Name = SD7003-085-88 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 -0.544 0.27506 0.030 1.000 0.002 1.000 0.003 -1.977 -0.239 0.304 -14.5 -0.548 0.27116 0.027 1.000 0.002 1.000 0.003 -2.023 -0.432 0.300 -14.0 -0.551 0.24431 0.025 1.000 0.002 1.000 0.002 -2.253 -2.866 0.295 -13.5 -0.550 0.22154 0.023 1.000 0.001 1.000 0.002 -2.482 1.637 0.291 -13.0 -0.547 0.18975 0.020 1.000 0.001 1.000 0.002 -2.884 0.737 0.287 -12.5 -0.541 0.16724 0.018 1.000 0.002 1.000 0.003 -3.232 0.549 0.284 -12.0 -0.532 0.15277 0.016 1.000 0.002 1.000 0.003 -3.481 0.476 0.280 -11.5 -0.520 0.13482 0.013 1.000 0.002 1.000 0.003 -3.857 0.425 0.276 -11.0 -0.505 0.12197 0.011 1.000 0.002 1.000 0.003 -4.143 0.393 0.272 -10.5 -0.488 0.11185 0.009 1.000 0.002 1.000 0.003 -4.358 0.372 0.268 -10.0 -0.467 0.10062 0.006 1.000 0.002 1.000 0.003 -4.640 0.357 0.264 -9.5 -0.444 0.08917 0.004 1.000 0.002 1.000 0.003 -4.975 0.347 0.259 -9.0 -0.418 0.08292 0.002 1.000 0.002 1.000 0.003 -5.047 0.338 0.254 -8.5 -0.390 0.07484 -0.001 1.000 0.003 1.000 0.004 -5.207 0.328 0.248 -8.0 -0.358 0.06798 -0.003 1.000 0.003 1.000 0.005 -5.272 0.322 0.242 -7.5 -0.325 0.06212 -0.005 0.987 0.004 1.000 0.007 -5.230 0.319 0.234 -7.0 -0.291 0.05717 -0.008 0.983 0.006 1.000 0.009 -5.082 0.319 0.224 -6.5 -0.256 0.05299 -0.010 0.979 0.007 1.000 0.010 -4.822 0.317 0.211 -6.0 -0.219 0.04785 -0.012 0.975 0.008 1.000 0.011 -4.569 0.315 0.193 -5.5 -0.181 0.04341 -0.015 0.969 0.009 1.000 0.012 -4.174 0.312 0.168 -5.0 -0.142 0.04039 -0.017 0.965 0.011 1.000 0.015 -3.505 0.308 0.128 -4.5 -0.100 0.03739 -0.020 0.960 0.013 1.000 0.023 -2.667 0.302 0.054 -4.0 -0.054 0.03571 -0.022 0.954 0.025 1.000 0.042 -1.523 0.300 -0.150 -3.5 -0.011 0.03362 -0.024 0.933 0.035 1.000 0.066 -0.340 0.040 -1.849 -3.0 -0.143 0.02991 -0.040 0.863 0.044 1.000 0.999 -4.775 0.023 -0.032 -2.5 -0.085 0.03117 -0.041 0.799 0.071 1.000 0.999 -2.716 0.255 -0.230 -2.0 -0.026 0.02826 -0.041 0.730 0.476 1.000 0.999 -0.933 0.255 -1.301 -1.5 0.032 0.02724 -0.041 0.682 0.581 1.000 0.998 1.175 0.255 1.537 -1.0 0.090 0.02753 -0.041 0.633 0.630 1.000 0.998 3.284 0.255 0.709 -0.5 0.149 0.02766 -0.042 0.586 0.664 1.000 0.998 5.381 0.255 0.531 0.0 0.207 0.02797 -0.042 0.536 0.689 1.000 0.999 7.406 0.255 0.453 0.5 0.265 0.02870 -0.042 0.476 0.715 1.000 0.999 9.249 0.255 0.410 1.0 0.324 0.02871 -0.043 0.430 0.742 1.000 0.999 11.275 0.255 0.382 1.5 0.382 0.02929 -0.043 0.377 0.773 1.000 0.999 13.044 0.255 0.363 2.0 0.440 0.02933 -0.043 0.331 0.811 1.000 0.999 15.006 0.255 0.348 2.5 0.498 0.02907 -0.044 0.283 0.856 1.000 0.998 17.136 0.255 0.338 3.0 0.556 0.02923 -0.044 0.238 0.904 1.000 0.998 19.026 0.256 0.329 3.5 0.614 0.02795 -0.044 0.196 0.998 1.000 0.998 21.967 0.262 0.322 4.0 0.666 0.02737 -0.045 0.157 0.998 0.987 0.998 24.343 0.276 0.318 4.5 0.714 0.02749 -0.047 0.125 0.998 0.967 0.998 25.967 0.319 0.316 5.0 0.745 0.02852 -0.051 0.097 0.998 0.912 0.998 26.116 2.709 0.318 5.5 0.720 0.03169 -0.061 0.073 0.998 0.738 0.998 22.705 0.065 0.335 6.0 0.616 0.04380 -0.075 0.061 0.998 0.370 0.998 14.061 0.103 0.371 6.5 0.607 0.05248 -0.078 0.045 0.998 0.164 0.998 11.573 0.405 0.378 7.0 0.646 0.05645 -0.079 0.028 0.998 0.086 0.999 11.446 0.287 0.373 7.5 0.694 0.05830 -0.081 0.015 0.998 0.043 0.998 11.908 0.285 0.366 8.0 0.745 0.05960 -0.083 0.007 0.998 0.018 0.999 12.495 0.297 0.361 8.5 0.784 0.06349 -0.085 0.006 0.998 0.012 0.999 12.341 0.313 0.359 9.0 0.819 0.06786 -0.087 0.005 0.998 0.007 0.998 12.069 0.325 0.357 9.5 0.848 0.07421 -0.090 0.004 0.998 0.006 0.998 11.427 0.339 0.356 10.0 0.875 0.08152 -0.092 0.004 0.998 0.006 0.998 10.730 0.348 0.356 10.5 0.899 0.08964 -0.095 0.003 0.998 0.005 0.998 10.028 0.359 0.356 11.0 0.921 0.09869 -0.097 0.003 0.998 0.005 0.998 9.330 0.370 0.356 11.5 0.940 0.10688 -0.100 0.003 0.998 0.004 0.999 8.799 0.388 0.356 12.0 0.957 0.11827 -0.102 0.003 0.998 0.004 0.998 8.091 0.414 0.357 12.5 0.971 0.12773 -0.105 0.003 0.998 0.004 0.998 7.600 0.447 0.358 13.0 0.982 0.13799 -0.107 0.003 0.998 0.004 0.998 7.119 0.575 0.359 13.5 0.986 0.15577 -0.110 0.003 0.998 0.004 0.998 6.331 2.200 0.361 14.0 0.985 0.17547 -0.112 0.002 0.998 0.004 0.998 5.613 -0.651 0.364 14.5 0.981 0.18436 -0.115 0.002 0.998 0.003 0.998 5.319 -0.140 0.367 15.0 0.972 0.20785 -0.117 0.002 0.998 0.003 0.999 4.677 -0.042 0.371 Name = SD7003-085-88 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 -0.544 0.21647 0.030 1.000 0.002 1.000 0.003 -2.511 -0.226 0.304 -14.5 -0.548 0.20359 0.027 1.000 0.002 1.000 0.003 -2.693 -0.419 0.300 -14.0 -0.550 0.18622 0.025 1.000 0.002 1.000 0.003 -2.955 -2.907 0.295 -13.5 -0.550 0.16878 0.023 1.000 0.001 1.000 0.003 -3.257 1.629 0.291 -13.0 -0.547 0.14812 0.020 1.000 0.001 1.000 0.002 -3.693 0.736 0.287 -12.5 -0.540 0.13127 0.018 1.000 0.002 1.000 0.003 -4.116 0.548 0.284 -12.0 -0.532 0.12127 0.016 1.000 0.002 1.000 0.003 -4.384 0.475 0.280 -11.5 -0.520 0.10707 0.013 1.000 0.002 1.000 0.003 -4.855 0.425 0.276 -11.0 -0.505 0.09739 0.011 1.000 0.002 1.000 0.003 -5.186 0.393 0.272 -10.5 -0.487 0.08930 0.009 1.000 0.002 1.000 0.003 -5.457 0.372 0.268 -10.0 -0.467 0.08058 0.006 1.000 0.002 1.000 0.003 -5.792 0.356 0.264 -9.5 -0.443 0.07321 0.004 1.000 0.002 1.000 0.004 -6.054 0.346 0.259 -9.0 -0.418 0.06903 0.002 1.000 0.002 1.000 0.004 -6.051 0.337 0.254 -8.5 -0.389 0.06213 -0.001 1.000 0.003 1.000 0.004 -6.260 0.328 0.249 -8.0 -0.358 0.05658 -0.003 1.000 0.003 1.000 0.006 -6.325 0.322 0.242 -7.5 -0.324 0.05207 -0.005 0.987 0.004 1.000 0.008 -6.229 0.319 0.234 -7.0 -0.290 0.04842 -0.008 0.983 0.006 1.000 0.009 -5.989 0.320 0.224 -6.5 -0.256 0.04406 -0.010 0.979 0.007 1.000 0.010 -5.800 0.317 0.211 -6.0 -0.218 0.04043 -0.012 0.975 0.008 1.000 0.012 -5.392 0.313 0.193 -5.5 -0.180 0.03729 -0.015 0.969 0.009 1.000 0.013 -4.824 0.310 0.168 -5.0 -0.139 0.03455 -0.017 0.965 0.011 1.000 0.020 -4.026 0.304 0.127 -4.5 -0.095 0.03251 -0.019 0.960 0.013 1.000 0.033 -2.927 0.297 0.046 -4.0 -0.050 0.03072 -0.021 0.954 0.025 1.000 0.070 -1.624 0.054 -0.178 -3.5 -0.201 0.02537 -0.040 0.933 0.035 1.000 0.999 -7.914 0.046 0.050 -3.0 -0.143 0.02640 -0.040 0.863 0.044 1.000 0.999 -5.409 0.255 -0.032 -2.5 -0.085 0.02701 -0.041 0.799 0.071 1.000 0.999 -3.134 0.255 -0.230 -2.0 -0.026 0.02404 -0.041 0.730 0.476 1.000 0.999 -1.097 0.255 -1.301 -1.5 0.032 0.02333 -0.041 0.682 0.581 1.000 0.999 1.372 0.255 1.537 -1.0 0.090 0.02337 -0.041 0.633 0.630 1.000 0.999 3.868 0.255 0.709 -0.5 0.149 0.02333 -0.042 0.586 0.664 1.000 0.999 6.377 0.255 0.531 0.0 0.207 0.02399 -0.042 0.536 0.689 1.000 0.999 8.635 0.255 0.453 0.5 0.265 0.02483 -0.042 0.476 0.715 1.000 0.999 10.693 0.255 0.410 1.0 0.324 0.02475 -0.043 0.430 0.742 1.000 0.999 13.081 0.255 0.382 1.5 0.382 0.02525 -0.043 0.377 0.773 1.000 0.999 15.131 0.255 0.363 2.0 0.440 0.02525 -0.043 0.331 0.811 1.000 0.999 17.430 0.255 0.348 2.5 0.498 0.02573 -0.044 0.283 0.856 1.000 0.998 19.359 0.255 0.338 3.0 0.556 0.02521 -0.044 0.238 0.904 1.000 0.998 22.061 0.256 0.329 3.5 0.614 0.02456 -0.044 0.196 0.998 1.000 0.998 24.994 0.256 0.322 4.0 0.671 0.02512 -0.045 0.157 0.998 1.000 0.998 26.727 0.256 0.316 4.5 0.729 0.02514 -0.045 0.125 0.998 1.000 0.998 28.989 0.256 0.312 5.0 0.785 0.02504 -0.045 0.097 0.998 1.000 0.998 31.373 0.256 0.308 5.5 0.842 0.02518 -0.046 0.073 0.998 1.000 0.998 33.427 0.278 0.304 6.0 0.884 0.02384 -0.048 0.061 0.998 0.974 0.998 37.070 0.345 0.304 6.5 0.912 0.02505 -0.052 0.045 0.998 0.926 0.998 36.414 -2.818 0.307 7.0 0.878 0.02857 -0.065 0.028 0.998 0.760 0.999 30.737 0.041 0.324 7.5 0.775 0.03927 -0.081 0.015 0.998 0.456 0.998 19.744 0.130 0.354 8.0 0.713 0.05455 -0.085 0.007 0.998 0.102 0.999 13.063 2.819 0.369 8.5 0.777 0.05528 -0.085 0.006 0.998 0.016 0.999 14.056 0.275 0.360 9.0 0.815 0.05908 -0.087 0.005 0.998 0.010 0.998 13.796 0.318 0.357 9.5 0.847 0.06347 -0.090 0.004 0.998 0.007 0.998 13.337 0.333 0.356 10.0 0.874 0.06855 -0.092 0.004 0.998 0.006 0.998 12.746 0.347 0.356 10.5 0.898 0.07501 -0.095 0.003 0.998 0.006 0.998 11.971 0.357 0.356 11.0 0.920 0.08055 -0.097 0.003 0.998 0.005 0.998 11.425 0.369 0.356 11.5 0.940 0.08721 -0.100 0.003 0.998 0.005 0.999 10.777 0.388 0.356 12.0 0.957 0.09580 -0.102 0.003 0.998 0.004 0.998 9.984 0.414 0.357 12.5 0.970 0.10377 -0.105 0.003 0.998 0.004 0.998 9.351 0.447 0.358 13.0 0.982 0.11162 -0.107 0.003 0.998 0.004 0.998 8.797 0.574 0.359 13.5 0.986 0.12626 -0.110 0.003 0.998 0.004 0.998 7.807 1.905 0.361 14.0 0.985 0.13272 -0.112 0.002 0.998 0.004 0.998 7.420 -0.657 0.364 14.5 0.980 0.14970 -0.115 0.002 0.998 0.003 0.998 6.548 -0.140 0.367 15.0 0.972 0.15637 -0.117 0.002 0.998 0.003 0.999 6.217 -0.054 0.371 Name = SD7003-085-88 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 -0.543 0.18402 0.030 1.000 0.002 1.000 0.003 -2.953 -0.227 0.304 -14.5 -0.548 0.17430 0.027 1.000 0.002 1.000 0.003 -3.145 -0.421 0.300 -14.0 -0.550 0.16108 0.025 1.000 0.002 1.000 0.003 -3.415 -2.948 0.295 -13.5 -0.550 0.14603 0.023 1.000 0.001 1.000 0.003 -3.763 1.622 0.291 -13.0 -0.547 0.13014 0.020 1.000 0.001 1.000 0.002 -4.202 0.735 0.287 -12.5 -0.540 0.11584 0.018 1.000 0.002 1.000 0.003 -4.663 0.553 0.284 -12.0 -0.532 0.10393 0.016 1.000 0.002 1.000 0.003 -5.115 0.475 0.280 -11.5 -0.520 0.09506 0.013 1.000 0.002 1.000 0.003 -5.466 0.423 0.276 -11.0 -0.505 0.08671 0.011 1.000 0.002 1.000 0.003 -5.822 0.393 0.272 -10.5 -0.487 0.07948 0.009 1.000 0.002 1.000 0.003 -6.127 0.371 0.268 -10.0 -0.466 0.07324 0.006 1.000 0.002 1.000 0.004 -6.365 0.356 0.264 -9.5 -0.443 0.06628 0.004 1.000 0.002 1.000 0.004 -6.679 0.346 0.259 -9.0 -0.417 0.06218 0.002 1.000 0.002 1.000 0.004 -6.709 0.336 0.254 -8.5 -0.388 0.05716 -0.001 1.000 0.003 1.000 0.005 -6.785 0.328 0.249 -8.0 -0.357 0.05152 -0.003 1.000 0.003 1.000 0.006 -6.935 0.323 0.242 -7.5 -0.324 0.04758 -0.005 0.987 0.004 1.000 0.008 -6.804 0.319 0.234 -7.0 -0.289 0.04447 -0.008 0.983 0.006 1.000 0.010 -6.507 0.320 0.224 -6.5 -0.255 0.04063 -0.010 0.979 0.007 1.000 0.010 -6.276 0.317 0.211 -6.0 -0.217 0.03738 -0.012 0.975 0.008 1.000 0.012 -5.815 0.313 0.193 -5.5 -0.179 0.03447 -0.015 0.969 0.009 1.000 0.014 -5.200 0.306 0.167 -5.0 -0.135 0.03249 -0.017 0.965 0.011 1.000 0.027 -4.161 0.294 0.124 -4.5 -0.089 0.03037 -0.019 0.960 0.013 1.000 0.071 -2.917 0.065 0.038 -4.0 -0.258 0.02322 -0.040 0.954 0.025 1.000 0.999 -11.133 0.060 0.096 -3.5 -0.201 0.02341 -0.040 0.933 0.035 1.000 0.999 -8.577 0.255 0.050 -3.0 -0.143 0.02426 -0.040 0.863 0.044 1.000 0.999 -5.886 0.255 -0.032 -2.5 -0.085 0.02504 -0.041 0.799 0.071 1.000 0.999 -3.381 0.255 -0.230 -2.0 -0.026 0.02212 -0.041 0.730 0.476 1.000 0.999 -1.192 0.255 -1.301 -1.5 0.032 0.02147 -0.041 0.682 0.581 1.000 0.999 1.491 0.255 1.537 -1.0 0.090 0.02131 -0.041 0.633 0.630 1.000 0.999 4.242 0.255 0.709 -0.5 0.149 0.02153 -0.042 0.586 0.664 1.000 0.999 6.911 0.255 0.531 0.0 0.207 0.02223 -0.042 0.536 0.689 1.000 0.999 9.320 0.255 0.453 0.5 0.265 0.02255 -0.042 0.476 0.715 1.000 0.999 11.772 0.255 0.410 1.0 0.324 0.02295 -0.043 0.430 0.742 1.000 0.999 14.109 0.255 0.382 1.5 0.382 0.02337 -0.043 0.377 0.773 1.000 0.999 16.346 0.255 0.363 2.0 0.440 0.02346 -0.043 0.331 0.811 1.000 0.999 18.762 0.255 0.348 2.5 0.498 0.02359 -0.044 0.283 0.856 1.000 0.998 21.120 0.255 0.338 3.0 0.556 0.02353 -0.044 0.238 0.904 1.000 0.998 23.636 0.256 0.329 3.5 0.614 0.02279 -0.044 0.196 0.998 1.000 0.998 26.933 0.256 0.322 4.0 0.671 0.02340 -0.045 0.157 0.998 1.000 0.998 28.692 0.256 0.316 4.5 0.729 0.02342 -0.045 0.125 0.998 1.000 0.998 31.112 0.256 0.312 5.0 0.785 0.02335 -0.045 0.097 0.998 1.000 0.998 33.639 0.256 0.308 5.5 0.842 0.02345 -0.046 0.073 0.998 1.000 0.998 35.904 0.256 0.304 6.0 0.897 0.02333 -0.046 0.061 0.998 1.000 0.998 38.446 0.270 0.301 6.5 0.943 0.02235 -0.048 0.045 0.998 0.984 0.998 42.173 0.306 0.300 7.0 0.979 0.02315 -0.051 0.028 0.998 0.956 0.999 42.305 0.499 0.302 7.5 0.986 0.02490 -0.058 0.015 0.998 0.874 0.998 39.577 -0.421 0.309 8.0 0.949 0.02896 -0.071 0.007 0.998 0.720 0.999 32.761 0.129 0.325 8.5 0.748 0.05452 -0.087 0.006 0.998 0.072 0.999 13.723 0.131 0.366 9.0 0.810 0.05521 -0.088 0.005 0.998 0.014 0.998 14.662 0.281 0.358 9.5 0.846 0.05809 -0.090 0.004 0.998 0.007 0.998 14.557 0.325 0.356 10.0 0.873 0.06289 -0.092 0.004 0.998 0.006 0.998 13.877 0.346 0.356 10.5 0.897 0.06743 -0.095 0.003 0.998 0.006 0.998 13.308 0.357 0.356 11.0 0.919 0.07413 -0.097 0.003 0.998 0.005 0.998 12.401 0.370 0.356 11.5 0.939 0.08050 -0.100 0.003 0.998 0.005 0.999 11.664 0.386 0.356 12.0 0.956 0.08601 -0.102 0.003 0.998 0.005 0.998 11.116 0.411 0.357 12.5 0.970 0.09338 -0.105 0.003 0.998 0.004 0.998 10.386 0.447 0.358 13.0 0.981 0.10021 -0.107 0.003 0.998 0.004 0.998 9.793 0.564 0.359 13.5 0.986 0.10892 -0.110 0.003 0.998 0.004 0.998 9.050 1.888 0.361 14.0 0.984 0.11928 -0.112 0.002 0.998 0.004 0.998 8.253 -0.657 0.364 14.5 0.980 0.12841 -0.115 0.002 0.998 0.003 0.998 7.634 -0.141 0.367 15.0 0.972 0.14095 -0.117 0.002 0.998 0.003 0.999 6.894 -0.042 0.371 Name = SD7003-085-88 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 -0.543 0.16485 0.030 1.000 0.002 1.000 0.003 -3.295 -0.243 0.304 -14.5 -0.548 0.16296 0.027 1.000 0.002 1.000 0.003 -3.362 -0.423 0.300 -14.0 -0.550 0.14622 0.025 1.000 0.002 1.000 0.003 -3.761 -2.653 0.295 -13.5 -0.549 0.13262 0.023 1.000 0.001 1.000 0.003 -4.143 1.614 0.291 -13.0 -0.547 0.11956 0.020 1.000 0.001 1.000 0.003 -4.572 0.734 0.287 -12.5 -0.540 0.10683 0.018 1.000 0.002 1.000 0.003 -5.054 0.552 0.284 -12.0 -0.531 0.09662 0.016 1.000 0.002 1.000 0.003 -5.500 0.475 0.280 -11.5 -0.519 0.08798 0.013 1.000 0.002 1.000 0.003 -5.903 0.423 0.276 -11.0 -0.505 0.08039 0.011 1.000 0.002 1.000 0.003 -6.277 0.393 0.272 -10.5 -0.487 0.07367 0.009 1.000 0.002 1.000 0.003 -6.608 0.371 0.268 -10.0 -0.466 0.06775 0.007 1.000 0.002 1.000 0.004 -6.877 0.355 0.264 -9.5 -0.442 0.06218 0.004 1.000 0.002 1.000 0.004 -7.111 0.346 0.259 -9.0 -0.417 0.05810 0.002 1.000 0.002 1.000 0.004 -7.171 0.336 0.254 -8.5 -0.387 0.05350 -0.001 1.000 0.003 1.000 0.006 -7.240 0.327 0.249 -8.0 -0.356 0.04958 -0.003 1.000 0.003 1.000 0.007 -7.185 0.323 0.242 -7.5 -0.323 0.04490 -0.005 0.987 0.004 1.000 0.009 -7.198 0.320 0.234 -7.0 -0.289 0.04213 -0.008 0.983 0.006 1.000 0.011 -6.855 0.320 0.224 -6.5 -0.254 0.03859 -0.010 0.979 0.007 1.000 0.011 -6.591 0.317 0.211 -6.0 -0.217 0.03543 -0.012 0.975 0.008 1.000 0.013 -6.118 0.309 0.193 -5.5 -0.176 0.03322 -0.015 0.969 0.009 1.000 0.020 -5.294 0.300 0.167 -5.0 -0.130 0.03128 -0.017 0.965 0.011 1.000 0.042 -4.171 0.072 0.122 -4.5 -0.316 0.02215 -0.040 0.960 0.013 1.000 0.999 -14.262 0.070 0.125 -4.0 -0.258 0.02210 -0.040 0.954 0.025 1.000 0.999 -11.698 0.255 0.096 -3.5 -0.201 0.02222 -0.040 0.933 0.035 1.000 0.999 -9.036 0.255 0.050 -3.0 -0.143 0.02334 -0.040 0.863 0.044 1.000 0.999 -6.118 0.255 -0.032 -2.5 -0.085 0.02412 -0.041 0.799 0.071 1.000 0.999 -3.510 0.255 -0.230 -2.0 -0.026 0.02076 -0.041 0.730 0.476 1.000 0.999 -1.270 0.255 -1.301 -1.5 0.032 0.02008 -0.041 0.682 0.581 1.000 0.999 1.594 0.255 1.537 -1.0 0.090 0.02012 -0.041 0.633 0.630 1.000 0.999 4.493 0.255 0.709 -0.5 0.149 0.02036 -0.042 0.586 0.664 1.000 0.999 7.307 0.255 0.531 0.0 0.207 0.02067 -0.042 0.536 0.689 1.000 0.999 10.020 0.255 0.453 0.5 0.265 0.02160 -0.042 0.476 0.715 1.000 0.999 12.289 0.255 0.410 1.0 0.324 0.02149 -0.043 0.430 0.742 1.000 0.999 15.069 0.255 0.382 1.5 0.382 0.02195 -0.043 0.377 0.773 1.000 0.999 17.401 0.255 0.363 2.0 0.440 0.02209 -0.043 0.331 0.811 1.000 0.999 19.922 0.255 0.348 2.5 0.498 0.02210 -0.044 0.283 0.856 1.000 0.998 22.544 0.255 0.338 3.0 0.556 0.02213 -0.044 0.238 0.904 1.000 0.998 25.132 0.256 0.329 3.5 0.614 0.02143 -0.044 0.196 0.998 1.000 0.998 28.640 0.256 0.322 4.0 0.671 0.02174 -0.045 0.157 0.998 1.000 0.998 30.890 0.256 0.316 4.5 0.729 0.02243 -0.045 0.125 0.998 1.000 0.998 32.489 0.256 0.312 5.0 0.785 0.02239 -0.045 0.097 0.998 1.000 0.998 35.087 0.256 0.308 5.5 0.842 0.02248 -0.046 0.073 0.998 1.000 0.998 37.451 0.256 0.304 6.0 0.897 0.02245 -0.046 0.061 0.998 1.000 0.998 39.949 0.256 0.301 6.5 0.951 0.02197 -0.046 0.045 0.998 1.000 0.998 43.286 0.277 0.299 7.0 0.992 0.02132 -0.049 0.028 0.998 0.979 0.999 46.542 0.324 0.299 7.5 1.026 0.02245 -0.052 0.015 0.998 0.949 0.998 45.708 0.601 0.300 8.0 1.026 0.02443 -0.060 0.007 0.998 0.862 0.999 42.005 -0.025 0.309 8.5 0.921 0.03264 -0.081 0.006 0.998 0.588 0.999 28.212 0.129 0.338 9.0 0.796 0.05417 -0.088 0.005 0.998 0.028 0.998 14.702 0.134 0.361 9.5 0.840 0.05627 -0.090 0.004 0.998 0.011 0.998 14.932 0.307 0.357 10.0 0.872 0.05952 -0.092 0.004 0.998 0.007 0.998 14.647 0.336 0.356 10.5 0.896 0.06388 -0.095 0.003 0.998 0.006 0.998 14.034 0.356 0.356 11.0 0.919 0.06905 -0.097 0.003 0.998 0.006 0.998 13.307 0.369 0.356 11.5 0.938 0.07496 -0.100 0.003 0.998 0.005 0.999 12.519 0.388 0.356 12.0 0.955 0.08225 -0.102 0.003 0.998 0.005 0.998 11.613 0.411 0.357 12.5 0.969 0.08725 -0.105 0.003 0.998 0.005 0.998 11.112 0.443 0.358 13.0 0.981 0.09349 -0.107 0.003 0.998 0.004 0.998 10.493 0.563 0.359 13.5 0.985 0.10225 -0.110 0.003 0.998 0.004 0.998 9.636 1.871 0.362 14.0 0.984 0.11152 -0.112 0.002 0.998 0.004 0.998 8.824 -0.662 0.364 14.5 0.980 0.12101 -0.115 0.002 0.998 0.004 0.998 8.098 -0.142 0.367 15.0 0.971 0.13234 -0.117 0.002 0.998 0.004 0.999 7.340 -0.043 0.371