Name = EPPLER 327 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 -0.435 0.25559 0.090 0.965 0.002 0.973 0.004 -1.702 0.009 0.456 -14.5 -0.446 0.23446 0.087 0.965 0.002 0.973 0.004 -1.900 -0.004 0.446 -14.0 -0.455 0.26607 0.085 0.965 0.002 0.973 0.003 -1.711 -0.038 0.436 -13.5 -0.463 0.20744 0.082 0.964 0.002 0.973 0.003 -2.234 -0.093 0.427 -13.0 -0.470 0.23210 0.079 0.964 0.002 0.973 0.003 -2.027 -0.188 0.419 -12.5 -0.476 0.20437 0.077 0.963 0.002 0.973 0.003 -2.327 -0.395 0.412 -12.0 -0.479 0.19829 0.074 0.962 0.002 0.973 0.003 -2.414 -1.032 0.405 -11.5 -0.480 0.18347 0.071 0.961 0.002 0.974 0.003 -2.615 17.434 0.399 -11.0 -0.478 0.16325 0.069 0.960 0.002 0.974 0.003 -2.930 1.226 0.394 -10.5 -0.474 0.14448 0.066 0.959 0.002 0.974 0.003 -3.281 0.740 0.389 -10.0 -0.467 0.13815 0.063 0.959 0.002 0.973 0.003 -3.381 0.582 0.385 -9.5 -0.457 0.12174 0.060 0.958 0.002 0.973 0.003 -3.756 0.498 0.382 -9.0 -0.444 0.10851 0.058 0.956 0.002 0.973 0.003 -4.095 0.445 0.379 -8.5 -0.428 0.09817 0.055 0.955 0.002 0.972 0.003 -4.360 0.412 0.378 -8.0 -0.409 0.09072 0.052 0.953 0.002 0.972 0.003 -4.508 0.391 0.377 -7.5 -0.387 0.08022 0.049 0.723 0.002 0.986 0.002 -4.825 0.375 0.376 -7.0 -0.362 0.07396 0.046 0.660 0.002 0.988 0.002 -4.896 0.363 0.377 -6.5 -0.335 0.06309 0.043 0.610 0.002 0.990 0.002 -5.308 0.354 0.378 -6.0 -0.305 0.05719 0.040 0.577 0.002 0.992 0.002 -5.335 0.347 0.381 -5.5 -0.273 0.05359 0.037 0.547 0.001 1.000 0.002 -5.102 0.342 0.385 -5.0 -0.240 0.04707 0.034 0.518 0.002 1.000 0.002 -5.089 0.337 0.392 -4.5 -0.204 0.04244 0.031 0.492 0.001 1.000 0.002 -4.809 0.335 0.401 -4.0 -0.167 0.03848 0.028 0.466 0.001 1.000 0.002 -4.350 0.332 0.416 -3.5 -0.130 0.03448 0.025 0.445 0.001 1.000 0.002 -3.759 0.331 0.441 -3.0 -0.091 0.03085 0.022 0.426 0.001 1.000 0.002 -2.949 0.330 0.488 -2.5 -0.051 0.02816 0.019 0.406 0.001 1.000 0.002 -1.828 0.329 0.610 -2.0 -0.011 0.02506 0.015 0.389 0.001 0.983 0.002 -0.453 1.459 1.606 -1.5 -0.046 0.02254 0.012 0.373 0.003 0.977 0.004 -2.052 0.649 0.515 -1.0 0.015 0.02833 0.005 0.359 0.005 0.967 0.998 0.544 0.311 -0.056 -0.5 0.076 0.02539 0.005 0.347 0.771 0.855 0.809 3.002 0.304 0.187 0.0 0.054 0.02593 0.003 0.336 0.772 0.747 0.811 2.072 1.026 0.201 0.5 0.082 0.02736 -0.000 0.327 0.774 0.675 0.814 3.013 0.347 0.251 1.0 0.114 0.02900 -0.003 0.317 0.776 0.617 0.816 3.928 0.346 0.278 1.5 0.150 0.03061 -0.007 0.308 0.777 0.575 0.819 4.898 0.345 0.294 2.0 0.186 0.03241 -0.010 0.299 0.779 0.537 0.822 5.740 0.349 0.304 2.5 0.222 0.03437 -0.014 0.292 0.780 0.501 0.824 6.462 0.349 0.312 3.0 0.260 0.03635 -0.017 0.285 0.782 0.471 0.827 7.147 0.346 0.317 3.5 0.299 0.03853 -0.021 0.278 0.783 0.446 0.830 7.762 0.342 0.320 4.0 0.340 0.04097 -0.025 0.270 0.785 0.427 0.833 8.303 0.340 0.323 4.5 0.382 0.04348 -0.028 0.261 0.786 0.411 0.836 8.775 0.339 0.325 5.0 0.424 0.04603 -0.032 0.253 0.788 0.396 0.838 9.204 0.340 0.326 5.5 0.465 0.04880 -0.036 0.245 0.790 0.381 0.842 9.526 0.343 0.327 6.0 0.505 0.05170 -0.040 0.238 0.792 0.366 0.845 9.771 0.339 0.329 6.5 0.549 0.05442 -0.043 0.228 0.793 0.358 0.849 10.083 0.335 0.329 7.0 0.592 0.05727 -0.047 0.216 0.795 0.351 0.854 10.342 0.338 0.330 7.5 0.634 0.06041 -0.051 0.206 0.798 0.341 0.858 10.496 0.340 0.330 8.0 0.676 0.06363 -0.055 0.194 0.800 0.333 0.863 10.620 0.338 0.331 8.5 0.719 0.06686 -0.058 0.178 0.802 0.329 0.869 10.753 0.338 0.331 9.0 0.761 0.07031 -0.062 0.161 0.804 0.324 0.875 10.819 0.333 0.332 9.5 0.807 0.07355 -0.066 0.133 0.806 0.330 0.879 10.978 0.322 0.331 10.0 0.858 0.07613 -0.069 0.091 0.808 0.346 0.888 11.274 0.324 0.331 10.5 0.903 0.07917 -0.073 0.048 0.811 0.355 0.897 11.401 0.349 0.331 11.0 0.934 0.08342 -0.077 0.019 0.813 0.344 0.910 11.192 0.821 0.332 11.5 0.917 0.08854 -0.081 0.013 0.815 0.242 1.000 10.362 0.332 0.339 12.0 0.971 0.09277 -0.080 0.006 0.818 0.026 1.000 10.469 0.263 0.332 12.5 1.016 0.09458 -0.082 0.002 0.821 0.010 1.000 10.746 0.326 0.331 13.0 1.049 0.09859 -0.086 0.000 0.824 0.004 1.000 10.644 0.358 0.332 13.5 1.077 0.10296 -0.089 0.000 0.828 0.001 1.000 10.457 0.420 0.333 14.0 1.089 0.11224 -0.092 0.000 0.832 0.000 1.000 9.706 0.604 0.335 14.5 1.096 0.12163 -0.096 0.000 0.835 0.000 1.000 9.014 1.086 0.338 15.0 1.098 0.13602 -0.099 0.000 0.841 0.000 1.000 8.071 2.665 0.341 Name = EPPLER 327 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 -0.435 0.19630 0.090 0.965 0.002 0.974 0.004 -2.216 0.009 0.456 -14.5 -0.445 0.17977 0.087 0.965 0.002 0.973 0.004 -2.478 -0.004 0.446 -14.0 -0.455 0.16704 0.085 0.965 0.002 0.973 0.004 -2.724 -0.039 0.436 -13.5 -0.463 0.16167 0.082 0.964 0.002 0.973 0.004 -2.866 -0.093 0.427 -13.0 -0.470 0.14766 0.079 0.964 0.002 0.973 0.003 -3.185 -0.189 0.419 -12.5 -0.475 0.15962 0.077 0.963 0.002 0.973 0.003 -2.978 -0.389 0.412 -12.0 -0.479 0.14490 0.074 0.962 0.002 0.974 0.003 -3.303 -1.003 0.405 -11.5 -0.480 0.13449 0.071 0.961 0.002 0.974 0.003 -3.567 11.528 0.399 -11.0 -0.478 0.13095 0.069 0.960 0.002 0.974 0.003 -3.652 1.198 0.394 -10.5 -0.474 0.11509 0.066 0.959 0.002 0.974 0.003 -4.118 0.748 0.389 -10.0 -0.467 0.10398 0.063 0.959 0.002 0.974 0.003 -4.492 0.586 0.385 -9.5 -0.457 0.09283 0.060 0.958 0.002 0.974 0.003 -4.926 0.496 0.382 -9.0 -0.444 0.08939 0.058 0.956 0.002 0.974 0.003 -4.968 0.445 0.379 -8.5 -0.428 0.07605 0.055 0.955 0.002 0.973 0.003 -5.629 0.413 0.378 -8.0 -0.409 0.07068 0.052 0.953 0.002 0.972 0.003 -5.786 0.391 0.377 -7.5 -0.387 0.06368 0.049 0.723 0.002 0.990 0.002 -6.078 0.375 0.376 -7.0 -0.362 0.05924 0.046 0.660 0.002 0.993 0.002 -6.113 0.362 0.377 -6.5 -0.335 0.05460 0.043 0.610 0.002 1.000 0.002 -6.129 0.354 0.378 -6.0 -0.305 0.04912 0.040 0.577 0.002 1.000 0.002 -6.206 0.348 0.381 -5.5 -0.273 0.04436 0.037 0.547 0.001 1.000 0.002 -6.163 0.342 0.385 -5.0 -0.239 0.04134 0.034 0.518 0.002 1.000 0.002 -5.791 0.337 0.392 -4.5 -0.204 0.03781 0.031 0.492 0.001 1.000 0.002 -5.392 0.335 0.402 -4.0 -0.167 0.03371 0.028 0.466 0.001 1.000 0.002 -4.966 0.333 0.416 -3.5 -0.129 0.03097 0.025 0.445 0.001 1.000 0.002 -4.179 0.331 0.441 -3.0 -0.091 0.02828 0.022 0.426 0.001 1.000 0.002 -3.210 0.330 0.489 -2.5 -0.051 0.02565 0.019 0.406 0.001 1.000 0.002 -2.007 0.329 0.610 -2.0 -0.011 0.02356 0.015 0.389 0.001 1.000 0.002 -0.482 1.458 1.606 -1.5 -0.046 0.02204 0.012 0.373 0.003 1.000 0.004 -2.098 0.649 0.515 -1.0 0.015 0.02937 0.005 0.359 0.005 1.000 0.998 0.525 0.311 -0.056 -0.5 0.076 0.02350 0.005 0.347 0.771 1.000 0.816 3.243 0.267 0.188 0.0 0.137 0.02259 0.003 0.336 0.772 1.000 0.819 6.053 0.276 0.231 0.5 0.197 0.02289 0.002 0.327 0.774 1.000 0.822 8.624 0.267 0.242 1.0 0.258 0.02263 0.001 0.317 0.776 1.000 0.825 11.405 0.272 0.248 1.5 0.311 0.02216 -0.001 0.308 0.777 0.981 0.828 14.028 0.281 0.253 2.0 0.362 0.02172 -0.003 0.299 0.779 0.960 0.832 16.658 0.374 0.257 2.5 0.366 0.02075 -0.008 0.292 0.780 0.828 0.835 17.640 0.658 0.271 3.0 0.385 0.02212 -0.012 0.285 0.782 0.745 0.839 17.413 0.460 0.282 3.5 0.408 0.02449 -0.017 0.278 0.783 0.679 0.843 16.667 0.409 0.291 4.0 0.439 0.02681 -0.021 0.270 0.785 0.633 0.846 16.356 0.377 0.297 4.5 0.472 0.02917 -0.025 0.261 0.786 0.597 0.851 16.187 0.372 0.302 5.0 0.505 0.03171 -0.029 0.253 0.788 0.562 0.855 15.929 0.374 0.307 5.5 0.539 0.03443 -0.033 0.245 0.790 0.530 0.860 15.647 0.374 0.311 6.0 0.572 0.03725 -0.037 0.238 0.792 0.499 0.865 15.356 0.359 0.315 6.5 0.612 0.03977 -0.041 0.228 0.793 0.482 0.871 15.393 0.345 0.317 7.0 0.653 0.04232 -0.045 0.216 0.795 0.468 0.878 15.433 0.347 0.319 7.5 0.692 0.04514 -0.049 0.206 0.798 0.452 0.885 15.331 0.348 0.320 8.0 0.732 0.04796 -0.053 0.194 0.800 0.439 0.893 15.273 0.338 0.322 8.5 0.778 0.05056 -0.056 0.178 0.802 0.436 0.906 15.383 0.333 0.322 9.0 0.821 0.05344 -0.060 0.161 0.804 0.431 0.919 15.361 0.323 0.323 9.5 0.873 0.05611 -0.063 0.133 0.806 0.442 0.943 15.566 0.308 0.322 10.0 0.928 0.05467 -0.066 0.091 0.808 0.458 1.000 16.978 0.317 0.321 10.5 0.970 0.05677 -0.070 0.048 0.811 0.459 1.000 17.090 0.356 0.322 11.0 1.000 0.06027 -0.074 0.019 0.813 0.446 1.000 16.587 0.469 0.324 11.5 1.011 0.06532 -0.079 0.013 0.815 0.411 1.000 15.473 0.880 0.328 12.0 1.015 0.07174 -0.083 0.006 0.818 0.369 1.000 14.151 -0.169 0.332 12.5 0.987 0.08244 -0.089 0.002 0.821 0.271 1.000 11.970 0.392 0.340 13.0 1.033 0.08678 -0.086 0.000 0.824 0.011 1.000 11.906 0.254 0.333 13.5 1.071 0.08823 -0.089 0.000 0.828 0.002 1.000 12.134 0.369 0.333 14.0 1.087 0.09420 -0.092 0.000 0.832 0.000 1.000 11.540 0.536 0.335 14.5 1.095 0.10241 -0.096 0.000 0.835 0.000 1.000 10.691 0.952 0.338 15.0 1.097 0.11159 -0.099 0.000 0.841 0.000 1.000 9.831 1.830 0.341 Name = EPPLER 327 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 -0.435 0.18094 0.090 0.965 0.002 0.974 0.004 -2.403 0.008 0.457 -14.5 -0.445 0.16552 0.087 0.965 0.002 0.973 0.004 -2.691 -0.004 0.446 -14.0 -0.455 0.14668 0.085 0.965 0.002 0.973 0.004 -3.102 -0.038 0.436 -13.5 -0.463 0.14224 0.082 0.964 0.002 0.974 0.004 -3.257 -0.093 0.427 -13.0 -0.470 0.13119 0.079 0.964 0.002 0.973 0.004 -3.584 -0.190 0.419 -12.5 -0.475 0.11931 0.077 0.963 0.002 0.974 0.004 -3.984 -0.391 0.412 -12.0 -0.479 0.12909 0.074 0.962 0.002 0.974 0.003 -3.707 -1.020 0.405 -11.5 -0.480 0.12021 0.071 0.961 0.002 0.974 0.003 -3.989 15.141 0.399 -11.0 -0.478 0.11017 0.069 0.960 0.002 0.974 0.003 -4.341 1.198 0.394 -10.5 -0.474 0.10282 0.066 0.959 0.002 0.974 0.003 -4.608 0.740 0.389 -10.0 -0.467 0.09373 0.063 0.959 0.002 0.974 0.003 -4.981 0.585 0.385 -9.5 -0.457 0.08468 0.060 0.958 0.002 0.974 0.003 -5.398 0.498 0.382 -9.0 -0.444 0.07736 0.058 0.956 0.002 0.974 0.003 -5.740 0.445 0.379 -8.5 -0.428 0.06992 0.055 0.955 0.002 0.973 0.003 -6.119 0.413 0.378 -8.0 -0.409 0.06198 0.052 0.953 0.002 0.973 0.003 -6.598 0.392 0.377 -7.5 -0.387 0.05680 0.049 0.723 0.002 0.992 0.002 -6.814 0.375 0.376 -7.0 -0.362 0.05283 0.046 0.660 0.002 0.996 0.002 -6.854 0.362 0.377 -6.5 -0.335 0.04891 0.043 0.610 0.002 1.000 0.002 -6.842 0.354 0.378 -6.0 -0.305 0.04446 0.040 0.577 0.002 1.000 0.002 -6.857 0.347 0.381 -5.5 -0.273 0.04239 0.037 0.547 0.001 1.000 0.002 -6.443 0.342 0.385 -5.0 -0.239 0.03779 0.034 0.518 0.002 1.000 0.002 -6.334 0.338 0.392 -4.5 -0.204 0.03459 0.031 0.492 0.001 1.000 0.002 -5.896 0.335 0.402 -4.0 -0.167 0.03174 0.028 0.466 0.001 1.000 0.002 -5.267 0.332 0.417 -3.5 -0.129 0.02894 0.025 0.445 0.001 1.000 0.002 -4.472 0.331 0.441 -3.0 -0.091 0.02657 0.022 0.426 0.001 1.000 0.002 -3.417 0.330 0.489 -2.5 -0.051 0.02443 0.019 0.406 0.001 1.000 0.002 -2.107 0.329 0.610 -2.0 -0.011 0.02264 0.015 0.389 0.001 1.000 0.003 -0.488 1.458 1.644 -1.5 -0.046 0.02113 0.012 0.373 0.003 1.000 0.004 -2.189 0.654 0.515 -1.0 0.015 0.02970 0.005 0.359 0.005 1.000 0.998 0.519 0.312 -0.055 -0.5 0.076 0.02160 0.005 0.347 0.771 1.000 0.823 3.528 0.267 0.188 0.0 0.137 0.02091 0.003 0.336 0.772 1.000 0.827 6.541 0.276 0.231 0.5 0.197 0.02163 0.002 0.327 0.774 1.000 0.830 9.129 0.267 0.242 1.0 0.258 0.02156 0.001 0.317 0.776 1.000 0.834 11.971 0.268 0.248 1.5 0.319 0.02201 -0.001 0.308 0.777 1.000 0.838 14.478 0.268 0.252 2.0 0.379 0.02219 -0.002 0.299 0.779 1.000 0.842 17.096 0.268 0.254 2.5 0.440 0.02218 -0.003 0.292 0.780 1.000 0.846 19.829 0.269 0.256 3.0 0.500 0.02235 -0.004 0.285 0.782 1.000 0.851 22.386 0.286 0.258 3.5 0.544 0.02205 -0.007 0.278 0.783 0.967 0.856 24.686 0.378 0.262 4.0 0.563 0.02170 -0.012 0.270 0.785 0.882 0.862 25.942 0.534 0.271 4.5 0.582 0.02212 -0.017 0.261 0.786 0.805 0.867 26.325 0.485 0.280 5.0 0.607 0.02309 -0.022 0.253 0.788 0.747 0.873 26.294 0.445 0.287 5.5 0.633 0.02547 -0.027 0.245 0.790 0.696 0.881 24.838 0.440 0.293 6.0 0.659 0.02806 -0.032 0.238 0.792 0.649 0.887 23.475 0.403 0.299 6.5 0.692 0.03054 -0.036 0.228 0.793 0.618 0.897 22.675 0.368 0.303 7.0 0.730 0.03303 -0.040 0.216 0.795 0.595 0.910 22.098 0.369 0.305 7.5 0.763 0.03587 -0.045 0.206 0.798 0.568 0.921 21.280 0.372 0.309 8.0 0.800 0.03883 -0.049 0.194 0.800 0.547 0.944 20.596 0.351 0.311 8.5 0.842 0.03976 -0.053 0.178 0.802 0.537 1.000 21.180 0.344 0.313 9.0 0.882 0.04149 -0.057 0.161 0.804 0.524 1.000 21.251 0.332 0.314 9.5 0.930 0.04324 -0.060 0.133 0.806 0.526 1.000 21.510 0.320 0.314 10.0 0.977 0.04542 -0.063 0.091 0.808 0.527 1.000 21.504 0.346 0.315 10.5 1.008 0.04841 -0.067 0.048 0.811 0.512 1.000 20.819 0.410 0.317 11.0 1.031 0.05255 -0.072 0.019 0.813 0.490 1.000 19.616 0.505 0.320 11.5 1.045 0.05703 -0.077 0.013 0.815 0.459 1.000 18.319 0.625 0.324 12.0 1.056 0.06235 -0.082 0.006 0.818 0.430 1.000 16.942 0.811 0.327 12.5 1.062 0.06762 -0.086 0.002 0.821 0.396 1.000 15.702 -0.331 0.331 13.0 1.039 0.07667 -0.092 0.000 0.824 0.323 1.000 13.548 -0.204 0.338 13.5 1.055 0.08438 -0.089 0.000 0.828 0.007 1.000 12.506 0.264 0.335 14.0 1.083 0.08724 -0.093 0.000 0.832 0.001 1.000 12.413 0.426 0.335 14.5 1.093 0.09369 -0.096 0.000 0.835 0.000 1.000 11.664 0.787 0.338 15.0 1.096 0.10099 -0.099 0.000 0.841 0.000 1.000 10.851 1.405 0.341 Name = EPPLER 327 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 -0.435 0.16400 0.090 0.965 0.002 0.974 0.004 -2.651 0.008 0.457 -14.5 -0.445 0.15003 0.087 0.965 0.002 0.974 0.004 -2.968 -0.004 0.446 -14.0 -0.455 0.13479 0.085 0.965 0.002 0.974 0.004 -3.375 -0.039 0.436 -13.5 -0.463 0.13091 0.082 0.964 0.002 0.974 0.004 -3.539 -0.094 0.427 -13.0 -0.470 0.12176 0.079 0.964 0.002 0.974 0.004 -3.861 -0.190 0.419 -12.5 -0.475 0.11058 0.077 0.963 0.002 0.974 0.004 -4.298 -0.392 0.412 -12.0 -0.478 0.10342 0.074 0.962 0.002 0.974 0.004 -4.626 -1.029 0.405 -11.5 -0.479 0.11216 0.071 0.961 0.002 0.974 0.003 -4.275 12.951 0.399 -11.0 -0.478 0.10367 0.069 0.960 0.002 0.974 0.003 -4.611 1.198 0.394 -10.5 -0.474 0.08418 0.066 0.959 0.002 0.974 0.003 -5.627 0.748 0.389 -10.0 -0.467 0.08392 0.063 0.959 0.002 0.974 0.003 -5.564 0.588 0.385 -9.5 -0.457 0.07617 0.060 0.958 0.002 0.974 0.003 -6.000 0.498 0.382 -9.0 -0.444 0.07031 0.058 0.956 0.002 0.974 0.003 -6.317 0.445 0.379 -8.5 -0.428 0.06340 0.055 0.955 0.002 0.974 0.003 -6.748 0.412 0.378 -8.0 -0.409 0.05915 0.052 0.953 0.002 0.973 0.003 -6.911 0.391 0.377 -7.5 -0.387 0.05470 0.049 0.723 0.002 0.994 0.003 -7.072 0.375 0.376 -7.0 -0.362 0.05105 0.046 0.660 0.002 1.000 0.003 -7.089 0.363 0.377 -6.5 -0.335 0.04562 0.043 0.610 0.002 1.000 0.002 -7.336 0.354 0.378 -6.0 -0.305 0.04170 0.040 0.577 0.002 1.000 0.002 -7.311 0.347 0.381 -5.5 -0.273 0.03975 0.037 0.547 0.001 1.000 0.002 -6.870 0.342 0.385 -5.0 -0.239 0.03574 0.034 0.518 0.002 1.000 0.002 -6.698 0.338 0.392 -4.5 -0.204 0.03281 0.031 0.492 0.001 1.000 0.002 -6.216 0.335 0.402 -4.0 -0.167 0.03022 0.028 0.466 0.001 1.000 0.002 -5.533 0.332 0.417 -3.5 -0.129 0.02766 0.025 0.445 0.001 1.000 0.002 -4.678 0.331 0.441 -3.0 -0.091 0.02558 0.022 0.426 0.001 1.000 0.002 -3.541 0.330 0.489 -2.5 -0.051 0.02364 0.019 0.406 0.001 1.000 0.002 -2.165 0.329 0.612 -2.0 -0.011 0.02174 0.015 0.389 0.001 1.000 0.003 -0.508 1.525 1.644 -1.5 -0.046 0.02064 0.012 0.373 0.003 1.000 0.004 -2.241 0.654 0.515 -1.0 0.015 0.02957 0.005 0.359 0.005 1.000 0.999 0.521 0.312 -0.055 -0.5 0.076 0.02033 0.005 0.347 0.771 1.000 0.830 3.748 0.267 0.189 0.0 0.137 0.01986 0.003 0.336 0.772 1.000 0.834 6.886 0.275 0.231 0.5 0.197 0.02055 0.002 0.327 0.774 1.000 0.838 9.605 0.267 0.242 1.0 0.258 0.02095 0.001 0.317 0.776 1.000 0.843 12.315 0.268 0.248 1.5 0.319 0.02136 -0.001 0.308 0.777 1.000 0.847 14.918 0.268 0.252 2.0 0.379 0.02150 -0.002 0.299 0.779 1.000 0.853 17.645 0.268 0.254 2.5 0.440 0.02203 -0.003 0.292 0.780 1.000 0.858 19.963 0.269 0.256 3.0 0.500 0.02282 -0.004 0.285 0.782 1.000 0.864 21.928 0.269 0.258 3.5 0.561 0.02310 -0.005 0.278 0.783 1.000 0.871 24.284 0.269 0.259 4.0 0.621 0.02395 -0.006 0.270 0.785 1.000 0.878 25.939 0.269 0.260 4.5 0.682 0.02395 -0.007 0.261 0.786 1.000 0.886 28.465 0.306 0.261 5.0 0.716 0.02354 -0.012 0.253 0.788 0.953 0.893 30.397 0.598 0.266 5.5 0.717 0.02344 -0.020 0.245 0.790 0.846 0.904 30.593 0.888 0.277 6.0 0.738 0.02414 -0.026 0.238 0.792 0.783 0.915 30.559 0.467 0.285 6.5 0.767 0.02538 -0.030 0.228 0.793 0.740 0.932 30.216 0.409 0.290 7.0 0.798 0.02813 -0.035 0.216 0.795 0.703 1.000 28.381 0.407 0.294 7.5 0.828 0.02968 -0.040 0.206 0.798 0.667 1.000 27.890 0.405 0.298 8.0 0.860 0.03157 -0.045 0.194 0.800 0.637 1.000 27.227 0.379 0.302 8.5 0.896 0.03295 -0.049 0.178 0.802 0.617 1.000 27.201 0.366 0.305 9.0 0.932 0.03493 -0.053 0.161 0.804 0.597 1.000 26.697 0.353 0.307 9.5 0.974 0.03710 -0.057 0.133 0.806 0.587 1.000 26.238 0.350 0.308 10.0 1.010 0.03998 -0.061 0.091 0.808 0.574 1.000 25.271 0.396 0.310 10.5 1.034 0.04357 -0.066 0.048 0.811 0.548 1.000 23.725 0.495 0.314 11.0 1.050 0.04814 -0.071 0.019 0.813 0.516 1.000 21.817 0.559 0.317 11.5 1.066 0.05226 -0.076 0.013 0.815 0.488 1.000 20.396 0.618 0.321 12.0 1.077 0.05737 -0.080 0.006 0.818 0.458 1.000 18.768 0.761 0.325 12.5 1.085 0.06201 -0.085 0.002 0.821 0.429 1.000 17.495 1.767 0.329 13.0 1.083 0.06807 -0.090 0.000 0.824 0.392 1.000 15.912 0.056 0.333 13.5 1.028 0.08135 -0.096 0.000 0.828 0.267 1.000 12.639 -0.159 0.344 14.0 1.077 0.08365 -0.093 0.000 0.832 0.002 1.000 12.880 0.247 0.336 14.5 1.090 0.08897 -0.096 0.000 0.835 0.001 1.000 12.251 0.667 0.338 15.0 1.094 0.09562 -0.099 0.000 0.841 0.000 1.000 11.441 1.098 0.341