Name = GOE 646 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 -0.461 0.13239 -0.052 0.806 0.019 1.000 0.024 -3.485 0.341 0.136 -14.5 -0.424 0.12244 -0.056 0.800 0.020 1.000 0.024 -3.465 0.339 0.119 -14.0 -0.386 0.11560 -0.059 0.795 0.020 1.000 0.025 -3.337 0.336 0.097 -13.5 -0.347 0.11211 -0.062 0.790 0.020 0.897 0.026 -3.092 0.336 0.070 -13.0 -0.307 0.10464 -0.066 0.779 0.021 0.897 0.026 -2.936 0.336 0.036 -12.5 -0.267 0.09922 -0.069 0.768 0.021 0.897 0.027 -2.690 0.328 -0.010 -12.0 -0.223 0.09589 -0.072 0.763 0.021 0.892 0.034 -2.329 0.323 -0.074 -11.5 -0.179 0.09012 -0.076 0.757 0.022 0.881 0.041 -1.992 0.318 -0.172 -11.0 -0.131 0.08768 -0.079 0.752 0.023 0.870 0.053 -1.500 0.317 -0.349 -10.5 -0.088 0.08395 -0.082 0.747 0.024 0.865 0.066 -1.044 0.323 -0.684 -10.0 -0.044 0.07767 -0.085 0.741 0.025 0.860 0.076 -0.561 0.236 -1.706 -9.5 -0.542 0.07502 -0.088 0.736 0.027 0.849 0.104 -7.225 0.233 0.088 -9.0 -0.471 0.07247 -0.093 0.731 0.060 0.843 0.076 -6.499 0.306 0.054 -8.5 -0.398 0.06994 -0.096 0.725 0.060 0.838 0.079 -5.690 0.291 0.008 -8.0 -0.323 0.06598 -0.099 0.722 0.063 0.835 0.145 -4.897 0.289 -0.055 -7.5 -0.251 0.06156 -0.102 0.715 0.066 0.832 0.191 -4.075 0.299 -0.156 -7.0 -0.180 0.05695 -0.106 0.711 0.069 0.824 0.243 -3.161 0.304 -0.336 -6.5 -0.111 0.05360 -0.109 0.704 0.076 0.821 0.279 -2.068 0.309 -0.737 -6.0 -0.043 0.04919 -0.114 0.700 0.079 0.810 0.323 -0.871 0.308 -2.402 -5.5 0.024 0.05119 -0.117 0.577 0.141 0.886 0.269 0.474 0.307 5.085 -5.0 0.091 0.04929 -0.121 0.558 0.155 0.883 0.282 1.842 0.310 1.585 -4.5 0.157 0.04753 -0.125 0.543 0.171 0.875 0.288 3.293 0.311 1.049 -4.0 0.221 0.04572 -0.129 0.528 0.185 0.868 0.298 4.844 0.312 0.833 -3.5 0.286 0.04445 -0.133 0.513 0.198 0.861 0.307 6.426 0.313 0.716 -3.0 0.349 0.04308 -0.137 0.502 0.211 0.846 0.323 8.099 0.314 0.643 -2.5 0.411 0.04182 -0.141 0.490 0.221 0.835 0.336 9.837 0.315 0.593 -2.0 0.473 0.04066 -0.145 0.479 0.227 0.828 0.362 11.633 0.316 0.557 -1.5 0.534 0.03973 -0.149 0.472 0.237 0.813 0.378 13.440 0.316 0.529 -1.0 0.594 0.03815 -0.153 0.461 0.247 0.802 0.397 15.581 0.318 0.508 -0.5 0.653 0.03559 -0.157 0.453 0.256 0.788 0.538 18.361 0.073 0.491 0.0 0.550 0.03637 -0.161 0.449 0.269 0.762 0.605 15.120 0.129 0.543 0.5 0.599 0.03771 -0.164 0.442 0.279 0.748 0.669 15.886 0.312 0.524 1.0 0.647 0.03896 -0.167 0.435 0.295 0.733 0.881 16.620 0.322 0.508 1.5 0.688 0.04040 -0.170 0.431 0.311 0.708 0.943 17.040 0.324 0.497 2.0 0.738 0.04192 -0.174 0.423 0.327 0.697 0.951 17.595 0.373 0.485 2.5 0.752 0.04502 -0.178 0.420 0.339 0.621 0.953 16.700 0.399 0.487 3.0 0.794 0.04656 -0.182 0.416 0.355 0.599 0.954 17.052 0.349 0.479 3.5 0.832 0.04908 -0.186 0.408 0.371 0.569 0.955 16.960 0.352 0.474 4.0 0.874 0.05173 -0.190 0.405 0.387 0.547 0.955 16.895 0.258 0.468 4.5 1.049 0.04547 -0.188 0.290 0.560 0.740 0.956 23.067 0.257 0.429 5.0 1.091 0.04687 -0.192 0.275 0.582 0.722 0.957 23.278 0.337 0.426 5.5 1.135 0.04974 -0.195 0.261 0.602 0.708 0.957 22.818 0.341 0.422 6.0 1.176 0.05260 -0.199 0.246 0.614 0.689 0.958 22.353 0.385 0.420 6.5 1.202 0.05562 -0.204 0.235 0.627 0.650 0.958 21.612 0.408 0.420 7.0 1.237 0.05874 -0.209 0.220 0.640 0.624 0.959 21.058 0.402 0.419 7.5 1.265 0.06291 -0.214 0.209 0.650 0.592 0.959 20.102 0.413 0.419 8.0 1.297 0.06547 -0.219 0.200 0.664 0.563 0.961 19.807 0.359 0.419 8.5 1.344 0.06845 -0.223 0.188 0.680 0.559 0.962 19.633 0.342 0.416 9.0 1.384 0.07143 -0.227 0.171 0.695 0.546 0.962 19.377 0.259 0.414 9.5 1.518 0.06901 -0.224 0.069 0.956 0.655 0.957 21.994 0.268 0.398 10.0 1.541 0.07463 -0.230 0.063 0.956 0.623 0.958 20.656 0.508 0.399 10.5 1.561 0.07988 -0.235 0.060 0.956 0.588 0.958 19.542 0.403 0.401 11.0 1.604 0.08330 -0.239 0.057 0.951 0.582 0.952 19.255 0.462 0.399 11.5 1.611 0.08939 -0.246 0.054 0.951 0.532 0.953 18.018 0.916 0.403 12.0 1.623 0.09977 -0.252 0.048 0.951 0.490 0.953 16.264 0.683 0.405 12.5 1.637 0.10562 -0.257 0.045 0.951 0.448 0.953 15.503 0.660 0.407 13.0 1.650 0.11155 -0.263 0.040 0.951 0.406 0.953 14.790 -0.272 0.409 13.5 1.621 0.12165 -0.266 0.040 0.951 0.072 0.953 13.326 1.404 0.414 14.0 1.656 0.12762 -0.270 0.037 0.951 0.069 0.953 12.973 0.351 0.413 14.5 1.692 0.14029 -0.273 0.037 0.952 0.063 0.953 12.059 0.353 0.411 15.0 1.725 0.14276 -0.277 0.035 0.952 0.060 0.953 12.081 0.360 0.410 Name = GOE 646 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 -0.460 0.11004 -0.052 0.806 0.019 1.000 0.026 -4.182 0.339 0.136 -14.5 -0.423 0.10539 -0.056 0.800 0.020 1.000 0.026 -4.011 0.338 0.118 -14.0 -0.384 0.09793 -0.059 0.795 0.020 1.000 0.027 -3.923 0.336 0.096 -13.5 -0.345 0.09471 -0.062 0.790 0.020 1.000 0.028 -3.642 0.327 0.069 -13.0 -0.302 0.09035 -0.065 0.779 0.021 1.000 0.037 -3.339 0.316 0.033 -12.5 -0.256 0.08776 -0.068 0.768 0.021 1.000 0.050 -2.916 0.316 -0.017 -12.0 -0.213 0.08443 -0.071 0.763 0.021 1.000 0.063 -2.521 0.323 -0.085 -11.5 -0.171 0.07919 -0.074 0.757 0.022 1.000 0.073 -2.153 0.325 -0.187 -11.0 -0.128 0.07312 -0.078 0.752 0.023 1.000 0.085 -1.751 0.320 -0.356 -10.5 -0.095 0.06714 -0.080 0.747 0.024 1.000 0.148 -1.419 0.349 -0.587 -10.0 -0.077 0.06176 -0.083 0.741 0.025 1.000 0.214 -1.246 0.434 -0.824 -9.5 -0.059 0.05487 -0.086 0.736 0.027 1.000 0.266 -1.079 0.229 -1.209 -9.0 -0.467 0.06193 -0.091 0.731 0.060 0.897 0.145 -7.533 0.226 0.055 -8.5 -0.393 0.05843 -0.094 0.725 0.060 0.887 0.168 -6.732 0.296 0.010 -8.0 -0.317 0.04969 -0.098 0.722 0.063 0.883 0.288 -6.387 0.302 -0.058 -7.5 -0.247 0.04562 -0.102 0.715 0.066 0.883 0.333 -5.407 0.311 -0.164 -7.0 -0.177 0.04119 -0.106 0.711 0.069 0.868 0.375 -4.307 0.313 -0.350 -6.5 -0.109 0.03860 -0.111 0.704 0.076 0.868 0.403 -2.835 0.325 -0.762 -6.0 -0.042 0.03369 -0.117 0.700 0.079 0.853 0.499 -1.249 0.304 -2.519 -5.5 0.024 0.03563 -0.118 0.577 0.141 1.000 0.371 0.674 0.291 5.158 -5.0 0.090 0.03424 -0.122 0.558 0.155 1.000 0.387 2.628 0.310 1.605 -4.5 0.155 0.03279 -0.126 0.543 0.171 1.000 0.391 4.738 0.311 1.060 -4.0 0.220 0.03127 -0.130 0.528 0.185 1.000 0.403 7.034 0.313 0.840 -3.5 0.284 0.02980 -0.134 0.513 0.198 1.000 0.429 9.517 0.322 0.722 -3.0 0.345 0.02970 -0.139 0.502 0.211 1.000 0.518 11.633 0.326 0.652 -2.5 0.407 0.02804 -0.143 0.490 0.221 1.000 0.579 14.520 0.323 0.602 -2.0 0.468 0.02604 -0.148 0.479 0.227 1.000 0.653 17.982 0.318 0.565 -1.5 0.530 0.02623 -0.152 0.472 0.237 1.000 0.701 20.187 0.325 0.536 -1.0 0.589 0.02472 -0.157 0.461 0.247 0.894 0.913 23.825 0.312 0.516 -0.5 0.651 0.02506 -0.159 0.453 0.256 0.883 0.950 25.969 0.405 0.494 0.0 0.616 0.02664 -0.161 0.449 0.269 0.868 0.952 23.122 0.532 0.511 0.5 0.666 0.02647 -0.163 0.442 0.279 0.853 0.953 25.168 0.299 0.495 1.0 0.718 0.02748 -0.166 0.435 0.295 0.843 0.954 26.128 0.304 0.481 1.5 0.764 0.02839 -0.169 0.431 0.311 0.824 0.955 26.917 0.308 0.471 2.0 0.815 0.02879 -0.172 0.423 0.327 0.813 0.955 28.306 0.315 0.461 2.5 0.857 0.03036 -0.175 0.420 0.339 0.791 0.956 28.233 0.318 0.454 3.0 0.907 0.03125 -0.178 0.416 0.355 0.780 0.957 29.036 0.328 0.446 3.5 0.944 0.03293 -0.182 0.408 0.371 0.751 0.957 28.668 0.351 0.442 4.0 0.982 0.03506 -0.185 0.405 0.387 0.726 0.958 28.009 0.264 0.439 4.5 1.120 0.03306 -0.184 0.290 0.560 0.832 0.959 33.887 0.260 0.414 5.0 1.169 0.03450 -0.187 0.275 0.582 0.821 0.959 33.881 0.316 0.410 5.5 1.217 0.03632 -0.190 0.261 0.602 0.810 0.960 33.499 0.319 0.406 6.0 1.264 0.03823 -0.194 0.246 0.614 0.799 0.960 33.066 0.326 0.403 6.5 1.308 0.04037 -0.197 0.235 0.627 0.784 0.960 32.414 0.334 0.401 7.0 1.352 0.04127 -0.201 0.220 0.640 0.770 0.960 32.751 0.339 0.399 7.5 1.394 0.04387 -0.205 0.209 0.650 0.755 0.961 31.771 0.349 0.397 8.0 1.433 0.04613 -0.209 0.200 0.664 0.738 0.963 31.059 0.344 0.396 8.5 1.477 0.04828 -0.213 0.188 0.680 0.728 0.963 30.600 0.340 0.394 9.0 1.518 0.05053 -0.217 0.171 0.695 0.715 0.964 30.043 0.304 0.393 9.5 1.585 0.05415 -0.219 0.069 0.956 0.731 0.957 29.274 0.310 0.388 10.0 1.621 0.05789 -0.223 0.063 0.956 0.715 0.958 28.011 0.382 0.387 10.5 1.653 0.06118 -0.228 0.060 0.956 0.696 0.958 27.023 0.376 0.388 11.0 1.692 0.06377 -0.232 0.057 0.951 0.684 0.952 26.529 0.482 0.387 11.5 1.701 0.06978 -0.239 0.054 0.951 0.639 0.953 24.374 0.847 0.390 12.0 1.714 0.07548 -0.245 0.048 0.951 0.601 0.953 22.703 0.538 0.393 12.5 1.740 0.07958 -0.250 0.045 0.951 0.579 0.953 21.868 0.458 0.394 13.0 1.764 0.08372 -0.255 0.040 0.951 0.554 0.953 21.065 0.563 0.395 13.5 1.776 0.09026 -0.261 0.040 0.951 0.519 0.953 19.677 0.691 0.397 14.0 1.789 0.09750 -0.267 0.037 0.951 0.487 0.953 18.354 1.361 0.399 14.5 1.787 0.10566 -0.273 0.037 0.952 0.432 0.953 16.911 -2.246 0.403 15.0 1.784 0.11551 -0.279 0.035 0.952 0.377 0.953 15.448 -2.166 0.406 Name = GOE 646 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 -0.459 0.09980 -0.052 0.806 0.019 1.000 0.027 -4.600 0.339 0.136 -14.5 -0.422 0.09549 -0.056 0.800 0.020 1.000 0.027 -4.415 0.321 0.118 -14.0 -0.377 0.09335 -0.058 0.795 0.020 1.000 0.044 -4.037 0.316 0.096 -13.5 -0.335 0.08733 -0.061 0.790 0.020 1.000 0.050 -3.840 0.323 0.067 -13.0 -0.294 0.08581 -0.064 0.779 0.021 1.000 0.063 -3.424 0.322 0.032 -12.5 -0.253 0.08279 -0.067 0.768 0.021 1.000 0.076 -3.050 0.323 -0.016 -12.0 -0.212 0.07726 -0.070 0.763 0.021 1.000 0.095 -2.749 0.323 -0.080 -11.5 -0.181 0.07192 -0.072 0.757 0.022 1.000 0.145 -2.521 0.348 -0.149 -11.0 -0.160 0.06282 -0.075 0.752 0.023 1.000 0.201 -2.545 0.442 -0.221 -10.5 -0.148 0.05729 -0.079 0.747 0.024 1.000 0.259 -2.587 0.446 -0.282 -10.0 -0.122 0.05140 -0.083 0.741 0.025 1.000 0.295 -2.372 0.406 -0.429 -9.5 -0.097 0.04661 -0.087 0.736 0.027 1.000 0.330 -2.072 0.319 -0.649 -9.0 -0.014 0.04902 -0.090 0.731 0.060 1.000 0.269 -0.287 0.225 -6.162 -8.5 -0.387 0.04521 -0.094 0.725 0.060 1.000 0.291 -8.560 0.221 0.007 -8.0 -0.314 0.03883 -0.099 0.722 0.063 1.000 0.375 -8.084 0.315 -0.065 -7.5 -0.244 0.03551 -0.103 0.715 0.066 1.000 0.413 -6.879 0.324 -0.173 -7.0 -0.175 0.03072 -0.109 0.711 0.069 1.000 0.493 -5.697 0.331 -0.373 -6.5 -0.108 0.02748 -0.114 0.704 0.076 1.000 0.547 -3.921 0.331 -0.812 -6.0 -0.042 0.02683 -0.120 0.700 0.079 0.897 0.605 -1.552 0.302 -2.628 -5.5 0.024 0.02575 -0.121 0.577 0.141 1.000 0.541 0.919 0.297 5.376 -5.0 0.089 0.02402 -0.126 0.558 0.155 1.000 0.582 3.686 0.318 1.672 -4.5 0.153 0.02263 -0.130 0.543 0.171 1.000 0.608 6.754 0.316 1.101 -4.0 0.216 0.02172 -0.134 0.528 0.185 1.000 0.643 9.963 0.314 0.871 -3.5 0.280 0.02083 -0.138 0.513 0.198 1.000 0.662 13.426 0.317 0.744 -3.0 0.342 0.02163 -0.143 0.502 0.211 1.000 0.723 15.804 0.343 0.668 -2.5 0.402 0.02139 -0.150 0.490 0.221 1.000 0.877 18.793 0.336 0.622 -2.0 0.464 0.02090 -0.153 0.479 0.227 1.000 0.940 22.180 0.297 0.580 -1.5 0.526 0.02148 -0.155 0.472 0.237 1.000 0.951 24.492 0.282 0.545 -1.0 0.589 0.02097 -0.157 0.461 0.247 1.000 0.952 28.065 0.280 0.517 -0.5 0.651 0.02131 -0.159 0.453 0.256 1.000 0.954 30.534 0.280 0.494 0.0 0.713 0.02230 -0.161 0.449 0.269 1.000 0.955 31.985 0.277 0.476 0.5 0.776 0.02242 -0.163 0.442 0.279 1.000 0.955 34.614 0.275 0.459 1.0 0.838 0.02192 -0.164 0.435 0.295 1.000 0.956 38.254 0.411 0.446 1.5 0.808 0.02388 -0.168 0.431 0.311 0.886 0.957 33.856 0.530 0.457 2.0 0.860 0.02410 -0.170 0.423 0.327 0.875 0.957 35.695 0.305 0.448 2.5 0.906 0.02513 -0.173 0.420 0.339 0.857 0.958 36.064 0.305 0.441 3.0 0.960 0.02570 -0.176 0.416 0.355 0.850 0.958 37.346 0.313 0.433 3.5 1.001 0.02691 -0.179 0.408 0.371 0.828 0.959 37.204 0.332 0.429 4.0 1.041 0.02770 -0.182 0.405 0.387 0.806 0.959 37.596 0.270 0.425 4.5 1.154 0.02810 -0.182 0.290 0.560 0.872 0.960 41.064 0.266 0.408 5.0 1.203 0.02908 -0.185 0.275 0.582 0.861 0.960 41.377 0.311 0.404 5.5 1.252 0.03035 -0.188 0.261 0.602 0.850 0.961 41.251 0.314 0.400 6.0 1.300 0.03171 -0.191 0.246 0.614 0.839 0.961 40.998 0.317 0.397 6.5 1.348 0.03346 -0.195 0.235 0.627 0.828 0.961 40.271 0.321 0.394 7.0 1.394 0.03517 -0.198 0.220 0.640 0.817 0.962 39.627 0.324 0.392 7.5 1.439 0.03768 -0.201 0.209 0.650 0.806 0.962 38.198 0.333 0.390 8.0 1.481 0.03888 -0.205 0.200 0.664 0.792 0.964 38.084 0.339 0.389 8.5 1.524 0.04009 -0.209 0.188 0.680 0.779 0.964 38.001 0.340 0.387 9.0 1.565 0.04224 -0.213 0.171 0.695 0.766 0.965 37.060 0.332 0.386 9.5 1.612 0.04848 -0.216 0.069 0.956 0.760 0.957 33.254 0.342 0.384 10.0 1.649 0.05090 -0.221 0.063 0.956 0.744 0.958 32.399 0.369 0.384 10.5 1.685 0.05363 -0.225 0.060 0.956 0.728 0.958 31.415 0.358 0.383 11.0 1.725 0.05516 -0.229 0.057 0.951 0.719 0.952 31.281 0.394 0.383 11.5 1.749 0.05992 -0.234 0.054 0.951 0.693 0.953 29.187 0.513 0.384 12.0 1.768 0.06508 -0.240 0.048 0.951 0.661 0.953 27.175 0.516 0.386 12.5 1.792 0.06838 -0.246 0.045 0.951 0.636 0.953 26.207 0.514 0.387 13.0 1.811 0.07474 -0.251 0.040 0.951 0.607 0.953 24.227 0.566 0.389 13.5 1.828 0.07768 -0.257 0.040 0.951 0.579 0.953 23.534 0.523 0.391 14.0 1.850 0.08315 -0.262 0.037 0.951 0.557 0.953 22.253 0.568 0.392 14.5 1.863 0.08863 -0.268 0.037 0.952 0.525 0.953 21.016 0.769 0.394 15.0 1.873 0.09504 -0.274 0.035 0.952 0.494 0.953 19.705 0.816 0.396 Name = GOE 646 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 -0.454 0.09641 -0.052 0.806 0.019 1.000 0.041 -4.705 0.327 0.136 -14.5 -0.414 0.09238 -0.055 0.800 0.020 1.000 0.047 -4.479 0.321 0.118 -14.0 -0.373 0.08951 -0.057 0.795 0.020 1.000 0.063 -4.164 0.321 0.096 -13.5 -0.333 0.08503 -0.060 0.790 0.020 1.000 0.073 -3.918 0.328 0.069 -13.0 -0.293 0.08010 -0.063 0.779 0.021 1.000 0.082 -3.661 0.323 0.034 -12.5 -0.261 0.07570 -0.066 0.768 0.021 1.000 0.124 -3.441 0.334 -0.002 -12.0 -0.237 0.06899 -0.068 0.763 0.021 1.000 0.178 -3.441 0.390 -0.037 -11.5 -0.219 0.06314 -0.071 0.757 0.022 1.000 0.227 -3.476 0.444 -0.075 -11.0 -0.202 0.05597 -0.075 0.752 0.023 1.000 0.272 -3.601 0.420 -0.123 -10.5 -0.174 0.05135 -0.079 0.747 0.024 1.000 0.304 -3.392 0.410 -0.204 -10.0 -0.151 0.04664 -0.083 0.741 0.025 1.000 0.339 -3.231 0.426 -0.302 -9.5 -0.126 0.04212 -0.088 0.736 0.027 1.000 0.375 -2.981 0.328 -0.448 -9.0 -0.055 0.04125 -0.091 0.731 0.060 1.000 0.339 -1.324 0.320 -1.412 -8.5 -0.022 0.03870 -0.095 0.725 0.060 1.000 0.365 -0.561 0.545 -4.120 -8.0 -0.022 0.03332 -0.101 0.722 0.063 1.000 0.448 -0.647 1.138 -4.413 -7.5 -0.009 0.02892 -0.106 0.715 0.066 1.000 0.515 -0.311 0.176 -11.557 -7.0 -0.173 0.02615 -0.112 0.711 0.069 1.000 0.570 -6.633 0.142 -0.394 -6.5 -0.107 0.02334 -0.117 0.704 0.076 1.000 0.611 -4.586 0.326 -0.841 -6.0 -0.041 0.02164 -0.122 0.700 0.079 1.000 0.653 -1.915 0.310 -2.688 -5.5 0.023 0.02103 -0.125 0.577 0.141 1.000 0.643 1.114 0.306 5.568 -5.0 0.088 0.01985 -0.129 0.558 0.155 1.000 0.675 4.425 0.316 1.718 -4.5 0.152 0.01879 -0.133 0.543 0.171 1.000 0.701 8.076 0.345 1.127 -4.0 0.214 0.01762 -0.141 0.528 0.185 1.000 0.836 12.117 0.347 0.910 -3.5 0.276 0.01710 -0.145 0.513 0.198 1.000 0.881 16.139 0.315 0.776 -3.0 0.338 0.01855 -0.149 0.502 0.211 1.000 0.930 18.236 0.302 0.691 -2.5 0.401 0.01819 -0.152 0.490 0.221 1.000 0.950 22.025 0.286 0.628 -2.0 0.463 0.01877 -0.154 0.479 0.227 1.000 0.952 24.692 0.280 0.581 -1.5 0.526 0.01879 -0.155 0.472 0.237 1.000 0.953 27.994 0.280 0.545 -1.0 0.589 0.01854 -0.157 0.461 0.247 1.000 0.954 31.753 0.280 0.517 -0.5 0.651 0.01957 -0.159 0.453 0.256 1.000 0.955 33.260 0.280 0.494 0.0 0.713 0.01895 -0.161 0.449 0.269 1.000 0.956 37.645 0.277 0.476 0.5 0.776 0.01928 -0.163 0.442 0.279 1.000 0.957 40.254 0.275 0.459 1.0 0.838 0.01935 -0.164 0.435 0.295 1.000 0.957 43.332 0.275 0.446 1.5 0.901 0.02028 -0.166 0.431 0.311 1.000 0.957 44.406 0.275 0.434 2.0 0.963 0.02114 -0.167 0.423 0.327 1.000 0.958 45.557 0.427 0.424 2.5 0.936 0.02204 -0.172 0.420 0.339 0.897 0.959 42.490 0.509 0.434 3.0 0.991 0.02243 -0.174 0.416 0.355 0.890 0.959 44.172 0.305 0.426 3.5 1.036 0.02352 -0.177 0.408 0.371 0.872 0.960 44.048 0.318 0.421 4.0 1.080 0.02383 -0.181 0.405 0.387 0.853 0.960 45.329 0.277 0.417 4.5 1.172 0.02465 -0.181 0.290 0.560 0.894 0.961 47.557 0.272 0.404 5.0 1.225 0.02674 -0.184 0.275 0.582 0.886 0.962 45.818 0.305 0.400 5.5 1.274 0.02761 -0.187 0.261 0.602 0.875 0.962 46.147 0.311 0.396 6.0 1.323 0.02879 -0.190 0.246 0.614 0.864 0.962 45.951 0.314 0.393 6.5 1.371 0.03009 -0.193 0.235 0.627 0.853 0.962 45.555 0.318 0.391 7.0 1.418 0.03162 -0.196 0.220 0.640 0.843 0.962 44.839 0.321 0.388 7.5 1.463 0.03337 -0.200 0.209 0.650 0.832 0.962 43.853 0.326 0.386 8.0 1.508 0.03479 -0.203 0.200 0.664 0.820 0.965 43.333 0.333 0.385 8.5 1.550 0.03582 -0.207 0.188 0.680 0.807 0.965 43.287 0.338 0.383 9.0 1.592 0.03772 -0.210 0.171 0.695 0.795 0.965 42.202 0.356 0.382 9.5 1.627 0.04386 -0.215 0.069 0.956 0.776 0.957 37.105 0.361 0.382 10.0 1.667 0.04740 -0.219 0.063 0.956 0.763 0.958 35.177 0.359 0.381 10.5 1.703 0.04923 -0.223 0.060 0.956 0.747 0.958 34.602 0.356 0.381 11.0 1.745 0.05068 -0.227 0.057 0.951 0.738 0.952 34.424 0.371 0.380 11.5 1.775 0.05616 -0.232 0.054 0.951 0.719 0.953 31.606 0.428 0.381 12.0 1.801 0.05907 -0.237 0.048 0.951 0.696 0.953 30.482 0.448 0.382 12.5 1.827 0.06231 -0.242 0.045 0.951 0.674 0.953 29.325 0.489 0.383 13.0 1.847 0.06750 -0.248 0.040 0.951 0.646 0.953 27.357 0.573 0.384 13.5 1.863 0.07161 -0.254 0.040 0.951 0.617 0.953 26.022 0.579 0.386 14.0 1.881 0.07699 -0.259 0.037 0.951 0.592 0.953 24.433 0.527 0.388 14.5 1.902 0.08189 -0.265 0.037 0.952 0.569 0.953 23.231 0.535 0.389 15.0 1.919 0.08708 -0.270 0.035 0.952 0.544 0.953 22.035 0.582 0.391