Name = AH 79-100 A 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 -0.390 0.24517 -0.046 0.948 0.003 0.984 0.004 -1.589 0.540 0.131 -14.5 -0.381 0.23402 -0.049 0.941 0.003 0.984 0.004 -1.628 0.511 0.122 -14.0 -0.370 0.20852 -0.051 0.934 0.003 0.983 0.003 -1.776 0.464 0.112 -13.5 -0.357 0.18418 -0.054 0.928 0.003 0.983 0.003 -1.940 0.428 0.100 -13.0 -0.342 0.17792 -0.056 0.922 0.002 0.982 0.003 -1.921 0.403 0.085 -12.5 -0.324 0.15689 -0.059 0.917 0.002 0.981 0.003 -2.066 0.386 0.069 -12.0 -0.304 0.13905 -0.061 0.907 0.002 0.980 0.003 -2.188 0.370 0.048 -11.5 -0.281 0.13020 -0.064 0.897 0.002 0.980 0.003 -2.162 0.358 0.023 -11.0 -0.257 0.11533 -0.067 0.887 0.002 0.979 0.003 -2.226 0.349 -0.009 -10.5 -0.230 0.10336 -0.069 0.877 0.002 0.978 0.003 -2.222 0.342 -0.051 -10.0 -0.201 0.09449 -0.072 0.852 0.003 0.981 0.003 -2.122 0.335 -0.107 -9.5 -0.169 0.08731 -0.074 0.840 0.003 0.979 0.004 -1.936 0.331 -0.189 -9.0 -0.137 0.07704 -0.077 0.829 0.003 0.977 0.004 -1.772 0.328 -0.313 -8.5 -0.102 0.07127 -0.079 0.818 0.003 0.975 0.004 -1.435 0.324 -0.527 -8.0 -0.066 0.06459 -0.082 0.807 0.004 0.973 0.005 -1.028 0.321 -0.986 -7.5 -0.029 0.05962 -0.085 0.799 0.004 0.969 0.006 -0.490 0.230 -2.647 -7.0 -0.322 0.05506 -0.087 0.792 0.005 0.965 0.008 -5.856 0.227 -0.021 -6.5 -0.259 0.05035 -0.090 0.785 0.006 0.960 0.009 -5.139 0.291 -0.097 -6.0 -0.195 0.04668 -0.092 0.778 0.007 0.954 0.010 -4.171 0.291 -0.225 -5.5 -0.131 0.04330 -0.095 0.768 0.009 0.950 0.012 -3.016 0.291 -0.478 -5.0 -0.067 0.04018 -0.098 0.760 0.010 0.942 0.014 -1.660 0.292 -1.215 -4.5 -0.003 0.03715 -0.100 0.751 0.012 0.933 0.015 -0.088 0.292 -30.459 -4.0 0.059 0.03467 -0.103 0.740 0.013 0.927 0.017 1.715 0.291 1.983 -3.5 0.121 0.03274 -0.106 0.730 0.015 0.921 0.032 3.706 0.413 1.120 -3.0 0.174 0.02717 -0.122 0.720 0.036 0.913 0.998 6.389 0.307 0.951 -2.5 0.237 0.02341 -0.112 0.707 0.291 0.905 0.562 10.126 0.198 0.723 -2.0 0.296 0.02238 -0.115 0.695 0.308 0.897 0.625 13.204 0.347 0.640 -1.5 0.351 0.02486 -0.123 0.682 0.340 0.890 0.997 14.109 0.323 0.601 -1.0 0.410 0.02602 -0.124 0.668 0.352 0.882 0.998 15.742 0.259 0.552 -0.5 0.469 0.02712 -0.124 0.650 0.365 0.878 0.998 17.278 0.267 0.515 0.0 0.470 0.02828 -0.125 0.626 0.384 0.879 0.999 16.611 0.282 0.516 0.5 0.524 0.02878 -0.126 0.605 0.407 0.875 0.999 18.207 0.270 0.490 1.0 0.589 0.02958 -0.127 0.558 0.419 0.892 0.999 19.898 0.264 0.466 1.5 0.655 0.03021 -0.128 0.497 0.432 0.912 0.999 21.697 0.270 0.445 2.0 0.703 0.03074 -0.129 0.483 0.470 0.896 0.999 22.881 0.282 0.434 2.5 0.750 0.03162 -0.131 0.470 0.488 0.879 1.000 23.731 0.279 0.424 3.0 0.805 0.03240 -0.132 0.437 0.529 0.876 1.000 24.835 0.282 0.414 3.5 0.850 0.03341 -0.134 0.417 0.549 0.859 1.000 25.439 0.284 0.408 4.0 0.904 0.03411 -0.136 0.379 0.602 0.857 1.000 26.499 0.285 0.400 4.5 0.948 0.03144 -0.138 0.352 0.999 0.843 0.999 30.163 0.283 0.395 5.0 1.003 0.03257 -0.139 0.300 0.999 0.846 0.999 30.799 0.275 0.388 5.5 1.054 0.03388 -0.140 0.249 0.999 0.846 0.999 31.122 0.239 0.383 6.0 1.151 0.03317 -0.137 0.008 0.999 0.913 0.999 34.703 0.004 0.369 6.5 0.975 0.04474 -0.160 0.004 0.999 0.008 0.999 21.786 0.070 0.414 7.0 1.011 0.04871 -0.163 0.003 0.999 0.005 0.999 20.759 0.327 0.411 7.5 1.043 0.05296 -0.165 0.003 0.999 0.004 0.999 19.697 0.337 0.408 8.0 1.072 0.05830 -0.168 0.003 0.999 0.004 1.000 18.392 0.346 0.407 8.5 1.099 0.06390 -0.170 0.003 0.999 0.003 1.000 17.200 0.354 0.405 9.0 1.124 0.07023 -0.173 0.002 0.999 0.003 1.000 15.998 0.365 0.404 9.5 1.145 0.07841 -0.176 0.002 0.999 0.003 1.000 14.609 0.379 0.403 10.0 1.165 0.08709 -0.178 0.002 0.999 0.003 1.000 13.374 0.398 0.403 10.5 1.181 0.09544 -0.181 0.002 1.000 0.003 1.000 12.378 0.424 0.403 11.0 1.195 0.10364 -0.184 0.002 1.000 0.003 1.000 11.533 0.493 0.404 11.5 1.203 0.11692 -0.186 0.002 1.000 0.003 1.000 10.290 0.766 0.405 12.0 1.206 0.13096 -0.189 0.002 1.000 0.003 1.000 9.205 4.377 0.407 12.5 1.204 0.13827 -0.192 0.002 1.000 0.002 1.000 8.711 -0.536 0.409 13.0 1.199 0.15279 -0.194 0.002 1.000 0.002 1.000 7.846 -0.103 0.412 13.5 1.190 0.16790 -0.197 0.002 1.000 0.002 1.000 7.085 0.017 0.416 14.0 1.176 0.18963 -0.200 0.002 1.000 0.002 1.000 6.204 0.075 0.420 14.5 1.160 0.21368 -0.202 0.001 1.000 0.002 1.000 5.427 0.107 0.424 15.0 1.140 0.22965 -0.205 0.001 1.000 0.002 1.000 4.965 0.118 0.430 Name = AH 79-100 A 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 -0.389 0.20057 -0.046 0.948 0.003 0.984 0.004 -1.941 0.547 0.131 -14.5 -0.381 0.18128 -0.049 0.941 0.003 0.985 0.004 -2.101 0.513 0.122 -14.0 -0.370 0.16426 -0.051 0.934 0.003 0.985 0.004 -2.253 0.464 0.112 -13.5 -0.357 0.14737 -0.054 0.928 0.003 0.985 0.003 -2.424 0.428 0.100 -13.0 -0.342 0.14065 -0.056 0.922 0.002 0.985 0.003 -2.429 0.403 0.085 -12.5 -0.324 0.12614 -0.059 0.917 0.002 0.984 0.003 -2.568 0.386 0.068 -12.0 -0.304 0.11351 -0.061 0.907 0.002 0.985 0.003 -2.678 0.371 0.048 -11.5 -0.281 0.10069 -0.064 0.897 0.002 0.985 0.003 -2.795 0.358 0.023 -11.0 -0.256 0.09486 -0.067 0.887 0.002 0.985 0.003 -2.704 0.349 -0.009 -10.5 -0.229 0.08487 -0.069 0.877 0.002 0.985 0.003 -2.702 0.342 -0.051 -10.0 -0.200 0.07792 -0.072 0.852 0.003 0.986 0.004 -2.570 0.336 -0.108 -9.5 -0.169 0.06995 -0.074 0.840 0.003 0.986 0.004 -2.417 0.330 -0.189 -9.0 -0.136 0.06557 -0.077 0.829 0.003 0.986 0.004 -2.074 0.327 -0.315 -8.5 -0.102 0.05969 -0.079 0.818 0.003 0.986 0.005 -1.707 0.324 -0.530 -8.0 -0.066 0.05488 -0.082 0.807 0.004 0.986 0.006 -1.199 0.321 -0.996 -7.5 -0.029 0.05050 -0.085 0.799 0.004 0.985 0.007 -0.567 0.230 -2.707 -7.0 -0.322 0.04675 -0.087 0.792 0.005 0.985 0.008 -6.898 0.227 -0.021 -6.5 -0.259 0.04324 -0.090 0.785 0.006 0.985 0.009 -5.984 0.291 -0.097 -6.0 -0.195 0.04006 -0.092 0.778 0.007 0.984 0.011 -4.860 0.291 -0.225 -5.5 -0.131 0.03700 -0.095 0.768 0.009 0.983 0.013 -3.529 0.291 -0.478 -5.0 -0.067 0.03436 -0.098 0.760 0.010 0.980 0.014 -1.941 0.292 -1.215 -4.5 -0.003 0.03181 -0.100 0.751 0.012 0.976 0.016 -0.103 0.292 -30.457 -4.0 0.059 0.02971 -0.103 0.740 0.013 0.973 0.022 2.002 0.426 1.982 -3.5 0.115 0.02273 -0.121 0.730 0.015 0.970 0.998 5.041 0.414 1.308 -3.0 0.174 0.02295 -0.122 0.720 0.036 0.967 0.998 7.565 0.259 0.951 -2.5 0.233 0.02091 -0.122 0.707 0.291 0.964 0.998 11.125 0.259 0.775 -2.0 0.292 0.02132 -0.123 0.695 0.308 0.961 0.998 13.685 0.259 0.671 -1.5 0.351 0.02135 -0.123 0.682 0.340 0.957 0.999 16.429 0.259 0.601 -1.0 0.410 0.02184 -0.124 0.668 0.352 0.954 0.999 18.757 0.259 0.552 -0.5 0.469 0.02218 -0.124 0.650 0.365 0.953 0.999 21.125 0.261 0.515 0.0 0.505 0.02262 -0.125 0.626 0.384 0.955 0.999 22.337 0.264 0.497 0.5 0.563 0.02295 -0.126 0.605 0.407 0.954 0.999 24.517 0.262 0.473 1.0 0.627 0.02337 -0.126 0.558 0.419 0.966 0.999 26.812 0.259 0.451 1.5 0.690 0.02394 -0.127 0.497 0.432 0.977 1.000 28.839 0.262 0.434 2.0 0.744 0.02418 -0.128 0.483 0.470 0.969 1.000 30.763 0.267 0.421 2.5 0.797 0.02475 -0.129 0.470 0.488 0.961 1.000 32.217 0.266 0.411 3.0 0.854 0.02520 -0.129 0.437 0.529 0.960 1.000 33.879 0.267 0.401 3.5 0.906 0.02584 -0.130 0.417 0.549 0.952 1.000 35.075 0.269 0.394 4.0 0.962 0.02581 -0.131 0.379 0.602 0.950 1.000 37.252 0.271 0.387 4.5 1.011 0.02272 -0.133 0.352 0.999 0.941 0.999 44.503 0.272 0.381 5.0 1.064 0.02379 -0.134 0.300 0.999 0.939 0.999 44.739 0.272 0.376 5.5 1.114 0.02501 -0.135 0.249 0.999 0.934 0.999 44.543 0.267 0.371 6.0 1.169 0.02746 -0.135 0.008 0.999 0.939 0.999 42.584 0.275 0.366 6.5 1.211 0.02834 -0.137 0.004 0.999 0.927 0.999 42.730 0.081 0.363 7.0 1.009 0.04235 -0.163 0.003 0.999 0.006 0.999 23.831 0.084 0.411 7.5 1.042 0.04582 -0.165 0.003 0.999 0.004 0.999 22.751 0.334 0.408 8.0 1.072 0.04963 -0.168 0.003 0.999 0.004 1.000 21.595 0.345 0.407 8.5 1.099 0.05437 -0.170 0.003 0.999 0.004 1.000 20.208 0.354 0.405 9.0 1.123 0.05958 -0.173 0.002 0.999 0.003 1.000 18.853 0.365 0.404 9.5 1.145 0.06608 -0.176 0.002 0.999 0.003 1.000 17.329 0.378 0.404 10.0 1.165 0.07080 -0.178 0.002 0.999 0.003 1.000 16.450 0.397 0.403 10.5 1.181 0.07959 -0.181 0.002 1.000 0.003 1.000 14.840 0.426 0.403 11.0 1.195 0.08604 -0.184 0.002 1.000 0.003 1.000 13.888 0.489 0.404 11.5 1.203 0.09286 -0.186 0.002 1.000 0.003 1.000 12.958 0.749 0.405 12.0 1.206 0.10226 -0.189 0.002 1.000 0.003 1.000 11.789 5.770 0.407 12.5 1.204 0.11458 -0.192 0.002 1.000 0.002 1.000 10.509 -0.502 0.409 13.0 1.199 0.12551 -0.194 0.002 1.000 0.002 1.000 9.550 -0.104 0.412 13.5 1.189 0.13818 -0.197 0.002 1.000 0.002 1.000 8.607 0.014 0.416 14.0 1.176 0.14549 -0.200 0.002 1.000 0.002 1.000 8.086 0.074 0.420 14.5 1.160 0.15994 -0.202 0.001 1.000 0.002 1.000 7.251 0.107 0.424 15.0 1.140 0.18374 -0.205 0.001 1.000 0.002 1.000 6.204 0.119 0.430 Name = AH 79-100 A 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 -0.389 0.17356 -0.046 0.948 0.003 0.985 0.004 -2.242 0.547 0.131 -14.5 -0.381 0.15877 -0.049 0.941 0.003 0.985 0.004 -2.397 0.513 0.122 -14.0 -0.370 0.14551 -0.051 0.934 0.003 0.985 0.004 -2.542 0.464 0.112 -13.5 -0.357 0.13192 -0.054 0.928 0.003 0.985 0.004 -2.706 0.430 0.099 -13.0 -0.342 0.11856 -0.056 0.922 0.002 0.985 0.003 -2.881 0.405 0.085 -12.5 -0.324 0.10777 -0.059 0.917 0.002 0.985 0.003 -3.006 0.386 0.068 -12.0 -0.304 0.09817 -0.061 0.907 0.002 0.986 0.003 -3.096 0.370 0.048 -11.5 -0.281 0.09145 -0.064 0.897 0.002 0.986 0.003 -3.075 0.358 0.023 -11.0 -0.256 0.08297 -0.067 0.887 0.002 0.987 0.003 -3.091 0.349 -0.009 -10.5 -0.229 0.07699 -0.069 0.877 0.002 0.987 0.004 -2.975 0.341 -0.052 -10.0 -0.200 0.07080 -0.072 0.852 0.003 0.988 0.004 -2.825 0.336 -0.108 -9.5 -0.169 0.06376 -0.074 0.840 0.003 0.989 0.004 -2.647 0.331 -0.190 -9.0 -0.136 0.05931 -0.077 0.829 0.003 0.989 0.004 -2.289 0.327 -0.316 -8.5 -0.102 0.05445 -0.079 0.818 0.003 0.989 0.005 -1.864 0.324 -0.532 -8.0 -0.065 0.05013 -0.082 0.807 0.004 0.989 0.006 -1.305 0.320 -1.004 -7.5 -0.028 0.04648 -0.085 0.799 0.004 0.989 0.007 -0.603 0.230 -2.769 -7.0 -0.322 0.04312 -0.087 0.792 0.005 0.988 0.009 -7.478 0.227 -0.021 -6.5 -0.259 0.03988 -0.090 0.785 0.006 0.988 0.010 -6.488 0.291 -0.097 -6.0 -0.195 0.03700 -0.092 0.778 0.007 0.987 0.012 -5.262 0.291 -0.225 -5.5 -0.131 0.03421 -0.095 0.768 0.009 0.987 0.013 -3.817 0.291 -0.478 -5.0 -0.067 0.03175 -0.098 0.760 0.010 0.987 0.015 -2.101 0.292 -1.215 -4.5 -0.003 0.02935 -0.100 0.751 0.012 0.986 0.016 -0.111 0.290 -30.455 -4.0 0.059 0.02773 -0.103 0.740 0.013 0.986 0.034 2.143 0.427 1.980 -3.5 0.115 0.02076 -0.121 0.730 0.015 0.986 0.998 5.520 0.416 1.308 -3.0 0.174 0.02106 -0.122 0.720 0.036 0.985 0.998 8.241 0.259 0.951 -2.5 0.233 0.01925 -0.122 0.707 0.291 0.985 0.999 12.086 0.259 0.775 -2.0 0.292 0.01944 -0.123 0.695 0.308 0.985 0.999 15.006 0.259 0.671 -1.5 0.351 0.01943 -0.123 0.682 0.340 0.984 0.999 18.056 0.259 0.601 -1.0 0.410 0.01973 -0.124 0.668 0.352 0.984 0.999 20.764 0.259 0.552 -0.5 0.469 0.02001 -0.124 0.650 0.365 0.984 0.999 23.418 0.259 0.515 0.0 0.519 0.02026 -0.125 0.626 0.384 0.984 0.999 25.641 0.260 0.490 0.5 0.578 0.02028 -0.125 0.605 0.407 0.984 1.000 28.488 0.260 0.467 1.0 0.637 0.02071 -0.126 0.558 0.419 0.986 1.000 30.773 0.260 0.448 1.5 0.697 0.02134 -0.126 0.497 0.432 0.988 1.000 32.656 0.260 0.432 2.0 0.754 0.02149 -0.127 0.483 0.470 0.987 1.000 35.104 0.261 0.418 2.5 0.811 0.02173 -0.128 0.470 0.488 0.985 1.000 37.347 0.261 0.407 3.0 0.869 0.02206 -0.128 0.437 0.529 0.985 1.000 39.405 0.261 0.398 3.5 0.926 0.02191 -0.129 0.417 0.549 0.983 1.000 42.257 0.263 0.389 4.0 0.981 0.02202 -0.130 0.379 0.602 0.980 1.000 44.552 0.268 0.382 4.5 1.032 0.01921 -0.131 0.352 0.999 0.972 0.999 53.706 0.269 0.377 5.0 1.084 0.02025 -0.132 0.300 0.999 0.969 0.999 53.546 0.270 0.372 5.5 1.134 0.02142 -0.133 0.249 0.999 0.963 0.999 52.948 0.278 0.367 6.0 1.179 0.02474 -0.134 0.008 0.999 0.953 0.999 47.647 0.288 0.364 6.5 1.221 0.02570 -0.136 0.004 0.999 0.940 0.999 47.494 0.087 0.362 7.0 1.007 0.03976 -0.163 0.003 0.999 0.008 0.999 25.319 0.089 0.412 7.5 1.041 0.04274 -0.165 0.003 0.999 0.005 0.999 24.362 0.332 0.409 8.0 1.071 0.04639 -0.168 0.003 0.999 0.004 1.000 23.088 0.343 0.407 8.5 1.098 0.05022 -0.170 0.003 0.999 0.004 1.000 21.866 0.353 0.405 9.0 1.123 0.05498 -0.173 0.002 0.999 0.003 1.000 20.423 0.364 0.404 9.5 1.145 0.05946 -0.176 0.002 0.999 0.003 1.000 19.256 0.378 0.404 10.0 1.164 0.06518 -0.178 0.002 0.999 0.003 1.000 17.864 0.397 0.403 10.5 1.181 0.07070 -0.181 0.002 1.000 0.003 1.000 16.704 0.426 0.403 11.0 1.195 0.07867 -0.184 0.002 1.000 0.003 1.000 15.184 0.493 0.404 11.5 1.203 0.08527 -0.186 0.002 1.000 0.003 1.000 14.106 0.748 0.405 12.0 1.205 0.09352 -0.189 0.002 1.000 0.003 1.000 12.887 4.309 0.407 12.5 1.204 0.10010 -0.192 0.002 1.000 0.002 1.000 12.030 -0.539 0.409 13.0 1.199 0.10860 -0.194 0.002 1.000 0.002 1.000 11.036 -0.104 0.412 13.5 1.189 0.11935 -0.197 0.002 1.000 0.002 1.000 9.965 0.016 0.416 14.0 1.176 0.13306 -0.200 0.002 1.000 0.002 1.000 8.839 0.075 0.420 14.5 1.159 0.14406 -0.202 0.001 1.000 0.002 1.000 8.048 0.107 0.424 15.0 1.140 0.15531 -0.205 0.001 1.000 0.002 1.000 7.339 0.118 0.430 Name = AH 79-100 A 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 -0.389 0.15770 -0.046 0.948 0.003 0.985 0.004 -2.466 0.554 0.131 -14.5 -0.381 0.13880 -0.049 0.941 0.003 0.986 0.004 -2.742 0.516 0.122 -14.0 -0.370 0.12835 -0.051 0.934 0.003 0.986 0.004 -2.882 0.464 0.112 -13.5 -0.357 0.11752 -0.054 0.928 0.003 0.986 0.004 -3.037 0.428 0.099 -13.0 -0.341 0.11039 -0.056 0.922 0.002 0.986 0.004 -3.093 0.403 0.085 -12.5 -0.324 0.10111 -0.059 0.917 0.002 0.986 0.003 -3.202 0.386 0.068 -12.0 -0.304 0.09275 -0.061 0.907 0.002 0.987 0.003 -3.275 0.370 0.048 -11.5 -0.281 0.08628 -0.064 0.897 0.002 0.987 0.003 -3.256 0.358 0.022 -11.0 -0.256 0.07846 -0.067 0.887 0.002 0.988 0.003 -3.265 0.349 -0.010 -10.5 -0.229 0.07241 -0.069 0.877 0.002 0.988 0.004 -3.160 0.341 -0.052 -10.0 -0.200 0.06664 -0.072 0.852 0.003 0.990 0.004 -2.997 0.336 -0.109 -9.5 -0.169 0.06024 -0.074 0.840 0.003 0.991 0.004 -2.797 0.330 -0.191 -9.0 -0.135 0.05609 -0.077 0.829 0.003 0.991 0.005 -2.414 0.327 -0.317 -8.5 -0.101 0.05197 -0.079 0.818 0.003 0.991 0.006 -1.943 0.323 -0.537 -8.0 -0.065 0.04783 -0.082 0.807 0.004 0.991 0.007 -1.356 0.320 -1.015 -7.5 -0.027 0.04425 -0.085 0.799 0.004 0.991 0.008 -0.620 0.230 -2.835 -7.0 -0.322 0.04112 -0.087 0.792 0.005 0.991 0.009 -7.842 0.227 -0.020 -6.5 -0.259 0.03803 -0.090 0.785 0.006 0.991 0.011 -6.803 0.291 -0.097 -6.0 -0.195 0.03521 -0.092 0.778 0.007 0.990 0.012 -5.529 0.291 -0.225 -5.5 -0.131 0.03260 -0.095 0.768 0.009 0.990 0.014 -4.005 0.291 -0.478 -5.0 -0.067 0.03022 -0.098 0.760 0.010 0.990 0.015 -2.207 0.292 -1.215 -4.5 -0.003 0.02796 -0.100 0.751 0.012 0.990 0.017 -0.117 0.438 -30.452 -4.0 0.056 0.01917 -0.121 0.740 0.013 0.989 0.998 2.904 0.427 2.417 -3.5 0.115 0.01954 -0.121 0.730 0.015 0.989 0.998 5.863 0.259 1.308 -3.0 0.174 0.01974 -0.122 0.720 0.036 0.989 0.999 8.795 0.259 0.951 -2.5 0.233 0.01790 -0.122 0.707 0.291 0.989 0.999 12.999 0.259 0.775 -2.0 0.292 0.01809 -0.123 0.695 0.308 0.989 0.999 16.123 0.259 0.671 -1.5 0.351 0.01808 -0.123 0.682 0.340 0.988 0.999 19.404 0.259 0.601 -1.0 0.410 0.01823 -0.124 0.668 0.352 0.988 0.999 22.475 0.259 0.552 -0.5 0.469 0.01840 -0.124 0.650 0.365 0.988 0.999 25.460 0.259 0.515 0.0 0.522 0.01861 -0.125 0.626 0.384 0.989 1.000 28.040 0.260 0.489 0.5 0.581 0.01886 -0.125 0.605 0.407 0.989 1.000 30.779 0.260 0.466 1.0 0.640 0.01953 -0.126 0.558 0.419 0.991 1.000 32.760 0.259 0.447 1.5 0.699 0.02036 -0.126 0.497 0.432 0.991 1.000 34.307 0.260 0.431 2.0 0.757 0.02009 -0.127 0.483 0.470 0.991 1.000 37.674 0.260 0.418 2.5 0.814 0.01946 -0.128 0.470 0.488 0.990 1.000 41.847 0.260 0.407 3.0 0.872 0.01974 -0.128 0.437 0.529 0.989 1.000 44.178 0.261 0.397 3.5 0.929 0.01970 -0.129 0.417 0.549 0.988 1.000 47.156 0.261 0.389 4.0 0.985 0.01983 -0.129 0.379 0.602 0.987 1.000 49.706 0.262 0.381 4.5 1.041 0.01715 -0.130 0.352 0.999 0.985 0.999 60.662 0.263 0.375 5.0 1.095 0.01816 -0.131 0.300 0.999 0.984 0.999 60.281 0.267 0.370 5.5 1.144 0.01932 -0.132 0.249 0.999 0.978 0.999 59.217 0.280 0.365 6.0 1.187 0.02296 -0.134 0.008 0.999 0.964 0.999 51.701 0.291 0.363 6.5 1.228 0.02398 -0.135 0.004 0.999 0.951 0.999 51.215 0.092 0.360 7.0 1.003 0.03844 -0.163 0.003 0.999 0.009 0.999 26.105 0.092 0.412 7.5 1.039 0.04109 -0.165 0.003 0.999 0.006 0.999 25.283 0.328 0.409 8.0 1.071 0.04405 -0.168 0.003 0.999 0.004 1.000 24.305 0.340 0.407 8.5 1.098 0.04779 -0.171 0.003 0.999 0.004 1.000 22.973 0.353 0.405 9.0 1.122 0.05229 -0.173 0.002 0.999 0.004 1.000 21.465 0.364 0.404 9.5 1.145 0.05658 -0.176 0.002 0.999 0.003 1.000 20.232 0.378 0.404 10.0 1.164 0.06201 -0.178 0.002 0.999 0.003 1.000 18.771 0.397 0.403 10.5 1.181 0.06714 -0.181 0.002 1.000 0.003 1.000 17.585 0.423 0.403 11.0 1.195 0.07221 -0.184 0.002 1.000 0.003 1.000 16.544 0.488 0.404 11.5 1.203 0.07835 -0.186 0.002 1.000 0.003 1.000 15.352 0.748 0.405 12.0 1.205 0.08526 -0.189 0.002 1.000 0.003 1.000 14.136 4.309 0.407 12.5 1.204 0.09157 -0.192 0.002 1.000 0.002 1.000 13.150 -0.505 0.409 13.0 1.198 0.10330 -0.194 0.002 1.000 0.003 1.000 11.600 -0.104 0.412 13.5 1.189 0.10828 -0.197 0.002 1.000 0.002 1.000 10.984 0.013 0.416 14.0 1.176 0.12001 -0.200 0.002 1.000 0.002 1.000 9.801 0.075 0.420 14.5 1.159 0.12853 -0.202 0.001 1.000 0.002 1.000 9.021 0.107 0.424 15.0 1.140 0.14600 -0.205 0.001 1.000 0.002 1.000 7.806 0.119 0.430