Name = AH 88-K-130/20 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 -0.260 0.40536 -0.046 0.737 0.003 0.781 0.004 -0.642 0.818 0.072 -14.5 -0.254 0.34472 -0.050 0.737 0.003 0.777 0.004 -0.737 0.731 0.054 -14.0 -0.246 0.32109 -0.053 0.736 0.003 0.774 0.004 -0.766 0.621 0.033 -13.5 -0.236 0.27483 -0.057 0.735 0.003 0.771 0.004 -0.857 0.549 0.009 -13.0 -0.223 0.25467 -0.060 0.735 0.003 0.769 0.004 -0.874 0.498 -0.021 -12.5 -0.207 0.24043 -0.064 0.734 0.002 0.766 0.004 -0.863 0.462 -0.058 -12.0 -0.190 0.20411 -0.067 0.733 0.002 0.764 0.003 -0.929 0.433 -0.105 -11.5 -0.169 0.18793 -0.071 0.733 0.002 0.762 0.003 -0.899 0.411 -0.169 -11.0 -0.146 0.16252 -0.074 0.732 0.002 0.760 0.003 -0.897 0.395 -0.260 -10.5 -0.120 0.15108 -0.078 0.731 0.002 0.758 0.003 -0.795 0.383 -0.399 -10.0 -0.092 0.12866 -0.082 0.731 0.002 0.756 0.003 -0.716 0.373 -0.635 -9.5 -0.062 0.11382 -0.085 0.730 0.002 0.754 0.003 -0.543 0.365 -1.127 -9.0 -0.029 0.10164 -0.089 0.729 0.002 0.752 0.003 -0.290 0.226 -2.764 -8.5 -0.360 0.08708 -0.092 0.728 0.002 0.750 0.003 -4.135 0.224 -0.006 -8.0 -0.303 0.07868 -0.096 0.728 0.002 0.749 0.003 -3.851 0.312 -0.067 -7.5 -0.244 0.06940 -0.100 0.727 0.002 0.749 0.003 -3.509 0.310 -0.159 -7.0 -0.182 0.06343 -0.103 0.726 0.002 0.747 0.003 -2.872 0.309 -0.316 -6.5 -0.119 0.05620 -0.107 0.725 0.002 0.746 0.003 -2.126 0.308 -0.644 -6.0 -0.056 0.05019 -0.110 0.725 0.002 0.745 0.003 -1.114 0.307 -1.726 -5.5 0.008 0.04514 -0.114 0.724 0.002 0.744 0.003 0.180 0.307 14.300 -5.0 0.072 0.04118 -0.118 0.723 0.002 0.743 0.003 1.754 0.307 1.881 -4.5 0.136 0.03789 -0.121 0.723 0.003 0.742 0.003 3.590 0.308 1.143 -4.0 0.199 0.03482 -0.125 0.722 0.003 0.741 0.004 5.724 0.308 0.878 -3.5 0.262 0.03268 -0.129 0.719 0.004 0.741 0.010 8.007 0.308 0.742 -3.0 0.323 0.03125 -0.132 0.716 0.012 0.740 0.016 10.341 0.310 0.659 -2.5 0.384 0.02939 -0.136 0.713 0.015 0.739 0.021 13.054 0.381 0.605 -2.0 0.428 0.02452 -0.146 0.710 0.051 0.738 0.895 17.456 0.348 0.591 -1.5 0.491 0.02572 -0.146 0.707 0.690 0.737 0.784 19.084 0.275 0.548 -1.0 0.550 0.02592 -0.149 0.705 0.750 0.736 0.774 21.229 0.296 0.521 -0.5 0.609 0.02608 -0.152 0.702 0.752 0.736 0.776 23.360 0.133 0.499 0.0 0.503 0.02961 -0.155 0.699 0.754 0.734 0.778 16.992 0.141 0.557 0.5 0.557 0.03011 -0.158 0.696 0.755 0.733 0.780 18.496 0.305 0.533 1.0 0.611 0.03066 -0.161 0.693 0.757 0.732 0.781 19.913 0.305 0.513 1.5 0.665 0.03123 -0.164 0.683 0.758 0.732 0.783 21.295 0.304 0.496 2.0 0.720 0.03185 -0.166 0.670 0.760 0.733 0.784 22.601 0.299 0.481 2.5 0.780 0.03238 -0.169 0.619 0.761 0.742 0.785 24.097 0.300 0.467 3.0 0.834 0.03315 -0.172 0.608 0.762 0.741 0.786 25.152 0.255 0.456 3.5 0.997 0.02955 -0.170 0.026 0.764 0.881 0.788 33.723 0.256 0.421 4.0 1.037 0.03101 -0.173 0.024 0.765 0.862 0.789 33.440 0.323 0.417 4.5 1.079 0.03259 -0.176 0.023 0.766 0.847 0.790 33.118 -1.206 0.413 5.0 1.024 0.03265 -0.192 0.004 0.767 0.008 0.791 31.378 -1.243 0.437 5.5 1.066 0.03570 -0.195 0.003 0.768 0.004 0.793 29.869 0.343 0.433 6.0 1.102 0.03947 -0.199 0.002 0.770 0.003 0.794 27.927 0.357 0.430 6.5 1.135 0.04470 -0.203 0.002 0.771 0.003 0.795 25.380 0.371 0.429 7.0 1.163 0.05011 -0.206 0.002 0.772 0.003 0.796 23.200 0.388 0.427 7.5 1.187 0.05591 -0.210 0.002 0.773 0.002 0.797 21.236 0.411 0.427 8.0 1.208 0.06230 -0.213 0.001 0.774 0.002 0.798 19.382 0.452 0.427 8.5 1.223 0.07153 -0.217 0.001 0.775 0.002 0.799 17.097 0.519 0.427 9.0 1.234 0.07953 -0.221 0.001 0.776 0.001 0.800 15.519 0.667 0.429 9.5 1.240 0.09309 -0.224 0.001 0.778 0.001 0.802 13.322 1.367 0.431 10.0 1.241 0.10368 -0.228 0.001 0.779 0.001 0.803 11.967 -1.432 0.434 10.5 1.236 0.11646 -0.231 0.001 0.780 0.001 0.804 10.612 -0.215 0.437 11.0 1.225 0.13218 -0.235 0.001 0.780 0.001 0.807 9.271 -0.022 0.442 11.5 1.210 0.15112 -0.238 0.000 0.781 0.001 0.810 8.006 0.061 0.447 12.0 1.188 0.16565 -0.242 0.000 0.782 0.001 0.815 7.171 0.104 0.454 12.5 1.162 0.19142 -0.245 0.001 0.783 0.001 0.819 6.069 0.126 0.461 13.0 1.132 0.21878 -0.249 0.001 0.784 0.001 0.824 5.172 0.139 0.470 13.5 1.099 0.25174 -0.252 0.001 0.784 0.001 0.829 4.364 0.150 0.480 14.0 1.062 0.28097 -0.256 0.001 0.785 0.001 0.837 3.780 0.158 0.491 14.5 1.024 0.32129 -0.259 0.001 0.786 0.001 0.849 3.186 0.162 0.503 15.0 0.984 0.36260 -0.263 0.001 0.787 0.001 0.886 2.713 0.164 0.517 Name = AH 88-K-130/20 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 -0.260 0.29617 -0.046 0.737 0.003 0.830 0.004 -0.878 0.804 0.072 -14.5 -0.254 0.27791 -0.050 0.737 0.003 0.800 0.004 -0.914 0.730 0.054 -14.0 -0.246 0.24124 -0.053 0.736 0.003 0.794 0.004 -1.019 0.624 0.033 -13.5 -0.235 0.21062 -0.057 0.735 0.003 0.788 0.004 -1.118 0.548 0.009 -13.0 -0.222 0.19663 -0.060 0.735 0.003 0.783 0.004 -1.132 0.498 -0.021 -12.5 -0.207 0.18644 -0.064 0.734 0.002 0.779 0.004 -1.112 0.462 -0.058 -12.0 -0.189 0.16120 -0.067 0.733 0.002 0.775 0.004 -1.175 0.433 -0.105 -11.5 -0.169 0.14976 -0.071 0.733 0.002 0.772 0.004 -1.127 0.411 -0.170 -11.0 -0.146 0.12913 -0.074 0.732 0.002 0.769 0.004 -1.127 0.396 -0.261 -10.5 -0.120 0.11233 -0.078 0.731 0.002 0.767 0.003 -1.069 0.383 -0.399 -10.0 -0.092 0.10503 -0.082 0.731 0.002 0.764 0.003 -0.875 0.373 -0.637 -9.5 -0.062 0.09024 -0.085 0.730 0.002 0.762 0.003 -0.684 0.365 -1.129 -9.0 -0.029 0.08159 -0.089 0.729 0.002 0.759 0.003 -0.359 0.226 -2.775 -8.5 -0.360 0.07081 -0.092 0.728 0.002 0.757 0.003 -5.085 0.224 -0.006 -8.0 -0.303 0.06277 -0.096 0.728 0.002 0.755 0.003 -4.827 0.312 -0.067 -7.5 -0.244 0.05750 -0.100 0.727 0.002 0.753 0.003 -4.235 0.310 -0.159 -7.0 -0.182 0.05152 -0.103 0.726 0.002 0.751 0.003 -3.536 0.309 -0.316 -6.5 -0.119 0.04608 -0.107 0.725 0.002 0.750 0.003 -2.593 0.308 -0.644 -6.0 -0.056 0.04228 -0.110 0.725 0.002 0.748 0.003 -1.322 0.307 -1.726 -5.5 0.008 0.03752 -0.114 0.724 0.002 0.747 0.003 0.216 0.307 14.300 -5.0 0.072 0.03426 -0.118 0.723 0.002 0.746 0.003 2.108 0.307 1.881 -4.5 0.136 0.03168 -0.121 0.723 0.003 0.745 0.004 4.294 0.308 1.143 -4.0 0.199 0.02897 -0.125 0.722 0.003 0.744 0.004 6.878 0.308 0.878 -3.5 0.262 0.02726 -0.129 0.719 0.004 0.744 0.012 9.597 0.308 0.742 -3.0 0.323 0.02564 -0.132 0.716 0.012 0.743 0.016 12.606 0.310 0.659 -2.5 0.384 0.02399 -0.136 0.713 0.015 0.742 0.025 15.990 0.401 0.604 -2.0 0.428 0.01846 -0.148 0.710 0.051 0.742 0.981 23.189 0.350 0.596 -1.5 0.491 0.01842 -0.147 0.707 0.690 0.741 0.793 26.639 0.258 0.549 -1.0 0.550 0.01858 -0.149 0.705 0.750 0.741 0.777 29.619 0.295 0.521 -0.5 0.609 0.01866 -0.152 0.702 0.752 0.740 0.779 32.656 0.126 0.499 0.0 0.506 0.02201 -0.155 0.699 0.754 0.739 0.781 22.979 0.135 0.556 0.5 0.560 0.02241 -0.158 0.696 0.755 0.738 0.782 24.977 0.304 0.532 1.0 0.614 0.02284 -0.161 0.693 0.757 0.737 0.784 26.860 0.304 0.512 1.5 0.669 0.02326 -0.163 0.683 0.758 0.738 0.785 28.758 0.302 0.494 2.0 0.725 0.02371 -0.166 0.670 0.760 0.740 0.786 30.567 0.294 0.479 2.5 0.792 0.02394 -0.169 0.619 0.761 0.758 0.788 33.082 0.294 0.463 3.0 0.846 0.02453 -0.172 0.608 0.762 0.758 0.789 34.504 0.238 0.453 3.5 1.085 0.02476 -0.165 0.026 0.764 1.000 0.791 43.832 0.242 0.402 4.0 1.099 0.02472 -0.170 0.024 0.765 0.943 0.792 44.442 0.422 0.404 4.5 1.131 0.02603 -0.173 0.023 0.766 0.913 0.793 43.454 0.326 0.403 5.0 1.178 0.02680 -0.176 0.004 0.767 0.904 0.794 43.942 -0.090 0.399 5.5 1.066 0.03135 -0.195 0.003 0.768 0.005 0.796 33.997 -0.057 0.433 6.0 1.102 0.03453 -0.199 0.002 0.770 0.004 0.796 31.911 0.356 0.430 6.5 1.135 0.03827 -0.203 0.002 0.771 0.003 0.798 29.646 0.370 0.429 7.0 1.163 0.04242 -0.206 0.002 0.772 0.003 0.799 27.407 0.389 0.427 7.5 1.187 0.04809 -0.210 0.002 0.773 0.002 0.800 24.681 0.413 0.427 8.0 1.207 0.05325 -0.213 0.001 0.774 0.002 0.801 22.670 0.452 0.427 8.5 1.223 0.06045 -0.217 0.001 0.775 0.002 0.803 20.223 0.518 0.428 9.0 1.234 0.06608 -0.221 0.001 0.776 0.002 0.804 18.674 0.666 0.429 9.5 1.240 0.07592 -0.224 0.001 0.778 0.001 0.807 16.330 1.383 0.431 10.0 1.240 0.08381 -0.228 0.001 0.779 0.001 0.810 14.798 -1.486 0.434 10.5 1.236 0.09179 -0.231 0.001 0.780 0.001 0.814 13.462 -0.223 0.437 11.0 1.225 0.10394 -0.235 0.001 0.780 0.001 0.820 11.787 -0.022 0.442 11.5 1.210 0.11820 -0.238 0.000 0.781 0.001 0.826 10.234 0.062 0.447 12.0 1.188 0.13194 -0.242 0.000 0.782 0.001 0.835 9.001 0.104 0.454 12.5 1.161 0.15071 -0.245 0.001 0.783 0.001 0.846 7.706 0.126 0.461 13.0 1.131 0.16919 -0.249 0.001 0.784 0.001 0.885 6.686 0.139 0.470 13.5 1.098 0.19449 -0.252 0.001 0.784 0.001 0.888 5.647 0.150 0.480 14.0 1.062 0.21340 -0.256 0.001 0.785 0.001 0.892 4.975 0.158 0.491 14.5 1.023 0.23885 -0.259 0.001 0.786 0.001 0.896 4.285 0.162 0.503 15.0 0.983 0.26762 -0.263 0.001 0.787 0.001 1.000 3.675 0.164 0.517 Name = AH 88-K-130/20 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 -0.260 0.24925 -0.046 0.737 0.003 0.981 0.004 -1.044 0.804 0.072 -14.5 -0.254 0.14676 -0.050 0.737 0.003 0.977 0.004 -1.730 0.728 0.054 -14.0 -0.246 0.20737 -0.053 0.736 0.003 0.969 0.004 -1.185 0.622 0.033 -13.5 -0.235 0.18331 -0.057 0.735 0.003 0.849 0.004 -1.284 0.548 0.009 -13.0 -0.222 0.17218 -0.060 0.735 0.003 0.807 0.004 -1.291 0.499 -0.021 -12.5 -0.207 0.15285 -0.064 0.734 0.002 0.798 0.004 -1.356 0.462 -0.058 -12.0 -0.189 0.14346 -0.067 0.733 0.002 0.791 0.004 -1.319 0.433 -0.106 -11.5 -0.169 0.12504 -0.071 0.733 0.002 0.786 0.004 -1.350 0.411 -0.170 -11.0 -0.145 0.11542 -0.074 0.732 0.002 0.781 0.004 -1.260 0.395 -0.261 -10.5 -0.120 0.10153 -0.078 0.731 0.002 0.777 0.004 -1.180 0.383 -0.400 -10.0 -0.092 0.08953 -0.082 0.731 0.002 0.773 0.003 -1.026 0.373 -0.637 -9.5 -0.062 0.08012 -0.085 0.730 0.002 0.770 0.003 -0.769 0.365 -1.132 -9.0 -0.029 0.07303 -0.089 0.729 0.002 0.767 0.003 -0.400 0.226 -2.787 -8.5 -0.360 0.06387 -0.092 0.728 0.002 0.764 0.003 -5.638 0.224 -0.006 -8.0 -0.303 0.05715 -0.096 0.728 0.002 0.761 0.003 -5.301 0.312 -0.067 -7.5 -0.244 0.05121 -0.100 0.727 0.002 0.760 0.003 -4.755 0.310 -0.159 -7.0 -0.182 0.04730 -0.103 0.726 0.002 0.757 0.003 -3.852 0.309 -0.316 -6.5 -0.119 0.04242 -0.107 0.725 0.002 0.754 0.003 -2.817 0.308 -0.644 -6.0 -0.056 0.03827 -0.110 0.725 0.002 0.751 0.003 -1.461 0.307 -1.726 -5.5 0.008 0.03453 -0.114 0.724 0.002 0.750 0.003 0.235 0.307 14.299 -5.0 0.072 0.03145 -0.118 0.723 0.002 0.748 0.003 2.296 0.307 1.881 -4.5 0.136 0.02879 -0.121 0.723 0.003 0.747 0.004 4.725 0.308 1.143 -4.0 0.199 0.02653 -0.125 0.722 0.003 0.746 0.005 7.510 0.307 0.878 -3.5 0.262 0.02492 -0.129 0.719 0.004 0.746 0.014 10.499 0.308 0.742 -3.0 0.323 0.02322 -0.132 0.716 0.012 0.746 0.017 13.915 0.420 0.659 -2.5 0.368 0.01570 -0.147 0.713 0.015 0.746 0.986 23.433 0.403 0.649 -2.0 0.428 0.01574 -0.148 0.710 0.051 0.745 0.991 27.197 0.251 0.597 -1.5 0.491 0.01517 -0.147 0.707 0.690 0.745 0.800 32.341 0.257 0.549 -1.0 0.550 0.01531 -0.149 0.705 0.750 0.744 0.779 35.934 0.294 0.521 -0.5 0.609 0.01537 -0.152 0.702 0.752 0.743 0.781 39.630 0.120 0.499 0.0 0.508 0.01860 -0.155 0.699 0.754 0.742 0.782 27.319 0.130 0.554 0.5 0.562 0.01895 -0.158 0.696 0.755 0.742 0.784 29.668 0.304 0.530 1.0 0.616 0.01933 -0.160 0.693 0.757 0.741 0.786 31.876 0.303 0.511 1.5 0.672 0.01967 -0.163 0.683 0.758 0.743 0.787 34.170 0.301 0.493 2.0 0.729 0.02004 -0.166 0.670 0.760 0.747 0.789 36.393 0.289 0.478 2.5 0.804 0.01999 -0.168 0.619 0.761 0.774 0.790 40.210 0.289 0.460 3.0 0.859 0.02048 -0.171 0.608 0.762 0.774 0.791 41.945 0.238 0.449 3.5 1.085 0.02430 -0.165 0.026 0.764 1.000 0.793 44.662 0.234 0.402 4.0 1.143 0.02257 -0.167 0.024 0.765 1.000 0.794 50.635 0.276 0.396 4.5 1.200 0.02178 -0.168 0.023 0.766 1.000 0.796 55.084 0.326 0.390 5.0 1.219 0.02402 -0.172 0.004 0.767 0.956 0.797 50.743 0.051 0.392 5.5 1.064 0.02967 -0.195 0.003 0.768 0.006 0.798 35.856 0.025 0.434 6.0 1.101 0.03239 -0.199 0.002 0.770 0.004 0.799 34.011 0.353 0.431 6.5 1.134 0.03583 -0.203 0.002 0.771 0.003 0.801 31.657 0.370 0.429 7.0 1.162 0.03958 -0.206 0.002 0.772 0.003 0.802 29.362 0.388 0.427 7.5 1.187 0.04391 -0.210 0.002 0.773 0.002 0.803 27.029 0.411 0.427 8.0 1.207 0.04833 -0.213 0.001 0.774 0.002 0.805 24.974 0.452 0.427 8.5 1.223 0.05421 -0.217 0.001 0.775 0.002 0.808 22.551 0.522 0.428 9.0 1.234 0.06040 -0.221 0.001 0.776 0.002 0.812 20.424 0.666 0.429 9.5 1.240 0.06624 -0.224 0.001 0.778 0.001 0.817 18.717 1.379 0.431 10.0 1.240 0.07574 -0.228 0.001 0.779 0.001 0.822 16.371 -1.319 0.434 10.5 1.235 0.08252 -0.231 0.001 0.780 0.001 0.829 14.968 -0.227 0.437 11.0 1.225 0.09176 -0.235 0.001 0.780 0.001 0.840 13.350 -0.025 0.442 11.5 1.209 0.10423 -0.238 0.000 0.781 0.001 0.883 11.604 0.062 0.447 12.0 1.187 0.11499 -0.242 0.000 0.782 0.001 0.888 10.326 0.104 0.454 12.5 1.161 0.12689 -0.245 0.001 0.783 0.001 0.891 9.153 0.126 0.461 13.0 1.131 0.14795 -0.249 0.001 0.784 0.001 0.895 7.644 0.139 0.470 13.5 1.098 0.15900 -0.252 0.001 0.784 0.001 1.000 6.908 0.150 0.480 14.0 1.061 0.18202 -0.256 0.001 0.785 0.001 1.000 5.831 0.158 0.491 14.5 1.023 0.20083 -0.259 0.001 0.786 0.001 1.000 5.094 0.162 0.503 15.0 0.983 0.22783 -0.263 0.001 0.787 0.001 1.000 4.316 0.164 0.517 Name = AH 88-K-130/20 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 -0.260 0.13810 -0.046 0.737 0.003 0.986 0.005 -1.883 0.810 0.072 -14.5 -0.254 0.12766 -0.050 0.737 0.003 0.985 0.004 -1.989 0.727 0.054 -14.0 -0.246 0.12288 -0.053 0.736 0.003 0.984 0.004 -1.999 0.619 0.033 -13.5 -0.235 0.16746 -0.057 0.735 0.003 0.982 0.004 -1.404 0.549 0.009 -13.0 -0.222 0.14880 -0.060 0.735 0.003 0.977 0.004 -1.494 0.499 -0.021 -12.5 -0.207 0.14165 -0.064 0.734 0.002 0.969 0.004 -1.462 0.462 -0.058 -12.0 -0.189 0.12552 -0.067 0.733 0.002 0.844 0.004 -1.508 0.433 -0.106 -11.5 -0.169 0.11742 -0.071 0.733 0.002 0.804 0.004 -1.436 0.411 -0.170 -11.0 -0.145 0.10134 -0.074 0.732 0.002 0.797 0.004 -1.435 0.396 -0.261 -10.5 -0.120 0.09030 -0.078 0.731 0.002 0.791 0.004 -1.327 0.383 -0.400 -10.0 -0.092 0.08510 -0.081 0.731 0.002 0.785 0.004 -1.077 0.373 -0.639 -9.5 -0.061 0.07423 -0.085 0.730 0.002 0.780 0.003 -0.828 0.365 -1.134 -9.0 -0.029 0.06632 -0.089 0.729 0.002 0.775 0.003 -0.440 0.226 -2.787 -8.5 -0.360 0.05846 -0.092 0.728 0.002 0.772 0.003 -6.159 0.224 -0.006 -8.0 -0.303 0.05277 -0.096 0.728 0.002 0.768 0.003 -5.742 0.312 -0.067 -7.5 -0.243 0.04848 -0.100 0.727 0.002 0.766 0.003 -5.023 0.310 -0.159 -7.0 -0.182 0.04400 -0.103 0.726 0.002 0.763 0.003 -4.140 0.309 -0.316 -6.5 -0.119 0.03963 -0.107 0.725 0.002 0.760 0.003 -3.015 0.308 -0.644 -6.0 -0.056 0.03591 -0.110 0.725 0.002 0.756 0.003 -1.557 0.307 -1.726 -5.5 0.008 0.03247 -0.114 0.724 0.002 0.755 0.003 0.250 0.307 14.299 -5.0 0.072 0.02982 -0.118 0.723 0.002 0.752 0.003 2.422 0.307 1.881 -4.5 0.136 0.02720 -0.121 0.723 0.003 0.749 0.004 5.000 0.307 1.143 -4.0 0.199 0.02513 -0.125 0.722 0.003 0.748 0.006 7.930 0.307 0.878 -3.5 0.262 0.02354 -0.129 0.719 0.004 0.749 0.016 11.115 0.308 0.742 -3.0 0.323 0.02178 -0.132 0.716 0.012 0.748 0.017 14.839 0.421 0.659 -2.5 0.368 0.01422 -0.147 0.713 0.015 0.748 0.991 25.871 0.403 0.649 -2.0 0.428 0.01463 -0.148 0.710 0.051 0.748 0.992 29.266 0.250 0.597 -1.5 0.491 0.01321 -0.147 0.707 0.690 0.748 0.808 37.127 0.256 0.549 -1.0 0.550 0.01337 -0.149 0.705 0.750 0.747 0.781 41.158 0.293 0.521 -0.5 0.609 0.01341 -0.152 0.702 0.752 0.747 0.782 45.442 0.113 0.499 0.0 0.510 0.01655 -0.155 0.699 0.754 0.746 0.784 30.843 0.124 0.553 0.5 0.564 0.01686 -0.158 0.696 0.755 0.745 0.786 33.475 0.304 0.529 1.0 0.618 0.01720 -0.160 0.693 0.757 0.744 0.788 35.951 0.302 0.509 1.5 0.675 0.01750 -0.163 0.683 0.758 0.747 0.789 38.594 0.299 0.492 2.0 0.734 0.01777 -0.166 0.670 0.760 0.753 0.791 41.279 0.285 0.476 2.5 0.815 0.01752 -0.168 0.619 0.761 0.789 0.792 46.530 0.284 0.456 3.0 0.871 0.01794 -0.171 0.608 0.762 0.790 0.793 48.532 0.239 0.446 3.5 1.085 0.02217 -0.165 0.026 0.764 1.000 0.795 48.964 0.235 0.402 4.0 1.143 0.02067 -0.167 0.024 0.765 1.000 0.796 55.294 0.276 0.396 4.5 1.200 0.01995 -0.168 0.023 0.766 1.000 0.798 60.145 0.277 0.390 5.0 1.255 0.01917 -0.170 0.004 0.767 1.000 0.799 65.495 0.055 0.385 5.5 1.061 0.02887 -0.195 0.003 0.768 0.007 0.801 36.732 0.061 0.434 6.0 1.101 0.03113 -0.199 0.002 0.770 0.004 0.802 35.369 0.349 0.431 6.5 1.134 0.03440 -0.203 0.002 0.771 0.003 0.803 32.954 0.370 0.429 7.0 1.162 0.03794 -0.206 0.002 0.772 0.003 0.805 30.623 0.388 0.427 7.5 1.186 0.04212 -0.210 0.002 0.773 0.003 0.809 28.166 0.411 0.427 8.0 1.207 0.04630 -0.213 0.001 0.774 0.002 0.814 26.065 0.452 0.427 8.5 1.222 0.05180 -0.217 0.001 0.775 0.002 0.818 23.594 0.522 0.428 9.0 1.233 0.05722 -0.221 0.001 0.776 0.002 0.824 21.550 0.666 0.429 9.5 1.239 0.06251 -0.224 0.001 0.778 0.001 0.830 19.829 1.316 0.431 10.0 1.240 0.06886 -0.228 0.001 0.779 0.001 0.841 18.006 -1.289 0.434 10.5 1.235 0.07736 -0.231 0.001 0.780 0.001 0.883 15.961 -0.214 0.437 11.0 1.225 0.08641 -0.235 0.001 0.780 0.001 0.888 14.171 -0.027 0.442 11.5 1.209 0.09586 -0.238 0.000 0.781 0.001 0.892 12.614 0.062 0.447 12.0 1.187 0.10733 -0.242 0.000 0.782 0.001 0.896 11.060 0.104 0.454 12.5 1.161 0.11598 -0.245 0.001 0.783 0.001 1.000 10.010 0.125 0.461 13.0 1.131 0.12730 -0.249 0.001 0.784 0.001 1.000 8.884 0.139 0.470 13.5 1.098 0.14602 -0.252 0.001 0.784 0.001 1.000 7.520 0.150 0.480 14.0 1.061 0.14510 -0.256 0.001 0.785 0.001 1.000 7.313 0.158 0.491 14.5 1.023 0.17976 -0.259 0.001 0.786 0.001 1.000 5.690 0.162 0.504 15.0 0.983 0.16956 -0.263 0.001 0.787 0.001 1.000 5.797 0.164 0.517