Name = Coanda 2 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 -0.414 0.36308 0.045 1.000 0.002 1.000 0.003 -1.139 -0.329 0.358 -14.5 -0.418 0.31308 0.042 1.000 0.002 1.000 0.003 -1.336 -0.503 0.350 -14.0 -0.421 0.28219 0.039 1.000 0.002 1.000 0.003 -1.491 -1.673 0.344 -13.5 -0.421 0.25485 0.037 1.000 0.002 1.000 0.003 -1.652 3.167 0.337 -13.0 -0.419 0.22535 0.034 1.000 0.002 1.000 0.003 -1.858 1.049 0.331 -12.5 -0.414 0.18774 0.031 1.000 0.002 1.000 0.003 -2.206 0.692 0.325 -12.0 -0.406 0.16649 0.028 1.000 0.002 1.000 0.003 -2.441 0.551 0.320 -11.5 -0.396 0.15607 0.026 1.000 0.002 1.000 0.003 -2.536 0.482 0.315 -11.0 -0.382 0.13322 0.023 1.000 0.002 1.000 0.003 -2.870 0.439 0.310 -10.5 -0.366 0.11617 0.020 1.000 0.002 1.000 0.003 -3.151 0.412 0.305 -10.0 -0.347 0.10141 0.017 1.000 0.002 1.000 0.003 -3.422 0.392 0.299 -9.5 -0.325 0.08981 0.014 0.895 0.002 1.000 0.004 -3.623 0.377 0.294 -9.0 -0.301 0.07829 0.011 0.884 0.003 1.000 0.004 -3.848 0.366 0.288 -8.5 -0.275 0.07096 0.008 0.879 0.003 1.000 0.005 -3.871 0.357 0.281 -8.0 -0.246 0.06185 0.005 0.874 0.003 1.000 0.005 -3.981 0.350 0.272 -7.5 -0.216 0.05525 0.002 0.868 0.004 1.000 0.006 -3.902 0.344 0.262 -7.0 -0.183 0.05174 -0.001 0.858 0.005 1.000 0.008 -3.533 0.339 0.247 -6.5 -0.148 0.04677 -0.004 0.852 0.007 1.000 0.010 -3.163 0.316 0.226 -6.0 -0.109 0.04343 -0.005 0.845 0.010 1.000 0.067 -2.514 0.317 0.201 -5.5 -0.070 0.04447 -0.009 0.839 0.055 1.000 0.058 -1.574 0.340 0.125 -5.0 -0.035 0.04099 -0.012 0.836 0.055 1.000 0.058 -0.859 0.343 -0.091 -4.5 -0.000 0.03846 -0.015 0.830 0.056 1.000 0.059 -0.000 0.189 0.250 -4.0 -0.142 0.03509 -0.019 0.824 0.056 1.000 0.059 -4.037 0.170 0.119 -3.5 -0.082 0.03204 -0.022 0.821 0.056 1.000 0.060 -2.573 0.306 -0.015 -3.0 -0.024 0.03048 -0.025 0.815 0.057 1.000 0.060 -0.784 0.307 -0.804 -2.5 0.034 0.02828 -0.029 0.809 0.057 1.000 0.061 1.198 0.309 1.092 -2.0 0.091 0.02674 -0.032 0.806 0.055 1.000 0.059 3.398 0.310 0.601 -1.5 0.147 0.02176 -0.035 0.794 0.058 1.000 0.062 6.758 0.311 0.490 -1.0 0.202 0.02031 -0.039 0.779 0.056 1.000 0.060 9.966 0.313 0.441 -0.5 0.257 0.01873 -0.042 0.764 0.056 1.000 0.061 13.717 0.314 0.414 0.0 0.311 0.01841 -0.046 0.594 0.056 1.000 0.062 16.875 0.292 0.397 0.5 0.366 0.01834 -0.047 0.394 0.059 1.000 0.064 19.976 0.271 0.378 1.0 0.422 0.01832 -0.048 0.370 0.059 1.000 0.065 23.044 0.272 0.364 1.5 0.478 0.01625 -0.049 0.348 0.060 1.000 0.066 29.408 0.272 0.353 2.0 0.534 0.01679 -0.050 0.327 0.061 1.000 0.068 31.800 0.272 0.345 2.5 0.590 0.01625 -0.052 0.306 0.063 1.000 0.071 36.276 0.273 0.338 3.0 0.645 0.01684 -0.053 0.282 0.065 1.000 0.074 38.327 0.273 0.332 3.5 0.701 0.01695 -0.054 0.258 0.069 1.000 0.081 41.341 0.273 0.327 4.0 0.757 0.01877 -0.056 0.209 0.073 1.000 0.086 40.295 0.274 0.323 4.5 0.812 0.01887 -0.057 0.141 0.081 1.000 0.097 43.027 0.274 0.320 5.0 0.867 0.01738 -0.058 0.011 0.089 1.000 0.103 49.875 0.078 0.317 5.5 0.656 0.03362 -0.084 0.007 0.095 0.010 0.976 19.506 0.084 0.378 6.0 0.692 0.04020 -0.087 0.005 0.955 0.007 0.956 17.223 0.350 0.376 6.5 0.726 0.04418 -0.091 0.004 0.955 0.006 0.956 16.434 0.359 0.375 7.0 0.757 0.04784 -0.094 0.003 0.957 0.005 0.959 15.822 0.370 0.375 7.5 0.785 0.05367 -0.098 0.003 0.957 0.004 0.959 14.634 0.382 0.375 8.0 0.811 0.05986 -0.101 0.002 0.960 0.004 0.961 13.551 0.397 0.375 8.5 0.834 0.06875 -0.105 0.002 0.960 0.003 0.961 12.130 0.419 0.376 9.0 0.854 0.07542 -0.109 0.002 0.960 0.003 0.961 11.318 0.451 0.377 9.5 0.870 0.08844 -0.112 0.002 0.960 0.003 0.961 9.834 0.504 0.379 10.0 0.882 0.10090 -0.116 0.002 0.955 0.003 0.956 8.742 0.596 0.381 10.5 0.891 0.11528 -0.119 0.002 0.955 0.003 0.956 7.725 0.808 0.384 11.0 0.895 0.12095 -0.123 0.001 0.960 0.002 0.961 7.401 1.792 0.388 11.5 0.895 0.14797 -0.127 0.001 0.960 0.002 0.961 6.050 -1.797 0.392 12.0 0.892 0.16666 -0.130 0.001 0.960 0.002 0.961 5.349 -0.366 0.396 12.5 0.883 0.17739 -0.134 0.002 0.960 0.003 0.961 4.980 -0.127 0.402 13.0 0.872 0.19794 -0.138 0.002 0.960 0.003 0.961 4.406 -0.029 0.408 13.5 0.857 0.22315 -0.141 0.002 0.960 0.003 0.961 3.841 0.026 0.415 14.0 0.839 0.25017 -0.145 0.002 0.959 0.003 0.961 3.355 0.059 0.423 14.5 0.819 0.27872 -0.149 0.002 0.959 0.003 0.961 2.938 0.080 0.432 15.0 0.796 0.31490 -0.152 0.002 0.954 0.003 0.956 2.528 0.089 0.441 Name = Coanda 2 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 -0.414 0.26295 0.045 1.000 0.002 1.000 0.003 -1.573 -0.330 0.358 -14.5 -0.418 0.23219 0.042 1.000 0.002 1.000 0.003 -1.801 -0.504 0.350 -14.0 -0.421 0.20806 0.039 1.000 0.002 1.000 0.003 -2.021 -1.683 0.344 -13.5 -0.421 0.19204 0.037 1.000 0.002 1.000 0.003 -2.191 3.333 0.337 -13.0 -0.419 0.16032 0.034 1.000 0.002 1.000 0.003 -2.612 1.047 0.331 -12.5 -0.414 0.14591 0.031 1.000 0.002 1.000 0.003 -2.837 0.687 0.325 -12.0 -0.406 0.12845 0.028 1.000 0.002 1.000 0.003 -3.163 0.551 0.320 -11.5 -0.396 0.12067 0.026 1.000 0.002 1.000 0.003 -3.279 0.482 0.315 -11.0 -0.382 0.10282 0.023 1.000 0.002 1.000 0.003 -3.717 0.439 0.310 -10.5 -0.366 0.09053 0.020 1.000 0.002 1.000 0.003 -4.041 0.411 0.305 -10.0 -0.347 0.08340 0.017 1.000 0.002 1.000 0.004 -4.158 0.391 0.300 -9.5 -0.325 0.07364 0.014 0.895 0.002 1.000 0.004 -4.414 0.377 0.294 -9.0 -0.301 0.06453 0.011 0.884 0.003 1.000 0.004 -4.663 0.366 0.288 -8.5 -0.274 0.05802 0.008 0.879 0.003 1.000 0.005 -4.729 0.357 0.281 -8.0 -0.246 0.05223 0.005 0.874 0.003 1.000 0.006 -4.704 0.350 0.272 -7.5 -0.215 0.04622 0.003 0.868 0.004 1.000 0.007 -4.652 0.344 0.262 -7.0 -0.182 0.04352 -0.000 0.858 0.005 1.000 0.009 -4.183 0.338 0.247 -6.5 -0.147 0.03984 -0.003 0.852 0.007 1.000 0.011 -3.685 0.318 0.226 -6.0 -0.111 0.03713 -0.005 0.845 0.010 1.000 0.072 -2.994 0.319 0.203 -5.5 -0.070 0.03726 -0.009 0.839 0.055 1.000 0.058 -1.883 0.339 0.125 -5.0 -0.036 0.03414 -0.012 0.836 0.055 1.000 0.059 -1.040 0.343 -0.087 -4.5 -0.000 0.03149 -0.015 0.830 0.056 1.000 0.059 -0.000 0.188 0.250 -4.0 -0.142 0.02877 -0.019 0.824 0.056 1.000 0.059 -4.924 0.170 0.119 -3.5 -0.082 0.02664 -0.022 0.821 0.056 1.000 0.060 -3.094 0.306 -0.015 -3.0 -0.024 0.02452 -0.025 0.815 0.057 1.000 0.060 -0.974 0.307 -0.804 -2.5 0.034 0.02282 -0.029 0.809 0.057 1.000 0.062 1.485 0.309 1.092 -2.0 0.091 0.02126 -0.032 0.806 0.055 1.000 0.060 4.275 0.310 0.601 -1.5 0.147 0.01707 -0.035 0.794 0.058 1.000 0.063 8.612 0.311 0.490 -1.0 0.202 0.01539 -0.039 0.779 0.056 1.000 0.061 13.150 0.313 0.441 -0.5 0.257 0.01431 -0.042 0.764 0.056 1.000 0.062 17.963 0.314 0.414 0.0 0.311 0.01278 -0.046 0.594 0.056 1.000 0.063 24.312 0.292 0.397 0.5 0.366 0.01384 -0.047 0.394 0.059 1.000 0.065 26.488 0.271 0.378 1.0 0.422 0.01368 -0.048 0.370 0.059 1.000 0.066 30.860 0.272 0.364 1.5 0.478 0.01202 -0.049 0.348 0.060 1.000 0.068 39.765 0.272 0.353 2.0 0.534 0.01195 -0.050 0.327 0.061 1.000 0.069 44.685 0.272 0.345 2.5 0.590 0.01312 -0.052 0.306 0.063 1.000 0.073 44.927 0.273 0.338 3.0 0.645 0.01312 -0.053 0.282 0.065 1.000 0.078 49.183 0.273 0.332 3.5 0.701 0.01359 -0.054 0.258 0.069 1.000 0.086 51.589 0.273 0.327 4.0 0.757 0.01388 -0.056 0.209 0.073 1.000 0.092 54.506 0.274 0.323 4.5 0.812 0.01462 -0.057 0.141 0.081 1.000 0.100 55.542 0.274 0.320 5.0 0.867 0.01814 -0.058 0.011 0.089 1.000 0.977 47.783 0.079 0.317 5.5 0.655 0.03093 -0.084 0.007 0.095 0.010 0.977 21.169 0.084 0.378 6.0 0.692 0.03555 -0.087 0.005 0.955 0.008 0.956 19.453 0.349 0.376 6.5 0.725 0.03918 -0.091 0.004 0.955 0.006 0.956 18.510 0.359 0.375 7.0 0.756 0.04195 -0.094 0.003 0.957 0.005 0.959 18.031 0.369 0.375 7.5 0.785 0.04686 -0.098 0.003 0.957 0.004 0.959 16.748 0.381 0.375 8.0 0.811 0.05064 -0.101 0.002 0.960 0.004 0.961 16.013 0.396 0.375 8.5 0.834 0.05765 -0.105 0.002 0.960 0.003 0.961 14.461 0.419 0.376 9.0 0.853 0.06277 -0.109 0.002 0.960 0.003 0.961 13.595 0.451 0.377 9.5 0.869 0.07316 -0.112 0.002 0.960 0.003 0.961 11.885 0.504 0.379 10.0 0.882 0.08260 -0.116 0.002 0.955 0.003 0.956 10.676 0.593 0.381 10.5 0.891 0.08883 -0.119 0.002 0.955 0.003 0.956 10.025 0.807 0.384 11.0 0.895 0.09900 -0.123 0.001 0.960 0.003 0.961 9.040 1.792 0.388 11.5 0.895 0.11080 -0.127 0.001 0.960 0.002 0.961 8.080 -1.910 0.392 12.0 0.892 0.12346 -0.130 0.001 0.960 0.002 0.961 7.221 -0.359 0.396 12.5 0.883 0.14020 -0.134 0.002 0.960 0.003 0.961 6.300 -0.125 0.402 13.0 0.872 0.15683 -0.138 0.002 0.960 0.003 0.961 5.560 -0.030 0.408 13.5 0.857 0.17276 -0.141 0.002 0.960 0.003 0.961 4.961 0.026 0.415 14.0 0.839 0.18935 -0.145 0.002 0.959 0.003 0.961 4.432 0.059 0.423 14.5 0.819 0.21185 -0.149 0.002 0.959 0.003 0.961 3.864 0.080 0.432 15.0 0.796 0.25389 -0.152 0.002 0.954 0.003 0.956 3.134 0.089 0.442 Name = Coanda 2 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 -0.414 0.21991 0.045 1.000 0.002 1.000 0.004 -1.880 -0.330 0.358 -14.5 -0.418 0.19738 0.042 1.000 0.002 1.000 0.004 -2.118 -0.506 0.350 -14.0 -0.420 0.17639 0.039 1.000 0.002 1.000 0.004 -2.384 -1.693 0.344 -13.5 -0.421 0.16528 0.037 1.000 0.002 1.000 0.003 -2.546 3.308 0.337 -13.0 -0.419 0.14122 0.034 1.000 0.002 1.000 0.003 -2.965 1.045 0.331 -12.5 -0.414 0.12823 0.031 1.000 0.002 1.000 0.003 -3.228 0.686 0.325 -12.0 -0.406 0.11220 0.028 1.000 0.002 1.000 0.003 -3.620 0.551 0.320 -11.5 -0.396 0.10556 0.026 1.000 0.002 1.000 0.003 -3.747 0.480 0.315 -11.0 -0.382 0.09447 0.023 1.000 0.002 1.000 0.004 -4.042 0.438 0.310 -10.5 -0.366 0.08296 0.020 1.000 0.002 1.000 0.004 -4.406 0.412 0.305 -10.0 -0.347 0.07296 0.017 1.000 0.002 1.000 0.004 -4.751 0.391 0.300 -9.5 -0.325 0.06668 0.014 0.895 0.002 1.000 0.004 -4.869 0.376 0.294 -9.0 -0.301 0.05850 0.011 0.884 0.003 1.000 0.005 -5.138 0.366 0.288 -8.5 -0.274 0.05229 0.008 0.879 0.003 1.000 0.005 -5.241 0.357 0.281 -8.0 -0.245 0.04708 0.005 0.874 0.003 1.000 0.006 -5.210 0.350 0.272 -7.5 -0.214 0.04241 0.003 0.868 0.004 1.000 0.007 -5.056 0.343 0.262 -7.0 -0.181 0.04018 -0.000 0.858 0.005 1.000 0.009 -4.512 0.337 0.247 -6.5 -0.146 0.03678 -0.003 0.852 0.007 1.000 0.012 -3.964 0.319 0.226 -6.0 -0.112 0.03438 -0.005 0.845 0.010 1.000 0.074 -3.263 0.320 0.203 -5.5 -0.070 0.03356 -0.009 0.839 0.055 1.000 0.058 -2.090 0.338 0.125 -5.0 -0.036 0.03070 -0.012 0.836 0.055 1.000 0.059 -1.157 0.343 -0.087 -4.5 -0.000 0.02832 -0.015 0.830 0.056 1.000 0.059 -0.001 0.188 0.250 -4.0 -0.142 0.02635 -0.019 0.824 0.056 1.000 0.060 -5.377 0.170 0.119 -3.5 -0.082 0.02375 -0.022 0.821 0.056 1.000 0.060 -3.471 0.306 -0.015 -3.0 -0.024 0.02211 -0.025 0.815 0.057 1.000 0.061 -1.080 0.307 -0.803 -2.5 0.034 0.01998 -0.029 0.809 0.057 1.000 0.062 1.696 0.309 1.092 -2.0 0.091 0.01843 -0.032 0.806 0.055 1.000 0.060 4.931 0.310 0.601 -1.5 0.147 0.01523 -0.035 0.794 0.058 1.000 0.063 9.653 0.311 0.490 -1.0 0.202 0.01365 -0.039 0.779 0.056 1.000 0.062 14.826 0.313 0.441 -0.5 0.257 0.01180 -0.042 0.764 0.056 1.000 0.063 21.774 0.314 0.414 0.0 0.311 0.01119 -0.046 0.594 0.056 1.000 0.064 27.768 0.292 0.397 0.5 0.366 0.01155 -0.047 0.394 0.059 1.000 0.065 31.732 0.271 0.378 1.0 0.422 0.01223 -0.048 0.370 0.059 1.000 0.067 34.531 0.272 0.364 1.5 0.478 0.01058 -0.049 0.348 0.060 1.000 0.068 45.177 0.272 0.353 2.0 0.534 0.01069 -0.050 0.327 0.061 1.000 0.071 49.953 0.272 0.345 2.5 0.590 0.01070 -0.052 0.306 0.063 1.000 0.074 55.090 0.273 0.338 3.0 0.645 0.01158 -0.053 0.282 0.065 1.000 0.081 55.700 0.273 0.332 3.5 0.701 0.01184 -0.054 0.258 0.069 1.000 0.089 59.178 0.273 0.327 4.0 0.757 0.01230 -0.056 0.209 0.073 1.000 0.097 61.490 0.274 0.323 4.5 0.812 0.01571 -0.057 0.141 0.081 1.000 0.978 51.664 0.274 0.320 5.0 0.867 0.01619 -0.058 0.011 0.089 1.000 0.978 53.525 0.080 0.317 5.5 0.654 0.02966 -0.084 0.007 0.095 0.011 0.979 22.052 0.085 0.378 6.0 0.691 0.03332 -0.087 0.005 0.955 0.008 0.956 20.743 0.349 0.376 6.5 0.725 0.03671 -0.091 0.004 0.955 0.006 0.956 19.746 0.359 0.375 7.0 0.756 0.03944 -0.094 0.003 0.957 0.005 0.959 19.166 0.369 0.375 7.5 0.785 0.04309 -0.098 0.003 0.957 0.005 0.959 18.208 0.381 0.375 8.0 0.810 0.04771 -0.101 0.002 0.960 0.004 0.961 16.986 0.396 0.375 8.5 0.833 0.05287 -0.105 0.002 0.960 0.004 0.961 15.764 0.419 0.376 9.0 0.853 0.05930 -0.109 0.002 0.960 0.003 0.961 14.383 0.450 0.377 9.5 0.869 0.06399 -0.112 0.002 0.960 0.003 0.961 13.587 0.502 0.379 10.0 0.882 0.07488 -0.116 0.002 0.955 0.003 0.956 11.775 0.596 0.381 10.5 0.890 0.08123 -0.119 0.002 0.955 0.003 0.956 10.961 0.807 0.384 11.0 0.895 0.08989 -0.123 0.001 0.960 0.003 0.961 9.953 1.786 0.388 11.5 0.895 0.10111 -0.127 0.001 0.960 0.003 0.961 8.853 -1.922 0.392 12.0 0.891 0.11214 -0.130 0.001 0.960 0.003 0.961 7.948 -0.360 0.396 12.5 0.883 0.12474 -0.134 0.002 0.960 0.003 0.961 7.080 -0.125 0.402 13.0 0.872 0.13966 -0.138 0.002 0.960 0.003 0.961 6.242 -0.030 0.408 13.5 0.857 0.15140 -0.141 0.002 0.960 0.003 0.961 5.660 0.027 0.415 14.0 0.839 0.17575 -0.145 0.002 0.959 0.003 0.961 4.773 0.059 0.423 14.5 0.819 0.18311 -0.149 0.002 0.959 0.003 0.961 4.470 0.080 0.432 15.0 0.796 0.21381 -0.152 0.002 0.954 0.004 0.956 3.721 0.089 0.442 Name = Coanda 2 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 -0.413 0.20678 0.045 1.000 0.002 1.000 0.004 -1.999 -0.323 0.358 -14.5 -0.418 0.17673 0.042 1.000 0.002 1.000 0.004 -2.365 -0.500 0.350 -14.0 -0.420 0.15771 0.039 1.000 0.002 1.000 0.004 -2.665 -1.704 0.344 -13.5 -0.421 0.14961 0.037 1.000 0.002 1.000 0.004 -2.812 3.284 0.337 -13.0 -0.419 0.13015 0.034 1.000 0.002 1.000 0.003 -3.216 1.043 0.331 -12.5 -0.414 0.11808 0.031 1.000 0.002 1.000 0.003 -3.504 0.680 0.325 -12.0 -0.406 0.10878 0.028 1.000 0.002 1.000 0.003 -3.731 0.550 0.320 -11.5 -0.395 0.09670 0.026 1.000 0.002 1.000 0.003 -4.089 0.482 0.315 -11.0 -0.382 0.08575 0.023 1.000 0.002 1.000 0.004 -4.452 0.438 0.310 -10.5 -0.365 0.07562 0.020 1.000 0.002 1.000 0.004 -4.832 0.411 0.305 -10.0 -0.346 0.06911 0.017 1.000 0.002 1.000 0.004 -5.011 0.391 0.300 -9.5 -0.325 0.06076 0.014 0.895 0.002 1.000 0.005 -5.341 0.376 0.294 -9.0 -0.300 0.05515 0.011 0.884 0.003 1.000 0.005 -5.444 0.365 0.288 -8.5 -0.273 0.04992 0.008 0.879 0.003 1.000 0.006 -5.479 0.356 0.281 -8.0 -0.245 0.04478 0.006 0.874 0.003 1.000 0.007 -5.466 0.349 0.273 -7.5 -0.214 0.04053 0.003 0.868 0.004 1.000 0.008 -5.273 0.343 0.262 -7.0 -0.181 0.03794 -0.000 0.858 0.005 1.000 0.010 -4.758 0.317 0.247 -6.5 -0.146 0.03490 -0.002 0.852 0.007 1.000 0.072 -4.174 0.320 0.236 -6.0 -0.113 0.03254 -0.005 0.845 0.010 1.000 0.075 -3.467 0.339 0.204 -5.5 -0.070 0.03147 -0.009 0.839 0.055 1.000 0.058 -2.234 0.338 0.126 -5.0 -0.036 0.02945 -0.012 0.836 0.055 1.000 0.060 -1.216 0.343 -0.084 -4.5 -0.000 0.02711 -0.015 0.830 0.056 1.000 0.060 -0.011 0.188 0.250 -4.0 -0.142 0.02468 -0.019 0.824 0.056 1.000 0.060 -5.739 0.170 0.119 -3.5 -0.082 0.02254 -0.022 0.821 0.056 1.000 0.061 -3.657 0.306 -0.015 -3.0 -0.024 0.02057 -0.025 0.815 0.057 1.000 0.061 -1.161 0.307 -0.803 -2.5 0.034 0.01872 -0.029 0.809 0.057 1.000 0.063 1.809 0.309 1.092 -2.0 0.091 0.01715 -0.032 0.806 0.055 1.000 0.060 5.300 0.310 0.601 -1.5 0.147 0.01409 -0.035 0.794 0.058 1.000 0.064 10.439 0.311 0.490 -1.0 0.202 0.01242 -0.039 0.779 0.056 1.000 0.063 16.296 0.313 0.441 -0.5 0.257 0.01055 -0.042 0.764 0.056 1.000 0.063 24.356 0.314 0.414 0.0 0.311 0.00972 -0.046 0.594 0.056 1.000 0.065 31.962 0.292 0.397 0.5 0.366 0.01050 -0.047 0.394 0.059 1.000 0.066 34.896 0.271 0.378 1.0 0.422 0.01117 -0.048 0.370 0.059 1.000 0.068 37.811 0.272 0.364 1.5 0.478 0.00924 -0.049 0.348 0.060 1.000 0.070 51.742 0.272 0.353 2.0 0.534 0.00992 -0.050 0.327 0.061 1.000 0.072 53.834 0.272 0.345 2.5 0.590 0.00994 -0.052 0.306 0.063 1.000 0.076 59.322 0.273 0.338 3.0 0.645 0.00998 -0.053 0.282 0.065 1.000 0.086 64.659 0.273 0.332 3.5 0.701 0.01108 -0.054 0.258 0.069 1.000 0.094 63.254 0.273 0.327 4.0 0.757 0.01159 -0.056 0.209 0.073 1.000 0.103 65.265 0.274 0.323 4.5 0.812 0.01503 -0.057 0.141 0.081 1.000 0.979 54.023 0.274 0.320 5.0 0.867 0.01643 -0.058 0.011 0.089 1.000 0.979 52.766 0.081 0.317 5.5 0.653 0.02902 -0.084 0.007 0.095 0.011 0.980 22.500 0.085 0.378 6.0 0.690 0.03234 -0.087 0.005 0.955 0.008 0.957 21.345 0.348 0.376 6.5 0.724 0.03525 -0.091 0.004 0.955 0.007 0.956 20.549 0.358 0.375 7.0 0.756 0.03752 -0.094 0.003 0.957 0.006 0.959 20.144 0.369 0.375 7.5 0.784 0.04148 -0.098 0.003 0.957 0.005 0.959 18.902 0.381 0.375 8.0 0.810 0.04512 -0.101 0.002 0.960 0.004 0.961 17.958 0.396 0.375 8.5 0.833 0.05005 -0.105 0.002 0.960 0.004 0.961 16.647 0.419 0.376 9.0 0.853 0.05571 -0.109 0.002 0.960 0.004 0.961 15.307 0.450 0.377 9.5 0.869 0.06062 -0.112 0.002 0.960 0.003 0.961 14.339 0.499 0.379 10.0 0.882 0.06753 -0.116 0.002 0.955 0.003 0.956 13.056 0.596 0.381 10.5 0.890 0.07695 -0.120 0.002 0.955 0.003 0.956 11.568 0.816 0.384 11.0 0.895 0.08478 -0.123 0.001 0.960 0.003 0.961 10.551 1.723 0.388 11.5 0.895 0.09022 -0.127 0.001 0.960 0.003 0.961 9.922 -1.933 0.392 12.0 0.891 0.10602 -0.130 0.001 0.960 0.003 0.961 8.406 -0.352 0.396 12.5 0.883 0.11596 -0.134 0.002 0.960 0.003 0.961 7.614 -0.128 0.402 13.0 0.872 0.12170 -0.138 0.002 0.960 0.003 0.961 7.163 -0.030 0.408 13.5 0.857 0.13894 -0.141 0.002 0.960 0.003 0.961 6.166 0.027 0.415 14.0 0.839 0.15802 -0.145 0.002 0.959 0.004 0.961 5.308 0.058 0.423 14.5 0.818 0.16615 -0.149 0.002 0.959 0.003 0.961 4.926 0.080 0.432 15.0 0.796 0.19015 -0.152 0.002 0.954 0.004 0.956 4.184 0.089 0.442