -3.5 -0.005 0.02830 -0.035 1.000 0.002 1.000 0.003 -0.186 0.181 -6.452 -3.0 -0.106 0.02496 -0.037 1.000 0.003 1.000 0.003 -4.256 0.142 -0.103 -2.5 -0.046 0.02225 -0.040 1.000 0.003 1.000 0.005 -2.068 0.286 -0.612 -2.0 0.014 0.02065 -0.042 1.000 0.005 1.000 0.015 0.660 0.344 3.318 -1.5 0.071 0.02904 -0.051 0.934 0.319 1.000 0.997 2.435 0.327 0.966 -1.0 0.128 0.01950 -0.051 0.889 0.995 1.000 0.995 6.582 0.251 0.645 -0.5 0.186 0.02050 -0.051 0.825 0.995 1.000 0.995 9.071 0.252 0.523 0.0 0.243 0.02200 -0.051 0.725 0.995 1.000 0.995 11.064 0.251 0.459 0.5 0.301 0.02360 -0.051 0.631 0.995 1.000 0.995 12.754 0.251 0.419 1.0 0.358 0.02503 -0.051 0.539 0.995 1.000 0.995 14.317 0.251 0.392 1.5 0.416 0.02636 -0.051 0.463 0.995 1.000 0.995 15.776 0.251 0.373 2.0 0.473 0.02744 -0.051 0.392 0.995 1.000 0.995 17.242 0.251 0.358 2.5 0.530 0.02814 -0.051 0.325 0.995 1.000 0.995 18.846 0.252 0.347 3.0 0.587 0.02951 -0.051 0.247 0.995 1.000 0.995 19.902 0.252 0.337 3.5 0.644 0.03020 -0.051 0.182 0.995 1.000 0.996 21.326 0.252 0.330 4.0 0.701 0.03081 -0.052 0.120 0.995 1.000 0.996 22.736 0.252 0.324 4.5 0.756 0.03161 -0.052 0.068 0.995 1.000 0.995 23.913 0.252 0.318 5.0 0.810 0.03140 -0.052 0.038 0.995 1.000 0.995 25.781 0.252 0.314 5.5 0.861 0.03069 -0.052 0.013 0.996 1.000 0.996 28.068 0.075 0.310 6.0 0.658 0.03815 -0.078 0.001 0.996 0.003 0.996 17.255 0.082 0.369 6.5 0.691 0.04273 -0.080 0.001 0.996 0.002 0.996 16.164 0.326 0.367 7.0 0.718 0.04761 -0.083 0.001 0.996 0.001 0.996 15.090 0.341 0.365 7.5 0.741 0.05323 -0.085 0.001 0.996 0.001 0.996 13.917 0.366 0.365 8.0 0.758 0.06070 -0.087 0.001 0.996 0.001 0.996 12.489 0.400 0.365 8.5 0.772 0.07018 -0.090 0.001 0.996 0.001 0.996 10.993 0.461 0.366 9.0 0.780 0.07991 -0.092 0.000 0.996 0.001 0.996 9.760 0.668 0.368 9.5 0.783 0.08876 -0.094 0.001 0.996 0.001 0.996 8.817 11.119 0.370 10.0 0.780 0.10228 -0.097 0.000 0.996 0.001 0.996 7.629 -0.210 0.374 10.5 0.772 0.11038 -0.099 0.001 0.996 0.001 0.996 6.998 0.023 0.378 11.0 0.760 0.11064 -0.101 0.001 0.996 0.001 0.996 6.869 0.092 0.383 11.5 0.743 0.12892 -0.104 0.001 0.996 0.002 0.996 5.764 0.125 0.389 12.0 0.723 0.13218 -0.106 0.001 0.996 0.001 0.996 5.470 0.145 0.396 12.5 0.699 0.14769 -0.108 0.001 0.996 0.002 0.996 4.734 0.157 0.405 13.0 0.673 0.20110 -0.110 0.001 0.996 0.001 0.996 3.348 0.165 0.414 13.5 0.645 0.19091 -0.113 0.001 0.996 0.002 0.996 3.377 0.170 0.425 14.0 0.616 0.19806 -0.115 0.001 0.996 0.002 0.996 3.108 0.172 0.437 14.5 0.586 0.21516 -0.117 0.001 0.996 0.002 0.996 2.722 0.173 0.451 15.0 0.555 0.23970 -0.120 0.001 0.996 0.002 0.996 2.317 0.173 0.466 Name = AG13 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 -0.250 0.21938 0.014 1.000 0.002 1.000 0.005 -1.140 0.057 0.305 -14.5 -0.261 0.21420 0.012 1.000 0.002 1.000 0.005 -1.217 0.054 0.295 -14.0 -0.271 0.18619 0.010 1.000 0.002 1.000 0.004 -1.456 0.046 0.286 -13.5 -0.281 0.17945 0.008 1.000 0.002 1.000 0.004 -1.565 0.032 0.277 -13.0 -0.290 0.17074 0.006 1.000 0.002 1.000 0.004 -1.699 0.010 0.269 -12.5 -0.298 0.15422 0.003 1.000 0.002 1.000 0.004 -1.934 -0.030 0.262 -12.0 -0.305 0.14625 0.001 1.000 0.002 1.000 0.004 -2.084 -0.103 0.254 -11.5 -0.310 0.13354 -0.001 1.000 0.002 1.000 0.004 -2.322 -0.258 0.248 -11.0 -0.313 0.12137 -0.003 1.000 0.002 1.000 0.004 -2.580 -0.816 0.241 -10.5 -0.314 0.15186 -0.005 1.000 0.002 1.000 0.003 -2.068 3.138 0.234 -10.0 -0.312 0.10477 -0.007 1.000 0.002 1.000 0.003 -2.975 0.806 0.227 -9.5 -0.306 0.09298 -0.009 1.000 0.002 1.000 0.003 -3.296 0.560 0.220 -9.0 -0.298 0.10101 -0.011 1.000 0.002 1.000 0.003 -2.950 0.458 0.212 -8.5 -0.286 0.09587 -0.013 1.000 0.002 1.000 0.003 -2.982 0.406 0.203 -8.0 -0.270 0.08224 -0.016 1.000 0.002 1.000 0.003 -3.289 0.378 0.192 -7.5 -0.252 0.07310 -0.018 1.000 0.001 1.000 0.002 -3.447 0.356 0.179 -7.0 -0.229 0.06579 -0.020 1.000 0.001 1.000 0.002 -3.488 0.340 0.163 -6.5 -0.204 0.05701 -0.022 1.000 0.002 1.000 0.002 -3.573 0.330 0.141 -6.0 -0.175 0.05003 -0.024 1.000 0.002 1.000 0.002 -3.501 0.324 0.111 -5.5 -0.145 0.04377 -0.026 1.000 0.002 1.000 0.002 -3.303 0.319 0.067 -5.0 -0.112 0.03851 -0.029 1.000 0.002 1.000 0.002 -2.900 0.315 -0.007 -4.5 -0.077 0.03349 -0.031 1.000 0.002 1.000 0.003 -2.308 0.313 -0.149 -4.0 -0.042 0.02939 -0.033 1.000 0.002 1.000 0.003 -1.423 0.311 -0.541 -3.5 -0.005 0.02599 -0.035 1.000 0.002 1.000 0.003 -0.193 0.181 -6.762 -3.0 -0.106 0.02259 -0.037 1.000 0.003 1.000 0.003 -4.702 0.142 -0.103 -2.5 -0.046 0.02021 -0.040 1.000 0.003 1.000 0.005 -2.277 0.360 -0.612 -2.0 0.013 0.02864 -0.051 1.000 0.005 1.000 0.997 0.460 0.344 4.088 -1.5 0.071 0.02644 -0.051 0.934 0.319 1.000 0.997 2.674 0.251 0.966 -1.0 0.128 0.01636 -0.051 0.889 0.995 1.000 0.995 7.844 0.251 0.645 -0.5 0.186 0.01737 -0.051 0.825 0.995 1.000 0.995 10.703 0.252 0.523 0.0 0.243 0.01905 -0.051 0.725 0.995 1.000 0.995 12.779 0.251 0.459 0.5 0.301 0.02074 -0.051 0.631 0.995 1.000 0.995 14.512 0.251 0.419 1.0 0.358 0.02258 -0.051 0.539 0.995 1.000 0.995 15.873 0.251 0.392 1.5 0.416 0.02364 -0.051 0.463 0.995 1.000 0.995 17.589 0.251 0.373 2.0 0.473 0.02473 -0.051 0.392 0.995 1.000 0.995 19.129 0.251 0.358 2.5 0.530 0.02596 -0.051 0.325 0.995 1.000 0.995 20.428 0.252 0.347 3.0 0.587 0.02715 -0.051 0.247 0.995 1.000 0.995 21.637 0.252 0.337 3.5 0.644 0.02787 -0.051 0.182 0.995 1.000 0.996 23.110 0.252 0.330 4.0 0.701 0.02864 -0.052 0.120 0.995 1.000 0.996 24.456 0.252 0.324 4.5 0.756 0.02911 -0.052 0.068 0.995 1.000 0.995 25.963 0.252 0.318 5.0 0.810 0.02946 -0.052 0.038 0.995 1.000 0.995 27.475 0.252 0.314 5.5 0.861 0.02951 -0.052 0.013 0.996 1.000 0.996 29.192 0.078 0.310 6.0 0.656 0.03561 -0.078 0.001 0.996 0.004 0.996 18.421 0.082 0.369 6.5 0.691 0.03899 -0.080 0.001 0.996 0.002 0.996 17.715 0.322 0.367 7.0 0.718 0.04335 -0.083 0.001 0.996 0.001 0.996 16.573 0.342 0.365 7.5 0.740 0.04954 -0.085 0.001 0.996 0.001 0.996 14.946 0.366 0.365 8.0 0.758 0.05432 -0.087 0.001 0.996 0.001 0.996 13.956 0.398 0.365 8.5 0.772 0.06222 -0.090 0.001 0.996 0.001 0.996 12.400 0.461 0.366 9.0 0.780 0.07025 -0.092 0.000 0.996 0.001 0.996 11.102 0.678 0.368 9.5 0.782 0.07987 -0.094 0.001 0.996 0.001 0.996 9.795 11.119 0.371 10.0 0.780 0.08820 -0.097 0.000 0.996 0.001 0.996 8.848 -0.202 0.374 10.5 0.772 0.09095 -0.099 0.001 0.996 0.001 0.996 8.489 0.027 0.378 11.0 0.760 0.10203 -0.101 0.001 0.996 0.002 0.996 7.444 0.090 0.383 11.5 0.743 0.10868 -0.104 0.001 0.996 0.002 0.996 6.837 0.124 0.389 12.0 0.723 0.12123 -0.106 0.001 0.996 0.002 0.996 5.961 0.145 0.396 12.5 0.699 0.13399 -0.108 0.001 0.996 0.002 0.996 5.215 0.157 0.405 13.0 0.673 0.14713 -0.110 0.001 0.996 0.002 0.996 4.574 0.164 0.414 13.5 0.645 0.15845 -0.113 0.001 0.996 0.002 0.996 4.069 0.170 0.425 14.0 0.615 0.17710 -0.115 0.001 0.996 0.002 0.996 3.474 0.172 0.437 14.5 0.585 0.19007 -0.117 0.001 0.996 0.002 0.996 3.080 0.173 0.451 15.0 0.555 0.20870 -0.120 0.001 0.996 0.002 0.996 2.660 0.173 0.466 Name = AG13 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 -0.250 0.19739 0.014 1.000 0.002 1.000 0.005 -1.267 0.057 0.305 -14.5 -0.261 0.19372 0.012 1.000 0.002 1.000 0.005 -1.346 0.053 0.295 -14.0 -0.271 0.17100 0.010 1.000 0.002 1.000 0.004 -1.585 0.045 0.286 -13.5 -0.281 0.16591 0.008 1.000 0.002 1.000 0.004 -1.693 0.032 0.277 -13.0 -0.290 0.15761 0.006 1.000 0.002 1.000 0.004 -1.840 0.009 0.269 -12.5 -0.298 0.14369 0.003 1.000 0.002 1.000 0.004 -2.075 -0.029 0.262 -12.0 -0.305 0.12636 0.001 1.000 0.002 1.000 0.004 -2.413 -0.101 0.254 -11.5 -0.310 0.11667 -0.001 1.000 0.002 1.000 0.004 -2.657 -0.258 0.248 -11.0 -0.313 0.10720 -0.003 1.000 0.002 1.000 0.004 -2.921 -0.849 0.241 -10.5 -0.314 0.10423 -0.005 1.000 0.002 1.000 0.003 -3.011 3.138 0.234 -10.0 -0.312 0.09239 -0.007 1.000 0.002 1.000 0.003 -3.373 0.817 0.227 -9.5 -0.306 0.08299 -0.009 1.000 0.002 1.000 0.003 -3.692 0.556 0.220 -9.0 -0.298 0.09550 -0.011 1.000 0.002 1.000 0.003 -3.118 0.458 0.212 -8.5 -0.286 0.08496 -0.013 1.000 0.002 1.000 0.003 -3.365 0.406 0.203 -8.0 -0.270 0.07821 -0.016 1.000 0.002 1.000 0.003 -3.454 0.378 0.192 -7.5 -0.252 0.06618 -0.018 1.000 0.001 1.000 0.002 -3.807 0.357 0.179 -7.0 -0.229 0.05958 -0.020 1.000 0.001 1.000 0.002 -3.851 0.340 0.163 -6.5 -0.204 0.05211 -0.022 1.000 0.002 1.000 0.002 -3.909 0.330 0.141 -6.0 -0.175 0.04596 -0.024 1.000 0.002 1.000 0.002 -3.811 0.324 0.111 -5.5 -0.145 0.04049 -0.026 1.000 0.002 1.000 0.002 -3.570 0.319 0.067 -5.0 -0.112 0.03572 -0.029 1.000 0.002 1.000 0.002 -3.127 0.315 -0.007 -4.5 -0.077 0.03122 -0.031 1.000 0.002 1.000 0.003 -2.476 0.313 -0.149 -4.0 -0.042 0.02749 -0.033 1.000 0.002 1.000 0.003 -1.521 0.311 -0.541 -3.5 -0.005 0.02432 -0.035 1.000 0.002 1.000 0.003 -0.207 0.182 -6.762 -3.0 -0.106 0.02138 -0.037 1.000 0.003 1.000 0.004 -4.970 0.142 -0.103 -2.5 -0.046 0.01890 -0.040 1.000 0.003 1.000 0.005 -2.435 0.360 -0.612 -2.0 0.013 0.02770 -0.051 1.000 0.005 1.000 0.997 0.476 0.344 4.089 -1.5 0.071 0.02539 -0.051 0.934 0.319 1.000 0.997 2.785 0.251 0.967 -1.0 0.128 0.01454 -0.051 0.889 0.995 1.000 0.995 8.824 0.251 0.645 -0.5 0.186 0.01584 -0.051 0.825 0.995 1.000 0.995 11.737 0.252 0.523 0.0 0.243 0.01752 -0.051 0.725 0.995 1.000 0.995 13.897 0.251 0.459 0.5 0.301 0.01937 -0.051 0.631 0.995 1.000 0.995 15.538 0.251 0.419 1.0 0.358 0.02097 -0.051 0.539 0.995 1.000 0.995 17.096 0.251 0.392 1.5 0.416 0.02205 -0.051 0.463 0.995 1.000 0.995 18.859 0.251 0.373 2.0 0.473 0.02321 -0.051 0.392 0.995 1.000 0.995 20.382 0.251 0.358 2.5 0.530 0.02411 -0.051 0.325 0.995 1.000 0.995 21.994 0.252 0.347 3.0 0.587 0.02536 -0.051 0.247 0.995 1.000 0.995 23.159 0.252 0.337 3.5 0.644 0.02616 -0.051 0.182 0.995 1.000 0.996 24.626 0.252 0.330 4.0 0.701 0.02702 -0.052 0.120 0.995 1.000 0.996 25.927 0.252 0.324 4.5 0.756 0.02805 -0.052 0.068 0.995 1.000 0.995 26.948 0.252 0.318 5.0 0.810 0.02845 -0.052 0.038 0.995 1.000 0.995 28.456 0.252 0.314 5.5 0.861 0.02868 -0.052 0.013 0.996 1.000 0.996 30.031 0.084 0.310 6.0 0.649 0.03474 -0.078 0.001 0.996 0.008 0.996 18.696 0.083 0.371 6.5 0.690 0.03723 -0.080 0.001 0.996 0.002 0.996 18.537 0.315 0.367 7.0 0.718 0.04154 -0.083 0.001 0.996 0.001 0.996 17.281 0.341 0.365 7.5 0.740 0.04634 -0.085 0.001 0.996 0.001 0.996 15.980 0.365 0.365 8.0 0.758 0.05169 -0.087 0.001 0.996 0.001 0.996 14.661 0.400 0.365 8.5 0.771 0.05913 -0.090 0.001 0.996 0.001 0.996 13.042 0.461 0.366 9.0 0.780 0.06642 -0.092 0.000 0.996 0.001 0.996 11.739 0.666 0.368 9.5 0.782 0.07266 -0.094 0.001 0.996 0.001 0.996 10.767 26.133 0.371 10.0 0.780 0.08498 -0.097 0.000 0.996 0.001 0.996 9.176 -0.202 0.374 10.5 0.772 0.08220 -0.099 0.001 0.996 0.001 0.996 9.393 0.021 0.378 11.0 0.760 0.09105 -0.101 0.001 0.996 0.002 0.996 8.342 0.090 0.383 11.5 0.743 0.09710 -0.104 0.001 0.996 0.002 0.996 7.653 0.124 0.389 12.0 0.723 0.10811 -0.106 0.001 0.996 0.002 0.996 6.685 0.145 0.396 12.5 0.699 0.11812 -0.108 0.001 0.996 0.002 0.996 5.916 0.157 0.405 13.0 0.673 0.12985 -0.110 0.001 0.996 0.002 0.996 5.183 0.164 0.414 13.5 0.645 0.13973 -0.113 0.001 0.996 0.002 0.996 4.614 0.170 0.425 14.0 0.615 0.15408 -0.115 0.001 0.996 0.002 0.996 3.993 0.172 0.437 14.5 0.585 0.17578 -0.117 0.001 0.996 0.002 0.996 3.329 0.173 0.451 15.0 0.555 0.19064 -0.120 0.001 0.996 0.002 0.996 2.911 0.173 0.466