Name = AG38 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 -0.394 0.34292 0.017 1.000 0.003 1.000 0.004 -1.148 -0.141 0.293 -14.5 -0.398 0.30472 0.015 1.000 0.003 1.000 0.004 -1.307 -0.228 0.288 -14.0 -0.402 0.28377 0.013 1.000 0.003 1.000 0.004 -1.415 -0.717 0.283 -13.5 -0.402 0.26789 0.011 1.000 0.002 1.000 0.004 -1.502 12.788 0.278 -13.0 -0.401 0.23311 0.009 1.000 0.002 1.000 0.004 -1.721 1.052 0.273 -12.5 -0.397 0.21840 0.007 1.000 0.002 1.000 0.004 -1.820 0.644 0.268 -12.0 -0.391 0.19031 0.005 1.000 0.002 1.000 0.003 -2.054 0.495 0.263 -11.5 -0.381 0.17321 0.003 1.000 0.003 1.000 0.003 -2.198 0.428 0.258 -11.0 -0.368 0.16053 0.001 1.000 0.003 1.000 0.003 -2.290 0.397 0.253 -10.5 -0.352 0.14461 -0.001 1.000 0.002 1.000 0.003 -2.434 0.373 0.247 -10.0 -0.333 0.12995 -0.003 1.000 0.002 1.000 0.003 -2.564 0.358 0.240 -9.5 -0.312 0.11548 -0.005 1.000 0.002 1.000 0.003 -2.702 0.347 0.233 -9.0 -0.288 0.10546 -0.008 1.000 0.002 1.000 0.003 -2.732 0.337 0.223 -8.5 -0.261 0.09787 -0.010 0.955 0.002 1.000 0.003 -2.672 0.331 0.212 -8.0 -0.233 0.08520 -0.012 0.934 0.003 1.000 0.003 -2.734 0.326 0.198 -7.5 -0.202 0.07756 -0.014 0.929 0.003 1.000 0.003 -2.610 0.322 0.179 -7.0 -0.170 0.06937 -0.017 0.924 0.003 1.000 0.004 -2.450 0.319 0.152 -6.5 -0.136 0.06217 -0.019 0.920 0.003 1.000 0.004 -2.184 0.317 0.110 -6.0 -0.101 0.05604 -0.021 0.915 0.003 1.000 0.004 -1.798 0.316 0.038 -5.5 -0.064 0.05059 -0.024 0.912 0.003 1.000 0.004 -1.271 0.314 -0.119 -5.0 -0.027 0.04596 -0.026 0.908 0.004 1.000 0.005 -0.588 0.201 -0.715 -4.5 -0.163 0.04215 -0.028 0.906 0.004 1.000 0.005 -3.856 0.183 0.075 -4.0 -0.100 0.03861 -0.031 0.904 0.005 1.000 0.006 -2.588 0.289 -0.060 -3.5 -0.038 0.03554 -0.033 0.901 0.005 1.000 0.007 -1.062 0.290 -0.635 -3.0 0.024 0.03319 -0.036 0.899 0.007 1.000 0.009 0.717 0.291 1.758 -2.5 0.085 0.03079 -0.038 0.896 0.009 1.000 0.013 2.745 0.369 0.704 -2.0 0.140 0.03999 -0.050 0.477 0.996 1.000 0.996 3.490 0.353 0.606 -1.5 0.198 0.03987 -0.050 0.468 0.996 1.000 0.996 4.969 0.257 0.503 -1.0 0.257 0.03946 -0.050 0.462 0.996 1.000 0.996 6.502 0.257 0.447 -0.5 0.315 0.03901 -0.051 0.459 0.996 1.000 0.996 8.075 0.258 0.412 0.0 0.373 0.03880 -0.051 0.455 0.996 1.000 0.996 9.622 0.258 0.388 0.5 0.432 0.03888 -0.052 0.447 0.996 1.000 0.996 11.102 0.258 0.370 1.0 0.490 0.03874 -0.052 0.435 0.996 1.000 0.996 12.644 0.259 0.357 1.5 0.548 0.03849 -0.053 0.417 0.996 1.000 0.997 14.235 0.259 0.346 2.0 0.606 0.03908 -0.053 0.369 0.996 1.000 0.997 15.504 0.259 0.338 2.5 0.664 0.04026 -0.054 0.302 0.996 1.000 0.996 16.480 0.260 0.331 3.0 0.721 0.04222 -0.054 0.205 0.996 1.000 0.996 17.072 0.260 0.326 3.5 0.778 0.04277 -0.055 0.135 0.996 1.000 0.997 18.182 0.261 0.321 4.0 0.834 0.04302 -0.056 0.063 0.996 1.000 0.996 19.381 0.312 0.317 4.5 0.855 0.03704 -0.060 0.021 0.996 0.937 0.996 23.080 0.114 0.320 5.0 0.661 0.05089 -0.079 0.013 0.997 0.024 0.997 12.982 0.106 0.370 5.5 0.702 0.05402 -0.082 0.010 0.997 0.016 0.997 12.994 0.320 0.367 6.0 0.739 0.05774 -0.085 0.008 0.997 0.013 0.997 12.802 0.329 0.365 6.5 0.773 0.06273 -0.088 0.007 0.996 0.011 0.996 12.327 0.337 0.363 7.0 0.805 0.06789 -0.091 0.006 0.996 0.009 0.996 11.861 0.344 0.362 7.5 0.834 0.07352 -0.093 0.005 0.996 0.008 0.996 11.348 0.354 0.362 8.0 0.861 0.08039 -0.096 0.004 0.996 0.006 0.997 10.709 0.366 0.362 8.5 0.885 0.08781 -0.099 0.003 0.997 0.005 0.998 10.076 0.383 0.362 9.0 0.905 0.09667 -0.102 0.003 0.997 0.005 0.998 9.360 0.411 0.363 9.5 0.921 0.10649 -0.105 0.002 0.996 0.004 0.997 8.651 0.459 0.364 10.0 0.933 0.11972 -0.108 0.002 0.996 0.003 0.997 7.795 0.571 0.366 10.5 0.940 0.12849 -0.111 0.001 0.997 0.003 0.998 7.314 0.988 0.368 11.0 0.941 0.14082 -0.114 0.001 0.997 0.002 0.998 6.685 -4.374 0.371 11.5 0.939 0.15979 -0.117 0.001 0.997 0.002 0.998 5.874 -0.361 0.375 12.0 0.931 0.17209 -0.120 0.001 0.997 0.002 0.998 5.412 -0.079 0.379 12.5 0.920 0.19842 -0.123 0.001 0.997 0.002 0.998 4.637 0.017 0.384 13.0 0.905 0.21187 -0.126 0.001 0.996 0.001 0.997 4.273 0.065 0.390 13.5 0.887 0.23460 -0.129 0.001 0.996 0.001 0.997 3.780 0.095 0.396 14.0 0.865 0.27290 -0.132 0.001 0.996 0.001 0.997 3.171 0.113 0.403 14.5 0.841 0.28735 -0.136 0.000 0.996 0.001 0.997 2.928 0.126 0.411 15.0 0.815 0.31811 -0.139 0.000 0.996 0.001 0.997 2.563 0.131 0.420 Name = AG38 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 -0.393 0.21590 0.017 1.000 0.003 1.000 0.004 -1.822 -0.145 0.293 -14.5 -0.398 0.20965 0.015 1.000 0.003 1.000 0.004 -1.900 -0.232 0.288 -14.0 -0.401 0.21932 0.013 1.000 0.003 1.000 0.004 -1.830 -0.706 0.283 -13.5 -0.402 0.20370 0.011 1.000 0.002 1.000 0.004 -1.975 12.006 0.278 -13.0 -0.401 0.18044 0.009 1.000 0.002 1.000 0.004 -2.223 1.041 0.273 -12.5 -0.397 0.17016 0.007 1.000 0.002 1.000 0.004 -2.335 0.644 0.268 -12.0 -0.391 0.15061 0.005 1.000 0.002 1.000 0.004 -2.595 0.495 0.263 -11.5 -0.381 0.13940 0.003 1.000 0.003 1.000 0.004 -2.730 0.430 0.258 -11.0 -0.368 0.12240 0.001 1.000 0.003 1.000 0.003 -3.004 0.397 0.253 -10.5 -0.352 0.11780 -0.001 1.000 0.002 1.000 0.003 -2.986 0.372 0.247 -10.0 -0.333 0.10586 -0.003 1.000 0.002 1.000 0.004 -3.145 0.358 0.240 -9.5 -0.312 0.09470 -0.005 1.000 0.002 1.000 0.003 -3.292 0.347 0.233 -9.0 -0.288 0.08713 -0.008 1.000 0.002 1.000 0.003 -3.304 0.338 0.223 -8.5 -0.261 0.07721 -0.010 0.955 0.002 1.000 0.003 -3.387 0.331 0.212 -8.0 -0.233 0.06857 -0.012 0.934 0.003 1.000 0.003 -3.397 0.326 0.198 -7.5 -0.202 0.06287 -0.014 0.929 0.003 1.000 0.003 -3.219 0.322 0.179 -7.0 -0.170 0.05666 -0.017 0.924 0.003 1.000 0.004 -2.999 0.319 0.152 -6.5 -0.136 0.05144 -0.019 0.920 0.003 1.000 0.004 -2.639 0.317 0.110 -6.0 -0.101 0.04659 -0.021 0.915 0.003 1.000 0.004 -2.163 0.316 0.038 -5.5 -0.064 0.04337 -0.024 0.912 0.003 1.000 0.005 -1.477 0.314 -0.120 -5.0 -0.027 0.03924 -0.026 0.908 0.004 1.000 0.005 -0.683 0.201 -0.723 -4.5 -0.163 0.03566 -0.028 0.906 0.004 1.000 0.005 -4.558 0.184 0.075 -4.0 -0.100 0.03289 -0.031 0.904 0.005 1.000 0.006 -3.038 0.289 -0.060 -3.5 -0.038 0.03025 -0.033 0.901 0.005 1.000 0.007 -1.247 0.290 -0.635 -3.0 0.024 0.02780 -0.036 0.899 0.007 1.000 0.009 0.856 0.291 1.757 -2.5 0.085 0.02595 -0.038 0.896 0.009 1.000 0.013 3.258 0.369 0.704 -2.0 0.140 0.03306 -0.050 0.477 0.996 1.000 0.996 4.221 0.353 0.606 -1.5 0.198 0.03331 -0.050 0.468 0.996 1.000 0.996 5.948 0.257 0.503 -1.0 0.257 0.03348 -0.050 0.462 0.996 1.000 0.996 7.663 0.257 0.447 -0.5 0.315 0.03299 -0.051 0.459 0.996 1.000 0.996 9.549 0.258 0.412 0.0 0.373 0.03326 -0.051 0.455 0.996 1.000 0.996 11.225 0.258 0.388 0.5 0.432 0.03316 -0.052 0.447 0.996 1.000 0.996 13.016 0.258 0.370 1.0 0.490 0.03348 -0.052 0.435 0.996 1.000 0.996 14.634 0.259 0.357 1.5 0.548 0.03359 -0.053 0.417 0.996 1.000 0.997 16.312 0.259 0.346 2.0 0.606 0.03431 -0.053 0.369 0.996 1.000 0.997 17.657 0.259 0.338 2.5 0.664 0.03580 -0.054 0.302 0.996 1.000 0.996 18.532 0.260 0.331 3.0 0.721 0.03730 -0.054 0.205 0.996 1.000 0.996 19.324 0.260 0.326 3.5 0.778 0.03827 -0.055 0.135 0.996 1.000 0.997 20.322 0.261 0.321 4.0 0.834 0.03928 -0.056 0.063 0.996 1.000 0.996 21.230 0.261 0.317 4.5 0.889 0.03919 -0.056 0.021 0.996 1.000 0.996 22.692 0.262 0.313 5.0 0.944 0.03747 -0.057 0.013 0.997 1.000 0.997 25.187 0.116 0.310 5.5 0.697 0.04744 -0.082 0.010 0.997 0.021 0.997 14.700 0.115 0.368 6.0 0.737 0.05044 -0.085 0.008 0.997 0.015 0.997 14.607 0.325 0.365 6.5 0.772 0.05402 -0.088 0.007 0.996 0.012 0.996 14.293 0.334 0.364 7.0 0.804 0.05819 -0.091 0.006 0.996 0.010 0.996 13.821 0.344 0.363 7.5 0.833 0.06286 -0.093 0.005 0.996 0.008 0.996 13.258 0.355 0.362 8.0 0.860 0.06834 -0.096 0.004 0.996 0.007 0.997 12.580 0.366 0.362 8.5 0.884 0.07433 -0.099 0.003 0.997 0.006 0.998 11.888 0.383 0.362 9.0 0.904 0.08041 -0.102 0.003 0.997 0.005 0.998 11.241 0.410 0.363 9.5 0.920 0.08876 -0.105 0.002 0.996 0.004 0.997 10.370 0.457 0.364 10.0 0.933 0.09722 -0.108 0.002 0.996 0.004 0.997 9.592 0.567 0.366 10.5 0.939 0.10489 -0.111 0.001 0.997 0.003 0.998 8.953 0.995 0.368 11.0 0.941 0.11462 -0.114 0.001 0.997 0.003 0.998 8.206 -5.940 0.371 11.5 0.938 0.12583 -0.117 0.001 0.997 0.002 0.998 7.456 -0.366 0.375 12.0 0.931 0.14059 -0.120 0.001 0.997 0.002 0.998 6.620 -0.079 0.379 12.5 0.920 0.15489 -0.123 0.001 0.997 0.002 0.998 5.938 0.016 0.384 13.0 0.905 0.17281 -0.126 0.001 0.996 0.002 0.997 5.234 0.067 0.390 13.5 0.886 0.19166 -0.129 0.001 0.996 0.001 0.997 4.624 0.093 0.396 14.0 0.865 0.20023 -0.132 0.001 0.996 0.001 0.997 4.322 0.112 0.403 14.5 0.841 0.22125 -0.136 0.000 0.996 0.001 0.997 3.802 0.126 0.411 15.0 0.815 0.23892 -0.139 0.000 0.996 0.001 0.997 3.411 0.131 0.420 Name = AG38 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 -0.393 0.18680 0.017 1.000 0.003 1.000 0.005 -2.106 -0.142 0.293 -14.5 -0.398 0.17198 0.015 1.000 0.003 1.000 0.004 -2.316 -0.233 0.288 -14.0 -0.401 0.19166 0.013 1.000 0.003 1.000 0.004 -2.094 -0.725 0.283 -13.5 -0.402 0.15365 0.011 1.000 0.002 1.000 0.004 -2.618 11.471 0.278 -13.0 -0.401 0.15786 0.009 1.000 0.002 1.000 0.004 -2.540 1.039 0.273 -12.5 -0.397 0.14975 0.007 1.000 0.002 1.000 0.004 -2.652 0.641 0.268 -12.0 -0.391 0.13390 0.005 1.000 0.002 1.000 0.004 -2.917 0.498 0.263 -11.5 -0.381 0.11874 0.003 1.000 0.003 1.000 0.004 -3.205 0.430 0.258 -11.0 -0.367 0.11107 0.001 1.000 0.003 1.000 0.004 -3.308 0.397 0.253 -10.5 -0.352 0.10101 -0.001 1.000 0.002 1.000 0.003 -3.483 0.373 0.247 -10.0 -0.333 0.09085 -0.003 1.000 0.002 1.000 0.004 -3.665 0.358 0.240 -9.5 -0.312 0.08222 -0.005 1.000 0.002 1.000 0.003 -3.792 0.347 0.233 -9.0 -0.288 0.07588 -0.008 1.000 0.002 1.000 0.003 -3.793 0.338 0.223 -8.5 -0.261 0.06826 -0.010 0.955 0.002 1.000 0.003 -3.831 0.331 0.212 -8.0 -0.233 0.06382 -0.012 0.934 0.003 1.000 0.004 -3.646 0.326 0.198 -7.5 -0.202 0.05737 -0.014 0.929 0.003 1.000 0.004 -3.525 0.323 0.179 -7.0 -0.170 0.05195 -0.017 0.924 0.003 1.000 0.004 -3.269 0.319 0.152 -6.5 -0.136 0.04669 -0.019 0.920 0.003 1.000 0.004 -2.908 0.317 0.110 -6.0 -0.101 0.04357 -0.021 0.915 0.003 1.000 0.004 -2.308 0.316 0.038 -5.5 -0.064 0.03947 -0.024 0.912 0.003 1.000 0.005 -1.623 0.314 -0.120 -5.0 -0.027 0.03601 -0.026 0.908 0.004 1.000 0.005 -0.744 0.201 -0.723 -4.5 -0.163 0.03304 -0.028 0.906 0.004 1.000 0.006 -4.919 0.184 0.075 -4.0 -0.100 0.03034 -0.031 0.904 0.005 1.000 0.007 -3.293 0.289 -0.060 -3.5 -0.038 0.02779 -0.033 0.901 0.005 1.000 0.007 -1.358 0.290 -0.635 -3.0 0.024 0.02578 -0.036 0.899 0.007 1.000 0.010 0.923 0.290 1.757 -2.5 0.085 0.02374 -0.038 0.896 0.009 1.000 0.015 3.561 0.369 0.704 -2.0 0.140 0.03034 -0.050 0.477 0.996 1.000 0.996 4.600 0.353 0.606 -1.5 0.198 0.03041 -0.050 0.468 0.996 1.000 0.996 6.514 0.257 0.503 -1.0 0.257 0.03056 -0.050 0.462 0.996 1.000 0.996 8.396 0.257 0.447 -0.5 0.315 0.03065 -0.051 0.459 0.996 1.000 0.996 10.278 0.258 0.412 0.0 0.373 0.03028 -0.051 0.455 0.996 1.000 0.996 12.328 0.258 0.388 0.5 0.432 0.03065 -0.052 0.447 0.996 1.000 0.996 14.085 0.258 0.370 1.0 0.490 0.03049 -0.052 0.435 0.996 1.000 0.996 16.067 0.259 0.357 1.5 0.548 0.03104 -0.053 0.417 0.996 1.000 0.997 17.653 0.259 0.346 2.0 0.606 0.03185 -0.053 0.369 0.996 1.000 0.997 19.021 0.259 0.338 2.5 0.664 0.03351 -0.054 0.302 0.996 1.000 0.996 19.802 0.260 0.331 3.0 0.721 0.03478 -0.054 0.205 0.996 1.000 0.996 20.727 0.260 0.326 3.5 0.778 0.03595 -0.055 0.135 0.996 1.000 0.997 21.632 0.261 0.321 4.0 0.834 0.03730 -0.056 0.063 0.996 1.000 0.996 22.358 0.261 0.317 4.5 0.889 0.03758 -0.056 0.021 0.996 1.000 0.996 23.664 0.262 0.313 5.0 0.944 0.03692 -0.057 0.013 0.997 1.000 0.997 25.563 0.289 0.310 5.5 0.979 0.03139 -0.060 0.010 0.997 0.969 0.997 31.176 0.117 0.311 6.0 0.733 0.04736 -0.085 0.008 0.997 0.018 0.997 15.488 0.116 0.366 6.5 0.771 0.05034 -0.088 0.007 0.996 0.013 0.996 15.307 0.331 0.364 7.0 0.803 0.05425 -0.091 0.006 0.996 0.011 0.996 14.798 0.343 0.363 7.5 0.832 0.05821 -0.093 0.005 0.996 0.009 0.996 14.298 0.354 0.362 8.0 0.859 0.06304 -0.096 0.004 0.996 0.008 0.997 13.621 0.366 0.362 8.5 0.883 0.06782 -0.099 0.003 0.997 0.007 0.998 13.017 0.382 0.362 9.0 0.903 0.07327 -0.102 0.003 0.997 0.006 0.998 12.325 0.409 0.363 9.5 0.920 0.07994 -0.105 0.002 0.996 0.004 0.997 11.506 0.455 0.364 10.0 0.932 0.08730 -0.108 0.002 0.996 0.004 0.997 10.675 0.575 0.366 10.5 0.938 0.09593 -0.111 0.001 0.997 0.003 0.998 9.780 0.999 0.368 11.0 0.940 0.10317 -0.114 0.001 0.997 0.003 0.998 9.111 -8.286 0.371 11.5 0.937 0.11443 -0.117 0.001 0.997 0.002 0.998 8.192 -0.386 0.375 12.0 0.930 0.12350 -0.120 0.001 0.997 0.002 0.998 7.534 -0.087 0.379 12.5 0.919 0.13592 -0.123 0.001 0.997 0.002 0.998 6.764 0.016 0.384 13.0 0.904 0.15023 -0.126 0.001 0.996 0.002 0.997 6.019 0.067 0.390 13.5 0.886 0.16619 -0.129 0.001 0.996 0.002 0.997 5.330 0.093 0.396 14.0 0.865 0.17669 -0.132 0.001 0.996 0.001 0.997 4.896 0.112 0.403 14.5 0.841 0.19378 -0.136 0.000 0.996 0.001 0.997 4.339 0.127 0.411 15.0 0.815 0.21844 -0.139 0.000 0.996 0.001 0.997 3.729 0.132 0.420 Name = AG38 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 -0.393 0.16960 0.017 1.000 0.003 1.000 0.005 -2.319 -0.143 0.293 -14.5 -0.398 0.15752 0.015 1.000 0.003 1.000 0.005 -2.528 -0.234 0.288 -14.0 -0.401 0.15227 0.013 1.000 0.003 1.000 0.004 -2.635 -0.729 0.283 -13.5 -0.402 0.14097 0.011 1.000 0.002 1.000 0.005 -2.853 10.979 0.278 -13.0 -0.401 0.12839 0.009 1.000 0.002 1.000 0.004 -3.123 1.057 0.273 -12.5 -0.397 0.13077 0.007 1.000 0.002 1.000 0.004 -3.037 0.641 0.268 -12.0 -0.391 0.12441 0.005 1.000 0.002 1.000 0.004 -3.139 0.494 0.263 -11.5 -0.380 0.11166 0.003 1.000 0.003 1.000 0.004 -3.406 0.431 0.258 -11.0 -0.367 0.09988 0.001 1.000 0.003 1.000 0.004 -3.679 0.398 0.253 -10.5 -0.352 0.09119 -0.001 1.000 0.002 1.000 0.003 -3.858 0.372 0.247 -10.0 -0.333 0.08601 -0.003 1.000 0.002 1.000 0.004 -3.868 0.357 0.240 -9.5 -0.312 0.07795 -0.005 1.000 0.002 1.000 0.004 -3.997 0.348 0.233 -9.0 -0.288 0.06930 -0.008 1.000 0.002 1.000 0.003 -4.154 0.338 0.223 -8.5 -0.261 0.06508 -0.010 0.955 0.002 1.000 0.004 -4.014 0.331 0.212 -8.0 -0.233 0.05890 -0.012 0.934 0.003 1.000 0.004 -3.950 0.327 0.198 -7.5 -0.202 0.05350 -0.014 0.929 0.003 1.000 0.004 -3.781 0.323 0.179 -7.0 -0.170 0.04856 -0.017 0.924 0.003 1.000 0.004 -3.497 0.319 0.152 -6.5 -0.136 0.04478 -0.019 0.920 0.003 1.000 0.004 -3.027 0.317 0.110 -6.0 -0.101 0.04096 -0.021 0.915 0.003 1.000 0.004 -2.455 0.316 0.038 -5.5 -0.064 0.03721 -0.024 0.912 0.003 1.000 0.005 -1.722 0.314 -0.120 -5.0 -0.027 0.03397 -0.026 0.908 0.004 1.000 0.005 -0.789 0.201 -0.723 -4.5 -0.163 0.03132 -0.028 0.906 0.004 1.000 0.006 -5.190 0.184 0.075 -4.0 -0.100 0.02877 -0.031 0.904 0.005 1.000 0.007 -3.473 0.289 -0.060 -3.5 -0.038 0.02638 -0.033 0.901 0.005 1.000 0.008 -1.430 0.290 -0.635 -3.0 0.024 0.02443 -0.036 0.899 0.007 1.000 0.010 0.974 0.290 1.757 -2.5 0.084 0.02266 -0.038 0.896 0.009 1.000 0.023 3.728 0.369 0.703 -2.0 0.140 0.02856 -0.050 0.477 0.996 1.000 0.996 4.886 0.354 0.606 -1.5 0.198 0.02856 -0.050 0.468 0.996 1.000 0.996 6.937 0.257 0.503 -1.0 0.257 0.02870 -0.050 0.462 0.996 1.000 0.996 8.941 0.257 0.447 -0.5 0.315 0.02879 -0.051 0.459 0.996 1.000 0.996 10.940 0.258 0.412 0.0 0.373 0.02900 -0.051 0.455 0.996 1.000 0.996 12.875 0.258 0.388 0.5 0.432 0.02893 -0.052 0.447 0.996 1.000 0.996 14.921 0.258 0.370 1.0 0.490 0.02880 -0.052 0.435 0.996 1.000 0.996 17.012 0.259 0.357 1.5 0.548 0.02933 -0.053 0.417 0.996 1.000 0.997 18.683 0.259 0.346 2.0 0.606 0.03020 -0.053 0.369 0.996 1.000 0.997 20.065 0.259 0.338 2.5 0.664 0.03142 -0.054 0.302 0.996 1.000 0.996 21.116 0.260 0.331 3.0 0.721 0.03339 -0.054 0.205 0.996 1.000 0.996 21.589 0.260 0.326 3.5 0.778 0.03471 -0.055 0.135 0.996 1.000 0.997 22.401 0.261 0.321 4.0 0.834 0.03568 -0.056 0.063 0.996 1.000 0.996 23.371 0.261 0.317 4.5 0.889 0.03617 -0.056 0.021 0.996 1.000 0.996 24.584 0.262 0.313 5.0 0.944 0.03613 -0.057 0.013 0.997 1.000 0.997 26.124 0.262 0.310 5.5 0.997 0.03566 -0.058 0.010 0.997 1.000 0.997 27.955 0.120 0.308 6.0 0.728 0.04593 -0.085 0.008 0.997 0.025 0.997 15.847 0.118 0.367 6.5 0.768 0.04841 -0.088 0.007 0.996 0.015 0.996 15.865 0.325 0.364 7.0 0.801 0.05178 -0.091 0.006 0.996 0.012 0.996 15.474 0.340 0.363 7.5 0.831 0.05545 -0.093 0.005 0.996 0.010 0.996 14.991 0.353 0.362 8.0 0.858 0.05989 -0.096 0.004 0.996 0.009 0.997 14.319 0.366 0.362 8.5 0.882 0.06445 -0.099 0.003 0.997 0.007 0.998 13.679 0.382 0.363 9.0 0.902 0.06965 -0.102 0.003 0.997 0.006 0.998 12.950 0.408 0.363 9.5 0.919 0.07555 -0.105 0.002 0.996 0.005 0.997 12.162 0.453 0.364 10.0 0.931 0.08244 -0.108 0.002 0.996 0.004 0.997 11.294 0.571 0.366 10.5 0.937 0.08905 -0.111 0.001 0.997 0.004 0.998 10.527 0.977 0.369 11.0 0.939 0.09570 -0.114 0.001 0.997 0.003 0.998 9.815 -14.656 0.372 11.5 0.937 0.10480 -0.117 0.001 0.997 0.003 0.998 8.942 -0.405 0.375 12.0 0.930 0.11332 -0.120 0.001 0.997 0.002 0.998 8.207 -0.087 0.379 12.5 0.919 0.12475 -0.123 0.001 0.997 0.002 0.998 7.367 0.016 0.384 13.0 0.904 0.13683 -0.126 0.001 0.996 0.002 0.997 6.606 0.067 0.390 13.5 0.885 0.15112 -0.129 0.001 0.996 0.002 0.997 5.859 0.093 0.396 14.0 0.865 0.16289 -0.132 0.001 0.996 0.001 0.997 5.309 0.112 0.403 14.5 0.841 0.17767 -0.136 0.000 0.996 0.001 0.997 4.731 0.126 0.411 15.0 0.814 0.19701 -0.139 0.000 0.996 0.001 0.997 4.133 0.131 0.420