Name = EPPLER EA 6(-1)-012 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 -1.014 0.16268 0.096 0.810 0.015 1.000 0.022 -6.236 0.398 0.344 -14.5 -0.994 0.15206 0.093 0.800 0.016 1.000 0.022 -6.535 0.378 0.343 -14.0 -0.967 0.14047 0.090 0.790 0.016 1.000 0.023 -6.884 0.362 0.343 -13.5 -0.939 0.13230 0.086 0.780 0.017 1.000 0.023 -7.100 0.356 0.342 -13.0 -0.910 0.13107 0.083 0.780 0.017 1.000 0.025 -6.939 0.352 0.342 -12.5 -0.880 0.11846 0.080 0.770 0.018 1.000 0.025 -7.426 0.349 0.341 -12.0 -0.848 0.11544 0.077 0.760 0.018 1.000 0.027 -7.344 0.346 0.341 -11.5 -0.816 0.10182 0.074 0.760 0.019 1.000 0.027 -8.011 0.345 0.341 -11.0 -0.782 0.09552 0.071 0.750 0.020 1.000 0.028 -8.191 0.341 0.341 -10.5 -0.748 0.09357 0.068 0.750 0.021 1.000 0.030 -7.990 0.339 0.341 -10.0 -0.713 0.08621 0.065 0.740 0.022 1.000 0.031 -8.267 0.338 0.341 -9.5 -0.676 0.08102 0.062 0.740 0.022 1.000 0.033 -8.347 0.335 0.341 -9.0 -0.639 0.07251 0.059 0.727 0.024 1.000 0.035 -8.813 0.334 0.342 -8.5 -0.601 0.06659 0.055 0.718 0.026 1.000 0.037 -9.028 0.331 0.342 -8.0 -0.562 0.06654 0.052 0.718 0.028 0.809 0.040 -8.444 0.329 0.343 -7.5 -0.522 0.06227 0.049 0.718 0.030 0.791 0.043 -8.381 0.328 0.344 -7.0 -0.481 0.05873 0.046 0.709 0.033 0.800 0.047 -8.183 0.325 0.346 -6.5 -0.439 0.05513 0.043 0.709 0.036 0.782 0.055 -7.956 0.322 0.348 -6.0 -0.396 0.05297 0.040 0.691 0.040 0.791 0.071 -7.476 0.321 0.351 -5.5 -0.353 0.04995 0.037 0.682 0.046 0.791 0.084 -7.075 0.324 0.354 -5.0 -0.311 0.04691 0.034 0.664 0.059 0.791 0.092 -6.627 0.326 0.358 -4.5 -0.268 0.04517 0.030 0.655 0.067 0.791 0.100 -5.929 0.328 0.364 -4.0 -0.226 0.04161 0.027 0.645 0.075 0.782 0.104 -5.438 0.096 0.370 -3.5 -0.405 0.03011 0.009 0.636 0.079 0.782 0.952 -13.453 0.091 0.273 -3.0 -0.348 0.02459 0.008 0.636 0.088 0.764 0.957 -14.143 0.274 0.273 -2.5 -0.289 0.02341 0.007 0.621 0.096 0.762 0.957 -12.332 0.238 0.273 -2.0 -0.137 0.02997 0.010 0.608 0.554 0.758 0.700 -4.571 0.244 0.326 -1.5 -0.086 0.02979 0.008 0.604 0.562 0.750 0.708 -2.896 0.304 0.339 -1.0 -0.037 0.02908 0.005 0.600 0.567 0.742 0.721 -1.264 0.452 0.387 -0.5 -0.061 0.02890 0.003 0.592 0.575 0.737 0.725 -2.095 0.387 0.291 0.0 0.000 0.02806 -0.000 0.583 0.583 0.729 0.729 0.000 0.291 0.250 0.5 0.060 0.02890 -0.003 0.575 0.592 0.725 0.737 2.085 0.387 0.292 1.0 0.037 0.02908 -0.005 0.567 0.600 0.721 0.742 1.264 0.450 0.387 1.5 0.086 0.02979 -0.008 0.562 0.604 0.708 0.750 2.896 0.304 0.339 2.0 0.137 0.02997 -0.010 0.554 0.608 0.700 0.758 4.571 0.238 0.326 2.5 0.302 0.02337 -0.005 0.096 0.621 1.000 0.762 12.904 0.231 0.267 3.0 0.362 0.02454 -0.006 0.088 0.636 1.000 0.764 14.737 0.267 0.267 3.5 0.421 0.03004 -0.007 0.079 0.636 1.000 0.782 14.029 0.095 0.267 4.0 0.226 0.04161 -0.027 0.075 0.645 0.104 0.782 5.438 0.099 0.370 4.5 0.268 0.04517 -0.030 0.067 0.655 0.100 0.791 5.929 0.328 0.364 5.0 0.311 0.04691 -0.034 0.059 0.664 0.092 0.791 6.627 0.326 0.358 5.5 0.353 0.04995 -0.037 0.046 0.682 0.084 0.791 7.075 0.324 0.354 6.0 0.396 0.05297 -0.040 0.040 0.691 0.071 0.791 7.476 0.321 0.351 6.5 0.439 0.05513 -0.043 0.036 0.709 0.055 0.782 7.956 0.322 0.348 7.0 0.481 0.05873 -0.046 0.033 0.709 0.047 0.800 8.183 0.325 0.346 7.5 0.522 0.06227 -0.049 0.030 0.718 0.043 0.791 8.381 0.328 0.344 8.0 0.562 0.06654 -0.052 0.028 0.718 0.040 0.809 8.444 0.329 0.343 8.5 0.601 0.06659 -0.055 0.026 0.718 0.037 0.963 9.028 0.331 0.342 9.0 0.639 0.07251 -0.059 0.024 0.727 0.035 0.963 8.813 0.334 0.342 9.5 0.676 0.08102 -0.062 0.022 0.740 0.033 0.954 8.347 0.335 0.341 10.0 0.713 0.08621 -0.065 0.022 0.740 0.031 0.955 8.267 0.338 0.341 10.5 0.748 0.09357 -0.068 0.021 0.750 0.030 0.955 7.990 0.339 0.341 11.0 0.782 0.09552 -0.071 0.020 0.750 0.028 0.955 8.191 0.341 0.341 11.5 0.816 0.10182 -0.074 0.019 0.760 0.027 0.955 8.011 0.345 0.341 12.0 0.848 0.11544 -0.077 0.018 0.760 0.027 0.956 7.344 0.346 0.341 12.5 0.880 0.11846 -0.080 0.018 0.770 0.025 0.956 7.426 0.349 0.341 13.0 0.910 0.13107 -0.083 0.017 0.780 0.025 0.956 6.939 0.352 0.342 13.5 0.939 0.13230 -0.086 0.017 0.780 0.023 0.957 7.100 0.356 0.342 14.0 0.967 0.14047 -0.090 0.016 0.790 0.023 0.965 6.884 0.362 0.343 14.5 0.994 0.15206 -0.093 0.016 0.800 0.022 0.966 6.535 0.378 0.343 15.0 1.014 0.16268 -0.096 0.015 0.810 0.022 0.966 6.236 0.398 0.344 Name = EPPLER EA 6(-1)-012 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 -1.014 0.12717 0.096 0.810 0.015 1.000 0.024 -7.970 0.398 0.344 -14.5 -0.993 0.12242 0.093 0.800 0.016 1.000 0.024 -8.111 0.375 0.343 -14.0 -0.966 0.11822 0.090 0.790 0.016 1.000 0.026 -8.168 0.360 0.343 -13.5 -0.938 0.11323 0.087 0.780 0.017 1.000 0.026 -8.283 0.356 0.342 -13.0 -0.908 0.10783 0.084 0.780 0.017 1.000 0.028 -8.421 0.352 0.342 -12.5 -0.878 0.09945 0.081 0.770 0.018 1.000 0.028 -8.830 0.349 0.342 -12.0 -0.846 0.09283 0.077 0.760 0.018 1.000 0.030 -9.116 0.345 0.342 -11.5 -0.814 0.08837 0.074 0.760 0.019 1.000 0.031 -9.206 0.344 0.341 -11.0 -0.780 0.08269 0.071 0.750 0.020 1.000 0.032 -9.434 0.342 0.341 -10.5 -0.746 0.07603 0.068 0.750 0.021 1.000 0.033 -9.809 0.339 0.341 -10.0 -0.710 0.07321 0.065 0.740 0.022 1.000 0.035 -9.701 0.336 0.342 -9.5 -0.673 0.06813 0.062 0.740 0.022 1.000 0.037 -9.884 0.334 0.342 -9.0 -0.636 0.06217 0.059 0.727 0.024 1.000 0.040 -10.226 0.332 0.343 -8.5 -0.597 0.05753 0.056 0.718 0.026 1.000 0.042 -10.383 0.330 0.343 -8.0 -0.558 0.05458 0.053 0.718 0.028 1.000 0.046 -10.214 0.328 0.344 -7.5 -0.517 0.05126 0.049 0.718 0.030 1.000 0.049 -10.087 0.323 0.346 -7.0 -0.476 0.04809 0.047 0.709 0.033 1.000 0.067 -9.889 0.320 0.348 -6.5 -0.433 0.04528 0.044 0.709 0.036 1.000 0.084 -9.572 0.322 0.351 -6.0 -0.391 0.04160 0.040 0.691 0.040 1.000 0.096 -9.400 0.108 0.353 -5.5 -0.596 0.02297 0.020 0.682 0.046 1.000 0.858 -25.952 0.107 0.284 -5.0 -0.580 0.02152 0.013 0.664 0.059 1.000 0.951 -26.953 0.365 0.273 -4.5 -0.522 0.02121 0.012 0.655 0.067 1.000 0.952 -24.625 0.274 0.273 -4.0 -0.464 0.02061 0.011 0.645 0.075 1.000 0.953 -22.516 0.273 0.273 -3.5 -0.406 0.01886 0.009 0.636 0.079 1.000 0.953 -21.503 0.274 0.273 -3.0 -0.348 0.01426 0.008 0.636 0.088 1.000 0.958 -24.412 0.274 0.272 -2.5 -0.289 0.01593 0.006 0.621 0.096 1.000 0.959 -18.145 0.240 0.272 -2.0 -0.157 0.01935 0.010 0.608 0.554 1.000 0.746 -8.096 0.246 0.312 -1.5 -0.105 0.02139 0.007 0.604 0.562 0.800 0.754 -4.907 0.299 0.318 -1.0 -0.055 0.02069 0.005 0.600 0.567 0.792 0.767 -2.635 0.297 0.335 -0.5 -0.002 0.02103 0.002 0.592 0.575 0.787 0.775 -0.096 0.335 1.385 0.0 0.000 0.02040 -0.000 0.583 0.583 0.779 0.779 0.000 1.385 0.250 0.5 0.002 0.02103 -0.002 0.575 0.592 0.775 0.787 0.096 0.335 1.385 1.0 0.055 0.02069 -0.005 0.567 0.600 0.767 0.792 2.635 0.297 0.335 1.5 0.105 0.02139 -0.007 0.562 0.604 0.754 0.800 4.907 0.299 0.318 2.0 0.157 0.01935 -0.010 0.554 0.608 0.746 0.957 8.096 0.240 0.312 2.5 0.302 0.01589 -0.005 0.096 0.621 1.000 0.957 18.977 0.233 0.267 3.0 0.362 0.01421 -0.006 0.088 0.636 1.000 0.962 25.439 0.267 0.267 3.5 0.421 0.01880 -0.007 0.079 0.636 1.000 0.963 22.420 0.267 0.267 4.0 0.481 0.02054 -0.008 0.075 0.645 1.000 0.964 23.418 0.267 0.267 4.5 0.540 0.02113 -0.009 0.067 0.655 1.000 0.964 25.575 0.267 0.267 5.0 0.600 0.02144 -0.010 0.059 0.664 1.000 0.964 27.971 0.452 0.267 5.5 0.596 0.02297 -0.020 0.046 0.682 0.858 0.964 25.952 0.105 0.284 6.0 0.391 0.04160 -0.040 0.040 0.691 0.096 0.964 9.400 0.108 0.353 6.5 0.433 0.04528 -0.044 0.036 0.709 0.084 0.964 9.572 0.322 0.351 7.0 0.476 0.04809 -0.047 0.033 0.709 0.067 0.964 9.889 0.320 0.348 7.5 0.517 0.05126 -0.049 0.030 0.718 0.049 0.964 10.087 0.323 0.346 8.0 0.558 0.05458 -0.053 0.028 0.718 0.046 0.964 10.214 0.328 0.344 8.5 0.597 0.05753 -0.056 0.026 0.718 0.042 0.965 10.383 0.330 0.343 9.0 0.636 0.06217 -0.059 0.024 0.727 0.040 0.965 10.226 0.332 0.343 9.5 0.673 0.06813 -0.062 0.022 0.740 0.037 0.956 9.884 0.334 0.342 10.0 0.710 0.07321 -0.065 0.022 0.740 0.035 0.957 9.701 0.336 0.342 10.5 0.746 0.07603 -0.068 0.021 0.750 0.033 0.956 9.809 0.339 0.341 11.0 0.780 0.08269 -0.071 0.020 0.750 0.032 0.957 9.434 0.342 0.341 11.5 0.814 0.08837 -0.074 0.019 0.760 0.031 0.957 9.206 0.344 0.341 12.0 0.846 0.09283 -0.077 0.018 0.760 0.030 0.957 9.116 0.345 0.342 12.5 0.878 0.09945 -0.081 0.018 0.770 0.028 0.957 8.830 0.349 0.342 13.0 0.908 0.10783 -0.084 0.017 0.780 0.028 0.957 8.421 0.352 0.342 13.5 0.938 0.11323 -0.087 0.017 0.780 0.026 0.958 8.283 0.356 0.342 14.0 0.966 0.11822 -0.090 0.016 0.790 0.026 0.966 8.168 0.360 0.343 14.5 0.993 0.12242 -0.093 0.016 0.800 0.024 0.966 8.111 0.375 0.343 15.0 1.014 0.12717 -0.096 0.015 0.810 0.024 0.967 7.970 0.398 0.344 Name = EPPLER EA 6(-1)-012 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 -1.012 0.11677 0.096 0.810 0.015 1.000 0.027 -8.670 0.398 0.345 -14.5 -0.992 0.11464 0.093 0.800 0.016 1.000 0.027 -8.651 0.375 0.344 -14.0 -0.964 0.10745 0.090 0.790 0.016 1.000 0.029 -8.974 0.362 0.343 -13.5 -0.937 0.09879 0.087 0.780 0.017 1.000 0.028 -9.484 0.356 0.343 -13.0 -0.907 0.09657 0.084 0.780 0.017 1.000 0.031 -9.388 0.351 0.342 -12.5 -0.877 0.09013 0.081 0.770 0.018 1.000 0.031 -9.726 0.348 0.342 -12.0 -0.844 0.08605 0.078 0.760 0.018 1.000 0.034 -9.809 0.345 0.342 -11.5 -0.812 0.07838 0.075 0.760 0.019 1.000 0.034 -10.358 0.344 0.342 -11.0 -0.778 0.07641 0.071 0.750 0.020 1.000 0.036 -10.179 0.341 0.342 -10.5 -0.743 0.06993 0.068 0.750 0.021 1.000 0.037 -10.631 0.339 0.342 -10.0 -0.708 0.06667 0.065 0.740 0.022 1.000 0.039 -10.616 0.335 0.342 -9.5 -0.670 0.06273 0.062 0.740 0.022 1.000 0.042 -10.682 0.332 0.343 -9.0 -0.632 0.05714 0.059 0.727 0.024 1.000 0.045 -11.066 0.331 0.343 -8.5 -0.593 0.05393 0.056 0.718 0.026 1.000 0.048 -10.999 0.327 0.344 -8.0 -0.554 0.05045 0.053 0.718 0.028 1.000 0.059 -10.974 0.323 0.346 -7.5 -0.513 0.04721 0.050 0.718 0.030 1.000 0.075 -10.870 0.320 0.347 -7.0 -0.471 0.04530 0.047 0.709 0.033 1.000 0.096 -10.396 0.115 0.350 -6.5 -0.675 0.02304 0.028 0.709 0.036 1.000 0.796 -29.272 0.111 0.292 -6.0 -0.695 0.02146 0.016 0.691 0.040 1.000 0.951 -32.384 0.623 0.273 -5.5 -0.638 0.02027 0.015 0.682 0.046 1.000 0.952 -31.481 0.274 0.273 -5.0 -0.581 0.01919 0.013 0.664 0.059 1.000 0.952 -30.247 0.274 0.273 -4.5 -0.523 0.01857 0.012 0.655 0.067 1.000 0.953 -28.138 0.273 0.273 -4.0 -0.464 0.01818 0.011 0.645 0.075 1.000 0.954 -25.542 0.273 0.273 -3.5 -0.406 0.01662 0.009 0.636 0.079 1.000 0.954 -24.426 0.274 0.273 -3.0 -0.348 0.01265 0.008 0.636 0.088 1.000 0.959 -27.541 0.274 0.272 -2.5 -0.290 0.01467 0.006 0.621 0.096 1.000 0.960 -19.731 0.243 0.272 -2.0 -0.174 0.01605 0.009 0.608 0.554 1.000 0.787 -10.870 0.249 0.301 -1.5 -0.122 0.01598 0.007 0.604 0.562 1.000 0.796 -7.633 0.348 0.304 -1.0 -0.110 0.01278 0.003 0.600 0.567 1.000 0.956 -8.619 0.324 0.274 -0.5 -0.051 0.01264 0.001 0.592 0.575 1.000 0.956 -4.023 0.274 0.276 0.0 0.000 0.01310 -0.000 0.583 0.583 1.000 0.957 0.000 0.271 0.250 0.5 0.060 0.01260 -0.001 0.575 0.592 1.000 0.957 4.791 0.267 0.267 1.0 0.121 0.01274 -0.002 0.567 0.600 1.000 0.958 9.474 0.340 0.267 1.5 0.122 0.01598 -0.007 0.562 0.604 0.796 0.958 7.633 0.377 0.304 2.0 0.174 0.01605 -0.009 0.554 0.608 0.787 0.958 10.870 0.242 0.301 2.5 0.302 0.01463 -0.005 0.096 0.621 1.000 0.959 20.608 0.235 0.267 3.0 0.362 0.01261 -0.006 0.088 0.636 1.000 0.964 28.679 0.267 0.267 3.5 0.421 0.01656 -0.007 0.079 0.636 1.000 0.965 25.451 0.267 0.267 4.0 0.481 0.01812 -0.008 0.075 0.645 1.000 0.965 26.551 0.267 0.267 4.5 0.540 0.01850 -0.009 0.067 0.655 1.000 0.965 29.211 0.267 0.267 5.0 0.600 0.01911 -0.010 0.059 0.664 1.000 0.965 31.369 0.267 0.267 5.5 0.658 0.02018 -0.011 0.046 0.682 1.000 0.965 32.621 0.267 0.267 6.0 0.717 0.02137 -0.012 0.040 0.691 1.000 0.965 33.542 1.299 0.267 6.5 0.675 0.02304 -0.028 0.036 0.709 0.796 0.965 29.272 0.108 0.292 7.0 0.471 0.04530 -0.047 0.033 0.709 0.096 0.965 10.396 0.115 0.350 7.5 0.513 0.04721 -0.050 0.030 0.718 0.075 0.965 10.870 0.320 0.347 8.0 0.554 0.05045 -0.053 0.028 0.718 0.059 0.965 10.974 0.323 0.346 8.5 0.593 0.05393 -0.056 0.026 0.718 0.048 0.966 10.999 0.327 0.344 9.0 0.632 0.05714 -0.059 0.024 0.727 0.045 0.966 11.066 0.331 0.343 9.5 0.670 0.06273 -0.062 0.022 0.740 0.042 0.957 10.682 0.332 0.343 10.0 0.708 0.06667 -0.065 0.022 0.740 0.039 0.958 10.616 0.335 0.342 10.5 0.743 0.06993 -0.068 0.021 0.750 0.037 0.957 10.631 0.339 0.342 11.0 0.778 0.07641 -0.071 0.020 0.750 0.036 0.958 10.179 0.341 0.342 11.5 0.812 0.07838 -0.075 0.019 0.760 0.034 0.958 10.358 0.344 0.342 12.0 0.844 0.08605 -0.078 0.018 0.760 0.034 0.958 9.809 0.345 0.342 12.5 0.877 0.09013 -0.081 0.018 0.770 0.031 0.958 9.726 0.348 0.342 13.0 0.907 0.09657 -0.084 0.017 0.780 0.031 0.958 9.388 0.351 0.342 13.5 0.937 0.09879 -0.087 0.017 0.780 0.028 0.958 9.484 0.356 0.343 14.0 0.964 0.10745 -0.090 0.016 0.790 0.029 0.967 8.974 0.362 0.343 14.5 0.992 0.11464 -0.093 0.016 0.800 0.027 0.967 8.651 0.375 0.344 15.0 1.012 0.11677 -0.096 0.015 0.810 0.027 0.967 8.670 0.398 0.345 Name = EPPLER EA 6(-1)-012 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 -1.011 0.10988 0.096 0.810 0.015 1.000 0.030 -9.203 0.403 0.345 -14.5 -0.991 0.10286 0.093 0.800 0.016 1.000 0.029 -9.633 0.375 0.344 -14.0 -0.963 0.10022 0.090 0.790 0.016 1.000 0.032 -9.608 0.360 0.344 -13.5 -0.936 0.09298 0.087 0.780 0.017 1.000 0.031 -10.062 0.356 0.343 -13.0 -0.905 0.08877 0.084 0.780 0.017 1.000 0.034 -10.196 0.351 0.343 -12.5 -0.875 0.08371 0.081 0.770 0.018 1.000 0.034 -10.453 0.346 0.342 -12.0 -0.842 0.08199 0.078 0.760 0.018 1.000 0.038 -10.268 0.343 0.342 -11.5 -0.810 0.07452 0.075 0.760 0.019 1.000 0.038 -10.865 0.344 0.342 -11.0 -0.776 0.07233 0.072 0.750 0.020 1.000 0.040 -10.723 0.340 0.342 -10.5 -0.740 0.06869 0.068 0.750 0.021 1.000 0.042 -10.781 0.338 0.343 -10.0 -0.705 0.06446 0.065 0.740 0.022 1.000 0.044 -10.931 0.334 0.343 -9.5 -0.667 0.06093 0.062 0.740 0.022 1.000 0.048 -10.940 0.332 0.343 -9.0 -0.629 0.05492 0.059 0.727 0.024 1.000 0.051 -11.452 0.326 0.344 -8.5 -0.590 0.05167 0.056 0.718 0.026 1.000 0.071 -11.419 0.320 0.346 -8.0 -0.550 0.04882 0.054 0.718 0.028 1.000 0.088 -11.268 0.324 0.347 -7.5 -0.510 0.04487 0.051 0.718 0.030 1.000 0.100 -11.360 0.120 0.349 -7.0 -0.735 0.02269 0.030 0.709 0.033 1.000 0.808 -32.399 0.113 0.290 -6.5 -0.752 0.02118 0.017 0.709 0.036 1.000 0.951 -35.492 0.594 0.273 -6.0 -0.695 0.02003 0.016 0.691 0.040 1.000 0.952 -34.723 0.274 0.273 -5.5 -0.638 0.01849 0.015 0.682 0.046 1.000 0.952 -34.519 0.274 0.273 -5.0 -0.581 0.01758 0.013 0.664 0.059 1.000 0.953 -33.036 0.274 0.273 -4.5 -0.523 0.01692 0.012 0.655 0.067 1.000 0.954 -30.904 0.273 0.273 -4.0 -0.465 0.01633 0.011 0.645 0.075 1.000 0.955 -28.459 0.273 0.273 -3.5 -0.406 0.01567 0.009 0.636 0.079 1.000 0.955 -25.928 0.274 0.273 -3.0 -0.349 0.01220 0.008 0.636 0.088 1.000 0.960 -28.598 0.274 0.272 -2.5 -0.290 0.01284 0.006 0.621 0.096 1.000 0.961 -22.560 0.271 0.272 -2.0 -0.229 0.01148 0.005 0.608 0.554 1.000 0.956 -19.963 0.271 0.273 -1.5 -0.170 0.01143 0.004 0.604 0.562 1.000 0.957 -14.860 0.272 0.273 -1.0 -0.111 0.01151 0.003 0.600 0.567 1.000 0.958 -9.613 0.272 0.274 -0.5 -0.051 0.01136 0.001 0.592 0.575 1.000 0.958 -4.507 0.274 0.275 0.0 0.000 0.01075 -0.000 0.583 0.583 1.000 0.958 0.000 0.271 0.250 0.5 0.060 0.01132 -0.001 0.575 0.592 1.000 0.959 5.332 0.267 0.267 1.0 0.121 0.01147 -0.002 0.567 0.600 1.000 0.959 10.526 0.267 0.267 1.5 0.181 0.01139 -0.003 0.562 0.604 1.000 0.959 15.897 0.267 0.267 2.0 0.241 0.01143 -0.004 0.554 0.608 1.000 0.960 21.111 0.267 0.267 2.5 0.302 0.01280 -0.005 0.096 0.621 1.000 0.960 23.550 0.267 0.267 3.0 0.362 0.01215 -0.006 0.088 0.636 1.000 0.965 29.750 0.267 0.267 3.5 0.421 0.01561 -0.007 0.079 0.636 1.000 0.966 26.994 0.267 0.267 4.0 0.481 0.01627 -0.008 0.075 0.645 1.000 0.966 29.574 0.267 0.267 4.5 0.540 0.01685 -0.009 0.067 0.655 1.000 0.966 32.071 0.267 0.267 5.0 0.600 0.01751 -0.010 0.059 0.664 1.000 0.966 34.250 0.267 0.267 5.5 0.658 0.01841 -0.011 0.046 0.682 1.000 0.966 35.760 0.267 0.267 6.0 0.717 0.01994 -0.012 0.040 0.691 1.000 0.966 35.945 0.267 0.267 6.5 0.775 0.02109 -0.013 0.036 0.709 1.000 0.966 36.732 1.195 0.267 7.0 0.735 0.02269 -0.030 0.033 0.709 0.808 0.966 32.399 0.109 0.290 7.5 0.510 0.04487 -0.051 0.030 0.718 0.100 0.966 11.360 0.120 0.349 8.0 0.550 0.04882 -0.054 0.028 0.718 0.088 0.966 11.268 0.324 0.347 8.5 0.590 0.05167 -0.056 0.026 0.718 0.071 0.966 11.419 0.320 0.346 9.0 0.629 0.05492 -0.059 0.024 0.727 0.051 0.966 11.452 0.326 0.344 9.5 0.667 0.06093 -0.062 0.022 0.740 0.048 0.958 10.940 0.332 0.343 10.0 0.705 0.06446 -0.065 0.022 0.740 0.044 0.958 10.931 0.334 0.343 10.5 0.740 0.06869 -0.068 0.021 0.750 0.042 0.958 10.781 0.338 0.343 11.0 0.776 0.07233 -0.072 0.020 0.750 0.040 0.958 10.723 0.340 0.342 11.5 0.810 0.07452 -0.075 0.019 0.760 0.038 0.958 10.865 0.344 0.342 12.0 0.842 0.08199 -0.078 0.018 0.760 0.038 0.959 10.268 0.343 0.342 12.5 0.875 0.08371 -0.081 0.018 0.770 0.034 0.959 10.453 0.346 0.342 13.0 0.905 0.08877 -0.084 0.017 0.780 0.034 0.958 10.196 0.351 0.343 13.5 0.936 0.09298 -0.087 0.017 0.780 0.031 0.959 10.062 0.356 0.343 14.0 0.963 0.10022 -0.090 0.016 0.790 0.032 0.967 9.608 0.360 0.344 14.5 0.991 0.10286 -0.093 0.016 0.800 0.029 0.967 9.633 0.375 0.344 15.0 1.011 0.10988 -0.096 0.015 0.810 0.030 0.969 9.203 0.403 0.345