Name = FX 63-158 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 -0.231 0.27474 -0.074 0.930 0.003 0.953 0.004 -0.841 0.461 -0.069 -14.5 -0.214 0.24126 -0.077 0.929 0.003 0.954 0.004 -0.889 0.448 -0.110 -14.0 -0.196 0.21301 -0.081 0.928 0.003 0.954 0.004 -0.918 0.427 -0.162 -13.5 -0.175 0.20843 -0.084 0.926 0.003 0.954 0.004 -0.838 0.411 -0.232 -13.0 -0.151 0.18249 -0.088 0.924 0.003 0.955 0.003 -0.830 0.396 -0.329 -12.5 -0.126 0.17539 -0.091 0.875 0.002 0.962 0.003 -0.718 0.384 -0.475 -12.0 -0.098 0.14509 -0.095 0.874 0.003 0.962 0.003 -0.676 0.375 -0.717 -11.5 -0.068 0.14156 -0.098 0.872 0.002 0.963 0.003 -0.483 0.367 -1.191 -11.0 -0.037 0.12268 -0.102 0.870 0.002 0.963 0.003 -0.298 0.360 -2.538 -10.5 -0.003 0.10735 -0.106 0.596 0.002 0.977 0.003 -0.026 0.230 -37.668 -10.0 -0.393 0.09849 -0.109 0.592 0.002 0.977 0.003 -3.994 0.228 -0.028 -9.5 -0.335 0.09131 -0.113 0.530 0.002 0.979 0.003 -3.665 0.311 -0.087 -9.0 -0.274 0.08058 -0.117 0.527 0.002 0.979 0.003 -3.398 0.309 -0.176 -8.5 -0.211 0.07382 -0.120 0.525 0.002 0.979 0.003 -2.860 0.308 -0.320 -8.0 -0.147 0.06543 -0.124 0.522 0.002 0.979 0.003 -2.247 0.307 -0.593 -7.5 -0.082 0.05962 -0.128 0.519 0.002 0.979 0.003 -1.374 0.306 -1.308 -7.0 -0.016 0.05355 -0.131 0.466 0.002 0.980 0.003 -0.301 0.306 -7.885 -6.5 0.050 0.04931 -0.135 0.465 0.002 0.980 0.003 1.012 0.306 2.954 -6.0 0.116 0.04603 -0.139 0.463 0.002 0.979 0.002 2.520 0.306 1.446 -5.5 0.182 0.04157 -0.142 0.462 0.002 0.979 0.002 4.372 0.307 1.034 -5.0 0.247 0.03892 -0.146 0.460 0.002 0.978 0.002 6.346 0.307 0.842 -4.5 0.312 0.03629 -0.150 0.459 0.002 0.977 0.002 8.585 0.308 0.731 -4.0 0.375 0.03187 -0.154 0.083 0.002 0.987 0.003 11.776 0.309 0.659 -3.5 0.438 0.02982 -0.157 0.081 0.002 0.987 0.003 14.684 0.310 0.609 -3.0 0.499 0.02768 -0.161 0.052 0.003 0.988 0.003 18.038 0.312 0.573 -2.5 0.559 0.02616 -0.165 0.049 0.003 0.988 0.004 21.373 0.313 0.545 -2.0 0.618 0.02607 -0.168 0.047 0.012 0.988 0.014 23.687 0.314 0.523 -1.5 0.675 0.02477 -0.172 0.046 0.013 0.989 0.015 27.268 0.316 0.505 -1.0 0.732 0.00882 -0.176 0.045 0.014 0.051 0.017 83.012 0.332 0.490 -0.5 0.781 0.00879 -0.181 0.045 0.017 0.050 0.797 88.795 -0.326 0.482 0.0 0.719 0.01458 -0.184 0.044 0.031 0.049 0.034 49.306 -0.087 0.505 0.5 0.761 0.01651 -0.187 0.044 0.032 0.048 0.035 46.110 0.341 0.496 1.0 0.803 0.01859 -0.191 0.044 0.033 0.047 0.037 43.215 0.341 0.488 1.5 0.846 0.02498 -0.195 0.043 0.035 0.047 0.853 33.854 0.341 0.481 2.0 0.888 0.02776 -0.199 0.043 0.146 0.046 0.847 31.975 0.342 0.474 2.5 0.929 0.03095 -0.203 0.043 0.605 0.046 0.627 30.008 0.342 0.468 3.0 0.971 0.03333 -0.207 0.043 0.606 0.046 0.628 29.126 0.342 0.463 3.5 1.012 0.03577 -0.210 0.042 0.607 0.045 0.631 28.288 0.343 0.458 4.0 1.052 0.03837 -0.214 0.042 0.608 0.046 0.632 27.427 0.343 0.453 4.5 1.094 0.04105 -0.218 0.042 0.609 0.045 0.635 26.641 0.342 0.449 5.0 1.135 0.04413 -0.222 0.042 0.610 0.045 0.638 25.712 0.343 0.445 5.5 1.175 0.04724 -0.226 0.042 0.611 0.045 0.642 24.872 0.354 0.442 6.0 1.209 0.04896 -0.229 0.025 0.611 0.051 0.644 24.690 0.354 0.440 6.5 1.248 0.05211 -0.233 0.024 0.612 0.050 0.648 23.958 0.345 0.437 7.0 1.287 0.05588 -0.237 0.022 0.614 0.049 0.651 23.037 0.347 0.434 7.5 1.326 0.06008 -0.241 0.021 0.615 0.047 0.655 22.070 0.235 0.432 8.0 1.528 0.05037 -0.233 0.001 0.615 0.698 0.660 30.341 0.243 0.403 8.5 1.541 0.05488 -0.239 0.001 0.617 0.654 0.663 28.083 -0.699 0.405 9.0 1.510 0.05467 -0.250 0.001 0.617 0.001 0.665 27.630 -5.521 0.416 9.5 1.539 0.05968 -0.254 0.001 0.619 0.001 0.667 25.784 0.387 0.415 10.0 1.563 0.06525 -0.257 0.000 0.620 0.001 0.669 23.956 0.410 0.415 10.5 1.584 0.07173 -0.261 0.000 0.621 0.001 0.672 22.078 0.440 0.415 11.0 1.601 0.07987 -0.265 0.000 0.621 0.001 0.674 20.043 0.493 0.415 11.5 1.613 0.08830 -0.268 0.000 0.623 0.001 0.677 18.269 0.600 0.416 12.0 1.621 0.09713 -0.272 0.000 0.624 0.000 0.680 16.691 0.866 0.418 12.5 1.625 0.10805 -0.275 0.000 0.625 0.000 0.683 15.037 3.639 0.419 13.0 1.623 0.11492 -0.279 0.000 0.627 0.000 0.686 14.125 -0.773 0.422 13.5 1.618 0.12788 -0.282 0.000 0.628 0.000 0.689 12.651 -0.200 0.425 14.0 1.608 0.13874 -0.286 0.000 0.630 0.000 0.721 11.589 -0.042 0.428 14.5 1.594 0.15556 -0.289 0.000 0.639 0.000 0.725 10.247 0.042 0.431 15.0 1.575 0.16762 -0.293 0.000 0.649 0.000 0.729 9.394 0.072 0.436 Name = FX 63-158 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 -0.231 0.21294 -0.074 0.930 0.003 0.955 0.004 -1.084 0.461 -0.069 -14.5 -0.214 0.19234 -0.077 0.929 0.003 0.955 0.004 -1.114 0.448 -0.110 -14.0 -0.195 0.16849 -0.081 0.928 0.003 0.956 0.004 -1.160 0.427 -0.162 -13.5 -0.175 0.16535 -0.084 0.926 0.003 0.956 0.004 -1.055 0.411 -0.232 -13.0 -0.151 0.14787 -0.088 0.924 0.003 0.957 0.004 -1.023 0.396 -0.330 -12.5 -0.126 0.13490 -0.091 0.875 0.002 0.965 0.004 -0.932 0.383 -0.476 -12.0 -0.098 0.11971 -0.095 0.874 0.003 0.965 0.004 -0.817 0.375 -0.719 -11.5 -0.068 0.11158 -0.098 0.872 0.002 0.966 0.003 -0.611 0.368 -1.193 -11.0 -0.037 0.09886 -0.102 0.870 0.002 0.966 0.003 -0.369 0.360 -2.545 -10.5 -0.003 0.08801 -0.106 0.596 0.002 0.980 0.003 -0.031 0.230 -39.112 -10.0 -0.393 0.08153 -0.109 0.592 0.002 0.980 0.003 -4.825 0.228 -0.028 -9.5 -0.335 0.07593 -0.113 0.530 0.002 0.982 0.003 -4.407 0.311 -0.087 -9.0 -0.274 0.06769 -0.117 0.527 0.002 0.982 0.003 -4.045 0.309 -0.176 -8.5 -0.211 0.06062 -0.120 0.525 0.002 0.982 0.003 -3.483 0.308 -0.320 -8.0 -0.147 0.05603 -0.124 0.522 0.002 0.983 0.003 -2.624 0.307 -0.593 -7.5 -0.082 0.05011 -0.128 0.519 0.002 0.983 0.003 -1.635 0.306 -1.308 -7.0 -0.016 0.04663 -0.131 0.466 0.002 0.984 0.003 -0.346 0.306 -7.885 -6.5 0.050 0.04226 -0.135 0.465 0.002 0.984 0.003 1.181 0.306 2.954 -6.0 0.116 0.03935 -0.139 0.463 0.002 0.984 0.002 2.948 0.306 1.446 -5.5 0.182 0.03614 -0.142 0.462 0.002 0.984 0.002 5.030 0.307 1.034 -5.0 0.247 0.03344 -0.146 0.460 0.002 0.984 0.002 7.387 0.307 0.842 -4.5 0.312 0.03108 -0.150 0.459 0.002 0.984 0.002 10.025 0.308 0.731 -4.0 0.375 0.02885 -0.154 0.083 0.002 0.991 0.003 13.008 0.309 0.659 -3.5 0.438 0.02708 -0.157 0.081 0.002 0.991 0.003 16.171 0.310 0.609 -3.0 0.499 0.02580 -0.161 0.052 0.003 0.991 0.003 19.351 0.375 0.573 -2.5 0.540 0.02078 -0.170 0.049 0.003 0.992 0.802 26.005 0.313 0.565 -2.0 0.618 0.02438 -0.168 0.047 0.012 0.992 0.014 25.330 0.266 0.523 -1.5 0.675 0.02345 -0.172 0.046 0.013 0.992 0.015 28.796 0.316 0.505 -1.0 0.732 0.00779 -0.176 0.045 0.014 0.052 0.017 93.934 0.336 0.490 -0.5 0.781 0.00703 -0.181 0.045 0.017 0.050 0.881 111.029 -0.289 0.482 0.0 0.718 0.01331 -0.184 0.044 0.031 0.050 0.034 53.939 -0.056 0.506 0.5 0.761 0.01509 -0.187 0.044 0.032 0.049 0.035 50.427 0.340 0.496 1.0 0.803 0.01701 -0.191 0.044 0.033 0.048 0.037 47.189 0.341 0.488 1.5 0.845 0.02343 -0.195 0.043 0.035 0.047 0.997 36.073 0.341 0.481 2.0 0.887 0.02555 -0.199 0.043 0.146 0.047 0.938 34.718 0.342 0.474 2.5 0.928 0.02709 -0.203 0.043 0.605 0.047 0.631 34.278 0.342 0.468 3.0 0.970 0.02923 -0.207 0.043 0.606 0.046 0.634 33.198 0.342 0.463 3.5 1.011 0.03152 -0.210 0.042 0.607 0.046 0.638 32.082 0.343 0.458 4.0 1.052 0.03372 -0.214 0.042 0.608 0.046 0.640 31.202 0.343 0.454 4.5 1.093 0.03610 -0.218 0.042 0.609 0.045 0.644 30.292 0.342 0.449 5.0 1.134 0.03875 -0.222 0.042 0.610 0.045 0.648 29.276 0.343 0.445 5.5 1.175 0.04141 -0.226 0.042 0.611 0.045 0.653 28.364 0.205 0.442 6.0 1.545 0.03236 -0.203 0.025 0.611 0.983 0.657 47.752 0.214 0.382 6.5 1.506 0.03469 -0.214 0.024 0.612 0.871 0.662 43.409 0.121 0.392 7.0 1.285 0.04930 -0.237 0.022 0.614 0.051 0.664 26.071 0.101 0.434 7.5 1.324 0.05278 -0.241 0.021 0.615 0.050 0.666 25.084 0.223 0.432 8.0 1.578 0.04197 -0.229 0.001 0.615 0.763 0.669 37.604 0.229 0.395 8.5 1.588 0.04582 -0.235 0.001 0.617 0.716 0.672 34.664 -0.059 0.398 9.0 1.509 0.04865 -0.250 0.001 0.617 0.001 0.674 31.020 -0.119 0.416 9.5 1.538 0.05258 -0.254 0.001 0.619 0.001 0.677 29.244 0.386 0.415 10.0 1.562 0.05718 -0.257 0.000 0.620 0.001 0.680 27.321 0.410 0.415 10.5 1.583 0.06248 -0.261 0.000 0.621 0.001 0.683 25.334 0.439 0.415 11.0 1.600 0.06835 -0.265 0.000 0.621 0.001 0.686 23.414 0.490 0.415 11.5 1.613 0.07492 -0.268 0.000 0.623 0.001 0.689 21.526 0.600 0.416 12.0 1.621 0.08227 -0.272 0.000 0.624 0.001 0.723 19.700 0.850 0.418 12.5 1.624 0.08937 -0.275 0.000 0.625 0.000 0.729 18.176 3.594 0.419 13.0 1.623 0.09665 -0.279 0.000 0.627 0.000 0.737 16.790 -0.775 0.422 13.5 1.618 0.10506 -0.282 0.000 0.628 0.000 0.744 15.397 -0.201 0.425 14.0 1.607 0.11616 -0.286 0.000 0.630 0.000 0.804 13.837 -0.039 0.428 14.5 1.593 0.12361 -0.289 0.000 0.639 0.000 1.000 12.891 0.042 0.432 15.0 1.574 0.13276 -0.293 0.000 0.649 0.000 1.000 11.856 0.072 0.436 Name = FX 63-158 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 -0.231 0.18701 -0.074 0.930 0.003 0.956 0.004 -1.234 0.461 -0.069 -14.5 -0.214 0.17271 -0.077 0.929 0.003 0.957 0.004 -1.240 0.448 -0.110 -14.0 -0.195 0.15024 -0.081 0.928 0.003 0.957 0.004 -1.300 0.427 -0.163 -13.5 -0.174 0.14795 -0.084 0.926 0.003 0.958 0.004 -1.179 0.411 -0.233 -13.0 -0.151 0.13429 -0.088 0.924 0.003 0.959 0.004 -1.126 0.396 -0.330 -12.5 -0.126 0.11761 -0.091 0.875 0.002 0.967 0.004 -1.069 0.384 -0.476 -12.0 -0.098 0.10528 -0.095 0.874 0.003 0.968 0.004 -0.929 0.375 -0.720 -11.5 -0.068 0.09881 -0.098 0.872 0.002 0.968 0.003 -0.689 0.368 -1.195 -11.0 -0.036 0.08877 -0.102 0.870 0.002 0.968 0.003 -0.410 0.360 -2.552 -10.5 -0.003 0.07994 -0.106 0.596 0.002 0.982 0.003 -0.032 0.230 -40.671 -10.0 -0.393 0.07444 -0.109 0.592 0.002 0.982 0.003 -5.284 0.228 -0.028 -9.5 -0.335 0.06716 -0.113 0.530 0.002 0.983 0.003 -4.983 0.311 -0.087 -9.0 -0.274 0.06232 -0.117 0.527 0.002 0.983 0.003 -4.394 0.309 -0.176 -8.5 -0.211 0.05631 -0.120 0.525 0.002 0.984 0.003 -3.749 0.308 -0.320 -8.0 -0.147 0.05083 -0.124 0.522 0.002 0.984 0.003 -2.892 0.307 -0.593 -7.5 -0.082 0.04587 -0.128 0.519 0.002 0.984 0.003 -1.785 0.306 -1.308 -7.0 -0.016 0.04285 -0.131 0.466 0.002 0.985 0.003 -0.377 0.306 -7.885 -6.5 0.050 0.03979 -0.135 0.465 0.002 0.985 0.003 1.255 0.306 2.954 -6.0 0.116 0.03652 -0.139 0.463 0.002 0.986 0.002 3.176 0.306 1.446 -5.5 0.182 0.03360 -0.142 0.462 0.002 0.986 0.002 5.409 0.307 1.034 -5.0 0.247 0.03128 -0.146 0.460 0.002 0.986 0.002 7.897 0.307 0.842 -4.5 0.312 0.02901 -0.150 0.459 0.002 0.986 0.003 10.741 0.308 0.731 -4.0 0.375 0.02910 -0.154 0.083 0.002 0.992 0.003 12.894 0.309 0.659 -3.5 0.438 0.02756 -0.157 0.081 0.002 0.992 0.003 15.886 0.310 0.609 -3.0 0.499 0.02629 -0.161 0.052 0.003 0.993 0.003 18.995 0.392 0.573 -2.5 0.536 0.02062 -0.171 0.049 0.003 0.993 0.847 25.989 0.313 0.570 -2.0 0.618 0.02498 -0.168 0.047 0.012 0.994 0.014 24.723 0.257 0.523 -1.5 0.675 0.02391 -0.172 0.046 0.013 0.994 0.015 28.249 0.316 0.505 -1.0 0.732 0.02327 -0.176 0.045 0.014 0.994 0.017 31.448 0.338 0.490 -0.5 0.781 0.00633 -0.182 0.045 0.017 0.051 0.926 123.372 -0.267 0.483 0.0 0.717 0.01275 -0.184 0.044 0.031 0.050 0.034 56.239 -0.034 0.506 0.5 0.760 0.01448 -0.187 0.044 0.032 0.049 0.036 52.482 0.340 0.497 1.0 0.802 0.01634 -0.191 0.044 0.033 0.049 0.038 49.089 0.341 0.488 1.5 0.845 0.02308 -0.195 0.043 0.035 0.048 0.997 36.596 0.341 0.481 2.0 0.887 0.02506 -0.199 0.043 0.146 0.047 0.998 35.378 0.342 0.474 2.5 0.928 0.02546 -0.203 0.043 0.605 0.047 0.638 36.444 0.342 0.468 3.0 0.970 0.02744 -0.207 0.043 0.606 0.046 0.641 35.352 0.342 0.463 3.5 1.011 0.02960 -0.210 0.042 0.607 0.046 0.647 34.153 0.343 0.458 4.0 1.052 0.03169 -0.214 0.042 0.608 0.046 0.649 33.193 0.343 0.454 4.5 1.093 0.03393 -0.218 0.042 0.609 0.046 0.654 32.215 0.342 0.449 5.0 1.134 0.03640 -0.222 0.042 0.610 0.045 0.660 31.157 0.343 0.446 5.5 1.175 0.03871 -0.226 0.042 0.611 0.045 0.663 30.341 0.205 0.442 6.0 1.566 0.02675 -0.202 0.025 0.611 1.000 0.666 58.562 0.201 0.379 6.5 1.623 0.02753 -0.204 0.024 0.612 1.000 0.668 58.969 0.277 0.375 7.0 1.680 0.02675 -0.205 0.022 0.614 1.000 0.671 62.795 0.127 0.372 7.5 1.322 0.04976 -0.241 0.021 0.615 0.051 0.674 26.574 -0.131 0.432 8.0 1.631 0.03704 -0.224 0.001 0.615 0.829 0.677 44.026 0.219 0.387 8.5 1.632 0.04067 -0.231 0.001 0.617 0.771 0.680 40.139 0.986 0.392 9.0 1.648 0.04373 -0.237 0.001 0.617 0.737 0.683 37.679 0.012 0.394 9.5 1.537 0.04957 -0.254 0.001 0.619 0.001 0.686 31.005 0.007 0.415 10.0 1.561 0.05376 -0.257 0.000 0.620 0.001 0.690 29.042 0.409 0.415 10.5 1.582 0.05841 -0.261 0.000 0.621 0.001 0.724 27.087 0.437 0.415 11.0 1.600 0.06372 -0.265 0.000 0.621 0.001 0.730 25.106 0.490 0.415 11.5 1.612 0.06956 -0.268 0.000 0.623 0.001 0.737 23.173 0.595 0.416 12.0 1.620 0.07507 -0.272 0.000 0.624 0.001 0.745 21.585 0.849 0.418 12.5 1.624 0.08292 -0.275 0.000 0.625 0.001 0.803 19.583 3.572 0.420 13.0 1.623 0.08360 -0.279 0.000 0.627 0.001 1.000 19.407 -0.822 0.422 13.5 1.617 0.09079 -0.282 0.000 0.628 0.000 1.000 17.813 -0.201 0.425 14.0 1.607 0.09919 -0.286 0.000 0.630 0.000 1.000 16.202 -0.039 0.428 14.5 1.593 0.11045 -0.289 0.000 0.639 0.000 1.000 14.424 0.042 0.432 15.0 1.574 0.11827 -0.293 0.000 0.649 0.000 1.000 13.307 0.072 0.436 Name = FX 63-158 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 -0.231 0.17206 -0.074 0.930 0.003 0.957 0.004 -1.340 0.463 -0.069 -14.5 -0.214 0.14854 -0.077 0.929 0.003 0.958 0.004 -1.442 0.448 -0.110 -14.0 -0.195 0.08859 -0.081 0.928 0.003 0.958 0.004 -2.204 0.427 -0.163 -13.5 -0.174 0.12728 -0.084 0.926 0.003 0.959 0.004 -1.370 0.411 -0.233 -13.0 -0.151 0.11710 -0.088 0.924 0.003 0.960 0.004 -1.291 0.396 -0.330 -12.5 -0.126 0.10748 -0.091 0.875 0.002 0.969 0.004 -1.169 0.383 -0.477 -12.0 -0.098 0.09691 -0.095 0.874 0.003 0.970 0.004 -1.008 0.375 -0.721 -11.5 -0.068 0.09142 -0.098 0.872 0.002 0.970 0.004 -0.744 0.368 -1.197 -11.0 -0.036 0.08295 -0.102 0.870 0.002 0.970 0.003 -0.438 0.360 -2.560 -10.5 -0.003 0.07289 -0.106 0.596 0.002 0.983 0.003 -0.035 0.230 -40.671 -10.0 -0.393 0.06828 -0.109 0.592 0.002 0.983 0.003 -5.761 0.228 -0.028 -9.5 -0.335 0.06374 -0.113 0.530 0.002 0.984 0.003 -5.251 0.311 -0.087 -9.0 -0.274 0.05759 -0.117 0.527 0.002 0.984 0.003 -4.754 0.309 -0.176 -8.5 -0.211 0.05255 -0.120 0.525 0.002 0.985 0.003 -4.017 0.308 -0.320 -8.0 -0.147 0.04875 -0.124 0.522 0.002 0.985 0.003 -3.016 0.307 -0.593 -7.5 -0.082 0.04422 -0.128 0.519 0.002 0.985 0.003 -1.852 0.306 -1.308 -7.0 -0.016 0.04066 -0.131 0.466 0.002 0.986 0.003 -0.397 0.306 -7.885 -6.5 0.050 0.03787 -0.135 0.465 0.002 0.986 0.003 1.318 0.306 2.954 -6.0 0.116 0.03526 -0.139 0.463 0.002 0.986 0.002 3.289 0.306 1.446 -5.5 0.182 0.03229 -0.142 0.462 0.002 0.987 0.002 5.629 0.307 1.034 -5.0 0.247 0.02987 -0.146 0.460 0.002 0.987 0.002 8.271 0.307 0.842 -4.5 0.312 0.02772 -0.150 0.459 0.002 0.987 0.003 11.241 0.308 0.731 -4.0 0.375 0.02902 -0.154 0.083 0.002 0.993 0.003 12.932 0.309 0.659 -3.5 0.438 0.02791 -0.157 0.081 0.002 0.994 0.003 15.691 0.310 0.609 -3.0 0.499 0.02709 -0.161 0.052 0.003 0.994 0.003 18.434 0.402 0.573 -2.5 0.536 0.02102 -0.172 0.049 0.003 0.995 0.884 25.490 0.313 0.571 -2.0 0.618 0.02552 -0.168 0.047 0.012 0.995 0.015 24.202 0.250 0.523 -1.5 0.675 0.02473 -0.172 0.046 0.013 0.995 0.016 27.304 0.359 0.505 -1.0 0.720 0.02232 -0.180 0.045 0.014 0.996 0.935 32.232 0.340 0.500 -0.5 0.781 0.02315 -0.182 0.045 0.017 0.996 0.954 33.731 -0.991 0.483 0.0 0.716 0.01247 -0.184 0.044 0.031 0.051 0.035 57.428 -0.015 0.506 0.5 0.759 0.01418 -0.187 0.044 0.032 0.050 0.036 53.555 0.340 0.497 1.0 0.802 0.01592 -0.191 0.044 0.033 0.049 0.038 50.364 0.340 0.488 1.5 0.844 0.02279 -0.195 0.043 0.035 0.048 0.998 37.053 0.341 0.481 2.0 0.886 0.02468 -0.199 0.043 0.146 0.047 0.998 35.914 0.342 0.474 2.5 0.928 0.02446 -0.203 0.043 0.605 0.047 0.645 37.919 0.342 0.469 3.0 0.970 0.02639 -0.207 0.043 0.606 0.046 0.649 36.748 0.342 0.463 3.5 1.011 0.02848 -0.210 0.042 0.607 0.046 0.656 35.496 0.343 0.458 4.0 1.052 0.03050 -0.214 0.042 0.608 0.046 0.660 34.481 0.343 0.454 4.5 1.093 0.03266 -0.218 0.042 0.609 0.046 0.663 33.464 0.342 0.449 5.0 1.134 0.03502 -0.222 0.042 0.610 0.045 0.666 32.385 0.343 0.446 5.5 1.174 0.03723 -0.226 0.042 0.611 0.045 0.669 31.540 0.205 0.442 6.0 1.566 0.02451 -0.202 0.025 0.611 1.000 0.672 63.894 0.201 0.379 6.5 1.623 0.02363 -0.204 0.024 0.612 1.000 0.675 68.697 0.277 0.375 7.0 1.680 0.02299 -0.205 0.022 0.614 1.000 0.678 73.072 0.277 0.372 7.5 1.735 0.02480 -0.207 0.021 0.615 1.000 0.681 69.967 -1.006 0.369 8.0 1.668 0.03401 -0.220 0.001 0.615 0.874 0.685 49.037 -0.099 0.382 8.5 1.679 0.03695 -0.226 0.001 0.617 0.828 0.688 45.427 1.510 0.385 9.0 1.679 0.04024 -0.233 0.001 0.617 0.776 0.702 41.715 0.058 0.389 9.5 1.536 0.04807 -0.254 0.001 0.619 0.001 0.726 31.953 0.046 0.415 10.0 1.561 0.05183 -0.257 0.000 0.620 0.001 0.733 30.115 0.407 0.415 10.5 1.582 0.05600 -0.261 0.000 0.621 0.001 0.742 28.244 0.437 0.415 11.0 1.599 0.06096 -0.265 0.000 0.621 0.001 0.749 26.232 0.490 0.415 11.5 1.611 0.06348 -0.268 0.000 0.623 0.001 1.000 25.386 0.594 0.416 12.0 1.620 0.06837 -0.272 0.000 0.624 0.001 1.000 23.691 0.833 0.418 12.5 1.624 0.07386 -0.275 0.000 0.625 0.001 1.000 21.983 3.530 0.420 13.0 1.622 0.07947 -0.279 0.000 0.627 0.001 1.000 20.410 -0.824 0.422 13.5 1.617 0.08508 -0.282 0.000 0.628 0.000 1.000 19.006 -0.210 0.425 14.0 1.607 0.09250 -0.286 0.000 0.630 0.000 1.000 17.370 -0.042 0.428 14.5 1.593 0.10069 -0.289 0.000 0.639 0.000 1.000 15.823 0.040 0.432 15.0 1.574 0.10749 -0.293 0.000 0.649 0.000 1.000 14.642 0.072 0.436