Name = AH 81-K-144/17 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 -0.457 0.26454 0.002 0.668 0.002 0.711 0.004 -1.727 0.683 0.255 -14.5 -0.450 0.23311 -0.001 0.666 0.002 0.709 0.003 -1.930 0.624 0.248 -14.0 -0.441 0.21481 -0.004 0.665 0.002 0.707 0.003 -2.052 0.544 0.241 -13.5 -0.429 0.19653 -0.007 0.663 0.002 0.704 0.003 -2.183 0.490 0.234 -13.0 -0.415 0.18090 -0.010 0.662 0.002 0.702 0.003 -2.293 0.454 0.226 -12.5 -0.398 0.16560 -0.013 0.660 0.002 0.701 0.003 -2.406 0.426 0.217 -12.0 -0.379 0.14390 -0.016 0.658 0.002 0.699 0.003 -2.635 0.408 0.207 -11.5 -0.358 0.13281 -0.019 0.655 0.002 0.697 0.003 -2.696 0.393 0.196 -11.0 -0.334 0.11994 -0.023 0.653 0.002 0.696 0.003 -2.788 0.379 0.182 -10.5 -0.308 0.10789 -0.026 0.651 0.002 0.694 0.003 -2.855 0.368 0.166 -10.0 -0.280 0.09883 -0.029 0.649 0.002 0.692 0.003 -2.829 0.359 0.146 -9.5 -0.249 0.08968 -0.032 0.647 0.002 0.690 0.003 -2.772 0.354 0.120 -9.0 -0.216 0.08051 -0.036 0.646 0.003 0.688 0.004 -2.687 0.350 0.085 -8.5 -0.183 0.07436 -0.039 0.644 0.003 0.686 0.004 -2.455 0.345 0.036 -8.0 -0.146 0.06754 -0.042 0.642 0.003 0.684 0.004 -2.167 0.341 -0.039 -7.5 -0.109 0.06230 -0.046 0.641 0.003 0.682 0.004 -1.752 0.339 -0.169 -7.0 -0.071 0.05626 -0.049 0.639 0.004 0.681 0.005 -1.263 0.337 -0.441 -6.5 -0.032 0.05189 -0.052 0.637 0.004 0.678 0.006 -0.613 0.217 -1.399 -6.0 -0.277 0.04819 -0.056 0.636 0.005 0.677 0.006 -5.739 0.212 0.048 -5.5 -0.211 0.04458 -0.059 0.634 0.005 0.675 0.007 -4.724 0.302 -0.032 -5.0 -0.145 0.04127 -0.063 0.633 0.006 0.673 0.008 -3.507 0.303 -0.183 -4.5 -0.079 0.03836 -0.066 0.632 0.007 0.671 0.009 -2.063 0.303 -0.587 -4.0 -0.014 0.03597 -0.070 0.630 0.008 0.669 0.010 -0.391 0.300 -4.703 -3.5 0.050 0.03515 -0.073 0.627 0.009 0.668 0.045 1.428 0.416 1.699 -3.0 0.108 0.02176 -0.090 0.624 0.093 0.667 1.000 4.973 0.358 1.081 -2.5 0.171 0.02620 -0.086 0.621 0.726 0.666 0.804 6.507 0.236 0.753 -2.0 0.232 0.02618 -0.088 0.618 0.739 0.665 0.806 8.846 0.291 0.631 -1.5 0.292 0.02622 -0.091 0.616 0.751 0.663 0.807 11.145 0.291 0.560 -1.0 0.353 0.02632 -0.093 0.613 0.757 0.661 0.810 13.401 0.292 0.514 -0.5 0.413 0.02649 -0.096 0.611 0.763 0.659 0.812 15.588 0.189 0.482 0.0 0.272 0.03218 -0.098 0.608 0.768 0.657 0.815 8.440 0.187 0.612 0.5 0.324 0.03278 -0.101 0.606 0.773 0.655 0.816 9.878 0.311 0.563 1.0 0.376 0.03345 -0.105 0.603 0.778 0.653 0.818 11.241 0.311 0.528 1.5 0.428 0.03413 -0.108 0.601 0.781 0.651 0.821 12.549 0.312 0.502 2.0 0.480 0.03492 -0.111 0.598 0.783 0.649 0.823 13.753 0.312 0.481 2.5 0.533 0.03569 -0.114 0.593 0.785 0.647 0.826 14.925 0.312 0.465 3.0 0.585 0.03654 -0.118 0.587 0.787 0.646 0.828 16.006 0.313 0.451 3.5 0.637 0.03744 -0.121 0.582 0.789 0.645 0.830 17.011 0.314 0.440 4.0 0.688 0.03842 -0.124 0.576 0.792 0.643 0.833 17.919 0.315 0.430 4.5 0.740 0.03948 -0.127 0.571 0.794 0.641 0.835 18.738 0.315 0.422 5.0 0.790 0.04065 -0.131 0.566 0.796 0.639 0.838 19.445 0.315 0.416 5.5 0.842 0.04189 -0.134 0.554 0.798 0.639 0.841 20.094 0.315 0.409 6.0 0.892 0.04327 -0.137 0.544 0.801 0.638 0.843 20.621 0.317 0.404 6.5 0.942 0.04475 -0.141 0.532 0.803 0.637 0.846 21.042 0.262 0.400 7.0 1.072 0.04163 -0.140 0.009 0.805 0.725 0.849 25.741 0.426 0.380 7.5 1.014 0.04865 -0.154 0.008 0.807 0.014 0.852 20.842 -0.790 0.401 8.0 1.055 0.05207 -0.157 0.006 0.808 0.010 0.855 20.253 0.344 0.399 8.5 1.091 0.05584 -0.161 0.005 0.810 0.008 0.861 19.542 0.353 0.397 9.0 1.125 0.06041 -0.165 0.004 0.812 0.006 0.867 18.630 0.362 0.396 9.5 1.156 0.06560 -0.168 0.003 0.813 0.005 0.873 17.629 0.377 0.395 10.0 1.183 0.06897 -0.172 0.003 0.815 0.004 1.000 17.157 0.395 0.395 10.5 1.207 0.07521 -0.176 0.002 0.817 0.004 1.000 16.054 0.417 0.395 11.0 1.228 0.08158 -0.179 0.002 0.818 0.003 1.000 15.049 0.451 0.396 11.5 1.244 0.09100 -0.183 0.002 0.820 0.003 1.000 13.673 0.494 0.397 12.0 1.258 0.09678 -0.187 0.002 0.823 0.003 1.000 12.998 0.572 0.398 12.5 1.267 0.10868 -0.190 0.001 0.824 0.003 1.000 11.658 0.744 0.400 13.0 1.273 0.11621 -0.194 0.001 0.827 0.002 1.000 10.953 1.270 0.402 13.5 1.274 0.12708 -0.198 0.001 0.829 0.002 1.000 10.028 -8.288 0.405 14.0 1.272 0.14743 -0.201 0.001 0.832 0.002 1.000 8.628 -0.634 0.408 14.5 1.266 0.15749 -0.205 0.001 0.834 0.002 1.000 8.038 -0.197 0.412 15.0 1.256 0.17532 -0.209 0.001 0.837 0.002 1.000 7.162 -0.103 0.416 Name = AH 81-K-144/17 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 -0.457 0.19783 0.002 0.668 0.002 0.725 0.004 -2.309 0.674 0.255 -14.5 -0.450 0.18253 -0.001 0.666 0.002 0.722 0.004 -2.464 0.621 0.248 -14.0 -0.440 0.17043 -0.004 0.665 0.002 0.720 0.004 -2.584 0.546 0.241 -13.5 -0.429 0.15203 -0.007 0.663 0.002 0.717 0.003 -2.821 0.491 0.234 -13.0 -0.415 0.14003 -0.010 0.662 0.002 0.714 0.003 -2.962 0.454 0.226 -12.5 -0.398 0.12975 -0.013 0.660 0.002 0.712 0.003 -3.069 0.426 0.217 -12.0 -0.379 0.11410 -0.016 0.658 0.002 0.710 0.003 -3.322 0.408 0.207 -11.5 -0.358 0.10635 -0.019 0.655 0.002 0.709 0.003 -3.366 0.393 0.196 -11.0 -0.334 0.09720 -0.023 0.653 0.002 0.707 0.003 -3.439 0.379 0.182 -10.5 -0.308 0.08758 -0.026 0.651 0.002 0.705 0.003 -3.516 0.368 0.166 -10.0 -0.279 0.08059 -0.029 0.649 0.002 0.703 0.003 -3.467 0.359 0.146 -9.5 -0.248 0.07311 -0.032 0.647 0.002 0.701 0.004 -3.398 0.353 0.120 -9.0 -0.216 0.06739 -0.036 0.646 0.003 0.699 0.004 -3.204 0.350 0.085 -8.5 -0.182 0.06230 -0.039 0.644 0.003 0.697 0.004 -2.924 0.345 0.036 -8.0 -0.146 0.05656 -0.042 0.642 0.003 0.695 0.004 -2.580 0.341 -0.040 -7.5 -0.109 0.05191 -0.046 0.641 0.003 0.693 0.005 -2.097 0.339 -0.170 -7.0 -0.071 0.04829 -0.049 0.639 0.004 0.692 0.005 -1.460 0.337 -0.446 -6.5 -0.031 0.04451 -0.052 0.637 0.004 0.689 0.006 -0.703 0.217 -1.427 -6.0 -0.277 0.04085 -0.056 0.636 0.005 0.687 0.007 -6.770 0.212 0.048 -5.5 -0.211 0.03772 -0.059 0.634 0.005 0.685 0.007 -5.583 0.302 -0.031 -5.0 -0.145 0.03488 -0.063 0.633 0.006 0.682 0.008 -4.149 0.303 -0.183 -4.5 -0.079 0.03252 -0.066 0.632 0.007 0.681 0.009 -2.433 0.303 -0.586 -4.0 -0.014 0.03050 -0.070 0.630 0.008 0.678 0.014 -0.461 0.427 -4.699 -3.5 0.047 0.01623 -0.089 0.627 0.009 0.678 1.000 2.922 0.416 2.118 -3.0 0.108 0.01640 -0.090 0.624 0.093 0.677 1.000 6.598 0.229 1.081 -2.5 0.170 0.01885 -0.086 0.621 0.726 0.675 0.815 9.043 0.238 0.754 -2.0 0.231 0.01883 -0.088 0.618 0.739 0.674 0.815 12.293 0.290 0.632 -1.5 0.292 0.01885 -0.091 0.616 0.751 0.672 0.815 15.498 0.291 0.561 -1.0 0.353 0.01890 -0.093 0.613 0.757 0.671 0.817 18.655 0.291 0.515 -0.5 0.413 0.01902 -0.096 0.611 0.763 0.669 0.819 21.704 0.184 0.482 0.0 0.278 0.02431 -0.098 0.608 0.768 0.668 0.822 11.441 0.182 0.603 0.5 0.331 0.02480 -0.101 0.606 0.773 0.666 0.823 13.336 0.310 0.556 1.0 0.383 0.02533 -0.105 0.603 0.778 0.664 0.825 15.129 0.310 0.523 1.5 0.436 0.02586 -0.108 0.601 0.781 0.663 0.827 16.852 0.311 0.497 2.0 0.488 0.02649 -0.111 0.598 0.783 0.660 0.830 18.416 0.311 0.477 2.5 0.541 0.02709 -0.114 0.593 0.785 0.660 0.833 19.974 0.310 0.461 3.0 0.594 0.02775 -0.117 0.587 0.787 0.660 0.836 21.411 0.311 0.447 3.5 0.647 0.02844 -0.120 0.582 0.789 0.659 0.839 22.741 0.312 0.436 4.0 0.699 0.02921 -0.124 0.576 0.792 0.657 0.842 23.927 0.313 0.427 4.5 0.751 0.03008 -0.127 0.571 0.794 0.656 0.844 24.956 0.314 0.419 5.0 0.802 0.03106 -0.130 0.566 0.796 0.654 0.848 25.816 0.312 0.413 5.5 0.855 0.03196 -0.134 0.554 0.798 0.656 0.851 26.754 0.311 0.406 6.0 0.907 0.03296 -0.137 0.544 0.801 0.656 0.854 27.522 0.312 0.401 6.5 0.958 0.03405 -0.140 0.532 0.803 0.657 0.859 28.129 0.257 0.396 7.0 1.096 0.03453 -0.138 0.009 0.805 0.750 0.865 31.752 0.259 0.376 7.5 1.137 0.03651 -0.142 0.008 0.807 0.741 0.872 31.146 -0.178 0.374 8.0 1.051 0.04460 -0.157 0.006 0.808 0.012 1.000 23.577 -0.150 0.400 8.5 1.089 0.04783 -0.161 0.005 0.810 0.009 1.000 22.766 0.351 0.398 9.0 1.124 0.05103 -0.165 0.004 0.812 0.007 1.000 22.020 0.362 0.396 9.5 1.155 0.05552 -0.168 0.003 0.813 0.006 1.000 20.796 0.375 0.396 10.0 1.183 0.05975 -0.172 0.003 0.815 0.005 1.000 19.792 0.391 0.395 10.5 1.207 0.06387 -0.176 0.002 0.817 0.004 1.000 18.895 0.417 0.395 11.0 1.227 0.07065 -0.179 0.002 0.818 0.004 1.000 17.363 0.451 0.396 11.5 1.244 0.07581 -0.183 0.002 0.820 0.003 1.000 16.405 0.494 0.397 12.0 1.257 0.08297 -0.187 0.002 0.823 0.003 1.000 15.150 0.571 0.399 12.5 1.267 0.08960 -0.190 0.001 0.824 0.003 1.000 14.136 0.742 0.400 13.0 1.272 0.09956 -0.194 0.001 0.827 0.003 1.000 12.776 1.336 0.403 13.5 1.273 0.10761 -0.198 0.001 0.829 0.002 1.000 11.833 -19.572 0.405 14.0 1.272 0.11704 -0.201 0.001 0.832 0.002 1.000 10.864 -0.688 0.408 14.5 1.266 0.12491 -0.205 0.001 0.834 0.002 1.000 10.132 -0.198 0.412 15.0 1.255 0.13780 -0.209 0.001 0.837 0.002 1.000 9.109 -0.104 0.416 Name = AH 81-K-144/17 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 -0.457 0.17456 0.002 0.668 0.002 0.740 0.004 -2.616 0.673 0.255 -14.5 -0.449 0.16120 -0.001 0.666 0.002 0.736 0.004 -2.788 0.624 0.248 -14.0 -0.440 0.14676 -0.004 0.665 0.002 0.734 0.004 -3.000 0.548 0.241 -13.5 -0.429 0.13274 -0.007 0.663 0.002 0.729 0.003 -3.230 0.491 0.234 -13.0 -0.415 0.12239 -0.010 0.662 0.002 0.726 0.003 -3.388 0.453 0.226 -12.5 -0.398 0.11432 -0.013 0.660 0.002 0.724 0.003 -3.482 0.426 0.217 -12.0 -0.379 0.10127 -0.016 0.658 0.002 0.722 0.003 -3.741 0.407 0.207 -11.5 -0.358 0.09499 -0.019 0.655 0.002 0.720 0.003 -3.766 0.393 0.196 -11.0 -0.334 0.08749 -0.023 0.653 0.002 0.718 0.003 -3.818 0.379 0.182 -10.5 -0.308 0.07883 -0.026 0.651 0.002 0.716 0.003 -3.904 0.368 0.166 -10.0 -0.279 0.07270 -0.029 0.649 0.002 0.713 0.003 -3.841 0.359 0.146 -9.5 -0.248 0.06594 -0.032 0.647 0.002 0.711 0.004 -3.765 0.353 0.119 -9.0 -0.216 0.06082 -0.036 0.646 0.003 0.709 0.004 -3.547 0.350 0.085 -8.5 -0.182 0.05635 -0.039 0.644 0.003 0.707 0.004 -3.229 0.345 0.036 -8.0 -0.146 0.05182 -0.042 0.642 0.003 0.705 0.004 -2.810 0.341 -0.041 -7.5 -0.109 0.04757 -0.046 0.641 0.003 0.702 0.005 -2.283 0.339 -0.171 -7.0 -0.070 0.04425 -0.049 0.639 0.004 0.701 0.006 -1.588 0.337 -0.448 -6.5 -0.031 0.04084 -0.052 0.637 0.004 0.698 0.006 -0.759 0.217 -1.442 -6.0 -0.277 0.03765 -0.056 0.636 0.005 0.697 0.007 -7.344 0.212 0.048 -5.5 -0.211 0.03474 -0.059 0.634 0.005 0.695 0.007 -6.062 0.302 -0.031 -5.0 -0.145 0.03233 -0.063 0.633 0.006 0.692 0.008 -4.476 0.303 -0.183 -4.5 -0.079 0.02984 -0.066 0.632 0.007 0.690 0.009 -2.652 0.437 -0.586 -4.0 -0.013 0.01396 -0.087 0.630 0.008 0.687 1.000 -0.943 0.427 -6.383 -3.5 0.047 0.01399 -0.089 0.627 0.009 0.686 1.000 3.391 0.272 2.118 -3.0 0.108 0.01398 -0.090 0.624 0.093 0.686 1.000 7.741 0.230 1.081 -2.5 0.170 0.01558 -0.086 0.621 0.726 0.684 0.823 10.934 0.239 0.756 -2.0 0.231 0.01556 -0.089 0.618 0.739 0.683 0.823 14.869 0.289 0.633 -1.5 0.292 0.01559 -0.091 0.616 0.751 0.681 0.822 18.742 0.290 0.561 -1.0 0.353 0.01562 -0.093 0.613 0.757 0.680 0.824 22.571 0.290 0.515 -0.5 0.413 0.01570 -0.096 0.611 0.763 0.678 0.826 26.295 0.180 0.482 0.0 0.284 0.02069 -0.098 0.608 0.768 0.676 0.828 13.711 0.178 0.596 0.5 0.337 0.02114 -0.101 0.606 0.773 0.675 0.829 15.921 0.309 0.551 1.0 0.389 0.02161 -0.104 0.603 0.778 0.672 0.831 18.004 0.309 0.519 1.5 0.442 0.02209 -0.108 0.601 0.781 0.671 0.834 20.004 0.310 0.493 2.0 0.494 0.02264 -0.111 0.598 0.783 0.669 0.837 21.824 0.310 0.474 2.5 0.548 0.02315 -0.114 0.593 0.785 0.669 0.840 23.671 0.309 0.458 3.0 0.602 0.02371 -0.117 0.587 0.787 0.669 0.844 25.377 0.309 0.445 3.5 0.655 0.02429 -0.120 0.582 0.789 0.669 0.847 26.956 0.310 0.434 4.0 0.708 0.02503 -0.123 0.576 0.792 0.668 0.850 28.271 0.311 0.424 4.5 0.760 0.02580 -0.127 0.571 0.794 0.667 0.854 29.453 0.312 0.417 5.0 0.812 0.02665 -0.130 0.566 0.796 0.666 0.859 30.457 0.310 0.410 5.5 0.866 0.02741 -0.133 0.554 0.798 0.669 0.865 31.584 0.308 0.404 6.0 0.919 0.02826 -0.136 0.544 0.801 0.670 0.872 32.513 0.310 0.398 6.5 0.970 0.02768 -0.139 0.532 0.803 0.671 1.000 35.064 0.254 0.394 7.0 1.116 0.02925 -0.137 0.009 0.805 0.770 1.000 38.144 0.256 0.373 7.5 1.156 0.03110 -0.140 0.008 0.807 0.760 1.000 37.166 -0.045 0.371 8.0 1.046 0.04271 -0.157 0.006 0.808 0.015 1.000 24.491 -0.050 0.400 8.5 1.087 0.04513 -0.161 0.005 0.810 0.010 1.000 24.085 0.345 0.398 9.0 1.122 0.04806 -0.165 0.004 0.812 0.008 1.000 23.347 0.361 0.397 9.5 1.153 0.05176 -0.168 0.003 0.813 0.007 1.000 22.280 0.374 0.396 10.0 1.181 0.05586 -0.172 0.003 0.815 0.005 1.000 21.146 0.390 0.396 10.5 1.206 0.05978 -0.176 0.002 0.817 0.004 1.000 20.171 0.414 0.396 11.0 1.226 0.06474 -0.179 0.002 0.818 0.004 1.000 18.939 0.448 0.396 11.5 1.243 0.06920 -0.183 0.002 0.820 0.004 1.000 17.964 0.493 0.397 12.0 1.256 0.07530 -0.187 0.002 0.823 0.003 1.000 16.685 0.571 0.399 12.5 1.266 0.08130 -0.190 0.001 0.824 0.003 1.000 15.574 0.741 0.400 13.0 1.271 0.08983 -0.194 0.001 0.827 0.003 1.000 14.154 1.332 0.403 13.5 1.273 0.09614 -0.198 0.001 0.829 0.003 1.000 13.240 -20.548 0.405 14.0 1.271 0.10393 -0.201 0.001 0.832 0.002 1.000 12.230 -0.644 0.408 14.5 1.265 0.11567 -0.205 0.001 0.834 0.002 1.000 10.934 -0.199 0.412 15.0 1.255 0.12162 -0.209 0.001 0.837 0.002 1.000 10.317 -0.118 0.416 Name = AH 81-K-144/17 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 -0.457 0.15618 0.002 0.668 0.002 0.757 0.004 -2.923 0.673 0.255 -14.5 -0.449 0.14430 -0.001 0.666 0.002 0.751 0.004 -3.114 0.623 0.248 -14.0 -0.440 0.13280 -0.004 0.665 0.002 0.747 0.004 -3.315 0.546 0.241 -13.5 -0.429 0.12499 -0.007 0.663 0.002 0.743 0.004 -3.429 0.491 0.234 -13.0 -0.414 0.11201 -0.010 0.662 0.002 0.739 0.004 -3.700 0.455 0.226 -12.5 -0.398 0.10528 -0.013 0.660 0.002 0.736 0.003 -3.780 0.426 0.217 -12.0 -0.379 0.09377 -0.016 0.658 0.002 0.734 0.004 -4.038 0.407 0.207 -11.5 -0.358 0.08839 -0.019 0.655 0.002 0.732 0.003 -4.046 0.394 0.196 -11.0 -0.334 0.07972 -0.023 0.653 0.002 0.729 0.003 -4.190 0.379 0.182 -10.5 -0.308 0.07372 -0.026 0.651 0.002 0.727 0.003 -4.172 0.368 0.166 -10.0 -0.279 0.06808 -0.029 0.649 0.002 0.724 0.003 -4.099 0.359 0.146 -9.5 -0.248 0.06172 -0.032 0.647 0.002 0.722 0.004 -4.019 0.353 0.119 -9.0 -0.216 0.05696 -0.036 0.646 0.003 0.719 0.004 -3.784 0.349 0.084 -8.5 -0.182 0.05349 -0.039 0.644 0.003 0.717 0.004 -3.394 0.345 0.035 -8.0 -0.145 0.04877 -0.042 0.642 0.003 0.714 0.005 -2.981 0.341 -0.041 -7.5 -0.108 0.04501 -0.046 0.641 0.003 0.712 0.005 -2.408 0.339 -0.172 -7.0 -0.070 0.04187 -0.049 0.639 0.004 0.710 0.006 -1.672 0.337 -0.451 -6.5 -0.031 0.03869 -0.052 0.637 0.004 0.707 0.007 -0.794 0.217 -1.456 -6.0 -0.277 0.03577 -0.056 0.636 0.005 0.705 0.007 -7.730 0.212 0.048 -5.5 -0.211 0.03299 -0.059 0.634 0.005 0.703 0.008 -6.384 0.302 -0.031 -5.0 -0.145 0.03065 -0.063 0.633 0.006 0.700 0.009 -4.722 0.303 -0.183 -4.5 -0.079 0.02826 -0.066 0.632 0.007 0.698 0.010 -2.800 0.437 -0.586 -4.0 -0.013 0.01269 -0.087 0.630 0.008 0.695 1.000 -1.037 0.427 -6.383 -3.5 0.047 0.01263 -0.089 0.627 0.009 0.695 1.000 3.756 0.272 2.118 -3.0 0.108 0.01251 -0.090 0.624 0.093 0.694 1.000 8.648 0.232 1.081 -2.5 0.170 0.01363 -0.086 0.621 0.726 0.693 0.832 12.500 0.240 0.757 -2.0 0.231 0.01361 -0.089 0.618 0.739 0.692 0.830 17.002 0.288 0.633 -1.5 0.292 0.01363 -0.091 0.616 0.751 0.690 0.828 21.424 0.289 0.562 -1.0 0.353 0.01368 -0.093 0.613 0.757 0.689 0.830 25.779 0.290 0.515 -0.5 0.413 0.01373 -0.096 0.611 0.763 0.687 0.833 30.059 0.174 0.482 0.0 0.289 0.01846 -0.098 0.608 0.768 0.685 0.835 15.675 0.173 0.590 0.5 0.342 0.01887 -0.101 0.606 0.773 0.683 0.836 18.134 0.308 0.546 1.0 0.395 0.01930 -0.104 0.603 0.778 0.681 0.837 20.450 0.309 0.514 1.5 0.448 0.01975 -0.107 0.601 0.781 0.679 0.840 22.674 0.309 0.490 2.0 0.500 0.02026 -0.111 0.598 0.783 0.677 0.844 24.686 0.309 0.471 2.5 0.554 0.02070 -0.114 0.593 0.785 0.678 0.848 26.776 0.308 0.455 3.0 0.608 0.02120 -0.117 0.587 0.787 0.678 0.851 28.698 0.308 0.442 3.5 0.662 0.02182 -0.120 0.582 0.789 0.678 0.856 30.344 0.309 0.431 4.0 0.715 0.02250 -0.123 0.576 0.792 0.678 0.862 31.780 0.310 0.422 4.5 0.768 0.02322 -0.126 0.571 0.794 0.677 0.868 33.060 0.311 0.415 5.0 0.820 0.02399 -0.130 0.566 0.796 0.676 0.876 34.174 0.308 0.408 5.5 0.875 0.02329 -0.133 0.554 0.798 0.679 1.000 37.575 0.306 0.402 6.0 0.929 0.02395 -0.136 0.544 0.801 0.681 1.000 38.773 0.308 0.396 6.5 0.981 0.02468 -0.139 0.532 0.803 0.683 1.000 39.747 0.250 0.391 7.0 1.132 0.02687 -0.136 0.009 0.805 0.787 1.000 42.133 0.253 0.370 7.5 1.170 0.02863 -0.139 0.008 0.807 0.774 1.000 40.868 0.346 0.369 8.0 1.208 0.03046 -0.143 0.006 0.808 0.763 1.000 39.639 0.004 0.368 8.5 1.082 0.04411 -0.161 0.005 0.810 0.013 1.000 24.524 0.003 0.399 9.0 1.120 0.04657 -0.165 0.004 0.812 0.009 1.000 24.046 0.354 0.397 9.5 1.151 0.04984 -0.168 0.003 0.813 0.008 1.000 23.101 0.372 0.396 10.0 1.180 0.05349 -0.172 0.003 0.815 0.006 1.000 22.059 0.388 0.396 10.5 1.205 0.05740 -0.176 0.002 0.817 0.005 1.000 20.986 0.411 0.396 11.0 1.226 0.06123 -0.179 0.002 0.818 0.004 1.000 20.015 0.447 0.396 11.5 1.242 0.06650 -0.183 0.002 0.820 0.004 1.000 18.677 0.493 0.397 12.0 1.256 0.07076 -0.187 0.002 0.823 0.003 1.000 17.750 0.563 0.399 12.5 1.266 0.07636 -0.190 0.001 0.824 0.003 1.000 16.574 0.740 0.400 13.0 1.271 0.08407 -0.194 0.001 0.827 0.003 1.000 15.118 1.327 0.403 13.5 1.272 0.08935 -0.198 0.001 0.829 0.003 1.000 14.241 -21.625 0.405 14.0 1.271 0.09617 -0.201 0.001 0.832 0.002 1.000 13.212 -0.647 0.409 14.5 1.264 0.10624 -0.205 0.001 0.834 0.002 1.000 11.900 -0.201 0.412 15.0 1.254 0.11204 -0.209 0.001 0.837 0.002 1.000 11.196 -0.119 0.416