Name = AG11 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 -0.199 0.44267 0.029 1.000 0.003 1.000 0.005 -0.449 0.024 0.398 -14.5 -0.208 0.40329 0.027 1.000 0.003 1.000 0.005 -0.515 0.023 0.382 -14.0 -0.216 0.36409 0.025 1.000 0.003 1.000 0.005 -0.594 0.021 0.368 -13.5 -0.225 0.33091 0.023 1.000 0.003 1.000 0.005 -0.680 0.014 0.354 -13.0 -0.233 0.30102 0.021 1.000 0.003 1.000 0.004 -0.775 0.002 0.342 -12.5 -0.241 0.27409 0.019 1.000 0.003 1.000 0.004 -0.880 -0.017 0.330 -12.0 -0.249 0.26680 0.017 1.000 0.003 1.000 0.004 -0.932 -0.050 0.320 -11.5 -0.255 0.23304 0.015 1.000 0.002 1.000 0.004 -1.094 -0.108 0.310 -11.0 -0.260 0.22561 0.013 1.000 0.002 1.000 0.004 -1.153 -0.223 0.301 -10.5 -0.264 0.20433 0.011 1.000 0.002 1.000 0.004 -1.291 -0.524 0.292 -10.0 -0.266 0.18283 0.009 1.000 0.002 1.000 0.004 -1.452 -2.958 0.284 -9.5 -0.265 0.16754 0.007 1.000 0.002 1.000 0.004 -1.582 1.454 0.276 -9.0 -0.262 0.15124 0.005 1.000 0.002 1.000 0.004 -1.732 0.732 0.268 -8.5 -0.256 0.21471 0.003 1.000 0.002 1.000 0.003 -1.193 0.537 0.260 -8.0 -0.247 0.18946 0.000 1.000 0.002 1.000 0.004 -1.304 0.450 0.252 -7.5 -0.235 0.16433 -0.002 1.000 0.002 1.000 0.003 -1.428 0.405 0.243 -7.0 -0.219 0.14455 -0.004 1.000 0.002 1.000 0.003 -1.514 0.376 0.232 -6.5 -0.200 0.12549 -0.006 1.000 0.002 1.000 0.003 -1.592 0.356 0.220 -6.0 -0.177 0.11109 -0.008 1.000 0.002 1.000 0.003 -1.594 0.341 0.203 -5.5 -0.151 0.09266 -0.011 1.000 0.002 1.000 0.003 -1.632 0.331 0.180 -5.0 -0.122 0.08003 -0.013 1.000 0.002 1.000 0.003 -1.529 0.324 0.146 -4.5 -0.091 0.07010 -0.015 1.000 0.002 1.000 0.003 -1.298 0.320 0.085 -4.0 -0.058 0.05681 -0.017 1.000 0.002 1.000 0.003 -1.018 0.316 -0.048 -3.5 -0.023 0.04946 -0.020 1.000 0.002 1.000 0.003 -0.463 0.182 -0.603 -3.0 -0.125 0.04330 -0.022 0.932 0.003 1.000 0.003 -2.881 0.143 0.075 -2.5 -0.066 0.03889 -0.024 0.893 0.002 1.000 0.003 -1.691 0.289 -0.116 -2.0 -0.007 0.03374 -0.026 0.861 0.002 1.000 0.003 -0.196 0.289 -3.735 -1.5 0.052 0.02967 -0.029 0.825 0.002 1.000 0.003 1.763 0.290 0.799 -1.0 0.111 0.02645 -0.031 0.773 0.003 1.000 0.003 4.185 0.290 0.531 -0.5 0.168 0.02510 -0.033 0.700 0.003 1.000 0.003 6.707 0.291 0.448 0.0 0.225 0.02220 -0.036 0.639 0.003 1.000 0.005 10.135 0.272 0.409 0.5 0.283 0.04159 -0.036 0.581 0.006 1.000 0.998 6.806 0.253 0.377 1.0 0.341 0.03235 -0.036 0.533 0.996 1.000 0.996 10.535 0.253 0.356 1.5 0.398 0.03288 -0.036 0.472 0.996 1.000 0.996 12.120 0.254 0.341 2.0 0.456 0.03380 -0.037 0.394 0.996 1.000 0.996 13.493 0.254 0.330 2.5 0.514 0.03497 -0.037 0.303 0.996 1.000 0.996 14.685 0.254 0.322 3.0 0.571 0.03539 -0.037 0.232 0.996 1.000 0.996 16.127 0.254 0.315 3.5 0.628 0.03566 -0.037 0.172 0.996 1.000 0.996 17.608 0.254 0.309 4.0 0.685 0.03578 -0.037 0.124 0.996 1.000 0.996 19.139 0.255 0.305 4.5 0.741 0.03439 -0.038 0.089 0.996 1.000 0.996 21.557 0.255 0.301 5.0 0.797 0.03372 -0.038 0.049 0.996 1.000 0.996 23.650 0.103 0.298 5.5 0.556 0.04775 -0.065 0.037 0.996 0.181 0.996 11.638 0.108 0.367 6.0 0.599 0.05136 -0.066 0.031 0.996 0.059 0.996 11.667 0.289 0.360 6.5 0.641 0.05424 -0.068 0.027 0.996 0.044 0.996 11.817 0.307 0.357 7.0 0.680 0.05782 -0.071 0.023 0.997 0.036 0.997 11.754 0.313 0.354 7.5 0.716 0.06182 -0.073 0.018 0.997 0.029 0.997 11.590 0.318 0.352 8.0 0.750 0.06634 -0.075 0.015 0.997 0.025 0.997 11.301 0.372 0.351 8.5 0.765 0.06621 -0.079 0.000 0.996 0.055 0.996 11.549 0.349 0.353 9.0 0.802 0.07196 -0.081 0.000 0.997 0.026 0.997 11.140 0.301 0.351 9.5 0.837 0.07765 -0.083 0.000 0.996 0.011 0.996 10.776 0.311 0.349 10.0 0.871 0.08412 -0.085 0.000 0.996 0.003 0.996 10.349 0.345 0.347 10.5 0.886 0.09295 -0.087 0.000 0.996 0.002 0.996 9.533 0.417 0.349 11.0 0.900 0.10414 -0.090 0.000 0.996 0.001 0.996 8.647 0.522 0.350 11.5 0.905 0.11644 -0.092 0.000 0.996 0.001 0.996 7.768 -2.956 0.352 12.0 0.899 0.13108 -0.095 0.000 0.996 0.001 0.996 6.858 -0.089 0.356 12.5 0.890 0.14812 -0.097 0.000 0.996 0.001 0.996 6.006 0.053 0.359 13.0 0.873 0.16364 -0.100 0.000 0.996 0.001 0.996 5.336 0.114 0.364 13.5 0.852 0.18845 -0.102 0.000 0.997 0.000 0.997 4.522 0.142 0.370 14.0 0.826 0.20443 -0.105 0.000 0.997 0.000 0.997 4.040 0.158 0.377 14.5 0.796 0.23532 -0.108 0.000 0.997 0.000 0.997 3.384 0.167 0.385 15.0 0.764 0.29532 -0.110 0.000 0.997 0.000 0.997 2.588 0.170 0.394 Name = AG11 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 -0.199 0.31726 0.029 1.000 0.003 1.000 0.005 -0.627 0.023 0.398 -14.5 -0.208 0.29406 0.027 1.000 0.003 1.000 0.005 -0.706 0.023 0.382 -14.0 -0.216 0.26999 0.025 1.000 0.003 1.000 0.005 -0.801 0.021 0.368 -13.5 -0.225 0.25895 0.023 1.000 0.003 1.000 0.005 -0.869 0.015 0.354 -13.0 -0.233 0.23934 0.021 1.000 0.003 1.000 0.005 -0.975 0.001 0.342 -12.5 -0.241 0.20843 0.019 1.000 0.003 1.000 0.004 -1.158 -0.018 0.330 -12.0 -0.249 0.19950 0.017 1.000 0.003 1.000 0.005 -1.246 -0.050 0.320 -11.5 -0.255 0.17717 0.015 1.000 0.002 1.000 0.004 -1.439 -0.109 0.310 -11.0 -0.260 0.16222 0.013 1.000 0.002 1.000 0.004 -1.603 -0.223 0.301 -10.5 -0.264 0.15533 0.011 1.000 0.002 1.000 0.004 -1.698 -0.527 0.292 -10.0 -0.265 0.14127 0.009 1.000 0.002 1.000 0.004 -1.879 -2.892 0.284 -9.5 -0.265 0.12378 0.007 1.000 0.002 1.000 0.004 -2.141 1.469 0.276 -9.0 -0.262 0.11158 0.005 1.000 0.002 1.000 0.004 -2.348 0.728 0.268 -8.5 -0.256 0.10491 0.003 1.000 0.002 1.000 0.004 -2.441 0.537 0.260 -8.0 -0.247 0.13543 0.000 1.000 0.002 1.000 0.004 -1.824 0.450 0.252 -7.5 -0.235 0.08618 -0.002 1.000 0.002 1.000 0.004 -2.722 0.405 0.243 -7.0 -0.219 0.10676 -0.004 1.000 0.002 1.000 0.003 -2.050 0.376 0.232 -6.5 -0.200 0.09976 -0.006 1.000 0.002 1.000 0.003 -2.001 0.356 0.220 -6.0 -0.177 0.08371 -0.008 1.000 0.002 1.000 0.003 -2.115 0.341 0.203 -5.5 -0.151 0.07522 -0.011 1.000 0.002 1.000 0.003 -2.008 0.331 0.180 -5.0 -0.122 0.06505 -0.013 1.000 0.002 1.000 0.003 -1.878 0.325 0.146 -4.5 -0.091 0.05422 -0.015 1.000 0.002 1.000 0.003 -1.679 0.320 0.085 -4.0 -0.058 0.04586 -0.017 1.000 0.002 1.000 0.003 -1.258 0.316 -0.049 -3.5 -0.023 0.03912 -0.020 1.000 0.002 1.000 0.003 -0.585 0.182 -0.603 -3.0 -0.125 0.03483 -0.022 0.932 0.003 1.000 0.003 -3.581 0.143 0.075 -2.5 -0.066 0.03158 -0.024 0.893 0.002 1.000 0.003 -2.083 0.289 -0.116 -2.0 -0.007 0.02781 -0.026 0.861 0.002 1.000 0.003 -0.238 0.289 -3.735 -1.5 0.052 0.02460 -0.029 0.825 0.002 1.000 0.003 2.126 0.290 0.799 -1.0 0.111 0.02213 -0.031 0.773 0.003 1.000 0.003 5.003 0.290 0.531 -0.5 0.168 0.02125 -0.033 0.700 0.003 1.000 0.003 7.921 0.291 0.448 0.0 0.225 0.01858 -0.036 0.639 0.003 1.000 0.005 12.109 0.272 0.409 0.5 0.283 0.04041 -0.036 0.581 0.006 1.000 0.998 7.004 0.253 0.377 1.0 0.341 0.02708 -0.036 0.533 0.996 1.000 0.996 12.584 0.253 0.356 1.5 0.398 0.02779 -0.036 0.472 0.996 1.000 0.996 14.342 0.254 0.341 2.0 0.456 0.02893 -0.037 0.394 0.996 1.000 0.996 15.766 0.254 0.330 2.5 0.514 0.02998 -0.037 0.303 0.996 1.000 0.996 17.126 0.254 0.322 3.0 0.571 0.03074 -0.037 0.232 0.996 1.000 0.996 18.571 0.254 0.315 3.5 0.628 0.03115 -0.037 0.172 0.996 1.000 0.996 20.159 0.254 0.309 4.0 0.685 0.03142 -0.037 0.124 0.996 1.000 0.996 21.794 0.255 0.305 4.5 0.741 0.03171 -0.038 0.089 0.996 1.000 0.996 23.380 0.255 0.301 5.0 0.797 0.03186 -0.038 0.049 0.996 1.000 0.996 25.030 0.255 0.298 5.5 0.853 0.03129 -0.038 0.037 0.996 1.000 0.996 27.261 0.255 0.295 6.0 0.908 0.02887 -0.039 0.031 0.996 1.000 0.996 31.451 0.111 0.292 6.5 0.629 0.04770 -0.069 0.027 0.996 0.095 0.996 13.183 0.111 0.360 7.0 0.674 0.05036 -0.071 0.023 0.997 0.047 0.997 13.390 0.297 0.355 7.5 0.712 0.05364 -0.073 0.018 0.997 0.037 0.997 13.279 0.315 0.353 8.0 0.746 0.05720 -0.076 0.015 0.997 0.030 0.997 13.047 0.396 0.351 8.5 0.766 0.05749 -0.081 0.000 0.996 0.156 0.996 13.328 0.384 0.356 9.0 0.791 0.06414 -0.082 0.000 0.997 0.055 0.997 12.325 0.287 0.353 9.5 0.823 0.06902 -0.083 0.000 0.996 0.027 0.996 11.922 0.304 0.351 10.0 0.857 0.07378 -0.085 0.000 0.996 0.010 0.996 11.611 0.323 0.349 10.5 0.880 0.07887 -0.087 0.000 0.996 0.005 0.996 11.155 0.361 0.349 11.0 0.899 0.08651 -0.090 0.000 0.996 0.001 0.996 10.394 0.460 0.350 11.5 0.903 0.09562 -0.092 0.000 0.996 0.001 0.996 9.446 -4.434 0.352 12.0 0.898 0.10594 -0.095 0.000 0.996 0.001 0.996 8.477 -0.100 0.356 12.5 0.889 0.11903 -0.097 0.000 0.996 0.001 0.996 7.467 0.053 0.360 13.0 0.872 0.13133 -0.100 0.000 0.996 0.001 0.996 6.643 0.113 0.365 13.5 0.852 0.14793 -0.102 0.000 0.997 0.000 0.997 5.757 0.141 0.370 14.0 0.826 0.16010 -0.105 0.000 0.997 0.000 0.997 5.157 0.158 0.377 14.5 0.796 0.17973 -0.108 0.000 0.997 0.000 0.997 4.429 0.167 0.385 15.0 0.764 0.22721 -0.110 0.000 0.997 0.000 0.997 3.363 0.170 0.394 Name = AG11 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 -0.199 0.17880 0.029 1.000 0.003 1.000 0.006 -1.112 0.023 0.398 -14.5 -0.208 0.25986 0.027 1.000 0.003 1.000 0.006 -0.799 0.022 0.382 -14.0 -0.216 0.22890 0.025 1.000 0.003 1.000 0.005 -0.945 0.020 0.368 -13.5 -0.225 0.21683 0.023 1.000 0.003 1.000 0.005 -1.037 0.015 0.354 -13.0 -0.233 0.20281 0.021 1.000 0.003 1.000 0.005 -1.150 0.001 0.342 -12.5 -0.241 0.17992 0.019 1.000 0.003 1.000 0.005 -1.341 -0.018 0.330 -12.0 -0.249 0.17051 0.017 1.000 0.003 1.000 0.005 -1.457 -0.050 0.320 -11.5 -0.255 0.16146 0.015 1.000 0.002 1.000 0.005 -1.579 -0.109 0.310 -11.0 -0.260 0.14154 0.013 1.000 0.002 1.000 0.004 -1.838 -0.224 0.301 -10.5 -0.264 0.13440 0.011 1.000 0.002 1.000 0.004 -1.962 -0.529 0.292 -10.0 -0.265 0.12359 0.009 1.000 0.002 1.000 0.004 -2.148 -2.917 0.284 -9.5 -0.265 0.11003 0.007 1.000 0.002 1.000 0.004 -2.408 1.465 0.276 -9.0 -0.262 0.09899 0.005 1.000 0.002 1.000 0.004 -2.646 0.728 0.268 -8.5 -0.256 0.09346 0.003 1.000 0.002 1.000 0.004 -2.740 0.537 0.260 -8.0 -0.247 0.08064 0.000 1.000 0.002 1.000 0.004 -3.062 0.451 0.252 -7.5 -0.235 0.07374 -0.002 1.000 0.002 1.000 0.004 -3.180 0.404 0.243 -7.0 -0.219 0.09493 -0.004 1.000 0.002 1.000 0.003 -2.304 0.376 0.232 -6.5 -0.200 0.08422 -0.006 1.000 0.002 1.000 0.003 -2.370 0.356 0.220 -6.0 -0.177 0.07542 -0.008 1.000 0.002 1.000 0.003 -2.346 0.341 0.203 -5.5 -0.151 0.06458 -0.011 1.000 0.002 1.000 0.003 -2.339 0.331 0.180 -5.0 -0.122 0.05594 -0.013 1.000 0.002 1.000 0.003 -2.184 0.325 0.146 -4.5 -0.091 0.04725 -0.015 1.000 0.002 1.000 0.003 -1.926 0.320 0.085 -4.0 -0.058 0.04028 -0.017 1.000 0.002 1.000 0.003 -1.433 0.316 -0.049 -3.5 -0.023 0.03524 -0.020 1.000 0.002 1.000 0.003 -0.646 0.182 -0.607 -3.0 -0.125 0.03153 -0.022 0.932 0.003 1.000 0.003 -3.956 0.143 0.075 -2.5 -0.066 0.02820 -0.024 0.893 0.002 1.000 0.003 -2.332 0.289 -0.116 -2.0 -0.007 0.02510 -0.026 0.861 0.002 1.000 0.003 -0.264 0.289 -3.735 -1.5 0.052 0.02225 -0.029 0.825 0.002 1.000 0.003 2.351 0.290 0.799 -1.0 0.111 0.02027 -0.031 0.773 0.003 1.000 0.003 5.461 0.290 0.531 -0.5 0.168 0.01949 -0.033 0.700 0.003 1.000 0.003 8.633 0.291 0.448 0.0 0.225 0.01745 -0.036 0.639 0.003 1.000 0.005 12.892 0.272 0.409 0.5 0.283 0.03941 -0.036 0.581 0.006 1.000 0.998 7.181 0.253 0.377 1.0 0.341 0.02425 -0.036 0.533 0.996 1.000 0.996 14.052 0.253 0.356 1.5 0.398 0.02506 -0.036 0.472 0.996 1.000 0.996 15.901 0.254 0.341 2.0 0.456 0.02633 -0.037 0.394 0.996 1.000 0.996 17.324 0.254 0.330 2.5 0.514 0.02767 -0.037 0.303 0.996 1.000 0.996 18.559 0.254 0.322 3.0 0.571 0.02860 -0.037 0.232 0.996 1.000 0.996 19.957 0.254 0.315 3.5 0.628 0.02909 -0.037 0.172 0.996 1.000 0.996 21.583 0.254 0.309 4.0 0.685 0.02946 -0.037 0.124 0.996 1.000 0.996 23.245 0.255 0.305 4.5 0.741 0.02993 -0.038 0.089 0.996 1.000 0.996 24.765 0.255 0.301 5.0 0.797 0.02953 -0.038 0.049 0.996 1.000 0.996 26.999 0.255 0.298 5.5 0.853 0.02953 -0.038 0.037 0.996 1.000 0.996 28.885 0.255 0.295 6.0 0.908 0.02919 -0.039 0.031 0.996 1.000 0.996 31.109 0.255 0.292 6.5 0.962 0.02728 -0.039 0.027 0.996 1.000 0.996 35.275 0.102 0.290 7.0 0.673 0.04528 -0.073 0.023 0.997 0.195 0.997 14.866 0.114 0.359 7.5 0.706 0.05035 -0.074 0.018 0.997 0.053 0.997 14.024 0.287 0.354 8.0 0.742 0.05348 -0.076 0.015 0.997 0.038 0.997 13.875 0.299 0.352 8.5 0.842 0.04433 -0.080 0.000 0.996 0.389 0.996 18.986 0.404 0.345 9.0 0.787 0.06001 -0.083 0.000 0.997 0.101 0.997 13.116 0.115 0.355 9.5 0.816 0.06514 -0.084 0.000 0.996 0.045 0.996 12.522 0.296 0.353 10.0 0.846 0.06977 -0.086 0.000 0.996 0.020 0.996 12.128 0.322 0.351 10.5 0.869 0.07466 -0.088 0.000 0.996 0.011 0.996 11.641 0.337 0.351 11.0 0.896 0.07921 -0.090 0.000 0.996 0.002 0.996 11.310 0.389 0.350 11.5 0.902 0.08591 -0.092 0.000 0.996 0.001 0.996 10.504 3.969 0.352 12.0 0.897 0.09509 -0.095 0.000 0.996 0.001 0.996 9.435 -0.102 0.356 12.5 0.888 0.10602 -0.097 0.000 0.996 0.001 0.996 8.376 0.052 0.360 13.0 0.872 0.11711 -0.100 0.000 0.996 0.001 0.996 7.443 0.111 0.365 13.5 0.851 0.13007 -0.102 0.000 0.997 0.001 0.997 6.545 0.140 0.370 14.0 0.825 0.14065 -0.105 0.000 0.997 0.001 0.997 5.868 0.158 0.377 14.5 0.796 0.15553 -0.108 0.000 0.997 0.001 0.997 5.116 0.167 0.385 15.0 0.764 0.17412 -0.110 0.000 0.997 0.000 0.997 4.387 0.170 0.394 Name = AG11 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 -0.199 0.16061 0.029 1.000 0.003 1.000 0.006 -1.238 0.023 0.398 -14.5 -0.208 0.15208 0.027 1.000 0.003 1.000 0.006 -1.365 0.022 0.382 -14.0 -0.216 0.21418 0.025 1.000 0.003 1.000 0.006 -1.010 0.020 0.368 -13.5 -0.225 0.19188 0.023 1.000 0.003 1.000 0.006 -1.172 0.014 0.354 -13.0 -0.233 0.18113 0.021 1.000 0.003 1.000 0.005 -1.288 0.001 0.342 -12.5 -0.241 0.16298 0.019 1.000 0.003 1.000 0.005 -1.480 -0.018 0.330 -12.0 -0.248 0.15338 0.017 1.000 0.003 1.000 0.005 -1.620 -0.051 0.320 -11.5 -0.255 0.14569 0.015 1.000 0.002 1.000 0.005 -1.749 -0.110 0.310 -11.0 -0.260 0.12940 0.013 1.000 0.002 1.000 0.004 -2.010 -0.224 0.301 -10.5 -0.264 0.12217 0.011 1.000 0.002 1.000 0.005 -2.158 -0.527 0.292 -10.0 -0.265 0.10796 0.009 1.000 0.002 1.000 0.004 -2.459 -2.942 0.284 -9.5 -0.265 0.10224 0.007 1.000 0.002 1.000 0.004 -2.592 1.446 0.276 -9.0 -0.262 0.09180 0.005 1.000 0.002 1.000 0.004 -2.853 0.731 0.268 -8.5 -0.256 0.08294 0.003 1.000 0.002 1.000 0.004 -3.087 0.537 0.260 -8.0 -0.247 0.07550 0.000 1.000 0.002 1.000 0.004 -3.270 0.450 0.252 -7.5 -0.234 0.06918 -0.002 1.000 0.002 1.000 0.004 -3.389 0.405 0.243 -7.0 -0.219 0.08405 -0.004 1.000 0.002 1.000 0.003 -2.602 0.376 0.232 -6.5 -0.199 0.07886 -0.006 1.000 0.002 1.000 0.003 -2.529 0.356 0.220 -6.0 -0.177 0.06743 -0.008 1.000 0.002 1.000 0.003 -2.624 0.342 0.203 -5.5 -0.151 0.05830 -0.011 1.000 0.002 1.000 0.003 -2.591 0.331 0.180 -5.0 -0.122 0.05059 -0.013 1.000 0.002 1.000 0.003 -2.415 0.324 0.146 -4.5 -0.091 0.04500 -0.015 1.000 0.002 1.000 0.003 -2.018 0.320 0.085 -4.0 -0.058 0.03770 -0.017 1.000 0.002 1.000 0.003 -1.528 0.317 -0.049 -3.5 -0.023 0.03239 -0.020 1.000 0.002 1.000 0.003 -0.703 0.182 -0.607 -3.0 -0.125 0.02932 -0.022 0.932 0.003 1.000 0.003 -4.254 0.143 0.075 -2.5 -0.066 0.02659 -0.024 0.893 0.002 1.000 0.003 -2.473 0.289 -0.116 -2.0 -0.007 0.02361 -0.026 0.861 0.002 1.000 0.003 -0.281 0.289 -3.735 -1.5 0.052 0.02107 -0.029 0.825 0.002 1.000 0.003 2.482 0.290 0.799 -1.0 0.111 0.01909 -0.031 0.773 0.003 1.000 0.003 5.800 0.290 0.531 -0.5 0.168 0.01834 -0.033 0.700 0.003 1.000 0.003 9.176 0.291 0.448 0.0 0.225 0.01639 -0.036 0.639 0.003 1.000 0.005 13.722 0.272 0.409 0.5 0.283 0.03929 -0.036 0.581 0.006 1.000 0.999 7.204 0.253 0.377 1.0 0.341 0.02254 -0.036 0.533 0.996 1.000 0.996 15.122 0.253 0.356 1.5 0.398 0.02342 -0.036 0.472 0.996 1.000 0.996 17.017 0.254 0.341 2.0 0.456 0.02477 -0.037 0.394 0.996 1.000 0.996 18.414 0.254 0.330 2.5 0.514 0.02564 -0.037 0.303 0.996 1.000 0.996 20.026 0.254 0.322 3.0 0.571 0.02662 -0.037 0.232 0.996 1.000 0.996 21.441 0.254 0.315 3.5 0.628 0.02718 -0.037 0.172 0.996 1.000 0.996 23.098 0.254 0.309 4.0 0.685 0.02828 -0.037 0.124 0.996 1.000 0.996 24.211 0.255 0.305 4.5 0.741 0.02815 -0.038 0.089 0.996 1.000 0.996 26.337 0.255 0.301 5.0 0.797 0.02858 -0.038 0.049 0.996 1.000 0.996 27.897 0.255 0.298 5.5 0.853 0.02851 -0.038 0.037 0.996 1.000 0.996 29.919 0.255 0.295 6.0 0.908 0.02809 -0.039 0.031 0.996 1.000 0.996 32.323 0.255 0.292 6.5 0.962 0.02713 -0.039 0.027 0.996 1.000 0.996 35.471 0.256 0.290 7.0 1.016 0.02548 -0.039 0.023 0.997 1.000 0.997 39.867 0.095 0.289 7.5 0.721 0.04421 -0.076 0.018 0.997 0.242 0.997 16.311 0.117 0.356 8.0 0.736 0.05154 -0.076 0.015 0.997 0.057 0.997 14.274 0.227 0.354 8.5 0.957 0.03294 -0.071 0.000 0.996 0.633 0.996 29.066 0.374 0.324 9.0 0.798 0.05543 -0.084 0.000 0.997 0.173 0.997 14.389 0.156 0.355 9.5 0.811 0.06263 -0.085 0.000 0.996 0.067 0.996 12.957 0.295 0.354 10.0 0.839 0.06737 -0.086 0.000 0.996 0.032 0.996 12.461 0.319 0.352 10.5 0.862 0.07175 -0.088 0.000 0.996 0.019 0.996 12.014 0.326 0.352 11.0 0.891 0.07556 -0.090 0.000 0.996 0.004 0.996 11.796 0.364 0.351 11.5 0.900 0.08176 -0.092 0.000 0.996 0.002 0.996 11.010 1.677 0.353 12.0 0.895 0.08938 -0.095 0.000 0.996 0.002 0.996 10.012 -0.151 0.356 12.5 0.888 0.09674 -0.097 0.000 0.996 0.001 0.996 9.175 0.039 0.360 13.0 0.871 0.10895 -0.100 0.000 0.996 0.001 0.996 7.994 0.111 0.365 13.5 0.851 0.11931 -0.102 0.000 0.997 0.001 0.997 7.133 0.139 0.370 14.0 0.825 0.12899 -0.105 0.000 0.997 0.001 0.997 6.396 0.158 0.377 14.5 0.795 0.14111 -0.108 0.000 0.997 0.001 0.997 5.637 0.167 0.385 15.0 0.764 0.15820 -0.110 0.000 0.997 0.000 0.997 4.827 0.170 0.394