Name = NACA M18 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 -0.678 0.24489 0.078 0.800 0.014 0.906 0.015 -2.770 0.422 0.365 -14.5 -0.663 0.23216 0.075 0.783 0.015 0.911 0.016 -2.854 0.419 0.364 -14.0 -0.645 0.23064 0.072 0.772 0.014 0.906 0.015 -2.798 0.409 0.362 -13.5 -0.627 0.20306 0.070 0.761 0.015 0.906 0.016 -3.087 0.397 0.361 -13.0 -0.607 0.18160 0.067 0.753 0.015 0.895 0.016 -3.341 0.389 0.360 -12.5 -0.585 0.17500 0.064 0.742 0.015 0.889 0.016 -3.343 0.382 0.359 -12.0 -0.562 0.16866 0.061 0.737 0.015 0.879 0.016 -3.333 0.376 0.358 -11.5 -0.538 0.15035 0.058 0.726 0.015 0.874 0.016 -3.577 0.370 0.358 -11.0 -0.512 0.14578 0.055 0.716 0.015 0.868 0.016 -3.513 0.366 0.357 -10.5 -0.485 0.13373 0.052 0.711 0.014 0.858 0.015 -3.629 0.362 0.357 -10.0 -0.457 0.12638 0.049 0.684 0.014 0.863 0.016 -3.618 0.357 0.356 -9.5 -0.428 0.11073 0.046 0.647 0.015 0.879 0.016 -3.863 0.354 0.356 -9.0 -0.397 0.10470 0.042 0.616 0.015 0.884 0.016 -3.795 0.352 0.357 -8.5 -0.366 0.09837 0.039 0.594 0.015 0.879 0.016 -3.719 0.350 0.357 -8.0 -0.334 0.08790 0.036 0.583 0.015 0.868 0.016 -3.794 0.348 0.358 -7.5 -0.300 0.08175 0.033 0.572 0.015 0.858 0.017 -3.672 0.346 0.359 -7.0 -0.266 0.07625 0.030 0.567 0.015 0.842 0.017 -3.488 0.345 0.361 -6.5 -0.231 0.07158 0.026 0.556 0.015 0.832 0.017 -3.228 0.344 0.364 -6.0 -0.196 0.06609 0.023 0.548 0.015 0.816 0.017 -2.959 0.343 0.367 -5.5 -0.159 0.06103 0.020 0.542 0.015 0.800 0.017 -2.611 0.342 0.373 -5.0 -0.123 0.05598 0.016 0.535 0.016 0.781 0.017 -2.191 0.342 0.382 -4.5 -0.085 0.05277 0.013 0.529 0.016 0.761 0.017 -1.617 0.342 0.400 -4.0 -0.048 0.04912 0.009 0.523 0.015 0.742 0.017 -0.975 0.341 0.445 -3.5 -0.010 0.04544 0.006 0.516 0.016 0.726 0.018 -0.212 0.182 0.863 -3.0 -0.150 0.04168 0.002 0.513 0.016 0.694 0.018 -3.603 0.161 0.266 -2.5 -0.088 0.03926 -0.001 0.506 0.016 0.674 0.019 -2.250 0.307 0.238 -2.0 -0.027 0.03631 -0.005 0.500 0.016 0.655 0.019 -0.746 0.308 0.079 -1.5 0.033 0.03427 -0.008 0.481 0.017 0.665 0.019 0.975 0.309 0.495 -1.0 0.093 0.03196 -0.012 0.461 0.017 0.665 0.020 2.916 0.311 0.376 -0.5 0.152 0.03013 -0.015 0.439 0.018 0.671 0.021 5.048 -0.098 0.351 0.0 0.072 0.02766 -0.019 0.423 0.020 0.661 0.023 2.618 0.013 0.512 0.5 0.123 0.02794 -0.022 0.403 0.021 0.658 0.025 4.416 0.317 0.430 1.0 0.168 0.03361 -0.025 0.390 0.024 0.642 0.966 5.012 0.322 0.401 1.5 0.216 0.03613 -0.029 0.377 0.874 0.632 0.955 5.976 0.333 0.383 2.0 0.253 0.03772 -0.032 0.371 0.882 0.603 0.955 6.719 0.338 0.378 2.5 0.299 0.03866 -0.036 0.365 0.889 0.590 0.955 7.723 0.329 0.371 3.0 0.345 0.04028 -0.040 0.355 0.903 0.581 0.955 8.564 0.334 0.365 3.5 0.388 0.04166 -0.044 0.348 0.953 0.565 0.954 9.302 0.344 0.362 4.0 0.428 0.04396 -0.048 0.345 0.953 0.545 0.954 9.734 0.345 0.361 4.5 0.471 0.04557 -0.051 0.339 0.953 0.532 0.955 10.333 0.346 0.359 5.0 0.512 0.04728 -0.056 0.335 0.953 0.516 0.955 10.820 0.355 0.359 5.5 0.550 0.05001 -0.060 0.332 0.954 0.497 0.955 11.001 0.368 0.359 6.0 0.585 0.05260 -0.064 0.329 0.954 0.468 0.955 11.127 0.360 0.360 6.5 0.629 0.05508 -0.068 0.323 0.954 0.458 0.955 11.412 0.365 0.359 7.0 0.661 0.05781 -0.073 0.319 0.954 0.429 0.956 11.440 0.368 0.360 7.5 0.703 0.06051 -0.077 0.313 0.954 0.419 0.956 11.618 0.242 0.360 8.0 0.912 0.04847 -0.071 0.024 0.954 0.668 0.956 18.818 0.243 0.328 8.5 0.948 0.05086 -0.076 0.022 0.954 0.648 0.956 18.647 0.379 0.330 9.0 0.984 0.05384 -0.080 0.020 0.954 0.629 0.956 18.268 -0.012 0.332 9.5 0.888 0.06719 -0.091 0.019 0.952 0.026 0.953 13.217 -0.017 0.353 10.0 0.927 0.07122 -0.095 0.019 0.952 0.024 0.953 13.016 0.351 0.353 10.5 0.965 0.07374 -0.099 0.018 0.957 0.023 0.958 13.083 0.354 0.353 11.0 1.002 0.07724 -0.103 0.017 0.957 0.022 0.958 12.974 0.358 0.353 11.5 1.037 0.08611 -0.107 0.017 0.952 0.021 0.954 12.048 0.368 0.353 12.0 1.069 0.09392 -0.111 0.016 0.952 0.021 0.954 11.382 0.373 0.354 12.5 1.101 0.09815 -0.115 0.015 0.952 0.019 0.954 11.220 0.376 0.354 13.0 1.131 0.10210 -0.119 0.015 0.957 0.018 0.959 11.077 0.392 0.355 13.5 1.157 0.11395 -0.123 0.014 0.957 0.019 0.959 10.152 0.401 0.356 14.0 1.183 0.11817 -0.127 0.013 0.957 0.017 0.959 10.012 0.409 0.357 14.5 1.206 0.12497 -0.131 0.011 0.957 0.017 0.959 9.650 0.429 0.358 15.0 1.227 0.13458 -0.135 0.010 0.957 0.016 0.959 9.117 0.436 0.360 Name = NACA M18 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 -0.678 0.20137 0.078 0.800 0.014 0.928 0.015 -3.368 0.423 0.365 -14.5 -0.663 0.17514 0.075 0.783 0.015 0.939 0.016 -3.783 0.420 0.364 -14.0 -0.645 0.17164 0.072 0.772 0.014 0.939 0.015 -3.760 0.409 0.362 -13.5 -0.627 0.15432 0.070 0.761 0.015 0.939 0.016 -4.061 0.397 0.361 -13.0 -0.607 0.14964 0.067 0.753 0.015 0.939 0.016 -4.054 0.389 0.360 -12.5 -0.585 0.14362 0.064 0.742 0.015 0.939 0.016 -4.074 0.382 0.359 -12.0 -0.562 0.12978 0.061 0.737 0.015 0.933 0.016 -4.332 0.376 0.358 -11.5 -0.538 0.12476 0.058 0.726 0.015 0.933 0.016 -4.311 0.370 0.358 -11.0 -0.512 0.11275 0.055 0.716 0.015 0.928 0.016 -4.543 0.366 0.357 -10.5 -0.485 0.11099 0.052 0.711 0.014 0.917 0.016 -4.373 0.362 0.357 -10.0 -0.457 0.09871 0.049 0.684 0.014 0.933 0.016 -4.632 0.357 0.356 -9.5 -0.428 0.09143 0.046 0.647 0.015 1.000 0.016 -4.678 0.354 0.357 -9.0 -0.397 0.08597 0.042 0.616 0.015 1.000 0.016 -4.621 0.352 0.357 -8.5 -0.366 0.07679 0.039 0.594 0.015 1.000 0.016 -4.765 0.350 0.357 -8.0 -0.333 0.07272 0.036 0.583 0.015 1.000 0.016 -4.586 0.348 0.358 -7.5 -0.300 0.06728 0.033 0.572 0.015 1.000 0.017 -4.461 0.346 0.359 -7.0 -0.266 0.06416 0.030 0.567 0.015 1.000 0.017 -4.145 0.345 0.361 -6.5 -0.231 0.06023 0.026 0.556 0.015 0.944 0.017 -3.836 0.344 0.364 -6.0 -0.195 0.05596 0.023 0.548 0.015 0.930 0.017 -3.494 0.343 0.367 -5.5 -0.159 0.05154 0.020 0.542 0.015 0.910 0.017 -3.090 0.342 0.373 -5.0 -0.123 0.04758 0.016 0.535 0.016 0.894 0.017 -2.576 0.342 0.382 -4.5 -0.085 0.04452 0.013 0.529 0.016 0.877 0.018 -1.915 0.342 0.400 -4.0 -0.048 0.04161 0.009 0.523 0.015 0.865 0.017 -1.149 0.341 0.446 -3.5 -0.010 0.03850 0.006 0.516 0.016 0.848 0.018 -0.248 0.182 0.869 -3.0 -0.150 0.03582 0.002 0.513 0.016 0.823 0.018 -4.193 0.161 0.266 -2.5 -0.088 0.03323 -0.001 0.506 0.016 0.810 0.019 -2.658 0.307 0.238 -2.0 -0.027 0.03107 -0.005 0.500 0.016 0.794 0.019 -0.872 0.308 0.079 -1.5 0.033 0.02892 -0.008 0.481 0.017 0.803 0.019 1.156 0.309 0.495 -1.0 0.093 0.02679 -0.012 0.461 0.017 0.806 0.020 3.477 0.311 0.376 -0.5 0.152 0.02519 -0.015 0.439 0.018 0.813 0.022 6.038 0.418 0.351 0.0 0.136 0.02018 -0.019 0.423 0.020 0.810 0.023 6.756 0.411 0.389 0.5 0.190 0.02444 -0.022 0.403 0.021 0.806 0.967 7.790 0.300 0.363 1.0 0.240 0.02515 -0.024 0.390 0.024 0.794 0.968 9.531 0.305 0.351 1.5 0.290 0.02590 -0.027 0.377 0.874 0.784 0.955 11.195 0.313 0.343 2.0 0.333 0.02704 -0.030 0.371 0.882 0.761 0.956 12.319 0.321 0.340 2.5 0.379 0.02772 -0.033 0.365 0.889 0.745 0.956 13.668 0.324 0.338 3.0 0.422 0.02885 -0.037 0.355 0.903 0.726 0.956 14.631 0.334 0.337 3.5 0.463 0.02972 -0.040 0.348 0.953 0.703 0.954 15.570 0.353 0.337 4.0 0.497 0.03169 -0.044 0.345 0.953 0.671 0.954 15.695 0.359 0.339 4.5 0.537 0.03306 -0.048 0.339 0.953 0.648 0.955 16.232 0.355 0.340 5.0 0.575 0.03508 -0.053 0.335 0.953 0.626 0.955 16.386 0.374 0.341 5.5 0.606 0.03700 -0.057 0.332 0.954 0.594 0.955 16.387 0.374 0.344 6.0 0.646 0.03914 -0.061 0.329 0.954 0.574 0.955 16.491 0.352 0.345 6.5 0.688 0.04043 -0.065 0.323 0.954 0.561 0.955 17.007 0.361 0.345 7.0 0.723 0.04309 -0.070 0.319 0.954 0.539 0.956 16.774 0.366 0.347 7.5 0.763 0.04495 -0.074 0.313 0.954 0.526 0.956 16.976 0.242 0.347 8.0 0.948 0.04038 -0.068 0.024 0.954 0.716 0.956 23.481 0.243 0.322 8.5 0.985 0.04247 -0.073 0.022 0.954 0.697 0.956 23.189 0.383 0.324 9.0 1.018 0.04538 -0.077 0.020 0.954 0.674 0.956 22.442 0.392 0.326 9.5 1.052 0.04818 -0.082 0.019 0.952 0.654 0.953 21.843 0.394 0.328 10.0 1.085 0.05149 -0.087 0.019 0.952 0.633 0.953 21.075 0.061 0.330 10.5 0.962 0.06684 -0.099 0.018 0.957 0.025 0.958 14.390 0.061 0.353 11.0 0.999 0.06997 -0.103 0.017 0.957 0.024 0.958 14.281 0.355 0.353 11.5 1.036 0.07511 -0.107 0.017 0.952 0.022 0.954 13.793 0.364 0.353 12.0 1.068 0.08044 -0.111 0.016 0.952 0.022 0.954 13.272 0.373 0.354 12.5 1.100 0.08475 -0.115 0.015 0.952 0.020 0.954 12.978 0.376 0.355 13.0 1.130 0.08881 -0.119 0.015 0.957 0.019 0.959 12.720 0.392 0.355 13.5 1.156 0.09634 -0.123 0.014 0.957 0.020 0.959 11.994 0.399 0.356 14.0 1.183 0.09720 -0.127 0.013 0.957 0.018 0.959 12.166 0.409 0.357 14.5 1.205 0.10246 -0.131 0.011 0.957 0.018 0.959 11.758 0.439 0.359 15.0 1.225 0.11585 -0.135 0.010 0.957 0.018 0.959 10.571 0.450 0.360 Name = NACA M18 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 -0.678 0.17073 0.078 0.800 0.014 1.000 0.015 -3.973 0.423 0.365 -14.5 -0.663 0.15026 0.075 0.783 0.015 1.000 0.016 -4.410 0.419 0.364 -14.0 -0.645 0.15732 0.072 0.772 0.014 1.000 0.015 -4.103 0.408 0.362 -13.5 -0.627 0.14222 0.070 0.761 0.015 1.000 0.016 -4.407 0.397 0.361 -13.0 -0.607 0.12768 0.067 0.753 0.015 1.000 0.016 -4.752 0.389 0.360 -12.5 -0.585 0.12194 0.064 0.742 0.015 1.000 0.016 -4.798 0.382 0.359 -12.0 -0.562 0.11192 0.061 0.737 0.015 1.000 0.016 -5.023 0.376 0.358 -11.5 -0.538 0.10705 0.058 0.726 0.015 1.000 0.016 -5.024 0.370 0.358 -11.0 -0.512 0.10381 0.055 0.716 0.015 1.000 0.016 -4.934 0.366 0.357 -10.5 -0.485 0.09661 0.052 0.711 0.014 1.000 0.016 -5.024 0.362 0.357 -10.0 -0.457 0.09075 0.049 0.684 0.014 1.000 0.016 -5.038 0.357 0.356 -9.5 -0.428 0.08045 0.046 0.647 0.015 1.000 0.016 -5.317 0.354 0.357 -9.0 -0.397 0.07577 0.042 0.616 0.015 1.000 0.016 -5.244 0.352 0.357 -8.5 -0.366 0.07080 0.039 0.594 0.015 1.000 0.017 -5.167 0.350 0.357 -8.0 -0.333 0.06723 0.036 0.583 0.015 1.000 0.017 -4.960 0.348 0.358 -7.5 -0.300 0.06231 0.033 0.572 0.015 1.000 0.017 -4.815 0.346 0.359 -7.0 -0.266 0.05744 0.030 0.567 0.015 1.000 0.017 -4.629 0.345 0.361 -6.5 -0.231 0.05370 0.026 0.556 0.015 1.000 0.017 -4.301 0.344 0.364 -6.0 -0.195 0.05021 0.023 0.548 0.015 1.000 0.017 -3.894 0.343 0.367 -5.5 -0.159 0.04731 0.020 0.542 0.015 1.000 0.017 -3.365 0.342 0.373 -5.0 -0.123 0.04376 0.016 0.535 0.016 1.000 0.017 -2.800 0.342 0.382 -4.5 -0.085 0.04091 0.013 0.529 0.016 1.000 0.018 -2.082 0.342 0.400 -4.0 -0.048 0.03820 0.009 0.523 0.015 1.000 0.017 -1.250 0.341 0.446 -3.5 -0.009 0.03546 0.006 0.516 0.016 0.940 0.018 -0.267 0.182 0.875 -3.0 -0.150 0.03291 0.002 0.513 0.016 0.900 0.019 -4.564 0.161 0.266 -2.5 -0.088 0.03067 -0.001 0.506 0.016 0.887 0.019 -2.880 0.307 0.238 -2.0 -0.027 0.02861 -0.005 0.500 0.016 0.874 0.019 -0.947 0.308 0.079 -1.5 0.033 0.02673 -0.008 0.481 0.017 0.884 0.020 1.250 0.309 0.495 -1.0 0.093 0.02457 -0.012 0.461 0.017 0.884 0.021 3.792 0.311 0.376 -0.5 0.152 0.02308 -0.015 0.439 0.018 0.887 0.022 6.590 0.349 0.351 0.0 0.166 0.01703 -0.019 0.423 0.020 0.881 0.024 9.758 0.333 0.364 0.5 0.222 0.02143 -0.021 0.403 0.021 0.877 0.969 10.348 0.291 0.345 1.0 0.274 0.02205 -0.023 0.390 0.024 0.868 0.970 12.434 0.295 0.336 1.5 0.326 0.02202 -0.026 0.377 0.874 0.858 0.956 14.809 0.302 0.329 2.0 0.373 0.02229 -0.029 0.371 0.882 0.839 0.956 16.726 0.307 0.327 2.5 0.422 0.02283 -0.031 0.365 0.889 0.826 0.956 18.490 0.310 0.324 3.0 0.469 0.02380 -0.034 0.355 0.903 0.810 0.956 19.716 0.319 0.323 3.5 0.514 0.02439 -0.038 0.348 0.953 0.790 0.954 21.051 0.333 0.323 4.0 0.553 0.02550 -0.041 0.345 0.953 0.765 0.954 21.689 0.336 0.325 4.5 0.597 0.02671 -0.045 0.339 0.953 0.748 0.955 22.366 0.338 0.325 5.0 0.637 0.02782 -0.049 0.335 0.953 0.726 0.955 22.904 0.362 0.327 5.5 0.672 0.02950 -0.053 0.332 0.954 0.697 0.955 22.765 0.386 0.329 6.0 0.703 0.03146 -0.058 0.329 0.954 0.665 0.955 22.363 0.370 0.332 6.5 0.745 0.03329 -0.062 0.323 0.954 0.648 0.955 22.368 0.392 0.333 7.0 0.769 0.03542 -0.067 0.319 0.954 0.610 0.956 21.714 0.392 0.337 7.5 0.810 0.03749 -0.071 0.313 0.954 0.597 0.956 21.616 0.243 0.338 8.0 0.975 0.03591 -0.066 0.024 0.954 0.752 0.956 27.161 0.245 0.317 8.5 1.013 0.03868 -0.070 0.022 0.954 0.732 0.956 26.178 0.381 0.319 9.0 1.046 0.04107 -0.075 0.020 0.954 0.710 0.956 25.473 0.389 0.322 9.5 1.081 0.04379 -0.080 0.019 0.952 0.690 0.953 24.686 0.414 0.324 10.0 1.108 0.04703 -0.085 0.019 0.952 0.662 0.953 23.557 0.086 0.327 10.5 0.961 0.06193 -0.099 0.018 0.957 0.026 0.958 15.513 0.085 0.353 11.0 0.998 0.06476 -0.103 0.017 0.957 0.025 0.958 15.406 0.355 0.354 11.5 1.035 0.07024 -0.107 0.017 0.952 0.023 0.954 14.730 0.364 0.354 12.0 1.066 0.07452 -0.111 0.016 0.952 0.023 0.954 14.309 0.373 0.354 12.5 1.099 0.07890 -0.115 0.015 0.952 0.021 0.954 13.923 0.374 0.355 13.0 1.129 0.08090 -0.119 0.015 0.957 0.020 0.959 13.956 0.392 0.355 13.5 1.154 0.08875 -0.123 0.014 0.957 0.021 0.959 13.006 0.401 0.357 14.0 1.181 0.09056 -0.127 0.013 0.957 0.019 0.959 13.043 0.414 0.357 14.5 1.202 0.09918 -0.131 0.011 0.957 0.020 0.959 12.123 0.439 0.359 15.0 1.223 0.10008 -0.135 0.010 0.957 0.019 0.959 12.224 0.436 0.360 Name = NACA M18 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 -0.678 0.15272 0.078 0.800 0.014 1.000 0.015 -4.441 0.422 0.365 -14.5 -0.663 0.14440 0.075 0.783 0.015 1.000 0.016 -4.589 0.419 0.364 -14.0 -0.645 0.13981 0.072 0.772 0.014 1.000 0.015 -4.616 0.409 0.362 -13.5 -0.627 0.12762 0.070 0.761 0.015 1.000 0.016 -4.911 0.397 0.361 -13.0 -0.607 0.12224 0.067 0.753 0.015 1.000 0.016 -4.963 0.389 0.360 -12.5 -0.585 0.11002 0.064 0.742 0.015 1.000 0.016 -5.318 0.382 0.359 -12.0 -0.562 0.10735 0.061 0.737 0.015 1.000 0.016 -5.237 0.376 0.358 -11.5 -0.538 0.09739 0.058 0.726 0.015 1.000 0.016 -5.522 0.370 0.358 -11.0 -0.512 0.09408 0.055 0.716 0.015 1.000 0.016 -5.444 0.366 0.357 -10.5 -0.485 0.08803 0.052 0.711 0.014 1.000 0.016 -5.513 0.362 0.357 -10.0 -0.457 0.08287 0.049 0.684 0.014 1.000 0.016 -5.517 0.357 0.356 -9.5 -0.428 0.07700 0.046 0.647 0.015 1.000 0.016 -5.555 0.354 0.357 -9.0 -0.397 0.07241 0.042 0.616 0.015 1.000 0.017 -5.487 0.352 0.357 -8.5 -0.366 0.06752 0.039 0.594 0.015 1.000 0.017 -5.417 0.350 0.357 -8.0 -0.333 0.06215 0.036 0.583 0.015 1.000 0.017 -5.365 0.348 0.358 -7.5 -0.300 0.05747 0.033 0.572 0.015 1.000 0.017 -5.221 0.346 0.359 -7.0 -0.266 0.05345 0.030 0.567 0.015 1.000 0.017 -4.974 0.345 0.361 -6.5 -0.231 0.04976 0.026 0.556 0.015 1.000 0.017 -4.642 0.344 0.364 -6.0 -0.195 0.04784 0.023 0.548 0.015 1.000 0.017 -4.085 0.343 0.367 -5.5 -0.159 0.04486 0.020 0.542 0.015 1.000 0.018 -3.548 0.342 0.373 -5.0 -0.122 0.04190 0.016 0.535 0.016 1.000 0.018 -2.922 0.342 0.382 -4.5 -0.085 0.03898 0.013 0.529 0.016 1.000 0.018 -2.183 0.341 0.400 -4.0 -0.048 0.03674 0.009 0.523 0.015 1.000 0.018 -1.295 0.341 0.447 -3.5 -0.009 0.03361 0.006 0.516 0.016 1.000 0.018 -0.279 0.182 0.880 -3.0 -0.150 0.03104 0.002 0.513 0.016 1.000 0.019 -4.838 0.161 0.266 -2.5 -0.088 0.02886 -0.001 0.506 0.016 1.000 0.019 -3.060 0.307 0.238 -2.0 -0.027 0.02693 -0.005 0.500 0.016 1.000 0.019 -1.006 0.308 0.080 -1.5 0.033 0.02517 -0.008 0.481 0.017 1.000 0.020 1.328 0.309 0.495 -1.0 0.093 0.02327 -0.012 0.461 0.017 1.000 0.021 4.004 0.311 0.376 -0.5 0.152 0.02046 -0.015 0.439 0.018 1.000 0.022 7.434 0.312 0.351 0.0 0.210 0.01580 -0.019 0.423 0.020 1.000 0.024 13.301 0.293 0.340 0.5 0.270 0.01947 -0.020 0.403 0.021 1.000 0.970 13.847 0.293 0.326 1.0 0.299 0.01997 -0.023 0.390 0.024 0.923 0.971 14.962 0.312 0.326 1.5 0.346 0.01953 -0.025 0.377 0.874 0.900 0.956 17.734 0.298 0.323 2.0 0.397 0.02013 -0.028 0.371 0.882 0.887 0.956 19.727 0.299 0.319 2.5 0.448 0.02044 -0.030 0.365 0.889 0.874 0.956 21.890 0.304 0.317 3.0 0.496 0.02113 -0.033 0.355 0.903 0.858 0.956 23.447 0.311 0.316 3.5 0.543 0.02157 -0.036 0.348 0.953 0.842 0.954 25.171 0.318 0.316 4.0 0.588 0.02265 -0.039 0.345 0.953 0.823 0.955 25.946 0.323 0.317 4.5 0.634 0.02331 -0.042 0.339 0.953 0.806 0.955 27.180 0.328 0.317 5.0 0.677 0.02417 -0.046 0.335 0.953 0.787 0.955 27.993 0.341 0.318 5.5 0.717 0.02556 -0.050 0.332 0.954 0.765 0.955 28.031 0.357 0.320 6.0 0.753 0.02702 -0.054 0.329 0.954 0.739 0.955 27.879 0.354 0.322 6.5 0.795 0.02841 -0.058 0.323 0.954 0.723 0.955 27.994 0.373 0.323 7.0 0.825 0.02999 -0.063 0.319 0.954 0.690 0.956 27.516 0.387 0.327 7.5 0.863 0.03187 -0.068 0.313 0.954 0.671 0.956 27.084 0.251 0.328 8.0 1.000 0.03337 -0.063 0.024 0.954 0.784 0.956 29.967 0.254 0.313 8.5 1.033 0.03497 -0.068 0.022 0.954 0.758 0.956 29.535 0.394 0.316 9.0 1.067 0.03739 -0.073 0.020 0.954 0.735 0.956 28.531 0.381 0.318 9.5 1.104 0.04025 -0.078 0.019 0.952 0.718 0.953 27.420 0.406 0.320 10.0 1.131 0.04327 -0.083 0.019 0.952 0.690 0.953 26.135 0.435 0.323 10.5 1.161 0.04518 -0.088 0.018 0.957 0.667 0.958 25.697 0.435 0.326 11.0 1.188 0.04854 -0.094 0.017 0.957 0.641 0.958 24.467 0.101 0.329 11.5 1.033 0.06724 -0.107 0.017 0.952 0.024 0.954 15.366 0.106 0.354 12.0 1.065 0.07092 -0.111 0.016 0.952 0.024 0.954 15.017 0.371 0.354 12.5 1.098 0.07380 -0.115 0.015 0.952 0.022 0.954 14.876 0.374 0.355 13.0 1.128 0.07775 -0.119 0.015 0.957 0.021 0.959 14.504 0.394 0.356 13.5 1.153 0.08417 -0.123 0.014 0.957 0.022 0.959 13.698 0.401 0.357 14.0 1.180 0.08664 -0.127 0.013 0.957 0.020 0.959 13.620 0.414 0.358 14.5 1.201 0.09160 -0.131 0.011 0.957 0.021 0.959 13.113 0.445 0.359 15.0 1.221 0.09740 -0.135 0.010 0.957 0.021 0.959 12.536 0.450 0.360