Name = AH 93-156 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 -0.563 0.19714 0.015 0.693 0.003 0.793 0.005 -2.858 0.460 0.276 -14.5 -0.548 0.18279 0.012 0.690 0.004 0.786 0.005 -3.000 0.443 0.271 -14.0 -0.531 0.16795 0.009 0.686 0.004 0.777 0.005 -3.159 0.421 0.266 -13.5 -0.511 0.15335 0.005 0.683 0.004 0.770 0.005 -3.331 0.404 0.260 -13.0 -0.488 0.13964 0.002 0.679 0.004 0.764 0.005 -3.498 0.388 0.254 -12.5 -0.464 0.12999 -0.001 0.676 0.004 0.759 0.006 -3.566 0.377 0.247 -12.0 -0.437 0.11804 -0.005 0.674 0.004 0.750 0.006 -3.702 0.370 0.240 -11.5 -0.408 0.11029 -0.008 0.671 0.005 0.747 0.006 -3.702 0.363 0.231 -11.0 -0.378 0.09952 -0.011 0.669 0.005 0.740 0.006 -3.797 0.358 0.220 -10.5 -0.346 0.09328 -0.015 0.666 0.005 0.736 0.006 -3.708 0.352 0.208 -10.0 -0.311 0.08545 -0.018 0.664 0.006 0.731 0.007 -3.644 0.347 0.192 -9.5 -0.276 0.07863 -0.021 0.660 0.006 0.728 0.008 -3.504 0.344 0.172 -9.0 -0.239 0.07275 -0.025 0.659 0.006 0.723 0.008 -3.279 0.341 0.146 -8.5 -0.200 0.06976 -0.028 0.655 0.007 0.721 0.009 -2.865 0.339 0.109 -8.0 -0.161 0.06403 -0.032 0.653 0.007 0.716 0.010 -2.513 0.339 0.053 -7.5 -0.121 0.05990 -0.035 0.651 0.008 0.710 0.010 -2.026 0.338 -0.040 -7.0 -0.081 0.05501 -0.039 0.647 0.008 0.709 0.012 -1.467 0.336 -0.230 -6.5 -0.039 0.05127 -0.042 0.645 0.009 0.705 0.013 -0.768 0.217 -0.824 -6.0 -0.296 0.04834 -0.046 0.642 0.010 0.702 0.015 -6.126 0.212 0.095 -5.5 -0.228 0.04488 -0.049 0.638 0.012 0.700 0.017 -5.079 0.303 0.033 -5.0 -0.160 0.04233 -0.053 0.636 0.014 0.695 0.020 -3.787 0.303 -0.081 -4.5 -0.093 0.04006 -0.057 0.631 0.017 0.693 0.025 -2.326 0.303 -0.357 -4.0 -0.027 0.03808 -0.060 0.629 0.021 0.689 0.034 -0.706 0.302 -1.987 -3.5 0.038 0.03668 -0.063 0.625 0.031 0.688 0.065 1.049 0.385 1.899 -3.0 0.099 0.02650 -0.077 0.621 0.047 0.685 0.891 3.724 0.364 1.032 -2.5 0.161 0.02716 -0.077 0.617 0.779 0.681 0.822 5.933 0.273 0.731 -2.0 0.223 0.02718 -0.080 0.614 0.784 0.679 0.824 8.207 0.292 0.609 -1.5 0.285 0.02723 -0.083 0.610 0.787 0.675 0.825 10.456 0.292 0.540 -1.0 0.346 0.02739 -0.085 0.607 0.791 0.673 0.827 12.635 0.292 0.496 -0.5 0.407 0.02759 -0.088 0.602 0.795 0.671 0.828 14.765 0.185 0.465 0.0 0.268 0.03282 -0.090 0.597 0.798 0.669 0.829 8.162 0.182 0.587 0.5 0.321 0.03343 -0.094 0.592 0.800 0.666 0.831 9.604 0.312 0.542 1.0 0.374 0.03408 -0.097 0.587 0.802 0.663 0.833 10.977 0.313 0.509 1.5 0.427 0.03482 -0.100 0.582 0.804 0.661 0.835 12.266 0.313 0.485 2.0 0.480 0.03558 -0.104 0.575 0.807 0.659 0.836 13.502 0.314 0.466 2.5 0.532 0.03644 -0.107 0.570 0.809 0.656 0.836 14.608 0.315 0.451 3.0 0.586 0.03730 -0.110 0.562 0.810 0.654 0.838 15.704 0.314 0.438 3.5 0.638 0.03823 -0.114 0.554 0.813 0.653 0.838 16.699 0.316 0.428 4.0 0.691 0.03924 -0.117 0.545 0.814 0.650 0.840 17.599 0.315 0.420 4.5 0.744 0.04029 -0.121 0.533 0.816 0.650 0.840 18.461 0.314 0.412 5.0 0.797 0.04138 -0.124 0.519 0.818 0.650 0.841 19.267 0.312 0.406 5.5 0.852 0.04243 -0.127 0.499 0.819 0.651 0.843 20.080 0.305 0.400 6.0 0.912 0.04327 -0.130 0.462 0.820 0.660 0.843 21.080 0.293 0.393 6.5 0.980 0.04401 -0.133 0.395 0.821 0.680 0.844 22.279 0.299 0.386 7.0 1.031 0.04542 -0.136 0.367 0.821 0.679 0.845 22.707 0.317 0.382 7.5 1.080 0.04719 -0.140 0.341 0.823 0.678 0.845 22.896 0.321 0.379 8.0 1.128 0.04907 -0.143 0.313 0.825 0.676 0.847 22.985 0.328 0.377 8.5 1.171 0.05109 -0.147 0.290 0.825 0.671 0.849 22.921 0.322 0.375 9.0 1.221 0.05301 -0.150 0.242 0.827 0.676 0.851 23.028 -0.431 0.373 9.5 1.146 0.06174 -0.164 0.004 0.829 0.017 0.851 18.566 -0.519 0.393 10.0 1.198 0.06334 -0.167 0.003 0.829 0.006 0.852 18.917 0.334 0.389 10.5 1.232 0.06647 -0.171 0.001 0.829 0.003 0.852 18.529 0.375 0.389 11.0 1.259 0.07214 -0.175 0.001 0.831 0.003 0.852 17.448 0.402 0.389 11.5 1.282 0.07899 -0.178 0.001 0.831 0.002 0.856 16.232 0.423 0.389 12.0 1.303 0.08343 -0.182 0.001 0.835 0.002 0.856 15.617 0.454 0.390 12.5 1.320 0.09391 -0.186 0.001 0.835 0.002 0.858 14.052 0.492 0.391 13.0 1.335 0.09848 -0.190 0.001 0.837 0.002 0.858 13.553 0.542 0.392 13.5 1.346 0.11017 -0.194 0.001 0.839 0.001 0.858 12.216 0.620 0.394 14.0 1.355 0.12063 -0.198 0.001 0.839 0.001 0.859 11.234 0.794 0.396 14.5 1.360 0.13164 -0.201 0.001 0.839 0.001 0.861 10.330 1.568 0.398 15.0 1.361 0.14391 -0.205 0.001 0.840 0.001 0.861 9.457 3.586 0.401 Name = AH 93-156 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 -0.563 0.15830 0.015 0.693 0.003 1.000 0.005 -3.557 0.460 0.276 -14.5 -0.548 0.14743 0.012 0.690 0.004 0.864 0.005 -3.717 0.443 0.271 -14.0 -0.530 0.13458 0.009 0.686 0.004 0.836 0.005 -3.940 0.421 0.266 -13.5 -0.510 0.12440 0.005 0.683 0.004 0.824 0.005 -4.104 0.404 0.260 -13.0 -0.488 0.11286 0.002 0.679 0.004 0.814 0.005 -4.325 0.388 0.254 -12.5 -0.463 0.10641 -0.001 0.676 0.004 0.805 0.006 -4.354 0.376 0.247 -12.0 -0.436 0.09811 -0.004 0.674 0.004 0.794 0.006 -4.448 0.370 0.240 -11.5 -0.408 0.08879 -0.008 0.671 0.005 0.787 0.006 -4.596 0.363 0.231 -11.0 -0.377 0.08484 -0.011 0.669 0.005 0.777 0.007 -4.446 0.357 0.220 -10.5 -0.345 0.07900 -0.015 0.666 0.005 0.771 0.007 -4.371 0.352 0.208 -10.0 -0.311 0.07294 -0.018 0.664 0.006 0.763 0.008 -4.261 0.347 0.192 -9.5 -0.275 0.06672 -0.021 0.660 0.006 0.759 0.008 -4.121 0.344 0.172 -9.0 -0.238 0.06194 -0.025 0.659 0.006 0.750 0.009 -3.841 0.342 0.146 -8.5 -0.200 0.05720 -0.028 0.655 0.007 0.749 0.009 -3.494 0.340 0.109 -8.0 -0.160 0.05417 -0.032 0.653 0.007 0.740 0.010 -2.962 0.338 0.052 -7.5 -0.121 0.05085 -0.035 0.651 0.008 0.735 0.011 -2.377 0.337 -0.041 -7.0 -0.080 0.04728 -0.039 0.647 0.008 0.733 0.013 -1.684 0.335 -0.236 -6.5 -0.038 0.04404 -0.042 0.645 0.009 0.728 0.014 -0.870 0.217 -0.853 -6.0 -0.296 0.04079 -0.046 0.642 0.010 0.724 0.016 -7.259 0.213 0.095 -5.5 -0.228 0.03857 -0.049 0.638 0.012 0.723 0.019 -5.910 0.302 0.033 -5.0 -0.160 0.03615 -0.053 0.636 0.014 0.716 0.022 -4.433 0.303 -0.080 -4.5 -0.093 0.03421 -0.056 0.631 0.017 0.715 0.031 -2.722 0.301 -0.356 -4.0 -0.027 0.03264 -0.060 0.629 0.021 0.710 0.062 -0.822 0.396 -1.977 -3.5 0.037 0.02055 -0.075 0.625 0.031 0.708 0.903 1.782 0.394 2.310 -3.0 0.099 0.02095 -0.078 0.621 0.047 0.706 0.910 4.706 0.267 1.039 -2.5 0.161 0.01970 -0.078 0.617 0.779 0.702 0.826 8.179 0.269 0.731 -2.0 0.223 0.01969 -0.080 0.614 0.784 0.699 0.828 11.329 0.292 0.609 -1.5 0.285 0.01972 -0.083 0.610 0.787 0.696 0.830 14.434 0.291 0.540 -1.0 0.346 0.01979 -0.085 0.607 0.791 0.693 0.831 17.487 0.291 0.496 -0.5 0.407 0.01992 -0.088 0.602 0.795 0.691 0.832 20.441 0.174 0.465 0.0 0.280 0.02446 -0.090 0.597 0.798 0.689 0.833 11.428 0.172 0.573 0.5 0.333 0.02496 -0.094 0.592 0.800 0.687 0.835 13.359 0.310 0.530 1.0 0.387 0.02549 -0.097 0.587 0.802 0.685 0.836 15.195 0.311 0.500 1.5 0.441 0.02603 -0.100 0.582 0.804 0.682 0.837 16.927 0.311 0.477 2.0 0.495 0.02664 -0.103 0.575 0.807 0.682 0.839 18.580 0.312 0.459 2.5 0.547 0.02731 -0.107 0.570 0.809 0.678 0.839 20.037 0.312 0.445 3.0 0.602 0.02793 -0.110 0.562 0.810 0.678 0.841 21.551 0.311 0.433 3.5 0.656 0.02863 -0.113 0.554 0.813 0.677 0.841 22.910 0.312 0.423 4.0 0.709 0.02937 -0.117 0.545 0.814 0.676 0.842 24.153 0.311 0.414 4.5 0.764 0.03014 -0.120 0.533 0.816 0.677 0.843 25.363 0.308 0.407 5.0 0.820 0.03087 -0.123 0.519 0.818 0.680 0.843 26.575 0.306 0.400 5.5 0.878 0.03155 -0.126 0.499 0.819 0.685 0.845 27.839 0.296 0.394 6.0 0.945 0.03204 -0.129 0.462 0.820 0.699 0.845 29.477 0.283 0.386 6.5 1.018 0.03252 -0.131 0.395 0.821 0.723 0.846 31.302 0.291 0.378 7.0 1.071 0.03369 -0.134 0.367 0.821 0.723 0.849 31.777 0.311 0.375 7.5 1.121 0.03506 -0.137 0.341 0.823 0.723 0.849 31.978 0.315 0.372 8.0 1.170 0.03654 -0.140 0.313 0.825 0.721 0.849 32.013 0.321 0.370 8.5 1.214 0.03815 -0.144 0.290 0.825 0.718 0.851 31.834 0.319 0.368 9.0 1.263 0.04003 -0.147 0.242 0.827 0.720 0.854 31.559 0.300 0.366 9.5 1.319 0.04392 -0.149 0.004 0.829 0.732 0.854 30.037 -0.020 0.363 10.0 1.187 0.05749 -0.167 0.003 0.829 0.010 0.856 20.653 0.014 0.391 10.5 1.226 0.05936 -0.171 0.001 0.829 0.005 0.856 20.660 0.357 0.389 11.0 1.256 0.06387 -0.175 0.001 0.831 0.003 0.856 19.672 0.389 0.389 11.5 1.281 0.06803 -0.178 0.001 0.831 0.003 0.858 18.830 0.418 0.389 12.0 1.302 0.07235 -0.182 0.001 0.835 0.002 0.858 17.994 0.447 0.390 12.5 1.320 0.07732 -0.186 0.001 0.835 0.002 0.861 17.067 0.492 0.391 13.0 1.333 0.08522 -0.190 0.001 0.837 0.002 0.861 15.647 0.548 0.392 13.5 1.345 0.09123 -0.194 0.001 0.839 0.002 0.859 14.746 0.605 0.394 14.0 1.355 0.10059 -0.198 0.001 0.839 0.001 0.861 13.470 0.784 0.396 14.5 1.360 0.10962 -0.201 0.001 0.839 0.001 0.865 12.402 1.565 0.398 15.0 1.361 0.11862 -0.205 0.001 0.840 0.001 0.863 11.471 3.564 0.401 Name = AH 93-156 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 -0.563 0.14192 0.015 0.693 0.003 1.000 0.005 -3.966 0.465 0.276 -14.5 -0.548 0.12742 0.012 0.690 0.004 1.000 0.005 -4.301 0.443 0.271 -14.0 -0.530 0.12197 0.009 0.686 0.004 1.000 0.005 -4.344 0.419 0.266 -13.5 -0.510 0.11344 0.005 0.683 0.004 1.000 0.005 -4.497 0.404 0.260 -13.0 -0.488 0.10244 0.002 0.679 0.004 1.000 0.006 -4.761 0.388 0.254 -12.5 -0.463 0.09630 -0.001 0.676 0.004 0.881 0.006 -4.808 0.377 0.247 -12.0 -0.436 0.08555 -0.004 0.674 0.004 0.850 0.006 -5.101 0.369 0.240 -11.5 -0.407 0.08283 -0.008 0.671 0.005 0.836 0.007 -4.919 0.363 0.231 -11.0 -0.377 0.07478 -0.011 0.669 0.005 0.817 0.007 -5.045 0.357 0.220 -10.5 -0.345 0.07314 -0.015 0.666 0.005 0.810 0.008 -4.712 0.352 0.208 -10.0 -0.311 0.06512 -0.018 0.664 0.006 0.798 0.008 -4.773 0.347 0.192 -9.5 -0.274 0.06166 -0.021 0.660 0.006 0.793 0.009 -4.449 0.343 0.172 -9.0 -0.237 0.05734 -0.025 0.659 0.006 0.782 0.009 -4.138 0.342 0.146 -8.5 -0.199 0.05298 -0.028 0.655 0.007 0.779 0.010 -3.760 0.340 0.108 -8.0 -0.160 0.04977 -0.032 0.653 0.007 0.770 0.011 -3.214 0.339 0.052 -7.5 -0.120 0.04676 -0.035 0.651 0.008 0.761 0.012 -2.575 0.337 -0.042 -7.0 -0.079 0.04336 -0.039 0.647 0.008 0.759 0.013 -1.825 0.335 -0.239 -6.5 -0.038 0.04046 -0.042 0.645 0.009 0.750 0.014 -0.934 0.217 -0.868 -6.0 -0.296 0.03804 -0.046 0.642 0.010 0.749 0.017 -7.784 0.213 0.095 -5.5 -0.228 0.03583 -0.049 0.638 0.012 0.745 0.022 -6.360 0.302 0.034 -5.0 -0.160 0.03359 -0.053 0.636 0.014 0.736 0.026 -4.770 0.301 -0.080 -4.5 -0.093 0.03191 -0.056 0.631 0.017 0.735 0.046 -2.915 0.380 -0.354 -4.0 -0.000 0.01844 -0.074 0.629 0.021 0.730 0.908 -0.025 0.403 0.250 -3.5 0.037 0.01879 -0.076 0.625 0.031 0.729 0.918 1.947 0.299 2.328 -3.0 0.098 0.01912 -0.078 0.621 0.047 0.727 0.928 5.150 0.263 1.046 -2.5 0.161 0.01638 -0.078 0.617 0.779 0.721 0.829 9.835 0.264 0.732 -2.0 0.223 0.01638 -0.080 0.614 0.784 0.719 0.831 13.612 0.291 0.610 -1.5 0.285 0.01639 -0.083 0.610 0.787 0.715 0.833 17.371 0.291 0.541 -1.0 0.346 0.01646 -0.085 0.607 0.791 0.712 0.835 21.031 0.291 0.496 -0.5 0.407 0.01659 -0.088 0.602 0.795 0.710 0.836 24.553 0.157 0.466 0.0 0.292 0.02050 -0.090 0.597 0.798 0.708 0.836 14.217 0.158 0.560 0.5 0.346 0.02094 -0.093 0.592 0.800 0.706 0.838 16.515 0.308 0.520 1.0 0.400 0.02139 -0.097 0.587 0.802 0.704 0.839 18.699 0.308 0.491 1.5 0.454 0.02187 -0.100 0.582 0.804 0.703 0.840 20.759 0.309 0.470 2.0 0.508 0.02235 -0.103 0.575 0.807 0.701 0.841 22.751 0.310 0.453 2.5 0.561 0.02295 -0.106 0.570 0.809 0.698 0.842 24.458 0.309 0.439 3.0 0.617 0.02345 -0.109 0.562 0.810 0.699 0.843 26.298 0.308 0.427 3.5 0.672 0.02404 -0.113 0.554 0.813 0.699 0.843 27.944 0.309 0.418 4.0 0.726 0.02464 -0.116 0.545 0.814 0.698 0.845 29.459 0.308 0.410 4.5 0.782 0.02524 -0.119 0.533 0.816 0.700 0.846 30.978 0.305 0.402 5.0 0.840 0.02581 -0.122 0.519 0.818 0.704 0.846 32.524 0.301 0.395 5.5 0.900 0.02636 -0.125 0.499 0.819 0.710 0.848 34.128 0.292 0.389 6.0 0.968 0.02674 -0.127 0.462 0.820 0.726 0.848 36.206 0.281 0.382 6.5 1.042 0.02728 -0.129 0.395 0.821 0.748 0.849 38.181 0.289 0.374 7.0 1.095 0.02840 -0.132 0.367 0.821 0.749 0.851 38.541 0.310 0.371 7.5 1.144 0.02961 -0.135 0.341 0.823 0.747 0.851 38.656 0.315 0.368 8.0 1.193 0.03100 -0.139 0.313 0.825 0.745 0.851 38.486 0.320 0.366 8.5 1.238 0.03254 -0.142 0.290 0.825 0.742 0.854 38.041 0.320 0.365 9.0 1.285 0.03443 -0.145 0.242 0.827 0.742 0.856 37.315 0.318 0.363 9.5 1.329 0.04019 -0.148 0.004 0.829 0.741 0.856 33.068 0.337 0.362 10.0 1.363 0.04215 -0.152 0.003 0.829 0.733 0.858 32.349 0.051 0.361 10.5 1.214 0.05747 -0.171 0.001 0.829 0.011 0.858 21.119 0.040 0.391 11.0 1.255 0.05892 -0.175 0.001 0.831 0.004 0.858 21.305 0.361 0.389 11.5 1.280 0.06313 -0.178 0.001 0.831 0.003 0.861 20.271 0.419 0.389 12.0 1.301 0.06741 -0.182 0.001 0.835 0.003 0.861 19.294 0.447 0.390 12.5 1.319 0.07223 -0.186 0.001 0.835 0.002 0.863 18.253 0.482 0.391 13.0 1.333 0.07643 -0.190 0.001 0.837 0.002 0.863 17.448 0.535 0.392 13.5 1.345 0.08203 -0.194 0.001 0.839 0.002 0.861 16.400 0.610 0.394 14.0 1.355 0.09206 -0.198 0.001 0.839 0.001 0.865 14.714 0.784 0.396 14.5 1.360 0.09722 -0.201 0.001 0.839 0.001 0.866 13.983 1.498 0.398 15.0 1.361 0.10428 -0.205 0.001 0.840 0.001 0.866 13.049 3.564 0.401 Name = AH 93-156 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 -0.563 0.12595 0.015 0.693 0.003 1.000 0.005 -4.469 0.460 0.276 -14.5 -0.548 0.12001 0.012 0.690 0.004 1.000 0.005 -4.564 0.441 0.271 -14.0 -0.530 0.11401 0.009 0.686 0.004 1.000 0.006 -4.645 0.421 0.266 -13.5 -0.510 0.10284 0.005 0.683 0.004 1.000 0.005 -4.961 0.404 0.260 -13.0 -0.488 0.09606 0.002 0.679 0.004 1.000 0.006 -5.075 0.387 0.254 -12.5 -0.463 0.09021 -0.001 0.676 0.004 1.000 0.006 -5.129 0.376 0.247 -12.0 -0.436 0.08360 -0.004 0.674 0.004 1.000 0.007 -5.213 0.370 0.240 -11.5 -0.407 0.07660 -0.008 0.671 0.005 1.000 0.007 -5.319 0.363 0.231 -11.0 -0.377 0.07195 -0.011 0.669 0.005 0.887 0.008 -5.234 0.357 0.220 -10.5 -0.345 0.06673 -0.015 0.666 0.005 0.866 0.008 -5.165 0.352 0.208 -10.0 -0.310 0.06247 -0.018 0.664 0.006 0.840 0.008 -4.965 0.346 0.192 -9.5 -0.274 0.05876 -0.021 0.660 0.006 0.831 0.009 -4.658 0.343 0.172 -9.0 -0.237 0.05469 -0.025 0.659 0.006 0.815 0.010 -4.327 0.342 0.145 -8.5 -0.199 0.05052 -0.028 0.655 0.007 0.812 0.010 -3.934 0.340 0.108 -8.0 -0.159 0.04712 -0.032 0.653 0.007 0.800 0.012 -3.384 0.339 0.051 -7.5 -0.120 0.04433 -0.035 0.651 0.008 0.789 0.012 -2.705 0.336 -0.044 -7.0 -0.078 0.04148 -0.039 0.647 0.008 0.786 0.014 -1.883 0.335 -0.245 -6.5 -0.037 0.03872 -0.042 0.645 0.009 0.777 0.016 -0.949 0.218 -0.900 -6.0 -0.296 0.03640 -0.046 0.642 0.010 0.773 0.020 -8.133 0.213 0.096 -5.5 -0.228 0.03415 -0.049 0.638 0.012 0.770 0.024 -6.672 0.302 0.034 -5.0 -0.160 0.03226 -0.053 0.636 0.014 0.761 0.034 -4.962 0.383 -0.079 -4.5 -0.060 0.01712 -0.072 0.631 0.017 0.757 0.908 -3.505 0.389 -0.943 -4.0 -0.006 0.01756 -0.074 0.629 0.021 0.752 0.920 -0.347 0.304 -11.926 -3.5 0.037 0.01785 -0.077 0.625 0.031 0.749 0.935 2.047 0.313 2.350 -3.0 0.098 0.01864 -0.081 0.621 0.047 0.746 0.992 5.265 0.258 1.073 -2.5 0.161 0.01443 -0.078 0.617 0.779 0.740 0.833 11.160 0.246 0.733 -2.0 0.223 0.01441 -0.080 0.614 0.784 0.737 0.835 15.469 0.291 0.610 -1.5 0.285 0.01442 -0.083 0.610 0.787 0.733 0.836 19.737 0.291 0.541 -1.0 0.346 0.01449 -0.085 0.607 0.791 0.730 0.837 23.886 0.291 0.496 -0.5 0.407 0.01458 -0.088 0.602 0.795 0.728 0.837 27.937 0.134 0.466 0.0 0.303 0.01797 -0.090 0.597 0.798 0.726 0.838 16.846 0.138 0.548 0.5 0.357 0.01836 -0.093 0.592 0.800 0.724 0.839 19.463 0.306 0.511 1.0 0.412 0.01876 -0.096 0.587 0.802 0.722 0.841 21.951 0.307 0.484 1.5 0.466 0.01918 -0.100 0.582 0.804 0.720 0.842 24.308 0.307 0.463 2.0 0.521 0.01961 -0.103 0.575 0.807 0.720 0.842 26.590 0.308 0.447 2.5 0.575 0.02016 -0.106 0.570 0.809 0.717 0.843 28.513 0.308 0.434 3.0 0.631 0.02058 -0.109 0.562 0.810 0.717 0.845 30.633 0.306 0.423 3.5 0.686 0.02108 -0.112 0.554 0.813 0.717 0.845 32.527 0.307 0.413 4.0 0.741 0.02163 -0.115 0.545 0.814 0.717 0.847 34.257 0.305 0.406 4.5 0.798 0.02215 -0.118 0.533 0.816 0.720 0.848 36.023 0.302 0.398 5.0 0.856 0.02264 -0.121 0.519 0.818 0.724 0.848 37.827 0.298 0.392 5.5 0.917 0.02311 -0.124 0.499 0.819 0.731 0.849 39.697 0.289 0.385 6.0 0.987 0.02348 -0.126 0.462 0.820 0.747 0.850 42.032 0.280 0.378 6.5 1.059 0.02413 -0.128 0.395 0.821 0.767 0.850 43.880 0.289 0.371 7.0 1.111 0.02522 -0.131 0.367 0.821 0.766 0.854 44.069 0.310 0.368 7.5 1.161 0.02637 -0.134 0.341 0.823 0.764 0.854 44.014 0.314 0.366 8.0 1.209 0.02771 -0.138 0.313 0.825 0.762 0.854 43.623 0.320 0.364 8.5 1.253 0.02912 -0.141 0.290 0.825 0.757 0.856 43.048 0.322 0.362 9.0 1.299 0.03103 -0.144 0.242 0.827 0.756 0.858 41.854 0.318 0.361 9.5 1.344 0.03729 -0.147 0.004 0.829 0.756 0.858 36.032 0.347 0.359 10.0 1.373 0.03959 -0.151 0.003 0.829 0.742 0.861 34.668 0.384 0.360 10.5 1.403 0.04162 -0.155 0.001 0.829 0.733 0.861 33.719 0.058 0.360 11.0 1.250 0.05757 -0.175 0.001 0.831 0.006 0.859 21.715 0.063 0.390 11.5 1.278 0.06141 -0.179 0.001 0.831 0.004 0.863 20.803 0.404 0.390 12.0 1.299 0.06436 -0.182 0.001 0.835 0.003 0.863 20.190 0.442 0.390 12.5 1.317 0.06913 -0.186 0.001 0.835 0.003 0.865 19.056 0.482 0.391 13.0 1.332 0.07333 -0.190 0.001 0.837 0.002 0.865 18.169 0.534 0.393 13.5 1.344 0.07917 -0.194 0.001 0.839 0.002 0.863 16.979 0.590 0.394 14.0 1.355 0.08500 -0.198 0.001 0.839 0.001 0.866 15.937 0.754 0.396 14.5 1.359 0.09229 -0.201 0.001 0.839 0.001 0.868 14.728 1.561 0.398 15.0 1.360 0.09864 -0.205 0.001 0.840 0.001 0.868 13.791 3.542 0.401