Name = GOE 366 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 -0.147 0.30192 -0.069 0.765 0.015 0.841 0.016 -0.488 0.387 -0.215 -14.5 -0.125 0.26440 -0.072 0.738 0.015 0.847 0.016 -0.472 0.384 -0.324 -14.0 -0.101 0.26226 -0.075 0.726 0.015 0.857 0.016 -0.384 0.377 -0.492 -13.5 -0.075 0.23244 -0.078 0.704 0.015 0.857 0.016 -0.323 0.372 -0.789 -13.0 -0.048 0.23004 -0.081 0.693 0.015 0.857 0.016 -0.209 0.367 -1.442 -12.5 -0.020 0.17310 -0.084 0.682 0.016 0.852 0.017 -0.116 0.235 -3.950 -12.0 -0.496 0.17070 -0.088 0.676 0.016 0.847 0.017 -2.905 0.234 0.073 -11.5 -0.446 0.15314 -0.091 0.671 0.016 0.847 0.017 -2.910 0.316 0.046 -11.0 -0.393 0.15654 -0.095 0.671 0.014 0.847 0.015 -2.513 0.314 0.010 -10.5 -0.339 0.15657 -0.098 0.671 0.014 0.841 0.015 -2.167 0.312 -0.039 -10.0 -0.284 0.13715 -0.101 0.660 0.014 0.831 0.015 -2.067 0.311 -0.108 -9.5 -0.226 0.13393 -0.105 0.654 0.014 0.831 0.015 -1.689 0.310 -0.213 -9.0 -0.168 0.10562 -0.108 0.654 0.015 0.820 0.016 -1.587 0.309 -0.396 -8.5 -0.108 0.10287 -0.112 0.648 0.015 0.820 0.016 -1.050 0.309 -0.786 -8.0 -0.047 0.09243 -0.115 0.648 0.015 0.810 0.016 -0.513 0.309 -2.187 -7.5 0.014 0.09080 -0.119 0.645 0.015 0.814 0.016 0.153 0.309 8.797 -7.0 0.076 0.08383 -0.123 0.641 0.015 0.810 0.015 0.904 0.309 1.870 -6.5 0.138 0.07836 -0.126 0.641 0.015 0.795 0.015 1.761 0.309 1.166 -6.0 0.200 0.07448 -0.130 0.637 0.015 0.780 0.015 2.690 0.310 0.900 -5.5 0.263 0.06930 -0.134 0.633 0.015 0.764 0.015 3.791 0.310 0.760 -5.0 0.325 0.06407 -0.138 0.629 0.015 0.749 0.015 5.071 0.311 0.674 -4.5 0.387 0.05885 -0.141 0.625 0.015 0.737 0.015 6.571 0.312 0.616 -4.0 0.448 0.05556 -0.145 0.621 0.015 0.726 0.016 8.065 0.313 0.574 -3.5 0.509 0.05282 -0.149 0.621 0.014 0.695 0.015 9.634 0.314 0.543 -3.0 0.569 0.04982 -0.153 0.617 0.014 0.695 0.015 11.419 0.315 0.519 -2.5 0.628 0.04656 -0.157 0.614 0.014 0.687 0.015 13.494 0.317 0.500 -2.0 0.687 0.04416 -0.161 0.486 0.014 0.829 0.015 15.549 0.318 0.484 -1.5 0.744 0.04142 -0.165 0.462 0.014 0.821 0.015 17.963 0.320 0.472 -1.0 0.800 0.04018 -0.169 0.438 0.014 0.825 0.015 19.923 0.322 0.461 -0.5 0.856 0.03752 -0.173 0.418 0.014 0.818 0.016 22.809 -0.058 0.452 0.0 0.774 0.03505 -0.177 0.394 0.015 0.818 0.016 22.092 0.014 0.478 0.5 0.826 0.03572 -0.180 0.382 0.015 0.810 0.016 23.129 0.310 0.468 1.0 0.874 0.03569 -0.183 0.370 0.015 0.799 0.016 24.499 0.322 0.459 1.5 0.916 0.03749 -0.186 0.362 0.015 0.776 0.016 24.423 0.339 0.453 2.0 0.953 0.03881 -0.190 0.354 0.015 0.749 0.017 24.564 0.347 0.449 2.5 0.992 0.04111 -0.194 0.346 0.016 0.726 0.017 24.143 0.355 0.445 3.0 1.028 0.04246 -0.198 0.338 0.016 0.699 0.017 24.212 0.351 0.442 3.5 1.072 0.04414 -0.202 0.330 0.016 0.683 0.018 24.289 0.338 0.438 4.0 1.118 0.04718 -0.206 0.322 0.017 0.672 0.020 23.701 0.353 0.434 4.5 1.154 0.05306 -0.210 0.316 0.928 0.646 0.951 21.752 0.365 0.432 5.0 1.195 0.05517 -0.214 0.310 0.929 0.629 0.953 21.665 0.361 0.429 5.5 1.234 0.05890 -0.219 0.306 0.934 0.610 0.954 20.948 0.358 0.427 6.0 1.277 0.06125 -0.223 0.290 0.939 0.598 0.954 20.857 0.398 0.425 6.5 1.302 0.06543 -0.229 0.278 0.947 0.552 0.954 19.894 0.567 0.426 7.0 1.315 0.06984 -0.235 0.270 0.953 0.490 0.954 18.827 0.425 0.429 7.5 1.362 0.07280 -0.240 0.258 0.953 0.486 0.955 18.708 0.373 0.426 8.0 1.394 0.07784 -0.245 0.254 0.953 0.454 0.955 17.905 0.393 0.426 8.5 1.433 0.08168 -0.250 0.246 0.953 0.438 0.955 17.542 0.391 0.424 9.0 1.464 0.08608 -0.255 0.241 0.951 0.410 0.953 17.012 0.386 0.424 9.5 1.505 0.09033 -0.260 0.233 0.951 0.400 0.953 16.660 0.240 0.422 10.0 1.730 0.07998 -0.252 0.099 0.952 0.648 0.953 21.626 0.242 0.396 10.5 1.762 0.08288 -0.258 0.094 0.952 0.628 0.953 21.256 0.422 0.396 11.0 1.792 0.08865 -0.263 0.091 0.957 0.608 0.959 20.211 0.576 0.397 11.5 1.800 0.09606 -0.270 0.089 0.952 0.561 0.954 18.741 1.287 0.400 12.0 1.806 0.10139 -0.277 0.084 0.957 0.511 0.959 17.808 -0.193 0.404 12.5 1.762 0.12514 -0.287 0.076 0.957 0.385 0.959 14.082 0.623 0.413 13.0 1.838 0.11505 -0.289 0.079 0.958 0.440 0.959 15.978 0.349 0.407 13.5 1.847 0.12430 -0.295 0.076 0.958 0.403 0.959 14.861 0.724 0.410 14.0 1.862 0.13232 -0.301 0.074 0.958 0.372 0.959 14.075 0.475 0.412 14.5 1.892 0.13646 -0.305 0.067 0.958 0.370 0.959 13.866 0.478 0.411 15.0 1.906 0.14403 -0.311 0.060 0.958 0.344 0.959 13.230 0.645 0.413 Name = GOE 366 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 -0.147 0.21779 -0.069 0.765 0.015 0.857 0.016 -0.677 0.388 -0.215 -14.5 -0.125 0.20879 -0.072 0.738 0.015 0.868 0.016 -0.599 0.384 -0.323 -14.0 -0.101 0.18891 -0.075 0.726 0.015 0.884 0.016 -0.533 0.377 -0.492 -13.5 -0.075 0.18759 -0.078 0.704 0.015 0.889 0.016 -0.401 0.372 -0.788 -13.0 -0.048 0.16905 -0.081 0.693 0.015 0.894 0.016 -0.284 0.367 -1.442 -12.5 -0.020 0.14193 -0.084 0.682 0.016 0.884 0.017 -0.142 0.235 -3.928 -12.0 -0.496 0.12977 -0.088 0.676 0.016 0.884 0.017 -3.822 0.234 0.073 -11.5 -0.446 0.12751 -0.091 0.671 0.016 0.878 0.017 -3.495 0.316 0.046 -11.0 -0.393 0.13055 -0.095 0.671 0.014 0.884 0.015 -3.013 0.314 0.010 -10.5 -0.339 0.11922 -0.098 0.671 0.014 0.878 0.015 -2.846 0.312 -0.039 -10.0 -0.284 0.11636 -0.101 0.660 0.014 0.868 0.015 -2.436 0.311 -0.108 -9.5 -0.226 0.10369 -0.105 0.654 0.014 0.868 0.015 -2.182 0.310 -0.213 -9.0 -0.168 0.09058 -0.108 0.654 0.015 0.857 0.016 -1.851 0.309 -0.396 -8.5 -0.108 0.08184 -0.112 0.648 0.015 0.857 0.016 -1.319 0.309 -0.786 -8.0 -0.047 0.07935 -0.115 0.648 0.015 0.847 0.016 -0.597 0.309 -2.187 -7.5 0.014 0.07226 -0.119 0.645 0.015 0.851 0.016 0.193 0.309 8.797 -7.0 0.076 0.06960 -0.123 0.641 0.015 0.847 0.015 1.089 0.309 1.870 -6.5 0.138 0.06525 -0.126 0.641 0.015 0.836 0.015 2.115 0.309 1.166 -6.0 0.200 0.05993 -0.130 0.637 0.015 0.836 0.015 3.343 0.310 0.900 -5.5 0.263 0.05626 -0.134 0.633 0.015 0.829 0.015 4.669 0.310 0.760 -5.0 0.325 0.05237 -0.138 0.629 0.015 0.825 0.015 6.203 0.311 0.674 -4.5 0.387 0.04882 -0.141 0.625 0.015 0.818 0.016 7.921 0.312 0.616 -4.0 0.448 0.04516 -0.145 0.621 0.015 0.814 0.016 9.923 0.313 0.574 -3.5 0.509 0.04301 -0.149 0.621 0.014 0.795 0.015 11.833 0.314 0.543 -3.0 0.569 0.04011 -0.153 0.617 0.014 0.784 0.015 14.185 0.315 0.519 -2.5 0.628 0.03765 -0.157 0.614 0.014 0.764 0.015 16.686 0.317 0.500 -2.0 0.687 0.03589 -0.161 0.486 0.014 0.881 0.015 19.132 0.318 0.484 -1.5 0.744 0.03399 -0.165 0.462 0.014 0.877 0.015 21.891 0.320 0.472 -1.0 0.800 0.03237 -0.169 0.438 0.014 0.881 0.016 24.726 0.322 0.461 -0.5 0.856 0.03079 -0.173 0.418 0.014 0.877 0.016 27.794 0.877 0.452 0.0 0.813 0.02582 -0.177 0.394 0.015 0.873 0.016 31.498 0.752 0.468 0.5 0.869 0.02655 -0.180 0.382 0.015 0.870 0.016 32.728 0.298 0.457 1.0 0.924 0.02764 -0.182 0.370 0.015 0.866 0.016 33.429 0.301 0.447 1.5 0.976 0.02839 -0.185 0.362 0.015 0.859 0.017 34.370 0.305 0.440 2.0 1.027 0.02945 -0.188 0.354 0.015 0.851 0.017 34.892 0.310 0.433 2.5 1.076 0.02926 -0.191 0.346 0.016 0.840 0.017 36.763 0.312 0.428 3.0 1.127 0.03076 -0.194 0.338 0.016 0.832 0.018 36.628 0.312 0.422 3.5 1.177 0.03259 -0.197 0.330 0.016 0.825 0.019 36.128 0.318 0.418 4.0 1.224 0.03305 -0.201 0.322 0.017 0.814 0.021 37.042 0.332 0.414 4.5 1.266 0.03772 -0.205 0.316 0.928 0.797 0.951 33.556 0.342 0.412 5.0 1.309 0.03944 -0.208 0.310 0.929 0.780 0.954 33.176 0.362 0.409 5.5 1.342 0.04155 -0.213 0.306 0.934 0.753 0.954 32.306 0.352 0.409 6.0 1.391 0.04298 -0.217 0.290 0.939 0.745 0.954 32.362 0.340 0.406 6.5 1.433 0.04476 -0.221 0.278 0.947 0.729 0.954 32.003 0.363 0.404 7.0 1.470 0.04764 -0.226 0.270 0.953 0.710 0.954 30.855 0.361 0.404 7.5 1.513 0.04937 -0.230 0.258 0.953 0.699 0.955 30.646 0.372 0.402 8.0 1.547 0.05255 -0.235 0.254 0.953 0.675 0.955 29.439 0.384 0.402 8.5 1.586 0.05456 -0.240 0.246 0.953 0.660 0.955 29.067 0.387 0.401 9.0 1.619 0.05873 -0.245 0.241 0.951 0.638 0.953 27.565 0.392 0.401 9.5 1.657 0.06148 -0.250 0.233 0.951 0.623 0.953 26.946 0.271 0.401 10.0 1.778 0.06229 -0.248 0.099 0.952 0.701 0.953 28.537 0.269 0.390 10.5 1.817 0.06636 -0.253 0.094 0.952 0.689 0.953 27.383 0.378 0.389 11.0 1.853 0.06888 -0.258 0.091 0.957 0.673 0.959 26.905 0.393 0.389 11.5 1.888 0.07388 -0.263 0.089 0.952 0.658 0.954 25.551 0.401 0.389 12.0 1.921 0.07826 -0.268 0.084 0.957 0.643 0.959 24.544 -0.565 0.390 12.5 1.867 0.09462 -0.280 0.076 0.957 0.531 0.959 19.728 0.482 0.400 13.0 1.969 0.08664 -0.279 0.079 0.958 0.603 0.959 22.729 0.315 0.392 13.5 1.969 0.09335 -0.287 0.076 0.958 0.558 0.959 21.090 -1.666 0.396 14.0 1.961 0.10044 -0.295 0.074 0.958 0.508 0.959 19.529 1.092 0.400 14.5 1.984 0.10446 -0.300 0.067 0.958 0.496 0.959 18.992 0.533 0.401 15.0 1.999 0.11216 -0.305 0.060 0.958 0.475 0.959 17.823 0.619 0.403 Name = GOE 366 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 -0.148 0.19700 -0.069 0.765 0.015 0.873 0.016 -0.749 0.388 -0.214 -14.5 -0.125 0.18687 -0.072 0.738 0.015 0.889 0.016 -0.669 0.384 -0.323 -14.0 -0.101 0.17053 -0.075 0.726 0.015 0.905 0.016 -0.591 0.377 -0.491 -13.5 -0.075 0.15594 -0.078 0.704 0.015 0.910 0.016 -0.482 0.372 -0.788 -13.0 -0.048 0.15474 -0.081 0.693 0.015 0.913 0.016 -0.311 0.367 -1.438 -12.5 -0.020 0.12094 -0.084 0.682 0.016 0.908 0.017 -0.167 0.235 -3.928 -12.0 -0.496 0.11944 -0.088 0.676 0.016 0.905 0.017 -4.152 0.234 0.073 -11.5 -0.446 0.10961 -0.091 0.671 0.016 0.905 0.017 -4.066 0.316 0.046 -11.0 -0.393 0.11136 -0.095 0.671 0.014 0.910 0.015 -3.533 0.314 0.010 -10.5 -0.339 0.10284 -0.098 0.671 0.014 0.905 0.015 -3.299 0.312 -0.039 -10.0 -0.284 0.10002 -0.101 0.660 0.014 0.894 0.015 -2.834 0.311 -0.108 -9.5 -0.226 0.09031 -0.105 0.654 0.014 0.894 0.015 -2.505 0.310 -0.213 -9.0 -0.168 0.07929 -0.108 0.654 0.015 0.884 0.016 -2.114 0.309 -0.396 -8.5 -0.108 0.07236 -0.112 0.648 0.015 0.884 0.016 -1.492 0.309 -0.786 -8.0 -0.047 0.06943 -0.115 0.648 0.015 0.873 0.016 -0.682 0.309 -2.187 -7.5 0.014 0.06379 -0.119 0.645 0.015 0.877 0.016 0.218 0.309 8.797 -7.0 0.076 0.06180 -0.123 0.641 0.015 0.877 0.015 1.226 0.309 1.870 -6.5 0.138 0.05802 -0.126 0.641 0.015 0.866 0.015 2.378 0.309 1.166 -6.0 0.200 0.05486 -0.130 0.637 0.015 0.866 0.016 3.652 0.310 0.900 -5.5 0.263 0.05033 -0.134 0.633 0.015 0.859 0.015 5.220 0.310 0.760 -5.0 0.325 0.04784 -0.138 0.629 0.015 0.855 0.016 6.791 0.311 0.674 -4.5 0.387 0.04416 -0.141 0.625 0.015 0.851 0.016 8.757 0.312 0.616 -4.0 0.448 0.04099 -0.145 0.621 0.015 0.844 0.016 10.931 0.313 0.574 -3.5 0.509 0.03892 -0.149 0.621 0.014 0.829 0.015 13.075 0.314 0.543 -3.0 0.569 0.03611 -0.153 0.617 0.014 0.829 0.015 15.758 0.315 0.519 -2.5 0.628 0.03422 -0.157 0.614 0.014 0.825 0.015 18.360 0.317 0.500 -2.0 0.687 0.03271 -0.161 0.486 0.014 0.923 0.015 20.989 0.318 0.484 -1.5 0.744 0.03055 -0.165 0.462 0.014 0.919 0.015 24.358 0.320 0.472 -1.0 0.800 0.02868 -0.169 0.438 0.014 0.919 0.016 27.905 0.322 0.461 -0.5 0.856 0.02702 -0.173 0.418 0.014 0.915 0.016 31.673 0.453 0.452 0.0 0.840 0.02259 -0.177 0.394 0.015 0.911 0.016 37.190 0.437 0.461 0.5 0.890 0.02317 -0.179 0.382 0.015 0.899 0.016 38.438 0.297 0.451 1.0 0.946 0.02387 -0.182 0.370 0.015 0.896 0.016 39.634 0.298 0.442 1.5 0.998 0.02396 -0.185 0.362 0.015 0.888 0.017 41.675 0.301 0.435 2.0 1.051 0.02422 -0.187 0.354 0.015 0.881 0.017 43.372 0.301 0.428 2.5 1.106 0.02583 -0.190 0.346 0.016 0.877 0.017 42.801 0.303 0.422 3.0 1.157 0.02640 -0.193 0.338 0.016 0.870 0.018 43.826 0.308 0.417 3.5 1.209 0.02715 -0.196 0.330 0.016 0.862 0.019 44.521 0.310 0.412 4.0 1.260 0.02805 -0.199 0.322 0.017 0.855 0.021 44.911 0.314 0.408 4.5 1.309 0.03194 -0.202 0.316 0.928 0.846 0.951 40.971 0.318 0.405 5.0 1.357 0.03230 -0.206 0.310 0.929 0.836 0.954 42.020 0.324 0.402 5.5 1.404 0.03344 -0.209 0.306 0.934 0.825 0.954 41.985 0.319 0.399 6.0 1.457 0.03536 -0.213 0.290 0.939 0.821 0.954 41.206 0.317 0.396 6.5 1.506 0.03688 -0.216 0.278 0.947 0.814 0.954 40.834 0.324 0.394 7.0 1.555 0.03870 -0.220 0.270 0.953 0.806 0.954 40.170 0.332 0.391 7.5 1.599 0.04067 -0.224 0.258 0.953 0.795 0.955 39.311 0.384 0.390 8.0 1.626 0.04242 -0.229 0.254 0.953 0.764 0.955 38.324 0.415 0.391 8.5 1.662 0.04476 -0.234 0.246 0.953 0.745 0.955 37.127 0.412 0.391 9.0 1.690 0.04896 -0.240 0.241 0.951 0.718 0.953 34.512 0.423 0.392 9.5 1.723 0.05078 -0.245 0.233 0.951 0.699 0.953 33.937 0.290 0.392 10.0 1.819 0.05576 -0.245 0.099 0.952 0.743 0.953 32.613 0.292 0.385 10.5 1.851 0.05877 -0.250 0.094 0.952 0.723 0.953 31.501 0.417 0.385 11.0 1.882 0.06152 -0.256 0.091 0.957 0.704 0.959 30.590 0.400 0.386 11.5 1.919 0.06595 -0.260 0.089 0.952 0.691 0.954 29.102 0.390 0.386 12.0 1.953 0.06789 -0.265 0.084 0.957 0.676 0.959 28.763 0.725 0.386 12.5 1.948 0.07946 -0.274 0.076 0.957 0.623 0.959 24.509 0.425 0.391 13.0 2.012 0.07599 -0.276 0.079 0.958 0.646 0.959 26.484 0.337 0.387 13.5 2.034 0.07991 -0.281 0.076 0.958 0.628 0.959 25.455 0.547 0.388 14.0 2.050 0.08340 -0.287 0.074 0.958 0.608 0.959 24.586 0.536 0.390 14.5 2.072 0.08880 -0.292 0.067 0.958 0.596 0.959 23.336 0.799 0.391 15.0 2.073 0.09539 -0.299 0.060 0.958 0.561 0.959 21.730 18.101 0.394 Name = GOE 366 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 -0.148 0.17180 -0.069 0.765 0.015 0.884 0.016 -0.859 0.388 -0.214 -14.5 -0.125 0.16129 -0.072 0.738 0.015 0.905 0.016 -0.775 0.384 -0.323 -14.0 -0.101 0.14890 -0.075 0.726 0.015 0.916 0.016 -0.677 0.377 -0.491 -13.5 -0.075 0.14840 -0.078 0.704 0.015 0.924 0.016 -0.507 0.372 -0.786 -13.0 -0.048 0.13617 -0.081 0.693 0.015 0.927 0.016 -0.353 0.367 -1.438 -12.5 -0.020 0.11539 -0.084 0.682 0.016 0.922 0.017 -0.176 0.235 -3.906 -12.0 -0.496 0.10704 -0.088 0.676 0.016 0.922 0.017 -4.633 0.234 0.073 -11.5 -0.446 0.09904 -0.091 0.671 0.016 0.922 0.017 -4.500 0.316 0.046 -11.0 -0.393 0.10762 -0.094 0.671 0.014 0.927 0.016 -3.655 0.314 0.010 -10.5 -0.339 0.09961 -0.098 0.671 0.014 0.922 0.015 -3.406 0.313 -0.039 -10.0 -0.284 0.09059 -0.101 0.660 0.014 0.916 0.015 -3.130 0.311 -0.108 -9.5 -0.226 0.08250 -0.105 0.654 0.014 0.916 0.015 -2.742 0.310 -0.213 -9.0 -0.168 0.07316 -0.108 0.654 0.015 0.911 0.016 -2.291 0.309 -0.396 -8.5 -0.108 0.06726 -0.112 0.648 0.015 0.911 0.016 -1.605 0.309 -0.786 -8.0 -0.047 0.06415 -0.115 0.648 0.015 0.899 0.016 -0.739 0.309 -2.187 -7.5 0.014 0.05933 -0.119 0.645 0.015 0.903 0.016 0.235 0.309 8.797 -7.0 0.076 0.05859 -0.123 0.641 0.015 0.899 0.016 1.294 0.309 1.870 -6.5 0.138 0.05493 -0.126 0.641 0.015 0.888 0.016 2.512 0.309 1.166 -6.0 0.200 0.05048 -0.130 0.637 0.015 0.888 0.016 3.969 0.310 0.900 -5.5 0.263 0.04654 -0.134 0.633 0.015 0.881 0.015 5.645 0.310 0.760 -5.0 0.325 0.04406 -0.138 0.629 0.015 0.877 0.016 7.373 0.311 0.674 -4.5 0.387 0.04136 -0.141 0.625 0.015 0.873 0.016 9.349 0.312 0.616 -4.0 0.448 0.03818 -0.145 0.621 0.015 0.870 0.016 11.736 0.313 0.574 -3.5 0.509 0.03611 -0.149 0.621 0.014 0.855 0.015 14.093 0.314 0.543 -3.0 0.569 0.03340 -0.153 0.617 0.014 0.855 0.015 17.034 0.315 0.519 -2.5 0.628 0.03155 -0.157 0.614 0.014 0.851 0.015 19.915 0.317 0.500 -2.0 0.687 0.02777 -0.161 0.486 0.014 1.000 0.015 24.723 0.318 0.484 -1.5 0.744 0.02822 -0.165 0.462 0.014 1.000 0.015 26.365 0.320 0.472 -1.0 0.800 0.02377 -0.169 0.438 0.014 1.000 0.016 33.676 0.322 0.461 -0.5 0.856 0.02485 -0.173 0.418 0.014 1.000 0.016 34.437 0.323 0.452 0.0 0.910 0.01993 -0.177 0.394 0.015 1.000 0.016 45.667 0.301 0.444 0.5 0.971 0.02076 -0.179 0.382 0.015 1.000 0.016 46.788 0.281 0.434 1.0 1.031 0.02009 -0.181 0.370 0.015 1.000 0.017 51.329 0.281 0.425 1.5 1.092 0.02149 -0.182 0.362 0.015 1.000 0.017 50.803 0.351 0.417 2.0 1.087 0.02223 -0.186 0.354 0.015 0.926 0.017 48.906 0.494 0.421 2.5 1.120 0.02284 -0.189 0.346 0.016 0.896 0.017 49.061 0.318 0.419 3.0 1.176 0.02420 -0.192 0.338 0.016 0.892 0.018 48.577 0.302 0.413 3.5 1.227 0.02454 -0.195 0.330 0.016 0.885 0.019 50.015 0.304 0.409 4.0 1.282 0.02629 -0.198 0.322 0.017 0.881 0.021 48.771 0.309 0.404 4.5 1.330 0.02840 -0.201 0.316 0.928 0.870 0.951 46.847 0.315 0.401 5.0 1.381 0.02880 -0.204 0.310 0.929 0.862 0.954 47.947 0.314 0.398 5.5 1.431 0.03019 -0.208 0.306 0.934 0.855 0.954 47.415 0.312 0.395 6.0 1.485 0.03212 -0.211 0.290 0.939 0.851 0.954 46.229 0.314 0.392 6.5 1.535 0.03329 -0.214 0.278 0.947 0.844 0.954 46.102 0.320 0.390 7.0 1.584 0.03412 -0.218 0.270 0.953 0.836 0.954 46.416 0.323 0.387 7.5 1.632 0.03558 -0.221 0.258 0.953 0.829 0.955 45.875 0.339 0.386 8.0 1.673 0.03741 -0.226 0.254 0.953 0.814 0.955 44.714 0.350 0.385 8.5 1.716 0.03885 -0.230 0.246 0.953 0.803 0.955 44.169 0.367 0.384 9.0 1.750 0.04249 -0.235 0.241 0.951 0.782 0.953 41.186 0.395 0.384 9.5 1.785 0.04443 -0.240 0.233 0.951 0.762 0.953 40.175 0.332 0.384 10.0 1.845 0.05105 -0.243 0.099 0.952 0.770 0.953 36.142 0.336 0.381 10.5 1.878 0.05364 -0.248 0.094 0.952 0.750 0.953 35.013 0.414 0.382 11.0 1.910 0.05584 -0.253 0.091 0.957 0.730 0.959 34.200 0.416 0.383 11.5 1.942 0.06014 -0.258 0.089 0.952 0.713 0.954 32.288 0.417 0.383 12.0 1.972 0.06249 -0.264 0.084 0.957 0.696 0.959 31.563 0.612 0.384 12.5 1.977 0.07204 -0.271 0.076 0.957 0.653 0.959 27.451 0.412 0.387 13.0 2.035 0.06868 -0.274 0.079 0.958 0.668 0.959 29.636 0.345 0.385 13.5 2.060 0.07211 -0.279 0.076 0.958 0.653 0.959 28.565 0.479 0.385 14.0 2.082 0.07682 -0.284 0.074 0.958 0.638 0.959 27.098 0.472 0.387 14.5 2.106 0.08140 -0.289 0.067 0.958 0.628 0.959 25.873 0.528 0.387 15.0 2.120 0.08567 -0.295 0.060 0.958 0.611 0.959 24.742 0.665 0.389