Name = NASA/LANGLEY MS(1)-0313 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 -0.607 0.17195 0.000 0.935 0.004 1.000 0.006 -3.531 0.400 0.251 -14.5 -0.587 0.15304 -0.003 0.915 0.005 1.000 0.006 -3.835 0.395 0.246 -14.0 -0.565 0.14530 -0.006 0.895 0.005 1.000 0.007 -3.888 0.388 0.240 -13.5 -0.542 0.14370 -0.009 0.867 0.004 1.000 0.006 -3.770 0.377 0.234 -13.0 -0.516 0.12483 -0.012 0.856 0.005 1.000 0.007 -4.131 0.366 0.227 -12.5 -0.488 0.11657 -0.015 0.847 0.005 1.000 0.008 -4.186 0.359 0.219 -12.0 -0.458 0.11766 -0.018 0.839 0.006 1.000 0.008 -3.896 0.354 0.210 -11.5 -0.427 0.10334 -0.021 0.831 0.006 1.000 0.008 -4.135 0.350 0.200 -11.0 -0.395 0.09909 -0.024 0.825 0.006 1.000 0.008 -3.989 0.346 0.188 -10.5 -0.361 0.09224 -0.028 0.814 0.006 1.000 0.009 -3.919 0.342 0.173 -10.0 -0.326 0.08412 -0.031 0.806 0.007 1.000 0.009 -3.880 0.339 0.155 -9.5 -0.290 0.07884 -0.034 0.797 0.008 1.000 0.010 -3.680 0.336 0.133 -9.0 -0.252 0.07254 -0.037 0.789 0.008 1.000 0.010 -3.479 0.334 0.103 -8.5 -0.214 0.07066 -0.040 0.781 0.008 1.000 0.011 -3.026 0.332 0.061 -8.0 -0.174 0.06845 -0.044 0.772 0.009 1.000 0.012 -2.548 0.330 0.000 -7.5 -0.134 0.06267 -0.047 0.764 0.010 1.000 0.013 -2.143 0.328 -0.098 -7.0 -0.093 0.05886 -0.050 0.756 0.011 1.000 0.016 -1.579 0.326 -0.288 -6.5 -0.051 0.05542 -0.053 0.747 0.013 0.947 0.019 -0.920 0.325 -0.792 -6.0 -0.008 0.05224 -0.056 0.740 0.016 0.933 0.022 -0.153 0.218 -6.806 -5.5 -0.253 0.04992 -0.060 0.733 0.019 0.920 0.026 -5.067 0.214 0.015 -5.0 -0.185 0.04757 -0.063 0.728 0.021 0.897 0.033 -3.899 0.296 -0.088 -4.5 -0.119 0.04582 -0.066 0.720 0.025 0.885 0.050 -2.589 0.371 -0.304 -4.0 -0.050 0.03359 -0.079 0.712 0.048 0.875 0.823 -1.495 0.331 -1.325 -3.5 0.012 0.03631 -0.076 0.705 0.533 0.863 0.658 0.320 0.250 6.821 -3.0 0.074 0.03589 -0.079 0.700 0.547 0.851 0.661 2.054 0.296 1.323 -2.5 0.135 0.03549 -0.082 0.693 0.558 0.843 0.665 3.818 0.296 0.855 -2.0 0.197 0.03504 -0.085 0.687 0.567 0.836 0.669 5.620 0.296 0.681 -1.5 0.258 0.03490 -0.088 0.682 0.577 0.826 0.673 7.392 0.296 0.590 -1.0 0.319 0.03458 -0.090 0.676 0.584 0.814 0.678 9.214 0.296 0.534 -0.5 0.379 0.03451 -0.093 0.670 0.590 0.807 0.684 10.977 0.466 0.496 0.0 0.344 0.03435 -0.096 0.663 0.597 0.799 0.688 10.007 0.533 0.529 0.5 0.396 0.03480 -0.098 0.657 0.603 0.789 0.695 11.390 0.294 0.497 1.0 0.448 0.03522 -0.100 0.650 0.609 0.780 0.699 12.731 0.295 0.474 1.5 0.501 0.03593 -0.103 0.642 0.613 0.772 0.706 13.933 0.296 0.455 2.0 0.553 0.03656 -0.105 0.633 0.618 0.766 0.712 15.133 0.243 0.440 2.5 0.742 0.03552 -0.101 0.101 0.624 1.000 0.718 20.891 0.238 0.386 3.0 0.802 0.03300 -0.102 0.092 0.631 1.000 0.723 24.313 0.267 0.377 3.5 0.862 0.03416 -0.103 0.083 0.635 1.000 0.731 25.244 0.323 0.370 4.0 0.878 0.03818 -0.108 0.074 0.638 0.931 0.740 22.991 0.516 0.373 4.5 0.896 0.03976 -0.112 0.069 0.644 0.870 0.744 22.538 0.115 0.375 5.0 0.713 0.05741 -0.130 0.066 0.650 0.110 0.753 12.414 0.100 0.432 5.5 0.757 0.06026 -0.133 0.062 0.656 0.096 0.758 12.554 0.324 0.426 6.0 0.799 0.06367 -0.136 0.059 0.658 0.088 0.769 12.552 0.325 0.421 6.5 0.842 0.06702 -0.140 0.057 0.664 0.080 0.778 12.556 0.327 0.416 7.0 0.882 0.07046 -0.143 0.055 0.669 0.075 0.786 12.517 0.330 0.412 7.5 0.922 0.07456 -0.146 0.054 0.675 0.071 0.794 12.368 0.331 0.408 8.0 0.961 0.07923 -0.149 0.052 0.681 0.069 0.806 12.134 0.333 0.405 8.5 1.000 0.08293 -0.152 0.049 0.686 0.066 0.819 12.059 0.335 0.402 9.0 1.037 0.08810 -0.156 0.046 0.692 0.064 0.836 11.772 0.337 0.400 9.5 1.073 0.09340 -0.159 0.045 0.700 0.061 0.853 11.493 0.339 0.398 10.0 1.108 0.09896 -0.162 0.043 0.706 0.058 0.977 11.197 0.343 0.396 10.5 1.141 0.10543 -0.165 0.040 0.714 0.056 0.977 10.822 0.347 0.395 11.0 1.173 0.11082 -0.168 0.039 0.722 0.054 0.977 10.582 0.354 0.393 11.5 1.202 0.11688 -0.171 0.024 0.731 0.056 0.977 10.283 0.357 0.393 12.0 1.231 0.11976 -0.174 0.022 0.740 0.051 0.982 10.278 0.360 0.392 12.5 1.256 0.12987 -0.177 0.018 0.745 0.047 0.982 9.672 0.374 0.391 13.0 1.279 0.13421 -0.180 0.016 0.755 0.044 0.982 9.531 0.372 0.391 13.5 1.303 0.14334 -0.183 0.013 0.765 0.035 0.983 9.087 0.365 0.391 14.0 1.325 0.14768 -0.186 0.011 0.775 0.026 0.983 8.973 0.391 0.390 14.5 1.341 0.15955 -0.189 0.009 0.785 0.023 0.983 8.407 0.442 0.391 15.0 1.355 0.16746 -0.191 0.006 0.795 0.020 0.983 8.091 0.461 0.391 Name = NASA/LANGLEY MS(1)-0313 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 -0.607 0.13837 0.000 0.935 0.004 1.000 0.006 -4.385 0.400 0.251 -14.5 -0.587 0.12700 -0.003 0.915 0.005 1.000 0.007 -4.618 0.395 0.246 -14.0 -0.565 0.11880 -0.006 0.895 0.005 1.000 0.007 -4.752 0.388 0.240 -13.5 -0.541 0.11728 -0.009 0.867 0.004 1.000 0.007 -4.616 0.377 0.234 -13.0 -0.515 0.10554 -0.012 0.856 0.005 1.000 0.008 -4.882 0.364 0.227 -12.5 -0.487 0.10425 -0.015 0.847 0.005 1.000 0.008 -4.672 0.360 0.219 -12.0 -0.458 0.09264 -0.018 0.839 0.006 1.000 0.008 -4.948 0.355 0.210 -11.5 -0.427 0.08599 -0.021 0.831 0.006 1.000 0.009 -4.965 0.349 0.200 -11.0 -0.395 0.08277 -0.024 0.825 0.006 1.000 0.009 -4.771 0.346 0.188 -10.5 -0.361 0.07790 -0.028 0.814 0.006 1.000 0.009 -4.634 0.342 0.173 -10.0 -0.326 0.07134 -0.031 0.806 0.007 1.000 0.010 -4.568 0.339 0.155 -9.5 -0.290 0.06672 -0.034 0.797 0.008 1.000 0.010 -4.341 0.336 0.133 -9.0 -0.252 0.06111 -0.037 0.789 0.008 1.000 0.011 -4.122 0.332 0.102 -8.5 -0.212 0.06261 -0.040 0.781 0.008 1.000 0.012 -3.390 0.332 0.060 -8.0 -0.174 0.05749 -0.044 0.772 0.009 1.000 0.013 -3.025 0.331 -0.001 -7.5 -0.133 0.05530 -0.047 0.764 0.010 1.000 0.015 -2.407 0.327 -0.101 -7.0 -0.092 0.05126 -0.050 0.756 0.011 1.000 0.018 -1.788 0.325 -0.295 -6.5 -0.049 0.04946 -0.053 0.747 0.013 1.000 0.021 -0.991 0.324 -0.833 -6.0 -0.006 0.04389 -0.056 0.740 0.016 1.000 0.025 -0.136 0.219 -9.188 -5.5 -0.253 0.04137 -0.059 0.733 0.019 1.000 0.034 -6.111 0.216 0.015 -5.0 -0.185 0.03934 -0.062 0.728 0.021 1.000 0.049 -4.708 0.349 -0.087 -4.5 -0.065 0.02511 -0.078 0.720 0.025 1.000 0.845 -2.577 0.356 -0.956 -4.0 -0.013 0.02429 -0.081 0.712 0.048 1.000 0.862 -0.544 0.240 -5.858 -3.5 0.012 0.02847 -0.077 0.705 0.533 1.000 0.697 0.407 0.241 6.925 -3.0 0.074 0.02788 -0.080 0.700 0.547 0.946 0.698 2.639 0.294 1.337 -2.5 0.135 0.02752 -0.083 0.693 0.558 0.932 0.702 4.916 0.294 0.861 -2.0 0.197 0.02727 -0.085 0.687 0.567 0.918 0.706 7.214 0.293 0.684 -1.5 0.258 0.02705 -0.088 0.682 0.577 0.900 0.708 9.528 0.293 0.591 -1.0 0.318 0.02680 -0.091 0.676 0.584 0.880 0.713 11.880 0.293 0.535 -0.5 0.379 0.02666 -0.093 0.670 0.590 0.868 0.719 14.209 0.348 0.496 0.0 0.371 0.02617 -0.096 0.663 0.597 0.858 0.725 14.182 0.350 0.508 0.5 0.424 0.02647 -0.098 0.657 0.603 0.847 0.732 16.018 0.288 0.481 1.0 0.477 0.02688 -0.100 0.650 0.609 0.838 0.737 17.744 0.290 0.459 1.5 0.529 0.02729 -0.102 0.642 0.613 0.829 0.745 19.403 0.290 0.443 2.0 0.584 0.02786 -0.104 0.633 0.618 0.824 0.754 20.951 0.246 0.428 2.5 0.742 0.03027 -0.101 0.101 0.624 1.000 0.760 24.516 0.241 0.386 3.0 0.802 0.02767 -0.102 0.092 0.631 1.000 0.765 28.997 0.267 0.377 3.5 0.862 0.02837 -0.103 0.083 0.635 1.000 0.775 30.398 0.267 0.370 4.0 0.922 0.02916 -0.104 0.074 0.638 1.000 0.787 31.619 0.267 0.363 4.5 0.982 0.03008 -0.105 0.069 0.644 1.000 0.792 32.637 0.313 0.357 5.0 1.006 0.03357 -0.109 0.066 0.650 0.949 0.800 29.973 0.370 0.359 5.5 1.044 0.03473 -0.113 0.062 0.656 0.920 0.811 30.063 0.540 0.358 6.0 1.042 0.03691 -0.120 0.059 0.658 0.837 0.833 28.219 0.119 0.365 6.5 0.836 0.05846 -0.140 0.057 0.664 0.104 0.850 14.304 0.107 0.417 7.0 0.878 0.06154 -0.143 0.055 0.669 0.095 0.894 14.260 0.326 0.413 7.5 0.919 0.06444 -0.146 0.054 0.675 0.084 0.977 14.261 0.327 0.409 8.0 0.959 0.06804 -0.149 0.052 0.681 0.076 0.977 14.091 0.332 0.406 8.5 0.997 0.07208 -0.153 0.049 0.686 0.074 0.977 13.830 0.335 0.403 9.0 1.035 0.07528 -0.156 0.046 0.692 0.071 0.978 13.742 0.336 0.401 9.5 1.071 0.07989 -0.159 0.045 0.700 0.069 0.978 13.405 0.338 0.398 10.0 1.106 0.08371 -0.162 0.043 0.706 0.065 0.978 13.213 0.342 0.397 10.5 1.139 0.08800 -0.165 0.040 0.714 0.063 0.978 12.944 0.347 0.395 11.0 1.171 0.09385 -0.168 0.039 0.722 0.060 0.978 12.477 0.363 0.394 11.5 1.198 0.09857 -0.172 0.024 0.731 0.070 0.978 12.157 0.368 0.393 12.0 1.227 0.10211 -0.175 0.022 0.740 0.067 0.983 12.020 0.364 0.393 12.5 1.252 0.10885 -0.178 0.018 0.745 0.064 0.983 11.502 0.381 0.392 13.0 1.274 0.11390 -0.181 0.016 0.755 0.061 0.983 11.187 0.389 0.392 13.5 1.294 0.12046 -0.184 0.013 0.765 0.055 0.983 10.745 0.407 0.392 14.0 1.311 0.12636 -0.187 0.011 0.775 0.051 0.983 10.377 0.435 0.393 14.5 1.326 0.13752 -0.190 0.009 0.785 0.047 0.983 9.642 0.467 0.393 15.0 1.338 0.14284 -0.193 0.006 0.795 0.044 0.983 9.366 0.490 0.394 Name = NASA/LANGLEY MS(1)-0313 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 -0.606 0.13360 0.001 0.935 0.004 1.000 0.007 -4.537 0.404 0.251 -14.5 -0.586 0.11553 -0.003 0.915 0.005 1.000 0.007 -5.074 0.397 0.246 -14.0 -0.564 0.10739 -0.006 0.895 0.005 1.000 0.008 -5.253 0.388 0.240 -13.5 -0.541 0.10531 -0.009 0.867 0.004 1.000 0.007 -5.137 0.377 0.234 -13.0 -0.515 0.09706 -0.012 0.856 0.005 1.000 0.008 -5.304 0.364 0.227 -12.5 -0.487 0.09405 -0.015 0.847 0.005 1.000 0.009 -5.175 0.360 0.219 -12.0 -0.458 0.08541 -0.018 0.839 0.006 1.000 0.008 -5.362 0.355 0.210 -11.5 -0.427 0.07698 -0.021 0.831 0.006 1.000 0.009 -5.541 0.349 0.200 -11.0 -0.394 0.07423 -0.024 0.825 0.006 1.000 0.009 -5.314 0.346 0.188 -10.5 -0.361 0.07148 -0.028 0.814 0.006 1.000 0.010 -5.044 0.342 0.173 -10.0 -0.325 0.06495 -0.031 0.806 0.007 1.000 0.010 -5.010 0.338 0.155 -9.5 -0.289 0.06407 -0.034 0.797 0.008 1.000 0.011 -4.505 0.335 0.132 -9.0 -0.251 0.05797 -0.037 0.789 0.008 1.000 0.012 -4.328 0.334 0.102 -8.5 -0.212 0.05621 -0.040 0.781 0.008 1.000 0.012 -3.776 0.331 0.060 -8.0 -0.173 0.05472 -0.044 0.772 0.009 1.000 0.014 -3.156 0.329 -0.002 -7.5 -0.132 0.05149 -0.047 0.764 0.010 1.000 0.017 -2.561 0.326 -0.104 -7.0 -0.090 0.04834 -0.050 0.756 0.011 1.000 0.021 -1.857 0.325 -0.305 -6.5 -0.047 0.04639 -0.053 0.747 0.013 1.000 0.024 -1.015 0.322 -0.876 -6.0 -0.003 0.04148 -0.056 0.740 0.016 1.000 0.032 -0.068 0.089 -19.650 -5.5 -0.173 0.02393 -0.073 0.733 0.019 1.000 0.831 -7.218 0.084 -0.174 -5.0 -0.126 0.02320 -0.076 0.728 0.021 1.000 0.853 -5.412 0.316 -0.359 -4.5 -0.077 0.02230 -0.080 0.720 0.025 1.000 0.877 -3.457 0.310 -0.782 -4.0 -0.026 0.02185 -0.082 0.712 0.048 1.000 0.901 -1.201 0.235 -2.891 -3.5 0.012 0.02419 -0.078 0.705 0.533 1.000 0.732 0.478 0.233 7.024 -3.0 0.073 0.02388 -0.081 0.700 0.547 1.000 0.731 3.076 0.291 1.349 -2.5 0.135 0.02347 -0.083 0.693 0.558 1.000 0.735 5.755 0.292 0.867 -2.0 0.196 0.02384 -0.086 0.687 0.567 1.000 0.738 8.240 0.291 0.687 -1.5 0.258 0.02385 -0.088 0.682 0.577 1.000 0.740 10.799 0.291 0.593 -1.0 0.318 0.02311 -0.091 0.676 0.584 1.000 0.747 13.768 0.291 0.536 -0.5 0.379 0.02313 -0.093 0.670 0.590 0.941 0.753 16.366 0.307 0.497 0.0 0.404 0.02243 -0.096 0.663 0.597 0.926 0.759 17.993 0.303 0.487 0.5 0.455 0.02266 -0.097 0.657 0.603 0.911 0.766 20.086 0.283 0.464 1.0 0.506 0.02298 -0.099 0.650 0.609 0.895 0.773 22.012 0.287 0.446 1.5 0.557 0.02334 -0.101 0.642 0.613 0.880 0.782 23.853 0.287 0.432 2.0 0.610 0.02377 -0.103 0.633 0.618 0.872 0.792 25.677 0.250 0.419 2.5 0.742 0.02683 -0.101 0.101 0.624 1.000 0.800 27.659 0.245 0.386 3.0 0.802 0.02551 -0.102 0.092 0.631 1.000 0.806 31.444 0.267 0.377 3.5 0.862 0.02549 -0.103 0.083 0.635 1.000 0.821 33.831 0.267 0.370 4.0 0.922 0.02637 -0.104 0.074 0.638 1.000 0.840 34.970 0.267 0.363 4.5 0.982 0.02749 -0.105 0.069 0.644 1.000 0.856 35.704 0.267 0.357 5.0 1.041 0.02773 -0.106 0.066 0.650 1.000 0.886 37.543 0.267 0.352 5.5 1.100 0.03116 -0.107 0.062 0.656 1.000 0.977 35.300 0.337 0.348 6.0 1.116 0.03261 -0.113 0.059 0.658 0.940 0.977 34.218 0.455 0.351 6.5 1.147 0.03407 -0.117 0.057 0.664 0.905 0.977 33.664 0.625 0.352 7.0 1.146 0.03616 -0.124 0.055 0.669 0.830 0.977 31.692 0.121 0.358 7.5 0.915 0.06012 -0.147 0.054 0.675 0.110 0.978 15.218 0.115 0.410 8.0 0.955 0.06343 -0.150 0.052 0.681 0.094 0.978 15.063 0.328 0.407 8.5 0.994 0.06652 -0.153 0.049 0.686 0.088 0.978 14.949 0.333 0.404 9.0 1.032 0.07018 -0.156 0.046 0.692 0.085 0.978 14.704 0.334 0.401 9.5 1.069 0.07380 -0.159 0.045 0.700 0.077 0.978 14.480 0.336 0.399 10.0 1.104 0.07756 -0.162 0.043 0.706 0.072 0.978 14.232 0.342 0.397 10.5 1.137 0.08111 -0.166 0.040 0.714 0.070 0.979 14.018 0.346 0.396 11.0 1.169 0.08574 -0.169 0.039 0.722 0.067 0.979 13.637 0.367 0.394 11.5 1.197 0.09020 -0.173 0.024 0.731 0.087 0.979 13.268 0.374 0.394 12.0 1.225 0.09360 -0.176 0.022 0.740 0.082 0.983 13.093 0.365 0.393 12.5 1.250 0.09940 -0.179 0.018 0.745 0.078 0.983 12.574 0.383 0.393 13.0 1.272 0.10518 -0.182 0.016 0.755 0.075 0.983 12.091 0.394 0.393 13.5 1.292 0.11222 -0.185 0.013 0.765 0.070 0.983 11.511 0.411 0.393 14.0 1.309 0.11740 -0.188 0.011 0.775 0.068 0.984 11.149 0.440 0.393 14.5 1.323 0.12262 -0.191 0.009 0.785 0.064 0.984 10.792 0.486 0.394 15.0 1.334 0.13372 -0.194 0.006 0.795 0.063 0.984 9.979 0.525 0.395 Name = NASA/LANGLEY MS(1)-0313 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 -0.606 0.12248 0.001 0.935 0.004 1.000 0.007 -4.946 0.404 0.251 -14.5 -0.586 0.10885 -0.003 0.915 0.005 1.000 0.008 -5.382 0.397 0.246 -14.0 -0.564 0.10027 -0.006 0.895 0.005 1.000 0.008 -5.623 0.388 0.240 -13.5 -0.541 0.09597 -0.009 0.867 0.004 1.000 0.008 -5.633 0.376 0.234 -13.0 -0.514 0.09196 -0.012 0.856 0.005 1.000 0.008 -5.594 0.364 0.227 -12.5 -0.486 0.08790 -0.015 0.847 0.005 1.000 0.009 -5.532 0.360 0.219 -12.0 -0.458 0.08104 -0.018 0.839 0.006 1.000 0.009 -5.646 0.355 0.210 -11.5 -0.426 0.07411 -0.021 0.831 0.006 1.000 0.010 -5.749 0.349 0.200 -11.0 -0.394 0.07168 -0.024 0.825 0.006 1.000 0.010 -5.497 0.346 0.188 -10.5 -0.360 0.06761 -0.028 0.814 0.006 1.000 0.010 -5.326 0.341 0.173 -10.0 -0.324 0.06335 -0.031 0.806 0.007 1.000 0.011 -5.121 0.339 0.155 -9.5 -0.289 0.05949 -0.034 0.797 0.008 1.000 0.011 -4.852 0.335 0.132 -9.0 -0.250 0.05620 -0.037 0.789 0.008 1.000 0.012 -4.446 0.332 0.101 -8.5 -0.212 0.05410 -0.040 0.781 0.008 1.000 0.013 -3.912 0.331 0.059 -8.0 -0.172 0.05242 -0.043 0.772 0.009 1.000 0.016 -3.272 0.328 -0.003 -7.5 -0.131 0.04917 -0.047 0.764 0.010 1.000 0.019 -2.657 0.325 -0.107 -7.0 -0.088 0.04684 -0.050 0.756 0.011 1.000 0.023 -1.876 0.323 -0.316 -6.5 -0.045 0.04455 -0.053 0.747 0.013 1.000 0.029 -1.004 0.224 -0.933 -6.0 -0.320 0.04017 -0.056 0.740 0.016 1.000 0.044 -7.977 0.093 0.076 -5.5 -0.183 0.02225 -0.075 0.733 0.019 1.000 0.854 -8.242 0.369 -0.157 -5.0 -0.136 0.02145 -0.078 0.728 0.021 1.000 0.879 -6.336 0.319 -0.323 -4.5 -0.087 0.02086 -0.081 0.720 0.025 1.000 0.910 -4.191 0.334 -0.679 -4.0 -0.038 0.01911 -0.086 0.712 0.048 1.000 0.977 -1.999 0.229 -2.003 -3.5 0.012 0.02167 -0.079 0.705 0.533 1.000 0.762 0.532 0.209 7.115 -3.0 0.073 0.02135 -0.082 0.700 0.547 1.000 0.761 3.436 0.289 1.361 -2.5 0.135 0.02153 -0.084 0.693 0.558 1.000 0.764 6.266 0.290 0.872 -2.0 0.196 0.02114 -0.086 0.687 0.567 1.000 0.768 9.283 0.289 0.690 -1.5 0.257 0.02102 -0.089 0.682 0.577 1.000 0.770 12.244 0.289 0.595 -1.0 0.318 0.02094 -0.091 0.676 0.584 1.000 0.777 15.191 0.289 0.537 -0.5 0.379 0.02078 -0.094 0.670 0.590 1.000 0.784 18.216 0.288 0.497 0.0 0.439 0.02019 -0.096 0.663 0.597 1.000 0.791 21.728 0.278 0.468 0.5 0.500 0.02036 -0.097 0.657 0.603 1.000 0.800 24.541 0.267 0.444 1.0 0.560 0.02068 -0.098 0.650 0.609 1.000 0.809 27.100 0.288 0.425 1.5 0.587 0.02095 -0.100 0.642 0.613 0.937 0.820 28.025 0.299 0.421 2.0 0.640 0.02126 -0.102 0.633 0.618 0.926 0.836 30.123 0.256 0.409 2.5 0.742 0.02538 -0.101 0.101 0.624 1.000 0.849 29.233 0.252 0.386 3.0 0.802 0.02346 -0.102 0.092 0.631 1.000 0.862 34.199 0.267 0.377 3.5 0.862 0.02433 -0.103 0.083 0.635 1.000 0.908 35.433 0.267 0.370 4.0 0.922 0.02455 -0.104 0.074 0.638 1.000 0.977 37.551 0.267 0.363 4.5 0.982 0.02559 -0.105 0.069 0.644 1.000 0.977 38.353 0.267 0.357 5.0 1.041 0.02582 -0.106 0.066 0.650 1.000 0.977 40.320 0.267 0.352 5.5 1.100 0.03007 -0.107 0.062 0.656 1.000 0.977 36.574 0.267 0.348 6.0 1.159 0.03086 -0.108 0.059 0.658 1.000 0.978 37.539 0.339 0.343 6.5 1.175 0.03142 -0.114 0.057 0.664 0.943 0.978 37.404 0.419 0.347 7.0 1.213 0.03263 -0.117 0.055 0.669 0.918 0.978 37.162 0.423 0.347 7.5 1.228 0.03425 -0.123 0.054 0.675 0.867 0.978 35.858 0.122 0.350 8.0 0.953 0.06009 -0.151 0.052 0.681 0.142 0.978 15.862 0.121 0.408 8.5 0.992 0.06348 -0.154 0.049 0.686 0.116 0.979 15.625 0.327 0.405 9.0 1.030 0.06655 -0.157 0.046 0.692 0.103 0.979 15.474 0.331 0.402 9.5 1.067 0.06990 -0.160 0.045 0.700 0.092 0.979 15.261 0.334 0.400 10.0 1.102 0.07353 -0.163 0.043 0.706 0.084 0.979 14.990 0.340 0.398 10.5 1.135 0.07721 -0.166 0.040 0.714 0.080 0.979 14.704 0.345 0.396 11.0 1.167 0.08208 -0.169 0.039 0.722 0.074 0.979 14.222 0.369 0.395 11.5 1.197 0.08588 -0.173 0.024 0.731 0.106 0.979 13.935 0.376 0.395 12.0 1.225 0.08949 -0.176 0.022 0.740 0.099 0.984 13.691 0.365 0.394 12.5 1.250 0.09489 -0.179 0.018 0.745 0.095 0.984 13.172 0.382 0.393 13.0 1.272 0.09855 -0.182 0.016 0.755 0.091 0.984 12.909 0.394 0.393 13.5 1.292 0.10558 -0.185 0.013 0.765 0.085 0.984 12.233 0.413 0.393 14.0 1.308 0.11076 -0.188 0.011 0.775 0.080 0.984 11.811 0.445 0.394 14.5 1.322 0.11704 -0.191 0.009 0.785 0.076 0.984 11.296 0.489 0.395 15.0 1.333 0.12324 -0.194 0.006 0.795 0.074 0.984 10.819 0.519 0.396