Name = EPPLER 548 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 -0.584 0.20026 0.049 0.987 0.001 0.992 0.002 -2.917 1.677 0.334 -14.5 -0.582 0.19414 0.046 0.987 0.001 0.994 0.002 -2.997 1.201 0.329 -14.0 -0.577 0.16540 0.043 0.988 0.001 0.996 0.002 -3.491 0.807 0.324 -13.5 -0.570 0.15561 0.040 0.988 0.001 1.000 0.002 -3.665 0.623 0.320 -13.0 -0.560 0.14703 0.036 0.988 0.001 1.000 0.002 -3.809 0.532 0.315 -12.5 -0.547 0.12952 0.033 0.988 0.001 1.000 0.002 -4.225 0.481 0.311 -12.0 -0.532 0.12127 0.030 1.000 0.001 1.000 0.002 -4.384 0.444 0.306 -11.5 -0.513 0.11402 0.027 1.000 0.001 1.000 0.002 -4.502 0.420 0.302 -11.0 -0.492 0.10052 0.023 1.000 0.001 1.000 0.002 -4.899 0.400 0.297 -10.5 -0.469 0.09698 0.020 0.707 0.001 1.000 0.002 -4.834 0.385 0.293 -10.0 -0.443 0.09141 0.017 0.649 0.001 1.000 0.002 -4.842 0.374 0.287 -9.5 -0.414 0.08246 0.013 0.610 0.001 1.000 0.002 -5.021 0.366 0.282 -9.0 -0.384 0.07733 0.010 0.581 0.001 1.000 0.002 -4.962 0.359 0.275 -8.5 -0.351 0.07059 0.006 0.555 0.001 1.000 0.002 -4.978 0.353 0.268 -8.0 -0.317 0.06542 0.003 0.531 0.001 1.000 0.002 -4.841 0.348 0.259 -7.5 -0.281 0.05966 -0.001 0.510 0.001 1.000 0.002 -4.708 0.346 0.248 -7.0 -0.244 0.05485 -0.004 0.494 0.001 1.000 0.001 -4.453 0.343 0.233 -6.5 -0.206 0.05115 -0.008 0.478 0.001 1.000 0.001 -4.026 0.341 0.213 -6.0 -0.167 0.04694 -0.011 0.466 0.001 1.000 0.001 -3.553 0.338 0.183 -5.5 -0.126 0.04377 -0.015 0.457 0.001 1.000 0.002 -2.871 0.336 0.134 -5.0 -0.085 0.04006 -0.018 0.450 0.001 1.000 0.002 -2.119 0.334 0.036 -4.5 -0.041 0.03723 -0.022 0.442 0.001 1.000 0.003 -1.110 0.147 -0.275 -4.0 -0.182 0.03364 -0.028 0.436 0.589 0.849 0.630 -5.416 0.124 0.095 -3.5 -0.119 0.03182 -0.031 0.430 0.593 0.738 0.632 -3.733 0.302 -0.015 -3.0 -0.056 0.03123 -0.035 0.425 0.597 0.678 0.634 -1.777 0.302 -0.376 -2.5 0.008 0.03073 -0.038 0.419 0.599 0.636 0.637 0.245 0.302 5.309 -2.0 0.070 0.03031 -0.041 0.415 0.600 0.602 0.640 2.315 0.302 0.839 -1.5 0.132 0.02999 -0.045 0.411 0.602 0.575 0.642 4.416 0.303 0.587 -1.0 0.194 0.02975 -0.048 0.406 0.603 0.556 0.645 6.530 0.303 0.496 -0.5 0.256 0.02957 -0.051 0.402 0.605 0.537 0.647 8.647 0.175 0.450 0.0 0.108 0.03447 -0.054 0.398 0.606 0.519 0.649 3.136 0.181 0.752 0.5 0.155 0.03552 -0.058 0.395 0.608 0.507 0.651 4.373 0.328 0.623 1.0 0.202 0.03670 -0.062 0.392 0.609 0.494 0.654 5.502 0.330 0.555 1.5 0.248 0.03793 -0.065 0.389 0.611 0.482 0.657 6.552 0.331 0.513 2.0 0.295 0.03921 -0.069 0.386 0.612 0.472 0.659 7.528 0.331 0.485 2.5 0.343 0.04048 -0.073 0.383 0.614 0.464 0.661 8.472 0.330 0.463 3.0 0.391 0.04183 -0.077 0.380 0.616 0.457 0.664 9.338 0.331 0.447 3.5 0.439 0.04320 -0.081 0.376 0.617 0.452 0.667 10.152 0.330 0.434 4.0 0.487 0.04456 -0.085 0.370 0.619 0.448 0.669 10.933 0.330 0.424 4.5 0.535 0.04627 -0.088 0.364 0.621 0.444 0.672 11.564 0.331 0.415 5.0 0.583 0.04829 -0.092 0.359 0.623 0.439 0.675 12.065 0.333 0.409 5.5 0.630 0.05032 -0.096 0.354 0.625 0.434 0.678 12.512 0.334 0.403 6.0 0.676 0.05259 -0.100 0.349 0.627 0.429 0.682 12.857 0.335 0.398 6.5 0.722 0.05486 -0.104 0.344 0.629 0.424 0.684 13.164 0.336 0.394 7.0 0.768 0.05724 -0.108 0.339 0.632 0.419 0.687 13.422 0.336 0.391 7.5 0.814 0.05972 -0.112 0.333 0.634 0.414 0.691 13.630 0.333 0.388 8.0 0.862 0.06212 -0.116 0.318 0.637 0.416 0.693 13.878 0.332 0.384 8.5 0.908 0.06470 -0.120 0.303 0.640 0.416 0.699 14.027 0.331 0.382 9.0 0.955 0.06701 -0.123 0.277 0.643 0.423 0.703 14.256 0.292 0.379 9.5 1.038 0.06643 -0.125 0.164 0.646 0.483 0.707 15.633 0.278 0.371 10.0 1.104 0.06759 -0.128 0.057 0.647 0.515 0.714 16.332 0.313 0.366 10.5 1.139 0.07047 -0.132 0.020 0.650 0.508 0.719 16.166 0.438 0.365 11.0 1.152 0.07576 -0.137 0.010 0.652 0.477 0.726 15.208 -1.155 0.369 11.5 1.133 0.08675 -0.140 0.002 0.655 0.017 0.733 13.061 0.443 0.374 12.0 1.186 0.08845 -0.143 0.001 0.657 0.003 0.742 13.405 0.336 0.371 12.5 1.211 0.09454 -0.147 0.000 0.659 0.002 0.758 12.804 0.421 0.371 13.0 1.228 0.10230 -0.150 0.000 0.663 0.001 0.774 12.005 0.494 0.372 13.5 1.240 0.11153 -0.154 0.000 0.666 0.001 0.799 11.121 0.568 0.374 14.0 1.251 0.11899 -0.158 0.000 0.669 0.000 1.000 10.513 0.758 0.376 14.5 1.255 0.12884 -0.161 0.000 0.672 0.000 1.000 9.737 2.420 0.379 15.0 1.254 0.13879 -0.165 0.000 0.676 0.000 1.000 9.037 -11.547 0.381 Name = EPPLER 548 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 -0.584 0.15857 0.049 0.987 0.001 0.992 0.002 -3.682 1.821 0.335 -14.5 -0.582 0.14536 0.046 0.987 0.001 0.995 0.002 -4.003 1.199 0.329 -14.0 -0.577 0.13521 0.043 0.988 0.001 1.000 0.002 -4.269 0.795 0.324 -13.5 -0.570 0.12755 0.040 0.988 0.001 1.000 0.002 -4.469 0.629 0.320 -13.0 -0.560 0.11468 0.036 0.988 0.001 1.000 0.002 -4.884 0.532 0.315 -12.5 -0.547 0.10679 0.033 0.988 0.001 1.000 0.002 -5.122 0.479 0.311 -12.0 -0.531 0.10065 0.030 1.000 0.001 1.000 0.002 -5.280 0.446 0.306 -11.5 -0.513 0.09005 0.027 1.000 0.001 1.000 0.002 -5.700 0.420 0.302 -11.0 -0.492 0.08492 0.023 1.000 0.001 1.000 0.002 -5.796 0.400 0.297 -10.5 -0.469 0.07939 0.020 0.707 0.001 1.000 0.002 -5.905 0.386 0.293 -10.0 -0.443 0.07562 0.017 0.649 0.001 1.000 0.002 -5.853 0.374 0.287 -9.5 -0.414 0.06914 0.013 0.610 0.001 1.000 0.002 -5.989 0.366 0.282 -9.0 -0.384 0.06555 0.010 0.581 0.001 1.000 0.002 -5.854 0.359 0.275 -8.5 -0.351 0.06155 0.006 0.555 0.001 1.000 0.002 -5.705 0.353 0.268 -8.0 -0.317 0.05671 0.003 0.531 0.001 1.000 0.002 -5.585 0.348 0.259 -7.5 -0.280 0.05326 -0.001 0.510 0.001 1.000 0.002 -5.267 0.345 0.248 -7.0 -0.244 0.04961 -0.004 0.494 0.001 1.000 0.002 -4.916 0.344 0.233 -6.5 -0.206 0.04653 -0.008 0.478 0.001 1.000 0.001 -4.427 0.341 0.213 -6.0 -0.166 0.04341 -0.011 0.466 0.001 1.000 0.002 -3.834 0.337 0.183 -5.5 -0.125 0.04054 -0.015 0.457 0.001 1.000 0.002 -3.082 0.336 0.133 -5.0 -0.084 0.03850 -0.018 0.450 0.001 1.000 0.002 -2.186 0.333 0.034 -4.5 -0.040 0.03635 -0.022 0.442 0.001 1.000 0.004 -1.093 0.145 -0.296 -4.0 -0.182 0.03200 -0.028 0.436 0.589 1.000 0.639 -5.691 0.124 0.094 -3.5 -0.119 0.03159 -0.032 0.430 0.593 1.000 0.641 -3.758 0.301 -0.017 -3.0 -0.055 0.03076 -0.035 0.425 0.597 1.000 0.643 -1.804 0.301 -0.379 -2.5 0.008 0.02999 -0.038 0.419 0.599 1.000 0.646 0.251 0.302 5.331 -2.0 0.070 0.02934 -0.041 0.415 0.600 1.000 0.649 2.391 0.302 0.841 -1.5 0.132 0.02803 -0.045 0.411 0.602 1.000 0.651 4.723 0.302 0.587 -1.0 0.194 0.02431 -0.048 0.406 0.603 0.824 0.654 7.989 0.302 0.497 -0.5 0.256 0.02294 -0.051 0.402 0.605 0.744 0.657 11.145 -0.166 0.450 0.0 0.179 0.02309 -0.054 0.398 0.606 0.688 0.659 7.743 0.092 0.554 0.5 0.215 0.02444 -0.058 0.395 0.608 0.646 0.662 8.790 0.342 0.518 1.0 0.252 0.02589 -0.061 0.392 0.609 0.609 0.666 9.738 0.343 0.492 1.5 0.292 0.02732 -0.065 0.389 0.611 0.580 0.669 10.681 0.341 0.472 2.0 0.334 0.02872 -0.068 0.386 0.612 0.557 0.672 11.616 0.341 0.455 2.5 0.375 0.03018 -0.072 0.383 0.614 0.535 0.675 12.440 0.341 0.443 3.0 0.418 0.03165 -0.076 0.380 0.616 0.517 0.679 13.215 0.337 0.432 3.5 0.464 0.03295 -0.080 0.376 0.617 0.506 0.681 14.097 0.330 0.422 4.0 0.513 0.03434 -0.084 0.370 0.619 0.501 0.684 14.944 0.329 0.413 4.5 0.560 0.03597 -0.088 0.364 0.621 0.494 0.689 15.578 0.333 0.406 5.0 0.607 0.03772 -0.092 0.359 0.623 0.485 0.693 16.082 0.335 0.401 5.5 0.653 0.03950 -0.095 0.354 0.625 0.478 0.697 16.522 0.336 0.396 6.0 0.698 0.04149 -0.099 0.349 0.627 0.470 0.704 16.832 0.336 0.392 6.5 0.744 0.04339 -0.103 0.344 0.629 0.463 0.708 17.152 0.337 0.389 7.0 0.789 0.04543 -0.107 0.339 0.632 0.456 0.713 17.376 0.337 0.386 7.5 0.835 0.04747 -0.111 0.333 0.634 0.451 0.719 17.584 0.327 0.383 8.0 0.887 0.04908 -0.115 0.318 0.637 0.458 0.723 18.078 0.322 0.379 8.5 0.936 0.05092 -0.118 0.303 0.640 0.462 0.731 18.378 0.317 0.377 9.0 0.991 0.05219 -0.122 0.277 0.643 0.477 0.736 18.990 0.271 0.373 9.5 1.096 0.05081 -0.122 0.164 0.646 0.560 0.743 21.573 0.268 0.361 10.0 1.150 0.05437 -0.125 0.057 0.647 0.574 0.762 21.148 0.332 0.358 10.5 1.181 0.05821 -0.129 0.020 0.650 0.562 0.778 20.296 0.402 0.359 11.0 1.206 0.06251 -0.133 0.010 0.652 0.546 0.805 19.301 0.433 0.360 11.5 1.230 0.06565 -0.138 0.002 0.655 0.532 1.000 18.732 0.066 0.362 12.0 1.148 0.08220 -0.144 0.001 0.657 0.022 1.000 13.960 -0.139 0.376 12.5 1.206 0.08144 -0.147 0.000 0.659 0.003 1.000 14.809 0.331 0.372 13.0 1.226 0.08642 -0.150 0.000 0.663 0.002 1.000 14.181 0.471 0.373 13.5 1.239 0.09195 -0.154 0.000 0.666 0.001 1.000 13.472 0.553 0.374 14.0 1.249 0.09831 -0.158 0.000 0.669 0.001 1.000 12.710 0.745 0.376 14.5 1.253 0.10669 -0.161 0.000 0.672 0.001 1.000 11.749 2.046 0.379 15.0 1.253 0.11400 -0.165 0.000 0.676 0.000 1.000 10.996 118.066 0.382 Name = EPPLER 548 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 -0.584 0.14096 0.049 0.987 0.001 0.993 0.002 -4.141 1.814 0.335 -14.5 -0.582 0.13039 0.046 0.987 0.001 0.995 0.002 -4.461 1.196 0.329 -14.0 -0.577 0.12281 0.043 0.988 0.001 1.000 0.002 -4.698 0.806 0.324 -13.5 -0.570 0.11034 0.040 0.988 0.001 1.000 0.002 -5.166 0.628 0.320 -13.0 -0.560 0.10538 0.037 0.988 0.001 1.000 0.002 -5.312 0.529 0.315 -12.5 -0.547 0.09750 0.033 0.988 0.001 1.000 0.002 -5.608 0.481 0.311 -12.0 -0.531 0.08782 0.030 1.000 0.001 1.000 0.002 -6.051 0.446 0.306 -11.5 -0.513 0.08317 0.027 1.000 0.001 1.000 0.002 -6.168 0.420 0.302 -11.0 -0.492 0.07522 0.023 1.000 0.001 1.000 0.002 -6.544 0.400 0.297 -10.5 -0.468 0.07445 0.020 0.707 0.001 1.000 0.002 -6.292 0.386 0.293 -10.0 -0.443 0.06867 0.017 0.649 0.001 1.000 0.002 -6.446 0.374 0.287 -9.5 -0.414 0.06487 0.013 0.610 0.001 1.000 0.002 -6.378 0.366 0.282 -9.0 -0.384 0.06023 0.010 0.581 0.001 1.000 0.002 -6.371 0.359 0.275 -8.5 -0.351 0.05702 0.006 0.555 0.001 1.000 0.002 -6.158 0.352 0.268 -8.0 -0.316 0.05354 0.003 0.531 0.001 1.000 0.002 -5.909 0.348 0.259 -7.5 -0.280 0.04972 -0.001 0.510 0.001 1.000 0.002 -5.641 0.346 0.248 -7.0 -0.244 0.04665 -0.004 0.494 0.001 1.000 0.002 -5.228 0.344 0.233 -6.5 -0.206 0.04395 -0.008 0.478 0.001 1.000 0.001 -4.686 0.340 0.213 -6.0 -0.166 0.04128 -0.011 0.466 0.001 1.000 0.002 -4.024 0.336 0.183 -5.5 -0.125 0.03899 -0.015 0.457 0.001 1.000 0.002 -3.195 0.335 0.133 -5.0 -0.083 0.03666 -0.018 0.450 0.001 1.000 0.003 -2.277 0.330 0.032 -4.5 -0.037 0.03534 -0.022 0.442 0.001 1.000 0.006 -1.037 0.378 -0.341 -4.0 -0.002 0.02958 -0.029 0.436 0.589 1.000 0.647 -0.055 0.126 -17.220 -3.5 -0.119 0.02915 -0.032 0.430 0.593 1.000 0.648 -4.070 0.131 -0.019 -3.0 -0.055 0.02880 -0.035 0.425 0.597 1.000 0.650 -1.926 0.301 -0.382 -2.5 0.008 0.02845 -0.038 0.419 0.599 1.000 0.653 0.264 0.302 5.350 -2.0 0.070 0.02816 -0.042 0.415 0.600 1.000 0.657 2.491 0.302 0.842 -1.5 0.132 0.02753 -0.045 0.411 0.602 1.000 0.660 4.808 0.302 0.588 -1.0 0.194 0.02668 -0.048 0.406 0.603 1.000 0.663 7.278 0.302 0.497 -0.5 0.256 0.02613 -0.051 0.402 0.605 1.000 0.667 9.783 0.302 0.450 0.0 0.317 0.02215 -0.054 0.398 0.606 1.000 0.670 14.303 0.288 0.421 0.5 0.379 0.02150 -0.056 0.395 0.608 1.000 0.673 17.610 0.440 0.397 1.0 0.344 0.01938 -0.060 0.392 0.609 0.802 0.677 17.763 -0.513 0.423 1.5 0.369 0.02005 -0.063 0.389 0.611 0.736 0.681 18.410 0.382 0.421 2.0 0.399 0.02160 -0.067 0.386 0.612 0.686 0.685 18.478 0.372 0.417 2.5 0.432 0.02325 -0.071 0.383 0.614 0.644 0.688 18.566 0.366 0.414 3.0 0.467 0.02490 -0.075 0.380 0.616 0.610 0.693 18.756 0.353 0.410 3.5 0.508 0.02663 -0.079 0.376 0.617 0.587 0.698 19.073 0.338 0.405 4.0 0.554 0.02807 -0.082 0.370 0.619 0.576 0.702 19.738 0.333 0.398 4.5 0.599 0.02970 -0.086 0.364 0.621 0.563 0.709 20.173 0.337 0.394 5.0 0.643 0.03142 -0.090 0.359 0.623 0.549 0.716 20.474 0.339 0.390 5.5 0.687 0.03318 -0.094 0.354 0.625 0.536 0.721 20.711 0.342 0.387 6.0 0.730 0.03518 -0.098 0.349 0.627 0.523 0.730 20.748 0.343 0.384 6.5 0.774 0.03707 -0.102 0.344 0.629 0.511 0.735 20.868 0.343 0.382 7.0 0.817 0.03909 -0.106 0.339 0.632 0.500 0.744 20.887 0.342 0.380 7.5 0.860 0.04114 -0.110 0.333 0.634 0.491 0.756 20.914 0.322 0.378 8.0 0.918 0.04231 -0.113 0.318 0.637 0.504 0.767 21.686 0.313 0.373 8.5 0.968 0.04392 -0.117 0.303 0.640 0.509 0.783 22.047 0.306 0.371 9.0 1.029 0.04492 -0.120 0.277 0.643 0.530 0.805 22.917 0.264 0.366 9.5 1.134 0.04461 -0.119 0.164 0.646 0.607 0.828 25.416 0.272 0.355 10.0 1.175 0.04971 -0.123 0.057 0.647 0.604 1.000 23.635 0.369 0.355 10.5 1.202 0.05314 -0.127 0.020 0.650 0.587 1.000 22.615 0.427 0.356 11.0 1.226 0.05637 -0.132 0.010 0.652 0.570 1.000 21.747 0.436 0.358 11.5 1.250 0.05930 -0.136 0.002 0.655 0.556 1.000 21.072 0.480 0.359 12.0 1.265 0.06264 -0.141 0.001 0.657 0.537 1.000 20.201 0.107 0.361 12.5 1.169 0.08112 -0.148 0.000 0.659 0.021 1.000 14.408 0.031 0.376 13.0 1.222 0.08009 -0.150 0.000 0.663 0.003 1.000 15.256 0.343 0.373 13.5 1.236 0.08469 -0.154 0.000 0.666 0.002 1.000 14.597 0.540 0.375 14.0 1.247 0.09113 -0.158 0.000 0.669 0.001 1.000 13.681 0.711 0.376 14.5 1.252 0.09687 -0.161 0.000 0.672 0.001 1.000 12.924 1.544 0.379 15.0 1.252 0.10318 -0.165 0.000 0.676 0.001 1.000 12.138 8.746 0.382 Name = EPPLER 548 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 -0.583 0.13077 0.049 0.987 0.001 0.993 0.003 -4.462 1.806 0.335 -14.5 -0.581 0.12188 0.046 0.987 0.001 0.995 0.002 -4.771 1.226 0.329 -14.0 -0.577 0.11060 0.043 0.988 0.001 1.000 0.002 -5.217 0.805 0.324 -13.5 -0.570 0.10443 0.040 0.988 0.001 1.000 0.002 -5.457 0.628 0.320 -13.0 -0.560 0.09585 0.037 0.988 0.001 1.000 0.002 -5.841 0.532 0.315 -12.5 -0.547 0.08828 0.033 0.988 0.001 1.000 0.002 -6.193 0.479 0.311 -12.0 -0.531 0.08369 0.030 1.000 0.001 1.000 0.002 -6.347 0.446 0.306 -11.5 -0.513 0.07617 0.027 1.000 0.001 1.000 0.002 -6.735 0.421 0.302 -11.0 -0.492 0.06953 0.023 1.000 0.001 1.000 0.002 -7.079 0.400 0.297 -10.5 -0.468 0.06918 0.020 0.707 0.001 1.000 0.002 -6.772 0.386 0.293 -10.0 -0.443 0.06436 0.017 0.649 0.001 1.000 0.002 -6.877 0.374 0.287 -9.5 -0.414 0.06095 0.013 0.610 0.001 1.000 0.002 -6.788 0.365 0.282 -9.0 -0.383 0.05839 0.010 0.581 0.001 1.000 0.002 -6.567 0.359 0.275 -8.5 -0.351 0.05419 0.006 0.555 0.001 1.000 0.002 -6.478 0.353 0.268 -8.0 -0.316 0.05094 0.003 0.531 0.001 1.000 0.002 -6.211 0.347 0.259 -7.5 -0.280 0.04813 -0.001 0.510 0.001 1.000 0.002 -5.821 0.346 0.248 -7.0 -0.244 0.04520 -0.004 0.494 0.001 1.000 0.002 -5.389 0.344 0.233 -6.5 -0.206 0.04274 -0.008 0.478 0.001 1.000 0.002 -4.811 0.341 0.213 -6.0 -0.166 0.03984 -0.011 0.466 0.001 1.000 0.002 -4.169 0.336 0.183 -5.5 -0.124 0.03790 -0.015 0.457 0.001 1.000 0.003 -3.268 0.335 0.132 -5.0 -0.083 0.03610 -0.018 0.450 0.001 1.000 0.003 -2.294 -0.002 0.031 -4.5 -0.209 0.02845 -0.036 0.442 0.001 1.000 0.903 -7.342 0.389 0.077 -4.0 -0.006 0.02801 -0.029 0.436 0.589 1.000 0.654 -0.214 0.205 -4.563 -3.5 -0.119 0.02758 -0.032 0.430 0.593 1.000 0.655 -4.302 0.122 -0.020 -3.0 -0.055 0.02720 -0.035 0.425 0.597 1.000 0.657 -2.038 0.301 -0.385 -2.5 0.008 0.02737 -0.038 0.419 0.599 1.000 0.660 0.274 0.301 5.369 -2.0 0.070 0.02702 -0.042 0.415 0.600 1.000 0.665 2.595 0.301 0.844 -1.5 0.132 0.02629 -0.045 0.411 0.602 1.000 0.668 5.033 0.301 0.589 -1.0 0.194 0.02606 -0.048 0.406 0.603 1.000 0.672 7.451 0.301 0.497 -0.5 0.256 0.02551 -0.051 0.402 0.605 1.000 0.676 10.022 0.301 0.450 0.0 0.317 0.02240 -0.054 0.398 0.606 1.000 0.680 14.144 0.288 0.421 0.5 0.379 0.02187 -0.056 0.395 0.608 1.000 0.684 17.313 0.274 0.397 1.0 0.440 0.02147 -0.057 0.392 0.609 1.000 0.689 20.513 0.274 0.380 1.5 0.502 0.02098 -0.059 0.389 0.611 1.000 0.694 23.931 0.364 0.367 2.0 0.494 0.01878 -0.063 0.386 0.612 0.869 0.699 26.311 1.536 0.378 2.5 0.509 0.01847 -0.068 0.383 0.614 0.787 0.705 27.560 0.465 0.383 3.0 0.534 0.01980 -0.072 0.380 0.616 0.729 0.712 26.972 0.391 0.385 3.5 0.568 0.02155 -0.076 0.376 0.617 0.691 0.718 26.347 0.354 0.384 4.0 0.609 0.02303 -0.080 0.370 0.619 0.669 0.723 26.469 0.343 0.381 4.5 0.650 0.02468 -0.084 0.364 0.621 0.647 0.731 26.355 0.350 0.379 5.0 0.689 0.02652 -0.088 0.359 0.623 0.624 0.739 25.991 0.351 0.377 5.5 0.731 0.02832 -0.092 0.354 0.625 0.605 0.750 25.799 0.350 0.376 6.0 0.771 0.03041 -0.096 0.349 0.627 0.586 0.767 25.353 0.354 0.375 6.5 0.810 0.03250 -0.100 0.344 0.629 0.567 0.779 24.925 0.355 0.374 7.0 0.850 0.03468 -0.104 0.339 0.632 0.551 0.797 24.524 0.350 0.373 7.5 0.892 0.03692 -0.108 0.333 0.634 0.539 0.823 24.167 0.320 0.371 8.0 0.952 0.03819 -0.111 0.318 0.637 0.553 0.855 24.935 0.307 0.367 8.5 1.004 0.04071 -0.115 0.303 0.640 0.558 1.000 24.655 0.302 0.364 9.0 1.066 0.04067 -0.117 0.277 0.643 0.579 1.000 26.216 0.265 0.360 9.5 1.161 0.04058 -0.117 0.164 0.646 0.641 1.000 28.611 0.282 0.351 10.0 1.193 0.04526 -0.121 0.057 0.647 0.626 1.000 26.352 0.413 0.352 10.5 1.217 0.04900 -0.126 0.020 0.650 0.605 1.000 24.831 0.450 0.354 11.0 1.240 0.05229 -0.131 0.010 0.652 0.587 1.000 23.709 0.458 0.356 11.5 1.261 0.05544 -0.135 0.002 0.655 0.570 1.000 22.742 0.480 0.357 12.0 1.279 0.05862 -0.140 0.001 0.657 0.554 1.000 21.821 0.572 0.359 12.5 1.290 0.06218 -0.145 0.000 0.659 0.533 1.000 20.747 0.109 0.362 13.0 1.201 0.07966 -0.151 0.000 0.663 0.010 1.000 15.080 0.087 0.376 13.5 1.233 0.08083 -0.154 0.000 0.666 0.003 1.000 15.251 0.410 0.375 14.0 1.244 0.08618 -0.158 0.000 0.669 0.002 1.000 14.434 0.664 0.377 14.5 1.250 0.09165 -0.161 0.000 0.672 0.001 1.000 13.641 1.278 0.379 15.0 1.251 0.09722 -0.165 0.000 0.676 0.001 1.000 12.868 4.598 0.382