Name = GOE 336 (MVA H.44) 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 -0.414 0.27606 0.026 0.852 0.013 0.911 0.014 -1.501 0.533 0.312 -14.5 -0.404 0.25272 0.023 0.847 0.013 0.917 0.014 -1.600 0.509 0.307 -14.0 -0.392 0.24909 0.020 0.842 0.013 0.911 0.014 -1.575 0.470 0.301 -13.5 -0.378 0.22833 0.017 0.837 0.013 0.911 0.014 -1.655 0.442 0.295 -13.0 -0.362 0.20212 0.014 0.837 0.013 0.911 0.015 -1.789 0.421 0.289 -12.5 -0.343 0.18808 0.011 0.831 0.014 0.911 0.015 -1.824 0.404 0.282 -12.0 -0.323 0.16801 0.008 0.831 0.014 0.905 0.015 -1.920 0.391 0.275 -11.5 -0.300 0.15735 0.005 0.831 0.014 0.911 0.015 -1.907 0.378 0.267 -11.0 -0.275 0.14767 0.002 0.700 0.014 1.000 0.015 -1.861 0.367 0.257 -10.5 -0.247 0.13811 -0.001 0.689 0.014 1.000 0.015 -1.792 0.362 0.246 -10.0 -0.219 0.12631 -0.004 0.679 0.014 1.000 0.015 -1.735 0.358 0.231 -9.5 -0.190 0.11818 -0.007 0.668 0.014 1.000 0.015 -1.606 0.355 0.211 -9.0 -0.160 0.10656 -0.010 0.663 0.015 1.000 0.016 -1.498 0.353 0.184 -8.5 -0.128 0.09321 -0.014 0.652 0.015 1.000 0.016 -1.377 0.351 0.143 -8.0 -0.096 0.08550 -0.017 0.647 0.015 0.939 0.016 -1.127 0.350 0.074 -7.5 -0.064 0.07945 -0.020 0.642 0.015 0.933 0.016 -0.800 0.348 -0.067 -7.0 -0.030 0.07405 -0.023 0.631 0.015 0.933 0.016 -0.406 0.223 -0.528 -6.5 -0.309 0.07018 -0.027 0.621 0.014 0.925 0.015 -4.407 0.220 0.164 -6.0 -0.249 0.06465 -0.030 0.614 0.014 0.918 0.016 -3.848 0.305 0.129 -5.5 -0.188 0.05941 -0.033 0.607 0.015 0.907 0.016 -3.169 0.305 0.073 -5.0 -0.128 0.05477 -0.037 0.596 0.015 0.900 0.016 -2.334 0.306 -0.037 -4.5 -0.068 0.05018 -0.040 0.566 0.015 0.907 0.016 -1.346 0.306 -0.343 -4.0 -0.008 0.04611 -0.043 0.533 0.015 0.914 0.016 -0.165 0.307 -5.469 -3.5 0.052 0.04326 -0.047 0.496 0.015 0.928 0.016 1.201 0.308 1.152 -3.0 0.111 0.03941 -0.050 0.481 0.015 0.911 0.016 2.818 0.308 0.703 -2.5 0.170 0.03708 -0.054 0.466 0.015 0.896 0.017 4.572 0.309 0.567 -2.0 0.227 0.03427 -0.057 0.451 0.015 0.886 0.017 6.635 0.310 0.502 -1.5 0.285 0.03209 -0.061 0.440 0.016 0.868 0.017 8.867 0.311 0.463 -1.0 0.341 0.02973 -0.064 0.429 0.016 0.846 0.018 11.469 0.313 0.438 -0.5 0.397 0.02770 -0.068 0.418 0.017 0.825 0.019 14.316 -1.035 0.421 0.0 0.335 0.02584 -0.071 0.411 0.018 0.739 0.020 12.980 -0.001 0.462 0.5 0.371 0.02689 -0.074 0.399 0.019 0.696 0.021 13.791 0.325 0.450 1.0 0.415 0.02775 -0.077 0.388 0.020 0.678 0.023 14.959 0.323 0.436 1.5 0.457 0.02874 -0.080 0.381 0.022 0.657 0.025 15.900 0.328 0.426 2.0 0.500 0.03369 -0.084 0.373 0.024 0.639 0.970 14.838 0.330 0.418 2.5 0.542 0.03256 -0.087 0.366 0.086 0.621 0.103 16.650 0.345 0.411 3.0 0.577 0.03740 -0.091 0.362 0.092 0.588 0.971 15.424 0.352 0.408 3.5 0.617 0.03999 -0.095 0.355 0.097 0.566 0.969 15.422 0.365 0.404 4.0 0.647 0.04425 -0.099 0.351 0.952 0.525 0.953 14.623 0.384 0.403 4.5 0.680 0.04612 -0.103 0.348 0.955 0.493 0.956 14.750 0.352 0.402 5.0 0.725 0.04817 -0.107 0.341 0.955 0.486 0.956 15.060 0.341 0.398 5.5 0.766 0.05044 -0.111 0.341 0.955 0.469 0.957 15.181 0.351 0.395 6.0 0.805 0.05312 -0.115 0.337 0.955 0.453 0.957 15.159 0.229 0.393 6.5 1.053 0.04172 -0.105 0.050 0.955 0.786 0.956 25.241 0.233 0.350 7.0 1.075 0.04424 -0.111 0.046 0.955 0.740 0.957 24.298 0.485 0.353 7.5 1.100 0.04692 -0.116 0.043 0.955 0.700 0.957 23.435 0.416 0.355 8.0 1.134 0.05020 -0.120 0.040 0.955 0.676 0.957 22.592 0.384 0.356 8.5 1.167 0.05373 -0.125 0.038 0.955 0.653 0.957 21.725 0.068 0.357 9.0 1.039 0.07195 -0.138 0.036 0.953 0.048 0.955 14.435 0.067 0.383 9.5 1.078 0.07589 -0.141 0.036 0.953 0.046 0.954 14.198 0.247 0.381 10.0 1.285 0.06318 -0.137 0.012 0.953 0.617 0.955 20.341 0.256 0.357 10.5 1.301 0.06770 -0.143 0.009 0.953 0.582 0.955 19.218 0.021 0.360 11.0 1.223 0.07610 -0.151 0.008 0.953 0.011 0.955 16.075 -0.017 0.374 11.5 1.256 0.08139 -0.155 0.007 0.953 0.010 0.955 15.427 0.369 0.373 12.0 1.284 0.08735 -0.158 0.006 0.953 0.009 0.955 14.702 0.387 0.373 12.5 1.309 0.09415 -0.162 0.005 0.953 0.008 0.955 13.903 0.406 0.374 13.0 1.331 0.10024 -0.166 0.004 0.959 0.007 0.960 13.278 0.432 0.375 13.5 1.349 0.10870 -0.169 0.004 0.959 0.006 0.960 12.410 0.475 0.376 14.0 1.363 0.11726 -0.173 0.004 0.959 0.006 0.960 11.628 0.544 0.377 14.5 1.374 0.12939 -0.177 0.003 0.959 0.005 0.960 10.618 0.665 0.379 15.0 1.381 0.13785 -0.180 0.003 0.959 0.005 0.960 10.019 0.761 0.381 Name = GOE 336 (MVA H.44) 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 -0.414 0.20593 0.026 0.852 0.013 0.922 0.014 -2.013 0.533 0.312 -14.5 -0.404 0.21070 0.023 0.847 0.013 0.922 0.014 -1.919 0.509 0.307 -14.0 -0.392 0.18495 0.020 0.842 0.013 0.922 0.014 -2.121 0.470 0.301 -13.5 -0.378 0.17163 0.017 0.837 0.013 0.922 0.014 -2.202 0.442 0.295 -13.0 -0.362 0.15228 0.014 0.837 0.013 0.917 0.015 -2.374 0.421 0.289 -12.5 -0.343 0.14337 0.011 0.831 0.014 0.922 0.015 -2.393 0.404 0.282 -12.0 -0.323 0.13941 0.008 0.831 0.014 0.917 0.015 -2.314 0.391 0.275 -11.5 -0.300 0.12174 0.005 0.831 0.014 0.928 0.015 -2.465 0.378 0.267 -11.0 -0.275 0.12302 0.002 0.700 0.014 1.000 0.015 -2.234 0.367 0.257 -10.5 -0.247 0.10730 -0.001 0.689 0.014 1.000 0.015 -2.307 0.362 0.246 -10.0 -0.219 0.09822 -0.004 0.679 0.014 1.000 0.015 -2.231 0.358 0.231 -9.5 -0.190 0.09251 -0.007 0.668 0.014 1.000 0.015 -2.052 0.355 0.211 -9.0 -0.160 0.08368 -0.010 0.663 0.015 1.000 0.016 -1.907 0.353 0.184 -8.5 -0.128 0.07861 -0.014 0.652 0.015 1.000 0.016 -1.633 0.351 0.143 -8.0 -0.096 0.07216 -0.017 0.647 0.015 1.000 0.016 -1.335 0.350 0.075 -7.5 -0.064 0.06760 -0.020 0.642 0.015 1.000 0.016 -0.941 0.348 -0.067 -7.0 -0.030 0.06266 -0.023 0.631 0.015 1.000 0.016 -0.480 0.223 -0.528 -6.5 -0.309 0.05821 -0.027 0.621 0.014 1.000 0.016 -5.313 0.220 0.164 -6.0 -0.249 0.05288 -0.030 0.614 0.014 1.000 0.016 -4.705 0.305 0.129 -5.5 -0.188 0.04892 -0.033 0.607 0.015 1.000 0.016 -3.849 0.305 0.073 -5.0 -0.128 0.04478 -0.037 0.596 0.015 1.000 0.016 -2.854 0.306 -0.037 -4.5 -0.068 0.04084 -0.040 0.566 0.015 1.000 0.016 -1.654 0.306 -0.343 -4.0 -0.008 0.03724 -0.043 0.533 0.015 1.000 0.016 -0.204 0.307 -5.469 -3.5 0.052 0.03447 -0.047 0.496 0.015 1.000 0.016 1.508 0.308 1.152 -3.0 0.111 0.03151 -0.050 0.481 0.015 1.000 0.017 3.524 0.308 0.703 -2.5 0.170 0.02881 -0.054 0.466 0.015 1.000 0.017 5.884 0.309 0.567 -2.0 0.227 0.02637 -0.057 0.451 0.015 1.000 0.017 8.624 0.310 0.502 -1.5 0.285 0.02392 -0.061 0.440 0.016 1.000 0.018 11.893 0.311 0.463 -1.0 0.341 0.02247 -0.064 0.429 0.016 1.000 0.018 15.174 0.313 0.438 -0.5 0.397 0.02035 -0.068 0.418 0.017 1.000 0.019 19.487 0.314 0.421 0.0 0.451 0.01655 -0.071 0.411 0.018 1.000 0.020 27.270 0.293 0.408 0.5 0.509 0.01622 -0.073 0.399 0.019 1.000 0.022 31.413 0.273 0.392 1.0 0.568 0.01672 -0.074 0.388 0.020 1.000 0.023 33.951 0.321 0.380 1.5 0.572 0.02274 -0.077 0.381 0.022 0.903 0.972 25.172 0.367 0.385 2.0 0.616 0.02331 -0.080 0.373 0.024 0.878 0.972 26.412 0.307 0.379 2.5 0.662 0.02437 -0.082 0.366 0.086 0.861 0.972 27.153 0.322 0.374 3.0 0.697 0.02553 -0.085 0.362 0.092 0.825 0.973 27.313 0.345 0.373 3.5 0.734 0.02745 -0.089 0.355 0.097 0.793 0.972 26.737 0.500 0.371 4.0 0.735 0.03111 -0.095 0.351 0.952 0.696 0.954 23.629 0.541 0.379 4.5 0.768 0.03228 -0.099 0.348 0.955 0.663 0.956 23.800 0.355 0.379 5.0 0.810 0.03372 -0.103 0.341 0.955 0.646 0.956 24.017 0.358 0.377 5.5 0.843 0.03565 -0.107 0.341 0.955 0.616 0.957 23.632 0.396 0.377 6.0 0.871 0.03859 -0.112 0.337 0.955 0.580 0.957 22.575 0.225 0.378 6.5 1.099 0.03429 -0.101 0.050 0.955 0.853 0.957 32.054 0.224 0.342 7.0 1.137 0.03600 -0.105 0.046 0.955 0.830 0.957 31.575 0.361 0.342 7.5 1.173 0.03820 -0.109 0.043 0.955 0.806 0.957 30.717 0.421 0.343 8.0 1.195 0.04059 -0.115 0.040 0.955 0.763 0.957 29.451 0.550 0.346 8.5 1.213 0.04345 -0.121 0.038 0.955 0.716 0.957 27.926 0.477 0.350 9.0 1.244 0.04645 -0.126 0.036 0.953 0.690 0.955 26.783 0.402 0.351 9.5 1.277 0.05051 -0.130 0.036 0.953 0.667 0.955 25.272 0.363 0.352 10.0 1.318 0.05230 -0.134 0.012 0.953 0.660 0.955 25.209 0.378 0.352 10.5 1.344 0.05701 -0.139 0.009 0.953 0.637 0.955 23.570 0.480 0.353 11.0 1.362 0.06051 -0.144 0.008 0.953 0.610 0.955 22.515 0.077 0.356 11.5 1.252 0.07109 -0.155 0.007 0.953 0.011 0.955 17.617 0.075 0.374 12.0 1.281 0.07585 -0.159 0.006 0.953 0.009 0.955 16.892 0.385 0.374 12.5 1.306 0.08106 -0.162 0.005 0.953 0.009 0.955 16.116 0.404 0.374 13.0 1.329 0.08584 -0.166 0.004 0.959 0.008 0.960 15.480 0.429 0.375 13.5 1.347 0.09212 -0.169 0.004 0.959 0.007 0.960 14.623 0.473 0.376 14.0 1.362 0.09892 -0.173 0.004 0.959 0.006 0.960 13.764 0.540 0.377 14.5 1.372 0.10663 -0.177 0.003 0.959 0.006 0.960 12.869 0.663 0.379 15.0 1.379 0.11607 -0.180 0.003 0.959 0.006 0.960 11.883 0.775 0.381 Name = GOE 336 (MVA H.44) 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 -0.415 0.19147 0.026 0.852 0.013 0.928 0.014 -2.165 0.533 0.312 -14.5 -0.404 0.17803 0.023 0.847 0.013 0.928 0.014 -2.271 0.509 0.307 -14.0 -0.392 0.15683 0.020 0.842 0.013 0.928 0.014 -2.501 0.470 0.301 -13.5 -0.378 0.14689 0.017 0.837 0.013 0.933 0.014 -2.573 0.442 0.295 -13.0 -0.362 0.14151 0.014 0.837 0.013 0.928 0.015 -2.555 0.420 0.289 -12.5 -0.343 0.13386 0.011 0.831 0.014 0.933 0.015 -2.563 0.404 0.282 -12.0 -0.323 0.11926 0.008 0.831 0.014 0.928 0.015 -2.705 0.391 0.275 -11.5 -0.300 0.11341 0.005 0.831 0.014 0.939 0.015 -2.647 0.378 0.267 -11.0 -0.275 0.10557 0.002 0.700 0.014 1.000 0.015 -2.603 0.367 0.257 -10.5 -0.248 0.10002 -0.001 0.689 0.014 1.000 0.015 -2.475 0.362 0.246 -10.0 -0.219 0.09137 -0.004 0.679 0.014 1.000 0.015 -2.399 0.359 0.231 -9.5 -0.190 0.08155 -0.007 0.668 0.014 1.000 0.015 -2.327 0.356 0.211 -9.0 -0.160 0.07351 -0.010 0.663 0.015 1.000 0.016 -2.171 0.353 0.184 -8.5 -0.128 0.06964 -0.014 0.652 0.015 1.000 0.016 -1.843 0.351 0.143 -8.0 -0.096 0.06398 -0.017 0.647 0.015 1.000 0.016 -1.506 0.350 0.075 -7.5 -0.064 0.06014 -0.020 0.642 0.015 1.000 0.016 -1.057 0.348 -0.067 -7.0 -0.030 0.05573 -0.023 0.631 0.015 1.000 0.016 -0.540 0.223 -0.528 -6.5 -0.309 0.05185 -0.027 0.621 0.014 1.000 0.016 -5.965 0.220 0.164 -6.0 -0.249 0.04716 -0.030 0.614 0.014 1.000 0.016 -5.276 0.305 0.129 -5.5 -0.188 0.04375 -0.033 0.607 0.015 1.000 0.016 -4.303 0.305 0.073 -5.0 -0.128 0.04003 -0.037 0.596 0.015 1.000 0.016 -3.193 0.306 -0.037 -4.5 -0.068 0.03673 -0.040 0.566 0.015 1.000 0.016 -1.839 0.306 -0.343 -4.0 -0.008 0.03425 -0.043 0.533 0.015 1.000 0.016 -0.222 0.307 -5.468 -3.5 0.052 0.03125 -0.047 0.496 0.015 1.000 0.016 1.663 0.308 1.152 -3.0 0.111 0.02889 -0.050 0.481 0.015 1.000 0.017 3.843 0.308 0.703 -2.5 0.170 0.02640 -0.054 0.466 0.015 1.000 0.017 6.421 0.309 0.567 -2.0 0.227 0.02390 -0.057 0.451 0.015 1.000 0.017 9.515 0.310 0.501 -1.5 0.285 0.02211 -0.061 0.440 0.016 1.000 0.018 12.867 0.311 0.463 -1.0 0.341 0.02030 -0.064 0.429 0.016 1.000 0.018 16.799 0.313 0.438 -0.5 0.397 0.01825 -0.068 0.418 0.017 1.000 0.019 21.725 0.314 0.421 0.0 0.451 0.01396 -0.071 0.411 0.018 1.000 0.021 32.327 0.293 0.408 0.5 0.509 0.01412 -0.073 0.399 0.019 1.000 0.022 36.080 0.273 0.392 1.0 0.568 0.01438 -0.074 0.388 0.020 1.000 0.024 39.458 0.273 0.380 1.5 0.626 0.01735 -0.075 0.381 0.022 1.000 0.973 36.057 0.273 0.370 2.0 0.684 0.01778 -0.077 0.373 0.024 1.000 0.974 38.467 0.274 0.362 2.5 0.742 0.01817 -0.078 0.366 0.086 1.000 0.974 40.851 0.274 0.355 3.0 0.800 0.01833 -0.079 0.362 0.092 1.000 0.974 43.660 0.274 0.349 3.5 0.859 0.01975 -0.081 0.355 0.097 1.000 0.973 43.485 0.459 0.344 4.0 0.841 0.02362 -0.088 0.351 0.952 0.882 0.954 35.602 1.031 0.354 4.5 0.873 0.02455 -0.092 0.348 0.955 0.843 0.956 35.557 0.360 0.355 5.0 0.911 0.02572 -0.096 0.341 0.955 0.816 0.956 35.416 0.462 0.355 5.5 0.920 0.02791 -0.102 0.341 0.955 0.743 0.957 32.958 0.709 0.361 6.0 0.937 0.03039 -0.107 0.337 0.955 0.686 0.957 30.826 0.232 0.365 6.5 1.125 0.03061 -0.098 0.050 0.955 0.890 0.957 36.740 0.226 0.337 7.0 1.163 0.03205 -0.102 0.046 0.955 0.866 0.957 36.288 0.356 0.338 7.5 1.200 0.03381 -0.106 0.043 0.955 0.843 0.957 35.502 0.373 0.338 8.0 1.234 0.03531 -0.111 0.040 0.955 0.816 0.957 34.943 0.410 0.340 8.5 1.262 0.03786 -0.116 0.038 0.955 0.783 0.957 33.331 0.510 0.342 9.0 1.279 0.04139 -0.122 0.036 0.953 0.736 0.955 30.899 0.578 0.346 9.5 1.299 0.04456 -0.128 0.036 0.953 0.697 0.955 29.161 0.428 0.349 10.0 1.336 0.04743 -0.133 0.012 0.953 0.682 0.955 28.165 0.396 0.349 10.5 1.362 0.05076 -0.137 0.009 0.953 0.660 0.955 26.826 0.451 0.351 11.0 1.385 0.05477 -0.142 0.008 0.953 0.637 0.955 25.282 0.095 0.353 11.5 1.249 0.06685 -0.155 0.007 0.953 0.012 0.955 18.683 0.098 0.374 12.0 1.278 0.07119 -0.159 0.006 0.953 0.011 0.955 17.954 0.383 0.374 12.5 1.304 0.07518 -0.162 0.005 0.953 0.009 0.955 17.343 0.402 0.374 13.0 1.326 0.08008 -0.166 0.004 0.959 0.008 0.960 16.561 0.428 0.375 13.5 1.345 0.08542 -0.169 0.004 0.959 0.008 0.960 15.743 0.471 0.376 14.0 1.359 0.09170 -0.173 0.004 0.959 0.007 0.960 14.823 0.536 0.377 14.5 1.370 0.09756 -0.177 0.003 0.959 0.007 0.960 14.047 0.649 0.379 15.0 1.378 0.10465 -0.180 0.003 0.959 0.006 0.960 13.165 0.754 0.381 Name = GOE 336 (MVA H.44) 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 -0.415 0.16980 0.026 0.852 0.013 0.933 0.014 -2.441 0.533 0.312 -14.5 -0.404 0.15898 0.023 0.847 0.013 0.939 0.014 -2.543 0.509 0.307 -14.0 -0.392 0.14032 0.020 0.842 0.013 0.933 0.014 -2.795 0.470 0.301 -13.5 -0.378 0.13210 0.017 0.837 0.013 0.939 0.014 -2.861 0.442 0.295 -13.0 -0.362 0.12636 0.014 0.837 0.013 0.933 0.015 -2.862 0.420 0.289 -12.5 -0.343 0.12002 0.011 0.831 0.014 0.939 0.015 -2.858 0.404 0.282 -12.0 -0.323 0.10728 0.008 0.831 0.014 0.933 0.015 -3.007 0.391 0.275 -11.5 -0.300 0.10256 0.005 0.831 0.014 1.000 0.015 -2.927 0.378 0.267 -11.0 -0.275 0.09540 0.002 0.700 0.014 1.000 0.015 -2.881 0.367 0.257 -10.5 -0.248 0.09096 -0.001 0.689 0.014 1.000 0.015 -2.721 0.362 0.246 -10.0 -0.219 0.08300 -0.004 0.679 0.014 1.000 0.015 -2.641 0.358 0.231 -9.5 -0.190 0.07876 -0.007 0.668 0.014 1.000 0.015 -2.410 0.355 0.211 -9.0 -0.160 0.07082 -0.010 0.663 0.015 1.000 0.016 -2.254 0.353 0.184 -8.5 -0.128 0.06423 -0.014 0.652 0.015 1.000 0.016 -1.999 0.351 0.143 -8.0 -0.096 0.06161 -0.017 0.647 0.015 1.000 0.016 -1.564 0.350 0.075 -7.5 -0.064 0.05563 -0.020 0.642 0.015 1.000 0.016 -1.143 0.348 -0.067 -7.0 -0.030 0.05189 -0.023 0.631 0.015 1.000 0.016 -0.580 0.223 -0.528 -6.5 -0.309 0.04787 -0.027 0.621 0.014 1.000 0.016 -6.460 0.220 0.164 -6.0 -0.249 0.04519 -0.030 0.614 0.014 1.000 0.016 -5.505 0.305 0.129 -5.5 -0.188 0.04088 -0.033 0.607 0.015 1.000 0.016 -4.605 0.305 0.073 -5.0 -0.128 0.03826 -0.037 0.596 0.015 1.000 0.016 -3.341 0.306 -0.037 -4.5 -0.068 0.03520 -0.040 0.566 0.015 1.000 0.016 -1.919 0.306 -0.343 -4.0 -0.008 0.03224 -0.043 0.533 0.015 1.000 0.016 -0.236 0.307 -5.468 -3.5 0.052 0.02995 -0.047 0.496 0.015 1.000 0.017 1.735 0.308 1.152 -3.0 0.111 0.02719 -0.050 0.481 0.015 1.000 0.017 4.084 0.308 0.703 -2.5 0.170 0.02489 -0.054 0.466 0.015 1.000 0.017 6.812 0.309 0.567 -2.0 0.227 0.02287 -0.057 0.451 0.015 1.000 0.018 9.941 0.310 0.501 -1.5 0.285 0.02092 -0.061 0.440 0.016 1.000 0.018 13.601 0.311 0.463 -1.0 0.341 0.01873 -0.064 0.429 0.016 1.000 0.019 18.203 0.313 0.438 -0.5 0.397 0.01708 -0.068 0.418 0.017 1.000 0.020 23.217 0.314 0.421 0.0 0.451 0.01272 -0.071 0.411 0.018 1.000 0.021 35.468 0.293 0.408 0.5 0.509 0.01287 -0.073 0.399 0.019 1.000 0.022 39.600 0.273 0.392 1.0 0.568 0.01295 -0.074 0.388 0.020 1.000 0.024 43.810 0.273 0.380 1.5 0.626 0.01561 -0.075 0.381 0.022 1.000 0.974 40.072 0.273 0.370 2.0 0.684 0.01637 -0.077 0.373 0.024 1.000 0.975 41.779 0.274 0.362 2.5 0.742 0.01647 -0.078 0.366 0.086 1.000 0.975 45.051 0.274 0.355 3.0 0.800 0.01699 -0.079 0.362 0.092 1.000 0.975 47.108 0.274 0.349 3.5 0.859 0.01782 -0.081 0.355 0.097 1.000 0.974 48.204 0.274 0.344 4.0 0.917 0.01799 -0.082 0.351 0.952 1.000 0.954 50.975 0.274 0.340 4.5 0.975 0.02067 -0.084 0.348 0.955 1.000 0.956 47.198 0.453 0.336 5.0 0.962 0.02228 -0.091 0.341 0.955 0.897 0.956 43.193 0.707 0.345 5.5 1.000 0.02336 -0.095 0.341 0.955 0.870 0.957 42.834 0.370 0.345 6.0 1.031 0.02437 -0.100 0.337 0.955 0.833 0.957 42.299 0.223 0.347 6.5 1.207 0.02766 -0.089 0.050 0.955 1.000 0.957 43.631 0.251 0.324 7.0 1.185 0.02955 -0.100 0.046 0.955 0.897 0.957 40.095 1.366 0.334 7.5 1.220 0.03084 -0.104 0.043 0.955 0.870 0.957 39.561 0.369 0.335 8.0 1.257 0.03294 -0.108 0.040 0.955 0.846 0.957 38.148 0.379 0.336 8.5 1.289 0.03463 -0.113 0.038 0.955 0.820 0.957 37.239 0.420 0.338 9.0 1.316 0.03745 -0.118 0.036 0.953 0.786 0.955 35.147 0.552 0.340 9.5 1.330 0.04085 -0.125 0.036 0.953 0.737 0.955 32.556 0.633 0.344 10.0 1.350 0.04480 -0.131 0.012 0.953 0.700 0.955 30.124 0.488 0.347 10.5 1.376 0.04798 -0.136 0.009 0.953 0.677 0.955 28.670 0.449 0.349 11.0 1.399 0.05118 -0.141 0.008 0.953 0.655 0.955 27.331 0.481 0.351 11.5 1.419 0.05496 -0.146 0.007 0.953 0.632 0.955 25.816 0.108 0.353 12.0 1.275 0.06837 -0.159 0.006 0.953 0.012 0.955 18.649 0.112 0.374 12.5 1.301 0.07205 -0.162 0.005 0.953 0.010 0.955 18.056 0.400 0.375 13.0 1.324 0.07654 -0.166 0.004 0.959 0.009 0.960 17.293 0.425 0.375 13.5 1.343 0.08125 -0.170 0.004 0.959 0.008 0.960 16.524 0.468 0.376 14.0 1.357 0.08724 -0.173 0.004 0.959 0.008 0.960 15.556 0.535 0.378 14.5 1.368 0.09302 -0.177 0.003 0.959 0.007 0.960 14.709 0.647 0.379 15.0 1.376 0.10023 -0.180 0.003 0.959 0.007 0.960 13.723 0.751 0.381