Name = naca-8410 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 -0.092 0.32102 -0.137 0.870 0.004 1.000 0.005 -0.287 0.380 -1.241 -14.5 -0.071 0.30525 -0.140 0.862 0.004 1.000 0.005 -0.234 0.373 -1.708 -14.0 -0.049 0.30178 -0.143 0.855 0.004 1.000 0.005 -0.161 0.364 -2.688 -13.5 -0.024 0.25489 -0.145 0.848 0.004 1.000 0.005 -0.093 0.237 -5.901 -13.0 -0.472 0.21717 -0.148 0.841 0.004 1.000 0.005 -2.173 0.236 -0.064 -12.5 -0.433 0.21928 -0.151 0.833 0.004 1.000 0.005 -1.973 0.318 -0.099 -12.0 -0.389 0.20603 -0.154 0.823 0.004 1.000 0.005 -1.890 0.313 -0.145 -11.5 -0.343 0.18092 -0.157 0.817 0.004 1.000 0.005 -1.894 0.308 -0.207 -11.0 -0.292 0.16672 -0.159 0.808 0.004 1.000 0.005 -1.754 0.305 -0.295 -10.5 -0.239 0.15133 -0.162 0.798 0.004 1.000 0.005 -1.579 0.303 -0.429 -10.0 -0.183 0.13249 -0.165 0.788 0.004 1.000 0.005 -1.379 0.301 -0.654 -9.5 -0.124 0.12058 -0.168 0.779 0.005 0.922 0.005 -1.027 0.299 -1.107 -9.0 -0.063 0.11483 -0.171 0.768 0.005 0.919 0.006 -0.548 0.298 -2.466 -8.5 -0.000 0.09955 -0.174 0.758 0.005 0.914 0.006 -0.004 0.297 0.250 -8.0 0.064 0.09177 -0.177 0.747 0.005 0.910 0.006 0.692 0.297 3.037 -7.5 0.128 0.08051 -0.180 0.736 0.005 0.907 0.006 1.593 0.296 1.653 -7.0 0.194 0.07725 -0.183 0.723 0.005 0.904 0.007 2.506 0.296 1.196 -6.5 0.259 0.07165 -0.186 0.712 0.006 0.899 0.007 3.611 0.297 0.969 -6.0 0.324 0.06465 -0.189 0.697 0.006 0.898 0.008 5.005 0.298 0.834 -5.5 0.388 0.05884 -0.192 0.683 0.007 0.894 0.008 6.594 0.298 0.745 -5.0 0.452 0.05452 -0.195 0.669 0.007 0.891 0.009 8.287 0.299 0.682 -4.5 0.515 0.05124 -0.198 0.654 0.008 0.888 0.011 10.045 0.300 0.636 -4.0 0.577 0.04724 -0.202 0.637 0.009 0.885 0.011 12.208 0.301 0.600 -3.5 0.637 0.04497 -0.205 0.619 0.010 0.884 0.013 14.174 0.302 0.571 -3.0 0.697 0.04239 -0.208 0.599 0.012 0.882 0.016 16.444 0.304 0.548 -2.5 0.755 0.04005 -0.211 0.578 0.014 0.880 0.018 18.859 0.306 0.529 -2.0 0.812 0.03816 -0.214 0.550 0.017 0.883 0.023 21.285 0.307 0.514 -1.5 0.868 0.03651 -0.217 0.510 0.022 0.890 0.031 23.766 0.309 0.501 -1.0 0.921 0.03503 -0.221 0.436 0.030 0.908 0.044 26.300 0.311 0.490 -0.5 0.974 0.03349 -0.224 0.425 0.042 0.899 0.068 29.081 0.703 0.480 0.0 0.936 0.03172 -0.227 0.417 0.061 0.887 0.114 29.506 0.838 0.493 0.5 0.983 0.03462 -0.229 0.410 0.087 0.873 0.969 28.392 0.294 0.483 1.0 1.026 0.03599 -0.231 0.407 0.122 0.854 0.970 28.509 0.302 0.475 1.5 1.067 0.03720 -0.234 0.403 0.169 0.833 0.971 28.691 0.312 0.469 2.0 1.105 0.03938 -0.236 0.400 0.961 0.809 0.962 28.067 0.325 0.464 2.5 1.140 0.04120 -0.239 0.398 0.961 0.781 0.962 27.677 0.342 0.460 3.0 1.172 0.04318 -0.242 0.395 0.961 0.749 0.962 27.151 0.360 0.457 3.5 1.202 0.04552 -0.246 0.392 0.961 0.714 0.963 26.407 0.389 0.455 4.0 1.227 0.04833 -0.250 0.390 0.961 0.671 0.963 25.389 0.399 0.454 4.5 1.256 0.05096 -0.254 0.387 0.962 0.634 0.963 24.644 0.406 0.452 5.0 1.281 0.05423 -0.258 0.384 0.962 0.590 0.963 23.619 0.395 0.452 5.5 1.314 0.05725 -0.262 0.378 0.962 0.561 0.963 22.958 0.375 0.450 6.0 1.346 0.06042 -0.267 0.372 0.962 0.533 0.963 22.285 0.375 0.448 6.5 1.379 0.06362 -0.271 0.367 0.962 0.509 0.963 21.682 0.374 0.446 7.0 1.412 0.06709 -0.275 0.362 0.961 0.486 0.962 21.041 0.370 0.445 7.5 1.446 0.07035 -0.279 0.356 0.961 0.471 0.962 20.550 0.217 0.443 8.0 1.730 0.05678 -0.264 0.008 0.963 0.803 0.964 30.464 0.290 0.403 8.5 1.603 0.05879 -0.285 0.005 0.963 0.011 0.964 27.275 -0.010 0.428 9.0 1.638 0.06258 -0.288 0.004 0.963 0.007 0.964 26.169 0.358 0.426 9.5 1.666 0.06819 -0.292 0.003 0.963 0.005 0.964 24.425 0.382 0.425 10.0 1.689 0.07331 -0.295 0.002 0.963 0.004 0.964 23.035 0.418 0.425 10.5 1.706 0.08133 -0.298 0.002 0.963 0.004 0.964 20.977 0.470 0.425 11.0 1.720 0.08690 -0.302 0.002 0.963 0.003 0.964 19.791 0.543 0.425 11.5 1.729 0.09562 -0.305 0.001 0.963 0.002 0.964 18.087 0.737 0.426 12.0 1.734 0.10765 -0.309 0.001 0.963 0.002 0.964 16.107 1.746 0.428 12.5 1.734 0.12153 -0.312 0.001 0.963 0.002 0.964 14.268 -1.357 0.430 13.0 1.730 0.12623 -0.316 0.001 0.963 0.002 0.964 13.702 -0.237 0.432 13.5 1.720 0.14754 -0.319 0.001 0.963 0.002 0.964 11.657 -0.052 0.435 14.0 1.707 0.16207 -0.322 0.001 0.962 0.001 0.963 10.531 0.028 0.439 14.5 1.689 0.17491 -0.326 0.001 0.962 0.001 0.963 9.656 0.073 0.443 15.0 1.668 0.19169 -0.329 0.001 0.964 0.001 0.965 8.702 0.087 0.447 Name = naca-8410 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 -0.092 0.24539 -0.137 0.870 0.004 1.000 0.005 -0.375 0.380 -1.243 -14.5 -0.071 0.24038 -0.140 0.862 0.004 1.000 0.005 -0.297 0.374 -1.711 -14.0 -0.049 0.20422 -0.143 0.855 0.004 1.000 0.005 -0.238 0.364 -2.688 -13.5 -0.023 0.20944 -0.145 0.848 0.004 1.000 0.005 -0.112 0.237 -5.940 -13.0 -0.472 0.17894 -0.148 0.841 0.004 1.000 0.005 -2.637 0.236 -0.064 -12.5 -0.433 0.15532 -0.151 0.833 0.004 1.000 0.005 -2.785 0.318 -0.099 -12.0 -0.389 0.15828 -0.154 0.823 0.004 1.000 0.005 -2.460 0.313 -0.145 -11.5 -0.343 0.13102 -0.157 0.817 0.004 1.000 0.005 -2.615 0.309 -0.207 -11.0 -0.292 0.12268 -0.159 0.808 0.004 1.000 0.005 -2.383 0.305 -0.295 -10.5 -0.239 0.11303 -0.162 0.798 0.004 1.000 0.005 -2.114 0.303 -0.429 -10.0 -0.183 0.10542 -0.165 0.788 0.004 1.000 0.006 -1.732 0.301 -0.654 -9.5 -0.124 0.09204 -0.168 0.779 0.005 1.000 0.005 -1.346 0.299 -1.107 -9.0 -0.063 0.08639 -0.171 0.768 0.005 1.000 0.006 -0.729 0.298 -2.466 -8.5 -0.000 0.08212 -0.174 0.758 0.005 1.000 0.006 -0.005 0.297 0.250 -8.0 0.064 0.07579 -0.177 0.747 0.005 1.000 0.006 0.838 0.297 3.037 -7.5 0.128 0.06618 -0.180 0.736 0.005 1.000 0.007 1.938 0.296 1.653 -7.0 0.194 0.06264 -0.183 0.723 0.005 1.000 0.007 3.090 0.297 1.196 -6.5 0.259 0.05461 -0.186 0.712 0.006 1.000 0.007 4.737 0.297 0.969 -6.0 0.324 0.05218 -0.189 0.697 0.006 1.000 0.008 6.201 0.297 0.834 -5.5 0.388 0.04711 -0.192 0.683 0.007 1.000 0.009 8.237 0.298 0.745 -5.0 0.452 0.04453 -0.195 0.669 0.007 1.000 0.009 10.147 0.299 0.682 -4.5 0.515 0.03969 -0.198 0.654 0.008 1.000 0.011 12.967 0.300 0.636 -4.0 0.577 0.03747 -0.202 0.637 0.009 1.000 0.012 15.388 0.301 0.600 -3.5 0.637 0.03730 -0.205 0.619 0.010 1.000 0.014 17.090 0.302 0.571 -3.0 0.697 0.03275 -0.208 0.599 0.012 1.000 0.016 21.282 0.304 0.548 -2.5 0.755 0.03250 -0.211 0.578 0.014 1.000 0.020 23.235 0.305 0.529 -2.0 0.812 0.03005 -0.214 0.550 0.017 1.000 0.025 27.022 0.307 0.514 -1.5 0.868 0.02958 -0.217 0.510 0.022 1.000 0.035 29.332 0.309 0.501 -1.0 0.921 0.02757 -0.221 0.436 0.030 1.000 0.055 33.407 0.311 0.490 -0.5 0.974 0.02443 -0.224 0.425 0.042 1.000 0.126 39.855 0.314 0.480 0.0 1.026 0.02421 -0.227 0.417 0.061 1.000 0.971 42.376 0.291 0.472 0.5 1.086 0.02556 -0.229 0.410 0.087 1.000 0.971 42.470 0.288 0.460 1.0 1.101 0.02673 -0.230 0.407 0.122 0.949 0.972 41.178 0.329 0.459 1.5 1.133 0.02747 -0.232 0.403 0.169 0.918 0.972 41.253 0.299 0.455 2.0 1.181 0.02836 -0.234 0.400 0.961 0.906 0.962 41.634 0.293 0.448 2.5 1.227 0.02923 -0.236 0.398 0.961 0.893 0.962 41.988 0.298 0.442 3.0 1.272 0.03032 -0.239 0.395 0.961 0.879 0.962 41.949 0.307 0.438 3.5 1.313 0.03157 -0.241 0.392 0.961 0.861 0.963 41.594 0.320 0.434 4.0 1.351 0.03300 -0.244 0.390 0.961 0.839 0.963 40.921 0.331 0.431 4.5 1.388 0.03432 -0.247 0.387 0.962 0.817 0.963 40.430 0.348 0.428 5.0 1.419 0.03621 -0.251 0.384 0.962 0.789 0.963 39.188 0.358 0.427 5.5 1.454 0.03812 -0.254 0.378 0.962 0.766 0.963 38.139 0.365 0.425 6.0 1.484 0.04028 -0.258 0.372 0.962 0.740 0.963 36.835 0.390 0.424 6.5 1.511 0.04277 -0.262 0.367 0.962 0.711 0.963 35.332 0.425 0.424 7.0 1.533 0.04561 -0.267 0.362 0.961 0.678 0.962 33.616 0.448 0.424 7.5 1.556 0.04861 -0.271 0.356 0.961 0.649 0.962 32.022 0.223 0.424 8.0 1.777 0.04737 -0.260 0.008 0.963 0.851 0.964 37.507 0.220 0.396 8.5 1.801 0.04993 -0.264 0.005 0.963 0.832 0.964 36.078 0.057 0.397 9.0 1.632 0.05496 -0.288 0.004 0.963 0.010 0.964 29.692 0.052 0.427 9.5 1.663 0.06025 -0.292 0.003 0.963 0.006 0.964 27.598 0.374 0.425 10.0 1.686 0.06508 -0.295 0.002 0.963 0.005 0.964 25.905 0.410 0.425 10.5 1.705 0.06802 -0.298 0.002 0.963 0.004 0.964 25.068 0.464 0.425 11.0 1.718 0.07789 -0.302 0.002 0.963 0.004 0.964 22.052 0.543 0.426 11.5 1.728 0.08070 -0.305 0.001 0.963 0.003 0.964 21.418 0.702 0.427 12.0 1.733 0.09023 -0.309 0.001 0.963 0.002 0.964 19.206 1.736 0.428 12.5 1.733 0.10259 -0.312 0.001 0.963 0.002 0.964 16.893 -1.376 0.430 13.0 1.729 0.10839 -0.316 0.001 0.963 0.002 0.964 15.948 -0.271 0.433 13.5 1.720 0.11037 -0.319 0.001 0.963 0.002 0.964 15.582 -0.058 0.435 14.0 1.706 0.12783 -0.322 0.001 0.962 0.002 0.963 13.348 0.031 0.439 14.5 1.689 0.13745 -0.326 0.001 0.962 0.001 0.963 12.285 0.073 0.443 15.0 1.668 0.15459 -0.329 0.001 0.964 0.001 0.965 10.787 0.087 0.447 Name = naca-8410 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 -0.092 0.21398 -0.137 0.870 0.004 1.000 0.006 -0.429 0.382 -1.245 -14.5 -0.071 0.18084 -0.140 0.862 0.004 1.000 0.005 -0.395 0.374 -1.711 -14.0 -0.048 0.18265 -0.143 0.855 0.004 1.000 0.006 -0.265 0.364 -2.696 -13.5 -0.023 0.16919 -0.145 0.848 0.004 1.000 0.005 -0.139 0.237 -5.940 -13.0 -0.472 0.14635 -0.148 0.841 0.004 1.000 0.005 -3.224 0.236 -0.064 -12.5 -0.433 0.14393 -0.151 0.833 0.004 1.000 0.006 -3.005 0.318 -0.099 -12.0 -0.389 0.12987 -0.154 0.823 0.004 1.000 0.005 -2.999 0.313 -0.145 -11.5 -0.343 0.12217 -0.157 0.817 0.004 1.000 0.005 -2.804 0.309 -0.207 -11.0 -0.292 0.10415 -0.159 0.808 0.004 1.000 0.005 -2.807 0.305 -0.295 -10.5 -0.239 0.10631 -0.162 0.798 0.004 1.000 0.005 -2.247 0.303 -0.429 -10.0 -0.183 0.09348 -0.165 0.788 0.004 1.000 0.006 -1.954 0.301 -0.654 -9.5 -0.124 0.08578 -0.168 0.779 0.005 1.000 0.006 -1.444 0.299 -1.107 -9.0 -0.063 0.07454 -0.171 0.768 0.005 1.000 0.006 -0.845 0.298 -2.466 -8.5 -0.000 0.07087 -0.174 0.758 0.005 1.000 0.006 -0.005 0.297 0.250 -8.0 0.064 0.06503 -0.177 0.747 0.005 1.000 0.006 0.977 0.296 3.037 -7.5 0.128 0.05941 -0.180 0.736 0.005 1.000 0.007 2.159 0.296 1.653 -7.0 0.194 0.05316 -0.183 0.723 0.005 1.000 0.007 3.641 0.296 1.196 -6.5 0.259 0.05152 -0.186 0.712 0.006 1.000 0.008 5.021 0.297 0.969 -6.0 0.324 0.04612 -0.189 0.697 0.006 1.000 0.008 7.016 0.298 0.834 -5.5 0.388 0.04363 -0.192 0.683 0.007 1.000 0.009 8.892 0.298 0.745 -5.0 0.452 0.03927 -0.195 0.669 0.007 1.000 0.009 11.505 0.299 0.682 -4.5 0.515 0.03615 -0.198 0.654 0.008 1.000 0.011 14.238 0.300 0.636 -4.0 0.577 0.03475 -0.202 0.637 0.009 1.000 0.012 16.593 0.301 0.600 -3.5 0.637 0.03285 -0.205 0.619 0.010 1.000 0.014 19.404 0.302 0.571 -3.0 0.697 0.02986 -0.208 0.599 0.012 1.000 0.017 23.339 0.304 0.548 -2.5 0.755 0.02846 -0.211 0.578 0.014 1.000 0.021 26.534 0.305 0.529 -2.0 0.812 0.02745 -0.214 0.550 0.017 1.000 0.027 29.580 0.307 0.514 -1.5 0.867 0.02591 -0.217 0.510 0.022 1.000 0.043 33.482 0.308 0.501 -1.0 0.921 0.02250 -0.221 0.436 0.030 1.000 0.096 40.912 0.338 0.490 -0.5 0.966 0.02210 -0.226 0.425 0.042 1.000 0.971 43.712 0.315 0.484 0.0 1.026 0.02068 -0.227 0.417 0.061 1.000 0.972 49.611 0.270 0.472 0.5 1.086 0.02128 -0.229 0.410 0.087 1.000 0.973 51.025 0.268 0.460 1.0 1.145 0.02134 -0.230 0.407 0.122 1.000 0.973 53.675 0.269 0.450 1.5 1.205 0.02286 -0.231 0.403 0.169 1.000 0.973 52.701 0.269 0.441 2.0 1.264 0.02253 -0.232 0.400 0.961 1.000 0.962 56.121 0.297 0.433 2.5 1.282 0.02460 -0.234 0.398 0.961 0.956 0.962 52.140 0.370 0.433 3.0 1.308 0.02542 -0.237 0.395 0.961 0.921 0.962 51.444 0.316 0.431 3.5 1.355 0.02634 -0.239 0.392 0.961 0.909 0.963 51.457 0.298 0.427 4.0 1.401 0.02728 -0.242 0.390 0.961 0.896 0.963 51.343 0.303 0.422 4.5 1.446 0.02805 -0.244 0.387 0.962 0.884 0.963 51.544 0.312 0.419 5.0 1.486 0.02933 -0.247 0.384 0.962 0.867 0.963 50.649 0.320 0.416 5.5 1.527 0.03062 -0.250 0.378 0.962 0.852 0.963 49.885 0.326 0.413 6.0 1.565 0.03217 -0.253 0.372 0.962 0.834 0.963 48.637 0.342 0.412 6.5 1.599 0.03376 -0.256 0.367 0.962 0.816 0.963 47.359 0.365 0.410 7.0 1.628 0.03566 -0.260 0.362 0.961 0.793 0.962 45.653 0.388 0.410 7.5 1.655 0.03775 -0.264 0.356 0.961 0.771 0.962 43.848 0.237 0.410 8.0 1.806 0.04245 -0.258 0.008 0.963 0.880 0.964 42.540 0.235 0.393 8.5 1.832 0.04473 -0.261 0.005 0.963 0.862 0.964 40.950 0.417 0.393 9.0 1.852 0.04734 -0.265 0.004 0.963 0.841 0.964 39.120 0.075 0.393 9.5 1.659 0.05605 -0.292 0.003 0.963 0.008 0.964 29.592 0.074 0.426 10.0 1.684 0.05948 -0.295 0.002 0.963 0.006 0.964 28.313 0.401 0.425 10.5 1.703 0.06333 -0.298 0.002 0.963 0.005 0.964 26.895 0.457 0.425 11.0 1.717 0.06960 -0.302 0.002 0.963 0.004 0.964 24.666 0.532 0.426 11.5 1.727 0.07414 -0.305 0.001 0.963 0.003 0.964 23.299 0.703 0.427 12.0 1.732 0.08266 -0.309 0.001 0.963 0.003 0.964 20.951 1.470 0.428 12.5 1.733 0.08701 -0.312 0.001 0.963 0.002 0.964 19.918 -1.859 0.430 13.0 1.729 0.09286 -0.316 0.001 0.963 0.002 0.964 18.616 -0.239 0.433 13.5 1.719 0.10297 -0.319 0.001 0.963 0.002 0.964 16.694 -0.051 0.436 14.0 1.706 0.11313 -0.322 0.001 0.962 0.002 0.963 15.079 0.028 0.439 14.5 1.688 0.12141 -0.326 0.001 0.962 0.002 0.963 13.903 0.073 0.443 15.0 1.667 0.13913 -0.329 0.001 0.964 0.001 0.965 11.982 0.087 0.448 Name = naca-8410 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 -0.092 0.18545 -0.137 0.870 0.004 1.000 0.006 -0.494 0.382 -1.246 -14.5 -0.071 0.17927 -0.140 0.862 0.004 1.000 0.006 -0.397 0.374 -1.714 -14.0 -0.048 0.17122 -0.143 0.855 0.004 1.000 0.006 -0.282 0.364 -2.705 -13.5 -0.023 0.14654 -0.145 0.848 0.004 1.000 0.005 -0.160 0.237 -5.940 -13.0 -0.472 0.14150 -0.148 0.841 0.004 1.000 0.006 -3.335 0.236 -0.064 -12.5 -0.433 0.12453 -0.151 0.833 0.004 1.000 0.006 -3.473 0.318 -0.099 -12.0 -0.389 0.11997 -0.154 0.823 0.004 1.000 0.005 -3.246 0.313 -0.145 -11.5 -0.343 0.10640 -0.157 0.817 0.004 1.000 0.005 -3.220 0.308 -0.207 -11.0 -0.292 0.10301 -0.159 0.808 0.004 1.000 0.006 -2.838 0.305 -0.295 -10.5 -0.239 0.09441 -0.162 0.798 0.004 1.000 0.005 -2.531 0.303 -0.429 -10.0 -0.183 0.08324 -0.165 0.788 0.004 1.000 0.006 -2.194 0.301 -0.654 -9.5 -0.124 0.07718 -0.168 0.779 0.005 1.000 0.006 -1.605 0.299 -1.107 -9.0 -0.063 0.07243 -0.171 0.768 0.005 1.000 0.006 -0.869 0.298 -2.466 -8.5 -0.000 0.06822 -0.174 0.758 0.005 1.000 0.006 -0.005 0.297 0.250 -8.0 0.064 0.05950 -0.177 0.747 0.005 1.000 0.006 1.067 0.296 3.037 -7.5 0.128 0.05630 -0.180 0.736 0.005 1.000 0.007 2.279 0.296 1.653 -7.0 0.194 0.05140 -0.183 0.723 0.005 1.000 0.007 3.765 0.297 1.196 -6.5 0.259 0.04703 -0.186 0.712 0.006 1.000 0.008 5.501 0.297 0.969 -6.0 0.324 0.04466 -0.189 0.697 0.006 1.000 0.009 7.245 0.298 0.834 -5.5 0.388 0.04006 -0.192 0.683 0.007 1.000 0.009 9.686 0.298 0.745 -5.0 0.452 0.03673 -0.195 0.669 0.007 1.000 0.009 12.300 0.299 0.682 -4.5 0.515 0.03456 -0.198 0.654 0.008 1.000 0.012 14.893 0.300 0.636 -4.0 0.577 0.03251 -0.202 0.637 0.009 1.000 0.013 17.736 0.301 0.600 -3.5 0.637 0.03031 -0.205 0.619 0.010 1.000 0.015 21.027 0.302 0.571 -3.0 0.697 0.02785 -0.208 0.599 0.012 1.000 0.018 25.027 0.304 0.548 -2.5 0.755 0.02661 -0.211 0.578 0.014 1.000 0.022 28.377 0.305 0.529 -2.0 0.812 0.02485 -0.214 0.550 0.017 1.000 0.031 32.667 0.306 0.514 -1.5 0.867 0.02349 -0.217 0.510 0.022 1.000 0.062 36.909 0.363 0.501 -1.0 0.906 0.01884 -0.225 0.436 0.030 1.000 0.971 48.089 0.339 0.498 -0.5 0.966 0.02003 -0.226 0.425 0.042 1.000 0.972 48.240 0.271 0.484 0.0 1.026 0.01971 -0.227 0.417 0.061 1.000 0.973 52.062 0.270 0.472 0.5 1.086 0.02008 -0.229 0.410 0.087 1.000 0.973 54.073 0.268 0.460 1.0 1.145 0.02086 -0.230 0.407 0.122 1.000 0.974 54.896 0.269 0.450 1.5 1.205 0.01996 -0.231 0.403 0.169 1.000 0.974 60.363 0.269 0.441 2.0 1.264 0.02047 -0.232 0.400 0.961 1.000 0.962 61.747 0.269 0.433 2.5 1.323 0.02037 -0.233 0.398 0.961 1.000 0.962 64.975 0.269 0.426 3.0 1.383 0.02227 -0.234 0.395 0.961 1.000 0.962 62.094 0.270 0.419 3.5 1.442 0.02283 -0.235 0.392 0.961 1.000 0.963 63.144 0.379 0.413 4.0 1.429 0.02407 -0.240 0.390 0.961 0.927 0.963 59.352 0.479 0.418 4.5 1.473 0.02482 -0.242 0.387 0.962 0.913 0.963 59.336 0.303 0.415 5.0 1.518 0.02573 -0.245 0.384 0.962 0.902 0.963 59.010 0.303 0.411 5.5 1.565 0.02690 -0.247 0.378 0.962 0.891 0.963 58.173 0.308 0.408 6.0 1.606 0.02788 -0.250 0.372 0.962 0.879 0.963 57.623 0.320 0.406 6.5 1.645 0.02919 -0.253 0.367 0.962 0.865 0.963 56.369 0.333 0.404 7.0 1.680 0.03060 -0.256 0.362 0.961 0.849 0.962 54.904 0.350 0.402 7.5 1.712 0.03217 -0.260 0.356 0.961 0.832 0.962 53.221 0.249 0.402 8.0 1.827 0.03947 -0.256 0.008 0.963 0.900 0.964 46.287 0.248 0.390 8.5 1.855 0.04160 -0.259 0.005 0.963 0.885 0.964 44.598 0.396 0.390 9.0 1.876 0.04402 -0.263 0.004 0.963 0.865 0.964 42.630 0.089 0.390 9.5 1.653 0.05386 -0.292 0.003 0.963 0.011 0.964 30.696 0.087 0.426 10.0 1.681 0.05706 -0.295 0.002 0.963 0.007 0.964 29.467 0.389 0.426 10.5 1.701 0.06021 -0.298 0.002 0.963 0.005 0.964 28.257 0.452 0.425 11.0 1.715 0.06597 -0.302 0.002 0.963 0.005 0.964 25.998 0.521 0.426 11.5 1.726 0.07011 -0.305 0.001 0.963 0.003 0.964 24.623 0.678 0.427 12.0 1.731 0.07806 -0.309 0.001 0.963 0.003 0.964 22.173 1.464 0.428 12.5 1.732 0.08315 -0.312 0.001 0.963 0.002 0.964 20.830 -1.891 0.430 13.0 1.728 0.08949 -0.316 0.001 0.963 0.002 0.964 19.306 -0.241 0.433 13.5 1.718 0.09860 -0.319 0.001 0.963 0.002 0.964 17.425 -0.057 0.436 14.0 1.705 0.10437 -0.322 0.001 0.962 0.002 0.963 16.340 0.025 0.439 14.5 1.688 0.11191 -0.326 0.001 0.962 0.002 0.963 15.079 0.071 0.443 15.0 1.667 0.12173 -0.329 0.001 0.964 0.001 0.965 13.694 0.083 0.448