Name = AG27 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 -0.244 0.42780 -0.002 1.000 0.002 1.000 0.004 -0.569 0.016 0.241 -14.5 -0.252 0.40414 -0.004 1.000 0.002 1.000 0.004 -0.624 0.008 0.234 -14.0 -0.260 0.36361 -0.006 1.000 0.002 1.000 0.004 -0.716 -0.014 0.226 -13.5 -0.268 0.31895 -0.008 1.000 0.002 1.000 0.004 -0.839 -0.048 0.219 -13.0 -0.274 0.28525 -0.010 1.000 0.002 1.000 0.003 -0.961 -0.112 0.212 -12.5 -0.279 0.26833 -0.012 1.000 0.002 1.000 0.003 -1.041 -0.245 0.206 -12.0 -0.283 0.25855 -0.014 1.000 0.002 1.000 0.003 -1.093 -0.629 0.199 -11.5 -0.284 0.23637 -0.017 1.000 0.002 1.000 0.003 -1.201 -7.357 0.192 -11.0 -0.283 0.19160 -0.019 1.000 0.002 1.000 0.003 -1.478 1.174 0.184 -10.5 -0.279 0.18318 -0.021 1.000 0.002 1.000 0.003 -1.525 0.661 0.176 -10.0 -0.273 0.16250 -0.023 1.000 0.002 1.000 0.003 -1.679 0.513 0.166 -9.5 -0.263 0.14758 -0.025 1.000 0.002 1.000 0.003 -1.783 0.440 0.155 -9.0 -0.250 0.12946 -0.027 1.000 0.002 1.000 0.003 -1.933 0.396 0.141 -8.5 -0.234 0.11708 -0.029 1.000 0.002 1.000 0.003 -1.996 0.370 0.124 -8.0 -0.214 0.10652 -0.032 1.000 0.002 1.000 0.003 -2.009 0.350 0.103 -7.5 -0.190 0.09180 -0.034 1.000 0.002 1.000 0.003 -2.072 0.337 0.073 -7.0 -0.164 0.08346 -0.036 1.000 0.002 1.000 0.003 -1.965 0.330 0.031 -6.5 -0.135 0.08236 -0.038 1.000 0.002 1.000 0.003 -1.642 0.324 -0.032 -6.0 -0.104 0.07289 -0.040 1.000 0.002 1.000 0.003 -1.431 0.319 -0.136 -5.5 -0.071 0.05656 -0.043 1.000 0.002 1.000 0.003 -1.262 0.316 -0.346 -5.0 -0.037 0.05144 -0.045 0.979 0.002 1.000 0.003 -0.722 0.314 -0.955 -4.5 -0.002 0.04544 -0.047 0.959 0.002 1.000 0.003 -0.043 0.208 -24.024 -4.0 -0.145 0.04019 -0.049 0.935 0.002 1.000 0.003 -3.598 0.196 -0.090 -3.5 -0.084 0.03630 -0.051 0.884 0.002 1.000 0.003 -2.325 0.287 -0.360 -3.0 -0.024 0.03271 -0.054 0.849 0.003 1.000 0.003 -0.737 0.287 -1.978 -2.5 0.036 0.02941 -0.056 0.821 0.003 1.000 0.004 1.220 0.288 1.809 -2.0 0.095 0.02698 -0.058 0.792 0.004 1.000 0.006 3.531 0.347 0.861 -1.5 0.150 0.03738 -0.067 0.759 0.189 1.000 0.996 4.012 0.329 0.697 -1.0 0.208 0.03529 -0.067 0.722 0.452 1.000 0.996 5.890 0.252 0.573 -0.5 0.266 0.02790 -0.067 0.681 0.995 1.000 0.995 9.522 0.252 0.503 0.0 0.323 0.02832 -0.067 0.638 0.995 1.000 0.995 11.417 0.252 0.458 0.5 0.381 0.02844 -0.068 0.597 0.995 1.000 0.995 13.398 0.252 0.427 1.0 0.439 0.02886 -0.068 0.554 0.995 1.000 0.995 15.200 0.252 0.404 1.5 0.496 0.02942 -0.068 0.510 0.995 1.000 0.995 16.866 0.252 0.387 2.0 0.554 0.03022 -0.068 0.464 0.995 1.000 0.995 18.322 0.252 0.373 2.5 0.611 0.03048 -0.068 0.410 0.995 1.000 0.995 20.043 0.253 0.361 3.0 0.668 0.03133 -0.068 0.345 0.995 1.000 0.995 21.324 0.253 0.352 3.5 0.725 0.03249 -0.068 0.272 0.995 1.000 0.995 22.314 0.253 0.344 4.0 0.782 0.03362 -0.069 0.161 0.995 1.000 0.995 23.254 0.253 0.338 4.5 0.838 0.03390 -0.069 0.087 0.995 1.000 0.995 24.716 0.253 0.332 5.0 0.893 0.03307 -0.069 0.060 0.995 1.000 0.995 27.010 0.726 0.327 5.5 0.862 0.03188 -0.080 0.041 0.996 0.828 0.996 27.033 0.112 0.343 6.0 0.689 0.05095 -0.097 0.027 0.996 0.072 0.996 13.532 0.090 0.391 6.5 0.748 0.05022 -0.098 0.005 0.995 0.019 0.995 14.892 0.279 0.381 7.0 0.801 0.05117 -0.100 0.001 0.995 0.002 0.995 15.652 0.303 0.375 7.5 0.829 0.05790 -0.103 0.001 0.995 0.001 0.995 14.309 0.345 0.374 8.0 0.851 0.06317 -0.105 0.001 0.995 0.001 0.995 13.464 0.370 0.373 8.5 0.868 0.07274 -0.107 0.001 0.995 0.001 0.995 11.932 0.402 0.374 9.0 0.882 0.08259 -0.110 0.000 0.995 0.001 0.995 10.676 0.481 0.374 9.5 0.889 0.09275 -0.112 0.001 0.996 0.001 0.996 9.581 0.748 0.376 10.0 0.891 0.10460 -0.114 0.001 0.996 0.001 0.996 8.521 11.361 0.378 10.5 0.889 0.11942 -0.117 0.001 0.996 0.001 0.996 7.444 -0.255 0.381 11.0 0.882 0.13801 -0.119 0.001 0.996 0.001 0.996 6.390 -0.006 0.385 11.5 0.870 0.14688 -0.122 0.001 0.996 0.001 0.996 5.925 0.073 0.390 12.0 0.855 0.17035 -0.124 0.000 0.996 0.001 0.996 5.018 0.115 0.395 12.5 0.835 0.18759 -0.126 0.001 0.996 0.001 0.996 4.451 0.141 0.401 13.0 0.811 0.21816 -0.129 0.001 0.996 0.001 0.996 3.717 0.154 0.409 13.5 0.785 0.24168 -0.131 0.001 0.996 0.001 0.996 3.249 0.162 0.417 14.0 0.756 0.25855 -0.134 0.001 0.996 0.001 0.996 2.926 0.168 0.427 14.5 0.727 0.28193 -0.136 0.001 0.996 0.001 0.996 2.577 0.174 0.437 15.0 0.693 0.28651 -0.138 0.001 0.995 0.001 0.995 2.420 0.178 0.450 Name = AG27 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 -0.243 0.31656 -0.002 1.000 0.002 1.000 0.004 -0.769 0.016 0.241 -14.5 -0.252 0.30138 -0.004 1.000 0.002 1.000 0.004 -0.836 0.008 0.234 -14.0 -0.260 0.26797 -0.006 1.000 0.002 1.000 0.004 -0.971 -0.014 0.226 -13.5 -0.268 0.24004 -0.008 1.000 0.002 1.000 0.004 -1.115 -0.049 0.219 -13.0 -0.274 0.21877 -0.010 1.000 0.002 1.000 0.004 -1.253 -0.115 0.212 -12.5 -0.279 0.22149 -0.012 1.000 0.002 1.000 0.004 -1.260 -0.246 0.206 -12.0 -0.282 0.19814 -0.014 1.000 0.002 1.000 0.004 -1.426 -0.618 0.199 -11.5 -0.284 0.18253 -0.017 1.000 0.002 1.000 0.004 -1.555 -7.674 0.192 -11.0 -0.283 0.15242 -0.019 1.000 0.002 1.000 0.003 -1.857 1.202 0.184 -10.5 -0.279 0.13417 -0.021 1.000 0.002 1.000 0.003 -2.082 0.667 0.176 -10.0 -0.273 0.12016 -0.023 1.000 0.002 1.000 0.003 -2.271 0.513 0.166 -9.5 -0.263 0.11081 -0.025 1.000 0.002 1.000 0.003 -2.375 0.440 0.155 -9.0 -0.250 0.09827 -0.027 1.000 0.002 1.000 0.003 -2.546 0.396 0.141 -8.5 -0.234 0.08936 -0.029 1.000 0.002 1.000 0.003 -2.615 0.370 0.124 -8.0 -0.214 0.08038 -0.032 1.000 0.002 1.000 0.003 -2.662 0.349 0.103 -7.5 -0.190 0.07270 -0.034 1.000 0.002 1.000 0.003 -2.614 0.337 0.073 -7.0 -0.164 0.06547 -0.036 1.000 0.002 1.000 0.003 -2.505 0.330 0.031 -6.5 -0.135 0.05960 -0.038 1.000 0.002 1.000 0.003 -2.267 0.324 -0.032 -6.0 -0.104 0.05736 -0.040 1.000 0.002 1.000 0.003 -1.818 0.319 -0.136 -5.5 -0.071 0.04703 -0.043 1.000 0.002 1.000 0.003 -1.514 0.316 -0.347 -5.0 -0.037 0.04185 -0.045 0.979 0.002 1.000 0.003 -0.887 0.314 -0.955 -4.5 -0.002 0.03738 -0.047 0.959 0.002 1.000 0.003 -0.047 0.208 -26.212 -4.0 -0.145 0.03313 -0.049 0.935 0.002 1.000 0.003 -4.365 0.196 -0.090 -3.5 -0.084 0.03025 -0.051 0.884 0.002 1.000 0.003 -2.789 0.287 -0.360 -3.0 -0.024 0.02750 -0.054 0.849 0.003 1.000 0.003 -0.876 0.287 -1.978 -2.5 0.036 0.02503 -0.056 0.821 0.003 1.000 0.004 1.434 0.288 1.809 -2.0 0.095 0.02319 -0.058 0.792 0.004 1.000 0.007 4.108 0.347 0.861 -1.5 0.150 0.03253 -0.067 0.759 0.189 1.000 0.997 4.610 0.329 0.697 -1.0 0.208 0.02999 -0.067 0.722 0.452 1.000 0.996 6.930 0.252 0.573 -0.5 0.266 0.02199 -0.067 0.681 0.995 1.000 0.995 12.081 0.252 0.503 0.0 0.323 0.02279 -0.067 0.638 0.995 1.000 0.995 14.192 0.252 0.458 0.5 0.381 0.02332 -0.068 0.597 0.995 1.000 0.995 16.341 0.252 0.427 1.0 0.439 0.02387 -0.068 0.554 0.995 1.000 0.995 18.373 0.252 0.404 1.5 0.496 0.02448 -0.068 0.510 0.995 1.000 0.995 20.266 0.252 0.387 2.0 0.554 0.02530 -0.068 0.464 0.995 1.000 0.995 21.882 0.252 0.373 2.5 0.611 0.02595 -0.068 0.410 0.995 1.000 0.995 23.543 0.253 0.361 3.0 0.668 0.02718 -0.068 0.345 0.995 1.000 0.995 24.583 0.253 0.352 3.5 0.725 0.02819 -0.068 0.272 0.995 1.000 0.995 25.723 0.253 0.344 4.0 0.782 0.02962 -0.069 0.161 0.995 1.000 0.995 26.392 0.253 0.338 4.5 0.838 0.03020 -0.069 0.087 0.995 1.000 0.995 27.747 0.253 0.332 5.0 0.893 0.03022 -0.069 0.060 0.995 1.000 0.995 29.556 0.253 0.327 5.5 0.947 0.03004 -0.069 0.041 0.996 1.000 0.996 31.508 0.254 0.323 6.0 0.998 0.02896 -0.069 0.027 0.996 1.000 0.996 34.466 0.277 0.319 6.5 1.034 0.02754 -0.071 0.005 0.995 0.976 0.995 37.534 0.094 0.319 7.0 0.799 0.04418 -0.100 0.001 0.995 0.003 0.995 18.095 0.099 0.375 7.5 0.828 0.04906 -0.103 0.001 0.995 0.002 0.995 16.877 0.343 0.374 8.0 0.850 0.05471 -0.105 0.001 0.995 0.001 0.995 15.536 0.369 0.373 8.5 0.868 0.05965 -0.107 0.001 0.995 0.001 0.995 14.550 0.401 0.374 9.0 0.881 0.06917 -0.110 0.000 0.995 0.001 0.995 12.743 0.481 0.374 9.5 0.889 0.07447 -0.112 0.001 0.996 0.001 0.996 11.932 0.747 0.376 10.0 0.891 0.08590 -0.114 0.001 0.996 0.001 0.996 10.373 11.361 0.378 10.5 0.889 0.09295 -0.117 0.001 0.996 0.001 0.996 9.564 -0.270 0.381 11.0 0.882 0.10610 -0.119 0.001 0.996 0.001 0.996 8.311 -0.000 0.385 11.5 0.870 0.12102 -0.122 0.001 0.996 0.001 0.996 7.188 0.074 0.390 12.0 0.855 0.13382 -0.124 0.000 0.996 0.001 0.996 6.387 0.115 0.395 12.5 0.835 0.15331 -0.126 0.001 0.996 0.001 0.996 5.443 0.140 0.401 13.0 0.811 0.16142 -0.129 0.001 0.996 0.001 0.996 5.023 0.153 0.409 13.5 0.785 0.19253 -0.131 0.001 0.996 0.001 0.996 4.076 0.162 0.417 14.0 0.756 0.20532 -0.134 0.001 0.996 0.001 0.996 3.683 0.168 0.427 14.5 0.726 0.22194 -0.136 0.001 0.996 0.001 0.996 3.272 0.174 0.437 15.0 0.693 0.20669 -0.138 0.001 0.995 0.001 0.995 3.354 0.177 0.450 Name = AG27 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 -0.243 0.26797 -0.002 1.000 0.002 1.000 0.004 -0.908 0.016 0.242 -14.5 -0.252 0.23954 -0.004 1.000 0.002 1.000 0.004 -1.052 0.007 0.234 -14.0 -0.260 0.22668 -0.006 1.000 0.002 1.000 0.004 -1.148 -0.014 0.226 -13.5 -0.268 0.20597 -0.008 1.000 0.002 1.000 0.004 -1.299 -0.049 0.219 -13.0 -0.274 0.19028 -0.010 1.000 0.002 1.000 0.004 -1.440 -0.114 0.213 -12.5 -0.279 0.17664 -0.012 1.000 0.002 1.000 0.004 -1.580 -0.248 0.206 -12.0 -0.282 0.17261 -0.014 1.000 0.002 1.000 0.004 -1.636 -0.618 0.199 -11.5 -0.284 0.14837 -0.017 1.000 0.002 1.000 0.004 -1.913 -8.019 0.192 -11.0 -0.283 0.13649 -0.019 1.000 0.002 1.000 0.004 -2.072 1.169 0.184 -10.5 -0.279 0.12047 -0.021 1.000 0.002 1.000 0.004 -2.318 0.666 0.176 -10.0 -0.273 0.10835 -0.023 1.000 0.002 1.000 0.004 -2.517 0.512 0.166 -9.5 -0.263 0.10163 -0.025 1.000 0.002 1.000 0.003 -2.587 0.440 0.155 -9.0 -0.250 0.08994 -0.027 1.000 0.002 1.000 0.003 -2.780 0.396 0.141 -8.5 -0.234 0.08226 -0.029 1.000 0.002 1.000 0.003 -2.839 0.369 0.124 -8.0 -0.214 0.07468 -0.032 1.000 0.002 1.000 0.003 -2.862 0.350 0.103 -7.5 -0.190 0.06345 -0.034 1.000 0.002 1.000 0.003 -2.996 0.338 0.073 -7.0 -0.164 0.05842 -0.036 1.000 0.002 1.000 0.003 -2.804 0.330 0.031 -6.5 -0.135 0.05254 -0.038 1.000 0.002 1.000 0.003 -2.571 0.324 -0.032 -6.0 -0.104 0.05054 -0.040 1.000 0.002 1.000 0.003 -2.064 0.319 -0.136 -5.5 -0.071 0.04188 -0.043 1.000 0.002 1.000 0.003 -1.701 0.316 -0.347 -5.0 -0.037 0.03747 -0.045 0.979 0.002 1.000 0.003 -0.991 0.314 -0.955 -4.5 -0.002 0.03376 -0.047 0.959 0.002 1.000 0.003 -0.053 0.208 -26.212 -4.0 -0.145 0.03008 -0.049 0.935 0.002 1.000 0.003 -4.807 0.196 -0.090 -3.5 -0.084 0.02790 -0.051 0.884 0.002 1.000 0.003 -3.024 0.287 -0.360 -3.0 -0.024 0.02547 -0.054 0.849 0.003 1.000 0.004 -0.946 0.287 -1.978 -2.5 0.036 0.02320 -0.056 0.821 0.003 1.000 0.005 1.547 0.288 1.809 -2.0 0.095 0.02135 -0.058 0.792 0.004 1.000 0.007 4.463 0.347 0.861 -1.5 0.150 0.03079 -0.067 0.759 0.189 1.000 0.997 4.871 0.329 0.697 -1.0 0.208 0.02778 -0.067 0.722 0.452 1.000 0.997 7.482 0.252 0.573 -0.5 0.266 0.01947 -0.067 0.681 0.995 1.000 0.995 13.647 0.252 0.503 0.0 0.323 0.02026 -0.067 0.638 0.995 1.000 0.995 15.960 0.252 0.458 0.5 0.381 0.02098 -0.068 0.597 0.995 1.000 0.995 18.163 0.252 0.427 1.0 0.439 0.02174 -0.068 0.554 0.995 1.000 0.995 20.181 0.252 0.404 1.5 0.496 0.02227 -0.068 0.510 0.995 1.000 0.995 22.284 0.252 0.387 2.0 0.554 0.02313 -0.068 0.464 0.995 1.000 0.995 23.933 0.252 0.373 2.5 0.611 0.02401 -0.068 0.410 0.995 1.000 0.995 25.443 0.253 0.361 3.0 0.668 0.02486 -0.068 0.345 0.995 1.000 0.995 26.871 0.253 0.352 3.5 0.725 0.02602 -0.068 0.272 0.995 1.000 0.995 27.869 0.253 0.344 4.0 0.782 0.02735 -0.069 0.161 0.995 1.000 0.995 28.586 0.253 0.338 4.5 0.838 0.02827 -0.069 0.087 0.995 1.000 0.995 29.640 0.253 0.332 5.0 0.893 0.02836 -0.069 0.060 0.995 1.000 0.995 31.499 0.253 0.327 5.5 0.947 0.02852 -0.069 0.041 0.996 1.000 0.996 33.194 0.254 0.323 6.0 0.998 0.02811 -0.069 0.027 0.996 1.000 0.996 35.511 0.254 0.319 6.5 1.046 0.02788 -0.069 0.005 0.995 1.000 0.995 37.534 0.096 0.316 7.0 0.797 0.04121 -0.100 0.001 0.995 0.004 0.995 19.336 0.099 0.376 7.5 0.827 0.04517 -0.103 0.001 0.995 0.002 0.995 18.321 0.338 0.374 8.0 0.850 0.04963 -0.105 0.001 0.995 0.001 0.995 17.124 0.368 0.373 8.5 0.868 0.05493 -0.107 0.001 0.995 0.001 0.995 15.797 0.401 0.374 9.0 0.881 0.06181 -0.110 0.000 0.995 0.001 0.995 14.261 0.481 0.374 9.5 0.888 0.06813 -0.112 0.001 0.996 0.001 0.996 13.038 0.747 0.376 10.0 0.891 0.07555 -0.114 0.001 0.996 0.001 0.996 11.795 10.890 0.378 10.5 0.889 0.08364 -0.117 0.001 0.996 0.001 0.996 10.626 -0.270 0.381 11.0 0.882 0.09224 -0.119 0.001 0.996 0.001 0.996 9.560 -0.003 0.385 11.5 0.870 0.10342 -0.122 0.001 0.996 0.001 0.996 8.411 0.076 0.390 12.0 0.854 0.11806 -0.124 0.000 0.996 0.001 0.996 7.237 0.115 0.395 12.5 0.835 0.13007 -0.126 0.001 0.996 0.001 0.996 6.416 0.140 0.401 13.0 0.811 0.14695 -0.129 0.001 0.996 0.001 0.996 5.515 0.153 0.409 13.5 0.785 0.15992 -0.131 0.001 0.996 0.001 0.996 4.907 0.162 0.417 14.0 0.756 0.17018 -0.134 0.001 0.996 0.001 0.996 4.444 0.168 0.427 14.5 0.726 0.16954 -0.136 0.001 0.996 0.002 0.996 4.282 0.174 0.437 15.0 0.693 0.18340 -0.138 0.001 0.995 0.002 0.995 3.779 0.177 0.450 Name = AG27 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 -0.243 0.23876 -0.002 1.000 0.002 1.000 0.004 -1.019 0.015 0.242 -14.5 -0.252 0.21607 -0.004 1.000 0.002 1.000 0.004 -1.166 0.007 0.234 -14.0 -0.260 0.20214 -0.006 1.000 0.002 1.000 0.005 -1.287 -0.015 0.227 -13.5 -0.267 0.18576 -0.008 1.000 0.002 1.000 0.004 -1.440 -0.050 0.219 -13.0 -0.274 0.17356 -0.010 1.000 0.002 1.000 0.004 -1.578 -0.114 0.213 -12.5 -0.279 0.16037 -0.012 1.000 0.002 1.000 0.004 -1.739 -0.244 0.206 -12.0 -0.282 0.14741 -0.014 1.000 0.002 1.000 0.004 -1.915 -0.623 0.199 -11.5 -0.284 0.13684 -0.017 1.000 0.002 1.000 0.004 -2.073 -8.019 0.192 -11.0 -0.283 0.11935 -0.019 1.000 0.002 1.000 0.004 -2.370 1.197 0.184 -10.5 -0.279 0.10613 -0.021 1.000 0.002 1.000 0.004 -2.631 0.659 0.176 -10.0 -0.273 0.10212 -0.023 1.000 0.002 1.000 0.004 -2.669 0.512 0.166 -9.5 -0.263 0.09044 -0.025 1.000 0.002 1.000 0.003 -2.908 0.441 0.155 -9.0 -0.250 0.08058 -0.027 1.000 0.002 1.000 0.003 -3.102 0.396 0.141 -8.5 -0.234 0.07388 -0.029 1.000 0.002 1.000 0.003 -3.161 0.369 0.124 -8.0 -0.214 0.06744 -0.032 1.000 0.002 1.000 0.003 -3.169 0.349 0.103 -7.5 -0.190 0.06133 -0.034 1.000 0.002 1.000 0.003 -3.095 0.338 0.073 -7.0 -0.164 0.05358 -0.036 1.000 0.002 1.000 0.003 -3.058 0.330 0.031 -6.5 -0.135 0.04838 -0.038 1.000 0.002 1.000 0.003 -2.793 0.324 -0.032 -6.0 -0.104 0.04434 -0.040 1.000 0.002 1.000 0.003 -2.349 0.319 -0.137 -5.5 -0.071 0.03883 -0.043 1.000 0.002 1.000 0.003 -1.834 0.316 -0.347 -5.0 -0.037 0.03488 -0.045 0.979 0.002 1.000 0.003 -1.064 0.314 -0.955 -4.5 -0.002 0.03146 -0.047 0.959 0.002 1.000 0.003 -0.056 0.208 -26.212 -4.0 -0.145 0.02853 -0.049 0.935 0.002 1.000 0.003 -5.068 0.196 -0.090 -3.5 -0.084 0.02621 -0.051 0.884 0.002 1.000 0.003 -3.219 0.287 -0.360 -3.0 -0.024 0.02395 -0.054 0.849 0.003 1.000 0.004 -1.006 0.287 -1.978 -2.5 0.036 0.02189 -0.056 0.821 0.003 1.000 0.005 1.640 0.288 1.809 -2.0 0.095 0.02042 -0.058 0.792 0.004 1.000 0.008 4.666 0.347 0.861 -1.5 0.150 0.02951 -0.067 0.759 0.189 1.000 0.997 5.081 0.329 0.697 -1.0 0.208 0.02628 -0.067 0.722 0.452 1.000 0.997 7.908 0.252 0.573 -0.5 0.266 0.01801 -0.067 0.681 0.995 1.000 0.995 14.753 0.252 0.503 0.0 0.323 0.01882 -0.067 0.638 0.995 1.000 0.995 17.181 0.252 0.458 0.5 0.381 0.01942 -0.068 0.597 0.995 1.000 0.995 19.616 0.252 0.427 1.0 0.439 0.02003 -0.068 0.554 0.995 1.000 0.995 21.900 0.252 0.404 1.5 0.496 0.02061 -0.068 0.510 0.995 1.000 0.995 24.079 0.252 0.387 2.0 0.554 0.02149 -0.068 0.464 0.995 1.000 0.995 25.759 0.252 0.373 2.5 0.611 0.02248 -0.068 0.410 0.995 1.000 0.995 27.177 0.253 0.361 3.0 0.668 0.02335 -0.068 0.345 0.995 1.000 0.995 28.611 0.253 0.352 3.5 0.725 0.02459 -0.068 0.272 0.995 1.000 0.995 29.487 0.253 0.344 4.0 0.782 0.02611 -0.069 0.161 0.995 1.000 0.995 29.941 0.253 0.338 4.5 0.838 0.02677 -0.069 0.087 0.995 1.000 0.995 31.297 0.253 0.332 5.0 0.893 0.02691 -0.069 0.060 0.995 1.000 0.995 33.197 0.253 0.327 5.5 0.947 0.02703 -0.069 0.041 0.996 1.000 0.996 35.023 0.254 0.323 6.0 0.998 0.02748 -0.069 0.027 0.996 1.000 0.996 36.324 0.254 0.319 6.5 1.046 0.02699 -0.069 0.005 0.995 1.000 0.995 38.767 0.112 0.316 7.0 0.768 0.04289 -0.101 0.001 0.995 0.028 0.995 17.915 0.099 0.381 7.5 0.827 0.04283 -0.103 0.001 0.995 0.002 0.995 19.306 0.299 0.374 8.0 0.850 0.04664 -0.105 0.001 0.995 0.001 0.995 18.223 0.367 0.373 8.5 0.867 0.05221 -0.107 0.001 0.995 0.001 0.995 16.613 0.402 0.374 9.0 0.881 0.05813 -0.110 0.000 0.995 0.001 0.995 15.157 0.478 0.374 9.5 0.888 0.06301 -0.112 0.001 0.996 0.001 0.996 14.098 0.746 0.376 10.0 0.891 0.07134 -0.114 0.001 0.996 0.001 0.996 12.487 23.267 0.378 10.5 0.889 0.07825 -0.117 0.001 0.996 0.001 0.996 11.355 -0.260 0.381 11.0 0.881 0.08860 -0.119 0.001 0.996 0.001 0.996 9.948 -0.002 0.385 11.5 0.869 0.09192 -0.122 0.001 0.996 0.001 0.996 9.459 0.074 0.390 12.0 0.854 0.10882 -0.124 0.000 0.996 0.001 0.996 7.849 0.115 0.395 12.5 0.834 0.12386 -0.126 0.001 0.996 0.001 0.996 6.734 0.140 0.402 13.0 0.811 0.12977 -0.129 0.001 0.996 0.001 0.996 6.246 0.153 0.409 13.5 0.784 0.13171 -0.131 0.001 0.996 0.001 0.996 5.956 0.162 0.417 14.0 0.756 0.13991 -0.134 0.001 0.996 0.002 0.996 5.403 0.168 0.427 14.5 0.726 0.14844 -0.136 0.001 0.996 0.002 0.996 4.891 0.174 0.437 15.0 0.693 0.17016 -0.138 0.001 0.995 0.002 0.995 4.071 0.177 0.450