Name = GOE 279 (DAIMLER X) 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 -0.213 0.31635 0.006 0.808 0.002 0.839 0.004 -0.672 0.704 0.277 -14.5 -0.204 0.28091 0.002 0.808 0.002 0.837 0.004 -0.728 0.661 0.260 -14.0 -0.194 0.26401 -0.002 0.800 0.003 0.837 0.004 -0.737 0.595 0.241 -13.5 -0.183 0.22775 -0.006 0.800 0.003 0.842 0.004 -0.802 0.545 0.220 -13.0 -0.169 0.21900 -0.009 0.795 0.003 0.842 0.005 -0.772 0.510 0.195 -12.5 -0.154 0.19130 -0.013 0.789 0.003 0.842 0.005 -0.803 0.481 0.165 -12.0 -0.136 0.17435 -0.017 0.789 0.003 0.842 0.005 -0.781 0.455 0.126 -11.5 -0.117 0.16204 -0.021 0.784 0.003 0.842 0.005 -0.721 0.436 0.074 -11.0 -0.096 0.14892 -0.024 0.784 0.003 0.842 0.006 -0.642 0.422 -0.005 -10.5 -0.073 0.13269 -0.028 0.779 0.004 0.842 0.006 -0.548 0.409 -0.138 -10.0 -0.048 0.12229 -0.032 0.779 0.004 0.837 0.007 -0.392 0.398 -0.417 -9.5 -0.022 0.11063 -0.036 0.773 0.005 0.837 0.008 -0.195 0.228 -1.408 -9.0 -0.394 0.10072 -0.040 0.773 0.006 0.831 0.009 -3.910 0.226 0.150 -8.5 -0.343 0.09226 -0.043 0.768 0.007 0.837 0.011 -3.718 0.323 0.124 -8.0 -0.290 0.08465 -0.047 0.768 0.009 0.837 0.013 -3.431 0.321 0.088 -7.5 -0.236 0.07601 -0.051 0.763 0.011 0.837 0.014 -3.110 0.320 0.034 -7.0 -0.181 0.07344 -0.055 0.757 0.013 0.830 0.014 -2.467 0.319 -0.052 -6.5 -0.125 0.06533 -0.059 0.754 0.013 0.830 0.014 -1.915 0.318 -0.219 -6.0 -0.068 0.06054 -0.063 0.751 0.013 0.830 0.015 -1.131 0.318 -0.663 -5.5 -0.012 0.05594 -0.066 0.748 0.014 0.827 0.015 -0.207 0.318 -5.486 -5.0 0.045 0.05061 -0.070 0.745 0.014 0.827 0.015 0.895 0.318 1.800 -4.5 0.102 0.04781 -0.074 0.742 0.014 0.827 0.016 2.130 0.318 0.977 -4.0 0.158 0.04388 -0.078 0.742 0.014 0.821 0.016 3.602 0.319 0.743 -3.5 0.214 0.03912 -0.082 0.739 0.016 0.818 0.017 5.465 0.319 0.632 -3.0 0.269 0.03680 -0.086 0.736 0.016 0.815 0.018 7.311 0.320 0.568 -2.5 0.324 0.03400 -0.089 0.733 0.016 0.812 0.018 9.523 0.321 0.526 -2.0 0.378 0.03169 -0.093 0.727 0.016 0.812 0.017 11.926 0.321 0.497 -1.5 0.432 0.02980 -0.097 0.724 0.015 0.809 0.017 14.482 0.322 0.475 -1.0 0.484 0.02768 -0.101 0.721 0.016 0.803 0.018 17.500 0.323 0.458 -0.5 0.537 0.02618 -0.105 0.575 0.017 0.876 0.019 20.497 0.430 0.445 0.0 0.527 0.02368 -0.109 0.545 0.017 0.879 0.020 22.246 0.386 0.456 0.5 0.582 0.02425 -0.111 0.518 0.019 0.882 0.021 23.995 0.291 0.441 1.0 0.637 0.02510 -0.113 0.488 0.020 0.885 0.022 25.380 0.292 0.428 1.5 0.690 0.02584 -0.115 0.466 0.022 0.882 0.025 26.697 0.275 0.417 2.0 0.773 0.02572 -0.117 0.288 0.024 0.934 0.035 30.073 0.274 0.401 2.5 0.825 0.02993 -0.119 0.272 0.043 0.928 0.963 27.576 0.294 0.394 3.0 0.875 0.03350 -0.121 0.260 0.908 0.919 0.934 26.120 0.255 0.388 3.5 0.985 0.03119 -0.119 0.024 0.913 1.000 0.937 31.571 0.250 0.371 4.0 1.041 0.02938 -0.121 0.022 0.916 1.000 0.947 35.445 0.081 0.366 4.5 0.848 0.03825 -0.143 0.020 0.918 0.025 0.953 22.181 0.086 0.418 5.0 0.888 0.04007 -0.146 0.019 0.924 0.023 0.953 22.149 0.345 0.415 5.5 0.926 0.04342 -0.150 0.018 0.929 0.022 0.954 21.332 0.346 0.412 6.0 0.964 0.04662 -0.154 0.017 0.937 0.021 0.954 20.683 0.347 0.409 6.5 1.001 0.05059 -0.157 0.017 0.945 0.020 0.954 19.795 0.348 0.407 7.0 1.038 0.05500 -0.161 0.016 0.953 0.020 0.954 18.880 0.349 0.405 7.5 1.075 0.06084 -0.164 0.016 0.953 0.019 0.954 17.663 0.349 0.403 8.0 1.111 0.06453 -0.168 0.016 0.953 0.019 0.955 17.216 0.350 0.401 8.5 1.146 0.07012 -0.172 0.016 0.953 0.018 0.955 16.348 0.352 0.400 9.0 1.181 0.07436 -0.175 0.016 0.957 0.018 0.958 15.880 0.352 0.398 9.5 1.216 0.08543 -0.179 0.016 0.957 0.018 0.958 14.229 0.354 0.397 10.0 1.249 0.09396 -0.182 0.015 0.957 0.018 0.958 13.289 0.355 0.396 10.5 1.282 0.09665 -0.186 0.015 0.957 0.017 0.958 13.264 0.356 0.395 11.0 1.314 0.10321 -0.189 0.014 0.957 0.017 0.958 12.730 0.365 0.394 11.5 1.342 0.11250 -0.193 0.015 0.957 0.016 0.959 11.930 0.389 0.393 12.0 1.363 0.12600 -0.196 0.014 0.952 0.016 0.953 10.818 0.431 0.394 12.5 1.380 0.14393 -0.199 0.013 0.952 0.016 0.953 9.587 0.471 0.395 13.0 1.394 0.15067 -0.203 0.013 0.952 0.015 0.954 9.251 0.531 0.395 13.5 1.404 0.16440 -0.206 0.013 0.952 0.015 0.954 8.538 0.686 0.397 14.0 1.409 0.16654 -0.209 0.012 0.952 0.014 0.954 8.461 1.202 0.399 14.5 1.411 0.17704 -0.213 0.010 0.958 0.014 0.959 7.967 -4.829 0.401 15.0 1.408 0.20480 -0.216 0.008 0.953 0.013 0.954 6.874 -0.926 0.403 Name = GOE 279 (DAIMLER X) 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 -0.213 0.24560 0.006 0.808 0.002 0.845 0.004 -0.866 0.704 0.277 -14.5 -0.204 0.21485 0.002 0.808 0.002 0.842 0.004 -0.951 0.661 0.260 -14.0 -0.194 0.20194 -0.002 0.800 0.003 0.842 0.005 -0.963 0.594 0.241 -13.5 -0.183 0.18283 -0.005 0.800 0.003 0.852 0.005 -0.999 0.545 0.220 -13.0 -0.169 0.16396 -0.009 0.795 0.003 0.852 0.005 -1.030 0.510 0.195 -12.5 -0.153 0.15292 -0.013 0.789 0.003 0.858 0.005 -1.004 0.480 0.165 -12.0 -0.136 0.13745 -0.017 0.789 0.003 0.852 0.005 -0.990 0.455 0.126 -11.5 -0.117 0.12540 -0.021 0.784 0.003 0.858 0.006 -0.930 0.436 0.073 -11.0 -0.095 0.11854 -0.024 0.784 0.003 0.852 0.006 -0.804 0.421 -0.006 -10.5 -0.072 0.10602 -0.028 0.779 0.004 0.858 0.007 -0.683 0.409 -0.139 -10.0 -0.048 0.09599 -0.032 0.779 0.004 0.847 0.008 -0.496 0.398 -0.421 -9.5 -0.021 0.08841 -0.036 0.773 0.005 0.853 0.009 -0.239 0.228 -1.444 -9.0 -0.394 0.08156 -0.040 0.773 0.006 0.847 0.010 -4.827 0.227 0.150 -8.5 -0.343 0.07480 -0.043 0.768 0.007 0.852 0.012 -4.586 0.323 0.124 -8.0 -0.290 0.06914 -0.047 0.768 0.009 0.852 0.013 -4.201 0.322 0.088 -7.5 -0.236 0.06618 -0.051 0.763 0.011 0.852 0.014 -3.572 0.320 0.035 -7.0 -0.181 0.05936 -0.055 0.757 0.013 0.848 0.014 -3.052 0.319 -0.052 -6.5 -0.125 0.05319 -0.059 0.754 0.013 0.848 0.014 -2.352 0.318 -0.219 -6.0 -0.068 0.04953 -0.063 0.751 0.013 0.848 0.015 -1.383 0.318 -0.663 -5.5 -0.012 0.04602 -0.066 0.748 0.014 0.848 0.015 -0.251 0.318 -5.486 -5.0 0.045 0.04283 -0.070 0.745 0.014 0.845 0.015 1.058 0.318 1.800 -4.5 0.102 0.03930 -0.074 0.742 0.014 0.848 0.016 2.592 0.318 0.977 -4.0 0.158 0.03598 -0.078 0.742 0.014 0.839 0.016 4.393 0.319 0.743 -3.5 0.214 0.03281 -0.082 0.739 0.016 0.836 0.017 6.515 0.319 0.632 -3.0 0.269 0.03015 -0.086 0.736 0.016 0.833 0.018 8.926 0.320 0.568 -2.5 0.324 0.02806 -0.089 0.733 0.016 0.830 0.018 11.540 0.321 0.526 -2.0 0.378 0.02646 -0.093 0.727 0.016 0.836 0.017 14.283 0.321 0.497 -1.5 0.432 0.02422 -0.097 0.724 0.015 0.830 0.017 17.819 0.322 0.475 -1.0 0.484 0.02230 -0.101 0.721 0.016 0.824 0.018 21.721 0.323 0.458 -0.5 0.537 0.02129 -0.105 0.575 0.017 0.925 0.019 25.207 0.363 0.445 0.0 0.552 0.01857 -0.109 0.545 0.017 0.931 0.020 29.719 0.329 0.447 0.5 0.610 0.01889 -0.111 0.518 0.019 0.937 0.021 32.279 0.283 0.431 1.0 0.668 0.01938 -0.112 0.488 0.020 0.944 0.023 34.473 0.284 0.418 1.5 0.723 0.01929 -0.114 0.466 0.022 0.944 0.025 37.495 0.267 0.408 2.0 0.814 0.02157 -0.115 0.288 0.024 1.000 0.043 37.719 0.264 0.391 2.5 0.871 0.02535 -0.116 0.272 0.043 1.000 0.965 34.336 0.277 0.384 3.0 0.928 0.02548 -0.118 0.260 0.908 1.000 0.937 36.404 0.277 0.377 3.5 0.985 0.02737 -0.119 0.024 0.913 1.000 0.939 35.975 0.277 0.371 4.0 1.041 0.02549 -0.121 0.022 0.916 1.000 0.950 40.854 0.277 0.366 4.5 1.098 0.02809 -0.122 0.020 0.918 1.000 0.953 39.092 0.088 0.362 5.0 0.886 0.03651 -0.146 0.019 0.924 0.024 0.953 24.268 0.092 0.415 5.5 0.925 0.03881 -0.150 0.018 0.929 0.023 0.954 23.830 0.345 0.412 6.0 0.963 0.04210 -0.154 0.017 0.937 0.022 0.954 22.874 0.347 0.410 6.5 1.000 0.04563 -0.157 0.017 0.945 0.021 0.954 21.920 0.347 0.407 7.0 1.038 0.04850 -0.161 0.016 0.953 0.020 0.954 21.394 0.347 0.405 7.5 1.074 0.05215 -0.164 0.016 0.953 0.020 0.954 20.601 0.349 0.403 8.0 1.110 0.05679 -0.168 0.016 0.953 0.019 0.955 19.549 0.351 0.401 8.5 1.146 0.06154 -0.172 0.016 0.953 0.019 0.955 18.616 0.352 0.400 9.0 1.180 0.06567 -0.175 0.016 0.957 0.019 0.958 17.970 0.351 0.398 9.5 1.216 0.07015 -0.179 0.016 0.957 0.018 0.958 17.327 0.352 0.397 10.0 1.249 0.07555 -0.182 0.015 0.957 0.018 0.958 16.529 0.356 0.396 10.5 1.282 0.08114 -0.186 0.015 0.957 0.017 0.958 15.797 0.358 0.395 11.0 1.313 0.08992 -0.189 0.014 0.957 0.017 0.958 14.606 0.365 0.394 11.5 1.342 0.09473 -0.193 0.015 0.957 0.017 0.959 14.164 0.388 0.394 12.0 1.363 0.10433 -0.196 0.014 0.952 0.016 0.953 13.064 0.429 0.394 12.5 1.380 0.11048 -0.199 0.013 0.952 0.016 0.953 12.489 0.470 0.395 13.0 1.394 0.12253 -0.203 0.013 0.952 0.016 0.954 11.373 0.534 0.396 13.5 1.403 0.13390 -0.206 0.013 0.952 0.015 0.954 10.481 0.693 0.397 14.0 1.409 0.13806 -0.209 0.012 0.952 0.015 0.954 10.203 1.306 0.399 14.5 1.410 0.14797 -0.213 0.010 0.958 0.015 0.959 9.527 -3.694 0.401 15.0 1.407 0.15648 -0.216 0.008 0.953 0.014 0.954 8.991 -0.944 0.404 Name = GOE 279 (DAIMLER X) 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 -0.213 0.20221 0.006 0.808 0.002 0.850 0.004 -1.051 0.700 0.277 -14.5 -0.204 0.18666 0.002 0.808 0.002 0.847 0.005 -1.094 0.659 0.260 -14.0 -0.194 0.17554 -0.002 0.800 0.003 0.853 0.005 -1.107 0.594 0.241 -13.5 -0.182 0.15580 -0.005 0.800 0.003 0.858 0.005 -1.171 0.544 0.220 -13.0 -0.169 0.14682 -0.009 0.795 0.003 0.863 0.005 -1.149 0.509 0.195 -12.5 -0.153 0.13632 -0.013 0.789 0.003 0.868 0.005 -1.124 0.480 0.165 -12.0 -0.136 0.12128 -0.017 0.789 0.003 0.863 0.006 -1.120 0.454 0.126 -11.5 -0.116 0.11287 -0.021 0.784 0.003 0.868 0.006 -1.031 0.436 0.073 -11.0 -0.095 0.10180 -0.024 0.784 0.003 0.863 0.007 -0.934 0.421 -0.006 -10.5 -0.072 0.09384 -0.028 0.779 0.004 0.868 0.008 -0.768 0.408 -0.141 -10.0 -0.047 0.08619 -0.032 0.779 0.004 0.858 0.008 -0.547 0.397 -0.427 -9.5 -0.021 0.07974 -0.036 0.773 0.005 0.863 0.010 -0.258 0.228 -1.488 -9.0 -0.394 0.07424 -0.039 0.773 0.006 0.863 0.011 -5.302 0.227 0.150 -8.5 -0.343 0.06742 -0.043 0.768 0.007 0.868 0.013 -5.087 0.324 0.124 -8.0 -0.290 0.06295 -0.047 0.768 0.009 0.863 0.014 -4.613 0.322 0.088 -7.5 -0.236 0.05737 -0.051 0.763 0.011 0.868 0.014 -4.121 0.321 0.035 -7.0 -0.181 0.05327 -0.055 0.757 0.013 0.867 0.014 -3.402 0.319 -0.052 -6.5 -0.125 0.04962 -0.059 0.754 0.013 0.867 0.015 -2.522 0.318 -0.219 -6.0 -0.068 0.04624 -0.062 0.751 0.013 0.867 0.015 -1.481 0.318 -0.663 -5.5 -0.012 0.04279 -0.066 0.748 0.014 0.867 0.015 -0.270 0.318 -5.486 -5.0 0.045 0.03882 -0.070 0.745 0.014 0.867 0.015 1.167 0.318 1.800 -4.5 0.102 0.03625 -0.074 0.742 0.014 0.867 0.016 2.810 0.318 0.977 -4.0 0.158 0.03346 -0.078 0.742 0.014 0.860 0.016 4.724 0.319 0.743 -3.5 0.214 0.03016 -0.082 0.739 0.016 0.854 0.018 7.089 0.319 0.632 -3.0 0.269 0.02786 -0.086 0.736 0.016 0.854 0.018 9.658 0.320 0.568 -2.5 0.324 0.02553 -0.089 0.733 0.016 0.851 0.018 12.685 0.321 0.526 -2.0 0.378 0.02351 -0.093 0.727 0.016 0.854 0.017 16.075 0.321 0.497 -1.5 0.432 0.02186 -0.097 0.724 0.015 0.851 0.018 19.741 0.322 0.475 -1.0 0.484 0.01971 -0.101 0.721 0.016 0.842 0.018 24.583 0.323 0.458 -0.5 0.537 0.01875 -0.105 0.575 0.017 1.000 0.019 28.618 0.324 0.445 0.0 0.588 0.01636 -0.109 0.545 0.017 1.000 0.020 35.956 0.300 0.435 0.5 0.644 0.01650 -0.110 0.518 0.019 1.000 0.022 39.055 0.278 0.421 1.0 0.701 0.01696 -0.112 0.488 0.020 1.000 0.023 41.292 0.278 0.410 1.5 0.757 0.01677 -0.113 0.466 0.022 1.000 0.030 45.139 0.278 0.400 2.0 0.814 0.01967 -0.115 0.288 0.024 1.000 0.050 41.360 0.277 0.391 2.5 0.871 0.02270 -0.116 0.272 0.043 1.000 0.966 38.353 0.277 0.384 3.0 0.928 0.02235 -0.118 0.260 0.908 1.000 0.939 41.500 0.277 0.377 3.5 0.985 0.02501 -0.119 0.024 0.913 1.000 0.942 39.366 0.277 0.371 4.0 1.041 0.02144 -0.121 0.022 0.916 1.000 0.953 48.573 0.277 0.366 4.5 1.098 0.02578 -0.122 0.020 0.918 1.000 0.953 42.608 0.089 0.362 5.0 0.885 0.03454 -0.146 0.019 0.924 0.025 0.953 25.616 0.093 0.415 5.5 0.924 0.03707 -0.150 0.018 0.929 0.024 0.954 24.917 0.345 0.412 6.0 0.962 0.03955 -0.154 0.017 0.937 0.022 0.954 24.322 0.346 0.410 6.5 0.999 0.04279 -0.157 0.017 0.945 0.022 0.954 23.358 0.347 0.407 7.0 1.037 0.04571 -0.161 0.016 0.953 0.021 0.954 22.685 0.347 0.405 7.5 1.074 0.04923 -0.164 0.016 0.953 0.020 0.954 21.807 0.349 0.403 8.0 1.110 0.05246 -0.168 0.016 0.953 0.020 0.955 21.156 0.350 0.401 8.5 1.145 0.05662 -0.172 0.016 0.953 0.019 0.955 20.225 0.352 0.400 9.0 1.180 0.06058 -0.175 0.016 0.957 0.019 0.958 19.474 0.350 0.399 9.5 1.216 0.06358 -0.179 0.016 0.957 0.018 0.958 19.117 0.353 0.397 10.0 1.248 0.07144 -0.182 0.015 0.957 0.018 0.958 17.472 0.356 0.396 10.5 1.281 0.07449 -0.186 0.015 0.957 0.017 0.958 17.202 0.356 0.395 11.0 1.313 0.07940 -0.189 0.014 0.957 0.017 0.958 16.541 0.365 0.394 11.5 1.342 0.08735 -0.193 0.015 0.957 0.017 0.959 15.358 0.389 0.394 12.0 1.363 0.09519 -0.196 0.014 0.952 0.016 0.953 14.314 0.431 0.394 12.5 1.379 0.10449 -0.199 0.013 0.952 0.017 0.953 13.201 0.470 0.395 13.0 1.393 0.11074 -0.203 0.013 0.952 0.016 0.954 12.583 0.527 0.396 13.5 1.403 0.11538 -0.206 0.013 0.952 0.015 0.954 12.164 0.701 0.397 14.0 1.408 0.12717 -0.209 0.012 0.952 0.016 0.954 11.073 1.489 0.399 14.5 1.409 0.13997 -0.213 0.010 0.958 0.016 0.959 10.065 -2.980 0.401 15.0 1.406 0.13896 -0.216 0.008 0.953 0.016 0.954 10.119 -0.963 0.404 Name = GOE 279 (DAIMLER X) 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 -0.212 0.18704 0.006 0.808 0.002 0.858 0.005 -1.136 0.699 0.277 -14.5 -0.204 0.16987 0.002 0.808 0.002 0.855 0.005 -1.202 0.659 0.260 -14.0 -0.194 0.15947 -0.002 0.800 0.003 0.858 0.005 -1.218 0.592 0.241 -13.5 -0.182 0.14635 -0.005 0.800 0.003 0.868 0.006 -1.246 0.544 0.220 -13.0 -0.169 0.13076 -0.009 0.795 0.003 0.874 0.006 -1.290 0.509 0.195 -12.5 -0.153 0.12125 -0.013 0.789 0.003 0.879 0.006 -1.263 0.478 0.165 -12.0 -0.136 0.11546 -0.017 0.789 0.003 0.874 0.006 -1.174 0.453 0.126 -11.5 -0.116 0.10549 -0.021 0.784 0.003 0.884 0.007 -1.100 0.435 0.073 -11.0 -0.095 0.09716 -0.024 0.784 0.003 0.879 0.008 -0.975 0.421 -0.007 -10.5 -0.072 0.08867 -0.028 0.779 0.004 0.884 0.008 -0.808 0.408 -0.142 -10.0 -0.047 0.08211 -0.032 0.779 0.004 0.874 0.009 -0.568 0.396 -0.434 -9.5 -0.020 0.07452 -0.036 0.773 0.005 0.879 0.011 -0.268 0.228 -1.536 -9.0 -0.394 0.06937 -0.039 0.773 0.006 0.874 0.012 -5.674 0.227 0.150 -8.5 -0.343 0.06266 -0.043 0.768 0.007 0.884 0.013 -5.473 0.324 0.124 -8.0 -0.290 0.06016 -0.047 0.768 0.009 0.879 0.014 -4.827 0.322 0.088 -7.5 -0.236 0.05243 -0.051 0.763 0.011 0.884 0.014 -4.509 0.321 0.035 -7.0 -0.181 0.04952 -0.055 0.757 0.013 0.882 0.014 -3.659 0.319 -0.052 -6.5 -0.125 0.04619 -0.059 0.754 0.013 0.885 0.015 -2.709 0.318 -0.219 -6.0 -0.068 0.04314 -0.062 0.751 0.013 0.885 0.015 -1.588 0.318 -0.663 -5.5 -0.012 0.03990 -0.066 0.748 0.014 0.885 0.015 -0.290 0.318 -5.486 -5.0 0.045 0.03717 -0.070 0.745 0.014 0.885 0.016 1.219 0.318 1.800 -4.5 0.102 0.03404 -0.074 0.742 0.014 0.888 0.016 2.993 0.318 0.977 -4.0 0.158 0.03128 -0.078 0.742 0.014 0.879 0.016 5.052 0.319 0.743 -3.5 0.214 0.02848 -0.082 0.739 0.016 0.876 0.018 7.506 0.319 0.632 -3.0 0.269 0.02606 -0.086 0.736 0.016 0.873 0.018 10.325 0.320 0.568 -2.5 0.324 0.02404 -0.089 0.733 0.016 0.870 0.018 13.471 0.321 0.526 -2.0 0.378 0.02221 -0.093 0.727 0.016 0.876 0.018 17.017 0.321 0.497 -1.5 0.432 0.02052 -0.097 0.724 0.015 0.873 0.018 21.027 0.322 0.475 -1.0 0.484 0.01845 -0.101 0.721 0.016 0.864 0.019 26.263 0.323 0.458 -0.5 0.537 0.01694 -0.105 0.575 0.017 1.000 0.019 31.679 0.324 0.445 0.0 0.588 0.01486 -0.109 0.545 0.017 1.000 0.021 39.588 0.300 0.435 0.5 0.644 0.01510 -0.110 0.518 0.019 1.000 0.022 42.673 0.278 0.421 1.0 0.701 0.01572 -0.112 0.488 0.020 1.000 0.023 44.564 0.278 0.410 1.5 0.757 0.01558 -0.113 0.466 0.022 1.000 0.035 48.579 0.278 0.400 2.0 0.814 0.02042 -0.115 0.288 0.024 1.000 0.967 39.851 0.277 0.391 2.5 0.871 0.02122 -0.116 0.272 0.043 1.000 0.968 41.027 0.277 0.384 3.0 0.928 0.02068 -0.118 0.260 0.908 1.000 0.942 44.865 0.277 0.377 3.5 0.985 0.02232 -0.119 0.024 0.913 1.000 0.945 44.114 0.277 0.371 4.0 1.041 0.02058 -0.121 0.022 0.916 1.000 0.953 50.604 0.277 0.366 4.5 1.098 0.02406 -0.122 0.020 0.918 1.000 0.953 45.647 0.276 0.362 5.0 1.155 0.02706 -0.124 0.019 0.924 1.000 0.954 42.684 0.094 0.357 5.5 0.922 0.03587 -0.150 0.018 0.929 0.025 0.954 25.717 0.097 0.413 6.0 0.961 0.03842 -0.154 0.017 0.937 0.023 0.954 25.010 0.346 0.410 6.5 0.999 0.04110 -0.157 0.017 0.945 0.022 0.954 24.297 0.346 0.407 7.0 1.036 0.04405 -0.161 0.016 0.953 0.021 0.954 23.519 0.347 0.405 7.5 1.073 0.04753 -0.164 0.016 0.953 0.021 0.954 22.568 0.349 0.403 8.0 1.109 0.05076 -0.168 0.016 0.953 0.020 0.955 21.846 0.349 0.402 8.5 1.145 0.05373 -0.172 0.016 0.953 0.020 0.955 21.306 0.351 0.400 9.0 1.179 0.05759 -0.175 0.016 0.957 0.020 0.958 20.480 0.351 0.399 9.5 1.215 0.06202 -0.179 0.016 0.957 0.018 0.958 19.591 0.352 0.397 10.0 1.248 0.06585 -0.182 0.015 0.957 0.018 0.958 18.955 0.356 0.396 10.5 1.281 0.07060 -0.186 0.015 0.957 0.018 0.958 18.146 0.358 0.395 11.0 1.313 0.07748 -0.189 0.014 0.957 0.018 0.958 16.942 0.364 0.394 11.5 1.342 0.08010 -0.193 0.015 0.957 0.017 0.959 16.748 0.387 0.394 12.0 1.363 0.08692 -0.196 0.014 0.952 0.016 0.953 15.677 0.431 0.394 12.5 1.379 0.09397 -0.199 0.013 0.952 0.017 0.953 14.678 0.470 0.395 13.0 1.393 0.09980 -0.203 0.013 0.952 0.016 0.954 13.961 0.530 0.396 13.5 1.403 0.10892 -0.206 0.013 0.952 0.015 0.954 12.882 0.717 0.397 14.0 1.408 0.12197 -0.209 0.012 0.952 0.016 0.954 11.541 1.539 0.399 14.5 1.408 0.12395 -0.213 0.010 0.958 0.017 0.959 11.362 -2.489 0.401 15.0 1.405 0.13103 -0.216 0.008 0.953 0.017 0.954 10.725 -0.817 0.404