Name = GOE 573 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 -0.327 0.21978 0.002 0.800 0.012 1.000 0.014 -1.489 0.431 0.255 -14.5 -0.308 0.20752 -0.002 0.783 0.013 1.000 0.014 -1.484 0.423 0.244 -14.0 -0.287 0.18435 -0.005 0.766 0.013 1.000 0.014 -1.555 0.410 0.231 -13.5 -0.264 0.17506 -0.009 0.755 0.013 1.000 0.015 -1.506 0.399 0.216 -13.0 -0.239 0.15957 -0.013 0.739 0.013 1.000 0.015 -1.497 0.390 0.198 -12.5 -0.212 0.15385 -0.016 0.727 0.014 1.000 0.015 -1.380 0.383 0.174 -12.0 -0.184 0.14019 -0.020 0.711 0.013 1.000 0.015 -1.313 0.377 0.142 -11.5 -0.154 0.12883 -0.024 0.694 0.014 1.000 0.015 -1.199 0.372 0.098 -11.0 -0.123 0.12396 -0.027 0.605 0.014 1.000 0.015 -0.995 0.368 0.029 -10.5 -0.091 0.11163 -0.031 0.588 0.014 1.000 0.015 -0.816 0.364 -0.090 -10.0 -0.057 0.10464 -0.035 0.576 0.014 1.000 0.016 -0.549 0.361 -0.355 -9.5 -0.023 0.09448 -0.039 0.564 0.014 1.000 0.016 -0.244 0.229 -1.423 -9.0 -0.414 0.08925 -0.042 0.552 0.014 1.000 0.015 -4.639 0.226 0.148 -8.5 -0.351 0.08080 -0.046 0.535 0.014 1.000 0.015 -4.340 0.311 0.118 -8.0 -0.287 0.07365 -0.050 0.529 0.014 1.000 0.016 -3.897 0.311 0.075 -7.5 -0.223 0.07274 -0.054 0.517 0.015 0.905 0.016 -3.071 0.312 0.008 -7.0 -0.160 0.06671 -0.058 0.505 0.015 0.889 0.016 -2.393 0.312 -0.113 -6.5 -0.096 0.06160 -0.062 0.489 0.015 0.876 0.017 -1.560 0.313 -0.394 -6.0 -0.033 0.05551 -0.066 0.471 0.015 0.865 0.017 -0.592 0.313 -1.758 -5.5 0.030 0.05308 -0.070 0.460 0.015 0.838 0.017 0.567 0.314 2.575 -5.0 0.093 0.04869 -0.074 0.446 0.016 0.820 0.017 1.902 0.315 1.049 -4.5 0.155 0.04549 -0.078 0.432 0.016 0.803 0.017 3.398 0.316 0.755 -4.0 0.216 0.04211 -0.082 0.421 0.017 0.772 0.018 5.128 0.317 0.630 -3.5 0.277 0.03973 -0.086 0.410 0.017 0.741 0.019 6.963 0.318 0.562 -3.0 0.337 0.03729 -0.090 0.396 0.017 0.727 0.019 9.028 0.319 0.518 -2.5 0.396 0.03531 -0.095 0.389 0.017 0.685 0.019 11.212 0.321 0.489 -2.0 0.454 0.03301 -0.099 0.378 0.017 0.660 0.020 13.761 0.322 0.467 -1.5 0.512 0.03129 -0.103 0.371 0.017 0.625 0.020 16.355 0.323 0.451 -1.0 0.568 0.02968 -0.107 0.367 0.018 0.585 0.021 19.151 0.325 0.438 -0.5 0.624 0.02817 -0.111 0.360 0.020 0.571 0.023 22.135 0.191 0.428 0.0 0.425 0.03407 -0.115 0.357 0.022 0.546 0.025 12.473 0.197 0.522 0.5 0.466 0.03599 -0.120 0.353 0.024 0.524 0.039 12.937 0.354 0.507 1.0 0.506 0.04216 -0.124 0.349 0.042 0.503 0.965 11.992 0.352 0.495 1.5 0.550 0.04408 -0.128 0.346 0.050 0.489 0.965 12.467 0.349 0.483 2.0 0.593 0.04737 -0.133 0.342 0.932 0.474 0.951 12.530 0.351 0.473 2.5 0.637 0.04919 -0.137 0.339 0.934 0.460 0.951 12.947 0.351 0.465 3.0 0.681 0.05091 -0.141 0.335 0.937 0.449 0.951 13.381 0.349 0.458 3.5 0.727 0.05351 -0.146 0.332 0.939 0.442 0.951 13.585 0.361 0.451 4.0 0.764 0.05631 -0.151 0.332 0.942 0.417 0.952 13.565 0.353 0.447 4.5 0.815 0.05755 -0.155 0.329 0.947 0.423 0.952 14.156 0.352 0.440 5.0 0.853 0.06044 -0.160 0.329 0.950 0.403 0.952 14.109 0.360 0.437 5.5 0.899 0.06243 -0.164 0.326 0.953 0.399 0.954 14.399 0.347 0.433 6.0 0.946 0.06473 -0.169 0.323 0.953 0.396 0.955 14.610 0.353 0.428 6.5 0.988 0.06739 -0.173 0.323 0.953 0.383 0.955 14.669 0.354 0.425 7.0 1.035 0.07053 -0.178 0.319 0.951 0.379 0.952 14.670 0.349 0.422 7.5 1.081 0.07270 -0.183 0.316 0.951 0.376 0.953 14.865 0.347 0.419 8.0 1.128 0.07580 -0.187 0.313 0.953 0.376 0.955 14.881 0.355 0.416 8.5 1.169 0.07879 -0.192 0.313 0.954 0.363 0.956 14.839 0.252 0.414 9.0 1.383 0.06400 -0.188 0.026 0.956 0.602 0.958 21.605 0.253 0.386 9.5 1.421 0.06731 -0.193 0.023 0.956 0.587 0.958 21.112 0.393 0.386 10.0 1.454 0.07250 -0.198 0.021 0.956 0.567 0.958 20.049 0.406 0.386 10.5 1.486 0.07599 -0.203 0.021 0.957 0.552 0.958 19.560 4.409 0.386 11.0 1.457 0.07426 -0.211 0.019 0.957 0.025 0.958 19.615 2.399 0.395 11.5 1.492 0.07838 -0.215 0.017 0.957 0.023 0.958 19.038 0.373 0.394 12.0 1.526 0.08348 -0.219 0.014 0.952 0.021 0.954 18.275 0.386 0.394 12.5 1.555 0.09211 -0.224 0.011 0.952 0.020 0.954 16.878 0.392 0.394 13.0 1.585 0.09772 -0.228 0.010 0.952 0.017 0.954 16.220 0.394 0.394 13.5 1.612 0.10525 -0.232 0.008 0.952 0.014 0.954 15.319 0.407 0.394 14.0 1.638 0.10835 -0.236 0.007 0.957 0.011 0.958 15.118 0.434 0.394 14.5 1.658 0.11724 -0.240 0.007 0.952 0.010 0.954 14.141 0.486 0.395 15.0 1.674 0.12419 -0.245 0.006 0.957 0.009 0.959 13.478 0.515 0.396 Name = GOE 573 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 -0.327 0.16311 0.002 0.800 0.012 1.000 0.014 -2.007 0.431 0.255 -14.5 -0.308 0.15693 -0.002 0.783 0.013 1.000 0.014 -1.962 0.423 0.244 -14.0 -0.287 0.15174 -0.005 0.766 0.013 1.000 0.014 -1.890 0.410 0.231 -13.5 -0.264 0.14278 -0.009 0.755 0.013 1.000 0.015 -1.847 0.399 0.216 -13.0 -0.239 0.13128 -0.013 0.739 0.013 1.000 0.015 -1.819 0.391 0.198 -12.5 -0.212 0.11863 -0.016 0.727 0.014 1.000 0.015 -1.789 0.383 0.174 -12.0 -0.184 0.11524 -0.020 0.711 0.013 1.000 0.015 -1.598 0.377 0.142 -11.5 -0.154 0.10659 -0.023 0.694 0.014 1.000 0.015 -1.449 0.372 0.098 -11.0 -0.123 0.09703 -0.027 0.605 0.014 1.000 0.015 -1.272 0.368 0.029 -10.5 -0.091 0.09241 -0.031 0.588 0.014 1.000 0.015 -0.985 0.364 -0.090 -10.0 -0.057 0.08277 -0.035 0.576 0.014 1.000 0.016 -0.694 0.361 -0.355 -9.5 -0.023 0.07907 -0.039 0.564 0.014 1.000 0.016 -0.291 0.229 -1.422 -9.0 -0.414 0.07111 -0.042 0.552 0.014 1.000 0.015 -5.823 0.226 0.148 -8.5 -0.351 0.06779 -0.046 0.535 0.014 1.000 0.016 -5.172 0.311 0.118 -8.0 -0.287 0.06181 -0.050 0.529 0.014 1.000 0.016 -4.644 0.311 0.075 -7.5 -0.223 0.05663 -0.054 0.517 0.015 1.000 0.016 -3.944 0.312 0.008 -7.0 -0.160 0.05352 -0.058 0.505 0.015 1.000 0.016 -2.984 0.312 -0.113 -6.5 -0.096 0.04844 -0.062 0.489 0.015 1.000 0.017 -1.984 0.313 -0.394 -6.0 -0.033 0.04592 -0.066 0.471 0.015 1.000 0.017 -0.715 0.313 -1.758 -5.5 0.030 0.04233 -0.070 0.460 0.015 1.000 0.017 0.711 0.314 2.575 -5.0 0.093 0.03904 -0.074 0.446 0.016 1.000 0.017 2.372 0.315 1.049 -4.5 0.155 0.03589 -0.078 0.432 0.016 1.000 0.018 4.307 0.316 0.755 -4.0 0.216 0.03327 -0.082 0.421 0.017 1.000 0.019 6.491 0.317 0.630 -3.5 0.277 0.03078 -0.086 0.410 0.017 1.000 0.019 8.987 0.318 0.562 -3.0 0.337 0.02899 -0.090 0.396 0.017 1.000 0.019 11.612 0.319 0.518 -2.5 0.396 0.02694 -0.095 0.389 0.017 1.000 0.019 14.692 0.321 0.489 -2.0 0.454 0.02499 -0.099 0.378 0.017 1.000 0.020 18.176 0.322 0.467 -1.5 0.512 0.02571 -0.103 0.371 0.017 0.883 0.020 19.903 0.323 0.451 -1.0 0.568 0.02433 -0.107 0.367 0.018 0.845 0.021 23.359 0.325 0.438 -0.5 0.624 0.02287 -0.111 0.360 0.020 0.817 0.024 27.261 -0.024 0.428 0.0 0.538 0.02179 -0.115 0.357 0.022 0.776 0.031 24.668 0.107 0.465 0.5 0.570 0.02330 -0.119 0.353 0.024 0.734 0.047 24.448 0.365 0.459 1.0 0.600 0.02883 -0.123 0.349 0.042 0.692 0.967 20.831 0.380 0.454 1.5 0.630 0.03082 -0.127 0.346 0.050 0.650 0.968 20.455 0.390 0.451 2.0 0.661 0.03328 -0.131 0.342 0.932 0.610 0.951 19.855 0.373 0.449 2.5 0.701 0.03519 -0.135 0.339 0.934 0.589 0.951 19.916 0.356 0.443 3.0 0.743 0.03700 -0.140 0.335 0.937 0.571 0.951 20.072 0.356 0.438 3.5 0.784 0.03864 -0.144 0.332 0.939 0.553 0.951 20.280 0.387 0.434 4.0 0.811 0.04183 -0.149 0.332 0.942 0.514 0.952 19.394 0.362 0.434 4.5 0.864 0.04281 -0.153 0.329 0.947 0.519 0.952 20.194 0.361 0.427 5.0 0.894 0.04574 -0.158 0.329 0.950 0.483 0.952 19.542 0.380 0.427 5.5 0.938 0.04759 -0.163 0.326 0.953 0.473 0.954 19.713 0.354 0.424 6.0 0.982 0.04945 -0.168 0.323 0.953 0.463 0.955 19.857 0.382 0.421 6.5 1.012 0.05258 -0.173 0.323 0.953 0.429 0.955 19.245 0.380 0.421 7.0 1.056 0.05550 -0.177 0.319 0.951 0.423 0.952 19.032 0.354 0.418 7.5 1.101 0.05763 -0.182 0.316 0.951 0.416 0.953 19.095 0.351 0.415 8.0 1.146 0.05926 -0.186 0.313 0.953 0.413 0.955 19.346 0.368 0.413 8.5 1.181 0.06270 -0.191 0.313 0.954 0.389 0.956 18.839 0.238 0.412 9.0 1.453 0.05042 -0.183 0.026 0.956 0.685 0.958 28.819 0.238 0.376 9.5 1.488 0.05429 -0.188 0.023 0.956 0.665 0.958 27.407 0.449 0.376 10.0 1.510 0.05841 -0.194 0.021 0.956 0.632 0.958 25.845 0.491 0.378 10.5 1.536 0.06236 -0.199 0.021 0.957 0.610 0.958 24.631 0.454 0.380 11.0 1.563 0.06613 -0.205 0.019 0.957 0.590 0.958 23.632 0.447 0.381 11.5 1.590 0.07113 -0.210 0.017 0.957 0.572 0.958 22.350 -0.096 0.382 12.0 1.520 0.07550 -0.220 0.014 0.952 0.024 0.954 20.133 -0.079 0.394 12.5 1.547 0.08088 -0.224 0.011 0.952 0.024 0.954 19.133 0.397 0.395 13.0 1.578 0.08252 -0.228 0.010 0.952 0.021 0.954 19.121 0.394 0.395 13.5 1.605 0.08943 -0.232 0.008 0.952 0.018 0.954 17.950 0.409 0.395 14.0 1.630 0.09318 -0.236 0.007 0.957 0.014 0.959 17.492 0.426 0.395 14.5 1.652 0.09989 -0.241 0.007 0.952 0.012 0.954 16.540 0.465 0.396 15.0 1.669 0.10529 -0.245 0.006 0.957 0.011 0.959 15.850 0.504 0.397 Name = GOE 573 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 -0.327 0.15371 0.002 0.800 0.012 1.000 0.015 -2.130 0.431 0.255 -14.5 -0.308 0.14376 -0.002 0.783 0.013 1.000 0.014 -2.142 0.424 0.244 -14.0 -0.287 0.13039 -0.005 0.766 0.013 1.000 0.014 -2.199 0.410 0.231 -13.5 -0.264 0.12193 -0.009 0.755 0.013 1.000 0.015 -2.163 0.399 0.216 -13.0 -0.239 0.11311 -0.013 0.739 0.013 1.000 0.015 -2.112 0.390 0.198 -12.5 -0.212 0.10916 -0.016 0.727 0.014 1.000 0.015 -1.945 0.383 0.174 -12.0 -0.184 0.09939 -0.020 0.711 0.013 1.000 0.015 -1.852 0.377 0.142 -11.5 -0.154 0.09262 -0.023 0.694 0.014 1.000 0.015 -1.667 0.372 0.098 -11.0 -0.123 0.08520 -0.027 0.605 0.014 1.000 0.015 -1.448 0.368 0.029 -10.5 -0.091 0.08067 -0.031 0.588 0.014 1.000 0.015 -1.129 0.364 -0.090 -10.0 -0.057 0.07611 -0.035 0.576 0.014 1.000 0.016 -0.754 0.361 -0.355 -9.5 -0.023 0.06974 -0.039 0.564 0.014 1.000 0.016 -0.330 0.229 -1.422 -9.0 -0.414 0.06564 -0.042 0.552 0.014 1.000 0.016 -6.307 0.226 0.148 -8.5 -0.351 0.06009 -0.046 0.535 0.014 1.000 0.016 -5.835 0.311 0.118 -8.0 -0.287 0.05685 -0.050 0.529 0.014 1.000 0.016 -5.049 0.311 0.075 -7.5 -0.223 0.05219 -0.054 0.517 0.015 1.000 0.016 -4.280 0.312 0.008 -7.0 -0.160 0.04776 -0.058 0.505 0.015 1.000 0.016 -3.343 0.312 -0.113 -6.5 -0.096 0.04470 -0.062 0.489 0.015 1.000 0.017 -2.150 0.313 -0.394 -6.0 -0.033 0.04151 -0.066 0.471 0.015 1.000 0.017 -0.791 0.313 -1.758 -5.5 0.030 0.03814 -0.070 0.460 0.015 1.000 0.017 0.789 0.314 2.575 -5.0 0.093 0.03572 -0.074 0.446 0.016 1.000 0.018 2.592 0.315 1.049 -4.5 0.155 0.03340 -0.078 0.432 0.016 1.000 0.018 4.628 0.316 0.755 -4.0 0.216 0.03065 -0.082 0.421 0.017 1.000 0.019 7.045 0.317 0.630 -3.5 0.277 0.02815 -0.086 0.410 0.017 1.000 0.019 9.829 0.318 0.562 -3.0 0.337 0.02649 -0.090 0.396 0.017 1.000 0.020 12.710 0.319 0.518 -2.5 0.396 0.02459 -0.095 0.389 0.017 1.000 0.020 16.097 0.321 0.489 -2.0 0.454 0.02254 -0.099 0.378 0.017 1.000 0.020 20.150 0.322 0.467 -1.5 0.512 0.02092 -0.103 0.371 0.017 1.000 0.021 24.463 0.323 0.451 -1.0 0.568 0.02155 -0.107 0.367 0.018 1.000 0.022 26.374 0.325 0.438 -0.5 0.624 0.01768 -0.111 0.360 0.020 1.000 0.024 35.270 0.327 0.428 0.0 0.678 0.01380 -0.115 0.357 0.022 1.000 0.036 49.110 0.466 0.420 0.5 0.656 0.02114 -0.118 0.353 0.024 0.886 0.968 31.026 0.646 0.430 1.0 0.693 0.02203 -0.121 0.349 0.042 0.852 0.969 31.434 0.340 0.425 1.5 0.728 0.02311 -0.125 0.346 0.050 0.817 0.970 31.512 0.353 0.421 2.0 0.763 0.02424 -0.129 0.342 0.932 0.783 0.951 31.466 0.360 0.419 2.5 0.799 0.02592 -0.133 0.339 0.934 0.751 0.951 30.808 0.366 0.416 3.0 0.833 0.02755 -0.137 0.335 0.937 0.720 0.951 30.246 0.377 0.414 3.5 0.867 0.02957 -0.141 0.332 0.939 0.689 0.952 29.317 0.484 0.413 4.0 0.876 0.03250 -0.147 0.332 0.942 0.621 0.952 26.964 0.403 0.418 4.5 0.929 0.03350 -0.151 0.329 0.947 0.622 0.952 27.742 0.377 0.412 5.0 0.950 0.03685 -0.156 0.329 0.950 0.574 0.952 25.771 0.414 0.414 5.5 0.990 0.03844 -0.161 0.326 0.953 0.558 0.954 25.770 0.365 0.412 6.0 1.031 0.04016 -0.165 0.323 0.953 0.541 0.955 25.662 0.415 0.411 6.5 1.052 0.04384 -0.171 0.323 0.953 0.499 0.955 24.000 0.405 0.412 7.0 1.096 0.04652 -0.176 0.319 0.951 0.489 0.952 23.558 0.356 0.410 7.5 1.139 0.04841 -0.180 0.316 0.951 0.479 0.953 23.539 0.354 0.408 8.0 1.185 0.04980 -0.185 0.313 0.953 0.473 0.955 23.787 0.393 0.406 8.5 1.210 0.05397 -0.190 0.313 0.954 0.436 0.956 22.413 0.230 0.407 9.0 1.504 0.04447 -0.178 0.026 0.956 0.742 0.958 33.819 0.231 0.369 9.5 1.534 0.04665 -0.184 0.023 0.956 0.717 0.958 32.890 0.461 0.370 10.0 1.559 0.05098 -0.190 0.021 0.956 0.687 0.958 30.575 0.474 0.372 10.5 1.586 0.05452 -0.195 0.021 0.957 0.665 0.958 29.091 0.492 0.373 11.0 1.606 0.05835 -0.201 0.019 0.957 0.637 0.958 27.528 0.569 0.375 11.5 1.623 0.06265 -0.207 0.017 0.957 0.610 0.958 25.912 0.050 0.378 12.0 1.515 0.07020 -0.220 0.014 0.952 0.027 0.954 21.579 0.481 0.395 12.5 1.669 0.07245 -0.218 0.011 0.952 0.575 0.954 23.042 0.274 0.381 13.0 1.683 0.07594 -0.224 0.010 0.952 0.552 0.954 22.167 0.051 0.383 13.5 1.597 0.08445 -0.233 0.008 0.952 0.023 0.954 18.906 0.042 0.396 14.0 1.621 0.08931 -0.237 0.007 0.957 0.020 0.959 18.154 0.430 0.396 14.5 1.643 0.09517 -0.241 0.007 0.952 0.017 0.954 17.260 0.444 0.397 15.0 1.663 0.09797 -0.245 0.006 0.957 0.012 0.959 16.977 0.445 0.397 Name = GOE 573 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 -0.327 0.13277 0.002 0.800 0.012 1.000 0.015 -2.466 0.431 0.255 -14.5 -0.308 0.12882 -0.002 0.783 0.013 1.000 0.014 -2.391 0.424 0.244 -14.0 -0.287 0.11781 -0.005 0.766 0.013 1.000 0.014 -2.434 0.410 0.231 -13.5 -0.264 0.10976 -0.009 0.755 0.013 1.000 0.015 -2.402 0.399 0.216 -13.0 -0.239 0.10245 -0.013 0.739 0.013 1.000 0.015 -2.331 0.390 0.198 -12.5 -0.212 0.09881 -0.016 0.727 0.014 1.000 0.015 -2.149 0.383 0.174 -12.0 -0.184 0.09474 -0.020 0.711 0.013 1.000 0.015 -1.944 0.377 0.143 -11.5 -0.154 0.08849 -0.023 0.694 0.014 1.000 0.015 -1.745 0.372 0.098 -11.0 -0.123 0.08162 -0.027 0.605 0.014 1.000 0.015 -1.512 0.368 0.029 -10.5 -0.091 0.07701 -0.031 0.588 0.014 1.000 0.015 -1.182 0.364 -0.090 -10.0 -0.057 0.06983 -0.035 0.576 0.014 1.000 0.016 -0.822 0.362 -0.355 -9.5 -0.023 0.06441 -0.039 0.564 0.014 1.000 0.016 -0.358 0.229 -1.422 -9.0 -0.414 0.06056 -0.042 0.552 0.014 1.000 0.016 -6.836 0.226 0.148 -8.5 -0.351 0.05743 -0.046 0.535 0.014 1.000 0.016 -6.105 0.311 0.118 -8.0 -0.287 0.05255 -0.050 0.529 0.014 1.000 0.016 -5.462 0.311 0.075 -7.5 -0.223 0.04877 -0.054 0.517 0.015 1.000 0.016 -4.579 0.312 0.008 -7.0 -0.160 0.04539 -0.058 0.505 0.015 1.000 0.016 -3.518 0.312 -0.113 -6.5 -0.096 0.04259 -0.062 0.489 0.015 1.000 0.017 -2.257 0.313 -0.394 -6.0 -0.033 0.03900 -0.066 0.471 0.015 1.000 0.017 -0.842 0.313 -1.758 -5.5 0.030 0.03626 -0.070 0.460 0.015 1.000 0.018 0.830 0.314 2.575 -5.0 0.093 0.03393 -0.074 0.446 0.016 1.000 0.018 2.729 0.315 1.049 -4.5 0.155 0.03110 -0.078 0.432 0.016 1.000 0.018 4.970 0.316 0.755 -4.0 0.216 0.02894 -0.082 0.421 0.017 1.000 0.019 7.462 0.317 0.630 -3.5 0.277 0.02649 -0.086 0.410 0.017 1.000 0.019 10.444 0.318 0.562 -3.0 0.337 0.02479 -0.090 0.396 0.017 1.000 0.020 13.578 0.319 0.518 -2.5 0.396 0.02289 -0.094 0.389 0.017 1.000 0.020 17.290 0.321 0.489 -2.0 0.454 0.02155 -0.099 0.378 0.017 1.000 0.021 21.079 0.322 0.467 -1.5 0.512 0.01974 -0.103 0.371 0.017 1.000 0.021 25.925 0.323 0.451 -1.0 0.568 0.02047 -0.107 0.367 0.018 1.000 0.022 27.767 0.325 0.438 -0.5 0.624 0.01590 -0.111 0.360 0.020 1.000 0.025 39.207 0.327 0.428 0.0 0.678 0.01234 -0.115 0.357 0.022 1.000 0.045 54.930 0.305 0.420 0.5 0.738 0.01620 -0.118 0.353 0.024 1.000 0.970 45.541 0.284 0.409 1.0 0.797 0.01616 -0.120 0.349 0.042 1.000 0.971 49.336 0.284 0.400 1.5 0.857 0.01618 -0.122 0.346 0.050 1.000 0.971 52.985 0.472 0.392 2.0 0.828 0.02009 -0.126 0.342 0.932 0.886 0.951 41.241 1.039 0.403 2.5 0.868 0.02124 -0.130 0.339 0.934 0.858 0.951 40.852 0.348 0.400 3.0 0.904 0.02220 -0.134 0.335 0.937 0.827 0.951 40.722 0.363 0.398 3.5 0.939 0.02358 -0.138 0.332 0.939 0.796 0.952 39.817 0.410 0.397 4.0 0.961 0.02576 -0.143 0.332 0.942 0.748 0.952 37.317 0.376 0.399 4.5 1.009 0.02645 -0.147 0.329 0.947 0.738 0.952 38.153 0.418 0.395 5.0 1.020 0.02966 -0.153 0.329 0.950 0.677 0.952 34.378 0.502 0.400 5.5 1.053 0.03151 -0.158 0.326 0.953 0.648 0.954 33.401 0.398 0.400 6.0 1.086 0.03380 -0.163 0.323 0.953 0.622 0.955 32.148 0.461 0.400 6.5 1.104 0.03690 -0.169 0.323 0.953 0.574 0.955 29.912 0.436 0.403 7.0 1.144 0.03927 -0.173 0.319 0.951 0.558 0.952 29.125 0.366 0.402 7.5 1.185 0.04145 -0.178 0.316 0.951 0.545 0.953 28.591 0.360 0.400 8.0 1.228 0.04307 -0.183 0.313 0.953 0.535 0.955 28.523 0.428 0.399 8.5 1.245 0.04701 -0.189 0.313 0.954 0.489 0.956 26.478 0.226 0.402 9.0 1.540 0.03963 -0.175 0.026 0.956 0.782 0.958 38.859 0.226 0.364 9.5 1.573 0.04222 -0.181 0.023 0.956 0.760 0.958 37.271 0.446 0.365 10.0 1.598 0.04638 -0.187 0.021 0.956 0.730 0.958 34.449 0.490 0.367 10.5 1.623 0.04934 -0.192 0.021 0.957 0.705 0.958 32.883 0.510 0.369 11.0 1.643 0.05256 -0.198 0.019 0.957 0.677 0.958 31.263 0.564 0.371 11.5 1.661 0.05635 -0.204 0.017 0.957 0.650 0.958 29.476 0.699 0.373 12.0 1.671 0.06248 -0.211 0.014 0.952 0.617 0.954 26.743 0.597 0.376 12.5 1.695 0.06655 -0.216 0.011 0.952 0.602 0.954 25.464 0.518 0.377 13.0 1.711 0.07066 -0.222 0.010 0.952 0.582 0.954 24.213 0.666 0.380 13.5 1.722 0.07474 -0.227 0.008 0.952 0.560 0.954 23.038 0.092 0.382 14.0 1.614 0.08296 -0.237 0.007 0.957 0.024 0.959 19.459 0.091 0.397 14.5 1.636 0.08778 -0.241 0.007 0.952 0.021 0.954 18.636 0.449 0.397 15.0 1.655 0.09131 -0.245 0.006 0.957 0.017 0.959 18.131 0.456 0.398