Name = AH 63-K-127/24 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 -0.295 0.23444 -0.029 0.701 0.003 0.724 0.004 -1.257 1.213 0.152 -14.5 -0.291 0.37917 -0.032 0.701 0.003 0.723 0.004 -0.768 0.985 0.140 -14.0 -0.286 0.30990 -0.035 0.700 0.003 0.723 0.004 -0.923 0.751 0.128 -13.5 -0.279 0.30420 -0.038 0.699 0.003 0.722 0.004 -0.917 0.625 0.113 -13.0 -0.269 0.24858 -0.041 0.699 0.003 0.721 0.004 -1.083 0.542 0.096 -12.5 -0.257 0.22209 -0.045 0.698 0.003 0.720 0.004 -1.158 0.486 0.077 -12.0 -0.242 0.21300 -0.048 0.697 0.003 0.719 0.004 -1.138 0.450 0.053 -11.5 -0.225 0.18912 -0.051 0.696 0.003 0.718 0.004 -1.190 0.424 0.024 -11.0 -0.205 0.16576 -0.054 0.695 0.003 0.717 0.004 -1.238 0.403 -0.014 -10.5 -0.183 0.14969 -0.057 0.695 0.002 0.716 0.003 -1.221 0.386 -0.064 -10.0 -0.157 0.12900 -0.061 0.694 0.003 0.715 0.003 -1.221 0.373 -0.135 -9.5 -0.130 0.11758 -0.064 0.693 0.003 0.714 0.003 -1.104 0.365 -0.242 -9.0 -0.100 0.10488 -0.067 0.693 0.002 0.713 0.003 -0.955 0.356 -0.421 -8.5 -0.068 0.09167 -0.071 0.692 0.002 0.712 0.003 -0.742 0.350 -0.787 -8.0 -0.034 0.08042 -0.074 0.690 0.002 0.711 0.003 -0.426 0.225 -1.904 -7.5 -0.330 0.07109 -0.077 0.687 0.002 0.711 0.003 -4.639 0.222 0.016 -7.0 -0.270 0.06486 -0.081 0.684 0.002 0.710 0.003 -4.162 0.305 -0.048 -6.5 -0.208 0.05711 -0.084 0.682 0.002 0.709 0.003 -3.650 0.304 -0.152 -6.0 -0.146 0.05223 -0.087 0.679 0.002 0.709 0.003 -2.790 0.303 -0.349 -5.5 -0.082 0.04607 -0.091 0.677 0.002 0.708 0.003 -1.785 0.303 -0.851 -5.0 -0.018 0.04170 -0.094 0.675 0.002 0.707 0.003 -0.442 0.303 -4.845 -4.5 0.045 0.03829 -0.097 0.672 0.003 0.706 0.003 1.183 0.303 2.398 -4.0 0.109 0.03487 -0.101 0.670 0.003 0.705 0.004 3.117 0.304 1.177 -3.5 0.171 0.03225 -0.104 0.668 0.004 0.704 0.006 5.317 0.304 0.857 -3.0 0.233 0.03003 -0.107 0.665 0.006 0.703 0.008 7.771 0.305 0.711 -2.5 0.294 0.02801 -0.111 0.663 0.007 0.702 0.010 10.508 0.345 0.627 -2.0 0.345 0.02502 -0.118 0.661 0.679 0.701 0.771 13.795 0.339 0.592 -1.5 0.405 0.02501 -0.121 0.657 0.686 0.700 0.778 16.179 0.293 0.548 -1.0 0.464 0.02509 -0.123 0.653 0.692 0.700 0.784 18.493 0.293 0.516 -0.5 0.523 0.02523 -0.126 0.649 0.697 0.699 0.790 20.729 0.132 0.490 0.0 0.422 0.02922 -0.128 0.645 0.701 0.698 0.796 14.445 0.140 0.554 0.5 0.475 0.02977 -0.131 0.642 0.706 0.697 0.802 15.953 0.304 0.526 1.0 0.528 0.03033 -0.134 0.638 0.710 0.695 0.807 17.390 0.305 0.504 1.5 0.580 0.03098 -0.137 0.634 0.715 0.694 0.811 18.722 0.305 0.486 2.0 0.632 0.03168 -0.140 0.630 0.720 0.693 0.815 19.962 0.304 0.471 2.5 0.686 0.03237 -0.142 0.615 0.725 0.694 0.819 21.204 0.303 0.458 3.0 0.740 0.03313 -0.145 0.601 0.732 0.694 0.822 22.329 0.303 0.447 3.5 0.794 0.03396 -0.148 0.578 0.739 0.696 0.825 23.393 0.302 0.437 4.0 0.848 0.03482 -0.151 0.556 0.747 0.698 0.827 24.354 0.303 0.428 4.5 0.901 0.03585 -0.154 0.535 0.753 0.698 0.830 25.125 0.304 0.421 5.0 0.953 0.03693 -0.157 0.510 0.758 0.699 0.833 25.796 0.305 0.414 5.5 1.004 0.03817 -0.159 0.484 0.763 0.700 0.836 26.298 0.278 0.409 6.0 1.088 0.03870 -0.160 0.077 0.768 0.739 0.839 28.114 0.631 0.397 6.5 1.040 0.04258 -0.173 0.003 0.774 0.009 0.841 24.429 -2.103 0.417 7.0 1.081 0.04592 -0.177 0.002 0.780 0.004 0.844 23.540 0.345 0.413 7.5 1.111 0.05038 -0.180 0.001 0.784 0.003 0.847 22.055 0.371 0.412 8.0 1.138 0.05599 -0.183 0.001 0.789 0.002 0.850 20.319 0.388 0.411 8.5 1.161 0.06198 -0.187 0.001 0.793 0.001 0.853 18.725 0.424 0.411 9.0 1.177 0.06944 -0.190 0.001 0.798 0.001 0.857 16.946 0.491 0.412 9.5 1.189 0.07780 -0.194 0.001 0.804 0.001 0.862 15.281 0.596 0.413 10.0 1.197 0.08921 -0.197 0.000 0.807 0.001 0.868 13.412 0.963 0.415 10.5 1.198 0.10055 -0.201 0.000 0.810 0.001 0.875 11.920 -3.974 0.417 11.0 1.195 0.11722 -0.204 0.000 0.813 0.001 0.999 10.194 -0.294 0.421 11.5 1.186 0.12908 -0.207 0.000 0.816 0.001 1.000 9.188 -0.062 0.425 12.0 1.173 0.15064 -0.211 0.000 0.819 0.001 1.000 7.788 0.029 0.430 12.5 1.155 0.16689 -0.214 0.000 0.822 0.001 1.000 6.922 0.081 0.435 13.0 1.133 0.19186 -0.218 0.000 0.826 0.001 1.000 5.906 0.111 0.442 13.5 1.107 0.20802 -0.221 0.001 0.830 0.001 1.000 5.321 0.129 0.450 14.0 1.078 0.23816 -0.224 0.001 0.832 0.001 1.000 4.525 0.141 0.458 14.5 1.046 0.26034 -0.228 0.001 0.835 0.001 1.000 4.017 0.149 0.468 15.0 1.011 0.28840 -0.231 0.001 0.838 0.001 1.000 3.507 0.153 0.478 Name = AH 63-K-127/24 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 -0.295 0.17882 -0.029 0.701 0.003 0.727 0.005 -1.647 1.212 0.152 -14.5 -0.291 0.16588 -0.032 0.701 0.003 0.726 0.004 -1.756 0.979 0.140 -14.0 -0.286 0.15301 -0.035 0.700 0.003 0.725 0.005 -1.869 0.748 0.128 -13.5 -0.279 0.22560 -0.038 0.699 0.003 0.724 0.004 -1.235 0.625 0.113 -13.0 -0.269 0.19078 -0.041 0.699 0.003 0.724 0.004 -1.411 0.539 0.096 -12.5 -0.257 0.18159 -0.045 0.698 0.003 0.723 0.004 -1.414 0.486 0.077 -12.0 -0.242 0.16406 -0.048 0.697 0.003 0.722 0.004 -1.476 0.453 0.053 -11.5 -0.225 0.13895 -0.051 0.696 0.003 0.722 0.004 -1.620 0.424 0.024 -11.0 -0.205 0.13242 -0.054 0.695 0.003 0.721 0.004 -1.549 0.402 -0.014 -10.5 -0.183 0.11903 -0.057 0.695 0.002 0.719 0.004 -1.534 0.386 -0.065 -10.0 -0.157 0.10400 -0.061 0.694 0.003 0.718 0.004 -1.512 0.374 -0.136 -9.5 -0.130 0.09289 -0.064 0.693 0.003 0.717 0.003 -1.397 0.365 -0.243 -9.0 -0.100 0.08347 -0.067 0.693 0.002 0.716 0.003 -1.199 0.356 -0.422 -8.5 -0.068 0.07379 -0.071 0.692 0.002 0.715 0.003 -0.920 0.350 -0.789 -8.0 -0.034 0.06574 -0.074 0.690 0.002 0.714 0.003 -0.520 0.225 -1.912 -7.5 -0.330 0.05860 -0.077 0.687 0.002 0.714 0.003 -5.627 0.222 0.016 -7.0 -0.270 0.05383 -0.081 0.684 0.002 0.714 0.003 -5.015 0.305 -0.048 -6.5 -0.208 0.04779 -0.084 0.682 0.002 0.714 0.003 -4.362 0.304 -0.152 -6.0 -0.146 0.04285 -0.087 0.679 0.002 0.713 0.003 -3.401 0.303 -0.349 -5.5 -0.082 0.03865 -0.091 0.677 0.002 0.712 0.003 -2.128 0.303 -0.851 -5.0 -0.018 0.03498 -0.094 0.675 0.002 0.712 0.003 -0.527 0.303 -4.845 -4.5 0.045 0.03199 -0.097 0.672 0.003 0.711 0.004 1.417 0.303 2.398 -4.0 0.109 0.02922 -0.101 0.670 0.003 0.710 0.004 3.721 0.304 1.177 -3.5 0.171 0.02678 -0.104 0.668 0.004 0.709 0.006 6.402 0.304 0.857 -3.0 0.233 0.02475 -0.107 0.665 0.006 0.708 0.008 9.430 0.305 0.711 -2.5 0.294 0.02298 -0.111 0.663 0.007 0.707 0.012 12.810 0.349 0.627 -2.0 0.345 0.01791 -0.119 0.661 0.679 0.706 0.797 19.254 0.342 0.594 -1.5 0.404 0.01789 -0.121 0.657 0.686 0.706 0.803 22.603 0.291 0.549 -1.0 0.464 0.01794 -0.123 0.653 0.692 0.705 0.808 25.856 0.290 0.516 -0.5 0.523 0.01801 -0.126 0.649 0.697 0.705 0.813 29.026 0.125 0.491 0.0 0.426 0.02189 -0.128 0.645 0.701 0.704 0.818 19.467 0.132 0.551 0.5 0.479 0.02232 -0.131 0.642 0.706 0.703 0.823 21.469 0.303 0.523 1.0 0.532 0.02279 -0.134 0.638 0.710 0.702 0.827 23.357 0.304 0.501 1.5 0.585 0.02329 -0.137 0.634 0.715 0.701 0.832 25.112 0.304 0.484 2.0 0.637 0.02382 -0.140 0.630 0.720 0.700 0.835 26.751 0.302 0.469 2.5 0.693 0.02432 -0.142 0.615 0.725 0.702 0.838 28.490 0.301 0.455 3.0 0.748 0.02488 -0.145 0.601 0.732 0.704 0.841 30.050 0.299 0.444 3.5 0.804 0.02544 -0.148 0.578 0.739 0.709 0.842 31.609 0.298 0.434 4.0 0.860 0.02608 -0.151 0.556 0.747 0.712 0.844 32.974 0.299 0.425 4.5 0.914 0.02680 -0.153 0.535 0.753 0.714 0.846 34.109 0.300 0.418 5.0 0.968 0.02763 -0.156 0.510 0.758 0.718 0.849 35.043 0.300 0.411 5.5 1.021 0.02852 -0.159 0.484 0.763 0.720 0.852 35.788 0.280 0.405 6.0 1.098 0.03161 -0.160 0.077 0.768 0.749 0.855 34.736 0.282 0.396 6.5 1.145 0.03255 -0.162 0.003 0.774 0.749 0.858 35.158 -0.689 0.392 7.0 1.080 0.04016 -0.177 0.002 0.780 0.004 0.863 26.893 -0.263 0.414 7.5 1.110 0.04379 -0.180 0.001 0.784 0.003 0.868 25.356 0.370 0.412 8.0 1.137 0.04762 -0.183 0.001 0.789 0.002 0.874 23.879 0.388 0.411 8.5 1.160 0.05414 -0.187 0.001 0.793 0.001 0.999 21.424 0.423 0.411 9.0 1.177 0.05937 -0.190 0.001 0.798 0.001 0.999 19.815 0.487 0.412 9.5 1.189 0.06591 -0.194 0.001 0.804 0.001 0.999 18.034 0.596 0.413 10.0 1.196 0.07481 -0.197 0.000 0.807 0.001 0.999 15.991 0.962 0.415 10.5 1.198 0.08347 -0.201 0.000 0.810 0.001 1.000 14.355 -4.014 0.417 11.0 1.195 0.09506 -0.204 0.000 0.813 0.001 1.000 12.568 -0.295 0.421 11.5 1.186 0.10347 -0.207 0.000 0.816 0.001 1.000 11.459 -0.062 0.425 12.0 1.173 0.11904 -0.211 0.000 0.819 0.001 1.000 9.853 0.031 0.430 12.5 1.155 0.13437 -0.214 0.000 0.822 0.001 1.000 8.595 0.081 0.435 13.0 1.133 0.14794 -0.218 0.000 0.826 0.001 1.000 7.658 0.111 0.442 13.5 1.106 0.16386 -0.221 0.001 0.830 0.001 1.000 6.753 0.129 0.450 14.0 1.077 0.17956 -0.224 0.001 0.832 0.001 1.000 6.001 0.140 0.458 14.5 1.045 0.20051 -0.228 0.001 0.835 0.001 1.000 5.214 0.149 0.468 15.0 1.011 0.17600 -0.231 0.001 0.838 0.001 1.000 5.745 0.153 0.478 Name = AH 63-K-127/24 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 -0.295 0.15509 -0.029 0.701 0.003 0.729 0.005 -1.899 1.211 0.152 -14.5 -0.291 0.14551 -0.032 0.701 0.003 0.728 0.005 -2.002 0.978 0.140 -14.0 -0.286 0.13408 -0.035 0.700 0.003 0.728 0.005 -2.133 0.748 0.128 -13.5 -0.279 0.12466 -0.038 0.699 0.003 0.727 0.004 -2.235 0.623 0.113 -13.0 -0.269 0.16588 -0.041 0.699 0.003 0.726 0.004 -1.622 0.539 0.096 -12.5 -0.257 0.15643 -0.045 0.698 0.003 0.725 0.004 -1.641 0.488 0.077 -12.0 -0.242 0.13497 -0.048 0.697 0.003 0.724 0.004 -1.794 0.452 0.053 -11.5 -0.225 0.12356 -0.051 0.696 0.003 0.724 0.004 -1.821 0.424 0.024 -11.0 -0.205 0.11169 -0.054 0.695 0.003 0.723 0.004 -1.836 0.402 -0.014 -10.5 -0.182 0.10630 -0.057 0.695 0.002 0.722 0.004 -1.716 0.386 -0.065 -10.0 -0.157 0.09104 -0.061 0.694 0.003 0.721 0.004 -1.726 0.374 -0.136 -9.5 -0.130 0.08225 -0.064 0.693 0.003 0.720 0.004 -1.576 0.365 -0.243 -9.0 -0.100 0.07424 -0.067 0.693 0.002 0.719 0.003 -1.346 0.356 -0.423 -8.5 -0.068 0.06610 -0.071 0.692 0.002 0.718 0.003 -1.025 0.350 -0.791 -8.0 -0.034 0.05946 -0.074 0.690 0.002 0.718 0.003 -0.573 0.225 -1.919 -7.5 -0.330 0.05326 -0.077 0.687 0.002 0.718 0.003 -6.192 0.222 0.016 -7.0 -0.270 0.04811 -0.081 0.684 0.002 0.717 0.003 -5.611 0.305 -0.048 -6.5 -0.208 0.04298 -0.084 0.682 0.002 0.717 0.003 -4.850 0.304 -0.152 -6.0 -0.146 0.03933 -0.087 0.679 0.002 0.717 0.003 -3.705 0.303 -0.348 -5.5 -0.082 0.03544 -0.091 0.677 0.002 0.716 0.003 -2.321 0.303 -0.851 -5.0 -0.018 0.03205 -0.094 0.675 0.002 0.715 0.003 -0.575 0.303 -4.845 -4.5 0.045 0.02923 -0.097 0.672 0.003 0.715 0.004 1.550 0.303 2.398 -4.0 0.109 0.02664 -0.101 0.670 0.003 0.714 0.004 4.081 0.304 1.177 -3.5 0.171 0.02448 -0.104 0.668 0.004 0.713 0.006 7.004 0.304 0.857 -3.0 0.233 0.02243 -0.107 0.665 0.006 0.713 0.008 10.403 0.305 0.711 -2.5 0.294 0.02096 -0.111 0.663 0.007 0.712 0.017 14.037 0.353 0.627 -2.0 0.345 0.01471 -0.119 0.661 0.679 0.711 0.815 23.425 0.345 0.595 -1.5 0.404 0.01472 -0.121 0.657 0.686 0.711 0.820 27.466 0.290 0.550 -1.0 0.464 0.01474 -0.124 0.653 0.692 0.710 0.824 31.447 0.289 0.517 -0.5 0.523 0.01482 -0.126 0.649 0.697 0.710 0.829 35.271 0.116 0.491 0.0 0.430 0.01858 -0.128 0.645 0.701 0.709 0.834 23.121 0.124 0.548 0.5 0.483 0.01896 -0.131 0.642 0.706 0.708 0.838 25.470 0.303 0.521 1.0 0.536 0.01936 -0.134 0.638 0.710 0.708 0.843 27.690 0.303 0.500 1.5 0.589 0.01980 -0.137 0.634 0.715 0.707 0.847 29.740 0.304 0.482 2.0 0.642 0.02028 -0.139 0.630 0.720 0.706 0.851 31.646 0.301 0.467 2.5 0.698 0.02066 -0.142 0.615 0.725 0.710 0.854 33.796 0.299 0.454 3.0 0.754 0.02112 -0.145 0.601 0.732 0.713 0.858 35.710 0.297 0.442 3.5 0.812 0.02155 -0.148 0.578 0.739 0.719 0.860 37.680 0.296 0.432 4.0 0.869 0.02206 -0.150 0.556 0.747 0.723 0.861 39.381 0.298 0.423 4.5 0.923 0.02271 -0.153 0.535 0.753 0.725 0.865 40.652 0.299 0.416 5.0 0.977 0.02343 -0.156 0.510 0.758 0.728 0.869 41.716 0.300 0.409 5.5 1.030 0.02423 -0.158 0.484 0.763 0.730 0.875 42.504 0.277 0.404 6.0 1.111 0.02786 -0.159 0.077 0.768 0.764 0.893 39.885 0.278 0.393 6.5 1.157 0.03001 -0.162 0.003 0.774 0.763 0.998 38.546 -0.222 0.390 7.0 1.074 0.03912 -0.177 0.002 0.780 0.007 0.998 27.447 -0.137 0.415 7.5 1.109 0.04180 -0.180 0.001 0.784 0.004 0.999 26.541 0.358 0.412 8.0 1.136 0.04536 -0.184 0.001 0.789 0.002 0.999 25.046 0.386 0.412 8.5 1.159 0.04997 -0.187 0.001 0.793 0.001 0.999 23.200 0.422 0.411 9.0 1.176 0.05526 -0.190 0.001 0.798 0.001 0.999 21.282 0.486 0.412 9.5 1.188 0.06036 -0.194 0.001 0.804 0.001 0.999 19.689 0.591 0.413 10.0 1.196 0.06817 -0.197 0.000 0.807 0.001 1.000 17.544 0.961 0.415 10.5 1.198 0.07573 -0.201 0.000 0.810 0.001 1.000 15.820 -4.056 0.417 11.0 1.194 0.08568 -0.204 0.000 0.813 0.001 1.000 13.941 -0.296 0.421 11.5 1.185 0.09247 -0.207 0.000 0.816 0.001 1.000 12.820 -0.062 0.425 12.0 1.173 0.10544 -0.211 0.000 0.819 0.001 1.000 11.122 0.031 0.430 12.5 1.155 0.11742 -0.214 0.000 0.822 0.001 1.000 9.833 0.082 0.435 13.0 1.133 0.13264 -0.218 0.000 0.826 0.001 1.000 8.538 0.111 0.442 13.5 1.106 0.14088 -0.221 0.001 0.830 0.001 1.000 7.852 0.129 0.450 14.0 1.077 0.15877 -0.224 0.001 0.832 0.001 1.000 6.784 0.141 0.458 14.5 1.045 0.14192 -0.228 0.001 0.835 0.001 1.000 7.364 0.149 0.468 15.0 1.011 0.15598 -0.231 0.001 0.838 0.001 1.000 6.481 0.153 0.478 Name = AH 63-K-127/24 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 -0.294 0.14118 -0.029 0.701 0.003 0.731 0.005 -2.086 1.209 0.152 -14.5 -0.291 0.13365 -0.032 0.701 0.003 0.730 0.005 -2.179 0.978 0.141 -14.0 -0.286 0.12309 -0.035 0.700 0.003 0.730 0.005 -2.323 0.747 0.128 -13.5 -0.279 0.11525 -0.038 0.699 0.003 0.728 0.005 -2.417 0.623 0.113 -13.0 -0.269 0.10559 -0.041 0.699 0.003 0.728 0.004 -2.547 0.539 0.096 -12.5 -0.257 0.10030 -0.044 0.698 0.003 0.727 0.005 -2.559 0.487 0.077 -12.0 -0.242 0.12412 -0.048 0.697 0.003 0.726 0.004 -1.950 0.452 0.053 -11.5 -0.225 0.11478 -0.051 0.696 0.003 0.726 0.004 -1.958 0.424 0.023 -11.0 -0.205 0.10472 -0.054 0.695 0.003 0.725 0.004 -1.956 0.403 -0.014 -10.5 -0.182 0.09387 -0.057 0.695 0.002 0.724 0.004 -1.943 0.386 -0.065 -10.0 -0.157 0.08343 -0.061 0.694 0.003 0.723 0.004 -1.883 0.374 -0.136 -9.5 -0.130 0.07602 -0.064 0.693 0.003 0.722 0.004 -1.704 0.365 -0.244 -9.0 -0.100 0.06884 -0.067 0.693 0.002 0.722 0.003 -1.451 0.356 -0.423 -8.5 -0.068 0.06163 -0.071 0.692 0.002 0.721 0.003 -1.098 0.350 -0.793 -8.0 -0.034 0.05467 -0.074 0.690 0.002 0.720 0.003 -0.623 0.225 -1.919 -7.5 -0.330 0.04922 -0.077 0.687 0.002 0.721 0.003 -6.700 0.222 0.016 -7.0 -0.270 0.04553 -0.081 0.684 0.002 0.721 0.003 -5.929 0.305 -0.048 -6.5 -0.208 0.04014 -0.084 0.682 0.002 0.721 0.003 -5.193 0.304 -0.152 -6.0 -0.146 0.03677 -0.087 0.679 0.002 0.720 0.003 -3.963 0.303 -0.348 -5.5 -0.082 0.03357 -0.091 0.677 0.002 0.720 0.003 -2.450 0.303 -0.851 -5.0 -0.018 0.03010 -0.094 0.675 0.002 0.719 0.003 -0.612 0.303 -4.845 -4.5 0.045 0.02762 -0.097 0.672 0.003 0.719 0.004 1.641 0.303 2.398 -4.0 0.109 0.02513 -0.101 0.670 0.003 0.718 0.004 4.325 0.304 1.177 -3.5 0.171 0.02305 -0.104 0.668 0.004 0.718 0.006 7.439 0.304 0.857 -3.0 0.233 0.02112 -0.107 0.665 0.006 0.716 0.008 11.052 0.410 0.711 -2.5 0.282 0.01561 -0.122 0.663 0.007 0.715 0.997 18.069 0.355 0.682 -2.0 0.344 0.01281 -0.119 0.661 0.679 0.715 0.829 26.895 0.247 0.596 -1.5 0.404 0.01281 -0.121 0.657 0.686 0.715 0.834 31.551 0.288 0.551 -1.0 0.463 0.01285 -0.124 0.653 0.692 0.715 0.837 36.072 0.288 0.517 -0.5 0.523 0.01291 -0.126 0.649 0.697 0.714 0.842 40.477 0.106 0.491 0.0 0.433 0.01657 -0.128 0.645 0.701 0.714 0.848 26.121 0.114 0.546 0.5 0.486 0.01691 -0.131 0.642 0.706 0.713 0.852 28.751 0.302 0.519 1.0 0.540 0.01728 -0.134 0.638 0.710 0.713 0.858 31.231 0.303 0.498 1.5 0.593 0.01768 -0.137 0.634 0.715 0.712 0.865 33.512 0.303 0.480 2.0 0.646 0.01811 -0.139 0.630 0.720 0.711 0.871 35.640 0.300 0.466 2.5 0.703 0.01843 -0.142 0.615 0.725 0.716 0.876 38.158 0.297 0.452 3.0 0.760 0.01883 -0.145 0.601 0.732 0.720 0.885 40.356 0.296 0.441 3.5 0.818 0.01922 -0.147 0.578 0.739 0.725 0.893 42.538 0.296 0.430 4.0 0.874 0.02010 -0.150 0.556 0.747 0.729 0.997 43.498 0.297 0.422 4.5 0.929 0.02076 -0.153 0.535 0.753 0.731 0.997 44.752 0.298 0.414 5.0 0.983 0.02147 -0.155 0.510 0.758 0.734 0.997 45.802 0.299 0.408 5.5 1.036 0.02235 -0.158 0.484 0.763 0.736 0.998 46.370 0.273 0.402 6.0 1.121 0.02617 -0.158 0.077 0.768 0.775 0.998 42.847 0.275 0.391 6.5 1.166 0.02799 -0.161 0.003 0.774 0.773 0.998 41.662 0.321 0.388 7.0 1.202 0.02963 -0.164 0.002 0.780 0.764 0.999 40.569 -0.078 0.387 7.5 1.108 0.04023 -0.180 0.001 0.784 0.004 0.999 27.551 -0.037 0.412 8.0 1.135 0.04403 -0.184 0.001 0.789 0.003 0.999 25.770 0.386 0.412 8.5 1.158 0.04810 -0.187 0.001 0.793 0.002 0.999 24.085 0.417 0.411 9.0 1.176 0.05241 -0.190 0.001 0.798 0.001 0.999 22.430 0.480 0.412 9.5 1.188 0.05709 -0.194 0.001 0.804 0.001 0.999 20.809 0.587 0.413 10.0 1.196 0.06428 -0.197 0.000 0.807 0.001 1.000 18.603 0.960 0.415 10.5 1.198 0.07122 -0.201 0.000 0.810 0.001 1.000 16.818 -4.906 0.417 11.0 1.194 0.07823 -0.204 0.000 0.813 0.001 1.000 15.268 -0.296 0.421 11.5 1.185 0.08601 -0.207 0.000 0.816 0.001 1.000 13.781 -0.059 0.425 12.0 1.172 0.09738 -0.211 0.000 0.819 0.001 1.000 12.040 0.031 0.430 12.5 1.154 0.10738 -0.214 0.000 0.822 0.001 1.000 10.750 0.082 0.436 13.0 1.132 0.12048 -0.218 0.000 0.826 0.001 1.000 9.398 0.111 0.442 13.5 1.106 0.11508 -0.221 0.001 0.830 0.001 1.000 9.609 0.129 0.450 14.0 1.077 0.12275 -0.224 0.001 0.832 0.001 1.000 8.773 0.140 0.458 14.5 1.045 0.13168 -0.228 0.001 0.835 0.001 1.000 7.935 0.149 0.468 15.0 1.011 0.14455 -0.231 0.001 0.838 0.002 1.000 6.991 0.153 0.479