Name = AG19 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 -0.215 0.33706 0.007 1.000 0.003 1.000 0.004 -0.638 0.033 0.284 -14.5 -0.224 0.32815 0.005 1.000 0.003 1.000 0.004 -0.683 0.030 0.274 -14.0 -0.233 0.29963 0.003 1.000 0.003 1.000 0.004 -0.779 0.023 0.264 -13.5 -0.242 0.29097 0.001 1.000 0.003 1.000 0.004 -0.832 0.010 0.255 -13.0 -0.250 0.24895 -0.001 1.000 0.002 1.000 0.004 -1.005 -0.012 0.247 -12.5 -0.258 0.22040 -0.003 1.000 0.002 1.000 0.004 -1.168 -0.051 0.239 -12.0 -0.264 0.21418 -0.005 1.000 0.002 1.000 0.004 -1.231 -0.120 0.232 -11.5 -0.269 0.29482 -0.007 1.000 0.002 1.000 0.004 -0.911 -0.273 0.224 -11.0 -0.272 0.25578 -0.009 1.000 0.002 1.000 0.004 -1.062 -0.809 0.217 -10.5 -0.273 0.24302 -0.011 1.000 0.002 1.000 0.004 -1.121 9.299 0.210 -10.0 -0.271 0.22579 -0.013 1.000 0.002 1.000 0.003 -1.201 0.974 0.202 -9.5 -0.267 0.19658 -0.015 1.000 0.002 1.000 0.003 -1.357 0.605 0.193 -9.0 -0.259 0.16975 -0.017 1.000 0.002 1.000 0.003 -1.528 0.477 0.183 -8.5 -0.248 0.14276 -0.019 1.000 0.002 1.000 0.003 -1.739 0.417 0.172 -8.0 -0.234 0.12175 -0.022 1.000 0.002 1.000 0.003 -1.922 0.382 0.158 -7.5 -0.216 0.11404 -0.024 1.000 0.002 1.000 0.003 -1.895 0.359 0.140 -7.0 -0.195 0.09936 -0.026 1.000 0.002 1.000 0.002 -1.962 0.345 0.118 -6.5 -0.171 0.08837 -0.028 1.000 0.001 1.000 0.002 -1.933 0.333 0.086 -6.0 -0.143 0.07885 -0.030 1.000 0.001 1.000 0.002 -1.818 0.325 0.040 -5.5 -0.113 0.06468 -0.032 1.000 0.001 1.000 0.002 -1.753 0.320 -0.035 -5.0 -0.081 0.05737 -0.034 1.000 0.001 1.000 0.002 -1.416 0.315 -0.174 -4.5 -0.047 0.04862 -0.037 1.000 0.002 1.000 0.002 -0.967 0.312 -0.529 -4.0 -0.012 0.04191 -0.039 1.000 0.002 1.000 0.003 -0.276 0.199 -3.104 -3.5 -0.133 0.03612 -0.041 1.000 0.002 1.000 0.003 -3.677 0.179 -0.058 -3.0 -0.073 0.03180 -0.043 1.000 0.002 1.000 0.003 -2.294 0.287 -0.342 -2.5 -0.013 0.02806 -0.045 0.966 0.003 1.000 0.003 -0.470 0.287 -3.190 -2.0 0.046 0.02564 -0.048 0.913 0.003 1.000 0.005 1.797 0.287 1.282 -1.5 0.105 0.02458 -0.050 0.855 0.006 1.000 0.012 4.256 0.327 0.725 -1.0 0.160 0.02726 -0.056 0.810 0.995 1.000 0.995 5.852 0.309 0.603 -0.5 0.217 0.02772 -0.056 0.736 0.995 1.000 0.995 7.830 0.251 0.510 0.0 0.274 0.02869 -0.056 0.681 0.995 1.000 0.995 9.565 0.251 0.456 0.5 0.332 0.02859 -0.057 0.657 0.995 1.000 0.995 11.607 0.251 0.420 1.0 0.389 0.02907 -0.057 0.618 0.995 1.000 0.995 13.388 0.251 0.395 1.5 0.446 0.02975 -0.057 0.570 0.995 1.000 0.995 15.004 0.251 0.377 2.0 0.504 0.03027 -0.057 0.507 0.995 1.000 0.995 16.634 0.251 0.363 2.5 0.561 0.03336 -0.057 0.344 0.995 1.000 0.995 16.807 0.251 0.351 3.0 0.618 0.03456 -0.057 0.225 0.995 1.000 0.995 17.869 0.252 0.342 3.5 0.674 0.03486 -0.057 0.168 0.995 1.000 0.996 19.337 0.252 0.335 4.0 0.730 0.03526 -0.057 0.113 0.995 1.000 0.996 20.717 0.252 0.328 4.5 0.786 0.03469 -0.057 0.068 0.995 1.000 0.995 22.660 0.252 0.323 5.0 0.840 0.03132 -0.057 0.040 0.995 1.000 0.995 26.812 0.104 0.318 5.5 0.612 0.04696 -0.083 0.023 0.995 0.058 0.995 13.043 0.081 0.385 6.0 0.683 0.04466 -0.084 0.002 0.995 0.005 0.995 15.302 0.282 0.373 6.5 0.719 0.04891 -0.086 0.001 0.995 0.002 0.995 14.691 0.322 0.370 7.0 0.746 0.05640 -0.088 0.001 0.996 0.001 0.996 13.221 0.342 0.368 7.5 0.768 0.06355 -0.091 0.001 0.996 0.001 0.996 12.089 0.367 0.368 8.0 0.785 0.07282 -0.093 0.000 0.996 0.001 0.996 10.778 0.416 0.368 8.5 0.796 0.08300 -0.095 0.000 0.996 0.001 0.996 9.591 0.518 0.370 9.0 0.802 0.09615 -0.098 0.000 0.996 0.001 0.996 8.342 0.983 0.372 9.5 0.802 0.11390 -0.100 0.000 0.996 0.001 0.996 7.044 -0.668 0.374 10.0 0.797 0.12365 -0.102 0.000 0.996 0.001 0.996 6.446 -0.056 0.378 10.5 0.787 0.14659 -0.105 0.000 0.995 0.001 0.995 5.370 0.070 0.383 11.0 0.771 0.16797 -0.107 0.000 0.995 0.001 0.995 4.592 0.120 0.389 11.5 0.751 0.19292 -0.109 0.000 0.995 0.001 0.995 3.895 0.144 0.395 12.0 0.727 0.17257 -0.111 0.001 0.995 0.001 0.995 4.213 0.158 0.403 12.5 0.700 0.19900 -0.114 0.001 0.995 0.001 0.995 3.520 0.167 0.412 13.0 0.671 0.22059 -0.116 0.001 0.995 0.002 0.995 3.040 0.173 0.423 13.5 0.640 0.22981 -0.119 0.001 0.995 0.002 0.995 2.784 0.176 0.435 14.0 0.608 0.26232 -0.121 0.001 0.996 0.002 0.996 2.318 0.177 0.449 14.5 0.576 0.30107 -0.123 0.001 0.996 0.002 0.996 1.913 0.177 0.464 15.0 0.544 0.33734 -0.126 0.001 0.996 0.002 0.996 1.612 0.177 0.481 Name = AG19 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 -0.215 0.25447 0.007 1.000 0.003 1.000 0.005 -0.845 0.033 0.284 -14.5 -0.224 0.24913 0.005 1.000 0.003 1.000 0.005 -0.900 0.030 0.274 -14.0 -0.233 0.22971 0.003 1.000 0.003 1.000 0.004 -1.016 0.023 0.264 -13.5 -0.242 0.20740 0.001 1.000 0.003 1.000 0.004 -1.167 0.010 0.255 -13.0 -0.250 0.19138 -0.001 1.000 0.002 1.000 0.004 -1.307 -0.013 0.247 -12.5 -0.257 0.17250 -0.003 1.000 0.002 1.000 0.004 -1.493 -0.051 0.239 -12.0 -0.264 0.15605 -0.005 1.000 0.002 1.000 0.004 -1.690 -0.121 0.232 -11.5 -0.269 0.15042 -0.007 1.000 0.002 1.000 0.004 -1.785 -0.277 0.224 -11.0 -0.272 0.13312 -0.009 1.000 0.002 1.000 0.004 -2.040 -0.792 0.217 -10.5 -0.273 0.17275 -0.011 1.000 0.002 1.000 0.004 -1.577 11.401 0.210 -10.0 -0.271 0.16370 -0.013 1.000 0.002 1.000 0.003 -1.657 0.949 0.202 -9.5 -0.267 0.15373 -0.015 1.000 0.002 1.000 0.003 -1.734 0.598 0.193 -9.0 -0.259 0.13520 -0.017 1.000 0.002 1.000 0.003 -1.917 0.476 0.183 -8.5 -0.248 0.11549 -0.019 1.000 0.002 1.000 0.003 -2.147 0.416 0.172 -8.0 -0.234 0.09991 -0.022 1.000 0.002 1.000 0.003 -2.340 0.384 0.158 -7.5 -0.216 0.08614 -0.024 1.000 0.002 1.000 0.003 -2.508 0.360 0.140 -7.0 -0.195 0.07904 -0.026 1.000 0.002 1.000 0.003 -2.465 0.344 0.118 -6.5 -0.171 0.06938 -0.028 1.000 0.001 1.000 0.002 -2.460 0.333 0.086 -6.0 -0.143 0.06198 -0.030 1.000 0.001 1.000 0.002 -2.311 0.325 0.040 -5.5 -0.113 0.05275 -0.032 1.000 0.001 1.000 0.002 -2.146 0.319 -0.035 -5.0 -0.081 0.04702 -0.034 1.000 0.001 1.000 0.002 -1.724 0.315 -0.175 -4.5 -0.047 0.03921 -0.037 1.000 0.002 1.000 0.002 -1.199 0.313 -0.529 -4.0 -0.012 0.03403 -0.039 1.000 0.002 1.000 0.003 -0.340 0.199 -3.104 -3.5 -0.133 0.02980 -0.041 1.000 0.002 1.000 0.003 -4.457 0.179 -0.058 -3.0 -0.073 0.02597 -0.043 1.000 0.002 1.000 0.003 -2.809 0.287 -0.342 -2.5 -0.013 0.02326 -0.045 0.966 0.003 1.000 0.003 -0.567 0.287 -3.190 -2.0 0.046 0.02134 -0.048 0.913 0.003 1.000 0.005 2.160 0.345 1.282 -1.5 0.102 0.03252 -0.056 0.855 0.006 1.000 0.997 3.136 0.327 0.802 -1.0 0.160 0.02055 -0.056 0.810 0.995 1.000 0.995 7.762 0.251 0.603 -0.5 0.217 0.02160 -0.056 0.736 0.995 1.000 0.995 10.051 0.251 0.510 0.0 0.274 0.02278 -0.056 0.681 0.995 1.000 0.995 12.050 0.251 0.456 0.5 0.332 0.02277 -0.057 0.657 0.995 1.000 0.995 14.571 0.251 0.420 1.0 0.389 0.02340 -0.057 0.618 0.995 1.000 0.995 16.631 0.251 0.395 1.5 0.446 0.02440 -0.057 0.570 0.995 1.000 0.995 18.299 0.251 0.377 2.0 0.504 0.02540 -0.057 0.507 0.995 1.000 0.995 19.827 0.251 0.363 2.5 0.561 0.02786 -0.057 0.344 0.995 1.000 0.995 20.123 0.251 0.351 3.0 0.618 0.02960 -0.057 0.225 0.995 1.000 0.995 20.860 0.252 0.342 3.5 0.674 0.03060 -0.057 0.168 0.995 1.000 0.996 22.030 0.252 0.335 4.0 0.730 0.03124 -0.057 0.113 0.995 1.000 0.996 23.379 0.252 0.328 4.5 0.786 0.03135 -0.057 0.068 0.995 1.000 0.995 25.068 0.252 0.323 5.0 0.840 0.03156 -0.057 0.040 0.995 1.000 0.995 26.605 0.252 0.318 5.5 0.891 0.03056 -0.057 0.023 0.995 1.000 0.995 29.176 0.087 0.314 6.0 0.677 0.03927 -0.084 0.002 0.995 0.009 0.995 17.231 0.085 0.374 6.5 0.718 0.04184 -0.086 0.001 0.995 0.002 0.995 17.159 0.314 0.370 7.0 0.746 0.04697 -0.088 0.001 0.996 0.001 0.996 15.876 0.342 0.368 7.5 0.768 0.05411 -0.091 0.001 0.996 0.001 0.996 14.191 0.368 0.368 8.0 0.785 0.06136 -0.093 0.000 0.996 0.001 0.996 12.786 0.416 0.368 8.5 0.796 0.06915 -0.095 0.000 0.996 0.001 0.996 11.508 0.519 0.370 9.0 0.802 0.07881 -0.098 0.000 0.996 0.001 0.996 10.175 0.947 0.372 9.5 0.802 0.08841 -0.100 0.000 0.996 0.001 0.996 9.076 -0.646 0.374 10.0 0.797 0.10243 -0.102 0.000 0.996 0.001 0.996 7.778 -0.051 0.378 10.5 0.787 0.11620 -0.105 0.000 0.995 0.001 0.995 6.773 0.069 0.383 11.0 0.771 0.11863 -0.107 0.000 0.995 0.001 0.995 6.498 0.120 0.389 11.5 0.751 0.14915 -0.109 0.000 0.995 0.001 0.995 5.036 0.144 0.395 12.0 0.727 0.14029 -0.112 0.001 0.995 0.001 0.995 5.180 0.159 0.403 12.5 0.700 0.15937 -0.114 0.001 0.995 0.001 0.995 4.393 0.167 0.413 13.0 0.671 0.16088 -0.116 0.001 0.995 0.002 0.995 4.168 0.173 0.423 13.5 0.640 0.17965 -0.119 0.001 0.995 0.002 0.995 3.560 0.176 0.435 14.0 0.608 0.20698 -0.121 0.001 0.996 0.002 0.996 2.936 0.177 0.449 14.5 0.576 0.23211 -0.123 0.001 0.996 0.002 0.996 2.480 0.177 0.464 15.0 0.543 0.25463 -0.126 0.001 0.996 0.002 0.996 2.134 0.177 0.481 Name = AG19 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 -0.215 0.21862 0.007 1.000 0.003 1.000 0.005 -0.984 0.033 0.284 -14.5 -0.224 0.21528 0.005 1.000 0.003 1.000 0.005 -1.041 0.030 0.274 -14.0 -0.233 0.19973 0.003 1.000 0.003 1.000 0.005 -1.168 0.022 0.264 -13.5 -0.242 0.18253 0.001 1.000 0.003 1.000 0.004 -1.326 0.010 0.255 -13.0 -0.250 0.16695 -0.001 1.000 0.002 1.000 0.005 -1.498 -0.013 0.247 -12.5 -0.257 0.15235 -0.003 1.000 0.002 1.000 0.004 -1.690 -0.051 0.239 -12.0 -0.264 0.13935 -0.005 1.000 0.002 1.000 0.004 -1.892 -0.120 0.232 -11.5 -0.269 0.12613 -0.007 1.000 0.002 1.000 0.004 -2.129 -0.278 0.224 -11.0 -0.271 0.11901 -0.009 1.000 0.002 1.000 0.004 -2.281 -0.814 0.217 -10.5 -0.272 0.10768 -0.011 1.000 0.002 1.000 0.004 -2.530 9.278 0.210 -10.0 -0.271 0.14612 -0.013 1.000 0.002 1.000 0.003 -1.855 0.963 0.202 -9.5 -0.267 0.12611 -0.015 1.000 0.002 1.000 0.003 -2.113 0.604 0.193 -9.0 -0.259 0.11257 -0.017 1.000 0.002 1.000 0.003 -2.302 0.476 0.183 -8.5 -0.248 0.09664 -0.019 1.000 0.002 1.000 0.003 -2.566 0.416 0.172 -8.0 -0.234 0.08499 -0.022 1.000 0.002 1.000 0.003 -2.751 0.383 0.158 -7.5 -0.216 0.07650 -0.024 1.000 0.002 1.000 0.003 -2.823 0.360 0.140 -7.0 -0.195 0.06811 -0.026 1.000 0.002 1.000 0.003 -2.861 0.345 0.118 -6.5 -0.171 0.06024 -0.028 1.000 0.001 1.000 0.002 -2.834 0.333 0.086 -6.0 -0.143 0.05385 -0.030 1.000 0.001 1.000 0.002 -2.660 0.325 0.040 -5.5 -0.113 0.04584 -0.032 1.000 0.001 1.000 0.002 -2.469 0.319 -0.035 -5.0 -0.081 0.04151 -0.034 1.000 0.001 1.000 0.002 -1.953 0.315 -0.175 -4.5 -0.047 0.03585 -0.037 1.000 0.002 1.000 0.002 -1.307 0.312 -0.531 -4.0 -0.011 0.03122 -0.039 1.000 0.002 1.000 0.003 -0.364 0.199 -3.158 -3.5 -0.133 0.02680 -0.041 1.000 0.002 1.000 0.003 -4.956 0.179 -0.058 -3.0 -0.073 0.02339 -0.043 1.000 0.002 1.000 0.003 -3.119 0.287 -0.342 -2.5 -0.013 0.02102 -0.045 0.966 0.003 1.000 0.003 -0.627 0.287 -3.190 -2.0 0.046 0.01925 -0.048 0.913 0.003 1.000 0.005 2.394 0.345 1.282 -1.5 0.102 0.03109 -0.056 0.855 0.006 1.000 0.997 3.280 0.327 0.802 -1.0 0.160 0.01756 -0.056 0.810 0.995 1.000 0.995 9.085 0.251 0.603 -0.5 0.217 0.01893 -0.056 0.736 0.995 1.000 0.995 11.467 0.251 0.510 0.0 0.274 0.02005 -0.056 0.681 0.995 1.000 0.995 13.687 0.251 0.456 0.5 0.332 0.02023 -0.057 0.657 0.995 1.000 0.995 16.401 0.251 0.420 1.0 0.389 0.02078 -0.057 0.618 0.995 1.000 0.995 18.728 0.251 0.395 1.5 0.446 0.02177 -0.057 0.570 0.995 1.000 0.995 20.501 0.251 0.377 2.0 0.504 0.02285 -0.057 0.507 0.995 1.000 0.995 22.041 0.251 0.363 2.5 0.561 0.02529 -0.057 0.344 0.995 1.000 0.995 22.168 0.251 0.351 3.0 0.618 0.02729 -0.057 0.225 0.995 1.000 0.995 22.628 0.252 0.342 3.5 0.674 0.02791 -0.057 0.168 0.995 1.000 0.996 24.155 0.252 0.335 4.0 0.730 0.02867 -0.057 0.113 0.995 1.000 0.996 25.479 0.252 0.328 4.5 0.786 0.02941 -0.057 0.068 0.995 1.000 0.995 26.721 0.252 0.323 5.0 0.840 0.02968 -0.057 0.040 0.995 1.000 0.995 28.292 0.252 0.318 5.5 0.891 0.02955 -0.057 0.023 0.995 1.000 0.995 30.164 0.252 0.314 6.0 0.941 0.02893 -0.058 0.002 0.995 1.000 0.995 32.524 0.086 0.311 6.5 0.718 0.03861 -0.086 0.001 0.995 0.002 0.995 18.585 0.093 0.370 7.0 0.745 0.04364 -0.088 0.001 0.996 0.001 0.996 17.075 0.341 0.369 7.5 0.768 0.04890 -0.091 0.001 0.996 0.001 0.996 15.703 0.366 0.368 8.0 0.785 0.05503 -0.093 0.000 0.996 0.001 0.996 14.257 0.416 0.368 8.5 0.796 0.06136 -0.095 0.000 0.996 0.001 0.996 12.968 0.519 0.370 9.0 0.802 0.06913 -0.098 0.000 0.996 0.001 0.996 11.598 0.981 0.372 9.5 0.802 0.07997 -0.100 0.000 0.996 0.001 0.996 10.029 -0.646 0.375 10.0 0.797 0.08781 -0.102 0.000 0.996 0.001 0.996 9.072 -0.052 0.378 10.5 0.787 0.10321 -0.105 0.000 0.995 0.001 0.995 7.622 0.069 0.383 11.0 0.771 0.10080 -0.107 0.000 0.995 0.001 0.995 7.648 0.120 0.389 11.5 0.751 0.11397 -0.109 0.000 0.995 0.001 0.995 6.588 0.144 0.395 12.0 0.727 0.11831 -0.112 0.001 0.995 0.001 0.995 6.143 0.158 0.403 12.5 0.700 0.13347 -0.114 0.001 0.995 0.001 0.995 5.246 0.167 0.413 13.0 0.670 0.14366 -0.116 0.001 0.995 0.002 0.995 4.666 0.173 0.423 13.5 0.639 0.15847 -0.119 0.001 0.995 0.002 0.995 4.034 0.175 0.435 14.0 0.608 0.17136 -0.121 0.001 0.996 0.002 0.996 3.546 0.177 0.449 14.5 0.576 0.18901 -0.123 0.001 0.996 0.002 0.996 3.045 0.177 0.464 15.0 0.543 0.21924 -0.126 0.001 0.996 0.002 0.996 2.478 0.177 0.481 Name = AG19 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 -0.215 0.19723 0.007 1.000 0.003 1.000 0.005 -1.090 0.032 0.284 -14.5 -0.224 0.18316 0.005 1.000 0.003 1.000 0.005 -1.224 0.030 0.274 -14.0 -0.233 0.18211 0.003 1.000 0.003 1.000 0.005 -1.281 0.023 0.264 -13.5 -0.242 0.16814 0.001 1.000 0.003 1.000 0.005 -1.439 0.009 0.255 -13.0 -0.250 0.15278 -0.001 1.000 0.002 1.000 0.005 -1.636 -0.013 0.247 -12.5 -0.257 0.14086 -0.003 1.000 0.002 1.000 0.005 -1.827 -0.051 0.239 -12.0 -0.264 0.13008 -0.005 1.000 0.002 1.000 0.004 -2.027 -0.121 0.232 -11.5 -0.268 0.11865 -0.007 1.000 0.002 1.000 0.004 -2.263 -0.275 0.224 -11.0 -0.271 0.10450 -0.009 1.000 0.002 1.000 0.004 -2.598 -0.820 0.217 -10.5 -0.272 0.10147 -0.011 1.000 0.002 1.000 0.004 -2.684 9.278 0.210 -10.0 -0.271 0.12769 -0.013 1.000 0.002 1.000 0.003 -2.122 0.960 0.202 -9.5 -0.266 0.11719 -0.015 1.000 0.002 1.000 0.004 -2.273 0.597 0.193 -9.0 -0.259 0.10576 -0.017 1.000 0.002 1.000 0.003 -2.448 0.476 0.183 -8.5 -0.248 0.09180 -0.019 1.000 0.002 1.000 0.004 -2.699 0.416 0.172 -8.0 -0.234 0.08139 -0.022 1.000 0.002 1.000 0.003 -2.869 0.383 0.158 -7.5 -0.216 0.07094 -0.024 1.000 0.002 1.000 0.003 -3.042 0.360 0.140 -7.0 -0.195 0.06340 -0.026 1.000 0.002 1.000 0.003 -3.071 0.344 0.117 -6.5 -0.170 0.05784 -0.028 1.000 0.001 1.000 0.002 -2.946 0.334 0.086 -6.0 -0.143 0.04907 -0.030 1.000 0.001 1.000 0.002 -2.919 0.325 0.040 -5.5 -0.113 0.04367 -0.032 1.000 0.001 1.000 0.002 -2.589 0.319 -0.035 -5.0 -0.081 0.03785 -0.034 1.000 0.001 1.000 0.002 -2.141 0.315 -0.175 -4.5 -0.047 0.03321 -0.037 1.000 0.002 1.000 0.002 -1.411 0.312 -0.531 -4.0 -0.011 0.02901 -0.039 1.000 0.002 1.000 0.003 -0.392 0.199 -3.158 -3.5 -0.133 0.02522 -0.041 1.000 0.002 1.000 0.003 -5.265 0.179 -0.058 -3.0 -0.073 0.02186 -0.043 1.000 0.002 1.000 0.003 -3.338 0.287 -0.342 -2.5 -0.013 0.01958 -0.045 0.966 0.003 1.000 0.003 -0.673 0.287 -3.190 -2.0 0.046 0.01819 -0.048 0.913 0.003 1.000 0.005 2.533 0.345 1.282 -1.5 0.102 0.03064 -0.056 0.855 0.006 1.000 0.997 3.328 0.327 0.802 -1.0 0.160 0.01591 -0.056 0.810 0.995 1.000 0.995 10.026 0.251 0.603 -0.5 0.217 0.01708 -0.056 0.736 0.995 1.000 0.995 12.712 0.251 0.510 0.0 0.274 0.01847 -0.056 0.681 0.995 1.000 0.995 14.863 0.251 0.456 0.5 0.332 0.01856 -0.057 0.657 0.995 1.000 0.995 17.880 0.251 0.420 1.0 0.389 0.01936 -0.057 0.618 0.995 1.000 0.995 20.106 0.251 0.395 1.5 0.446 0.02006 -0.057 0.570 0.995 1.000 0.995 22.249 0.251 0.377 2.0 0.504 0.02119 -0.057 0.507 0.995 1.000 0.995 23.769 0.251 0.363 2.5 0.561 0.02386 -0.057 0.344 0.995 1.000 0.995 23.495 0.251 0.351 3.0 0.618 0.02555 -0.057 0.225 0.995 1.000 0.995 24.166 0.252 0.342 3.5 0.674 0.02625 -0.057 0.168 0.995 1.000 0.996 25.685 0.252 0.335 4.0 0.730 0.02709 -0.057 0.113 0.995 1.000 0.996 26.967 0.252 0.328 4.5 0.786 0.02791 -0.057 0.068 0.995 1.000 0.995 28.165 0.252 0.323 5.0 0.840 0.02821 -0.057 0.040 0.995 1.000 0.995 29.763 0.252 0.318 5.5 0.891 0.02859 -0.057 0.023 0.995 1.000 0.995 31.186 0.252 0.314 6.0 0.941 0.02839 -0.058 0.002 0.995 1.000 0.995 33.140 0.087 0.311 6.5 0.716 0.03694 -0.086 0.001 0.995 0.003 0.995 19.382 0.093 0.370 7.0 0.745 0.04098 -0.088 0.001 0.996 0.001 0.996 18.181 0.338 0.369 7.5 0.768 0.04582 -0.091 0.001 0.996 0.001 0.996 16.761 0.366 0.368 8.0 0.785 0.05128 -0.093 0.000 0.996 0.001 0.996 15.299 0.418 0.368 8.5 0.795 0.05836 -0.095 0.000 0.996 0.001 0.996 13.629 0.524 0.370 9.0 0.802 0.06526 -0.098 0.000 0.996 0.001 0.996 12.283 0.945 0.372 9.5 0.802 0.07276 -0.100 0.000 0.996 0.001 0.996 11.023 -0.703 0.375 10.0 0.797 0.07934 -0.102 0.000 0.996 0.001 0.996 10.040 -0.048 0.378 10.5 0.786 0.09570 -0.105 0.000 0.995 0.001 0.995 8.218 0.072 0.383 11.0 0.771 0.09593 -0.107 0.000 0.995 0.001 0.995 8.032 0.119 0.389 11.5 0.751 0.10152 -0.109 0.000 0.995 0.001 0.995 7.396 0.144 0.395 12.0 0.726 0.11224 -0.112 0.001 0.995 0.002 0.995 6.471 0.158 0.404 12.5 0.700 0.12546 -0.114 0.001 0.995 0.001 0.995 5.578 0.167 0.413 13.0 0.670 0.13402 -0.116 0.001 0.995 0.002 0.995 4.999 0.173 0.423 13.5 0.639 0.14631 -0.119 0.001 0.995 0.002 0.995 4.367 0.175 0.436 14.0 0.607 0.15969 -0.121 0.001 0.996 0.002 0.996 3.804 0.177 0.449 14.5 0.575 0.17381 -0.123 0.001 0.996 0.002 0.996 3.310 0.177 0.464 15.0 0.543 0.18593 -0.126 0.001 0.996 0.002 0.996 2.922 0.177 0.481