Name = AH 83-150 Q 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 -0.353 0.41097 0.018 0.629 0.003 0.930 0.004 -0.859 4.153 0.300 -14.5 -0.352 0.40630 0.015 0.624 0.003 0.909 0.004 -0.867 2.096 0.292 -14.0 -0.350 0.36253 0.012 0.621 0.003 0.871 0.004 -0.965 1.141 0.284 -13.5 -0.346 0.32538 0.009 0.617 0.003 0.791 0.004 -1.063 0.820 0.276 -13.0 -0.340 0.28760 0.006 0.614 0.003 0.758 0.004 -1.181 0.650 0.268 -12.5 -0.331 0.25333 0.003 0.611 0.003 0.733 0.004 -1.307 0.560 0.260 -12.0 -0.321 0.22594 0.000 0.608 0.003 0.713 0.004 -1.419 0.505 0.251 -11.5 -0.308 0.19848 -0.003 0.606 0.003 0.698 0.004 -1.550 0.460 0.241 -11.0 -0.292 0.19337 -0.006 0.603 0.003 0.687 0.004 -1.509 0.431 0.230 -10.5 -0.274 0.16895 -0.009 0.600 0.003 0.679 0.004 -1.621 0.410 0.218 -10.0 -0.253 0.14648 -0.012 0.598 0.003 0.672 0.004 -1.730 0.394 0.203 -9.5 -0.230 0.13597 -0.015 0.594 0.002 0.666 0.003 -1.695 0.380 0.184 -9.0 -0.205 0.11933 -0.018 0.591 0.002 0.660 0.003 -1.718 0.369 0.161 -8.5 -0.177 0.10861 -0.021 0.587 0.002 0.656 0.003 -1.630 0.360 0.129 -8.0 -0.147 0.09424 -0.025 0.584 0.002 0.652 0.003 -1.558 0.353 0.082 -7.5 -0.115 0.08533 -0.028 0.581 0.002 0.648 0.003 -1.344 0.348 0.007 -7.0 -0.081 0.07512 -0.031 0.579 0.002 0.644 0.003 -1.076 0.344 -0.135 -6.5 -0.045 0.06609 -0.034 0.576 0.002 0.640 0.003 -0.685 0.341 -0.510 -6.0 -0.008 0.05981 -0.038 0.573 0.002 0.637 0.003 -0.141 0.211 -4.232 -5.5 -0.214 0.05277 -0.041 0.571 0.002 0.633 0.003 -4.062 0.203 0.058 -5.0 -0.152 0.04730 -0.044 0.568 0.002 0.629 0.003 -3.206 0.303 -0.043 -4.5 -0.088 0.04355 -0.048 0.566 0.002 0.626 0.003 -2.028 0.303 -0.291 -4.0 -0.025 0.03843 -0.051 0.562 0.002 0.623 0.003 -0.642 0.304 -1.825 -3.5 0.039 0.03521 -0.055 0.558 0.002 0.621 0.003 1.106 0.304 1.652 -3.0 0.102 0.03206 -0.058 0.554 0.003 0.618 0.003 3.189 0.305 0.818 -2.5 0.165 0.02951 -0.062 0.550 0.003 0.616 0.004 5.590 0.306 0.623 -2.0 0.227 0.02727 -0.065 0.547 0.004 0.613 0.006 8.323 0.307 0.536 -1.5 0.288 0.02538 -0.068 0.544 0.005 0.610 0.007 11.346 0.308 0.488 -1.0 0.348 0.02367 -0.072 0.540 0.006 0.608 0.008 14.702 0.330 0.457 -0.5 0.403 0.02506 -0.078 0.537 0.008 0.604 0.990 16.078 0.176 0.443 0.0 0.252 0.03390 -0.079 0.534 0.753 0.601 0.783 7.430 0.202 0.564 0.5 0.303 0.03457 -0.082 0.529 0.754 0.599 0.784 8.774 0.315 0.522 1.0 0.355 0.03533 -0.086 0.524 0.756 0.597 0.785 10.045 0.316 0.492 1.5 0.406 0.03614 -0.089 0.519 0.757 0.595 0.786 11.234 0.317 0.470 2.0 0.457 0.03702 -0.093 0.513 0.758 0.592 0.787 12.341 0.318 0.453 2.5 0.507 0.03797 -0.096 0.509 0.760 0.589 0.789 13.363 0.319 0.439 3.0 0.558 0.03898 -0.100 0.504 0.761 0.586 0.790 14.306 0.319 0.428 3.5 0.608 0.04004 -0.103 0.498 0.762 0.583 0.791 15.191 0.319 0.419 4.0 0.660 0.04110 -0.107 0.488 0.764 0.582 0.792 16.051 0.319 0.411 4.5 0.711 0.04225 -0.110 0.479 0.766 0.581 0.793 16.819 0.320 0.405 5.0 0.761 0.04350 -0.114 0.470 0.767 0.579 0.795 17.490 0.321 0.399 5.5 0.812 0.04476 -0.117 0.458 0.768 0.577 0.796 18.131 0.321 0.394 6.0 0.862 0.04613 -0.121 0.446 0.770 0.576 0.797 18.686 0.321 0.390 6.5 0.913 0.04756 -0.124 0.431 0.771 0.576 0.798 19.193 0.311 0.386 7.0 0.972 0.04876 -0.127 0.394 0.773 0.587 0.799 19.928 0.305 0.381 7.5 1.028 0.05040 -0.131 0.359 0.775 0.593 0.800 20.386 0.309 0.377 8.0 1.082 0.05224 -0.134 0.324 0.776 0.598 0.801 20.705 0.309 0.374 8.5 1.138 0.05419 -0.137 0.278 0.778 0.605 0.802 20.995 0.282 0.371 9.0 1.221 0.05506 -0.139 0.102 0.779 0.642 0.803 22.180 0.294 0.363 9.5 1.260 0.05819 -0.143 0.091 0.780 0.632 0.805 21.650 0.333 0.363 10.0 1.309 0.06015 -0.146 0.026 0.781 0.635 0.806 21.757 0.316 0.361 10.5 1.357 0.05999 -0.149 0.001 0.781 0.639 0.807 22.613 0.342 0.360 11.0 1.388 0.06382 -0.153 0.001 0.782 0.629 0.809 21.755 -0.158 0.360 11.5 1.318 0.07308 -0.165 0.001 0.783 0.001 0.810 18.034 -0.107 0.375 12.0 1.345 0.07908 -0.169 0.001 0.784 0.001 0.811 17.010 0.400 0.375 12.5 1.369 0.08749 -0.172 0.000 0.785 0.001 0.813 15.644 0.420 0.376 13.0 1.390 0.09623 -0.176 0.000 0.786 0.001 0.814 14.443 0.446 0.377 13.5 1.408 0.10382 -0.180 0.000 0.787 0.001 0.816 13.558 0.491 0.378 14.0 1.422 0.11501 -0.184 0.000 0.788 0.001 0.817 12.361 0.560 0.379 14.5 1.432 0.12500 -0.188 0.000 0.789 0.001 0.819 11.458 0.692 0.381 15.0 1.439 0.14009 -0.191 0.000 0.790 0.001 0.821 10.271 0.823 0.383 Name = AH 83-150 Q 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 -0.353 0.17683 0.018 0.629 0.003 0.965 0.005 -1.996 4.131 0.300 -14.5 -0.352 0.16788 0.015 0.624 0.003 0.963 0.005 -2.098 2.091 0.292 -14.0 -0.350 0.26460 0.012 0.621 0.003 0.961 0.004 -1.322 1.129 0.284 -13.5 -0.346 0.24272 0.009 0.617 0.003 0.956 0.004 -1.424 0.815 0.276 -13.0 -0.340 0.21913 0.006 0.614 0.003 0.951 0.004 -1.550 0.650 0.268 -12.5 -0.331 0.19258 0.003 0.611 0.003 0.942 0.004 -1.719 0.560 0.260 -12.0 -0.320 0.17529 0.000 0.608 0.003 0.926 0.004 -1.828 0.505 0.251 -11.5 -0.308 0.15691 -0.003 0.606 0.003 0.896 0.004 -1.960 0.462 0.241 -11.0 -0.292 0.13887 -0.006 0.603 0.003 0.835 0.004 -2.102 0.431 0.230 -10.5 -0.274 0.13399 -0.009 0.600 0.003 0.783 0.004 -2.043 0.409 0.218 -10.0 -0.253 0.11730 -0.012 0.598 0.003 0.753 0.004 -2.159 0.394 0.203 -9.5 -0.230 0.10582 -0.015 0.594 0.002 0.735 0.003 -2.177 0.380 0.184 -9.0 -0.205 0.09712 -0.018 0.591 0.002 0.718 0.003 -2.108 0.369 0.161 -8.5 -0.177 0.08621 -0.021 0.587 0.002 0.707 0.003 -2.053 0.360 0.129 -8.0 -0.147 0.07562 -0.025 0.584 0.002 0.695 0.003 -1.939 0.353 0.082 -7.5 -0.115 0.06692 -0.028 0.581 0.002 0.687 0.003 -1.714 0.348 0.007 -7.0 -0.081 0.06136 -0.031 0.579 0.002 0.679 0.003 -1.315 0.344 -0.136 -6.5 -0.045 0.05437 -0.034 0.576 0.002 0.672 0.003 -0.831 0.341 -0.512 -6.0 -0.008 0.04822 -0.038 0.573 0.002 0.665 0.003 -0.175 0.211 -4.232 -5.5 -0.214 0.04394 -0.041 0.571 0.002 0.659 0.003 -4.878 0.203 0.058 -5.0 -0.152 0.03871 -0.044 0.568 0.002 0.654 0.003 -3.918 0.303 -0.043 -4.5 -0.088 0.03555 -0.048 0.566 0.002 0.649 0.003 -2.484 0.303 -0.291 -4.0 -0.025 0.03194 -0.051 0.562 0.002 0.646 0.003 -0.772 0.304 -1.825 -3.5 0.039 0.02908 -0.055 0.558 0.002 0.644 0.003 1.339 0.304 1.652 -3.0 0.102 0.02631 -0.058 0.554 0.003 0.641 0.003 3.887 0.305 0.818 -2.5 0.165 0.02403 -0.061 0.550 0.003 0.638 0.004 6.864 0.306 0.623 -2.0 0.227 0.02199 -0.065 0.547 0.004 0.635 0.006 10.318 0.307 0.536 -1.5 0.288 0.02016 -0.068 0.544 0.005 0.632 0.007 14.285 0.308 0.488 -1.0 0.348 0.01847 -0.072 0.540 0.006 0.628 0.008 18.841 0.330 0.457 -0.5 0.403 0.02075 -0.078 0.537 0.008 0.625 0.992 19.414 0.166 0.443 0.0 0.263 0.02564 -0.079 0.534 0.753 0.621 0.786 10.240 0.197 0.551 0.5 0.315 0.02620 -0.082 0.529 0.754 0.620 0.787 12.016 0.313 0.512 1.0 0.367 0.02678 -0.086 0.524 0.756 0.618 0.788 13.701 0.313 0.483 1.5 0.419 0.02743 -0.089 0.519 0.757 0.616 0.789 15.272 0.314 0.462 2.0 0.471 0.02813 -0.092 0.513 0.758 0.614 0.791 16.727 0.315 0.446 2.5 0.522 0.02888 -0.096 0.509 0.760 0.612 0.792 18.068 0.316 0.433 3.0 0.573 0.02968 -0.099 0.504 0.761 0.609 0.793 19.296 0.317 0.423 3.5 0.624 0.03050 -0.103 0.498 0.762 0.608 0.795 20.468 0.315 0.414 4.0 0.677 0.03127 -0.106 0.488 0.764 0.609 0.796 21.663 0.314 0.406 4.5 0.730 0.03212 -0.109 0.479 0.766 0.609 0.797 22.724 0.316 0.400 5.0 0.781 0.03305 -0.113 0.470 0.767 0.608 0.798 23.644 0.316 0.394 5.5 0.834 0.03396 -0.116 0.458 0.768 0.609 0.799 24.560 0.315 0.389 6.0 0.887 0.03495 -0.120 0.446 0.770 0.609 0.801 25.363 0.315 0.385 6.5 0.940 0.03597 -0.123 0.431 0.771 0.611 0.802 26.125 0.303 0.381 7.0 1.004 0.03674 -0.126 0.394 0.773 0.626 0.803 27.316 0.296 0.375 7.5 1.063 0.03791 -0.129 0.359 0.775 0.635 0.804 28.045 0.302 0.371 8.0 1.120 0.03932 -0.132 0.324 0.776 0.642 0.805 28.479 0.302 0.368 8.5 1.178 0.04097 -0.135 0.278 0.778 0.649 0.806 28.743 0.288 0.364 9.0 1.249 0.04417 -0.137 0.102 0.779 0.672 0.807 28.280 0.302 0.359 9.5 1.290 0.04663 -0.141 0.091 0.780 0.663 0.808 27.655 0.342 0.359 10.0 1.331 0.04993 -0.144 0.026 0.781 0.658 0.810 26.660 0.338 0.358 10.5 1.372 0.05155 -0.148 0.001 0.781 0.655 0.811 26.618 0.352 0.358 11.0 1.406 0.05469 -0.152 0.001 0.782 0.647 0.813 25.707 0.376 0.358 11.5 1.436 0.05779 -0.156 0.001 0.783 0.638 0.815 24.855 -0.021 0.359 12.0 1.344 0.06905 -0.169 0.001 0.784 0.001 0.816 19.465 0.009 0.375 12.5 1.368 0.07462 -0.172 0.000 0.785 0.001 0.818 18.335 0.418 0.376 13.0 1.389 0.08148 -0.176 0.000 0.786 0.001 0.820 17.052 0.446 0.377 13.5 1.407 0.08763 -0.180 0.000 0.787 0.001 0.822 16.058 0.491 0.378 14.0 1.421 0.09622 -0.184 0.000 0.788 0.001 0.823 14.770 0.560 0.379 14.5 1.432 0.10391 -0.188 0.000 0.789 0.001 0.826 13.780 0.680 0.381 15.0 1.439 0.11214 -0.191 0.000 0.790 0.001 0.828 12.831 0.787 0.383 Name = AH 83-150 Q 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 -0.353 0.15571 0.018 0.629 0.003 0.973 0.005 -2.267 4.110 0.300 -14.5 -0.352 0.14599 0.015 0.624 0.003 0.972 0.005 -2.413 2.086 0.292 -14.0 -0.350 0.13596 0.012 0.621 0.003 0.970 0.005 -2.573 1.128 0.284 -13.5 -0.346 0.20690 0.009 0.617 0.003 0.969 0.004 -1.671 0.810 0.276 -13.0 -0.339 0.18955 0.006 0.614 0.003 0.967 0.004 -1.791 0.649 0.268 -12.5 -0.331 0.16643 0.003 0.611 0.003 0.965 0.004 -1.989 0.560 0.260 -12.0 -0.320 0.15367 0.000 0.608 0.003 0.963 0.004 -2.084 0.504 0.251 -11.5 -0.307 0.13943 -0.003 0.606 0.003 0.959 0.004 -2.204 0.462 0.241 -11.0 -0.292 0.12309 -0.006 0.603 0.003 0.953 0.004 -2.370 0.432 0.230 -10.5 -0.274 0.11149 -0.009 0.600 0.003 0.943 0.004 -2.455 0.410 0.218 -10.0 -0.253 0.10198 -0.012 0.598 0.003 0.925 0.004 -2.482 0.394 0.203 -9.5 -0.230 0.09307 -0.015 0.594 0.002 0.901 0.003 -2.474 0.380 0.184 -9.0 -0.205 0.08555 -0.018 0.591 0.002 0.865 0.003 -2.392 0.369 0.161 -8.5 -0.177 0.07680 -0.021 0.587 0.002 0.813 0.003 -2.303 0.360 0.129 -8.0 -0.147 0.06784 -0.025 0.584 0.002 0.782 0.003 -2.160 0.353 0.082 -7.5 -0.115 0.06061 -0.028 0.581 0.002 0.760 0.003 -1.891 0.349 0.007 -7.0 -0.081 0.05412 -0.031 0.579 0.002 0.739 0.003 -1.491 0.344 -0.136 -6.5 -0.045 0.04829 -0.034 0.576 0.002 0.722 0.003 -0.935 0.341 -0.512 -6.0 -0.008 0.04419 -0.038 0.573 0.002 0.709 0.003 -0.187 0.211 -4.303 -5.5 -0.214 0.03940 -0.041 0.571 0.002 0.696 0.003 -5.440 0.203 0.058 -5.0 -0.152 0.03561 -0.044 0.568 0.002 0.687 0.003 -4.259 0.303 -0.043 -4.5 -0.088 0.03209 -0.048 0.566 0.002 0.678 0.003 -2.752 0.303 -0.291 -4.0 -0.025 0.02887 -0.051 0.562 0.002 0.674 0.003 -0.854 0.304 -1.825 -3.5 0.039 0.02646 -0.055 0.558 0.002 0.671 0.003 1.472 0.304 1.652 -3.0 0.102 0.02383 -0.058 0.554 0.003 0.666 0.004 4.291 0.305 0.818 -2.5 0.165 0.02170 -0.061 0.550 0.003 0.662 0.005 7.601 0.306 0.623 -2.0 0.227 0.01972 -0.065 0.547 0.004 0.657 0.006 11.505 0.307 0.536 -1.5 0.288 0.01792 -0.068 0.544 0.005 0.654 0.007 16.071 0.308 0.488 -1.0 0.348 0.01623 -0.072 0.540 0.006 0.650 0.008 21.441 0.330 0.457 -0.5 0.403 0.01907 -0.078 0.537 0.008 0.646 0.993 21.126 0.154 0.443 0.0 0.274 0.02166 -0.079 0.534 0.753 0.641 0.788 12.645 0.190 0.539 0.5 0.326 0.02215 -0.082 0.529 0.754 0.640 0.790 14.734 0.311 0.502 1.0 0.379 0.02266 -0.086 0.524 0.756 0.638 0.791 16.731 0.311 0.476 1.5 0.431 0.02323 -0.089 0.519 0.757 0.637 0.792 18.576 0.313 0.456 2.0 0.483 0.02384 -0.092 0.513 0.758 0.635 0.794 20.275 0.314 0.440 2.5 0.535 0.02451 -0.095 0.509 0.760 0.632 0.795 21.824 0.315 0.428 3.0 0.586 0.02521 -0.099 0.504 0.761 0.629 0.796 23.238 0.315 0.419 3.5 0.638 0.02591 -0.102 0.498 0.762 0.628 0.798 24.624 0.312 0.410 4.0 0.692 0.02653 -0.105 0.488 0.764 0.630 0.799 26.095 0.311 0.402 4.5 0.746 0.02723 -0.109 0.479 0.766 0.630 0.800 27.390 0.313 0.396 5.0 0.798 0.02801 -0.112 0.470 0.767 0.630 0.801 28.496 0.312 0.390 5.5 0.852 0.02875 -0.115 0.458 0.768 0.632 0.803 29.643 0.311 0.385 6.0 0.906 0.02956 -0.119 0.446 0.770 0.634 0.804 30.643 0.311 0.381 6.5 0.961 0.03044 -0.122 0.431 0.771 0.636 0.805 31.553 0.297 0.377 7.0 1.028 0.03099 -0.124 0.394 0.773 0.654 0.806 33.164 0.292 0.371 7.5 1.088 0.03201 -0.127 0.359 0.775 0.664 0.807 33.994 0.299 0.367 8.0 1.145 0.03331 -0.130 0.324 0.776 0.670 0.808 34.391 0.301 0.364 8.5 1.203 0.03493 -0.133 0.278 0.778 0.676 0.810 34.431 0.296 0.361 9.0 1.264 0.03921 -0.136 0.102 0.779 0.687 0.811 32.235 0.312 0.357 9.5 1.305 0.04140 -0.139 0.091 0.780 0.679 0.812 31.529 0.347 0.357 10.0 1.343 0.04515 -0.143 0.026 0.781 0.671 0.814 29.751 0.352 0.357 10.5 1.381 0.04740 -0.147 0.001 0.781 0.664 0.815 29.135 0.358 0.357 11.0 1.415 0.05028 -0.151 0.001 0.782 0.656 0.817 28.143 0.372 0.357 11.5 1.447 0.05312 -0.155 0.001 0.783 0.648 0.819 27.237 0.006 0.357 12.0 1.344 0.06411 -0.169 0.001 0.784 0.001 0.821 20.958 0.032 0.375 12.5 1.368 0.06905 -0.172 0.000 0.785 0.001 0.823 19.807 0.418 0.376 13.0 1.389 0.07511 -0.176 0.000 0.786 0.001 0.825 18.493 0.446 0.377 13.5 1.407 0.08064 -0.180 0.000 0.787 0.001 0.827 17.445 0.490 0.378 14.0 1.421 0.08816 -0.184 0.000 0.788 0.001 0.829 16.115 0.560 0.379 14.5 1.431 0.09489 -0.188 0.000 0.789 0.001 0.832 15.085 0.680 0.381 15.0 1.438 0.10277 -0.191 0.000 0.790 0.001 0.836 13.998 0.786 0.383 Name = AH 83-150 Q 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 -0.353 0.14340 0.018 0.629 0.003 0.975 0.005 -2.461 4.089 0.300 -14.5 -0.352 0.13322 0.015 0.624 0.003 0.975 0.005 -2.644 2.081 0.292 -14.0 -0.350 0.12520 0.012 0.621 0.003 0.975 0.005 -2.794 1.127 0.284 -13.5 -0.346 0.11825 0.009 0.617 0.003 0.974 0.005 -2.923 0.810 0.276 -13.0 -0.339 0.17206 0.006 0.614 0.003 0.974 0.004 -1.973 0.649 0.268 -12.5 -0.331 0.10361 0.003 0.611 0.003 0.973 0.005 -3.194 0.559 0.260 -12.0 -0.320 0.09933 0.000 0.608 0.003 0.971 0.004 -3.224 0.505 0.251 -11.5 -0.307 0.12168 -0.003 0.606 0.003 0.969 0.004 -2.526 0.461 0.241 -11.0 -0.292 0.11397 -0.006 0.603 0.003 0.967 0.004 -2.558 0.431 0.230 -10.5 -0.274 0.10429 -0.009 0.600 0.003 0.965 0.004 -2.623 0.410 0.218 -10.0 -0.253 0.09281 -0.012 0.598 0.003 0.961 0.004 -2.726 0.394 0.203 -9.5 -0.230 0.08797 -0.015 0.594 0.002 0.956 0.004 -2.616 0.380 0.184 -9.0 -0.205 0.07867 -0.018 0.591 0.002 0.950 0.004 -2.600 0.369 0.161 -8.5 -0.177 0.07136 -0.021 0.587 0.002 0.938 0.003 -2.477 0.360 0.129 -8.0 -0.147 0.06177 -0.025 0.584 0.002 0.919 0.003 -2.372 0.354 0.082 -7.5 -0.115 0.05572 -0.028 0.581 0.002 0.891 0.003 -2.056 0.348 0.007 -7.0 -0.081 0.05116 -0.031 0.579 0.002 0.848 0.003 -1.574 0.344 -0.136 -6.5 -0.045 0.04574 -0.034 0.576 0.002 0.804 0.003 -0.985 0.341 -0.514 -6.0 -0.008 0.04111 -0.038 0.573 0.002 0.778 0.003 -0.201 0.211 -4.303 -5.5 -0.214 0.03681 -0.041 0.571 0.002 0.756 0.003 -5.824 0.203 0.058 -5.0 -0.152 0.03336 -0.044 0.568 0.002 0.738 0.003 -4.547 0.303 -0.043 -4.5 -0.088 0.03048 -0.048 0.566 0.002 0.720 0.003 -2.897 0.303 -0.291 -4.0 -0.025 0.02736 -0.051 0.562 0.002 0.713 0.003 -0.902 0.304 -1.825 -3.5 0.039 0.02479 -0.055 0.558 0.002 0.707 0.003 1.571 0.304 1.652 -3.0 0.102 0.02241 -0.058 0.554 0.003 0.699 0.004 4.562 0.305 0.818 -2.5 0.165 0.02025 -0.061 0.550 0.003 0.692 0.005 8.147 0.306 0.623 -2.0 0.227 0.01834 -0.065 0.547 0.004 0.686 0.006 12.371 0.307 0.536 -1.5 0.288 0.01657 -0.068 0.544 0.005 0.680 0.007 17.378 0.308 0.488 -1.0 0.348 0.01493 -0.072 0.540 0.006 0.674 0.009 23.305 0.330 0.457 -0.5 0.403 0.01801 -0.078 0.537 0.008 0.668 0.994 22.372 0.136 0.443 0.0 0.286 0.01906 -0.079 0.534 0.753 0.662 0.790 14.985 0.180 0.527 0.5 0.338 0.01950 -0.082 0.529 0.754 0.660 0.792 17.350 0.309 0.493 1.0 0.392 0.01996 -0.085 0.524 0.756 0.659 0.793 19.617 0.310 0.468 1.5 0.444 0.02047 -0.089 0.519 0.757 0.657 0.795 21.708 0.311 0.449 2.0 0.497 0.02102 -0.092 0.513 0.758 0.655 0.796 23.621 0.312 0.435 2.5 0.548 0.02162 -0.095 0.509 0.760 0.652 0.798 25.357 0.313 0.423 3.0 0.600 0.02227 -0.098 0.504 0.761 0.649 0.799 26.929 0.313 0.414 3.5 0.652 0.02289 -0.102 0.498 0.762 0.647 0.801 28.485 0.310 0.406 4.0 0.707 0.02342 -0.105 0.488 0.764 0.650 0.802 30.211 0.309 0.398 4.5 0.761 0.02402 -0.108 0.479 0.766 0.651 0.803 31.703 0.311 0.392 5.0 0.814 0.02471 -0.111 0.470 0.767 0.651 0.805 32.962 0.310 0.387 5.5 0.869 0.02535 -0.115 0.458 0.768 0.653 0.806 34.288 0.309 0.382 6.0 0.924 0.02607 -0.118 0.446 0.770 0.655 0.807 35.425 0.308 0.377 6.5 0.979 0.02690 -0.121 0.431 0.771 0.658 0.808 36.387 0.294 0.374 7.0 1.048 0.02733 -0.123 0.394 0.773 0.678 0.809 38.360 0.288 0.368 7.5 1.109 0.02830 -0.126 0.359 0.775 0.687 0.810 39.186 0.298 0.364 8.0 1.165 0.02961 -0.129 0.324 0.776 0.692 0.812 39.348 0.303 0.361 8.5 1.221 0.03127 -0.132 0.278 0.778 0.696 0.813 39.040 0.300 0.358 9.0 1.278 0.03590 -0.135 0.102 0.779 0.702 0.814 35.612 0.320 0.355 9.5 1.317 0.03813 -0.139 0.091 0.780 0.691 0.816 34.527 0.354 0.355 10.0 1.354 0.04196 -0.142 0.026 0.781 0.682 0.817 32.275 0.359 0.355 10.5 1.389 0.04467 -0.146 0.001 0.781 0.672 0.819 31.102 0.370 0.355 11.0 1.422 0.04748 -0.151 0.001 0.782 0.663 0.821 29.946 0.376 0.356 11.5 1.453 0.05014 -0.155 0.001 0.783 0.655 0.823 28.990 0.386 0.356 12.0 1.482 0.05309 -0.159 0.001 0.784 0.646 0.826 27.907 0.045 0.357 12.5 1.367 0.06650 -0.172 0.000 0.785 0.001 0.828 20.554 0.062 0.376 13.0 1.389 0.07137 -0.176 0.000 0.786 0.001 0.830 19.456 0.443 0.377 13.5 1.406 0.07656 -0.180 0.000 0.787 0.001 0.834 18.367 0.490 0.378 14.0 1.420 0.08350 -0.184 0.000 0.788 0.001 0.837 17.008 0.560 0.379 14.5 1.431 0.08969 -0.188 0.000 0.789 0.001 0.841 15.954 0.669 0.381 15.0 1.438 0.09501 -0.191 0.000 0.790 0.001 0.845 15.140 0.754 0.383