Name = naca-2208 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 -0.437 0.49061 0.039 1.000 0.002 1.000 0.003 -0.891 -0.032 0.340 -14.5 -0.446 0.47815 0.037 1.000 0.002 1.000 0.003 -0.932 -0.060 0.333 -14.0 -0.453 0.41095 0.035 1.000 0.002 1.000 0.003 -1.102 -0.149 0.326 -13.5 -0.458 0.35956 0.032 1.000 0.002 1.000 0.003 -1.273 -0.320 0.320 -13.0 -0.461 0.34225 0.030 1.000 0.002 1.000 0.003 -1.348 -0.905 0.314 -12.5 -0.462 0.29268 0.027 1.000 0.002 1.000 0.003 -1.579 6.983 0.309 -12.0 -0.461 0.26721 0.025 1.000 0.002 1.000 0.003 -1.724 1.112 0.304 -11.5 -0.456 0.24145 0.022 1.000 0.002 1.000 0.003 -1.890 0.689 0.299 -11.0 -0.449 0.21424 0.020 1.000 0.002 1.000 0.003 -2.096 0.545 0.294 -10.5 -0.439 0.17830 0.017 1.000 0.003 1.000 0.003 -2.463 0.466 0.289 -10.0 -0.426 0.17387 0.015 1.000 0.002 1.000 0.003 -2.448 0.420 0.284 -9.5 -0.409 0.15702 0.012 1.000 0.003 1.000 0.003 -2.606 0.394 0.280 -9.0 -0.390 0.12530 0.010 1.000 0.003 1.000 0.003 -3.111 0.372 0.274 -8.5 -0.367 0.11604 0.007 1.000 0.003 1.000 0.003 -3.163 0.355 0.269 -8.0 -0.341 0.10074 0.004 1.000 0.003 1.000 0.004 -3.382 0.346 0.263 -7.5 -0.313 0.08392 0.002 1.000 0.003 1.000 0.004 -3.725 0.340 0.256 -7.0 -0.282 0.07451 -0.001 1.000 0.003 1.000 0.004 -3.787 0.334 0.247 -6.5 -0.250 0.06879 -0.004 1.000 0.003 1.000 0.005 -3.633 0.330 0.236 -6.0 -0.216 0.06372 -0.006 0.915 0.003 1.000 0.005 -3.396 0.327 0.221 -5.5 -0.181 0.05254 -0.009 0.905 0.004 1.000 0.005 -3.446 0.324 0.201 -5.0 -0.144 0.04898 -0.012 0.894 0.004 1.000 0.006 -2.949 0.322 0.170 -4.5 -0.107 0.04286 -0.014 0.884 0.005 1.000 0.006 -2.495 0.321 0.117 -4.0 -0.069 0.04019 -0.017 0.867 0.006 1.000 0.007 -1.710 0.320 0.004 -3.5 -0.030 0.03572 -0.020 0.851 0.006 1.000 0.009 -0.828 0.174 -0.412 -3.0 -0.140 0.03285 -0.022 0.831 0.008 1.000 0.011 -4.266 0.138 0.091 -2.5 -0.078 0.02968 -0.025 0.812 0.010 1.000 0.013 -2.622 0.294 -0.071 -2.0 -0.016 0.02597 -0.028 0.787 0.013 1.000 0.019 -0.624 0.294 -1.461 -1.5 0.045 0.02402 -0.030 0.759 0.020 1.000 0.031 1.855 0.331 0.933 -1.0 0.103 0.02391 -0.037 0.727 0.037 1.000 0.968 4.296 0.315 0.613 -0.5 0.162 0.02345 -0.038 0.690 0.866 1.000 0.962 6.907 0.263 0.485 0.0 0.221 0.02312 -0.039 0.647 0.892 1.000 0.962 9.568 0.262 0.426 0.5 0.280 0.02364 -0.040 0.596 0.913 1.000 0.962 11.859 0.260 0.391 1.0 0.339 0.02421 -0.040 0.537 0.961 1.000 0.962 14.023 0.260 0.368 1.5 0.399 0.02610 -0.041 0.210 0.961 1.000 0.962 15.270 0.260 0.352 2.0 0.458 0.02613 -0.041 0.206 0.961 1.000 0.962 17.511 0.261 0.340 2.5 0.517 0.02702 -0.042 0.203 0.961 1.000 0.962 19.123 0.261 0.331 3.0 0.576 0.02787 -0.043 0.200 0.962 1.000 0.962 20.650 0.261 0.324 3.5 0.634 0.02703 -0.043 0.197 0.962 1.000 0.963 23.471 0.261 0.318 4.0 0.693 0.02905 -0.044 0.194 0.961 1.000 0.962 23.845 0.689 0.313 4.5 0.659 0.03142 -0.054 0.188 0.961 0.812 0.962 20.985 0.089 0.332 5.0 0.534 0.04333 -0.069 0.182 0.962 0.337 0.963 12.323 0.069 0.380 5.5 0.556 0.04782 -0.073 0.176 0.962 0.246 0.963 11.635 0.191 0.381 6.0 0.920 0.03048 -0.047 0.010 0.962 1.000 0.963 30.175 0.274 0.301 6.5 0.680 0.04705 -0.076 0.006 0.961 0.012 0.962 14.454 0.090 0.361 7.0 0.719 0.05126 -0.079 0.005 0.961 0.008 0.962 14.028 0.325 0.359 7.5 0.754 0.05508 -0.081 0.004 0.962 0.006 0.963 13.689 0.333 0.358 8.0 0.787 0.05904 -0.084 0.003 0.963 0.005 0.963 13.327 0.341 0.357 8.5 0.816 0.06828 -0.087 0.002 0.963 0.004 0.964 11.952 0.351 0.357 9.0 0.843 0.07597 -0.090 0.002 0.963 0.003 0.964 11.096 0.363 0.357 9.5 0.866 0.08397 -0.093 0.002 0.962 0.003 0.963 10.317 0.379 0.357 10.0 0.887 0.09364 -0.096 0.002 0.962 0.003 0.963 9.475 0.399 0.358 10.5 0.905 0.10147 -0.098 0.002 0.962 0.002 0.963 8.915 0.434 0.359 11.0 0.918 0.11772 -0.101 0.001 0.962 0.002 0.963 7.800 0.482 0.360 11.5 0.929 0.12783 -0.104 0.001 0.962 0.002 0.963 7.269 0.610 0.362 12.0 0.934 0.13917 -0.107 0.001 0.962 0.002 0.963 6.712 1.509 0.365 12.5 0.934 0.16351 -0.110 0.001 0.962 0.002 0.963 5.711 -0.962 0.368 13.0 0.929 0.19611 -0.113 0.001 0.964 0.001 0.964 4.739 -0.189 0.371 13.5 0.921 0.19270 -0.116 0.001 0.964 0.001 0.964 4.778 -0.022 0.376 14.0 0.908 0.21362 -0.118 0.001 0.964 0.001 0.964 4.252 0.046 0.380 14.5 0.893 0.23816 -0.121 0.001 0.964 0.001 0.965 3.748 0.084 0.386 15.0 0.874 0.26861 -0.124 0.001 0.964 0.001 0.965 3.254 0.098 0.392 Name = naca-2208 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 -0.437 0.35193 0.039 1.000 0.002 1.000 0.003 -1.242 -0.032 0.340 -14.5 -0.446 0.35408 0.037 1.000 0.002 1.000 0.003 -1.258 -0.060 0.333 -14.0 -0.453 0.30655 0.035 1.000 0.002 1.000 0.003 -1.476 -0.149 0.327 -13.5 -0.458 0.27686 0.032 1.000 0.002 1.000 0.004 -1.653 -0.322 0.320 -13.0 -0.461 0.26604 0.030 1.000 0.002 1.000 0.003 -1.733 -0.912 0.314 -12.5 -0.462 0.22923 0.027 1.000 0.002 1.000 0.004 -2.015 9.568 0.309 -12.0 -0.461 0.18612 0.025 1.000 0.002 1.000 0.003 -2.475 1.148 0.304 -11.5 -0.456 0.16901 0.022 1.000 0.002 1.000 0.003 -2.700 0.689 0.299 -11.0 -0.449 0.15119 0.020 1.000 0.002 1.000 0.003 -2.971 0.541 0.294 -10.5 -0.439 0.14657 0.017 1.000 0.003 1.000 0.003 -2.995 0.466 0.289 -10.0 -0.426 0.12409 0.015 1.000 0.002 1.000 0.003 -3.430 0.422 0.284 -9.5 -0.409 0.11368 0.012 1.000 0.003 1.000 0.003 -3.600 0.393 0.280 -9.0 -0.390 0.10022 0.010 1.000 0.003 1.000 0.003 -3.889 0.372 0.274 -8.5 -0.367 0.08749 0.007 1.000 0.003 1.000 0.003 -4.196 0.356 0.269 -8.0 -0.341 0.07659 0.004 1.000 0.003 1.000 0.004 -4.448 0.345 0.263 -7.5 -0.312 0.07068 0.002 1.000 0.003 1.000 0.004 -4.420 0.339 0.256 -7.0 -0.282 0.06193 -0.001 1.000 0.003 1.000 0.004 -4.553 0.334 0.247 -6.5 -0.250 0.05686 -0.004 1.000 0.003 1.000 0.005 -4.391 0.331 0.236 -6.0 -0.216 0.04957 -0.006 0.915 0.003 1.000 0.005 -4.365 0.327 0.221 -5.5 -0.181 0.04353 -0.009 0.905 0.004 1.000 0.005 -4.154 0.324 0.201 -5.0 -0.144 0.03930 -0.012 0.894 0.004 1.000 0.006 -3.669 0.322 0.170 -4.5 -0.107 0.03654 -0.014 0.884 0.005 1.000 0.007 -2.918 0.321 0.117 -4.0 -0.069 0.03202 -0.017 0.867 0.006 1.000 0.007 -2.147 0.320 0.004 -3.5 -0.029 0.02949 -0.020 0.851 0.006 1.000 0.009 -0.990 0.174 -0.420 -3.0 -0.140 0.02633 -0.022 0.831 0.008 1.000 0.011 -5.321 0.138 0.091 -2.5 -0.078 0.02425 -0.025 0.812 0.010 1.000 0.014 -3.209 0.294 -0.071 -2.0 -0.016 0.02174 -0.028 0.787 0.013 1.000 0.022 -0.746 0.294 -1.460 -1.5 0.045 0.02004 -0.030 0.759 0.020 1.000 0.045 2.222 0.331 0.932 -1.0 0.103 0.01807 -0.037 0.727 0.037 1.000 0.969 5.685 0.316 0.614 -0.5 0.162 0.01681 -0.038 0.690 0.866 1.000 0.963 9.637 0.263 0.485 0.0 0.221 0.01738 -0.039 0.647 0.892 1.000 0.963 12.726 0.262 0.426 0.5 0.280 0.01707 -0.040 0.596 0.913 1.000 0.963 16.421 0.260 0.391 1.0 0.339 0.01827 -0.040 0.537 0.961 1.000 0.962 18.586 0.260 0.368 1.5 0.399 0.01934 -0.041 0.210 0.961 1.000 0.962 20.613 0.260 0.352 2.0 0.458 0.01968 -0.041 0.206 0.961 1.000 0.962 23.249 0.261 0.340 2.5 0.517 0.02033 -0.042 0.203 0.961 1.000 0.962 25.407 0.261 0.331 3.0 0.576 0.02034 -0.043 0.200 0.962 1.000 0.962 28.289 0.261 0.324 3.5 0.634 0.02065 -0.043 0.197 0.962 1.000 0.963 30.719 0.261 0.318 4.0 0.693 0.02191 -0.044 0.194 0.961 1.000 0.962 31.618 0.261 0.313 4.5 0.751 0.02243 -0.045 0.188 0.961 1.000 0.962 33.459 0.261 0.309 5.0 0.808 0.02308 -0.045 0.182 0.962 1.000 0.963 35.001 0.262 0.306 5.5 0.864 0.02381 -0.046 0.176 0.962 1.000 0.963 36.299 0.262 0.303 6.0 0.920 0.02505 -0.047 0.010 0.962 1.000 0.963 36.713 0.093 0.301 6.5 0.672 0.04158 -0.076 0.006 0.961 0.018 0.962 16.164 0.092 0.363 7.0 0.717 0.04433 -0.079 0.005 0.961 0.009 0.962 16.176 0.317 0.360 7.5 0.753 0.04799 -0.081 0.004 0.962 0.007 0.963 15.687 0.332 0.358 8.0 0.785 0.05213 -0.084 0.003 0.963 0.005 0.963 15.067 0.340 0.357 8.5 0.815 0.05799 -0.087 0.002 0.963 0.004 0.964 14.061 0.348 0.357 9.0 0.843 0.06135 -0.090 0.002 0.963 0.003 0.964 13.738 0.363 0.357 9.5 0.866 0.07272 -0.093 0.002 0.962 0.003 0.963 11.904 0.380 0.357 10.0 0.887 0.07761 -0.096 0.002 0.962 0.003 0.963 11.428 0.397 0.358 10.5 0.904 0.08143 -0.098 0.002 0.962 0.002 0.963 11.105 0.435 0.359 11.0 0.918 0.09678 -0.101 0.001 0.962 0.002 0.963 9.484 0.482 0.360 11.5 0.929 0.10411 -0.104 0.001 0.962 0.002 0.963 8.922 0.609 0.362 12.0 0.934 0.11477 -0.107 0.001 0.962 0.002 0.963 8.135 1.495 0.365 12.5 0.933 0.13444 -0.110 0.001 0.962 0.002 0.963 6.943 -1.055 0.368 13.0 0.929 0.14285 -0.113 0.001 0.964 0.001 0.964 6.506 -0.186 0.371 13.5 0.920 0.15696 -0.116 0.001 0.964 0.002 0.964 5.863 -0.018 0.376 14.0 0.908 0.17228 -0.118 0.001 0.964 0.002 0.964 5.271 0.046 0.380 14.5 0.892 0.19025 -0.121 0.001 0.964 0.002 0.965 4.690 0.084 0.386 15.0 0.874 0.21269 -0.124 0.001 0.964 0.002 0.965 4.107 0.097 0.392 Name = naca-2208 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 -0.437 0.32248 0.039 1.000 0.002 1.000 0.004 -1.354 -0.031 0.340 -14.5 -0.445 0.30086 0.037 1.000 0.002 1.000 0.004 -1.480 -0.060 0.333 -14.0 -0.452 0.26192 0.035 1.000 0.002 1.000 0.004 -1.727 -0.145 0.327 -13.5 -0.458 0.21783 0.032 1.000 0.002 1.000 0.004 -2.101 -0.311 0.320 -13.0 -0.461 0.20927 0.030 1.000 0.002 1.000 0.003 -2.203 -0.912 0.314 -12.5 -0.462 0.18162 0.027 1.000 0.002 1.000 0.004 -2.543 6.742 0.309 -12.0 -0.460 0.16775 0.025 1.000 0.002 1.000 0.004 -2.744 1.108 0.304 -11.5 -0.456 0.15351 0.022 1.000 0.002 1.000 0.004 -2.971 0.688 0.299 -11.0 -0.449 0.13842 0.020 1.000 0.002 1.000 0.004 -3.243 0.545 0.294 -10.5 -0.439 0.12105 0.017 1.000 0.003 1.000 0.003 -3.626 0.466 0.289 -10.0 -0.425 0.11543 0.015 1.000 0.002 1.000 0.004 -3.685 0.422 0.284 -9.5 -0.409 0.09526 0.012 1.000 0.003 1.000 0.003 -4.296 0.393 0.280 -9.0 -0.390 0.08998 0.010 1.000 0.003 1.000 0.004 -4.329 0.372 0.274 -8.5 -0.367 0.07514 0.007 1.000 0.003 1.000 0.003 -4.885 0.356 0.269 -8.0 -0.341 0.06618 0.004 1.000 0.003 1.000 0.004 -5.148 0.345 0.263 -7.5 -0.312 0.06073 0.002 1.000 0.003 1.000 0.004 -5.144 0.339 0.256 -7.0 -0.282 0.05705 -0.001 1.000 0.003 1.000 0.005 -4.939 0.334 0.247 -6.5 -0.250 0.04910 -0.004 1.000 0.003 1.000 0.005 -5.085 0.331 0.236 -6.0 -0.216 0.04572 -0.006 0.915 0.003 1.000 0.005 -4.728 0.327 0.221 -5.5 -0.181 0.03912 -0.009 0.905 0.004 1.000 0.006 -4.616 0.324 0.201 -5.0 -0.144 0.03476 -0.012 0.894 0.004 1.000 0.006 -4.149 0.322 0.170 -4.5 -0.107 0.03242 -0.014 0.884 0.005 1.000 0.007 -3.289 0.321 0.117 -4.0 -0.068 0.02966 -0.017 0.867 0.006 1.000 0.008 -2.306 0.319 0.003 -3.5 -0.029 0.02670 -0.020 0.851 0.006 1.000 0.010 -1.080 0.175 -0.429 -3.0 -0.140 0.02386 -0.022 0.831 0.008 1.000 0.012 -5.874 0.139 0.091 -2.5 -0.078 0.02191 -0.025 0.812 0.010 1.000 0.016 -3.550 0.294 -0.071 -2.0 -0.016 0.01957 -0.028 0.787 0.013 1.000 0.026 -0.828 0.346 -1.458 -1.5 0.043 0.01492 -0.037 0.759 0.020 1.000 0.970 2.915 0.332 1.092 -1.0 0.103 0.01533 -0.037 0.727 0.037 1.000 0.971 6.700 0.263 0.614 -0.5 0.162 0.01396 -0.038 0.690 0.866 1.000 0.963 11.602 0.263 0.485 0.0 0.221 0.01402 -0.039 0.647 0.892 1.000 0.963 15.772 0.262 0.426 0.5 0.280 0.01430 -0.040 0.596 0.913 1.000 0.963 19.604 0.260 0.391 1.0 0.339 0.01533 -0.040 0.537 0.961 1.000 0.962 22.141 0.260 0.368 1.5 0.399 0.01746 -0.041 0.210 0.961 1.000 0.962 22.830 0.260 0.352 2.0 0.458 0.01770 -0.041 0.206 0.961 1.000 0.962 25.852 0.261 0.340 2.5 0.517 0.01803 -0.042 0.203 0.961 1.000 0.962 28.657 0.261 0.331 3.0 0.576 0.01759 -0.043 0.200 0.962 1.000 0.962 32.724 0.261 0.324 3.5 0.634 0.01840 -0.043 0.197 0.962 1.000 0.963 34.468 0.261 0.318 4.0 0.693 0.01864 -0.044 0.194 0.961 1.000 0.962 37.168 0.261 0.313 4.5 0.751 0.01910 -0.045 0.188 0.961 1.000 0.962 39.289 0.261 0.309 5.0 0.808 0.02004 -0.045 0.182 0.962 1.000 0.963 40.307 0.262 0.306 5.5 0.864 0.02064 -0.046 0.176 0.962 1.000 0.963 41.886 0.262 0.303 6.0 0.920 0.02311 -0.047 0.010 0.962 1.000 0.963 39.799 0.262 0.301 6.5 0.974 0.02394 -0.047 0.006 0.961 1.000 0.962 40.674 0.093 0.298 7.0 0.715 0.04112 -0.079 0.005 0.961 0.010 0.962 17.396 0.096 0.360 7.5 0.752 0.04417 -0.081 0.004 0.962 0.008 0.963 17.015 0.331 0.358 8.0 0.785 0.04757 -0.084 0.003 0.963 0.006 0.963 16.496 0.339 0.357 8.5 0.815 0.05313 -0.087 0.002 0.963 0.005 0.964 15.335 0.349 0.357 9.0 0.842 0.05881 -0.090 0.002 0.963 0.004 0.964 14.318 0.362 0.357 9.5 0.866 0.06285 -0.093 0.002 0.962 0.003 0.963 13.773 0.378 0.357 10.0 0.887 0.07086 -0.096 0.002 0.962 0.003 0.963 12.512 0.400 0.358 10.5 0.904 0.07839 -0.098 0.002 0.962 0.003 0.963 11.527 0.432 0.359 11.0 0.918 0.08009 -0.101 0.001 0.962 0.002 0.963 11.460 0.479 0.360 11.5 0.928 0.09134 -0.104 0.001 0.962 0.002 0.963 10.166 0.618 0.362 12.0 0.933 0.10571 -0.107 0.001 0.962 0.002 0.963 8.830 1.404 0.365 12.5 0.933 0.11283 -0.110 0.001 0.962 0.002 0.963 8.273 -1.043 0.368 13.0 0.929 0.13299 -0.113 0.001 0.964 0.002 0.964 6.985 -0.177 0.371 13.5 0.920 0.14342 -0.116 0.001 0.964 0.002 0.964 6.415 -0.019 0.376 14.0 0.908 0.15614 -0.118 0.001 0.964 0.002 0.964 5.814 0.046 0.381 14.5 0.892 0.17113 -0.121 0.001 0.964 0.002 0.965 5.213 0.084 0.386 15.0 0.873 0.19004 -0.124 0.001 0.964 0.002 0.965 4.596 0.097 0.392 Name = naca-2208 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 -0.437 0.23860 0.040 1.000 0.002 1.000 0.004 -1.830 -0.029 0.340 -14.5 -0.445 0.24446 0.037 1.000 0.002 1.000 0.004 -1.822 -0.060 0.333 -14.0 -0.452 0.23536 0.035 1.000 0.002 1.000 0.004 -1.922 -0.150 0.327 -13.5 -0.457 0.18070 0.032 1.000 0.002 1.000 0.004 -2.532 -0.318 0.320 -13.0 -0.461 0.19478 0.030 1.000 0.002 1.000 0.004 -2.366 -0.922 0.315 -12.5 -0.462 0.15704 0.027 1.000 0.002 1.000 0.004 -2.940 7.268 0.309 -12.0 -0.460 0.15815 0.025 1.000 0.002 1.000 0.004 -2.910 1.148 0.304 -11.5 -0.456 0.13154 0.022 1.000 0.002 1.000 0.004 -3.467 0.695 0.299 -11.0 -0.449 0.11902 0.020 1.000 0.002 1.000 0.004 -3.772 0.541 0.294 -10.5 -0.439 0.11679 0.017 1.000 0.003 1.000 0.004 -3.756 0.466 0.289 -10.0 -0.425 0.09974 0.015 1.000 0.002 1.000 0.004 -4.265 0.422 0.284 -9.5 -0.409 0.09264 0.012 1.000 0.003 1.000 0.004 -4.415 0.393 0.280 -9.0 -0.390 0.07965 0.010 1.000 0.003 1.000 0.004 -4.891 0.372 0.274 -8.5 -0.367 0.07353 0.007 1.000 0.003 1.000 0.004 -4.988 0.356 0.269 -8.0 -0.340 0.06494 0.004 1.000 0.003 1.000 0.004 -5.243 0.345 0.263 -7.5 -0.312 0.05879 0.002 1.000 0.003 1.000 0.004 -5.310 0.339 0.256 -7.0 -0.282 0.05121 -0.001 1.000 0.003 1.000 0.005 -5.502 0.334 0.247 -6.5 -0.249 0.04674 -0.004 1.000 0.003 1.000 0.005 -5.337 0.330 0.236 -6.0 -0.216 0.04324 -0.006 0.915 0.003 1.000 0.005 -4.993 0.327 0.221 -5.5 -0.180 0.03791 -0.009 0.905 0.004 1.000 0.006 -4.758 0.324 0.201 -5.0 -0.144 0.03392 -0.011 0.894 0.004 1.000 0.006 -4.238 0.322 0.170 -4.5 -0.106 0.03103 -0.014 0.884 0.005 1.000 0.007 -3.425 0.321 0.117 -4.0 -0.068 0.02800 -0.017 0.867 0.006 1.000 0.008 -2.429 0.319 0.002 -3.5 -0.028 0.02522 -0.020 0.851 0.006 1.000 0.010 -1.129 0.175 -0.437 -3.0 -0.140 0.02251 -0.022 0.831 0.008 1.000 0.013 -6.224 0.140 0.091 -2.5 -0.078 0.02025 -0.025 0.812 0.010 1.000 0.017 -3.841 0.293 -0.071 -2.0 -0.016 0.01842 -0.028 0.787 0.013 1.000 0.038 -0.879 0.346 -1.453 -1.5 0.043 0.01362 -0.037 0.759 0.020 1.000 0.971 3.192 0.332 1.092 -1.0 0.103 0.01384 -0.037 0.727 0.037 1.000 0.972 7.422 0.262 0.614 -0.5 0.162 0.01268 -0.038 0.690 0.866 1.000 0.964 12.780 0.263 0.485 0.0 0.221 0.01284 -0.039 0.647 0.892 1.000 0.963 17.232 0.262 0.426 0.5 0.280 0.01296 -0.040 0.596 0.913 1.000 0.963 21.635 0.260 0.391 1.0 0.339 0.01311 -0.040 0.537 0.961 1.000 0.962 25.905 0.260 0.368 1.5 0.399 0.01516 -0.041 0.210 0.961 1.000 0.962 26.286 0.260 0.352 2.0 0.458 0.01587 -0.041 0.206 0.961 1.000 0.962 28.842 0.261 0.340 2.5 0.517 0.01554 -0.042 0.203 0.961 1.000 0.962 33.238 0.261 0.331 3.0 0.576 0.01614 -0.043 0.200 0.962 1.000 0.962 35.661 0.261 0.324 3.5 0.634 0.01667 -0.043 0.197 0.962 1.000 0.963 38.046 0.261 0.318 4.0 0.693 0.01769 -0.044 0.194 0.961 1.000 0.962 39.168 0.261 0.313 4.5 0.751 0.01767 -0.045 0.188 0.961 1.000 0.962 42.474 0.261 0.309 5.0 0.808 0.01789 -0.045 0.182 0.962 1.000 0.963 45.159 0.262 0.306 5.5 0.864 0.01865 -0.046 0.176 0.962 1.000 0.963 46.339 0.262 0.303 6.0 0.920 0.02196 -0.047 0.010 0.962 1.000 0.963 41.889 0.262 0.301 6.5 0.974 0.02255 -0.047 0.006 0.961 1.000 0.962 43.186 0.096 0.298 7.0 0.711 0.03968 -0.079 0.005 0.961 0.014 0.962 17.914 0.097 0.361 7.5 0.750 0.04209 -0.081 0.004 0.962 0.009 0.963 17.810 0.325 0.359 8.0 0.784 0.04482 -0.084 0.003 0.963 0.006 0.963 17.493 0.337 0.357 8.5 0.814 0.05016 -0.087 0.002 0.963 0.005 0.964 16.227 0.347 0.357 9.0 0.842 0.05403 -0.090 0.002 0.963 0.004 0.964 15.586 0.362 0.357 9.5 0.865 0.06132 -0.093 0.002 0.962 0.004 0.963 14.104 0.378 0.357 10.0 0.887 0.06426 -0.096 0.002 0.962 0.003 0.963 13.796 0.397 0.358 10.5 0.904 0.07040 -0.098 0.002 0.962 0.003 0.963 12.835 0.435 0.359 11.0 0.917 0.07836 -0.101 0.001 0.962 0.003 0.963 11.708 0.479 0.360 11.5 0.928 0.08170 -0.104 0.001 0.962 0.002 0.963 11.364 0.609 0.362 12.0 0.933 0.09030 -0.107 0.001 0.962 0.002 0.963 10.337 1.481 0.365 12.5 0.933 0.10379 -0.110 0.001 0.962 0.002 0.963 8.991 -1.043 0.368 13.0 0.929 0.11631 -0.113 0.001 0.964 0.002 0.964 7.987 -0.186 0.371 13.5 0.920 0.12383 -0.116 0.001 0.964 0.002 0.964 7.430 -0.019 0.376 14.0 0.908 0.13437 -0.118 0.001 0.964 0.002 0.964 6.756 0.046 0.381 14.5 0.892 0.14667 -0.121 0.001 0.964 0.002 0.965 6.082 0.084 0.386 15.0 0.873 0.16193 -0.124 0.001 0.964 0.002 0.965 5.393 0.097 0.392