Name = GOE 802 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 -0.268 0.26819 -0.031 0.779 0.014 0.837 0.015 -1.000 0.399 0.133 -14.5 -0.249 0.25552 -0.034 0.774 0.014 0.832 0.015 -0.973 0.395 0.113 -14.0 -0.228 0.24368 -0.037 0.769 0.014 0.837 0.015 -0.935 0.388 0.087 -13.5 -0.206 0.23298 -0.040 0.763 0.014 0.837 0.015 -0.883 0.381 0.055 -13.0 -0.182 0.22346 -0.043 0.758 0.014 0.837 0.015 -0.816 0.375 0.014 -12.5 -0.158 0.18857 -0.046 0.753 0.014 0.837 0.015 -0.836 0.370 -0.042 -12.0 -0.132 0.15510 -0.049 0.753 0.015 0.832 0.016 -0.853 0.366 -0.121 -11.5 -0.105 0.14820 -0.052 0.748 0.015 0.832 0.016 -0.710 0.362 -0.246 -11.0 -0.077 0.14188 -0.055 0.742 0.015 0.832 0.016 -0.542 0.358 -0.469 -10.5 -0.048 0.13565 -0.058 0.737 0.015 0.832 0.016 -0.351 0.355 -0.978 -10.0 -0.017 0.11735 -0.062 0.737 0.015 0.821 0.016 -0.145 0.233 -3.368 -9.5 -0.424 0.10736 -0.065 0.732 0.015 0.826 0.016 -3.949 0.232 0.097 -9.0 -0.367 0.10652 -0.068 0.727 0.015 0.826 0.016 -3.450 0.307 0.065 -8.5 -0.310 0.10996 -0.071 0.727 0.014 0.821 0.015 -2.819 0.307 0.020 -8.0 -0.252 0.09787 -0.075 0.721 0.014 0.821 0.015 -2.570 0.306 -0.046 -7.5 -0.192 0.08786 -0.078 0.716 0.014 0.821 0.015 -2.191 0.305 -0.154 -7.0 -0.133 0.07584 -0.081 0.711 0.015 0.811 0.016 -1.753 0.306 -0.360 -6.5 -0.073 0.07579 -0.084 0.707 0.015 0.807 0.016 -0.963 0.306 -0.907 -6.0 -0.013 0.06815 -0.088 0.696 0.015 0.811 0.016 -0.189 0.306 -6.553 -5.5 0.047 0.06237 -0.091 0.681 0.015 0.811 0.016 0.757 0.306 2.181 -5.0 0.107 0.05792 -0.095 0.667 0.015 0.811 0.016 1.853 0.307 1.132 -4.5 0.167 0.05563 -0.098 0.652 0.015 0.815 0.016 3.005 0.308 0.837 -4.0 0.227 0.05027 -0.102 0.641 0.015 0.811 0.016 4.510 0.308 0.698 -3.5 0.286 0.04785 -0.105 0.630 0.015 0.811 0.016 5.973 0.309 0.618 -3.0 0.344 0.04490 -0.109 0.619 0.015 0.807 0.016 7.669 0.310 0.565 -2.5 0.402 0.04169 -0.112 0.604 0.015 0.807 0.016 9.650 0.311 0.529 -2.0 0.459 0.03881 -0.116 0.570 0.015 0.815 0.016 11.840 0.312 0.502 -1.5 0.516 0.03733 -0.119 0.526 0.015 0.830 0.016 13.820 0.314 0.481 -1.0 0.572 0.03430 -0.123 0.493 0.015 0.833 0.016 16.664 0.315 0.465 -0.5 0.626 0.03337 -0.126 0.470 0.015 0.833 0.016 18.769 0.811 0.452 0.0 0.584 0.02980 -0.130 0.456 0.015 0.830 0.017 19.612 0.883 0.472 0.5 0.636 0.02982 -0.132 0.441 0.016 0.822 0.017 21.329 0.299 0.458 1.0 0.687 0.03014 -0.135 0.426 0.016 0.815 0.018 22.781 0.301 0.446 1.5 0.737 0.03080 -0.138 0.411 0.017 0.807 0.019 23.935 0.303 0.437 2.0 0.788 0.03273 -0.140 0.396 0.018 0.800 0.020 24.067 0.304 0.428 2.5 0.838 0.03313 -0.143 0.374 0.018 0.793 0.021 25.303 0.308 0.421 3.0 0.886 0.03430 -0.146 0.356 0.020 0.781 0.023 25.844 0.311 0.415 3.5 0.936 0.03919 -0.149 0.333 0.023 0.774 0.966 23.894 0.310 0.409 4.0 0.986 0.04214 -0.152 0.311 0.953 0.767 0.954 23.400 0.319 0.404 4.5 1.030 0.04423 -0.155 0.293 0.951 0.752 0.952 23.298 0.331 0.401 5.0 1.073 0.04643 -0.159 0.279 0.951 0.734 0.952 23.101 0.353 0.398 5.5 1.107 0.04894 -0.163 0.269 0.951 0.707 0.952 22.619 0.375 0.397 6.0 1.142 0.05130 -0.168 0.255 0.951 0.679 0.953 22.254 0.408 0.397 6.5 1.167 0.05479 -0.173 0.245 0.951 0.638 0.953 21.298 0.549 0.398 7.0 1.179 0.05975 -0.179 0.238 0.952 0.576 0.953 19.735 0.263 0.402 7.5 1.328 0.05615 -0.175 0.150 0.952 0.721 0.953 23.642 0.255 0.382 8.0 1.358 0.06002 -0.180 0.133 0.952 0.693 0.953 22.631 0.374 0.382 8.5 1.400 0.06191 -0.184 0.104 0.952 0.679 0.953 22.605 0.513 0.381 9.0 1.402 0.06866 -0.191 0.100 0.952 0.614 0.953 20.413 3.581 0.386 9.5 1.404 0.07497 -0.198 0.090 0.952 0.545 0.953 18.725 0.364 0.391 10.0 1.478 0.07656 -0.200 0.050 0.952 0.585 0.954 19.312 0.420 0.385 10.5 1.462 0.08400 -0.208 0.048 0.952 0.492 0.954 17.410 -0.325 0.392 11.0 1.451 0.09450 -0.216 0.044 0.952 0.400 0.954 15.356 -0.230 0.399 11.5 1.434 0.10630 -0.222 0.042 0.953 0.260 0.954 13.493 1.648 0.405 12.0 1.457 0.11434 -0.223 0.042 0.953 0.097 0.954 12.741 0.348 0.403 12.5 1.489 0.11968 -0.227 0.038 0.958 0.090 0.959 12.442 0.366 0.403 13.0 1.520 0.12659 -0.231 0.037 0.958 0.080 0.959 12.003 0.334 0.402 13.5 1.562 0.12904 -0.233 0.037 0.958 0.048 0.959 12.104 0.431 0.399 14.0 1.582 0.13180 -0.242 0.011 0.958 0.250 0.959 12.006 0.936 0.403 14.5 1.579 0.14554 -0.245 0.010 0.958 0.148 0.959 10.848 0.608 0.405 15.0 1.597 0.15467 -0.247 0.009 0.958 0.103 0.959 10.327 0.390 0.405 Name = GOE 802 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 -0.268 0.21880 -0.031 0.779 0.014 0.853 0.015 -1.226 0.399 0.133 -14.5 -0.249 0.20964 -0.034 0.774 0.014 0.847 0.015 -1.187 0.395 0.113 -14.0 -0.228 0.17989 -0.037 0.769 0.014 0.853 0.015 -1.267 0.387 0.087 -13.5 -0.206 0.17202 -0.040 0.763 0.014 0.853 0.015 -1.197 0.381 0.055 -13.0 -0.182 0.16529 -0.043 0.758 0.014 0.858 0.015 -1.104 0.375 0.014 -12.5 -0.158 0.15897 -0.046 0.753 0.014 0.858 0.015 -0.993 0.370 -0.042 -12.0 -0.132 0.13267 -0.049 0.753 0.015 0.853 0.016 -0.998 0.366 -0.121 -11.5 -0.105 0.11617 -0.052 0.748 0.015 0.853 0.016 -0.905 0.362 -0.246 -11.0 -0.077 0.11117 -0.055 0.742 0.015 0.853 0.016 -0.692 0.358 -0.469 -10.5 -0.048 0.10493 -0.058 0.737 0.015 0.853 0.016 -0.453 0.355 -0.978 -10.0 -0.017 0.10144 -0.062 0.737 0.015 0.842 0.016 -0.168 0.233 -3.353 -9.5 -0.424 0.09260 -0.065 0.732 0.015 0.847 0.016 -4.579 0.232 0.097 -9.0 -0.367 0.08477 -0.068 0.727 0.015 0.847 0.016 -4.335 0.307 0.065 -8.5 -0.310 0.08591 -0.071 0.727 0.014 0.842 0.015 -3.608 0.307 0.020 -8.0 -0.252 0.07727 -0.075 0.721 0.014 0.842 0.015 -3.255 0.306 -0.046 -7.5 -0.192 0.07519 -0.078 0.716 0.014 0.842 0.015 -2.560 0.305 -0.154 -7.0 -0.133 0.06522 -0.081 0.711 0.015 0.833 0.016 -2.038 0.306 -0.360 -6.5 -0.073 0.06131 -0.084 0.707 0.015 0.833 0.016 -1.191 0.306 -0.907 -6.0 -0.013 0.05535 -0.088 0.696 0.015 0.837 0.016 -0.233 0.306 -6.553 -5.5 0.047 0.05093 -0.091 0.681 0.015 0.841 0.016 0.927 0.306 2.181 -5.0 0.107 0.04787 -0.095 0.667 0.015 0.848 0.016 2.242 0.307 1.132 -4.5 0.167 0.04533 -0.098 0.652 0.015 0.852 0.016 3.688 0.308 0.837 -4.0 0.227 0.04275 -0.102 0.641 0.015 0.852 0.016 5.303 0.308 0.698 -3.5 0.286 0.03885 -0.105 0.630 0.015 0.852 0.016 7.356 0.309 0.618 -3.0 0.344 0.03649 -0.109 0.619 0.015 0.852 0.016 9.435 0.310 0.565 -2.5 0.402 0.03485 -0.112 0.604 0.015 0.856 0.016 11.544 0.311 0.529 -2.0 0.459 0.03241 -0.116 0.570 0.015 0.870 0.016 14.179 0.312 0.502 -1.5 0.516 0.03021 -0.119 0.526 0.015 0.889 0.016 17.081 0.314 0.481 -1.0 0.572 0.02823 -0.123 0.493 0.015 0.896 0.016 20.246 0.315 0.465 -0.5 0.626 0.02663 -0.126 0.470 0.015 0.896 0.017 23.522 0.396 0.452 0.0 0.621 0.02259 -0.130 0.456 0.015 0.896 0.017 27.488 0.364 0.459 0.5 0.676 0.02277 -0.132 0.441 0.016 0.893 0.017 29.687 0.288 0.445 1.0 0.730 0.02317 -0.134 0.426 0.016 0.889 0.018 31.530 0.290 0.434 1.5 0.785 0.02378 -0.136 0.411 0.017 0.885 0.019 32.997 0.291 0.424 2.0 0.839 0.02481 -0.139 0.396 0.018 0.881 0.020 33.826 0.292 0.415 2.5 0.893 0.02494 -0.141 0.374 0.018 0.878 0.021 35.824 0.293 0.408 3.0 0.947 0.02606 -0.143 0.356 0.020 0.874 0.023 36.360 0.294 0.401 3.5 1.001 0.03005 -0.146 0.333 0.023 0.870 0.968 33.325 0.295 0.395 4.0 1.055 0.03177 -0.148 0.311 0.953 0.867 0.954 33.207 0.299 0.390 4.5 1.106 0.03294 -0.151 0.293 0.951 0.859 0.952 33.560 0.304 0.386 5.0 1.157 0.03472 -0.153 0.279 0.951 0.852 0.952 33.310 0.312 0.383 5.5 1.202 0.03590 -0.157 0.269 0.951 0.838 0.952 33.483 0.319 0.380 6.0 1.249 0.03779 -0.160 0.255 0.951 0.828 0.953 33.057 0.327 0.378 6.5 1.290 0.03880 -0.164 0.245 0.951 0.810 0.953 33.250 0.354 0.377 7.0 1.325 0.04078 -0.168 0.238 0.952 0.786 0.953 32.502 0.289 0.377 7.5 1.407 0.04324 -0.168 0.150 0.952 0.821 0.953 32.547 0.285 0.369 8.0 1.446 0.04490 -0.172 0.133 0.952 0.803 0.953 32.217 0.340 0.369 8.5 1.491 0.04859 -0.176 0.104 0.952 0.793 0.953 30.691 0.366 0.368 9.0 1.521 0.04985 -0.181 0.100 0.952 0.766 0.953 30.505 0.410 0.369 9.5 1.553 0.05450 -0.186 0.090 0.952 0.742 0.953 28.494 0.380 0.369 10.0 1.591 0.05721 -0.190 0.050 0.952 0.727 0.954 27.808 0.411 0.369 10.5 1.614 0.06127 -0.195 0.048 0.952 0.697 0.954 26.348 0.595 0.371 11.0 1.627 0.06643 -0.202 0.044 0.952 0.652 0.954 24.492 1.608 0.374 11.5 1.625 0.07314 -0.210 0.042 0.953 0.592 0.954 22.220 -0.164 0.379 12.0 1.583 0.08201 -0.220 0.042 0.953 0.480 0.954 19.307 -0.078 0.389 12.5 1.573 0.09035 -0.227 0.038 0.958 0.410 0.959 17.413 -0.183 0.394 13.0 1.553 0.10071 -0.234 0.037 0.958 0.313 0.959 15.418 -0.004 0.400 13.5 1.543 0.11379 -0.235 0.037 0.958 0.085 0.959 13.558 0.298 0.402 14.0 1.665 0.10424 -0.239 0.011 0.958 0.413 0.959 15.978 0.339 0.393 14.5 1.654 0.11408 -0.245 0.010 0.958 0.354 0.959 14.503 -0.138 0.398 15.0 1.637 0.12438 -0.250 0.009 0.958 0.283 0.959 13.158 -0.046 0.403 Name = GOE 802 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 -0.268 0.18164 -0.031 0.779 0.014 0.863 0.015 -1.476 0.399 0.133 -14.5 -0.249 0.17406 -0.034 0.774 0.014 0.858 0.015 -1.429 0.395 0.113 -14.0 -0.228 0.16709 -0.037 0.769 0.014 0.868 0.015 -1.365 0.388 0.087 -13.5 -0.206 0.16060 -0.040 0.763 0.014 0.868 0.015 -1.282 0.381 0.055 -13.0 -0.182 0.14001 -0.043 0.758 0.014 0.874 0.015 -1.303 0.375 0.014 -12.5 -0.158 0.13455 -0.046 0.753 0.014 0.874 0.015 -1.173 0.370 -0.042 -12.0 -0.132 0.11479 -0.049 0.753 0.015 0.868 0.016 -1.153 0.366 -0.121 -11.5 -0.105 0.11021 -0.052 0.748 0.015 0.868 0.016 -0.955 0.362 -0.246 -11.0 -0.077 0.09785 -0.055 0.742 0.015 0.874 0.016 -0.786 0.358 -0.469 -10.5 -0.048 0.09174 -0.058 0.737 0.015 0.874 0.016 -0.518 0.355 -0.978 -10.0 -0.017 0.08867 -0.062 0.737 0.015 0.863 0.016 -0.193 0.233 -3.353 -9.5 -0.424 0.08133 -0.065 0.732 0.015 0.868 0.016 -5.213 0.232 0.097 -9.0 -0.367 0.07536 -0.068 0.727 0.015 0.868 0.016 -4.876 0.307 0.065 -8.5 -0.310 0.07559 -0.071 0.727 0.014 0.863 0.015 -4.101 0.307 0.020 -8.0 -0.252 0.07339 -0.075 0.721 0.014 0.863 0.015 -3.428 0.306 -0.046 -7.5 -0.192 0.06603 -0.078 0.716 0.014 0.863 0.015 -2.915 0.305 -0.154 -7.0 -0.133 0.05815 -0.081 0.711 0.015 0.856 0.016 -2.286 0.306 -0.360 -6.5 -0.073 0.05488 -0.084 0.707 0.015 0.856 0.016 -1.331 0.306 -0.907 -6.0 -0.013 0.05216 -0.088 0.696 0.015 0.863 0.016 -0.248 0.306 -6.553 -5.5 0.047 0.04633 -0.091 0.681 0.015 0.870 0.016 1.020 0.307 2.181 -5.0 0.107 0.04334 -0.095 0.667 0.015 0.878 0.016 2.476 0.307 1.132 -4.5 0.167 0.04121 -0.098 0.652 0.015 0.885 0.016 4.056 0.308 0.837 -4.0 0.227 0.03859 -0.102 0.641 0.015 0.885 0.016 5.874 0.308 0.698 -3.5 0.286 0.03587 -0.105 0.630 0.015 0.885 0.016 7.967 0.309 0.618 -3.0 0.344 0.03388 -0.109 0.619 0.015 0.889 0.016 10.164 0.310 0.565 -2.5 0.402 0.03145 -0.112 0.604 0.015 0.893 0.016 12.790 0.311 0.529 -2.0 0.459 0.02909 -0.116 0.570 0.015 0.908 0.016 15.798 0.312 0.502 -1.5 0.516 0.02758 -0.119 0.526 0.015 0.927 0.016 18.709 0.314 0.481 -1.0 0.572 0.02540 -0.123 0.493 0.015 0.935 0.016 22.501 0.315 0.465 -0.5 0.626 0.02389 -0.126 0.470 0.015 0.938 0.017 26.218 0.345 0.452 0.0 0.647 0.01956 -0.130 0.456 0.015 0.942 0.017 33.088 0.318 0.451 0.5 0.705 0.01986 -0.132 0.441 0.016 0.942 0.018 35.526 0.281 0.437 1.0 0.763 0.02028 -0.134 0.426 0.016 0.942 0.018 37.622 0.283 0.425 1.5 0.818 0.02035 -0.135 0.411 0.017 0.938 0.019 40.205 0.285 0.415 2.0 0.873 0.02081 -0.137 0.396 0.018 0.935 0.020 41.974 0.282 0.407 2.5 0.934 0.02189 -0.139 0.374 0.018 0.938 0.021 42.648 0.285 0.399 3.0 0.986 0.02229 -0.141 0.356 0.020 0.931 0.024 44.251 0.292 0.393 3.5 1.038 0.02562 -0.143 0.333 0.023 0.923 0.970 40.535 0.294 0.388 4.0 1.090 0.02693 -0.146 0.311 0.953 0.915 0.954 40.479 0.303 0.384 4.5 1.136 0.02842 -0.149 0.293 0.951 0.900 0.952 39.972 0.305 0.381 5.0 1.188 0.02931 -0.151 0.279 0.951 0.893 0.952 40.531 0.303 0.377 5.5 1.237 0.03021 -0.154 0.269 0.951 0.883 0.952 40.938 0.306 0.375 6.0 1.287 0.03229 -0.157 0.255 0.951 0.876 0.953 39.868 0.313 0.372 6.5 1.332 0.03284 -0.160 0.245 0.951 0.862 0.953 40.567 0.326 0.370 7.0 1.376 0.03453 -0.163 0.238 0.952 0.848 0.953 39.856 0.301 0.369 7.5 1.437 0.03736 -0.165 0.150 0.952 0.855 0.953 38.459 0.304 0.365 8.0 1.480 0.03923 -0.169 0.133 0.952 0.841 0.953 37.712 0.337 0.364 8.5 1.521 0.04135 -0.173 0.104 0.952 0.828 0.953 36.792 0.341 0.364 9.0 1.562 0.04476 -0.177 0.100 0.952 0.814 0.953 34.904 0.364 0.363 9.5 1.596 0.04691 -0.181 0.090 0.952 0.792 0.953 34.022 0.394 0.364 10.0 1.628 0.05095 -0.186 0.050 0.952 0.770 0.954 31.959 0.406 0.364 10.5 1.659 0.05349 -0.191 0.048 0.952 0.747 0.954 31.018 0.427 0.365 11.0 1.686 0.05776 -0.196 0.044 0.952 0.722 0.954 29.195 0.510 0.366 11.5 1.704 0.06148 -0.203 0.042 0.953 0.687 0.954 27.713 1.215 0.369 12.0 1.701 0.06729 -0.210 0.042 0.953 0.635 0.954 25.277 -1.689 0.374 12.5 1.696 0.07278 -0.218 0.038 0.958 0.582 0.959 23.301 -0.679 0.379 13.0 1.684 0.07913 -0.226 0.037 0.958 0.522 0.959 21.287 0.087 0.384 13.5 1.575 0.09893 -0.238 0.037 0.958 0.300 0.959 15.917 0.558 0.401 14.0 1.716 0.09109 -0.235 0.011 0.958 0.485 0.959 18.841 0.279 0.387 14.5 1.709 0.09940 -0.242 0.010 0.958 0.440 0.959 17.198 -0.315 0.391 15.0 1.694 0.10896 -0.248 0.009 0.958 0.387 0.959 15.551 -0.160 0.396 Name = GOE 802 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 -0.268 0.17487 -0.031 0.779 0.014 0.874 0.015 -1.534 0.399 0.133 -14.5 -0.249 0.15348 -0.034 0.774 0.014 0.868 0.015 -1.621 0.395 0.113 -14.0 -0.228 0.14727 -0.037 0.769 0.014 0.879 0.015 -1.548 0.388 0.087 -13.5 -0.206 0.14173 -0.040 0.763 0.014 0.884 0.015 -1.453 0.381 0.055 -13.0 -0.183 0.13682 -0.043 0.758 0.014 0.889 0.015 -1.334 0.375 0.014 -12.5 -0.158 0.12036 -0.046 0.753 0.014 0.889 0.015 -1.311 0.370 -0.042 -12.0 -0.132 0.10431 -0.049 0.753 0.015 0.884 0.016 -1.269 0.366 -0.121 -11.5 -0.105 0.10011 -0.052 0.748 0.015 0.884 0.016 -1.051 0.362 -0.246 -11.0 -0.077 0.08975 -0.055 0.742 0.015 0.889 0.016 -0.857 0.358 -0.469 -10.5 -0.048 0.08379 -0.058 0.737 0.015 0.889 0.016 -0.568 0.355 -0.978 -10.0 -0.017 0.08094 -0.062 0.737 0.015 0.879 0.016 -0.211 0.233 -3.353 -9.5 -0.424 0.07486 -0.065 0.732 0.015 0.889 0.016 -5.664 0.232 0.097 -9.0 -0.367 0.06991 -0.068 0.727 0.015 0.889 0.016 -5.256 0.307 0.065 -8.5 -0.310 0.06924 -0.071 0.727 0.014 0.879 0.015 -4.476 0.307 0.020 -8.0 -0.252 0.06719 -0.075 0.721 0.014 0.884 0.015 -3.744 0.306 -0.046 -7.5 -0.192 0.06080 -0.078 0.716 0.014 0.884 0.015 -3.166 0.305 -0.154 -7.0 -0.133 0.05414 -0.081 0.711 0.015 0.878 0.016 -2.455 0.306 -0.360 -6.5 -0.073 0.05091 -0.084 0.707 0.015 0.874 0.016 -1.434 0.306 -0.907 -6.0 -0.013 0.04811 -0.088 0.696 0.015 0.881 0.016 -0.268 0.306 -6.553 -5.5 0.047 0.04465 -0.091 0.681 0.015 0.893 0.017 1.058 0.307 2.181 -5.0 0.107 0.04203 -0.095 0.667 0.015 0.904 0.017 2.553 0.307 1.132 -4.5 0.167 0.03953 -0.098 0.652 0.015 0.908 0.016 4.229 0.308 0.837 -4.0 0.227 0.03643 -0.102 0.641 0.015 0.912 0.016 6.223 0.308 0.698 -3.5 0.286 0.03367 -0.105 0.630 0.015 0.912 0.016 8.486 0.309 0.618 -3.0 0.344 0.03172 -0.109 0.619 0.015 0.915 0.016 10.856 0.310 0.565 -2.5 0.402 0.02941 -0.112 0.604 0.015 0.919 0.016 13.677 0.311 0.529 -2.0 0.459 0.02760 -0.116 0.570 0.015 0.935 0.016 16.650 0.312 0.502 -1.5 0.516 0.02587 -0.119 0.526 0.015 1.000 0.016 19.946 0.314 0.481 -1.0 0.572 0.02163 -0.123 0.493 0.015 1.000 0.016 26.424 0.315 0.465 -0.5 0.626 0.02020 -0.126 0.470 0.015 1.000 0.017 31.009 0.316 0.452 0.0 0.680 0.01492 -0.130 0.456 0.015 1.000 0.017 45.586 0.294 0.441 0.5 0.740 0.01487 -0.131 0.441 0.016 1.000 0.018 49.726 0.274 0.428 1.0 0.798 0.01562 -0.133 0.426 0.016 1.000 0.019 51.109 0.274 0.416 1.5 0.857 0.01582 -0.134 0.411 0.017 1.000 0.019 54.197 0.275 0.407 2.0 0.916 0.01620 -0.136 0.396 0.018 1.000 0.020 56.545 0.275 0.398 2.5 0.975 0.01651 -0.137 0.374 0.018 1.000 0.022 59.085 0.275 0.391 3.0 1.034 0.01713 -0.139 0.356 0.020 1.000 0.024 60.362 0.275 0.384 3.5 1.093 0.01935 -0.140 0.333 0.023 1.000 0.971 56.501 0.276 0.378 4.0 1.152 0.02016 -0.142 0.311 0.953 1.000 0.954 57.159 0.276 0.373 4.5 1.211 0.02179 -0.143 0.293 0.951 1.000 0.952 55.607 0.276 0.368 5.0 1.270 0.02203 -0.145 0.279 0.951 1.000 0.952 57.668 0.276 0.364 5.5 1.330 0.02289 -0.146 0.269 0.951 1.000 0.952 58.092 0.511 0.360 6.0 1.310 0.02885 -0.155 0.255 0.951 0.904 0.953 45.392 0.666 0.368 6.5 1.357 0.03039 -0.158 0.245 0.951 0.893 0.953 44.660 0.313 0.366 7.0 1.405 0.03204 -0.161 0.238 0.952 0.883 0.953 43.850 0.311 0.365 7.5 1.454 0.03416 -0.164 0.150 0.952 0.876 0.953 42.576 0.314 0.363 8.0 1.501 0.03695 -0.167 0.133 0.952 0.866 0.953 40.615 0.328 0.361 8.5 1.543 0.03940 -0.171 0.104 0.952 0.852 0.953 39.160 0.346 0.361 9.0 1.581 0.03975 -0.175 0.100 0.952 0.834 0.953 39.774 0.354 0.361 9.5 1.620 0.04327 -0.179 0.090 0.952 0.820 0.953 37.447 0.381 0.360 10.0 1.650 0.04747 -0.184 0.050 0.952 0.795 0.954 34.760 0.405 0.361 10.5 1.684 0.04954 -0.189 0.048 0.952 0.775 0.954 33.987 0.404 0.362 11.0 1.714 0.05279 -0.194 0.044 0.952 0.752 0.954 32.465 0.438 0.363 11.5 1.740 0.05624 -0.199 0.042 0.953 0.727 0.954 30.936 0.556 0.364 12.0 1.752 0.05999 -0.205 0.042 0.953 0.695 0.954 29.200 1.029 0.367 12.5 1.757 0.06449 -0.212 0.038 0.958 0.655 0.959 27.239 2.532 0.371 13.0 1.758 0.06893 -0.219 0.037 0.958 0.615 0.959 25.501 -0.063 0.375 13.5 1.697 0.08002 -0.231 0.037 0.958 0.497 0.959 21.204 -2.482 0.386 14.0 1.753 0.08430 -0.232 0.011 0.958 0.532 0.959 20.793 0.437 0.383 14.5 1.741 0.09094 -0.239 0.010 0.958 0.485 0.959 19.149 -0.391 0.387 15.0 1.733 0.09994 -0.245 0.009 0.958 0.442 0.959 17.336 -0.445 0.392