Name = SG6040 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 -0.604 0.15159 -0.011 0.942 0.005 0.964 0.005 -3.985 0.388 0.233 -14.5 -0.581 0.14351 -0.014 0.939 0.004 0.963 0.005 -4.049 0.381 0.226 -14.0 -0.556 0.12938 -0.017 0.935 0.005 0.962 0.006 -4.294 0.373 0.220 -13.5 -0.529 0.12141 -0.020 0.919 0.004 0.963 0.005 -4.360 0.367 0.212 -13.0 -0.501 0.11361 -0.023 0.887 0.004 0.965 0.005 -4.408 0.359 0.204 -12.5 -0.471 0.10554 -0.026 0.867 0.004 0.965 0.006 -4.460 0.355 0.194 -12.0 -0.439 0.09972 -0.030 0.844 0.005 0.966 0.006 -4.404 0.350 0.182 -11.5 -0.406 0.08965 -0.033 0.818 0.005 0.967 0.006 -4.528 0.347 0.169 -11.0 -0.372 0.08456 -0.036 0.799 0.005 0.966 0.006 -4.403 0.345 0.153 -10.5 -0.337 0.07875 -0.039 0.786 0.005 0.965 0.006 -4.281 0.340 0.133 -10.0 -0.300 0.07321 -0.043 0.774 0.005 0.964 0.007 -4.098 0.339 0.108 -9.5 -0.263 0.06765 -0.046 0.763 0.005 0.962 0.007 -3.892 0.338 0.075 -9.0 -0.225 0.06346 -0.049 0.753 0.005 0.960 0.007 -3.545 0.335 0.031 -8.5 -0.186 0.05957 -0.053 0.743 0.005 0.958 0.007 -3.116 0.334 -0.034 -8.0 -0.146 0.05520 -0.056 0.733 0.006 0.955 0.008 -2.643 0.333 -0.134 -7.5 -0.105 0.05181 -0.059 0.724 0.006 0.951 0.008 -2.029 0.329 -0.314 -7.0 -0.062 0.04890 -0.063 0.716 0.007 0.945 0.011 -1.265 0.229 -0.762 -6.5 -0.352 0.04903 -0.064 0.704 0.008 0.942 0.075 -7.185 0.074 0.067 -6.0 -0.152 0.02954 -0.079 0.690 0.009 0.939 0.732 -5.155 0.305 -0.266 -5.5 -0.078 0.03081 -0.080 0.677 0.065 0.930 0.697 -2.530 0.299 -0.771 -5.0 -0.042 0.02933 -0.084 0.663 0.073 0.920 0.734 -1.448 21.803 -1.724 -4.5 -0.078 0.02828 -0.088 0.650 0.081 0.906 0.762 -2.743 0.269 -0.879 -4.0 -0.015 0.03243 -0.084 0.638 0.469 0.891 0.564 -0.470 0.251 -5.286 -3.5 0.048 0.03175 -0.088 0.623 0.479 0.881 0.568 1.509 0.302 2.080 -3.0 0.111 0.03118 -0.091 0.610 0.489 0.870 0.572 3.548 0.302 1.072 -2.5 0.173 0.03071 -0.094 0.592 0.500 0.863 0.575 5.631 0.303 0.795 -2.0 0.235 0.03032 -0.097 0.574 0.507 0.857 0.579 7.740 0.303 0.665 -1.5 0.296 0.02992 -0.101 0.559 0.511 0.845 0.585 9.891 0.303 0.590 -1.0 0.357 0.02955 -0.104 0.547 0.515 0.831 0.593 12.071 0.303 0.542 -0.5 0.417 0.02927 -0.107 0.535 0.519 0.814 0.601 14.246 0.992 0.507 0.0 0.365 0.02823 -0.110 0.520 0.522 0.804 0.610 12.937 9.931 0.552 0.5 0.418 0.02878 -0.113 0.504 0.526 0.795 0.618 14.508 0.296 0.520 1.0 0.470 0.02940 -0.115 0.488 0.530 0.786 0.628 15.984 0.298 0.495 1.5 0.522 0.03009 -0.118 0.471 0.535 0.778 0.638 17.341 0.301 0.476 2.0 0.573 0.03091 -0.120 0.455 0.539 0.767 0.649 18.521 0.304 0.460 2.5 0.622 0.03186 -0.123 0.441 0.543 0.755 0.661 19.516 0.308 0.448 3.0 0.670 0.03295 -0.126 0.427 0.547 0.742 0.676 20.328 0.309 0.438 3.5 0.720 0.03405 -0.129 0.409 0.551 0.733 0.695 21.130 0.309 0.429 4.0 0.769 0.03524 -0.132 0.391 0.556 0.723 0.714 21.814 0.314 0.422 4.5 0.815 0.03668 -0.135 0.375 0.560 0.711 0.736 22.222 0.323 0.416 5.0 0.858 0.03831 -0.139 0.360 0.565 0.694 0.765 22.407 0.330 0.411 5.5 0.901 0.04014 -0.142 0.345 0.570 0.677 0.798 22.445 0.333 0.408 6.0 0.943 0.04206 -0.146 0.328 0.575 0.662 0.838 22.431 0.329 0.404 6.5 0.988 0.04402 -0.149 0.307 0.581 0.651 0.899 22.452 0.323 0.401 7.0 1.035 0.04600 -0.152 0.283 0.589 0.645 0.975 22.500 0.334 0.397 7.5 1.074 0.04866 -0.156 0.264 0.598 0.627 0.992 22.063 0.249 0.395 8.0 1.208 0.04650 -0.152 0.068 0.609 0.743 0.993 25.976 0.246 0.376 8.5 1.250 0.04826 -0.155 0.028 0.621 0.733 0.994 25.904 0.410 0.374 9.0 1.264 0.05218 -0.161 0.024 0.635 0.689 0.995 24.234 0.099 0.377 9.5 1.105 0.07556 -0.177 0.021 0.651 0.074 0.995 14.621 0.068 0.410 10.0 1.163 0.07757 -0.180 0.017 0.669 0.039 0.996 14.996 0.303 0.404 10.5 1.205 0.08149 -0.183 0.015 0.691 0.029 0.996 14.785 0.331 0.402 11.0 1.240 0.08639 -0.186 0.014 0.715 0.025 0.997 14.357 0.342 0.400 11.5 1.275 0.09174 -0.189 0.012 0.742 0.022 0.997 13.895 0.347 0.398 12.0 1.306 0.09757 -0.192 0.011 0.778 0.019 0.997 13.389 0.354 0.397 12.5 1.337 0.10294 -0.195 0.010 0.832 0.017 0.997 12.984 0.362 0.396 13.0 1.364 0.10985 -0.199 0.009 0.992 0.016 0.994 12.415 0.371 0.396 13.5 1.390 0.11676 -0.202 0.008 0.992 0.015 0.995 11.905 0.378 0.395 14.0 1.414 0.12398 -0.205 0.008 0.992 0.013 0.995 11.404 0.396 0.395 14.5 1.434 0.13265 -0.208 0.007 0.993 0.012 0.995 10.809 0.420 0.395 15.0 1.452 0.13993 -0.211 0.007 0.993 0.011 0.995 10.373 0.430 0.396 Name = SG6040 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 -0.604 0.12477 -0.011 0.942 0.005 0.966 0.006 -4.840 0.388 0.233 -14.5 -0.581 0.11755 -0.014 0.939 0.004 0.965 0.005 -4.941 0.380 0.226 -14.0 -0.555 0.10688 -0.017 0.935 0.005 0.964 0.006 -5.196 0.373 0.220 -13.5 -0.529 0.10096 -0.020 0.919 0.004 0.966 0.005 -5.240 0.367 0.212 -13.0 -0.501 0.09445 -0.023 0.887 0.004 0.971 0.006 -5.299 0.359 0.204 -12.5 -0.470 0.08782 -0.026 0.867 0.004 0.972 0.006 -5.357 0.355 0.194 -12.0 -0.439 0.08322 -0.030 0.844 0.005 0.974 0.006 -5.274 0.349 0.182 -11.5 -0.405 0.07732 -0.033 0.818 0.005 0.975 0.006 -5.245 0.347 0.169 -11.0 -0.372 0.07150 -0.036 0.799 0.005 0.976 0.006 -5.205 0.345 0.153 -10.5 -0.337 0.06690 -0.039 0.786 0.005 0.975 0.006 -5.035 0.340 0.133 -10.0 -0.300 0.06222 -0.043 0.774 0.005 0.975 0.007 -4.817 0.339 0.107 -9.5 -0.263 0.05855 -0.046 0.763 0.005 0.974 0.007 -4.487 0.338 0.075 -9.0 -0.224 0.05505 -0.049 0.753 0.005 0.973 0.007 -4.076 0.335 0.030 -8.5 -0.185 0.05158 -0.053 0.743 0.005 0.972 0.008 -3.587 0.334 -0.035 -8.0 -0.145 0.04845 -0.056 0.733 0.006 0.971 0.008 -2.993 0.332 -0.136 -7.5 -0.104 0.04535 -0.059 0.724 0.006 0.969 0.009 -2.298 0.320 -0.319 -7.0 -0.054 0.04357 -0.062 0.716 0.007 0.967 0.018 -1.230 0.095 -0.915 -6.5 -0.218 0.02444 -0.077 0.704 0.008 0.966 0.752 -8.931 0.099 -0.103 -6.0 -0.174 0.02345 -0.081 0.690 0.009 0.965 0.773 -7.431 0.312 -0.213 -5.5 -0.119 0.02315 -0.083 0.677 0.065 0.963 0.774 -5.142 0.310 -0.449 -5.0 -0.074 0.02231 -0.087 0.663 0.073 0.962 0.797 -3.295 0.322 -0.929 -4.5 -0.025 0.02164 -0.090 0.650 0.081 0.960 0.818 -1.178 0.225 -3.277 -4.0 -0.015 0.02428 -0.085 0.638 0.469 0.959 0.600 -0.626 0.229 -5.354 -3.5 0.048 0.02373 -0.088 0.623 0.479 0.957 0.604 2.015 0.301 2.099 -3.0 0.110 0.02331 -0.092 0.610 0.489 0.955 0.607 4.737 0.301 1.079 -2.5 0.173 0.02300 -0.095 0.592 0.500 0.954 0.609 7.507 0.301 0.799 -2.0 0.234 0.02267 -0.098 0.574 0.507 0.952 0.613 10.337 0.302 0.668 -1.5 0.296 0.02228 -0.101 0.559 0.511 0.948 0.624 13.267 0.302 0.592 -1.0 0.356 0.02192 -0.104 0.547 0.515 0.943 0.637 16.262 0.301 0.543 -0.5 0.417 0.02165 -0.107 0.535 0.519 0.938 0.650 19.253 0.329 0.508 0.0 0.433 0.01992 -0.110 0.520 0.522 0.930 0.667 21.717 0.317 0.505 0.5 0.487 0.02027 -0.112 0.504 0.526 0.922 0.683 24.050 0.282 0.480 1.0 0.542 0.02067 -0.114 0.488 0.530 0.913 0.702 26.229 0.284 0.460 1.5 0.596 0.02114 -0.116 0.471 0.535 0.904 0.721 28.180 0.288 0.444 2.0 0.648 0.02169 -0.118 0.455 0.539 0.893 0.744 29.857 0.292 0.432 2.5 0.699 0.02232 -0.120 0.441 0.543 0.881 0.771 31.298 0.296 0.422 3.0 0.748 0.02305 -0.122 0.427 0.547 0.867 0.806 32.467 0.297 0.414 3.5 0.800 0.02384 -0.125 0.409 0.551 0.857 0.852 33.543 0.297 0.406 4.0 0.851 0.02471 -0.127 0.391 0.556 0.848 0.904 34.425 0.303 0.400 4.5 0.898 0.02570 -0.130 0.375 0.560 0.835 0.970 34.944 0.310 0.395 5.0 0.945 0.02680 -0.133 0.360 0.565 0.821 0.992 35.243 0.315 0.391 5.5 0.990 0.02827 -0.136 0.345 0.570 0.806 0.993 35.015 0.316 0.387 6.0 1.036 0.02971 -0.139 0.328 0.575 0.794 0.994 34.866 0.314 0.384 6.5 1.083 0.03119 -0.142 0.307 0.581 0.785 0.995 34.719 0.311 0.381 7.0 1.131 0.03276 -0.145 0.283 0.589 0.778 0.996 34.526 0.318 0.378 7.5 1.174 0.03464 -0.148 0.264 0.598 0.765 0.997 33.893 0.273 0.376 8.0 1.257 0.03734 -0.148 0.068 0.609 0.804 0.997 33.665 0.276 0.367 8.5 1.295 0.03967 -0.151 0.028 0.621 0.788 0.998 32.652 0.355 0.367 9.0 1.329 0.04196 -0.155 0.024 0.635 0.768 0.998 31.666 0.387 0.367 9.5 1.357 0.04452 -0.160 0.021 0.651 0.745 0.998 30.482 0.437 0.368 10.0 1.379 0.04754 -0.165 0.017 0.669 0.715 0.998 29.010 1.376 0.369 10.5 1.369 0.05270 -0.173 0.015 0.691 0.647 0.998 25.967 0.111 0.376 11.0 1.220 0.07717 -0.187 0.014 0.715 0.049 0.998 15.805 0.088 0.403 11.5 1.265 0.08003 -0.189 0.012 0.742 0.031 0.998 15.808 0.322 0.400 12.0 1.299 0.08422 -0.192 0.011 0.778 0.026 0.998 15.422 0.346 0.398 12.5 1.330 0.08858 -0.196 0.010 0.832 0.022 0.998 15.018 0.356 0.397 13.0 1.359 0.09329 -0.199 0.009 0.992 0.020 0.994 14.562 0.365 0.396 13.5 1.385 0.09850 -0.202 0.008 0.992 0.018 0.995 14.065 0.373 0.396 14.0 1.410 0.10385 -0.205 0.008 0.992 0.016 0.995 13.577 0.394 0.396 14.5 1.430 0.11132 -0.208 0.007 0.993 0.015 0.995 12.845 0.419 0.396 15.0 1.448 0.11762 -0.212 0.007 0.993 0.014 0.995 12.308 0.429 0.396 Name = SG6040 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 -0.604 0.10921 -0.011 0.942 0.005 0.967 0.006 -5.529 0.388 0.233 -14.5 -0.581 0.10289 -0.014 0.939 0.004 0.966 0.005 -5.645 0.380 0.226 -14.0 -0.555 0.09727 -0.017 0.935 0.005 0.966 0.006 -5.707 0.372 0.220 -13.5 -0.529 0.09222 -0.020 0.919 0.004 0.968 0.006 -5.735 0.367 0.212 -13.0 -0.500 0.08621 -0.023 0.887 0.004 0.974 0.006 -5.803 0.359 0.204 -12.5 -0.470 0.08015 -0.026 0.867 0.004 0.975 0.006 -5.866 0.354 0.194 -12.0 -0.439 0.07608 -0.030 0.844 0.005 0.978 0.006 -5.765 0.349 0.182 -11.5 -0.405 0.07080 -0.033 0.818 0.005 0.980 0.007 -5.724 0.347 0.169 -11.0 -0.372 0.06688 -0.036 0.799 0.005 0.981 0.006 -5.556 0.345 0.153 -10.5 -0.336 0.06262 -0.039 0.786 0.005 0.981 0.007 -5.371 0.340 0.133 -10.0 -0.299 0.05815 -0.043 0.774 0.005 0.981 0.007 -5.145 0.339 0.107 -9.5 -0.262 0.05462 -0.046 0.763 0.005 0.980 0.007 -4.800 0.338 0.074 -9.0 -0.224 0.05142 -0.049 0.753 0.005 0.979 0.008 -4.353 0.335 0.030 -8.5 -0.184 0.04811 -0.053 0.743 0.005 0.978 0.008 -3.834 0.334 -0.035 -8.0 -0.144 0.04524 -0.056 0.733 0.006 0.977 0.009 -3.193 0.328 -0.137 -7.5 -0.101 0.04287 -0.059 0.724 0.006 0.976 0.012 -2.349 0.106 -0.338 -7.0 -0.274 0.02256 -0.075 0.716 0.007 0.975 0.753 -12.129 0.103 -0.022 -6.5 -0.231 0.02154 -0.078 0.704 0.008 0.975 0.774 -10.710 0.332 -0.089 -6.0 -0.185 0.02063 -0.082 0.690 0.009 0.974 0.794 -8.973 0.319 -0.192 -5.5 -0.135 0.01992 -0.085 0.677 0.065 0.974 0.807 -6.788 0.316 -0.378 -5.0 -0.088 0.01921 -0.088 0.663 0.073 0.973 0.829 -4.586 0.322 -0.752 -4.5 -0.041 0.01856 -0.092 0.650 0.081 0.972 0.855 -2.197 0.222 -1.997 -4.0 -0.015 0.02001 -0.086 0.638 0.469 0.971 0.640 -0.757 0.224 -5.438 -3.5 0.048 0.01958 -0.089 0.623 0.479 0.970 0.645 2.437 0.299 2.123 -3.0 0.110 0.01924 -0.092 0.610 0.489 0.969 0.648 5.729 0.299 1.088 -2.5 0.172 0.01897 -0.095 0.592 0.500 0.968 0.650 9.085 0.299 0.804 -2.0 0.234 0.01871 -0.098 0.574 0.507 0.967 0.655 12.511 0.300 0.671 -1.5 0.295 0.01831 -0.102 0.559 0.511 0.966 0.672 16.127 0.301 0.594 -1.0 0.356 0.01791 -0.105 0.547 0.515 0.963 0.693 19.878 0.299 0.544 -0.5 0.417 0.01765 -0.108 0.535 0.519 0.960 0.714 23.607 0.310 0.508 0.0 0.450 0.01667 -0.110 0.520 0.522 0.958 0.740 26.984 0.296 0.495 0.5 0.509 0.01699 -0.112 0.504 0.526 0.957 0.767 29.976 0.276 0.470 1.0 0.568 0.01733 -0.113 0.488 0.530 0.954 0.799 32.759 0.277 0.450 1.5 0.625 0.01770 -0.115 0.471 0.535 0.950 0.833 35.328 0.278 0.434 2.0 0.682 0.01814 -0.117 0.455 0.539 0.946 0.876 37.619 0.280 0.421 2.5 0.739 0.01860 -0.118 0.441 0.543 0.941 0.927 39.701 0.282 0.410 3.0 0.793 0.01914 -0.120 0.427 0.547 0.933 0.976 41.420 0.286 0.402 3.5 0.846 0.01988 -0.122 0.409 0.551 0.924 0.992 42.556 0.289 0.394 4.0 0.898 0.02069 -0.124 0.391 0.556 0.916 0.993 43.408 0.295 0.388 4.5 0.947 0.02159 -0.127 0.375 0.560 0.902 0.994 43.854 0.302 0.384 5.0 0.995 0.02271 -0.129 0.360 0.565 0.889 0.995 43.795 0.305 0.380 5.5 1.042 0.02378 -0.132 0.345 0.570 0.876 0.996 43.796 0.308 0.377 6.0 1.088 0.02484 -0.135 0.328 0.575 0.863 0.997 43.820 0.309 0.374 6.5 1.135 0.02614 -0.138 0.307 0.581 0.852 0.998 43.432 0.310 0.371 7.0 1.182 0.02749 -0.140 0.283 0.589 0.842 0.998 42.997 0.318 0.369 7.5 1.224 0.02892 -0.144 0.264 0.598 0.828 0.998 42.331 0.301 0.367 8.0 1.281 0.03332 -0.145 0.068 0.609 0.833 0.998 38.445 0.312 0.363 8.5 1.316 0.03572 -0.149 0.028 0.621 0.813 0.998 36.835 0.360 0.363 9.0 1.351 0.03770 -0.153 0.024 0.635 0.795 0.998 35.836 0.366 0.363 9.5 1.383 0.03991 -0.157 0.021 0.651 0.776 0.998 34.661 0.383 0.364 10.0 1.413 0.04232 -0.161 0.017 0.669 0.755 0.998 33.386 0.416 0.364 10.5 1.437 0.04499 -0.166 0.015 0.691 0.731 0.998 31.954 0.539 0.365 11.0 1.449 0.04861 -0.172 0.014 0.715 0.693 0.999 29.820 -0.203 0.369 11.5 1.399 0.05660 -0.183 0.012 0.742 0.579 0.998 24.718 0.122 0.381 12.0 1.280 0.08031 -0.194 0.011 0.778 0.049 0.998 15.935 0.087 0.401 12.5 1.321 0.08299 -0.196 0.010 0.832 0.031 0.998 15.917 0.329 0.398 13.0 1.351 0.08651 -0.199 0.009 0.992 0.027 0.994 15.621 0.358 0.397 13.5 1.379 0.09124 -0.202 0.008 0.992 0.024 0.995 15.113 0.368 0.397 14.0 1.404 0.09658 -0.205 0.008 0.992 0.020 0.995 14.542 0.381 0.396 14.5 1.426 0.10127 -0.209 0.007 0.993 0.018 0.995 14.082 0.410 0.396 15.0 1.444 0.10714 -0.212 0.007 0.993 0.017 0.995 13.476 0.429 0.397 Name = SG6040 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 -0.604 0.10330 -0.011 0.942 0.005 0.968 0.006 -5.844 0.388 0.233 -14.5 -0.581 0.09700 -0.014 0.939 0.004 0.967 0.006 -5.986 0.380 0.226 -14.0 -0.555 0.09172 -0.017 0.935 0.005 0.967 0.006 -6.050 0.372 0.220 -13.5 -0.529 0.08714 -0.020 0.919 0.004 0.971 0.006 -6.066 0.367 0.212 -13.0 -0.500 0.08139 -0.023 0.887 0.004 0.976 0.006 -6.144 0.359 0.204 -12.5 -0.470 0.07565 -0.026 0.867 0.004 0.978 0.006 -6.213 0.354 0.194 -12.0 -0.438 0.07188 -0.030 0.844 0.005 0.981 0.006 -6.099 0.349 0.182 -11.5 -0.405 0.06697 -0.033 0.818 0.005 0.983 0.007 -6.048 0.347 0.169 -11.0 -0.371 0.06332 -0.036 0.799 0.005 0.984 0.007 -5.865 0.345 0.153 -10.5 -0.336 0.05939 -0.039 0.786 0.005 0.984 0.007 -5.658 0.340 0.133 -10.0 -0.299 0.05516 -0.043 0.774 0.005 0.984 0.007 -5.419 0.338 0.107 -9.5 -0.262 0.05232 -0.046 0.763 0.005 0.984 0.008 -5.000 0.338 0.074 -9.0 -0.224 0.04889 -0.049 0.753 0.005 0.984 0.008 -4.572 0.335 0.029 -8.5 -0.184 0.04607 -0.053 0.743 0.005 0.983 0.008 -3.992 0.333 -0.036 -8.0 -0.144 0.04336 -0.056 0.733 0.006 0.982 0.009 -3.318 0.115 -0.139 -7.5 -0.322 0.02186 -0.071 0.724 0.006 0.981 0.743 -14.739 0.109 0.029 -7.0 -0.283 0.02071 -0.076 0.716 0.007 0.980 0.769 -13.678 0.344 -0.017 -6.5 -0.239 0.01974 -0.079 0.704 0.008 0.980 0.790 -12.118 0.335 -0.081 -6.0 -0.195 0.01880 -0.083 0.690 0.009 0.979 0.814 -10.392 0.327 -0.175 -5.5 -0.147 0.01793 -0.086 0.677 0.065 0.979 0.833 -8.223 0.323 -0.335 -5.0 -0.101 0.01724 -0.090 0.663 0.073 0.979 0.861 -5.877 0.325 -0.637 -4.5 -0.053 0.01669 -0.093 0.650 0.081 0.978 0.890 -3.198 0.222 -1.498 -4.0 -0.015 0.01714 -0.087 0.638 0.469 0.977 0.684 -0.882 0.222 -5.538 -3.5 0.048 0.01673 -0.091 0.623 0.479 0.976 0.690 2.843 0.298 2.152 -3.0 0.110 0.01643 -0.093 0.610 0.489 0.975 0.695 6.691 0.297 1.100 -2.5 0.172 0.01624 -0.096 0.592 0.500 0.975 0.698 10.594 0.297 0.810 -2.0 0.234 0.01601 -0.099 0.574 0.507 0.974 0.706 14.591 0.299 0.675 -1.5 0.295 0.01563 -0.102 0.559 0.511 0.973 0.730 18.860 0.299 0.597 -1.0 0.356 0.01528 -0.105 0.547 0.515 0.971 0.759 23.272 0.296 0.546 -0.5 0.416 0.01512 -0.108 0.535 0.519 0.970 0.790 27.540 0.301 0.509 0.0 0.456 0.01490 -0.110 0.520 0.522 0.968 0.827 30.636 0.289 0.492 0.5 0.516 0.01515 -0.112 0.504 0.526 0.966 0.867 34.020 0.275 0.467 1.0 0.575 0.01545 -0.113 0.488 0.530 0.964 0.913 37.186 0.275 0.447 1.5 0.634 0.01583 -0.115 0.471 0.535 0.962 0.960 40.040 0.276 0.431 2.0 0.692 0.01617 -0.116 0.455 0.539 0.960 0.985 42.814 0.277 0.418 2.5 0.750 0.01682 -0.118 0.441 0.543 0.957 0.993 44.581 0.278 0.407 3.0 0.807 0.01741 -0.119 0.427 0.547 0.953 0.994 46.362 0.280 0.398 3.5 0.863 0.01807 -0.121 0.409 0.551 0.948 0.995 47.779 0.281 0.390 4.0 0.919 0.01879 -0.123 0.391 0.556 0.943 0.995 48.899 0.283 0.384 4.5 0.974 0.01958 -0.125 0.375 0.560 0.938 0.996 49.720 0.289 0.378 5.0 1.024 0.02042 -0.127 0.360 0.565 0.927 0.997 50.137 0.297 0.374 5.5 1.073 0.02122 -0.129 0.345 0.570 0.916 0.998 50.557 0.303 0.371 6.0 1.119 0.02224 -0.132 0.328 0.575 0.903 0.998 50.333 0.307 0.368 6.5 1.166 0.02330 -0.135 0.307 0.581 0.891 0.998 50.043 0.308 0.366 7.0 1.213 0.02456 -0.138 0.283 0.589 0.880 0.998 49.376 0.314 0.363 7.5 1.256 0.02579 -0.141 0.264 0.598 0.866 0.998 48.691 0.324 0.362 8.0 1.297 0.03082 -0.144 0.068 0.609 0.852 0.998 42.095 0.342 0.361 8.5 1.332 0.03326 -0.148 0.028 0.621 0.831 0.998 40.035 0.365 0.361 9.0 1.365 0.03517 -0.152 0.024 0.635 0.811 0.998 38.818 0.367 0.361 9.5 1.399 0.03706 -0.155 0.021 0.651 0.793 0.998 37.737 0.373 0.361 10.0 1.430 0.03928 -0.160 0.017 0.669 0.775 0.998 36.394 0.391 0.362 10.5 1.458 0.04166 -0.164 0.015 0.691 0.754 0.999 34.993 0.426 0.362 11.0 1.481 0.04436 -0.169 0.014 0.715 0.730 0.999 33.387 0.532 0.364 11.5 1.495 0.04762 -0.174 0.012 0.742 0.697 0.999 31.384 2.557 0.367 12.0 1.487 0.05249 -0.182 0.011 0.778 0.641 0.999 28.324 0.131 0.372 12.5 1.286 0.08245 -0.199 0.010 0.832 0.109 0.998 15.599 0.129 0.405 13.0 1.337 0.08399 -0.200 0.009 0.992 0.046 0.994 15.913 0.295 0.400 13.5 1.370 0.08787 -0.203 0.008 0.992 0.034 0.995 15.588 0.342 0.398 14.0 1.398 0.09201 -0.206 0.008 0.992 0.027 0.995 15.195 0.369 0.397 14.5 1.420 0.09646 -0.209 0.007 0.993 0.023 0.995 14.724 0.402 0.397 15.0 1.439 0.10182 -0.212 0.007 0.993 0.021 0.995 14.132 0.417 0.397