Name = NASA/AMES 63A108 MOD C 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 -0.669 0.30143 0.076 1.000 0.003 1.000 0.004 -2.218 -0.091 0.363 -14.5 -0.675 0.27934 0.074 1.000 0.003 1.000 0.004 -2.417 -0.147 0.359 -14.0 -0.680 0.26267 0.071 1.000 0.003 1.000 0.004 -2.588 -0.373 0.355 -13.5 -0.682 0.23877 0.069 1.000 0.003 1.000 0.004 -2.858 -1.341 0.351 -13.0 -0.683 0.21428 0.067 1.000 0.003 1.000 0.004 -3.186 2.678 0.348 -12.5 -0.680 0.19910 0.064 1.000 0.003 1.000 0.004 -3.418 0.898 0.345 -12.0 -0.676 0.18329 0.062 1.000 0.003 1.000 0.004 -3.686 0.617 0.342 -11.5 -0.668 0.16092 0.060 1.000 0.003 1.000 0.004 -4.151 0.512 0.340 -11.0 -0.658 0.15300 0.058 1.000 0.003 1.000 0.004 -4.301 0.451 0.337 -10.5 -0.645 0.13714 0.055 1.000 0.003 1.000 0.004 -4.702 0.409 0.336 -10.0 -0.629 0.12212 0.053 1.000 0.003 1.000 0.004 -5.150 0.384 0.334 -9.5 -0.610 0.11176 0.051 1.000 0.003 1.000 0.004 -5.460 0.367 0.333 -9.0 -0.589 0.10127 0.048 1.000 0.003 1.000 0.004 -5.812 0.354 0.332 -8.5 -0.565 0.09183 0.046 1.000 0.003 1.000 0.005 -6.151 0.345 0.331 -8.0 -0.539 0.08304 0.043 1.000 0.003 1.000 0.005 -6.490 0.338 0.331 -7.5 -0.511 0.07511 0.041 1.000 0.004 1.000 0.005 -6.804 0.333 0.330 -7.0 -0.481 0.06843 0.039 1.000 0.004 1.000 0.005 -7.035 0.329 0.330 -6.5 -0.450 0.06167 0.036 0.873 0.004 1.000 0.005 -7.298 0.325 0.331 -6.0 -0.418 0.05533 0.034 0.867 0.005 1.000 0.005 -7.548 0.322 0.331 -5.5 -0.383 0.05016 0.031 0.862 0.005 1.000 0.006 -7.643 0.320 0.332 -5.0 -0.348 0.04559 0.029 0.857 0.005 1.000 0.006 -7.639 0.318 0.333 -4.5 -0.312 0.04107 0.027 0.852 0.005 1.000 0.007 -7.597 0.316 0.335 -4.0 -0.274 0.03744 0.024 0.845 0.006 1.000 0.008 -7.325 0.314 0.338 -3.5 -0.236 0.03393 0.022 0.837 0.007 1.000 0.009 -6.954 0.313 0.342 -3.0 -0.197 0.03103 0.019 0.830 0.008 1.000 0.011 -6.333 0.310 0.348 -2.5 -0.155 0.02846 0.017 0.799 0.010 1.000 0.016 -5.447 0.306 0.359 -2.0 -0.110 0.02674 0.014 0.790 0.017 1.000 0.028 -4.123 -0.093 0.381 -1.5 -0.189 0.01414 0.005 0.782 0.597 1.000 1.000 -13.368 -0.227 0.278 -1.0 -0.130 0.01402 0.005 0.773 0.631 1.000 1.000 -9.290 0.255 0.288 -0.5 -0.071 0.01407 0.005 0.757 0.662 1.000 1.000 -5.073 0.255 0.314 0.0 -0.012 0.01402 0.004 0.743 0.690 1.000 1.000 -0.886 0.255 0.595 0.5 0.047 0.01394 0.004 0.728 0.715 1.000 1.000 3.335 0.255 0.165 1.0 0.105 0.01395 0.004 0.685 0.740 1.000 1.000 7.555 0.256 0.215 1.5 0.164 0.01331 0.003 0.669 1.000 1.000 1.000 12.346 0.275 0.230 2.0 0.209 0.02474 0.001 0.652 1.000 0.922 1.000 8.450 0.280 0.245 2.5 0.266 0.02534 0.000 0.616 1.000 0.922 1.000 10.512 0.240 0.249 3.0 0.341 0.01391 0.002 0.086 1.000 1.000 1.000 24.496 0.237 0.243 3.5 0.399 0.01407 0.002 0.047 1.000 1.000 1.000 28.375 0.057 0.245 4.0 0.241 0.03608 -0.017 0.034 1.000 0.083 1.000 6.669 0.061 0.321 4.5 0.287 0.03829 -0.019 0.026 1.000 0.045 1.000 7.504 0.300 0.317 5.0 0.330 0.04073 -0.022 0.020 1.000 0.033 1.000 8.109 0.308 0.315 5.5 0.371 0.04385 -0.024 0.017 1.000 0.026 1.000 8.463 0.311 0.315 6.0 0.411 0.04703 -0.027 0.014 1.000 0.021 1.000 8.740 0.312 0.315 6.5 0.451 0.05008 -0.029 0.010 1.000 0.017 1.000 8.999 0.314 0.314 7.0 0.489 0.05397 -0.031 0.009 1.000 0.014 1.000 9.052 0.317 0.314 7.5 0.525 0.05850 -0.034 0.008 1.000 0.012 1.000 8.975 0.320 0.315 8.0 0.560 0.06323 -0.037 0.007 1.000 0.010 1.000 8.858 0.324 0.315 8.5 0.593 0.06907 -0.039 0.007 1.000 0.009 1.000 8.593 0.328 0.316 9.0 0.626 0.07526 -0.042 0.006 1.000 0.009 1.000 8.312 0.331 0.317 9.5 0.656 0.08128 -0.044 0.006 1.000 0.008 1.000 8.072 0.337 0.317 10.0 0.684 0.08880 -0.047 0.006 1.000 0.008 1.000 7.708 0.343 0.318 10.5 0.711 0.09533 -0.049 0.005 1.000 0.007 1.000 7.461 0.350 0.319 11.0 0.736 0.10506 -0.052 0.005 1.000 0.007 1.000 7.001 0.358 0.320 11.5 0.758 0.11476 -0.054 0.005 1.000 0.007 1.000 6.609 0.368 0.322 12.0 0.779 0.12217 -0.057 0.005 1.000 0.007 1.000 6.375 0.382 0.323 12.5 0.797 0.13775 -0.059 0.005 1.000 0.006 1.000 5.787 0.399 0.325 13.0 0.813 0.14791 -0.062 0.005 1.000 0.006 1.000 5.498 0.421 0.326 13.5 0.827 0.16072 -0.065 0.004 1.000 0.006 1.000 5.146 0.453 0.328 14.0 0.838 0.17244 -0.067 0.004 1.000 0.006 1.000 4.861 0.502 0.330 14.5 0.847 0.18494 -0.070 0.004 1.000 0.005 1.000 4.581 0.577 0.332 15.0 0.854 0.20675 -0.072 0.004 1.000 0.005 1.000 4.129 0.635 0.335 Name = NASA/AMES 63A108 MOD C 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 -0.668 0.23246 0.076 1.000 0.003 1.000 0.004 -2.875 -0.092 0.363 -14.5 -0.675 0.21665 0.074 1.000 0.003 1.000 0.004 -3.115 -0.143 0.359 -14.0 -0.680 0.19504 0.071 1.000 0.003 1.000 0.004 -3.486 -0.377 0.355 -13.5 -0.682 0.18731 0.069 1.000 0.003 1.000 0.004 -3.642 -1.448 0.351 -13.0 -0.683 0.17187 0.067 1.000 0.003 1.000 0.004 -3.971 2.652 0.348 -12.5 -0.680 0.16071 0.064 1.000 0.003 1.000 0.004 -4.233 0.917 0.345 -12.0 -0.676 0.14096 0.062 1.000 0.003 1.000 0.004 -4.793 0.617 0.342 -11.5 -0.668 0.13001 0.060 1.000 0.003 1.000 0.004 -5.136 0.508 0.340 -11.0 -0.658 0.12453 0.058 1.000 0.003 1.000 0.004 -5.282 0.451 0.338 -10.5 -0.645 0.11153 0.055 1.000 0.003 1.000 0.004 -5.780 0.410 0.336 -10.0 -0.629 0.09935 0.053 1.000 0.003 1.000 0.004 -6.328 0.385 0.334 -9.5 -0.610 0.09154 0.051 1.000 0.003 1.000 0.004 -6.664 0.367 0.333 -9.0 -0.588 0.08509 0.048 1.000 0.003 1.000 0.005 -6.915 0.354 0.332 -8.5 -0.565 0.07792 0.046 1.000 0.003 1.000 0.005 -7.246 0.345 0.331 -8.0 -0.539 0.07116 0.043 1.000 0.003 1.000 0.005 -7.570 0.339 0.331 -7.5 -0.511 0.06277 0.041 1.000 0.004 1.000 0.005 -8.142 0.333 0.330 -7.0 -0.481 0.05800 0.039 1.000 0.004 1.000 0.005 -8.300 0.328 0.330 -6.5 -0.450 0.05357 0.036 0.873 0.004 1.000 0.006 -8.399 0.325 0.331 -6.0 -0.417 0.04857 0.034 0.867 0.005 1.000 0.006 -8.594 0.322 0.331 -5.5 -0.383 0.04427 0.031 0.862 0.005 1.000 0.006 -8.656 0.320 0.332 -5.0 -0.348 0.04050 0.029 0.857 0.005 1.000 0.006 -8.595 0.318 0.333 -4.5 -0.312 0.03697 0.027 0.852 0.005 1.000 0.007 -8.430 0.316 0.335 -4.0 -0.274 0.03369 0.024 0.845 0.006 1.000 0.008 -8.128 0.314 0.338 -3.5 -0.235 0.03083 0.022 0.837 0.007 1.000 0.010 -7.633 0.312 0.342 -3.0 -0.195 0.02831 0.019 0.830 0.008 1.000 0.013 -6.905 0.309 0.349 -2.5 -0.153 0.02612 0.017 0.799 0.010 1.000 0.019 -5.868 -0.015 0.360 -2.0 -0.248 0.01291 0.005 0.790 0.017 1.000 1.000 -19.173 -0.077 0.272 -1.5 -0.189 0.01229 0.005 0.782 0.597 1.000 1.000 -15.377 0.255 0.278 -1.0 -0.130 0.01219 0.005 0.773 0.631 1.000 1.000 -10.684 0.255 0.288 -0.5 -0.071 0.01222 0.005 0.757 0.662 1.000 1.000 -5.841 0.255 0.314 0.0 -0.012 0.01218 0.004 0.743 0.690 1.000 1.000 -1.021 0.255 0.595 0.5 0.047 0.01211 0.004 0.728 0.715 1.000 1.000 3.839 0.255 0.165 1.0 0.105 0.01213 0.004 0.685 0.740 1.000 1.000 8.693 0.256 0.215 1.5 0.164 0.01157 0.003 0.669 1.000 1.000 1.000 14.202 0.256 0.230 2.0 0.223 0.01169 0.003 0.652 1.000 1.000 1.000 19.092 0.256 0.237 2.5 0.282 0.01180 0.003 0.616 1.000 1.000 1.000 23.909 0.256 0.241 3.0 0.341 0.01248 0.002 0.086 1.000 1.000 1.000 27.303 0.256 0.243 3.5 0.399 0.01268 0.002 0.047 1.000 1.000 1.000 31.480 0.256 0.245 4.0 0.457 0.01289 0.002 0.034 1.000 1.000 1.000 35.460 0.256 0.246 4.5 0.515 0.01296 0.001 0.026 1.000 1.000 1.000 39.727 0.073 0.248 5.0 0.325 0.03727 -0.022 0.020 1.000 0.048 1.000 8.712 0.077 0.317 5.5 0.368 0.03972 -0.024 0.017 1.000 0.032 1.000 9.266 0.307 0.316 6.0 0.409 0.04243 -0.027 0.014 1.000 0.025 1.000 9.628 0.311 0.315 6.5 0.448 0.04505 -0.029 0.010 1.000 0.020 1.000 9.947 0.314 0.315 7.0 0.486 0.04829 -0.032 0.009 1.000 0.017 1.000 10.071 0.316 0.315 7.5 0.524 0.05176 -0.034 0.008 1.000 0.014 1.000 10.113 0.319 0.315 8.0 0.559 0.05567 -0.037 0.007 1.000 0.011 1.000 10.043 0.323 0.315 8.5 0.593 0.05989 -0.039 0.007 1.000 0.010 1.000 9.899 0.327 0.316 9.0 0.625 0.06491 -0.042 0.006 1.000 0.009 1.000 9.628 0.331 0.317 9.5 0.655 0.07002 -0.044 0.006 1.000 0.009 1.000 9.362 0.336 0.317 10.0 0.684 0.07506 -0.047 0.006 1.000 0.008 1.000 9.113 0.343 0.318 10.5 0.711 0.08171 -0.049 0.005 1.000 0.008 1.000 8.697 0.350 0.319 11.0 0.735 0.08784 -0.052 0.005 1.000 0.008 1.000 8.370 0.358 0.321 11.5 0.758 0.09558 -0.054 0.005 1.000 0.007 1.000 7.931 0.368 0.322 12.0 0.778 0.10135 -0.057 0.005 1.000 0.007 1.000 7.681 0.381 0.323 12.5 0.797 0.11121 -0.059 0.005 1.000 0.006 1.000 7.167 0.397 0.325 13.0 0.813 0.11875 -0.062 0.005 1.000 0.006 1.000 6.846 0.423 0.326 13.5 0.827 0.13228 -0.065 0.004 1.000 0.006 1.000 6.249 0.455 0.328 14.0 0.838 0.14126 -0.067 0.004 1.000 0.006 1.000 5.932 0.502 0.330 14.5 0.847 0.15092 -0.070 0.004 1.000 0.006 1.000 5.611 0.573 0.332 15.0 0.854 0.16312 -0.072 0.004 1.000 0.005 1.000 5.233 0.624 0.335 Name = NASA/AMES 63A108 MOD C 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 -0.668 0.19547 0.076 1.000 0.003 1.000 0.004 -3.419 -0.092 0.363 -14.5 -0.675 0.18383 0.074 1.000 0.003 1.000 0.004 -3.671 -0.145 0.359 -14.0 -0.680 0.17347 0.071 1.000 0.003 1.000 0.004 -3.918 -0.379 0.355 -13.5 -0.682 0.16555 0.069 1.000 0.003 1.000 0.004 -4.120 -1.351 0.351 -13.0 -0.683 0.14675 0.067 1.000 0.003 1.000 0.004 -4.651 2.858 0.348 -12.5 -0.680 0.13757 0.064 1.000 0.003 1.000 0.004 -4.945 0.896 0.345 -12.0 -0.675 0.12756 0.062 1.000 0.003 1.000 0.004 -5.295 0.611 0.342 -11.5 -0.668 0.11689 0.060 1.000 0.003 1.000 0.004 -5.711 0.512 0.340 -11.0 -0.658 0.10823 0.058 1.000 0.003 1.000 0.004 -6.078 0.451 0.338 -10.5 -0.644 0.10053 0.055 1.000 0.003 1.000 0.004 -6.411 0.408 0.336 -10.0 -0.629 0.09069 0.053 1.000 0.003 1.000 0.005 -6.931 0.385 0.334 -9.5 -0.610 0.08398 0.051 1.000 0.003 1.000 0.005 -7.262 0.367 0.333 -9.0 -0.588 0.07550 0.048 1.000 0.003 1.000 0.005 -7.794 0.355 0.332 -8.5 -0.565 0.06957 0.046 1.000 0.003 1.000 0.005 -8.116 0.345 0.331 -8.0 -0.539 0.06395 0.043 1.000 0.003 1.000 0.005 -8.424 0.338 0.331 -7.5 -0.511 0.05901 0.041 1.000 0.004 1.000 0.005 -8.657 0.333 0.330 -7.0 -0.481 0.05340 0.039 1.000 0.004 1.000 0.005 -9.015 0.329 0.330 -6.5 -0.450 0.04936 0.036 0.873 0.004 1.000 0.006 -9.115 0.325 0.331 -6.0 -0.417 0.04554 0.034 0.867 0.005 1.000 0.006 -9.163 0.322 0.331 -5.5 -0.383 0.04160 0.031 0.862 0.005 1.000 0.006 -9.208 0.320 0.332 -5.0 -0.348 0.03816 0.029 0.857 0.005 1.000 0.007 -9.116 0.318 0.334 -4.5 -0.311 0.03508 0.027 0.852 0.005 1.000 0.008 -8.873 0.315 0.336 -4.0 -0.273 0.03206 0.024 0.845 0.006 1.000 0.009 -8.528 0.314 0.339 -3.5 -0.235 0.02941 0.022 0.837 0.007 1.000 0.010 -7.990 0.311 0.343 -3.0 -0.194 0.02719 0.019 0.830 0.008 1.000 0.015 -7.143 0.306 0.350 -2.5 -0.149 0.02540 0.017 0.799 0.010 1.000 0.027 -5.878 -0.009 0.364 -2.0 -0.248 0.01225 0.005 0.790 0.017 1.000 1.000 -20.208 -0.046 0.272 -1.5 -0.189 0.01147 0.005 0.782 0.597 1.000 1.000 -16.476 0.255 0.278 -1.0 -0.130 0.01138 0.005 0.773 0.631 1.000 1.000 -11.446 0.255 0.288 -0.5 -0.071 0.01140 0.005 0.757 0.662 1.000 1.000 -6.262 0.255 0.314 0.0 -0.012 0.01136 0.004 0.743 0.690 1.000 1.000 -1.094 0.255 0.595 0.5 0.047 0.01130 0.004 0.728 0.715 1.000 1.000 4.115 0.255 0.165 1.0 0.105 0.01132 0.004 0.685 0.740 1.000 1.000 9.316 0.256 0.215 1.5 0.164 0.01080 0.003 0.669 1.000 1.000 1.000 15.216 0.256 0.230 2.0 0.223 0.01091 0.003 0.652 1.000 1.000 1.000 20.472 0.256 0.237 2.5 0.282 0.01100 0.003 0.616 1.000 1.000 1.000 25.639 0.256 0.241 3.0 0.341 0.01181 0.002 0.086 1.000 1.000 1.000 28.852 0.256 0.243 3.5 0.399 0.01202 0.002 0.047 1.000 1.000 1.000 33.197 0.256 0.245 4.0 0.457 0.01225 0.002 0.034 1.000 1.000 1.000 37.334 0.256 0.246 4.5 0.515 0.01236 0.001 0.026 1.000 1.000 1.000 41.667 0.256 0.248 5.0 0.572 0.01255 0.001 0.020 1.000 1.000 1.000 45.598 0.081 0.248 5.5 0.362 0.03827 -0.024 0.017 1.000 0.049 1.000 9.471 0.084 0.318 6.0 0.406 0.04053 -0.027 0.014 1.000 0.031 1.000 10.007 0.307 0.316 6.5 0.445 0.04314 -0.029 0.010 1.000 0.026 1.000 10.309 0.313 0.316 7.0 0.484 0.04587 -0.032 0.009 1.000 0.019 1.000 10.552 0.314 0.315 7.5 0.522 0.04893 -0.034 0.008 1.000 0.016 1.000 10.661 0.318 0.315 8.0 0.558 0.05241 -0.037 0.007 1.000 0.013 1.000 10.640 0.321 0.316 8.5 0.592 0.05617 -0.039 0.007 1.000 0.011 1.000 10.540 0.326 0.316 9.0 0.624 0.06041 -0.042 0.006 1.000 0.010 1.000 10.334 0.331 0.317 9.5 0.655 0.06515 -0.044 0.006 1.000 0.009 1.000 10.050 0.336 0.317 10.0 0.683 0.06979 -0.047 0.006 1.000 0.009 1.000 9.792 0.342 0.318 10.5 0.710 0.07498 -0.049 0.005 1.000 0.008 1.000 9.472 0.350 0.319 11.0 0.735 0.08036 -0.052 0.005 1.000 0.008 1.000 9.143 0.357 0.321 11.5 0.758 0.08594 -0.054 0.005 1.000 0.007 1.000 8.819 0.368 0.322 12.0 0.778 0.09237 -0.057 0.005 1.000 0.007 1.000 8.424 0.382 0.323 12.5 0.797 0.10157 -0.060 0.005 1.000 0.007 1.000 7.844 0.397 0.325 13.0 0.813 0.10823 -0.062 0.005 1.000 0.007 1.000 7.509 0.421 0.326 13.5 0.826 0.11742 -0.065 0.004 1.000 0.006 1.000 7.039 0.453 0.328 14.0 0.838 0.12484 -0.067 0.004 1.000 0.006 1.000 6.711 0.502 0.330 14.5 0.847 0.13297 -0.070 0.004 1.000 0.006 1.000 6.368 0.573 0.332 15.0 0.853 0.14419 -0.072 0.004 1.000 0.006 1.000 5.919 0.624 0.335 Name = NASA/AMES 63A108 MOD C 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 -0.668 0.17861 0.076 1.000 0.003 1.000 0.005 -3.741 -0.092 0.363 -14.5 -0.675 0.16851 0.074 1.000 0.003 1.000 0.005 -4.004 -0.146 0.359 -14.0 -0.680 0.15908 0.071 1.000 0.003 1.000 0.004 -4.272 -0.370 0.355 -13.5 -0.682 0.14608 0.069 1.000 0.003 1.000 0.004 -4.669 -1.385 0.351 -13.0 -0.682 0.13759 0.067 1.000 0.003 1.000 0.004 -4.959 2.591 0.348 -12.5 -0.680 0.12951 0.064 1.000 0.003 1.000 0.004 -5.251 0.915 0.345 -12.0 -0.675 0.11539 0.062 1.000 0.003 1.000 0.004 -5.854 0.612 0.342 -11.5 -0.667 0.10863 0.060 1.000 0.003 1.000 0.004 -6.144 0.508 0.340 -11.0 -0.658 0.10182 0.058 1.000 0.003 1.000 0.004 -6.458 0.453 0.338 -10.5 -0.644 0.09142 0.055 1.000 0.003 1.000 0.004 -7.050 0.410 0.336 -10.0 -0.629 0.08281 0.053 1.000 0.003 1.000 0.005 -7.590 0.385 0.334 -9.5 -0.610 0.07699 0.051 1.000 0.003 1.000 0.005 -7.920 0.367 0.333 -9.0 -0.588 0.07215 0.048 1.000 0.003 1.000 0.005 -8.152 0.354 0.332 -8.5 -0.564 0.06678 0.046 1.000 0.003 1.000 0.005 -8.452 0.346 0.331 -8.0 -0.539 0.05976 0.043 1.000 0.003 1.000 0.005 -9.015 0.339 0.331 -7.5 -0.511 0.05545 0.041 1.000 0.004 1.000 0.005 -9.213 0.333 0.330 -7.0 -0.481 0.05068 0.039 1.000 0.004 1.000 0.005 -9.500 0.328 0.330 -6.5 -0.450 0.04732 0.036 0.873 0.004 1.000 0.006 -9.503 0.325 0.331 -6.0 -0.417 0.04374 0.034 0.867 0.005 1.000 0.006 -9.535 0.322 0.331 -5.5 -0.383 0.04001 0.031 0.862 0.005 1.000 0.006 -9.568 0.320 0.332 -5.0 -0.348 0.03698 0.029 0.857 0.005 1.000 0.007 -9.399 0.317 0.334 -4.5 -0.311 0.03397 0.027 0.852 0.005 1.000 0.008 -9.152 0.315 0.336 -4.0 -0.273 0.03111 0.024 0.845 0.006 1.000 0.009 -8.777 0.313 0.339 -3.5 -0.234 0.02867 0.022 0.837 0.007 1.000 0.012 -8.159 0.310 0.343 -3.0 -0.193 0.02659 0.019 0.830 0.008 1.000 0.017 -7.245 0.028 0.351 -2.5 -0.306 0.01192 0.006 0.799 0.010 1.000 1.000 -25.664 -0.002 0.269 -2.0 -0.248 0.01183 0.005 0.790 0.017 1.000 1.000 -20.922 0.255 0.272 -1.5 -0.189 0.01098 0.005 0.782 0.597 1.000 1.000 -17.210 0.255 0.278 -1.0 -0.130 0.01090 0.005 0.773 0.631 1.000 1.000 -11.956 0.255 0.288 -0.5 -0.071 0.01091 0.005 0.757 0.662 1.000 1.000 -6.543 0.255 0.314 0.0 -0.012 0.01087 0.004 0.743 0.690 1.000 1.000 -1.144 0.255 0.595 0.5 0.047 0.01082 0.004 0.728 0.715 1.000 1.000 4.300 0.255 0.165 1.0 0.105 0.01083 0.004 0.685 0.740 1.000 1.000 9.733 0.256 0.215 1.5 0.164 0.01034 0.003 0.669 1.000 1.000 1.000 15.892 0.256 0.230 2.0 0.223 0.01044 0.003 0.652 1.000 1.000 1.000 21.393 0.256 0.237 2.5 0.282 0.01053 0.003 0.616 1.000 1.000 1.000 26.793 0.256 0.241 3.0 0.341 0.01139 0.002 0.086 1.000 1.000 1.000 29.917 0.256 0.243 3.5 0.399 0.01161 0.002 0.047 1.000 1.000 1.000 34.387 0.256 0.245 4.0 0.457 0.01183 0.002 0.034 1.000 1.000 1.000 38.641 0.256 0.246 4.5 0.515 0.01196 0.001 0.026 1.000 1.000 1.000 43.066 0.256 0.248 5.0 0.572 0.01217 0.001 0.020 1.000 1.000 1.000 47.009 0.256 0.248 5.5 0.629 0.01226 0.001 0.017 1.000 1.000 1.000 51.293 0.087 0.249 6.0 0.400 0.03970 -0.027 0.014 1.000 0.047 1.000 10.084 0.091 0.318 6.5 0.440 0.04214 -0.029 0.010 1.000 0.035 1.000 10.451 0.308 0.317 7.0 0.481 0.04470 -0.032 0.009 1.000 0.025 1.000 10.758 0.310 0.316 7.5 0.520 0.04742 -0.034 0.008 1.000 0.018 1.000 10.957 0.315 0.316 8.0 0.556 0.05061 -0.037 0.007 1.000 0.015 1.000 10.983 0.320 0.316 8.5 0.591 0.05414 -0.039 0.007 1.000 0.013 1.000 10.909 0.323 0.316 9.0 0.624 0.05773 -0.042 0.006 1.000 0.010 1.000 10.803 0.329 0.317 9.5 0.654 0.06177 -0.044 0.006 1.000 0.009 1.000 10.593 0.336 0.318 10.0 0.683 0.06607 -0.047 0.006 1.000 0.009 1.000 10.337 0.342 0.318 10.5 0.710 0.07098 -0.049 0.005 1.000 0.008 1.000 10.000 0.350 0.319 11.0 0.734 0.07594 -0.052 0.005 1.000 0.008 1.000 9.671 0.357 0.321 11.5 0.757 0.08126 -0.054 0.005 1.000 0.008 1.000 9.322 0.368 0.322 12.0 0.778 0.08708 -0.057 0.005 1.000 0.008 1.000 8.931 0.381 0.323 12.5 0.797 0.09429 -0.060 0.005 1.000 0.007 1.000 8.447 0.396 0.325 13.0 0.812 0.10023 -0.062 0.005 1.000 0.007 1.000 8.106 0.421 0.326 13.5 0.826 0.10863 -0.065 0.004 1.000 0.006 1.000 7.607 0.453 0.328 14.0 0.838 0.11513 -0.067 0.004 1.000 0.006 1.000 7.275 0.502 0.330 14.5 0.847 0.12236 -0.070 0.004 1.000 0.006 1.000 6.919 0.573 0.332 15.0 0.853 0.13300 -0.072 0.004 1.000 0.006 1.000 6.416 0.624 0.335