Name = EPPLER 393 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 -0.329 0.29382 -0.052 1.000 0.002 1.000 0.003 -1.120 0.667 0.092 -14.5 -0.323 0.26600 -0.055 1.000 0.002 1.000 0.003 -1.214 0.607 0.081 -14.0 -0.314 0.24096 -0.057 1.000 0.002 1.000 0.003 -1.305 0.522 0.068 -13.5 -0.303 0.22217 -0.060 1.000 0.002 1.000 0.003 -1.365 0.467 0.053 -13.0 -0.290 0.19707 -0.063 1.000 0.002 1.000 0.003 -1.470 0.431 0.034 -12.5 -0.273 0.17665 -0.065 1.000 0.002 1.000 0.003 -1.548 0.404 0.011 -12.0 -0.254 0.16252 -0.068 1.000 0.002 1.000 0.003 -1.565 0.384 -0.017 -11.5 -0.233 0.14709 -0.071 1.000 0.002 1.000 0.003 -1.582 0.370 -0.054 -11.0 -0.209 0.13150 -0.073 1.000 0.002 1.000 0.002 -1.586 0.358 -0.102 -10.5 -0.182 0.11476 -0.076 1.000 0.002 1.000 0.002 -1.585 0.349 -0.169 -10.0 -0.153 0.10534 -0.079 1.000 0.002 1.000 0.002 -1.448 0.341 -0.268 -9.5 -0.121 0.09374 -0.082 1.000 0.002 1.000 0.003 -1.290 0.336 -0.426 -9.0 -0.087 0.08450 -0.085 1.000 0.002 1.000 0.003 -1.035 0.332 -0.717 -8.5 -0.052 0.07562 -0.087 1.000 0.002 1.000 0.003 -0.692 0.328 -1.419 -8.0 -0.016 0.06815 -0.090 1.000 0.002 1.000 0.003 -0.228 0.229 -5.556 -7.5 -0.319 0.05744 -0.093 0.841 0.002 1.000 0.003 -5.548 0.226 -0.042 -7.0 -0.255 0.05209 -0.096 0.731 0.003 1.000 0.004 -4.895 0.294 -0.126 -6.5 -0.190 0.04737 -0.099 0.677 0.003 1.000 0.005 -4.020 0.294 -0.268 -6.0 -0.125 0.04369 -0.101 0.644 0.004 1.000 0.006 -2.871 0.294 -0.559 -5.5 -0.060 0.04002 -0.104 0.625 0.006 1.000 0.009 -1.508 0.294 -1.478 -5.0 0.004 0.03680 -0.107 0.607 0.007 1.000 0.010 0.120 0.295 24.617 -4.5 0.069 0.03408 -0.110 0.595 0.009 1.000 0.012 2.012 0.295 1.855 -4.0 0.132 0.03168 -0.113 0.584 0.010 1.000 0.013 4.158 0.296 1.108 -3.5 0.194 0.02977 -0.116 0.574 0.012 1.000 0.017 6.511 0.358 0.848 -3.0 0.245 0.04644 -0.125 0.566 0.342 1.000 0.796 5.277 0.370 0.761 -2.5 0.302 0.04659 -0.129 0.558 0.378 1.000 0.866 6.485 0.322 0.676 -2.0 0.362 0.01710 -0.134 0.546 0.402 1.000 1.000 21.156 0.296 0.619 -1.5 0.421 0.01795 -0.134 0.536 0.425 1.000 1.000 23.469 0.263 0.569 -1.0 0.481 0.03838 -0.135 0.527 0.442 0.942 1.000 12.533 0.263 0.531 -0.5 0.540 0.03478 -0.136 0.518 0.460 0.886 1.000 15.541 0.295 0.501 0.0 0.515 0.03315 -0.137 0.509 0.479 0.837 1.000 15.535 0.484 0.515 0.5 0.552 0.03160 -0.139 0.499 0.496 0.796 1.000 17.469 0.303 0.501 1.0 0.593 0.03052 -0.141 0.488 0.515 0.766 1.000 19.414 0.309 0.488 1.5 0.631 0.02965 -0.143 0.479 0.537 0.734 1.000 21.299 0.316 0.477 2.0 0.671 0.03181 -0.146 0.471 0.570 0.705 1.000 21.101 0.318 0.467 2.5 0.712 0.03226 -0.149 0.463 0.621 0.680 1.000 22.071 0.315 0.459 3.0 0.757 0.03390 -0.152 0.451 0.722 0.666 1.000 22.323 0.314 0.450 3.5 0.801 0.03567 -0.154 0.439 0.850 0.651 1.000 22.445 0.316 0.443 4.0 0.845 0.03976 -0.157 0.428 1.000 0.638 1.000 21.239 0.318 0.436 4.5 0.887 0.04249 -0.160 0.418 1.000 0.624 1.000 20.887 0.320 0.431 5.0 0.931 0.04415 -0.163 0.405 1.000 0.612 1.000 21.076 0.322 0.426 5.5 0.973 0.04546 -0.166 0.392 0.999 0.600 1.000 21.403 0.325 0.421 6.0 1.013 0.04687 -0.170 0.380 0.999 0.589 0.999 21.611 0.330 0.417 6.5 1.051 0.04851 -0.173 0.365 0.999 0.578 0.999 21.677 0.319 0.414 7.0 1.096 0.04963 -0.175 0.336 0.999 0.582 0.999 22.090 0.385 0.410 7.5 1.117 0.05017 -0.182 0.001 0.999 0.007 0.999 22.256 0.391 0.413 8.0 1.160 0.05219 -0.184 0.001 0.999 0.001 0.999 22.220 0.337 0.409 8.5 1.184 0.05660 -0.187 0.001 0.998 0.001 0.999 20.909 0.380 0.408 9.0 1.205 0.06278 -0.190 0.001 0.998 0.001 0.998 19.202 0.403 0.408 9.5 1.223 0.06947 -0.193 0.001 0.998 0.001 0.998 17.598 0.454 0.408 10.0 1.235 0.07585 -0.196 0.001 0.998 0.001 0.998 16.278 0.534 0.409 10.5 1.243 0.08597 -0.199 0.001 0.998 0.001 0.998 14.465 0.705 0.410 11.0 1.248 0.09658 -0.202 0.001 0.997 0.001 0.997 12.919 1.468 0.412 11.5 1.248 0.11056 -0.205 0.001 0.992 0.001 0.995 11.292 -1.170 0.414 12.0 1.244 0.12528 -0.208 0.001 0.990 0.001 0.992 9.926 -0.157 0.417 12.5 1.234 0.13399 -0.211 0.001 0.989 0.001 0.990 9.208 -0.011 0.421 13.0 1.221 0.14988 -0.214 0.001 0.988 0.001 0.989 8.146 0.052 0.425 13.5 1.204 0.15864 -0.217 0.001 0.988 0.001 0.989 7.589 0.095 0.430 14.0 1.183 0.18593 -0.220 0.001 0.988 0.001 0.988 6.362 0.119 0.436 14.5 1.159 0.20774 -0.223 0.001 0.987 0.001 0.988 5.578 0.135 0.442 15.0 1.132 0.23025 -0.226 0.001 0.987 0.001 0.988 4.915 0.142 0.450 Name = EPPLER 393 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 -0.329 0.22888 -0.052 1.000 0.002 1.000 0.003 -1.437 0.666 0.092 -14.5 -0.323 0.20728 -0.055 1.000 0.002 1.000 0.003 -1.556 0.607 0.081 -14.0 -0.314 0.19002 -0.057 1.000 0.002 1.000 0.003 -1.653 0.524 0.068 -13.5 -0.303 0.16979 -0.060 1.000 0.002 1.000 0.003 -1.785 0.469 0.053 -13.0 -0.289 0.15248 -0.063 1.000 0.002 1.000 0.003 -1.898 0.431 0.034 -12.5 -0.273 0.13834 -0.065 1.000 0.002 1.000 0.003 -1.975 0.404 0.011 -12.0 -0.254 0.12751 -0.068 1.000 0.002 1.000 0.003 -1.993 0.385 -0.017 -11.5 -0.233 0.11339 -0.071 1.000 0.002 1.000 0.003 -2.052 0.371 -0.054 -11.0 -0.209 0.10263 -0.073 1.000 0.002 1.000 0.002 -2.032 0.358 -0.102 -10.5 -0.182 0.09290 -0.076 1.000 0.002 1.000 0.002 -1.956 0.349 -0.169 -10.0 -0.153 0.08358 -0.079 1.000 0.002 1.000 0.002 -1.825 0.341 -0.268 -9.5 -0.121 0.07658 -0.082 1.000 0.002 1.000 0.003 -1.576 0.335 -0.427 -9.0 -0.087 0.06942 -0.085 1.000 0.002 1.000 0.003 -1.257 0.332 -0.719 -8.5 -0.052 0.06252 -0.087 1.000 0.002 1.000 0.003 -0.833 0.328 -1.427 -8.0 -0.015 0.05725 -0.090 1.000 0.002 1.000 0.003 -0.262 0.229 -5.760 -7.5 -0.319 0.04908 -0.093 0.841 0.002 1.000 0.004 -6.493 0.226 -0.042 -7.0 -0.255 0.04476 -0.096 0.731 0.003 1.000 0.004 -5.697 0.294 -0.126 -6.5 -0.190 0.04097 -0.099 0.677 0.003 1.000 0.005 -4.648 0.294 -0.268 -6.0 -0.125 0.03796 -0.101 0.644 0.004 1.000 0.007 -3.304 0.294 -0.559 -5.5 -0.060 0.03473 -0.104 0.625 0.006 1.000 0.009 -1.738 0.294 -1.478 -5.0 0.004 0.03203 -0.107 0.607 0.007 1.000 0.010 0.137 0.295 24.616 -4.5 0.069 0.02966 -0.110 0.595 0.009 1.000 0.012 2.311 0.295 1.855 -4.0 0.132 0.02758 -0.113 0.584 0.010 1.000 0.014 4.775 0.295 1.108 -3.5 0.194 0.02626 -0.116 0.574 0.012 1.000 0.030 7.376 0.423 0.847 -3.0 0.243 0.01245 -0.132 0.566 0.342 1.000 1.000 19.474 0.408 0.795 -2.5 0.302 0.01291 -0.133 0.558 0.378 1.000 1.000 23.411 0.262 0.690 -2.0 0.362 0.01348 -0.134 0.546 0.402 1.000 1.000 26.842 0.263 0.619 -1.5 0.421 0.01378 -0.134 0.536 0.425 1.000 1.000 30.584 0.263 0.569 -1.0 0.481 0.01455 -0.135 0.527 0.442 1.000 1.000 33.062 0.263 0.531 -0.5 0.540 0.01539 -0.136 0.518 0.460 1.000 1.000 35.126 0.263 0.501 0.0 0.600 0.01745 -0.137 0.509 0.479 1.000 1.000 34.387 0.263 0.478 0.5 0.659 0.01861 -0.137 0.499 0.496 1.000 1.000 35.429 0.263 0.458 1.0 0.719 0.01935 -0.138 0.488 0.515 1.000 1.000 37.136 0.274 0.442 1.5 0.754 0.02919 -0.140 0.479 0.537 0.962 1.000 25.819 0.289 0.435 2.0 0.797 0.02871 -0.141 0.471 0.570 0.939 1.000 27.770 0.296 0.427 2.5 0.835 0.02591 -0.143 0.463 0.621 0.907 1.000 32.228 0.308 0.422 3.0 0.874 0.02480 -0.146 0.451 0.722 0.878 1.000 35.242 0.314 0.417 3.5 0.913 0.02388 -0.148 0.439 0.850 0.850 1.000 38.216 0.321 0.413 4.0 0.950 0.02634 -0.151 0.428 1.000 0.822 1.000 36.071 0.332 0.409 4.5 0.986 0.02842 -0.154 0.418 1.000 0.792 1.000 34.675 0.333 0.407 5.0 1.024 0.02975 -0.157 0.405 1.000 0.769 1.000 34.419 0.332 0.404 5.5 1.062 0.03087 -0.161 0.392 0.999 0.747 1.000 34.387 0.340 0.401 6.0 1.096 0.03215 -0.164 0.380 0.999 0.724 0.999 34.094 0.348 0.399 6.5 1.130 0.03358 -0.167 0.365 0.999 0.705 0.999 33.646 0.312 0.398 7.0 1.180 0.03428 -0.169 0.336 0.999 0.713 0.999 34.427 0.222 0.393 7.5 1.323 0.03439 -0.162 0.001 0.999 0.851 0.999 38.461 -0.468 0.372 8.0 1.159 0.04565 -0.184 0.001 0.999 0.002 0.999 25.388 0.067 0.409 8.5 1.183 0.04891 -0.187 0.001 0.998 0.001 0.999 24.193 0.379 0.408 9.0 1.205 0.05388 -0.190 0.001 0.998 0.001 0.998 22.363 0.403 0.408 9.5 1.222 0.05941 -0.193 0.001 0.998 0.001 0.998 20.573 0.454 0.408 10.0 1.234 0.06468 -0.196 0.001 0.998 0.001 0.998 19.082 0.529 0.409 10.5 1.243 0.07049 -0.199 0.001 0.998 0.001 0.998 17.641 0.693 0.410 11.0 1.248 0.07780 -0.202 0.001 0.997 0.001 0.997 16.038 1.468 0.412 11.5 1.248 0.08811 -0.205 0.001 0.992 0.001 0.995 14.169 -1.170 0.414 12.0 1.244 0.09797 -0.208 0.001 0.990 0.001 0.992 12.693 -0.157 0.417 12.5 1.234 0.10380 -0.211 0.001 0.989 0.001 0.990 11.886 -0.011 0.421 13.0 1.221 0.11552 -0.214 0.001 0.988 0.001 0.989 10.568 0.054 0.425 13.5 1.204 0.12766 -0.217 0.001 0.988 0.001 0.989 9.428 0.096 0.430 14.0 1.183 0.14574 -0.220 0.001 0.988 0.001 0.988 8.114 0.119 0.436 14.5 1.159 0.16271 -0.223 0.001 0.987 0.001 0.988 7.121 0.135 0.442 15.0 1.131 0.17727 -0.226 0.001 0.987 0.001 0.988 6.383 0.142 0.450 Name = EPPLER 393 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 -0.329 0.19533 -0.052 1.000 0.002 1.000 0.004 -1.683 0.666 0.092 -14.5 -0.322 0.17701 -0.054 1.000 0.002 1.000 0.004 -1.822 0.606 0.081 -14.0 -0.314 0.16359 -0.057 1.000 0.002 1.000 0.003 -1.919 0.524 0.068 -13.5 -0.303 0.14698 -0.060 1.000 0.002 1.000 0.003 -2.061 0.467 0.052 -13.0 -0.289 0.13692 -0.063 1.000 0.002 1.000 0.003 -2.111 0.431 0.034 -12.5 -0.273 0.12171 -0.065 1.000 0.002 1.000 0.003 -2.243 0.405 0.011 -12.0 -0.254 0.11235 -0.068 1.000 0.002 1.000 0.003 -2.260 0.385 -0.018 -11.5 -0.233 0.10092 -0.071 1.000 0.002 1.000 0.003 -2.304 0.370 -0.054 -11.0 -0.208 0.09199 -0.073 1.000 0.002 1.000 0.003 -2.265 0.358 -0.103 -10.5 -0.181 0.08349 -0.076 1.000 0.002 1.000 0.003 -2.174 0.349 -0.170 -10.0 -0.152 0.07561 -0.079 1.000 0.002 1.000 0.003 -2.014 0.341 -0.269 -9.5 -0.121 0.06790 -0.082 1.000 0.002 1.000 0.003 -1.778 0.335 -0.427 -9.0 -0.087 0.06288 -0.085 1.000 0.002 1.000 0.003 -1.383 0.331 -0.722 -8.5 -0.052 0.05680 -0.087 1.000 0.002 1.000 0.003 -0.913 0.328 -1.435 -8.0 -0.015 0.05202 -0.090 1.000 0.002 1.000 0.004 -0.283 0.229 -5.868 -7.5 -0.319 0.04510 -0.093 0.841 0.002 1.000 0.004 -7.066 0.226 -0.042 -7.0 -0.255 0.04131 -0.096 0.731 0.003 1.000 0.004 -6.172 0.294 -0.126 -6.5 -0.190 0.03828 -0.099 0.677 0.003 1.000 0.006 -4.975 0.294 -0.268 -6.0 -0.125 0.03526 -0.101 0.644 0.004 1.000 0.007 -3.556 0.294 -0.559 -5.5 -0.060 0.03240 -0.104 0.625 0.006 1.000 0.009 -1.863 0.294 -1.478 -5.0 0.004 0.03003 -0.107 0.607 0.007 1.000 0.011 0.146 0.295 24.614 -4.5 0.069 0.02779 -0.110 0.595 0.009 1.000 0.013 2.467 0.295 1.855 -4.0 0.132 0.02580 -0.113 0.584 0.010 1.000 0.015 5.105 0.436 1.107 -3.5 0.183 0.01270 -0.131 0.574 0.012 1.000 1.000 14.402 0.423 0.968 -3.0 0.243 0.01076 -0.132 0.566 0.342 1.000 1.000 22.537 0.262 0.795 -2.5 0.302 0.01114 -0.133 0.558 0.378 1.000 1.000 27.134 0.262 0.690 -2.0 0.362 0.01162 -0.134 0.546 0.402 1.000 1.000 31.123 0.263 0.619 -1.5 0.421 0.01187 -0.134 0.536 0.425 1.000 1.000 35.490 0.263 0.569 -1.0 0.481 0.01253 -0.135 0.527 0.442 1.000 1.000 38.383 0.263 0.531 -0.5 0.540 0.01324 -0.136 0.518 0.460 1.000 1.000 40.807 0.263 0.501 0.0 0.600 0.01500 -0.137 0.509 0.479 1.000 1.000 39.997 0.263 0.478 0.5 0.659 0.01599 -0.137 0.499 0.496 1.000 1.000 41.244 0.263 0.458 1.0 0.719 0.01608 -0.138 0.488 0.515 1.000 1.000 44.712 0.263 0.442 1.5 0.778 0.01732 -0.139 0.479 0.537 1.000 1.000 44.929 0.263 0.429 2.0 0.837 0.01991 -0.140 0.471 0.570 1.000 1.000 42.055 0.263 0.417 2.5 0.896 0.02168 -0.141 0.463 0.621 1.000 1.000 41.345 0.278 0.407 3.0 0.934 0.02528 -0.142 0.451 0.722 0.970 1.000 36.946 0.291 0.403 3.5 0.982 0.02407 -0.144 0.439 0.850 0.957 1.000 40.804 0.286 0.397 4.0 1.028 0.02408 -0.146 0.428 1.000 0.942 1.000 42.701 0.294 0.392 4.5 1.072 0.02348 -0.148 0.418 1.000 0.924 1.000 45.640 0.309 0.388 5.0 1.110 0.02320 -0.151 0.405 1.000 0.899 1.000 47.856 0.326 0.386 5.5 1.147 0.02395 -0.154 0.392 0.999 0.874 1.000 47.878 0.341 0.384 6.0 1.179 0.02486 -0.157 0.380 0.999 0.847 0.999 47.437 0.353 0.383 6.5 1.211 0.02596 -0.160 0.365 0.999 0.823 0.999 46.643 0.317 0.382 7.0 1.257 0.02679 -0.162 0.336 0.999 0.822 0.999 46.926 0.243 0.379 7.5 1.345 0.03085 -0.159 0.001 0.999 0.881 0.999 43.606 0.054 0.368 8.0 1.143 0.04468 -0.185 0.001 0.999 0.007 0.999 25.583 0.079 0.411 8.5 1.182 0.04608 -0.187 0.001 0.998 0.001 0.999 25.663 0.343 0.408 9.0 1.205 0.05004 -0.190 0.001 0.998 0.001 0.998 24.074 0.401 0.408 9.5 1.222 0.05511 -0.193 0.001 0.998 0.001 0.998 22.172 0.451 0.408 10.0 1.234 0.05853 -0.196 0.001 0.998 0.001 0.998 21.087 0.529 0.409 10.5 1.243 0.06560 -0.199 0.001 0.998 0.001 0.998 18.950 0.704 0.410 11.0 1.247 0.07209 -0.202 0.001 0.997 0.001 0.997 17.303 1.465 0.412 11.5 1.248 0.08131 -0.205 0.001 0.992 0.001 0.995 15.349 -1.175 0.414 12.0 1.243 0.08958 -0.208 0.001 0.990 0.001 0.992 13.878 -0.158 0.417 12.5 1.233 0.09423 -0.211 0.001 0.989 0.001 0.990 13.090 -0.011 0.421 13.0 1.221 0.10469 -0.214 0.001 0.988 0.001 0.989 11.659 0.054 0.425 13.5 1.203 0.11450 -0.217 0.001 0.988 0.001 0.989 10.509 0.096 0.430 14.0 1.182 0.12860 -0.220 0.001 0.988 0.001 0.988 9.193 0.118 0.436 14.5 1.159 0.13689 -0.223 0.001 0.987 0.001 0.988 8.464 0.135 0.442 15.0 1.131 0.15450 -0.226 0.001 0.987 0.001 0.988 7.322 0.143 0.450 Name = EPPLER 393 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 -0.329 0.17540 -0.052 1.000 0.002 1.000 0.004 -1.874 0.654 0.092 -14.5 -0.322 0.16334 -0.054 1.000 0.002 1.000 0.004 -1.972 0.606 0.081 -14.0 -0.314 0.14794 -0.057 1.000 0.002 1.000 0.004 -2.121 0.524 0.068 -13.5 -0.303 0.13678 -0.060 1.000 0.002 1.000 0.003 -2.212 0.466 0.052 -13.0 -0.289 0.12477 -0.063 1.000 0.002 1.000 0.003 -2.316 0.432 0.034 -12.5 -0.273 0.11192 -0.065 1.000 0.002 1.000 0.003 -2.438 0.406 0.011 -12.0 -0.254 0.10107 -0.068 1.000 0.002 1.000 0.003 -2.512 0.385 -0.018 -11.5 -0.232 0.09362 -0.071 1.000 0.002 1.000 0.003 -2.482 0.370 -0.054 -11.0 -0.208 0.08582 -0.073 1.000 0.002 1.000 0.003 -2.425 0.358 -0.103 -10.5 -0.181 0.07804 -0.076 1.000 0.002 1.000 0.003 -2.323 0.349 -0.170 -10.0 -0.152 0.06959 -0.079 1.000 0.002 1.000 0.003 -2.188 0.341 -0.269 -9.5 -0.120 0.06373 -0.082 1.000 0.002 1.000 0.003 -1.891 0.335 -0.429 -9.0 -0.087 0.05820 -0.085 1.000 0.002 1.000 0.003 -1.495 0.331 -0.722 -8.5 -0.052 0.05343 -0.087 1.000 0.002 1.000 0.003 -0.965 0.327 -1.444 -8.0 -0.014 0.04894 -0.090 1.000 0.002 1.000 0.004 -0.296 0.229 -5.980 -7.5 -0.319 0.04275 -0.093 0.841 0.002 1.000 0.004 -7.455 0.227 -0.042 -7.0 -0.255 0.03948 -0.096 0.731 0.003 1.000 0.005 -6.458 0.294 -0.126 -6.5 -0.190 0.03647 -0.099 0.677 0.003 1.000 0.006 -5.221 0.294 -0.268 -6.0 -0.125 0.03382 -0.101 0.644 0.004 1.000 0.008 -3.707 0.294 -0.559 -5.5 -0.060 0.03115 -0.104 0.625 0.006 1.000 0.010 -1.938 0.294 -1.478 -5.0 0.004 0.02877 -0.107 0.607 0.007 1.000 0.011 0.153 0.295 24.613 -4.5 0.069 0.02663 -0.110 0.595 0.009 1.000 0.013 2.575 0.295 1.855 -4.0 0.132 0.02475 -0.113 0.584 0.010 1.000 0.015 5.321 0.436 1.107 -3.5 0.183 0.01173 -0.131 0.574 0.012 1.000 1.000 15.588 0.423 0.968 -3.0 0.243 0.00975 -0.132 0.566 0.342 1.000 1.000 24.868 0.262 0.795 -2.5 0.302 0.01008 -0.133 0.558 0.378 1.000 1.000 29.973 0.262 0.690 -2.0 0.362 0.01052 -0.134 0.546 0.402 1.000 1.000 34.389 0.263 0.619 -1.5 0.421 0.01103 -0.134 0.536 0.425 1.000 1.000 38.212 0.263 0.569 -1.0 0.481 0.01133 -0.135 0.527 0.442 1.000 1.000 42.443 0.263 0.531 -0.5 0.540 0.01197 -0.136 0.518 0.460 1.000 1.000 45.144 0.263 0.501 0.0 0.600 0.01355 -0.137 0.509 0.479 1.000 1.000 44.279 0.263 0.478 0.5 0.659 0.01444 -0.137 0.499 0.496 1.000 1.000 45.676 0.263 0.458 1.0 0.719 0.01451 -0.138 0.488 0.515 1.000 1.000 49.530 0.263 0.442 1.5 0.778 0.01559 -0.139 0.479 0.537 1.000 1.000 49.906 0.263 0.429 2.0 0.837 0.01780 -0.140 0.471 0.570 1.000 1.000 47.041 0.263 0.417 2.5 0.896 0.01914 -0.141 0.463 0.621 1.000 1.000 46.815 0.264 0.407 3.0 0.955 0.02036 -0.141 0.451 0.722 1.000 1.000 46.887 0.264 0.398 3.5 1.013 0.02324 -0.142 0.439 0.850 1.000 1.000 43.593 0.264 0.390 4.0 1.071 0.02467 -0.143 0.428 1.000 1.000 1.000 43.420 0.292 0.383 4.5 1.101 0.02324 -0.146 0.418 1.000 0.963 1.000 47.382 0.309 0.382 5.0 1.149 0.02215 -0.148 0.405 1.000 0.953 1.000 51.876 0.290 0.378 5.5 1.194 0.02073 -0.150 0.392 0.999 0.939 1.000 57.598 0.302 0.375 6.0 1.234 0.02122 -0.152 0.380 0.999 0.922 0.999 58.146 0.324 0.373 6.5 1.267 0.02201 -0.155 0.365 0.999 0.900 0.999 57.558 0.318 0.372 7.0 1.308 0.02287 -0.157 0.336 0.999 0.891 0.999 57.216 0.272 0.370 7.5 1.366 0.02848 -0.157 0.001 0.999 0.907 0.999 47.960 0.311 0.365 8.0 1.382 0.03012 -0.162 0.001 0.999 0.874 0.999 45.875 0.095 0.367 8.5 1.170 0.04551 -0.187 0.001 0.998 0.006 0.999 25.708 0.088 0.410 9.0 1.204 0.04779 -0.190 0.001 0.998 0.001 0.998 25.200 0.363 0.408 9.5 1.221 0.05263 -0.193 0.001 0.998 0.001 0.998 23.209 0.451 0.408 10.0 1.234 0.05600 -0.196 0.001 0.998 0.001 0.998 22.033 0.524 0.409 10.5 1.243 0.06115 -0.199 0.001 0.998 0.001 0.998 20.328 0.692 0.410 11.0 1.247 0.06668 -0.202 0.001 0.997 0.001 0.997 18.706 1.465 0.412 11.5 1.248 0.07480 -0.205 0.001 0.992 0.001 0.995 16.685 -1.175 0.414 12.0 1.243 0.08175 -0.208 0.001 0.990 0.001 0.992 15.208 -0.149 0.417 12.5 1.233 0.08881 -0.211 0.001 0.989 0.001 0.990 13.886 -0.011 0.421 13.0 1.221 0.09490 -0.214 0.001 0.988 0.001 0.989 12.861 0.053 0.425 13.5 1.203 0.10693 -0.217 0.001 0.988 0.001 0.989 11.251 0.096 0.430 14.0 1.182 0.11386 -0.220 0.001 0.988 0.001 0.988 10.384 0.118 0.436 14.5 1.158 0.12665 -0.223 0.001 0.987 0.001 0.988 9.146 0.135 0.442 15.0 1.131 0.14110 -0.226 0.001 0.987 0.001 0.988 8.015 0.143 0.450