Name = N-10 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 -0.446 0.16164 -0.005 0.895 0.013 1.000 0.015 -2.758 0.355 0.239 -14.5 -0.421 0.14340 -0.008 0.868 0.014 1.000 0.015 -2.934 0.351 0.232 -14.0 -0.394 0.13779 -0.010 0.847 0.014 1.000 0.016 -2.857 0.346 0.224 -13.5 -0.365 0.12601 -0.013 0.821 0.014 1.000 0.016 -2.898 0.341 0.214 -13.0 -0.334 0.12149 -0.016 0.800 0.014 1.000 0.016 -2.749 0.338 0.203 -12.5 -0.302 0.11065 -0.019 0.795 0.014 1.000 0.016 -2.728 0.337 0.188 -12.0 -0.269 0.10209 -0.021 0.789 0.014 1.000 0.016 -2.631 0.335 0.170 -11.5 -0.235 0.09339 -0.024 0.784 0.014 1.000 0.016 -2.512 0.334 0.146 -11.0 -0.200 0.08343 -0.027 0.779 0.015 1.000 0.017 -2.397 0.334 0.114 -10.5 -0.165 0.07762 -0.030 0.774 0.015 1.000 0.017 -2.121 0.334 0.067 -10.0 -0.129 0.07224 -0.033 0.763 0.016 1.000 0.017 -1.784 0.334 -0.007 -9.5 -0.093 0.07074 -0.036 0.758 0.015 1.000 0.017 -1.310 0.334 -0.141 -9.0 -0.056 0.06222 -0.039 0.753 0.016 1.000 0.018 -0.894 0.334 -0.457 -8.5 -0.019 0.06096 -0.042 0.742 0.016 1.000 0.018 -0.307 0.225 -2.022 -8.0 -0.312 0.05581 -0.046 0.739 0.016 1.000 0.018 -5.593 0.222 0.104 -7.5 -0.246 0.05311 -0.049 0.732 0.016 1.000 0.018 -4.625 0.299 0.051 -7.0 -0.180 0.04784 -0.052 0.726 0.016 1.000 0.019 -3.754 0.300 -0.040 -6.5 -0.114 0.04459 -0.055 0.723 0.016 1.000 0.019 -2.557 0.300 -0.235 -6.0 -0.049 0.04406 -0.059 0.716 0.017 0.894 0.020 -1.115 0.302 -0.944 -5.5 0.015 0.03863 -0.062 0.600 0.017 1.000 0.021 0.392 0.303 4.343 -5.0 0.079 0.03709 -0.065 0.590 0.018 1.000 0.022 2.120 0.304 1.081 -4.5 0.141 0.03446 -0.069 0.584 0.019 1.000 0.023 4.102 0.305 0.737 -4.0 0.203 0.03211 -0.072 0.574 0.021 1.000 0.025 6.327 0.441 0.605 -3.5 0.250 0.02393 -0.090 0.568 0.023 1.000 0.959 10.443 0.428 0.608 -3.0 0.309 0.02713 -0.091 0.561 0.092 1.000 0.960 11.396 0.277 0.545 -2.5 0.368 0.02778 -0.093 0.555 0.189 0.900 0.960 13.260 0.277 0.502 -2.0 0.427 0.02835 -0.094 0.548 0.194 0.868 0.960 15.076 0.277 0.471 -1.5 0.486 0.02856 -0.096 0.542 0.827 0.835 0.953 17.036 0.278 0.447 -1.0 0.545 0.02888 -0.098 0.535 0.843 0.803 0.954 18.891 0.280 0.429 -0.5 0.604 0.03073 -0.099 0.303 0.862 1.000 0.954 19.672 0.280 0.414 0.0 0.663 0.03007 -0.101 0.294 0.884 1.000 0.954 22.061 0.278 0.403 0.5 0.723 0.03197 -0.103 0.281 0.905 1.000 0.954 22.601 0.276 0.392 1.0 0.782 0.03282 -0.104 0.271 0.914 1.000 0.954 23.818 0.277 0.383 1.5 0.841 0.02941 -0.106 0.265 0.919 1.000 0.952 28.585 0.471 0.376 2.0 0.811 0.03619 -0.111 0.258 0.931 0.865 0.952 22.398 -1.550 0.387 2.5 0.836 0.03799 -0.114 0.252 0.942 0.813 0.952 21.998 0.378 0.387 3.0 0.869 0.03906 -0.118 0.245 0.953 0.777 0.954 22.258 0.242 0.386 3.5 1.076 0.03179 -0.112 0.100 0.953 1.000 0.955 33.842 0.259 0.355 4.0 1.047 0.03953 -0.120 0.097 0.953 0.884 0.955 26.496 -3.524 0.364 4.5 1.073 0.04127 -0.124 0.097 0.953 0.839 0.955 25.994 0.435 0.366 5.0 1.098 0.04390 -0.129 0.094 0.953 0.797 0.955 25.013 0.461 0.368 5.5 1.120 0.04712 -0.134 0.094 0.954 0.752 0.955 23.770 0.614 0.370 6.0 1.129 0.05181 -0.141 0.091 0.954 0.690 0.955 21.797 -1.663 0.374 6.5 1.113 0.05719 -0.149 0.089 0.957 0.584 0.958 19.455 -0.577 0.384 7.0 1.111 0.06368 -0.155 0.086 0.957 0.503 0.958 17.455 0.020 0.390 7.5 1.054 0.07804 -0.162 0.086 0.957 0.100 0.958 13.507 0.281 0.404 8.0 1.255 0.06352 -0.160 0.027 0.957 0.589 0.958 19.757 0.289 0.377 8.5 1.223 0.07327 -0.169 0.025 0.957 0.470 0.958 16.696 0.041 0.388 9.0 1.175 0.08628 -0.176 0.021 0.957 0.286 0.959 13.622 -0.025 0.400 9.5 1.186 0.09913 -0.179 0.019 0.957 0.094 0.959 11.961 0.310 0.401 10.0 1.252 0.09701 -0.181 0.015 0.957 0.027 0.959 12.906 0.314 0.395 10.5 1.281 0.10211 -0.185 0.011 0.957 0.023 0.959 12.544 0.386 0.395 11.0 1.311 0.10374 -0.189 0.009 0.958 0.017 0.959 12.633 0.396 0.394 11.5 1.335 0.11433 -0.193 0.008 0.958 0.012 0.959 11.676 0.438 0.395 12.0 1.354 0.12243 -0.197 0.007 0.958 0.011 0.959 11.059 0.493 0.396 12.5 1.369 0.13222 -0.201 0.006 0.952 0.010 0.954 10.356 0.561 0.397 13.0 1.381 0.13967 -0.205 0.006 0.958 0.009 0.959 9.886 0.673 0.399 13.5 1.389 0.15168 -0.210 0.005 0.958 0.008 0.959 9.158 0.955 0.401 14.0 1.393 0.15908 -0.214 0.005 0.958 0.008 0.959 8.755 2.239 0.404 14.5 1.393 0.17622 -0.218 0.005 0.958 0.008 0.959 7.907 -4.840 0.407 15.0 1.391 0.18313 -0.222 0.004 0.958 0.007 0.959 7.596 -1.665 0.410 Name = N-10 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 -0.446 0.12478 -0.005 0.895 0.013 1.000 0.015 -3.573 0.354 0.239 -14.5 -0.421 0.11819 -0.008 0.868 0.014 1.000 0.015 -3.559 0.351 0.232 -14.0 -0.394 0.10724 -0.010 0.847 0.014 1.000 0.016 -3.671 0.346 0.224 -13.5 -0.365 0.10353 -0.013 0.821 0.014 1.000 0.016 -3.527 0.341 0.214 -13.0 -0.334 0.09558 -0.016 0.800 0.014 1.000 0.016 -3.494 0.338 0.203 -12.5 -0.302 0.09202 -0.019 0.795 0.014 1.000 0.016 -3.279 0.336 0.188 -12.0 -0.269 0.08430 -0.021 0.789 0.014 1.000 0.016 -3.185 0.335 0.170 -11.5 -0.235 0.08085 -0.024 0.784 0.014 1.000 0.017 -2.900 0.334 0.146 -11.0 -0.200 0.07251 -0.027 0.779 0.015 1.000 0.017 -2.755 0.334 0.114 -10.5 -0.164 0.06702 -0.030 0.774 0.015 1.000 0.018 -2.454 0.334 0.067 -10.0 -0.129 0.06277 -0.033 0.763 0.016 1.000 0.018 -2.051 0.335 -0.008 -9.5 -0.093 0.05842 -0.036 0.758 0.015 1.000 0.017 -1.586 0.334 -0.141 -9.0 -0.055 0.05389 -0.039 0.753 0.016 1.000 0.018 -1.029 0.334 -0.458 -8.5 -0.019 0.05111 -0.042 0.742 0.016 1.000 0.018 -0.366 0.225 -2.022 -8.0 -0.312 0.04824 -0.046 0.739 0.016 1.000 0.018 -6.471 0.222 0.104 -7.5 -0.246 0.04453 -0.049 0.732 0.016 1.000 0.018 -5.516 0.299 0.051 -7.0 -0.180 0.04176 -0.052 0.726 0.016 1.000 0.019 -4.300 0.299 -0.040 -6.5 -0.114 0.03822 -0.055 0.723 0.016 1.000 0.020 -2.983 0.300 -0.235 -6.0 -0.049 0.03614 -0.059 0.716 0.017 1.000 0.020 -1.359 0.301 -0.944 -5.5 0.015 0.03407 -0.062 0.600 0.017 1.000 0.021 0.444 0.303 4.342 -5.0 0.079 0.03141 -0.065 0.590 0.018 1.000 0.022 2.503 0.304 1.081 -4.5 0.141 0.02965 -0.069 0.584 0.019 1.000 0.024 4.766 0.452 0.736 -4.0 0.191 0.01945 -0.088 0.574 0.021 1.000 0.960 9.808 0.442 0.711 -3.5 0.250 0.01985 -0.090 0.568 0.023 1.000 0.960 12.591 0.277 0.608 -3.0 0.309 0.02238 -0.091 0.561 0.092 1.000 0.961 13.813 0.277 0.545 -2.5 0.368 0.02212 -0.093 0.555 0.189 1.000 0.961 16.650 0.277 0.502 -2.0 0.427 0.02258 -0.094 0.548 0.194 1.000 0.962 18.923 0.277 0.471 -1.5 0.486 0.02228 -0.096 0.542 0.827 1.000 0.954 21.832 0.277 0.447 -1.0 0.545 0.02196 -0.098 0.535 0.843 1.000 0.955 24.840 0.280 0.429 -0.5 0.604 0.02314 -0.099 0.303 0.862 1.000 0.955 26.122 0.280 0.414 0.0 0.663 0.02508 -0.101 0.294 0.884 1.000 0.955 26.453 0.278 0.403 0.5 0.723 0.02541 -0.103 0.281 0.905 1.000 0.954 28.439 0.276 0.392 1.0 0.782 0.02648 -0.104 0.271 0.914 1.000 0.955 29.514 0.277 0.383 1.5 0.841 0.02325 -0.106 0.265 0.919 1.000 0.952 36.157 0.277 0.376 2.0 0.900 0.02450 -0.107 0.258 0.931 1.000 0.952 36.719 0.278 0.369 2.5 0.958 0.02443 -0.109 0.252 0.942 1.000 0.952 39.235 0.278 0.364 3.0 1.017 0.02408 -0.111 0.245 0.953 1.000 0.954 42.241 0.279 0.359 3.5 1.076 0.02593 -0.112 0.100 0.953 1.000 0.955 41.496 0.279 0.355 4.0 1.134 0.02793 -0.114 0.097 0.953 1.000 0.955 40.613 0.280 0.351 4.5 1.193 0.02843 -0.116 0.097 0.953 1.000 0.955 41.953 0.280 0.347 5.0 1.251 0.02981 -0.118 0.094 0.953 1.000 0.955 41.955 1.279 0.344 5.5 1.205 0.03630 -0.128 0.094 0.954 0.871 0.955 33.179 -0.499 0.356 6.0 1.230 0.03869 -0.133 0.091 0.954 0.832 0.955 31.795 0.432 0.358 6.5 1.259 0.04046 -0.138 0.089 0.957 0.800 0.958 31.116 0.434 0.359 7.0 1.285 0.04324 -0.143 0.086 0.957 0.766 0.958 29.723 0.811 0.361 7.5 1.282 0.04759 -0.151 0.086 0.957 0.695 0.958 26.933 0.351 0.368 8.0 1.364 0.04824 -0.151 0.027 0.957 0.742 0.958 28.281 0.317 0.361 8.5 1.377 0.05237 -0.157 0.025 0.957 0.703 0.958 26.301 -1.650 0.364 9.0 1.356 0.05844 -0.166 0.021 0.957 0.616 0.959 23.209 -0.189 0.372 9.5 1.338 0.06545 -0.174 0.019 0.957 0.534 0.959 20.446 0.049 0.380 10.0 1.264 0.08096 -0.185 0.015 0.957 0.341 0.959 15.613 0.109 0.396 10.5 1.235 0.09455 -0.189 0.011 0.957 0.153 0.959 13.059 0.384 0.403 11.0 1.299 0.09056 -0.189 0.009 0.958 0.025 0.959 14.346 0.301 0.396 11.5 1.323 0.10087 -0.193 0.008 0.958 0.021 0.959 13.120 0.416 0.396 12.0 1.347 0.10543 -0.197 0.007 0.958 0.015 0.959 12.777 0.441 0.396 12.5 1.365 0.11017 -0.201 0.006 0.952 0.011 0.954 12.392 0.526 0.398 13.0 1.377 0.11717 -0.206 0.006 0.958 0.011 0.959 11.751 0.664 0.399 13.5 1.385 0.12651 -0.210 0.005 0.958 0.010 0.959 10.951 0.900 0.401 14.0 1.390 0.13123 -0.214 0.005 0.958 0.009 0.959 10.591 1.785 0.404 14.5 1.391 0.14034 -0.218 0.005 0.958 0.009 0.959 9.911 -5.428 0.407 15.0 1.388 0.15195 -0.222 0.004 0.958 0.008 0.959 9.137 -1.386 0.410 Name = N-10 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 -0.446 0.11343 -0.005 0.895 0.013 1.000 0.015 -3.930 0.354 0.239 -14.5 -0.421 0.10749 -0.008 0.868 0.014 1.000 0.015 -3.913 0.351 0.232 -14.0 -0.394 0.10143 -0.010 0.847 0.014 1.000 0.016 -3.881 0.346 0.224 -13.5 -0.365 0.09412 -0.013 0.821 0.014 1.000 0.016 -3.878 0.341 0.214 -13.0 -0.334 0.09027 -0.016 0.800 0.014 1.000 0.017 -3.699 0.338 0.203 -12.5 -0.302 0.08399 -0.019 0.795 0.014 1.000 0.016 -3.592 0.337 0.188 -12.0 -0.268 0.07683 -0.021 0.789 0.014 1.000 0.017 -3.494 0.335 0.170 -11.5 -0.235 0.07140 -0.024 0.784 0.014 1.000 0.017 -3.284 0.335 0.146 -11.0 -0.200 0.06508 -0.027 0.779 0.015 1.000 0.017 -3.070 0.334 0.114 -10.5 -0.164 0.06024 -0.030 0.774 0.015 1.000 0.018 -2.731 0.334 0.067 -10.0 -0.129 0.05707 -0.033 0.763 0.016 1.000 0.018 -2.256 0.334 -0.008 -9.5 -0.093 0.05496 -0.036 0.758 0.015 1.000 0.018 -1.683 0.333 -0.142 -9.0 -0.055 0.05027 -0.039 0.753 0.016 1.000 0.019 -1.100 0.334 -0.460 -8.5 -0.019 0.04782 -0.042 0.742 0.016 1.000 0.018 -0.387 0.225 -2.044 -8.0 -0.312 0.04483 -0.046 0.739 0.016 1.000 0.019 -6.962 0.222 0.104 -7.5 -0.246 0.04138 -0.049 0.732 0.016 1.000 0.019 -5.936 0.299 0.051 -7.0 -0.180 0.03852 -0.052 0.726 0.016 1.000 0.020 -4.661 0.299 -0.040 -6.5 -0.114 0.03632 -0.055 0.723 0.016 1.000 0.020 -3.139 0.300 -0.235 -6.0 -0.049 0.03387 -0.059 0.716 0.017 1.000 0.021 -1.449 0.302 -0.944 -5.5 0.015 0.03141 -0.062 0.600 0.017 1.000 0.022 0.482 0.303 4.341 -5.0 0.079 0.02941 -0.065 0.590 0.018 1.000 0.023 2.673 0.304 1.081 -4.5 0.141 0.02774 -0.069 0.584 0.019 1.000 0.025 5.094 0.453 0.736 -4.0 0.191 0.01732 -0.088 0.574 0.021 1.000 0.961 11.015 0.443 0.712 -3.5 0.250 0.01804 -0.090 0.568 0.023 1.000 0.962 13.850 0.277 0.609 -3.0 0.309 0.01894 -0.091 0.561 0.092 1.000 0.962 16.320 0.277 0.545 -2.5 0.368 0.01989 -0.093 0.555 0.189 1.000 0.963 18.515 0.277 0.502 -2.0 0.427 0.01982 -0.094 0.548 0.194 1.000 0.963 21.562 0.276 0.471 -1.5 0.486 0.01887 -0.096 0.542 0.827 1.000 0.955 25.785 0.277 0.447 -1.0 0.545 0.01942 -0.098 0.535 0.843 1.000 0.955 28.095 0.279 0.429 -0.5 0.604 0.02080 -0.099 0.303 0.862 1.000 0.955 29.060 0.280 0.414 0.0 0.663 0.02099 -0.101 0.294 0.884 1.000 0.955 31.601 0.278 0.403 0.5 0.723 0.02262 -0.103 0.281 0.905 1.000 0.955 31.944 0.276 0.392 1.0 0.782 0.02291 -0.104 0.271 0.914 1.000 0.955 34.116 0.277 0.383 1.5 0.841 0.02018 -0.106 0.265 0.919 1.000 0.952 41.645 0.277 0.376 2.0 0.900 0.02072 -0.107 0.258 0.931 1.000 0.952 43.417 0.278 0.369 2.5 0.958 0.02116 -0.109 0.252 0.942 1.000 0.952 45.293 0.278 0.364 3.0 1.017 0.02162 -0.111 0.245 0.953 1.000 0.954 47.044 0.279 0.359 3.5 1.076 0.02277 -0.112 0.100 0.953 1.000 0.955 47.248 0.279 0.355 4.0 1.134 0.02398 -0.114 0.097 0.953 1.000 0.955 47.310 0.280 0.351 4.5 1.193 0.02559 -0.116 0.097 0.953 1.000 0.955 46.620 0.280 0.347 5.0 1.251 0.02580 -0.118 0.094 0.953 1.000 0.955 48.471 0.281 0.344 5.5 1.308 0.02648 -0.119 0.094 0.954 1.000 0.955 49.384 0.660 0.341 6.0 1.278 0.03390 -0.129 0.091 0.954 0.897 0.955 37.697 5.208 0.351 6.5 1.311 0.03456 -0.133 0.089 0.957 0.868 0.958 37.926 0.421 0.352 7.0 1.335 0.03713 -0.139 0.086 0.957 0.832 0.958 35.962 0.510 0.354 7.5 1.354 0.04003 -0.145 0.086 0.957 0.789 0.958 33.826 0.410 0.357 8.0 1.395 0.04340 -0.148 0.027 0.957 0.782 0.958 32.150 0.392 0.356 8.5 1.417 0.04642 -0.154 0.025 0.957 0.753 0.958 30.534 0.551 0.358 9.0 1.432 0.04987 -0.159 0.021 0.957 0.718 0.959 28.725 5.341 0.361 9.5 1.420 0.05505 -0.168 0.019 0.957 0.650 0.959 25.797 -0.310 0.368 10.0 1.403 0.06203 -0.176 0.015 0.957 0.576 0.959 22.611 -0.133 0.376 10.5 1.377 0.07103 -0.184 0.011 0.957 0.492 0.959 19.382 0.038 0.384 11.0 1.321 0.08359 -0.193 0.009 0.958 0.341 0.959 15.803 0.125 0.396 11.5 1.282 0.09681 -0.196 0.008 0.958 0.097 0.959 13.243 0.530 0.403 12.0 1.336 0.09717 -0.198 0.007 0.958 0.023 0.959 13.752 0.321 0.398 12.5 1.357 0.10407 -0.202 0.006 0.952 0.017 0.954 13.039 0.468 0.399 13.0 1.373 0.10785 -0.206 0.006 0.958 0.012 0.959 12.729 0.579 0.400 13.5 1.382 0.11456 -0.210 0.005 0.958 0.011 0.959 12.062 0.863 0.402 14.0 1.386 0.12102 -0.214 0.005 0.958 0.010 0.959 11.456 1.706 0.404 14.5 1.388 0.13064 -0.218 0.005 0.958 0.010 0.959 10.622 -9.892 0.407 15.0 1.386 0.13711 -0.222 0.004 0.958 0.009 0.959 10.106 -1.831 0.411 Name = N-10 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 -0.446 0.10716 -0.005 0.895 0.013 1.000 0.015 -4.159 0.355 0.239 -14.5 -0.421 0.09782 -0.008 0.868 0.014 1.000 0.015 -4.300 0.351 0.232 -14.0 -0.394 0.09190 -0.010 0.847 0.014 1.000 0.016 -4.283 0.346 0.224 -13.5 -0.365 0.08865 -0.013 0.821 0.014 1.000 0.016 -4.117 0.341 0.214 -13.0 -0.334 0.08220 -0.016 0.800 0.014 1.000 0.017 -4.062 0.338 0.203 -12.5 -0.302 0.07700 -0.019 0.795 0.014 1.000 0.016 -3.918 0.336 0.188 -12.0 -0.268 0.07246 -0.021 0.789 0.014 1.000 0.017 -3.704 0.335 0.170 -11.5 -0.235 0.06589 -0.024 0.784 0.014 1.000 0.017 -3.559 0.334 0.146 -11.0 -0.200 0.06349 -0.027 0.779 0.015 1.000 0.018 -3.145 0.334 0.114 -10.5 -0.164 0.05846 -0.030 0.774 0.015 1.000 0.018 -2.811 0.334 0.067 -10.0 -0.129 0.05523 -0.033 0.763 0.016 1.000 0.018 -2.328 0.335 -0.008 -9.5 -0.093 0.05145 -0.036 0.758 0.015 1.000 0.018 -1.798 0.334 -0.142 -9.0 -0.055 0.04716 -0.039 0.753 0.016 1.000 0.019 -1.173 0.334 -0.460 -8.5 -0.019 0.04478 -0.042 0.742 0.016 1.000 0.018 -0.413 0.225 -2.044 -8.0 -0.312 0.04222 -0.046 0.739 0.016 1.000 0.019 -7.393 0.222 0.104 -7.5 -0.246 0.03991 -0.049 0.732 0.016 1.000 0.019 -6.154 0.298 0.051 -7.0 -0.180 0.03700 -0.052 0.726 0.016 1.000 0.020 -4.852 0.299 -0.040 -6.5 -0.114 0.03477 -0.055 0.723 0.016 1.000 0.021 -3.279 0.300 -0.235 -6.0 -0.049 0.03237 -0.059 0.716 0.017 1.000 0.021 -1.517 0.302 -0.944 -5.5 0.015 0.03045 -0.062 0.600 0.017 1.000 0.022 0.497 0.303 4.341 -5.0 0.079 0.02798 -0.065 0.590 0.018 1.000 0.024 2.810 0.461 1.081 -4.5 0.132 0.01642 -0.087 0.584 0.019 1.000 0.961 8.019 0.453 0.907 -4.0 0.191 0.01664 -0.088 0.574 0.021 1.000 0.962 11.465 0.276 0.712 -3.5 0.250 0.01595 -0.090 0.568 0.023 1.000 0.963 15.671 0.276 0.609 -3.0 0.309 0.01742 -0.091 0.561 0.092 1.000 0.963 17.740 0.277 0.545 -2.5 0.368 0.01810 -0.093 0.555 0.189 1.000 0.964 20.345 0.277 0.502 -2.0 0.427 0.01788 -0.094 0.548 0.194 1.000 0.964 23.892 0.276 0.471 -1.5 0.486 0.01686 -0.096 0.542 0.827 1.000 0.956 28.855 0.277 0.447 -1.0 0.545 0.01693 -0.098 0.535 0.843 1.000 0.956 32.211 0.279 0.429 -0.5 0.604 0.01986 -0.099 0.303 0.862 1.000 0.956 30.428 0.280 0.414 0.0 0.663 0.01972 -0.101 0.294 0.884 1.000 0.955 33.648 0.278 0.403 0.5 0.723 0.01985 -0.103 0.281 0.905 1.000 0.955 36.406 0.276 0.392 1.0 0.782 0.02142 -0.104 0.271 0.914 1.000 0.955 36.494 0.277 0.383 1.5 0.841 0.01851 -0.106 0.265 0.919 1.000 0.952 45.404 0.277 0.376 2.0 0.900 0.01885 -0.107 0.258 0.931 1.000 0.952 47.727 0.278 0.369 2.5 0.958 0.01930 -0.109 0.252 0.942 1.000 0.952 49.663 0.278 0.364 3.0 1.017 0.01921 -0.111 0.245 0.953 1.000 0.954 52.957 0.279 0.359 3.5 1.076 0.02180 -0.112 0.100 0.953 1.000 0.955 49.363 0.279 0.355 4.0 1.134 0.02290 -0.114 0.097 0.953 1.000 0.955 49.540 0.280 0.351 4.5 1.193 0.02422 -0.116 0.097 0.953 1.000 0.955 49.257 0.280 0.347 5.0 1.251 0.02398 -0.118 0.094 0.953 1.000 0.955 52.143 0.281 0.344 5.5 1.308 0.02601 -0.119 0.094 0.954 1.000 0.955 50.272 0.282 0.341 6.0 1.365 0.02670 -0.121 0.091 0.954 1.000 0.955 51.103 0.282 0.339 6.5 1.421 0.03136 -0.123 0.089 0.957 1.000 0.958 45.304 2.876 0.337 7.0 1.370 0.03373 -0.135 0.086 0.957 0.876 0.958 40.608 -0.359 0.349 7.5 1.391 0.03546 -0.141 0.086 0.957 0.837 0.958 39.233 0.520 0.351 8.0 1.412 0.03976 -0.147 0.027 0.957 0.803 0.958 35.507 0.472 0.354 8.5 1.438 0.04298 -0.152 0.025 0.957 0.779 0.958 33.472 0.490 0.355 9.0 1.456 0.04514 -0.157 0.021 0.957 0.747 0.959 32.253 0.645 0.358 9.5 1.468 0.04883 -0.163 0.019 0.957 0.713 0.959 30.069 -4.358 0.361 10.0 1.453 0.05516 -0.172 0.015 0.957 0.645 0.959 26.340 -0.222 0.368 10.5 1.432 0.06246 -0.180 0.011 0.957 0.571 0.959 22.926 -0.319 0.376 11.0 1.426 0.06798 -0.187 0.009 0.958 0.521 0.959 20.974 0.021 0.381 11.5 1.358 0.08175 -0.197 0.008 0.958 0.365 0.959 16.610 0.143 0.395 12.0 1.300 0.10027 -0.201 0.007 0.958 0.097 0.959 12.963 -0.171 0.404 12.5 1.347 0.09895 -0.202 0.006 0.952 0.025 0.954 13.610 0.333 0.400 13.0 1.364 0.10075 -0.206 0.006 0.958 0.019 0.959 13.539 0.500 0.401 13.5 1.378 0.10862 -0.210 0.005 0.958 0.013 0.959 12.686 0.677 0.402 14.0 1.383 0.11483 -0.214 0.005 0.958 0.012 0.959 12.044 1.485 0.405 14.5 1.385 0.12119 -0.218 0.005 0.958 0.011 0.959 11.427 -47.367 0.408 15.0 1.383 0.12764 -0.223 0.004 0.958 0.010 0.959 10.834 -1.925 0.411