Name = AG36 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 -0.462 0.27639 0.018 1.000 0.002 1.000 0.003 -1.671 -13.357 0.289 -14.5 -0.462 0.25820 0.016 1.000 0.002 1.000 0.003 -1.790 1.986 0.285 -14.0 -0.460 0.23091 0.014 1.000 0.002 1.000 0.003 -1.991 0.777 0.281 -13.5 -0.455 0.21299 0.012 1.000 0.002 1.000 0.003 -2.136 0.548 0.277 -13.0 -0.447 0.19979 0.011 1.000 0.002 1.000 0.003 -2.238 0.463 0.274 -12.5 -0.437 0.17481 0.009 1.000 0.002 1.000 0.003 -2.500 0.416 0.270 -12.0 -0.424 0.15998 0.007 1.000 0.002 1.000 0.003 -2.647 0.383 0.266 -11.5 -0.407 0.13820 0.005 1.000 0.002 1.000 0.003 -2.946 0.362 0.261 -11.0 -0.387 0.12585 0.003 1.000 0.003 1.000 0.003 -3.079 0.348 0.257 -10.5 -0.365 0.11250 0.000 1.000 0.003 1.000 0.003 -3.247 0.338 0.251 -10.0 -0.340 0.10362 -0.002 1.000 0.003 1.000 0.004 -3.284 0.331 0.245 -9.5 -0.313 0.09220 -0.004 1.000 0.003 1.000 0.004 -3.396 0.326 0.238 -9.0 -0.284 0.08206 -0.006 0.946 0.003 1.000 0.004 -3.460 0.322 0.229 -8.5 -0.253 0.07495 -0.008 0.935 0.003 1.000 0.004 -3.373 0.319 0.218 -8.0 -0.220 0.06883 -0.010 0.931 0.004 1.000 0.005 -3.194 0.317 0.203 -7.5 -0.186 0.06096 -0.013 0.923 0.004 1.000 0.005 -3.045 0.316 0.182 -7.0 -0.150 0.05562 -0.015 0.914 0.004 1.000 0.005 -2.705 0.314 0.151 -6.5 -0.114 0.04948 -0.017 0.908 0.004 1.000 0.005 -2.300 0.313 0.099 -6.0 -0.076 0.04479 -0.020 0.905 0.005 1.000 0.006 -1.707 0.312 -0.005 -5.5 -0.038 0.04345 -0.022 0.743 0.005 1.000 0.007 -0.876 0.205 -0.325 -5.0 -0.182 0.04007 -0.024 0.724 0.006 1.000 0.008 -4.539 0.190 0.117 -4.5 -0.118 0.03712 -0.027 0.713 0.007 1.000 0.009 -3.181 0.288 0.024 -4.0 -0.055 0.03446 -0.029 0.706 0.009 1.000 0.013 -1.589 0.289 -0.282 -3.5 0.008 0.03630 -0.032 0.481 0.012 1.000 0.018 0.214 0.400 4.313 -3.0 0.066 0.03385 -0.047 0.472 0.881 1.000 0.995 1.952 0.388 0.965 -2.5 0.125 0.03345 -0.048 0.469 0.914 1.000 0.996 3.734 0.257 0.632 -2.0 0.184 0.03287 -0.048 0.467 0.938 1.000 0.996 5.589 0.258 0.512 -1.5 0.242 0.03236 -0.049 0.465 0.959 1.000 0.996 7.494 0.258 0.450 -1.0 0.301 0.03161 -0.049 0.463 0.995 1.000 0.995 9.529 0.259 0.413 -0.5 0.360 0.03115 -0.050 0.461 0.995 1.000 0.995 11.552 0.259 0.388 0.0 0.418 0.03108 -0.050 0.437 0.995 1.000 0.996 13.466 0.259 0.370 0.5 0.477 0.03098 -0.051 0.421 0.995 1.000 0.995 15.398 0.264 0.356 1.0 0.524 0.03006 -0.052 0.402 0.995 0.973 0.995 17.443 0.272 0.348 1.5 0.573 0.02955 -0.053 0.380 0.995 0.952 0.995 19.380 0.275 0.342 2.0 0.623 0.02961 -0.054 0.350 0.995 0.936 0.995 21.041 0.268 0.337 2.5 0.685 0.03067 -0.055 0.284 0.995 0.947 0.995 22.324 0.271 0.330 3.0 0.733 0.03078 -0.056 0.245 0.995 0.931 0.995 23.816 0.283 0.327 3.5 0.782 0.03112 -0.058 0.195 0.996 0.919 0.996 25.140 0.280 0.324 4.0 0.835 0.03221 -0.059 0.124 0.996 0.915 0.996 25.921 0.292 0.321 4.5 0.875 0.03371 -0.062 0.082 0.996 0.892 0.996 25.951 0.278 0.321 5.0 0.937 0.03309 -0.062 0.009 0.996 0.911 0.996 28.308 0.101 0.316 5.5 0.742 0.04941 -0.082 0.003 0.996 0.006 0.996 15.024 0.109 0.360 6.0 0.778 0.05321 -0.085 0.002 0.995 0.004 0.995 14.617 0.341 0.359 6.5 0.808 0.05848 -0.088 0.002 0.995 0.003 0.995 13.816 0.355 0.358 7.0 0.835 0.06548 -0.091 0.001 0.995 0.002 0.995 12.754 0.368 0.358 7.5 0.859 0.07041 -0.094 0.001 0.995 0.002 0.995 12.205 0.386 0.359 8.0 0.880 0.07743 -0.097 0.001 0.995 0.002 0.995 11.370 0.413 0.360 8.5 0.897 0.08926 -0.100 0.001 0.995 0.002 0.995 10.053 0.453 0.361 9.0 0.911 0.09475 -0.103 0.001 0.995 0.002 0.995 9.616 0.517 0.363 9.5 0.921 0.10828 -0.106 0.001 0.995 0.002 0.995 8.504 0.656 0.365 10.0 0.927 0.12200 -0.109 0.001 0.995 0.002 0.995 7.596 1.010 0.368 10.5 0.929 0.14216 -0.112 0.001 0.995 0.001 0.995 6.536 9.087 0.371 11.0 0.927 0.15373 -0.116 0.001 0.995 0.001 0.995 6.033 -0.650 0.375 11.5 0.922 0.16430 -0.119 0.001 0.995 0.001 0.995 5.611 -0.182 0.379 12.0 0.912 0.17215 -0.122 0.001 0.995 0.002 0.995 5.300 -0.053 0.384 12.5 0.901 0.21028 -0.125 0.001 0.995 0.002 0.996 4.283 0.008 0.389 13.0 0.885 0.22360 -0.129 0.001 0.995 0.002 0.996 3.960 0.052 0.395 13.5 0.867 0.23474 -0.132 0.001 0.995 0.002 0.996 3.695 0.077 0.402 14.0 0.847 0.24082 -0.135 0.001 0.995 0.002 0.995 3.518 0.093 0.410 14.5 0.825 0.27584 -0.139 0.001 0.995 0.002 0.995 2.991 0.105 0.418 15.0 0.801 0.28457 -0.142 0.001 0.995 0.002 0.995 2.816 0.109 0.427 Name = AG36 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 -0.462 0.21762 0.018 1.000 0.002 1.000 0.003 -2.122 -14.955 0.289 -14.5 -0.462 0.20485 0.016 1.000 0.002 1.000 0.003 -2.255 1.959 0.285 -14.0 -0.460 0.18497 0.014 1.000 0.002 1.000 0.003 -2.485 0.775 0.281 -13.5 -0.455 0.17191 0.012 1.000 0.002 1.000 0.003 -2.645 0.555 0.277 -13.0 -0.447 0.14705 0.011 1.000 0.002 1.000 0.003 -3.041 0.465 0.274 -12.5 -0.437 0.13637 0.009 1.000 0.002 1.000 0.003 -3.203 0.416 0.270 -12.0 -0.424 0.12118 0.007 1.000 0.002 1.000 0.003 -3.495 0.382 0.266 -11.5 -0.407 0.11438 0.005 1.000 0.002 1.000 0.004 -3.556 0.361 0.261 -11.0 -0.387 0.10160 0.003 1.000 0.003 1.000 0.003 -3.812 0.349 0.257 -10.5 -0.365 0.09107 0.000 1.000 0.003 1.000 0.003 -4.009 0.339 0.251 -10.0 -0.340 0.08142 -0.002 1.000 0.003 1.000 0.004 -4.179 0.331 0.245 -9.5 -0.313 0.07315 -0.004 1.000 0.003 1.000 0.004 -4.280 0.326 0.238 -9.0 -0.284 0.06694 -0.006 0.946 0.003 1.000 0.004 -4.240 0.322 0.229 -8.5 -0.253 0.06164 -0.008 0.935 0.003 1.000 0.004 -4.099 0.319 0.218 -8.0 -0.220 0.05613 -0.010 0.931 0.004 1.000 0.005 -3.917 0.317 0.203 -7.5 -0.186 0.05048 -0.013 0.923 0.004 1.000 0.005 -3.677 0.316 0.182 -7.0 -0.150 0.04611 -0.015 0.914 0.004 1.000 0.005 -3.263 0.314 0.151 -6.5 -0.114 0.04228 -0.017 0.908 0.004 1.000 0.006 -2.685 0.313 0.099 -6.0 -0.076 0.03838 -0.020 0.905 0.005 1.000 0.006 -1.985 0.312 -0.006 -5.5 -0.038 0.03774 -0.022 0.743 0.005 1.000 0.007 -1.002 0.205 -0.328 -5.0 -0.182 0.03530 -0.024 0.724 0.006 1.000 0.008 -5.152 0.190 0.117 -4.5 -0.118 0.03277 -0.027 0.713 0.007 1.000 0.010 -3.602 0.288 0.024 -4.0 -0.055 0.03039 -0.029 0.706 0.009 1.000 0.013 -1.802 0.288 -0.282 -3.5 0.008 0.03261 -0.032 0.481 0.012 1.000 0.023 0.238 0.400 4.305 -3.0 0.066 0.02863 -0.047 0.472 0.881 1.000 0.995 2.308 0.388 0.965 -2.5 0.125 0.02814 -0.048 0.469 0.914 1.000 0.996 4.438 0.257 0.632 -2.0 0.184 0.02765 -0.048 0.467 0.938 1.000 0.996 6.646 0.258 0.512 -1.5 0.242 0.02729 -0.049 0.465 0.959 1.000 0.996 8.886 0.258 0.450 -1.0 0.301 0.02677 -0.049 0.463 0.995 1.000 0.995 11.254 0.258 0.413 -0.5 0.360 0.02680 -0.050 0.461 0.995 1.000 0.995 13.430 0.259 0.388 0.0 0.418 0.02675 -0.050 0.437 0.995 1.000 0.996 15.646 0.259 0.370 0.5 0.477 0.02683 -0.051 0.421 0.995 1.000 0.995 17.779 0.259 0.356 1.0 0.536 0.02711 -0.051 0.402 0.995 1.000 0.995 19.752 0.260 0.346 1.5 0.594 0.02729 -0.052 0.380 0.995 1.000 0.995 21.762 0.260 0.337 2.0 0.652 0.02769 -0.052 0.350 0.995 1.000 0.995 23.548 0.261 0.330 2.5 0.710 0.02877 -0.053 0.284 0.995 1.000 0.995 24.688 0.261 0.325 3.0 0.768 0.02907 -0.054 0.245 0.995 1.000 0.995 26.415 0.262 0.320 3.5 0.825 0.02986 -0.054 0.195 0.996 1.000 0.996 27.610 0.263 0.316 4.0 0.880 0.03039 -0.055 0.124 0.996 1.000 0.996 28.970 0.277 0.313 4.5 0.923 0.03004 -0.057 0.082 0.996 0.979 0.996 30.728 0.289 0.312 5.0 0.970 0.03018 -0.059 0.009 0.996 0.969 0.996 32.134 0.117 0.311 5.5 0.739 0.04370 -0.082 0.003 0.996 0.008 0.996 16.911 0.116 0.360 6.0 0.776 0.04678 -0.085 0.002 0.995 0.004 0.995 16.591 0.336 0.359 6.5 0.808 0.05031 -0.088 0.002 0.995 0.003 0.995 16.051 0.352 0.358 7.0 0.835 0.05499 -0.091 0.001 0.995 0.002 0.995 15.188 0.368 0.358 7.5 0.859 0.06043 -0.094 0.001 0.995 0.002 0.995 14.212 0.387 0.359 8.0 0.880 0.06666 -0.097 0.001 0.995 0.002 0.995 13.200 0.411 0.360 8.5 0.897 0.07284 -0.100 0.001 0.995 0.002 0.995 12.319 0.453 0.361 9.0 0.911 0.08099 -0.103 0.001 0.995 0.002 0.995 11.244 0.517 0.363 9.5 0.921 0.08690 -0.106 0.001 0.995 0.002 0.995 10.596 0.644 0.365 10.0 0.927 0.09665 -0.109 0.001 0.995 0.002 0.995 9.588 1.010 0.368 10.5 0.929 0.11065 -0.112 0.001 0.995 0.001 0.995 8.397 9.087 0.371 11.0 0.927 0.11911 -0.116 0.001 0.995 0.001 0.995 7.786 -0.608 0.375 11.5 0.922 0.13481 -0.119 0.001 0.995 0.002 0.995 6.836 -0.172 0.379 12.0 0.912 0.14047 -0.122 0.001 0.995 0.002 0.995 6.493 -0.058 0.384 12.5 0.901 0.15828 -0.125 0.001 0.995 0.002 0.996 5.690 0.008 0.389 13.0 0.885 0.16655 -0.129 0.001 0.995 0.002 0.996 5.314 0.052 0.395 13.5 0.867 0.17389 -0.132 0.001 0.995 0.002 0.996 4.988 0.077 0.402 14.0 0.847 0.18997 -0.135 0.001 0.995 0.002 0.995 4.458 0.094 0.410 14.5 0.825 0.21345 -0.139 0.001 0.995 0.002 0.995 3.864 0.105 0.418 15.0 0.801 0.21932 -0.142 0.001 0.995 0.002 0.995 3.653 0.109 0.427 Name = AG36 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 -0.462 0.19323 0.018 1.000 0.002 1.000 0.004 -2.388 -5.253 0.289 -14.5 -0.462 0.16981 0.016 1.000 0.002 1.000 0.003 -2.720 2.155 0.285 -14.0 -0.460 0.15431 0.014 1.000 0.002 1.000 0.003 -2.978 0.775 0.281 -13.5 -0.455 0.14371 0.012 1.000 0.002 1.000 0.003 -3.164 0.548 0.277 -13.0 -0.447 0.13293 0.011 1.000 0.002 1.000 0.004 -3.362 0.463 0.274 -12.5 -0.437 0.11984 0.009 1.000 0.002 1.000 0.003 -3.644 0.415 0.270 -12.0 -0.423 0.11158 0.007 1.000 0.002 1.000 0.004 -3.793 0.383 0.266 -11.5 -0.407 0.09784 0.005 1.000 0.002 1.000 0.004 -4.158 0.363 0.261 -11.0 -0.387 0.08828 0.003 1.000 0.003 1.000 0.003 -4.387 0.349 0.257 -10.5 -0.365 0.07944 0.000 1.000 0.003 1.000 0.003 -4.596 0.338 0.251 -10.0 -0.340 0.07365 -0.002 1.000 0.003 1.000 0.004 -4.618 0.331 0.245 -9.5 -0.313 0.06800 -0.004 1.000 0.003 1.000 0.004 -4.600 0.326 0.238 -9.0 -0.284 0.05975 -0.006 0.946 0.003 1.000 0.004 -4.750 0.322 0.229 -8.5 -0.253 0.05521 -0.008 0.935 0.003 1.000 0.004 -4.576 0.319 0.218 -8.0 -0.220 0.05064 -0.010 0.931 0.004 1.000 0.005 -4.342 0.317 0.203 -7.5 -0.186 0.04571 -0.013 0.923 0.004 1.000 0.005 -4.061 0.316 0.182 -7.0 -0.150 0.04217 -0.015 0.914 0.004 1.000 0.005 -3.568 0.314 0.151 -6.5 -0.114 0.03852 -0.017 0.908 0.004 1.000 0.006 -2.948 0.312 0.099 -6.0 -0.076 0.03556 -0.020 0.905 0.005 1.000 0.006 -2.136 0.312 -0.007 -5.5 -0.038 0.03528 -0.022 0.743 0.005 1.000 0.007 -1.065 0.205 -0.332 -5.0 -0.182 0.03308 -0.024 0.724 0.006 1.000 0.009 -5.499 0.190 0.117 -4.5 -0.118 0.03083 -0.027 0.713 0.007 1.000 0.010 -3.829 0.288 0.024 -4.0 -0.055 0.02864 -0.029 0.706 0.009 1.000 0.015 -1.912 0.412 -0.281 -3.5 0.007 0.03678 -0.047 0.481 0.012 1.000 0.997 0.199 0.400 6.654 -3.0 0.066 0.02591 -0.047 0.472 0.881 1.000 0.995 2.550 0.256 0.966 -2.5 0.125 0.02569 -0.048 0.469 0.914 1.000 0.996 4.861 0.257 0.632 -2.0 0.184 0.02527 -0.048 0.467 0.938 1.000 0.996 7.270 0.258 0.512 -1.5 0.242 0.02491 -0.049 0.465 0.959 1.000 0.996 9.733 0.258 0.450 -1.0 0.301 0.02431 -0.049 0.463 0.995 1.000 0.995 12.390 0.258 0.413 -0.5 0.360 0.02457 -0.050 0.461 0.995 1.000 0.995 14.648 0.259 0.388 0.0 0.418 0.02456 -0.050 0.437 0.995 1.000 0.996 17.041 0.259 0.370 0.5 0.477 0.02492 -0.051 0.421 0.995 1.000 0.995 19.140 0.259 0.356 1.0 0.536 0.02515 -0.051 0.402 0.995 1.000 0.995 21.289 0.260 0.346 1.5 0.594 0.02532 -0.052 0.380 0.995 1.000 0.995 23.454 0.260 0.337 2.0 0.652 0.02607 -0.052 0.350 0.995 1.000 0.995 25.016 0.261 0.330 2.5 0.710 0.02702 -0.053 0.284 0.995 1.000 0.995 26.279 0.261 0.325 3.0 0.768 0.02736 -0.054 0.245 0.995 1.000 0.995 28.064 0.262 0.320 3.5 0.825 0.02789 -0.054 0.195 0.996 1.000 0.996 29.564 0.263 0.316 4.0 0.880 0.02866 -0.055 0.124 0.996 1.000 0.996 30.712 0.263 0.313 4.5 0.935 0.02906 -0.056 0.082 0.996 1.000 0.996 32.164 0.264 0.310 5.0 0.988 0.02947 -0.057 0.009 0.996 1.000 0.996 33.514 0.294 0.307 5.5 1.020 0.02811 -0.060 0.003 0.996 0.969 0.996 36.302 0.119 0.308 6.0 0.775 0.04389 -0.085 0.002 0.995 0.005 0.995 17.648 0.120 0.359 6.5 0.807 0.04718 -0.088 0.002 0.995 0.003 0.995 17.097 0.350 0.359 7.0 0.835 0.05113 -0.091 0.001 0.995 0.002 0.995 16.326 0.367 0.359 7.5 0.858 0.05619 -0.094 0.001 0.995 0.002 0.995 15.276 0.386 0.359 8.0 0.880 0.06048 -0.097 0.001 0.995 0.002 0.995 14.550 0.409 0.360 8.5 0.897 0.06568 -0.100 0.001 0.995 0.002 0.995 13.662 0.453 0.361 9.0 0.911 0.07222 -0.103 0.001 0.995 0.002 0.995 12.610 0.522 0.363 9.5 0.920 0.08088 -0.106 0.001 0.995 0.002 0.995 11.379 0.655 0.365 10.0 0.926 0.08899 -0.109 0.001 0.995 0.002 0.995 10.409 0.973 0.368 10.5 0.929 0.09693 -0.112 0.001 0.995 0.001 0.995 9.586 8.713 0.371 11.0 0.927 0.10687 -0.116 0.001 0.995 0.002 0.995 8.675 -0.608 0.375 11.5 0.922 0.11598 -0.119 0.001 0.995 0.002 0.995 7.947 -0.182 0.379 12.0 0.912 0.11992 -0.122 0.001 0.995 0.002 0.995 7.606 -0.054 0.384 12.5 0.900 0.13526 -0.125 0.001 0.995 0.002 0.996 6.656 0.008 0.389 13.0 0.885 0.14145 -0.129 0.001 0.995 0.002 0.996 6.257 0.052 0.395 13.5 0.867 0.15584 -0.132 0.001 0.995 0.002 0.996 5.564 0.078 0.402 14.0 0.847 0.16842 -0.135 0.001 0.995 0.002 0.995 5.027 0.094 0.410 14.5 0.824 0.18691 -0.139 0.001 0.995 0.002 0.995 4.411 0.105 0.418 15.0 0.801 0.19121 -0.142 0.001 0.995 0.002 0.995 4.189 0.108 0.427 Name = AG36 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 -0.462 0.16766 0.018 1.000 0.002 1.000 0.004 -2.753 -16.977 0.289 -14.5 -0.462 0.15891 0.016 1.000 0.002 1.000 0.004 -2.905 1.932 0.285 -14.0 -0.459 0.14533 0.014 1.000 0.002 1.000 0.004 -3.161 0.794 0.281 -13.5 -0.455 0.12738 0.012 1.000 0.002 1.000 0.003 -3.570 0.555 0.277 -13.0 -0.447 0.11733 0.011 1.000 0.002 1.000 0.004 -3.809 0.461 0.274 -12.5 -0.437 0.11017 0.009 1.000 0.002 1.000 0.004 -3.962 0.415 0.270 -12.0 -0.423 0.09975 0.007 1.000 0.002 1.000 0.004 -4.243 0.384 0.266 -11.5 -0.407 0.08824 0.005 1.000 0.002 1.000 0.004 -4.610 0.362 0.261 -11.0 -0.387 0.08280 0.003 1.000 0.003 1.000 0.004 -4.675 0.348 0.257 -10.5 -0.365 0.07453 0.000 1.000 0.003 1.000 0.004 -4.896 0.339 0.251 -10.0 -0.340 0.06747 -0.002 1.000 0.003 1.000 0.004 -5.041 0.331 0.245 -9.5 -0.313 0.06229 -0.004 1.000 0.003 1.000 0.004 -5.022 0.326 0.238 -9.0 -0.284 0.05776 -0.006 0.946 0.003 1.000 0.004 -4.909 0.322 0.229 -8.5 -0.253 0.05144 -0.008 0.935 0.003 1.000 0.004 -4.911 0.319 0.218 -8.0 -0.220 0.04731 -0.010 0.931 0.004 1.000 0.005 -4.647 0.316 0.203 -7.5 -0.185 0.04399 -0.013 0.923 0.004 1.000 0.005 -4.213 0.315 0.182 -7.0 -0.150 0.04036 -0.015 0.914 0.004 1.000 0.005 -3.722 0.314 0.151 -6.5 -0.113 0.03689 -0.017 0.908 0.004 1.000 0.006 -3.071 0.313 0.099 -6.0 -0.076 0.03352 -0.020 0.905 0.005 1.000 0.006 -2.266 0.312 -0.007 -5.5 -0.037 0.03385 -0.022 0.743 0.005 1.000 0.007 -1.103 0.205 -0.336 -5.0 -0.182 0.03173 -0.024 0.724 0.006 1.000 0.009 -5.732 0.190 0.117 -4.5 -0.118 0.02959 -0.027 0.713 0.007 1.000 0.011 -3.989 0.288 0.024 -4.0 -0.055 0.02754 -0.029 0.706 0.009 1.000 0.017 -1.988 0.412 -0.281 -3.5 0.007 0.03572 -0.047 0.481 0.012 1.000 0.997 0.205 0.401 6.655 -3.0 0.066 0.02427 -0.047 0.472 0.881 1.000 0.996 2.722 0.256 0.966 -2.5 0.125 0.02388 -0.048 0.469 0.914 1.000 0.996 5.230 0.257 0.632 -2.0 0.184 0.02374 -0.048 0.467 0.938 1.000 0.996 7.738 0.258 0.512 -1.5 0.242 0.02339 -0.049 0.465 0.959 1.000 0.996 10.367 0.258 0.450 -1.0 0.301 0.02304 -0.049 0.463 0.995 1.000 0.995 13.074 0.258 0.413 -0.5 0.360 0.02291 -0.050 0.461 0.995 1.000 0.995 15.705 0.259 0.388 0.0 0.418 0.02325 -0.050 0.437 0.995 1.000 0.996 17.998 0.259 0.370 0.5 0.477 0.02359 -0.051 0.421 0.995 1.000 0.995 20.223 0.259 0.356 1.0 0.536 0.02380 -0.051 0.402 0.995 1.000 0.995 22.504 0.260 0.346 1.5 0.594 0.02430 -0.052 0.380 0.995 1.000 0.995 24.436 0.260 0.337 2.0 0.652 0.02470 -0.052 0.350 0.995 1.000 0.995 26.398 0.261 0.330 2.5 0.710 0.02580 -0.053 0.284 0.995 1.000 0.995 27.532 0.261 0.325 3.0 0.768 0.02615 -0.054 0.245 0.995 1.000 0.995 29.359 0.262 0.320 3.5 0.825 0.02676 -0.054 0.195 0.996 1.000 0.996 30.814 0.263 0.316 4.0 0.880 0.02767 -0.055 0.124 0.996 1.000 0.996 31.810 0.263 0.313 4.5 0.935 0.02812 -0.056 0.082 0.996 1.000 0.996 33.239 0.264 0.310 5.0 0.988 0.02814 -0.057 0.009 0.996 1.000 0.996 35.101 0.281 0.307 5.5 1.028 0.02746 -0.059 0.003 0.996 0.981 0.996 37.420 0.120 0.307 6.0 0.772 0.04231 -0.085 0.002 0.995 0.006 0.995 18.252 0.120 0.360 6.5 0.806 0.04495 -0.088 0.002 0.995 0.004 0.995 17.937 0.346 0.359 7.0 0.834 0.04874 -0.091 0.001 0.995 0.003 0.995 17.120 0.366 0.359 7.5 0.858 0.05266 -0.094 0.001 0.995 0.002 0.995 16.300 0.386 0.359 8.0 0.880 0.05816 -0.097 0.001 0.995 0.002 0.995 15.121 0.411 0.360 8.5 0.897 0.06314 -0.100 0.001 0.995 0.002 0.995 14.204 0.453 0.361 9.0 0.910 0.06947 -0.103 0.001 0.995 0.002 0.995 13.103 0.516 0.363 9.5 0.920 0.07452 -0.106 0.001 0.995 0.002 0.995 12.350 0.643 0.365 10.0 0.926 0.08153 -0.109 0.001 0.995 0.002 0.995 11.361 1.008 0.368 10.5 0.929 0.09151 -0.112 0.001 0.995 0.002 0.995 10.149 8.713 0.371 11.0 0.927 0.09699 -0.116 0.001 0.995 0.002 0.995 9.558 -0.612 0.375 11.5 0.921 0.10634 -0.119 0.001 0.995 0.002 0.995 8.664 -0.173 0.379 12.0 0.912 0.11361 -0.122 0.001 0.995 0.002 0.995 8.025 -0.059 0.384 12.5 0.900 0.12128 -0.125 0.001 0.995 0.002 0.996 7.423 0.008 0.389 13.0 0.885 0.13316 -0.129 0.001 0.995 0.002 0.996 6.645 0.054 0.395 13.5 0.867 0.14567 -0.132 0.001 0.995 0.002 0.996 5.950 0.078 0.402 14.0 0.846 0.15600 -0.135 0.001 0.995 0.002 0.995 5.426 0.093 0.410 14.5 0.824 0.16209 -0.139 0.001 0.995 0.002 0.995 5.086 0.104 0.418 15.0 0.801 0.17461 -0.142 0.001 0.995 0.002 0.995 4.585 0.109 0.427