Name = RAF 25 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 -0.502 0.37299 0.065 0.940 0.002 1.000 0.003 -1.345 -0.078 0.380 -14.5 -0.511 0.33779 0.062 0.940 0.002 1.000 0.003 -1.513 -0.118 0.371 -14.0 -0.519 0.27779 0.059 0.935 0.002 1.000 0.003 -1.867 -0.252 0.364 -13.5 -0.524 0.26696 0.056 0.930 0.002 1.000 0.004 -1.961 -0.597 0.357 -13.0 -0.526 0.22751 0.053 0.930 0.002 1.000 0.004 -2.312 -2.925 0.350 -12.5 -0.526 0.20687 0.050 0.925 0.002 1.000 0.004 -2.540 1.946 0.344 -12.0 -0.522 0.18581 0.046 0.920 0.002 1.000 0.004 -2.811 0.896 0.339 -11.5 -0.516 0.15666 0.043 0.920 0.003 1.000 0.004 -3.292 0.640 0.334 -11.0 -0.506 0.14542 0.040 0.915 0.003 1.000 0.004 -3.479 0.528 0.329 -10.5 -0.493 0.12411 0.037 0.915 0.003 1.000 0.005 -3.970 0.467 0.325 -10.0 -0.476 0.11131 0.034 0.910 0.003 1.000 0.005 -4.280 0.429 0.320 -9.5 -0.457 0.09965 0.030 0.905 0.004 1.000 0.006 -4.584 0.402 0.316 -9.0 -0.434 0.08799 0.027 0.900 0.004 1.000 0.007 -4.935 0.383 0.313 -8.5 -0.409 0.08037 0.024 0.880 0.006 1.000 0.009 -5.083 0.368 0.309 -8.0 -0.380 0.07154 0.021 0.870 0.007 1.000 0.011 -5.307 0.357 0.305 -7.5 -0.349 0.06678 0.018 0.855 0.010 1.000 0.014 -5.220 0.355 0.300 -7.0 -0.318 0.06135 0.014 0.844 0.013 1.000 0.016 -5.189 0.356 0.295 -6.5 -0.287 0.05415 0.011 0.836 0.014 1.000 0.016 -5.299 0.354 0.288 -6.0 -0.255 0.04702 0.008 0.828 0.015 1.000 0.017 -5.414 0.350 0.280 -5.5 -0.221 0.04198 0.004 0.820 0.015 1.000 0.018 -5.260 0.348 0.270 -5.0 -0.187 0.03840 0.001 0.813 0.016 1.000 0.018 -4.864 0.347 0.255 -4.5 -0.152 0.03659 -0.002 0.805 0.016 1.000 0.019 -4.163 0.347 0.235 -4.0 -0.118 0.03341 -0.006 0.791 0.017 0.947 0.020 -3.521 0.346 0.202 -3.5 -0.083 0.03017 -0.009 0.776 0.017 0.945 0.020 -2.743 0.345 0.141 -3.0 -0.047 0.02744 -0.012 0.762 0.019 0.939 0.023 -1.713 0.345 -0.013 -2.5 -0.012 0.02543 -0.016 0.749 0.020 0.937 0.023 -0.469 0.085 -1.072 -2.0 -0.088 0.02331 -0.019 0.736 0.022 0.931 0.026 -3.765 -0.999 0.032 -1.5 -0.022 0.02072 -0.028 0.725 0.024 0.923 0.955 -1.063 0.344 -1.038 -1.0 0.025 0.02254 -0.030 0.715 0.629 0.915 0.951 1.117 0.278 1.432 -0.5 0.080 0.02232 -0.031 0.704 0.687 0.905 0.950 3.596 0.284 0.639 0.0 0.112 0.02209 -0.033 0.681 0.742 0.908 0.942 5.054 0.289 0.543 0.5 0.164 0.02239 -0.034 0.659 0.798 0.905 0.932 7.332 0.285 0.460 1.0 0.215 0.02245 -0.036 0.641 0.813 0.897 0.932 9.585 0.289 0.419 1.5 0.264 0.02280 -0.038 0.625 0.819 0.884 0.937 11.593 0.258 0.395 2.0 0.355 0.02012 -0.037 0.049 0.829 1.000 0.940 17.644 4.469 0.355 2.5 0.267 0.02441 -0.050 0.025 0.842 0.049 0.942 10.941 -0.089 0.437 3.0 0.308 0.02631 -0.053 0.022 0.853 0.033 0.945 11.714 0.333 0.423 3.5 0.346 0.02883 -0.057 0.020 0.863 0.024 0.947 12.003 0.341 0.413 4.0 0.381 0.03133 -0.060 0.018 0.874 0.022 0.947 12.174 0.346 0.407 4.5 0.416 0.03462 -0.063 0.017 0.887 0.021 0.947 12.024 0.347 0.402 5.0 0.450 0.03848 -0.067 0.016 0.900 0.020 0.947 11.706 0.348 0.398 5.5 0.484 0.04134 -0.070 0.015 0.905 0.018 0.947 11.718 0.352 0.394 6.0 0.516 0.04763 -0.073 0.015 0.905 0.018 0.950 10.844 0.356 0.392 6.5 0.547 0.05260 -0.077 0.013 0.911 0.016 0.950 10.405 0.360 0.390 7.0 0.577 0.05778 -0.080 0.010 0.911 0.015 0.950 9.978 0.361 0.389 7.5 0.606 0.06267 -0.083 0.007 0.916 0.011 0.950 9.671 0.363 0.387 8.0 0.634 0.06784 -0.086 0.006 0.922 0.009 0.956 9.342 0.377 0.386 8.5 0.657 0.07623 -0.090 0.004 0.922 0.007 0.956 8.624 0.399 0.386 9.0 0.678 0.08726 -0.093 0.004 0.922 0.006 0.956 7.765 0.429 0.387 9.5 0.694 0.09853 -0.096 0.003 0.928 0.005 0.956 7.043 0.473 0.389 10.0 0.707 0.11136 -0.099 0.003 0.928 0.005 0.956 6.346 0.551 0.391 10.5 0.716 0.12173 -0.103 0.003 0.928 0.004 0.956 5.879 0.709 0.393 11.0 0.721 0.14497 -0.106 0.002 0.933 0.004 0.951 4.972 1.236 0.397 11.5 0.722 0.16641 -0.109 0.002 0.933 0.004 0.951 4.340 -8.088 0.401 12.0 0.720 0.18645 -0.112 0.002 0.933 0.003 0.951 3.862 -0.559 0.406 12.5 0.714 0.19665 -0.116 0.002 0.939 0.003 0.951 3.632 -0.190 0.412 13.0 0.706 0.24204 -0.119 0.002 0.939 0.003 0.956 2.915 -0.061 0.418 13.5 0.694 0.25466 -0.122 0.002 0.939 0.003 0.957 2.724 0.008 0.426 14.0 0.679 0.31176 -0.125 0.002 0.939 0.003 0.951 2.178 0.047 0.434 14.5 0.662 0.34254 -0.128 0.002 0.944 0.003 0.957 1.933 0.071 0.444 15.0 0.644 0.37883 -0.132 0.002 0.944 0.003 0.957 1.699 0.080 0.454 Name = RAF 25 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 -0.502 0.27245 0.065 0.940 0.002 1.000 0.004 -1.841 -0.078 0.380 -14.5 -0.511 0.24449 0.062 0.940 0.002 1.000 0.004 -2.090 -0.120 0.371 -14.0 -0.518 0.22077 0.059 0.935 0.002 1.000 0.004 -2.348 -0.253 0.364 -13.5 -0.523 0.19497 0.056 0.930 0.002 1.000 0.004 -2.685 -0.601 0.357 -13.0 -0.526 0.17780 0.053 0.930 0.002 1.000 0.004 -2.957 -3.184 0.350 -12.5 -0.525 0.16162 0.050 0.925 0.002 1.000 0.004 -3.250 1.930 0.344 -12.0 -0.522 0.14506 0.046 0.920 0.002 1.000 0.004 -3.598 0.883 0.339 -11.5 -0.515 0.12969 0.043 0.920 0.003 1.000 0.005 -3.973 0.637 0.334 -11.0 -0.505 0.11440 0.040 0.915 0.003 1.000 0.005 -4.418 0.527 0.329 -10.5 -0.492 0.10093 0.037 0.915 0.003 1.000 0.005 -4.877 0.466 0.325 -10.0 -0.476 0.08961 0.034 0.910 0.003 1.000 0.006 -5.310 0.428 0.321 -9.5 -0.456 0.08195 0.030 0.905 0.004 1.000 0.007 -5.565 0.401 0.317 -9.0 -0.433 0.07079 0.027 0.900 0.004 1.000 0.008 -6.123 0.382 0.313 -8.5 -0.408 0.06562 0.024 0.880 0.006 1.000 0.009 -6.210 0.366 0.309 -8.0 -0.378 0.05997 0.021 0.870 0.007 1.000 0.012 -6.305 0.359 0.305 -7.5 -0.348 0.05359 0.018 0.855 0.010 1.000 0.014 -6.503 0.359 0.300 -7.0 -0.318 0.04896 0.014 0.844 0.013 1.000 0.016 -6.502 0.357 0.295 -6.5 -0.287 0.04423 0.011 0.836 0.014 1.000 0.016 -6.487 0.353 0.288 -6.0 -0.254 0.04066 0.008 0.828 0.015 1.000 0.017 -6.258 0.350 0.280 -5.5 -0.221 0.03612 0.004 0.820 0.015 1.000 0.018 -6.110 0.348 0.270 -5.0 -0.187 0.03303 0.001 0.813 0.016 1.000 0.018 -5.651 0.347 0.255 -4.5 -0.152 0.03030 -0.002 0.805 0.016 1.000 0.019 -5.023 0.347 0.235 -4.0 -0.117 0.02830 -0.006 0.791 0.017 1.000 0.020 -4.150 0.346 0.202 -3.5 -0.083 0.02531 -0.009 0.776 0.017 1.000 0.021 -3.263 0.345 0.141 -3.0 -0.047 0.02300 -0.012 0.762 0.019 1.000 0.023 -2.037 0.345 -0.014 -2.5 -0.012 0.02127 -0.016 0.749 0.020 1.000 0.024 -0.543 -0.245 -1.114 -2.0 -0.076 0.01651 -0.027 0.736 0.022 1.000 0.956 -4.621 -0.931 -0.103 -1.5 -0.022 0.01494 -0.028 0.725 0.024 1.000 0.957 -1.490 0.278 -1.026 -1.0 0.025 0.01509 -0.030 0.715 0.629 1.000 0.953 1.668 0.278 1.433 -0.5 0.080 0.01459 -0.031 0.704 0.687 1.000 0.952 5.503 0.277 0.639 0.0 0.135 0.01425 -0.033 0.681 0.742 1.000 0.951 9.494 0.274 0.492 0.5 0.190 0.01488 -0.034 0.659 0.798 1.000 0.950 12.792 0.271 0.428 1.0 0.245 0.01446 -0.035 0.641 0.813 1.000 0.950 16.964 0.271 0.393 1.5 0.300 0.01396 -0.036 0.625 0.819 1.000 0.950 21.511 0.271 0.371 2.0 0.355 0.01593 -0.037 0.049 0.829 1.000 0.951 22.285 0.271 0.355 2.5 0.410 0.01675 -0.039 0.025 0.842 1.000 0.951 24.455 -0.058 0.344 3.0 0.303 0.02310 -0.053 0.022 0.853 0.047 0.951 13.127 -0.027 0.426 3.5 0.345 0.02494 -0.057 0.020 0.863 0.028 0.951 13.823 0.334 0.414 4.0 0.381 0.02738 -0.060 0.018 0.874 0.023 0.951 13.904 0.344 0.407 4.5 0.416 0.02959 -0.063 0.017 0.887 0.022 0.950 14.053 0.346 0.402 5.0 0.450 0.03250 -0.067 0.016 0.900 0.020 0.950 13.854 0.348 0.398 5.5 0.484 0.03605 -0.070 0.015 0.905 0.019 0.950 13.424 0.351 0.395 6.0 0.516 0.03896 -0.073 0.015 0.905 0.018 0.950 13.254 0.355 0.392 6.5 0.547 0.04441 -0.077 0.013 0.911 0.017 0.951 12.321 0.361 0.390 7.0 0.576 0.04873 -0.080 0.010 0.911 0.015 0.951 11.824 0.364 0.389 7.5 0.604 0.05285 -0.083 0.007 0.916 0.012 0.951 11.437 0.365 0.388 8.0 0.632 0.05735 -0.086 0.006 0.922 0.009 0.956 11.028 0.375 0.387 8.5 0.656 0.06409 -0.090 0.004 0.922 0.008 0.956 10.241 0.397 0.387 9.0 0.677 0.06975 -0.093 0.004 0.922 0.006 0.956 9.705 0.426 0.387 9.5 0.693 0.07913 -0.096 0.003 0.928 0.006 0.956 8.762 0.473 0.389 10.0 0.706 0.09066 -0.099 0.003 0.928 0.005 0.956 7.789 0.550 0.391 10.5 0.715 0.10038 -0.103 0.003 0.928 0.005 0.957 7.124 0.702 0.394 11.0 0.721 0.11463 -0.106 0.002 0.933 0.004 0.951 6.285 1.205 0.397 11.5 0.722 0.12903 -0.109 0.002 0.933 0.004 0.951 5.595 -10.863 0.401 12.0 0.720 0.13912 -0.112 0.002 0.933 0.003 0.951 5.175 -0.564 0.406 12.5 0.714 0.15677 -0.116 0.002 0.939 0.004 0.951 4.554 -0.191 0.412 13.0 0.705 0.18078 -0.119 0.002 0.939 0.003 0.957 3.902 -0.062 0.418 13.5 0.693 0.20705 -0.122 0.002 0.939 0.003 0.957 3.349 0.008 0.426 14.0 0.679 0.23056 -0.125 0.002 0.939 0.003 0.951 2.945 0.047 0.434 14.5 0.662 0.24723 -0.128 0.002 0.944 0.003 0.957 2.678 0.071 0.444 15.0 0.643 0.27586 -0.132 0.002 0.944 0.003 0.957 2.333 0.080 0.454 Name = RAF 25 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 -0.501 0.22922 0.065 0.940 0.002 1.000 0.004 -2.188 -0.078 0.380 -14.5 -0.511 0.20501 0.062 0.940 0.002 1.000 0.004 -2.492 -0.121 0.371 -14.0 -0.518 0.18335 0.059 0.935 0.002 1.000 0.004 -2.826 -0.254 0.364 -13.5 -0.523 0.16395 0.056 0.930 0.002 1.000 0.004 -3.192 -0.602 0.357 -13.0 -0.526 0.14704 0.053 0.930 0.002 1.000 0.004 -3.574 -3.215 0.350 -12.5 -0.525 0.13388 0.050 0.925 0.002 1.000 0.004 -3.922 1.922 0.344 -12.0 -0.522 0.12060 0.046 0.920 0.002 1.000 0.004 -4.326 0.872 0.339 -11.5 -0.515 0.11315 0.043 0.920 0.003 1.000 0.005 -4.551 0.630 0.334 -11.0 -0.505 0.10099 0.040 0.915 0.003 1.000 0.005 -5.001 0.525 0.329 -10.5 -0.492 0.08813 0.037 0.915 0.003 1.000 0.006 -5.580 0.464 0.325 -10.0 -0.475 0.07977 0.034 0.910 0.003 1.000 0.006 -5.958 0.427 0.321 -9.5 -0.455 0.07192 0.030 0.905 0.004 1.000 0.007 -6.333 0.400 0.317 -9.0 -0.432 0.06435 0.027 0.900 0.004 1.000 0.009 -6.720 0.381 0.313 -8.5 -0.406 0.05967 0.024 0.880 0.006 1.000 0.010 -6.810 0.365 0.309 -8.0 -0.377 0.05437 0.021 0.870 0.007 1.000 0.013 -6.933 0.361 0.305 -7.5 -0.348 0.05071 0.018 0.855 0.010 1.000 0.015 -6.868 0.361 0.300 -7.0 -0.318 0.04577 0.014 0.844 0.013 1.000 0.016 -6.952 0.357 0.295 -6.5 -0.287 0.04127 0.011 0.836 0.014 1.000 0.017 -6.950 0.354 0.288 -6.0 -0.254 0.03663 0.008 0.828 0.015 1.000 0.017 -6.947 0.350 0.280 -5.5 -0.221 0.03403 0.004 0.820 0.015 1.000 0.018 -6.481 0.348 0.270 -5.0 -0.187 0.02991 0.001 0.813 0.016 1.000 0.018 -6.239 0.348 0.255 -4.5 -0.152 0.02731 -0.002 0.805 0.016 1.000 0.019 -5.571 0.346 0.235 -4.0 -0.117 0.02623 -0.006 0.791 0.017 1.000 0.020 -4.473 0.346 0.202 -3.5 -0.082 0.02357 -0.009 0.776 0.017 1.000 0.021 -3.489 0.345 0.140 -3.0 -0.047 0.02114 -0.012 0.762 0.019 1.000 0.024 -2.201 0.345 -0.016 -2.5 -0.011 0.01917 -0.016 0.749 0.020 1.000 0.024 -0.588 -0.237 -1.147 -2.0 -0.077 0.01407 -0.027 0.736 0.022 1.000 0.958 -5.441 -0.875 -0.103 -1.5 -0.023 0.01375 -0.028 0.725 0.024 1.000 0.958 -1.639 0.278 -1.011 -1.0 0.025 0.01215 -0.030 0.715 0.629 1.000 0.954 2.073 0.278 1.434 -0.5 0.080 0.01243 -0.031 0.704 0.687 1.000 0.953 6.458 0.276 0.639 0.0 0.135 0.01232 -0.033 0.681 0.742 1.000 0.952 10.980 0.274 0.492 0.5 0.190 0.01186 -0.034 0.659 0.798 1.000 0.951 16.052 0.271 0.428 1.0 0.245 0.01226 -0.035 0.641 0.813 1.000 0.951 20.008 0.271 0.393 1.5 0.300 0.01223 -0.036 0.625 0.819 1.000 0.951 24.541 0.271 0.371 2.0 0.355 0.01368 -0.037 0.049 0.829 1.000 0.951 25.949 0.271 0.355 2.5 0.410 0.01429 -0.039 0.025 0.842 1.000 0.951 28.671 0.271 0.344 3.0 0.464 0.01469 -0.040 0.022 0.853 1.000 0.951 31.590 -0.014 0.336 3.5 0.341 0.02319 -0.057 0.020 0.863 0.038 0.951 14.698 0.009 0.416 4.0 0.380 0.02517 -0.060 0.018 0.874 0.024 0.951 15.103 0.338 0.408 4.5 0.415 0.02793 -0.063 0.017 0.887 0.022 0.951 14.867 0.346 0.402 5.0 0.450 0.03050 -0.067 0.016 0.900 0.021 0.951 14.746 0.348 0.398 5.5 0.483 0.03401 -0.070 0.015 0.905 0.020 0.951 14.215 0.351 0.395 6.0 0.516 0.03701 -0.073 0.015 0.905 0.018 0.951 13.942 0.355 0.392 6.5 0.547 0.04060 -0.077 0.013 0.911 0.017 0.951 13.472 0.361 0.390 7.0 0.576 0.04462 -0.080 0.010 0.911 0.016 0.951 12.905 0.366 0.389 7.5 0.604 0.04716 -0.083 0.007 0.916 0.013 0.951 12.803 0.367 0.388 8.0 0.631 0.05211 -0.086 0.006 0.922 0.010 0.956 12.116 0.375 0.387 8.5 0.656 0.05737 -0.090 0.004 0.922 0.008 0.956 11.426 0.396 0.387 9.0 0.676 0.06375 -0.093 0.004 0.922 0.007 0.957 10.605 0.425 0.387 9.5 0.693 0.07044 -0.096 0.003 0.928 0.006 0.956 9.835 0.469 0.389 10.0 0.706 0.07899 -0.099 0.003 0.928 0.005 0.957 8.935 0.546 0.391 10.5 0.715 0.08760 -0.103 0.003 0.928 0.005 0.957 8.159 0.701 0.394 11.0 0.720 0.10133 -0.106 0.002 0.933 0.004 0.951 7.107 1.201 0.397 11.5 0.722 0.11306 -0.109 0.002 0.933 0.004 0.951 6.382 -11.570 0.401 12.0 0.720 0.12518 -0.112 0.002 0.933 0.004 0.951 5.749 -0.568 0.406 12.5 0.714 0.14059 -0.116 0.002 0.939 0.004 0.951 5.076 -0.196 0.412 13.0 0.705 0.15431 -0.119 0.002 0.939 0.003 0.957 4.570 -0.064 0.419 13.5 0.693 0.17442 -0.122 0.002 0.939 0.003 0.957 3.975 0.008 0.426 14.0 0.679 0.19595 -0.125 0.002 0.939 0.003 0.951 3.464 0.046 0.434 14.5 0.662 0.20652 -0.128 0.002 0.944 0.003 0.957 3.205 0.071 0.444 15.0 0.643 0.23146 -0.132 0.002 0.944 0.003 0.957 2.780 0.080 0.455 Name = RAF 25 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 -0.501 0.20346 0.065 0.940 0.002 1.000 0.004 -2.464 -0.079 0.380 -14.5 -0.511 0.18148 0.062 0.940 0.002 1.000 0.004 -2.815 -0.123 0.372 -14.0 -0.518 0.17301 0.059 0.935 0.002 1.000 0.004 -2.994 -0.258 0.364 -13.5 -0.523 0.15504 0.056 0.930 0.002 1.000 0.004 -3.374 -0.606 0.357 -13.0 -0.525 0.13631 0.053 0.930 0.002 1.000 0.005 -3.854 -3.280 0.350 -12.5 -0.525 0.12398 0.050 0.925 0.002 1.000 0.005 -4.233 1.906 0.344 -12.0 -0.521 0.11134 0.046 0.920 0.002 1.000 0.005 -4.684 0.870 0.339 -11.5 -0.515 0.10285 0.043 0.920 0.003 1.000 0.005 -5.003 0.627 0.334 -11.0 -0.505 0.09255 0.040 0.915 0.003 1.000 0.006 -5.453 0.522 0.329 -10.5 -0.491 0.08240 0.037 0.915 0.003 1.000 0.006 -5.961 0.462 0.325 -10.0 -0.474 0.07582 0.034 0.910 0.003 1.000 0.007 -6.258 0.425 0.321 -9.5 -0.455 0.06735 0.030 0.905 0.004 1.000 0.008 -6.751 0.399 0.317 -9.0 -0.431 0.06038 0.027 0.900 0.004 1.000 0.009 -7.146 0.379 0.313 -8.5 -0.405 0.05604 0.024 0.880 0.006 1.000 0.011 -7.231 0.367 0.309 -8.0 -0.377 0.05152 0.021 0.870 0.007 1.000 0.014 -7.314 0.363 0.305 -7.5 -0.348 0.04690 0.018 0.855 0.010 1.000 0.016 -7.424 0.362 0.301 -7.0 -0.318 0.04246 0.014 0.844 0.013 1.000 0.016 -7.494 0.358 0.295 -6.5 -0.287 0.03849 0.011 0.836 0.014 1.000 0.017 -7.451 0.353 0.288 -6.0 -0.254 0.03504 0.008 0.828 0.015 1.000 0.018 -7.259 0.350 0.280 -5.5 -0.221 0.03142 0.004 0.820 0.015 1.000 0.018 -7.020 0.348 0.270 -5.0 -0.186 0.02880 0.001 0.813 0.016 1.000 0.019 -6.476 0.347 0.255 -4.5 -0.152 0.02617 -0.002 0.805 0.016 1.000 0.020 -5.809 0.346 0.235 -4.0 -0.117 0.02479 -0.006 0.791 0.017 1.000 0.021 -4.725 0.346 0.202 -3.5 -0.082 0.02263 -0.009 0.776 0.017 1.000 0.022 -3.626 0.345 0.140 -3.0 -0.046 0.02023 -0.012 0.762 0.019 1.000 0.024 -2.291 0.345 -0.017 -2.5 -0.011 0.01831 -0.016 0.749 0.020 1.000 0.025 -0.600 -0.232 -1.182 -2.0 -0.077 0.01269 -0.027 0.736 0.022 1.000 0.959 -6.045 -0.828 -0.102 -1.5 -0.023 0.01229 -0.028 0.725 0.024 1.000 0.960 -1.853 0.278 -0.999 -1.0 0.025 0.01097 -0.030 0.715 0.629 1.000 0.955 2.295 0.277 1.434 -0.5 0.080 0.01059 -0.031 0.704 0.687 1.000 0.954 7.581 0.276 0.639 0.0 0.135 0.01058 -0.033 0.681 0.742 1.000 0.953 12.786 0.274 0.492 0.5 0.190 0.01036 -0.034 0.659 0.798 1.000 0.952 18.374 0.271 0.428 1.0 0.245 0.01074 -0.035 0.641 0.813 1.000 0.952 22.836 0.271 0.393 1.5 0.300 0.01090 -0.036 0.625 0.819 1.000 0.952 27.537 0.271 0.371 2.0 0.355 0.01271 -0.037 0.049 0.829 1.000 0.952 27.931 0.271 0.355 2.5 0.410 0.01300 -0.039 0.025 0.842 1.000 0.952 31.508 0.271 0.344 3.0 0.464 0.01360 -0.040 0.022 0.853 1.000 0.952 34.109 -0.002 0.336 3.5 0.337 0.02217 -0.057 0.020 0.863 0.049 0.951 15.201 0.010 0.419 4.0 0.380 0.02392 -0.060 0.018 0.874 0.025 0.951 15.879 0.333 0.408 4.5 0.415 0.02635 -0.063 0.017 0.887 0.023 0.951 15.745 0.346 0.403 5.0 0.450 0.02862 -0.067 0.016 0.900 0.021 0.951 15.709 0.348 0.398 5.5 0.483 0.03136 -0.070 0.015 0.905 0.020 0.951 15.416 0.351 0.395 6.0 0.516 0.03454 -0.073 0.015 0.905 0.018 0.951 14.938 0.355 0.392 6.5 0.547 0.03868 -0.077 0.013 0.911 0.017 0.951 14.136 0.362 0.390 7.0 0.575 0.04263 -0.080 0.010 0.911 0.017 0.951 13.496 0.367 0.389 7.5 0.603 0.04663 -0.083 0.007 0.916 0.015 0.951 12.934 0.369 0.388 8.0 0.630 0.04941 -0.086 0.006 0.922 0.011 0.956 12.751 0.376 0.387 8.5 0.654 0.05444 -0.090 0.004 0.922 0.009 0.957 12.023 0.394 0.387 9.0 0.675 0.05990 -0.093 0.004 0.922 0.008 0.957 11.272 0.424 0.388 9.5 0.692 0.06708 -0.096 0.003 0.928 0.007 0.957 10.315 0.467 0.389 10.0 0.705 0.07404 -0.099 0.003 0.928 0.006 0.957 9.524 0.543 0.391 10.5 0.714 0.08301 -0.103 0.003 0.928 0.005 0.957 8.603 0.693 0.394 11.0 0.720 0.09329 -0.106 0.002 0.933 0.005 0.951 7.716 1.171 0.397 11.5 0.721 0.10373 -0.109 0.002 0.933 0.005 0.951 6.953 -12.372 0.401 12.0 0.719 0.11723 -0.112 0.002 0.933 0.004 0.951 6.136 -0.587 0.406 12.5 0.713 0.12373 -0.116 0.002 0.939 0.004 0.951 5.767 -0.201 0.412 13.0 0.705 0.13855 -0.119 0.002 0.939 0.003 0.957 5.089 -0.064 0.419 13.5 0.693 0.15530 -0.122 0.002 0.939 0.003 0.957 4.463 0.007 0.426 14.0 0.679 0.17550 -0.125 0.002 0.939 0.003 0.951 3.867 0.047 0.435 14.5 0.662 0.19615 -0.128 0.002 0.944 0.004 0.957 3.374 0.071 0.444 15.0 0.643 0.22035 -0.132 0.002 0.944 0.004 0.957 2.919 0.080 0.455