Name = LOCKHEED L-188 ROOT 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 -0.757 0.16145 0.033 0.850 0.007 0.952 0.009 -4.691 0.392 0.293 -14.5 -0.736 0.15500 0.030 0.846 0.007 0.946 0.010 -4.750 0.387 0.290 -14.0 -0.714 0.14270 0.027 0.842 0.007 0.941 0.010 -5.000 0.374 0.287 -13.5 -0.687 0.13338 0.024 0.838 0.007 0.934 0.010 -5.154 0.363 0.284 -13.0 -0.660 0.12559 0.021 0.834 0.008 0.928 0.011 -5.253 0.357 0.281 -12.5 -0.630 0.11751 0.017 0.830 0.008 0.922 0.012 -5.365 0.353 0.278 -12.0 -0.600 0.10890 0.014 0.827 0.009 0.915 0.012 -5.510 0.349 0.274 -11.5 -0.568 0.10305 0.011 0.823 0.009 0.909 0.013 -5.513 0.345 0.270 -11.0 -0.535 0.09618 0.008 0.820 0.009 0.903 0.014 -5.564 0.343 0.265 -10.5 -0.501 0.09012 0.005 0.817 0.010 0.896 0.014 -5.559 0.340 0.260 -10.0 -0.466 0.08429 0.002 0.814 0.011 0.890 0.015 -5.524 0.337 0.254 -9.5 -0.429 0.07962 -0.001 0.811 0.012 0.884 0.016 -5.388 0.335 0.247 -9.0 -0.392 0.07430 -0.004 0.806 0.012 0.879 0.017 -5.272 0.334 0.239 -8.5 -0.353 0.06995 -0.008 0.799 0.013 0.876 0.018 -5.053 0.332 0.229 -8.0 -0.314 0.06543 -0.011 0.791 0.014 0.873 0.019 -4.806 0.331 0.216 -7.5 -0.275 0.06149 -0.014 0.784 0.015 0.870 0.021 -4.467 0.329 0.199 -7.0 -0.234 0.05802 -0.017 0.774 0.016 0.868 0.023 -4.033 0.328 0.177 -6.5 -0.193 0.05464 -0.020 0.759 0.018 0.868 0.026 -3.524 0.326 0.145 -6.0 -0.150 0.05174 -0.023 0.744 0.020 0.868 0.030 -2.903 0.325 0.094 -5.5 -0.107 0.04901 -0.027 0.731 0.023 0.866 0.035 -2.185 0.323 0.001 -5.0 -0.063 0.04653 -0.030 0.718 0.027 0.864 0.042 -1.354 0.320 -0.223 -4.5 -0.017 0.04431 -0.033 0.705 0.030 0.862 0.056 -0.387 0.214 -1.670 -4.0 -0.226 0.04242 -0.036 0.692 0.040 0.859 0.107 -5.334 0.071 0.092 -3.5 -0.140 0.02808 -0.055 0.680 0.054 0.856 0.983 -4.985 0.394 -0.142 -3.0 -0.082 0.02800 -0.056 0.667 0.090 0.852 0.990 -2.928 0.210 -0.439 -2.5 -0.031 0.02959 -0.051 0.656 0.518 0.848 0.724 -1.035 0.223 -1.401 -2.0 0.031 0.02911 -0.053 0.643 0.529 0.844 0.740 1.070 0.295 1.965 -1.5 0.093 0.02876 -0.056 0.632 0.541 0.839 0.756 3.219 0.293 0.856 -1.0 0.154 0.02852 -0.059 0.621 0.553 0.833 0.769 5.391 0.291 0.632 -0.5 0.215 0.02835 -0.061 0.609 0.564 0.828 0.787 7.573 0.414 0.535 0.0 0.183 0.02913 -0.063 0.598 0.575 0.823 0.897 6.279 0.450 0.597 0.5 0.237 0.02953 -0.066 0.588 0.587 0.817 0.939 8.032 0.291 0.527 1.0 0.291 0.02993 -0.068 0.577 0.598 0.811 0.961 9.726 0.293 0.483 1.5 0.344 0.03043 -0.070 0.567 0.609 0.802 0.974 11.295 0.297 0.454 2.0 0.394 0.03105 -0.073 0.557 0.622 0.791 0.983 12.700 0.300 0.434 2.5 0.445 0.03180 -0.075 0.547 0.633 0.780 0.992 13.988 0.304 0.419 3.0 0.493 0.02892 -0.078 0.536 0.646 0.765 1.000 17.037 0.310 0.408 3.5 0.540 0.02989 -0.081 0.526 0.659 0.750 1.000 18.055 0.313 0.400 4.0 0.586 0.03110 -0.084 0.516 0.671 0.735 1.000 18.851 0.315 0.393 4.5 0.633 0.03235 -0.087 0.504 0.685 0.722 1.000 19.583 0.317 0.387 5.0 0.679 0.03376 -0.090 0.493 0.698 0.708 1.000 20.109 0.239 0.383 5.5 0.841 0.03166 -0.085 0.075 0.711 0.867 1.000 26.578 0.236 0.351 6.0 0.889 0.03290 -0.087 0.056 0.725 0.856 1.000 27.036 0.312 0.348 6.5 0.933 0.03435 -0.090 0.043 0.739 0.841 1.000 27.156 0.397 0.347 7.0 0.948 0.03689 -0.096 0.038 0.753 0.790 1.000 25.699 0.092 0.351 7.5 0.776 0.05884 -0.115 0.030 0.766 0.071 1.000 13.186 0.074 0.398 8.0 0.822 0.06193 -0.118 0.027 0.780 0.053 1.000 13.276 0.317 0.394 8.5 0.865 0.06532 -0.121 0.024 0.975 0.042 1.000 13.249 0.325 0.390 9.0 0.906 0.06922 -0.124 0.021 0.979 0.037 1.000 13.084 0.330 0.387 9.5 0.945 0.07312 -0.128 0.019 0.984 0.032 1.000 12.918 0.334 0.385 10.0 0.982 0.07772 -0.131 0.017 0.988 0.028 1.000 12.634 0.338 0.383 10.5 1.018 0.08199 -0.134 0.015 1.000 0.025 1.000 12.411 0.342 0.382 11.0 1.052 0.08741 -0.137 0.014 1.000 0.023 1.000 12.034 0.346 0.380 11.5 1.085 0.09357 -0.140 0.013 1.000 0.021 1.000 11.591 0.350 0.379 12.0 1.116 0.09951 -0.144 0.012 1.000 0.019 1.000 11.215 0.355 0.379 12.5 1.146 0.10644 -0.147 0.012 1.000 0.018 1.000 10.764 0.361 0.378 13.0 1.174 0.11274 -0.150 0.011 1.000 0.017 1.000 10.412 0.369 0.378 13.5 1.199 0.12062 -0.153 0.010 1.000 0.016 1.000 9.941 0.382 0.378 14.0 1.222 0.12848 -0.156 0.009 1.000 0.015 1.000 9.512 0.395 0.378 14.5 1.243 0.13736 -0.159 0.009 1.000 0.014 1.000 9.050 0.410 0.378 15.0 1.262 0.14654 -0.163 0.008 1.000 0.013 1.000 8.611 0.418 0.379 Name = LOCKHEED L-188 ROOT 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 -0.756 0.13285 0.033 0.850 0.007 0.976 0.010 -5.694 0.394 0.293 -14.5 -0.736 0.12481 0.030 0.846 0.007 0.972 0.010 -5.894 0.387 0.290 -14.0 -0.713 0.11746 0.027 0.842 0.007 0.968 0.011 -6.066 0.373 0.287 -13.5 -0.686 0.11132 0.024 0.838 0.007 0.963 0.011 -6.165 0.363 0.284 -13.0 -0.659 0.10499 0.021 0.834 0.008 0.959 0.012 -6.275 0.357 0.281 -12.5 -0.630 0.09793 0.018 0.830 0.008 0.952 0.013 -6.429 0.352 0.278 -12.0 -0.599 0.09229 0.014 0.827 0.009 0.947 0.013 -6.491 0.349 0.274 -11.5 -0.567 0.08619 0.011 0.823 0.009 0.940 0.014 -6.582 0.345 0.270 -11.0 -0.534 0.08169 0.008 0.820 0.009 0.933 0.015 -6.538 0.342 0.265 -10.5 -0.500 0.07684 0.005 0.817 0.010 0.926 0.015 -6.505 0.340 0.260 -10.0 -0.464 0.07218 0.002 0.814 0.011 0.919 0.016 -6.434 0.337 0.254 -9.5 -0.428 0.06793 -0.001 0.811 0.012 0.912 0.017 -6.301 0.335 0.247 -9.0 -0.391 0.06394 -0.004 0.806 0.012 0.907 0.018 -6.108 0.334 0.239 -8.5 -0.352 0.06026 -0.007 0.799 0.013 0.905 0.019 -5.844 0.332 0.229 -8.0 -0.313 0.05685 -0.011 0.791 0.014 0.903 0.021 -5.506 0.330 0.216 -7.5 -0.273 0.05357 -0.014 0.784 0.015 0.900 0.024 -5.094 0.328 0.199 -7.0 -0.232 0.05056 -0.017 0.774 0.016 0.900 0.027 -4.587 0.327 0.177 -6.5 -0.190 0.04777 -0.020 0.759 0.018 0.905 0.030 -3.981 0.324 0.144 -6.0 -0.147 0.04532 -0.023 0.744 0.020 0.907 0.037 -3.245 0.322 0.091 -5.5 -0.103 0.04304 -0.026 0.731 0.023 0.907 0.045 -2.393 0.316 -0.007 -5.0 -0.056 0.04097 -0.029 0.718 0.027 0.906 0.070 -1.358 0.085 -0.278 -4.5 -0.261 0.02336 -0.053 0.705 0.030 0.906 0.983 -11.167 0.083 0.048 -4.0 -0.204 0.02325 -0.054 0.692 0.040 0.905 0.992 -8.776 0.279 -0.016 -3.5 -0.152 0.01722 -0.056 0.680 0.054 0.903 1.000 -8.839 0.273 -0.116 -3.0 -0.091 0.01686 -0.057 0.667 0.090 0.901 1.000 -5.417 0.249 -0.372 -2.5 -0.002 0.02133 -0.056 0.656 0.518 0.897 0.926 -0.100 0.258 -25.940 -2.0 0.031 0.02116 -0.058 0.643 0.529 0.894 0.953 1.461 0.291 2.120 -1.5 0.092 0.02109 -0.060 0.632 0.541 0.891 0.969 4.366 0.276 0.897 -1.0 0.153 0.02107 -0.061 0.621 0.553 0.885 0.978 7.271 0.272 0.648 -0.5 0.214 0.02111 -0.062 0.609 0.564 0.881 0.987 10.153 0.294 0.541 0.0 0.211 0.01801 -0.063 0.598 0.575 0.876 1.000 11.699 0.310 0.551 0.5 0.266 0.01840 -0.065 0.588 0.587 0.870 1.000 14.463 0.285 0.496 1.0 0.321 0.01882 -0.067 0.577 0.598 0.865 1.000 17.074 0.286 0.460 1.5 0.376 0.01967 -0.069 0.567 0.609 0.859 1.000 19.127 0.288 0.434 2.0 0.430 0.02017 -0.072 0.557 0.622 0.852 1.000 21.322 0.290 0.416 2.5 0.484 0.02072 -0.074 0.547 0.633 0.846 1.000 23.348 0.292 0.402 3.0 0.537 0.02133 -0.076 0.536 0.646 0.839 1.000 25.169 0.294 0.391 3.5 0.589 0.02191 -0.078 0.526 0.659 0.831 1.000 26.884 0.296 0.383 4.0 0.641 0.02265 -0.081 0.516 0.671 0.823 1.000 28.285 0.297 0.376 4.5 0.693 0.02343 -0.083 0.504 0.685 0.817 1.000 29.559 0.299 0.370 5.0 0.743 0.02430 -0.086 0.493 0.698 0.809 1.000 30.569 0.249 0.365 5.5 0.862 0.02620 -0.083 0.075 0.711 0.894 1.000 32.898 0.248 0.346 6.0 0.911 0.02734 -0.085 0.056 0.725 0.885 1.000 33.334 0.300 0.344 6.5 0.960 0.02857 -0.088 0.043 0.739 0.875 1.000 33.596 0.305 0.342 7.0 1.006 0.02984 -0.091 0.038 0.753 0.864 1.000 33.722 0.313 0.340 7.5 1.050 0.03132 -0.094 0.030 0.766 0.851 1.000 33.541 0.337 0.339 8.0 1.085 0.03301 -0.098 0.027 0.780 0.829 1.000 32.866 0.109 0.340 8.5 0.847 0.05888 -0.122 0.024 0.975 0.087 1.000 14.384 0.106 0.395 9.0 0.894 0.06181 -0.125 0.021 0.979 0.057 1.000 14.463 0.314 0.390 9.5 0.935 0.06493 -0.128 0.019 0.984 0.046 1.000 14.406 0.326 0.387 10.0 0.975 0.06838 -0.131 0.017 0.988 0.038 1.000 14.253 0.331 0.384 10.5 1.012 0.07180 -0.134 0.015 1.000 0.032 1.000 14.091 0.337 0.383 11.0 1.047 0.07622 -0.137 0.014 1.000 0.029 1.000 13.733 0.343 0.381 11.5 1.080 0.08085 -0.141 0.013 1.000 0.026 1.000 13.361 0.347 0.380 12.0 1.112 0.08549 -0.144 0.012 1.000 0.023 1.000 13.010 0.352 0.379 12.5 1.142 0.09057 -0.147 0.012 1.000 0.022 1.000 12.613 0.359 0.379 13.0 1.171 0.09547 -0.150 0.011 1.000 0.020 1.000 12.263 0.368 0.378 13.5 1.196 0.10184 -0.153 0.010 1.000 0.018 1.000 11.744 0.382 0.378 14.0 1.219 0.10830 -0.156 0.009 1.000 0.017 1.000 11.257 0.393 0.378 14.5 1.240 0.11462 -0.160 0.009 1.000 0.016 1.000 10.821 0.407 0.379 15.0 1.259 0.12094 -0.163 0.008 1.000 0.015 1.000 10.413 0.415 0.379 Name = LOCKHEED L-188 ROOT 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 -0.756 0.12036 0.033 0.850 0.007 0.989 0.011 -6.277 0.395 0.293 -14.5 -0.735 0.11313 0.030 0.846 0.007 0.986 0.011 -6.494 0.387 0.290 -14.0 -0.712 0.10754 0.027 0.842 0.007 0.983 0.012 -6.618 0.373 0.288 -13.5 -0.686 0.10130 0.024 0.838 0.007 0.980 0.012 -6.768 0.364 0.285 -13.0 -0.658 0.09467 0.021 0.834 0.008 0.976 0.013 -6.953 0.357 0.281 -12.5 -0.629 0.08920 0.018 0.830 0.008 0.972 0.014 -7.049 0.352 0.278 -12.0 -0.598 0.08413 0.015 0.827 0.009 0.968 0.014 -7.110 0.348 0.274 -11.5 -0.566 0.07938 0.011 0.823 0.009 0.963 0.015 -7.133 0.345 0.270 -11.0 -0.533 0.07531 0.008 0.820 0.009 0.957 0.016 -7.076 0.342 0.266 -10.5 -0.499 0.07101 0.005 0.817 0.010 0.950 0.017 -7.023 0.340 0.260 -10.0 -0.463 0.06687 0.002 0.814 0.011 0.944 0.018 -6.928 0.337 0.254 -9.5 -0.427 0.06315 -0.001 0.811 0.012 0.937 0.019 -6.759 0.335 0.247 -9.0 -0.389 0.05938 -0.004 0.806 0.012 0.931 0.020 -6.557 0.333 0.239 -8.5 -0.351 0.05619 -0.007 0.799 0.013 0.930 0.022 -6.245 0.331 0.229 -8.0 -0.311 0.05304 -0.011 0.791 0.014 0.928 0.024 -5.871 0.329 0.216 -7.5 -0.271 0.05022 -0.014 0.784 0.015 0.926 0.027 -5.392 0.327 0.199 -7.0 -0.230 0.04744 -0.017 0.774 0.016 0.927 0.031 -4.839 0.324 0.176 -6.5 -0.186 0.04503 -0.020 0.759 0.018 0.933 0.039 -4.140 0.320 0.143 -6.0 -0.142 0.04276 -0.023 0.744 0.020 0.936 0.051 -3.323 0.309 0.088 -5.5 -0.094 0.04034 -0.025 0.731 0.023 0.938 0.107 -2.336 0.091 -0.020 -5.0 -0.321 0.02136 -0.051 0.718 0.027 0.938 0.984 -15.042 0.088 0.090 -4.5 -0.265 0.02133 -0.053 0.705 0.030 0.938 0.994 -12.436 0.279 0.050 -4.0 -0.213 0.01498 -0.055 0.692 0.040 0.937 1.000 -14.224 0.273 -0.006 -3.5 -0.152 0.01531 -0.056 0.680 0.054 0.936 1.000 -9.945 0.268 -0.116 -3.0 -0.091 0.01493 -0.057 0.667 0.090 0.934 1.000 -6.118 0.262 -0.372 -2.5 -0.019 0.01822 -0.057 0.656 0.518 0.931 0.983 -1.036 0.266 -2.791 -2.0 0.031 0.01822 -0.059 0.643 0.529 0.929 0.991 1.695 0.275 2.154 -1.5 0.092 0.01445 -0.060 0.632 0.541 0.925 1.000 6.368 0.270 0.904 -1.0 0.153 0.01462 -0.061 0.621 0.553 0.921 1.000 10.478 0.268 0.650 -0.5 0.214 0.01482 -0.062 0.609 0.564 0.917 1.000 14.457 0.279 0.541 0.0 0.230 0.01538 -0.063 0.598 0.575 0.913 1.000 14.967 0.289 0.526 0.5 0.287 0.01568 -0.065 0.588 0.587 0.907 1.000 18.279 0.281 0.477 1.0 0.343 0.01601 -0.067 0.577 0.598 0.902 1.000 21.408 0.282 0.445 1.5 0.398 0.01670 -0.069 0.567 0.609 0.897 1.000 23.857 0.284 0.423 2.0 0.453 0.01710 -0.071 0.557 0.622 0.890 1.000 26.516 0.285 0.406 2.5 0.508 0.01754 -0.073 0.547 0.633 0.884 1.000 28.975 0.287 0.393 3.0 0.562 0.01802 -0.075 0.536 0.646 0.878 1.000 31.192 0.289 0.383 3.5 0.615 0.01848 -0.077 0.526 0.659 0.870 1.000 33.285 0.292 0.375 4.0 0.668 0.01907 -0.079 0.516 0.671 0.863 1.000 34.999 0.293 0.368 4.5 0.720 0.01970 -0.081 0.504 0.685 0.856 1.000 36.560 0.295 0.363 5.0 0.772 0.02041 -0.084 0.493 0.698 0.849 1.000 37.805 0.253 0.359 5.5 0.876 0.02352 -0.082 0.075 0.711 0.913 1.000 37.244 0.253 0.343 6.0 0.925 0.02465 -0.084 0.056 0.725 0.903 1.000 37.545 0.301 0.341 6.5 0.973 0.02584 -0.087 0.043 0.739 0.892 1.000 37.651 0.305 0.339 7.0 1.020 0.02706 -0.089 0.038 0.753 0.880 1.000 37.683 0.309 0.338 7.5 1.065 0.02841 -0.092 0.030 0.766 0.869 1.000 37.493 0.313 0.337 8.0 1.109 0.02976 -0.095 0.027 0.780 0.857 1.000 37.258 0.326 0.336 8.5 1.148 0.03120 -0.099 0.024 0.975 0.841 1.000 36.792 0.376 0.336 9.0 1.173 0.03324 -0.103 0.021 0.979 0.812 1.000 35.296 0.115 0.338 9.5 0.918 0.06186 -0.130 0.019 0.984 0.100 1.000 14.838 0.114 0.391 10.0 0.964 0.06499 -0.132 0.017 0.988 0.059 1.000 14.832 0.311 0.387 10.5 1.003 0.06797 -0.135 0.015 1.000 0.047 1.000 14.757 0.329 0.384 11.0 1.040 0.07170 -0.138 0.014 1.000 0.039 1.000 14.503 0.335 0.383 11.5 1.075 0.07553 -0.141 0.013 1.000 0.033 1.000 14.231 0.341 0.381 12.0 1.108 0.07958 -0.144 0.012 1.000 0.029 1.000 13.920 0.350 0.380 12.5 1.138 0.08417 -0.147 0.012 1.000 0.026 1.000 13.523 0.357 0.379 13.0 1.167 0.08850 -0.150 0.011 1.000 0.024 1.000 13.185 0.366 0.379 13.5 1.193 0.09395 -0.153 0.010 1.000 0.022 1.000 12.694 0.378 0.379 14.0 1.216 0.09922 -0.157 0.009 1.000 0.020 1.000 12.257 0.391 0.379 14.5 1.237 0.10500 -0.160 0.009 1.000 0.019 1.000 11.784 0.406 0.379 15.0 1.257 0.11097 -0.163 0.008 1.000 0.018 1.000 11.323 0.415 0.380 Name = LOCKHEED L-188 ROOT 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 -0.755 0.11077 0.033 0.850 0.007 1.000 0.012 -6.816 0.394 0.293 -14.5 -0.734 0.10394 0.030 0.846 0.007 1.000 0.012 -7.063 0.387 0.291 -14.0 -0.711 0.10004 0.027 0.842 0.007 0.993 0.013 -7.108 0.372 0.288 -13.5 -0.685 0.09513 0.024 0.838 0.007 0.990 0.014 -7.199 0.363 0.285 -13.0 -0.657 0.08919 0.021 0.834 0.008 0.987 0.014 -7.372 0.357 0.281 -12.5 -0.628 0.08466 0.018 0.830 0.008 0.984 0.015 -7.416 0.351 0.278 -12.0 -0.597 0.07984 0.015 0.827 0.009 0.981 0.016 -7.480 0.348 0.274 -11.5 -0.565 0.07526 0.011 0.823 0.009 0.977 0.017 -7.510 0.345 0.270 -11.0 -0.532 0.07146 0.008 0.820 0.009 0.972 0.017 -7.443 0.342 0.266 -10.5 -0.498 0.06749 0.005 0.817 0.010 0.968 0.018 -7.373 0.340 0.261 -10.0 -0.462 0.06368 0.002 0.814 0.011 0.962 0.019 -7.257 0.338 0.255 -9.5 -0.426 0.06023 -0.001 0.811 0.012 0.957 0.020 -7.070 0.334 0.248 -9.0 -0.388 0.05697 -0.004 0.806 0.012 0.951 0.022 -6.809 0.332 0.239 -8.5 -0.349 0.05391 -0.007 0.799 0.013 0.951 0.025 -6.478 0.330 0.229 -8.0 -0.310 0.05091 -0.010 0.791 0.014 0.949 0.027 -6.079 0.328 0.216 -7.5 -0.268 0.04823 -0.014 0.784 0.015 0.947 0.032 -5.566 0.324 0.199 -7.0 -0.226 0.04574 -0.017 0.774 0.016 0.949 0.040 -4.943 0.319 0.176 -6.5 -0.182 0.04345 -0.020 0.759 0.018 0.955 0.055 -4.181 0.100 0.142 -6.0 -0.428 0.02076 -0.047 0.744 0.020 0.958 0.956 -20.617 0.096 0.140 -5.5 -0.380 0.02030 -0.050 0.731 0.023 0.959 0.982 -18.720 0.298 0.118 -5.0 -0.325 0.02007 -0.052 0.718 0.027 0.959 0.992 -16.171 0.282 0.090 -4.5 -0.274 0.01391 -0.054 0.705 0.030 0.959 1.000 -19.675 0.274 0.054 -4.0 -0.213 0.01385 -0.055 0.692 0.040 0.958 1.000 -15.383 0.268 -0.006 -3.5 -0.152 0.01414 -0.056 0.680 0.054 0.958 1.000 -10.770 0.268 -0.116 -3.0 -0.091 0.01375 -0.057 0.667 0.090 0.956 1.000 -6.641 0.268 -0.372 -2.5 -0.030 0.01289 -0.058 0.656 0.518 0.953 1.000 -2.348 0.268 -1.664 -2.0 0.031 0.01300 -0.059 0.643 0.529 0.951 1.000 2.374 0.268 2.162 -1.5 0.092 0.01314 -0.060 0.632 0.541 0.948 1.000 7.002 0.268 0.904 -1.0 0.153 0.01329 -0.061 0.621 0.553 0.944 1.000 11.522 0.268 0.650 -0.5 0.214 0.01348 -0.062 0.609 0.564 0.941 1.000 15.899 0.275 0.541 0.0 0.243 0.01385 -0.063 0.598 0.575 0.937 1.000 17.560 0.281 0.511 0.5 0.300 0.01410 -0.065 0.588 0.587 0.932 1.000 21.297 0.278 0.467 1.0 0.357 0.01439 -0.067 0.577 0.598 0.928 1.000 24.845 0.279 0.436 1.5 0.414 0.01498 -0.068 0.567 0.609 0.923 1.000 27.629 0.280 0.415 2.0 0.470 0.01531 -0.070 0.557 0.622 0.917 1.000 30.671 0.282 0.399 2.5 0.525 0.01568 -0.072 0.547 0.633 0.911 1.000 33.487 0.284 0.387 3.0 0.580 0.01608 -0.074 0.536 0.646 0.905 1.000 36.059 0.286 0.377 3.5 0.634 0.01647 -0.076 0.526 0.659 0.898 1.000 38.485 0.288 0.370 4.0 0.687 0.01697 -0.078 0.516 0.671 0.891 1.000 40.493 0.289 0.363 4.5 0.740 0.01750 -0.080 0.504 0.685 0.885 1.000 42.305 0.291 0.358 5.0 0.792 0.01810 -0.082 0.493 0.698 0.877 1.000 43.781 0.256 0.354 5.5 0.888 0.02180 -0.081 0.075 0.711 0.928 1.000 40.712 0.257 0.341 6.0 0.937 0.02288 -0.083 0.056 0.725 0.917 1.000 40.935 0.300 0.339 6.5 0.984 0.02405 -0.086 0.043 0.739 0.906 1.000 40.931 0.306 0.337 7.0 1.030 0.02521 -0.088 0.038 0.753 0.894 1.000 40.870 0.310 0.336 7.5 1.076 0.02654 -0.091 0.030 0.766 0.882 1.000 40.523 0.314 0.335 8.0 1.119 0.02785 -0.094 0.027 0.780 0.869 1.000 40.174 0.319 0.334 8.5 1.161 0.02910 -0.097 0.024 0.975 0.857 1.000 39.896 0.329 0.334 9.0 1.200 0.03067 -0.100 0.021 0.979 0.842 1.000 39.120 0.354 0.334 9.5 1.232 0.03241 -0.105 0.019 0.984 0.822 1.000 38.003 -2.333 0.335 10.0 1.194 0.03745 -0.116 0.017 0.988 0.717 1.000 31.879 0.119 0.347 10.5 0.991 0.06591 -0.136 0.015 1.000 0.085 1.000 15.035 0.112 0.387 11.0 1.031 0.06927 -0.139 0.014 1.000 0.057 1.000 14.889 0.319 0.384 11.5 1.068 0.07281 -0.141 0.013 1.000 0.044 1.000 14.672 0.333 0.382 12.0 1.102 0.07646 -0.144 0.012 1.000 0.038 1.000 14.413 0.344 0.381 12.5 1.134 0.08062 -0.147 0.012 1.000 0.033 1.000 14.061 0.352 0.380 13.0 1.163 0.08474 -0.151 0.011 1.000 0.030 1.000 13.720 0.363 0.380 13.5 1.189 0.08955 -0.154 0.010 1.000 0.027 1.000 13.275 0.376 0.379 14.0 1.213 0.09418 -0.157 0.009 1.000 0.025 1.000 12.875 0.388 0.379 14.5 1.234 0.09938 -0.160 0.009 1.000 0.023 1.000 12.420 0.401 0.380 15.0 1.254 0.10457 -0.163 0.008 1.000 0.021 1.000 11.989 0.409 0.380