Name = AH 79-K-132/20 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 -0.442 0.30196 0.006 0.700 0.002 0.732 0.003 -1.464 1.535 0.264 -14.5 -0.440 0.28596 0.003 0.699 0.002 0.730 0.003 -1.537 1.081 0.258 -14.0 -0.435 0.24753 0.000 0.698 0.002 0.728 0.003 -1.757 0.733 0.251 -13.5 -0.427 0.22104 -0.003 0.697 0.002 0.726 0.003 -1.934 0.582 0.244 -13.0 -0.417 0.21448 -0.006 0.696 0.002 0.724 0.003 -1.944 0.498 0.237 -12.5 -0.403 0.19269 -0.009 0.695 0.002 0.722 0.003 -2.092 0.445 0.229 -12.0 -0.386 0.16166 -0.012 0.694 0.002 0.721 0.003 -2.386 0.412 0.220 -11.5 -0.366 0.15160 -0.015 0.693 0.002 0.719 0.003 -2.411 0.393 0.210 -11.0 -0.343 0.13329 -0.018 0.692 0.002 0.718 0.003 -2.571 0.378 0.198 -10.5 -0.317 0.12395 -0.021 0.692 0.002 0.717 0.003 -2.559 0.368 0.184 -10.0 -0.290 0.11298 -0.024 0.689 0.002 0.716 0.003 -2.566 0.360 0.167 -9.5 -0.260 0.09656 -0.027 0.687 0.002 0.715 0.003 -2.693 0.352 0.145 -9.0 -0.228 0.08885 -0.030 0.684 0.003 0.714 0.004 -2.569 0.348 0.117 -8.5 -0.195 0.07865 -0.034 0.682 0.003 0.713 0.004 -2.480 0.343 0.078 -8.0 -0.160 0.07141 -0.037 0.680 0.003 0.712 0.004 -2.240 0.339 0.020 -7.5 -0.123 0.06497 -0.040 0.677 0.003 0.711 0.005 -1.898 0.336 -0.074 -7.0 -0.086 0.05954 -0.043 0.675 0.004 0.709 0.006 -1.437 0.335 -0.254 -6.5 -0.047 0.05448 -0.046 0.673 0.004 0.708 0.006 -0.864 0.334 -0.736 -6.0 -0.008 0.04924 -0.050 0.671 0.005 0.707 0.007 -0.159 0.214 -6.110 -5.5 -0.229 0.04505 -0.053 0.669 0.006 0.706 0.007 -5.074 0.208 0.018 -5.0 -0.163 0.04138 -0.056 0.667 0.006 0.705 0.008 -3.943 0.301 -0.095 -4.5 -0.098 0.03828 -0.060 0.665 0.007 0.703 0.009 -2.559 0.300 -0.358 -4.0 -0.033 0.03611 -0.063 0.664 0.008 0.702 0.021 -0.920 0.300 -1.639 -3.5 0.031 0.03501 -0.066 0.662 0.024 0.701 0.034 0.878 0.301 2.397 -3.0 0.094 0.03307 -0.069 0.659 0.029 0.700 0.049 2.835 0.303 0.988 -2.5 0.156 0.03118 -0.073 0.656 0.035 0.699 0.062 4.998 0.377 0.716 -2.0 0.211 0.02460 -0.084 0.652 0.055 0.698 0.951 8.561 0.371 0.649 -1.5 0.271 0.02572 -0.087 0.649 0.059 0.697 0.999 10.523 0.281 0.570 -1.0 0.331 0.02615 -0.088 0.645 0.062 0.696 0.999 12.658 0.263 0.515 -0.5 0.392 0.02535 -0.088 0.642 0.769 0.694 0.840 15.455 0.189 0.475 0.0 0.290 0.02940 -0.090 0.639 0.774 0.693 0.843 9.870 0.146 0.561 0.5 0.343 0.02989 -0.093 0.635 0.808 0.691 0.835 11.478 0.305 0.521 1.0 0.395 0.03048 -0.096 0.632 0.810 0.688 0.838 12.960 0.305 0.493 1.5 0.448 0.03105 -0.099 0.623 0.811 0.688 0.841 14.443 0.303 0.471 2.0 0.504 0.03162 -0.102 0.606 0.813 0.691 0.843 15.942 0.302 0.452 2.5 0.559 0.03225 -0.105 0.588 0.814 0.692 0.846 17.327 0.303 0.437 3.0 0.613 0.03298 -0.108 0.570 0.816 0.693 0.849 18.588 0.303 0.425 3.5 0.667 0.03376 -0.110 0.550 0.817 0.694 0.852 19.765 0.303 0.416 4.0 0.722 0.03457 -0.113 0.527 0.818 0.696 0.854 20.878 0.302 0.407 4.5 0.777 0.03547 -0.116 0.497 0.820 0.698 0.856 21.909 0.303 0.399 5.0 0.830 0.03654 -0.119 0.475 0.821 0.698 0.858 22.725 0.305 0.393 5.5 0.883 0.03768 -0.122 0.448 0.822 0.699 0.860 23.426 0.305 0.388 6.0 0.934 0.03890 -0.125 0.416 0.823 0.700 0.862 24.017 0.272 0.384 6.5 1.028 0.03674 -0.125 0.003 0.825 0.748 0.863 27.993 0.658 0.372 7.0 0.970 0.04161 -0.139 0.002 0.826 0.004 0.865 23.306 -0.511 0.394 7.5 1.005 0.04493 -0.143 0.001 0.827 0.003 0.867 22.374 0.354 0.392 8.0 1.037 0.04937 -0.146 0.001 0.829 0.002 0.869 21.012 0.366 0.391 8.5 1.066 0.05447 -0.150 0.001 0.830 0.001 0.871 19.568 0.381 0.391 9.0 1.091 0.06030 -0.153 0.001 0.832 0.001 0.873 18.092 0.405 0.391 9.5 1.111 0.06828 -0.157 0.000 0.833 0.001 0.875 16.277 0.439 0.391 10.0 1.128 0.07520 -0.160 0.000 0.835 0.001 0.877 15.004 0.490 0.392 10.5 1.141 0.08518 -0.164 0.000 0.837 0.001 0.878 13.393 0.607 0.394 11.0 1.148 0.09341 -0.167 0.000 0.839 0.001 0.880 12.291 0.908 0.396 11.5 1.152 0.10602 -0.171 0.001 0.842 0.001 0.881 10.862 3.218 0.399 12.0 1.151 0.12018 -0.175 0.001 0.844 0.001 0.882 9.574 -0.909 0.402 12.5 1.145 0.13422 -0.178 0.000 0.846 0.001 0.883 8.534 -0.213 0.405 13.0 1.135 0.15032 -0.182 0.001 0.849 0.001 0.885 7.553 -0.045 0.410 13.5 1.122 0.17330 -0.185 0.001 0.851 0.001 0.886 6.472 0.029 0.415 14.0 1.103 0.18916 -0.189 0.001 0.854 0.001 0.887 5.834 0.072 0.421 14.5 1.082 0.21501 -0.192 0.001 0.855 0.001 0.889 5.033 0.096 0.428 15.0 1.058 0.22486 -0.196 0.001 0.857 0.001 0.890 4.706 0.104 0.435 Name = AH 79-K-132/20 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 -0.442 0.23233 0.006 0.700 0.002 0.742 0.003 -1.901 1.529 0.264 -14.5 -0.439 0.21888 0.003 0.699 0.002 0.739 0.003 -2.008 1.078 0.258 -14.0 -0.435 0.19299 0.000 0.698 0.002 0.736 0.003 -2.252 0.732 0.251 -13.5 -0.427 0.17354 -0.003 0.697 0.002 0.734 0.003 -2.462 0.586 0.244 -13.0 -0.417 0.15702 -0.006 0.696 0.002 0.732 0.003 -2.655 0.501 0.237 -12.5 -0.403 0.14449 -0.009 0.695 0.002 0.730 0.003 -2.790 0.443 0.229 -12.0 -0.385 0.13160 -0.012 0.694 0.002 0.728 0.003 -2.929 0.412 0.220 -11.5 -0.366 0.11589 -0.015 0.693 0.002 0.726 0.003 -3.154 0.393 0.210 -11.0 -0.342 0.10776 -0.018 0.692 0.002 0.723 0.003 -3.177 0.378 0.198 -10.5 -0.317 0.09566 -0.021 0.692 0.002 0.721 0.003 -3.315 0.369 0.184 -10.0 -0.290 0.08784 -0.024 0.689 0.002 0.721 0.003 -3.301 0.359 0.167 -9.5 -0.260 0.07864 -0.027 0.687 0.002 0.720 0.004 -3.304 0.352 0.145 -9.0 -0.228 0.07224 -0.030 0.684 0.003 0.719 0.004 -3.156 0.348 0.117 -8.5 -0.195 0.06469 -0.034 0.682 0.003 0.718 0.004 -3.010 0.343 0.078 -8.0 -0.159 0.05982 -0.037 0.680 0.003 0.717 0.004 -2.666 0.339 0.020 -7.5 -0.123 0.05381 -0.040 0.677 0.003 0.716 0.005 -2.287 0.337 -0.074 -7.0 -0.085 0.04942 -0.043 0.675 0.004 0.715 0.006 -1.727 0.335 -0.256 -6.5 -0.047 0.04555 -0.046 0.673 0.004 0.714 0.006 -1.029 0.334 -0.740 -6.0 -0.008 0.04144 -0.050 0.671 0.005 0.713 0.007 -0.183 0.214 -6.288 -5.5 -0.229 0.03822 -0.053 0.669 0.006 0.712 0.008 -5.980 0.208 0.018 -5.0 -0.163 0.03507 -0.056 0.667 0.006 0.711 0.009 -4.651 0.301 -0.095 -4.5 -0.098 0.03230 -0.060 0.665 0.007 0.709 0.010 -3.032 0.298 -0.358 -4.0 -0.033 0.03090 -0.063 0.664 0.008 0.708 0.034 -1.074 0.299 -1.635 -3.5 0.031 0.02935 -0.066 0.662 0.024 0.707 0.041 1.047 0.302 2.395 -3.0 0.094 0.02744 -0.069 0.659 0.029 0.706 0.062 3.415 0.403 0.988 -2.5 0.150 0.02026 -0.084 0.656 0.035 0.705 0.999 7.391 0.389 0.811 -2.0 0.210 0.02058 -0.085 0.652 0.055 0.704 0.999 10.217 0.270 0.656 -1.5 0.271 0.02111 -0.087 0.649 0.059 0.703 0.999 12.824 0.270 0.570 -1.0 0.331 0.02144 -0.088 0.645 0.062 0.702 1.000 15.437 0.263 0.515 -0.5 0.392 0.01815 -0.088 0.642 0.769 0.701 0.852 21.587 0.181 0.475 0.0 0.295 0.02200 -0.090 0.639 0.774 0.700 0.854 13.396 0.137 0.556 0.5 0.348 0.02236 -0.093 0.635 0.808 0.698 0.840 15.559 0.304 0.518 1.0 0.401 0.02281 -0.096 0.632 0.810 0.697 0.843 17.571 0.303 0.489 1.5 0.455 0.02325 -0.099 0.623 0.811 0.698 0.846 19.584 0.301 0.467 2.0 0.512 0.02366 -0.102 0.606 0.813 0.702 0.849 21.639 0.300 0.449 2.5 0.568 0.02411 -0.104 0.588 0.814 0.705 0.853 23.573 0.300 0.434 3.0 0.624 0.02463 -0.107 0.570 0.816 0.708 0.855 25.345 0.300 0.422 3.5 0.681 0.02519 -0.110 0.550 0.817 0.711 0.857 27.021 0.299 0.412 4.0 0.737 0.02577 -0.113 0.527 0.818 0.715 0.859 28.604 0.297 0.403 4.5 0.795 0.02642 -0.115 0.497 0.820 0.720 0.861 30.084 0.298 0.395 5.0 0.850 0.02721 -0.118 0.475 0.821 0.721 0.863 31.217 0.300 0.389 5.5 0.904 0.02808 -0.121 0.448 0.822 0.723 0.866 32.195 0.300 0.384 6.0 0.958 0.02904 -0.124 0.416 0.823 0.726 0.868 32.981 0.277 0.379 6.5 1.040 0.03109 -0.124 0.003 0.825 0.760 0.870 33.435 1.650 0.370 7.0 0.969 0.03706 -0.139 0.002 0.826 0.004 0.872 26.147 -0.270 0.394 7.5 1.004 0.03988 -0.143 0.001 0.827 0.003 0.874 25.187 0.354 0.392 8.0 1.036 0.04355 -0.146 0.001 0.829 0.002 0.876 23.798 0.365 0.391 8.5 1.065 0.04733 -0.150 0.001 0.830 0.001 0.878 22.513 0.380 0.391 9.0 1.090 0.05253 -0.153 0.001 0.832 0.001 0.880 20.757 0.404 0.391 9.5 1.111 0.05808 -0.157 0.000 0.833 0.001 0.881 19.130 0.437 0.391 10.0 1.128 0.06378 -0.160 0.000 0.835 0.001 0.883 17.688 0.490 0.392 10.5 1.141 0.07154 -0.164 0.000 0.837 0.001 0.884 15.943 0.607 0.394 11.0 1.148 0.07763 -0.167 0.000 0.839 0.001 0.885 14.788 0.907 0.396 11.5 1.151 0.08702 -0.171 0.001 0.842 0.001 0.887 13.230 3.202 0.399 12.0 1.150 0.09749 -0.175 0.001 0.844 0.001 0.888 11.800 -0.874 0.402 12.5 1.145 0.11043 -0.178 0.000 0.846 0.001 0.889 10.369 -0.213 0.406 13.0 1.135 0.11914 -0.182 0.001 0.849 0.001 0.890 9.528 -0.047 0.410 13.5 1.121 0.13438 -0.185 0.001 0.851 0.001 0.892 8.345 0.030 0.415 14.0 1.103 0.15068 -0.189 0.001 0.854 0.001 0.892 7.321 0.073 0.421 14.5 1.082 0.13917 -0.192 0.001 0.855 0.001 0.894 7.773 0.095 0.428 15.0 1.058 0.17774 -0.196 0.001 0.857 0.001 0.896 5.951 0.104 0.435 Name = AH 79-K-132/20 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 -0.442 0.20270 0.006 0.700 0.002 0.751 0.003 -2.179 1.523 0.264 -14.5 -0.439 0.19041 0.003 0.699 0.002 0.749 0.003 -2.307 1.076 0.258 -14.0 -0.434 0.17006 0.000 0.698 0.002 0.746 0.003 -2.555 0.731 0.251 -13.5 -0.427 0.15364 -0.003 0.697 0.002 0.742 0.003 -2.779 0.585 0.244 -13.0 -0.417 0.13972 -0.006 0.696 0.002 0.740 0.003 -2.982 0.503 0.237 -12.5 -0.403 0.12352 -0.009 0.695 0.002 0.737 0.003 -3.264 0.445 0.229 -12.0 -0.385 0.11300 -0.012 0.694 0.002 0.735 0.003 -3.411 0.411 0.220 -11.5 -0.365 0.10534 -0.015 0.693 0.002 0.732 0.003 -3.468 0.392 0.210 -11.0 -0.342 0.09719 -0.018 0.692 0.002 0.730 0.003 -3.520 0.378 0.198 -10.5 -0.317 0.08673 -0.021 0.692 0.002 0.727 0.003 -3.653 0.369 0.184 -10.0 -0.290 0.07964 -0.024 0.689 0.002 0.727 0.003 -3.637 0.359 0.167 -9.5 -0.259 0.07095 -0.027 0.687 0.002 0.726 0.004 -3.658 0.352 0.145 -9.0 -0.228 0.06507 -0.030 0.684 0.003 0.725 0.004 -3.499 0.348 0.117 -8.5 -0.194 0.05862 -0.034 0.682 0.003 0.724 0.004 -3.317 0.343 0.078 -8.0 -0.159 0.05401 -0.037 0.680 0.003 0.723 0.005 -2.949 0.340 0.020 -7.5 -0.123 0.04896 -0.040 0.677 0.003 0.722 0.005 -2.510 0.337 -0.075 -7.0 -0.085 0.04504 -0.043 0.675 0.004 0.721 0.006 -1.891 0.335 -0.257 -6.5 -0.047 0.04166 -0.046 0.673 0.004 0.720 0.006 -1.120 0.334 -0.745 -6.0 -0.007 0.03803 -0.050 0.671 0.005 0.718 0.007 -0.194 0.214 -6.476 -5.5 -0.229 0.03500 -0.053 0.669 0.006 0.717 0.008 -6.530 0.208 0.018 -5.0 -0.163 0.03214 -0.056 0.667 0.006 0.716 0.009 -5.076 0.299 -0.095 -4.5 -0.098 0.03041 -0.059 0.665 0.007 0.715 0.020 -3.219 0.295 -0.357 -4.0 -0.033 0.02853 -0.062 0.664 0.008 0.713 0.064 -1.161 0.299 -1.626 -3.5 0.031 0.02687 -0.066 0.662 0.024 0.712 0.059 1.142 0.419 2.390 -3.0 0.089 0.01808 -0.083 0.659 0.029 0.711 0.999 4.941 0.405 1.178 -2.5 0.150 0.01845 -0.084 0.656 0.035 0.710 0.999 8.116 0.270 0.812 -2.0 0.210 0.01892 -0.085 0.652 0.055 0.710 1.000 11.109 0.270 0.656 -1.5 0.271 0.01916 -0.087 0.649 0.059 0.709 1.000 14.125 0.270 0.570 -1.0 0.331 0.01973 -0.088 0.645 0.062 0.708 1.000 16.775 0.264 0.515 -0.5 0.392 0.01495 -0.088 0.642 0.769 0.707 0.860 26.203 0.173 0.475 0.0 0.299 0.01864 -0.090 0.639 0.774 0.706 0.862 16.016 0.127 0.552 0.5 0.352 0.01895 -0.093 0.635 0.808 0.705 0.845 18.578 0.303 0.514 1.0 0.405 0.01935 -0.096 0.632 0.810 0.703 0.848 20.935 0.302 0.487 1.5 0.460 0.01971 -0.099 0.623 0.811 0.705 0.851 23.348 0.299 0.465 2.0 0.518 0.02001 -0.101 0.606 0.813 0.711 0.854 25.901 0.297 0.446 2.5 0.576 0.02036 -0.104 0.588 0.814 0.715 0.857 28.291 0.298 0.431 3.0 0.633 0.02077 -0.107 0.570 0.816 0.719 0.859 30.474 0.297 0.419 3.5 0.691 0.02121 -0.110 0.550 0.817 0.724 0.861 32.574 0.295 0.409 4.0 0.749 0.02168 -0.112 0.527 0.818 0.730 0.864 34.569 0.294 0.400 4.5 0.809 0.02220 -0.115 0.497 0.820 0.736 0.866 36.453 0.295 0.392 5.0 0.865 0.02287 -0.117 0.475 0.821 0.738 0.868 37.810 0.298 0.386 5.5 0.920 0.02364 -0.120 0.448 0.822 0.741 0.871 38.911 0.298 0.381 6.0 0.974 0.02452 -0.123 0.416 0.823 0.744 0.873 39.718 0.278 0.376 6.5 1.052 0.02782 -0.124 0.003 0.825 0.773 0.876 37.824 -2.639 0.368 7.0 0.968 0.03509 -0.139 0.002 0.826 0.004 0.877 27.590 -0.139 0.394 7.5 1.003 0.03794 -0.143 0.001 0.827 0.003 0.879 26.437 0.353 0.392 8.0 1.036 0.04071 -0.146 0.001 0.829 0.002 0.881 25.450 0.363 0.391 8.5 1.065 0.04421 -0.150 0.001 0.830 0.001 0.883 24.090 0.380 0.391 9.0 1.090 0.04873 -0.153 0.001 0.832 0.001 0.884 22.371 0.404 0.391 9.5 1.111 0.05368 -0.157 0.000 0.833 0.001 0.886 20.697 0.437 0.391 10.0 1.128 0.05887 -0.160 0.000 0.835 0.001 0.887 19.160 0.488 0.392 10.5 1.141 0.06436 -0.164 0.000 0.837 0.001 0.889 17.723 0.607 0.394 11.0 1.148 0.07085 -0.167 0.000 0.839 0.001 0.890 16.199 0.921 0.396 11.5 1.151 0.07889 -0.171 0.001 0.842 0.001 0.892 14.592 2.951 0.399 12.0 1.150 0.08574 -0.175 0.001 0.844 0.001 0.893 13.416 -0.877 0.402 12.5 1.145 0.09810 -0.178 0.000 0.846 0.001 0.894 11.670 -0.207 0.406 13.0 1.135 0.10566 -0.182 0.001 0.849 0.001 0.895 10.741 -0.045 0.410 13.5 1.121 0.12063 -0.185 0.001 0.851 0.001 0.897 9.293 0.029 0.415 14.0 1.103 0.12745 -0.189 0.001 0.854 0.001 0.907 8.655 0.071 0.421 14.5 1.082 0.11901 -0.192 0.001 0.855 0.001 1.000 9.089 0.096 0.428 15.0 1.058 0.13068 -0.196 0.001 0.857 0.001 1.000 8.093 0.106 0.435 Name = AH 79-K-132/20 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 -0.441 0.18551 0.006 0.700 0.002 0.756 0.003 -2.379 1.633 0.264 -14.5 -0.439 0.16466 0.003 0.699 0.002 0.754 0.003 -2.668 1.098 0.258 -14.0 -0.434 0.14882 0.000 0.698 0.002 0.753 0.003 -2.919 0.722 0.251 -13.5 -0.427 0.14240 -0.003 0.697 0.002 0.751 0.003 -2.997 0.581 0.244 -13.0 -0.416 0.13004 -0.006 0.696 0.002 0.749 0.003 -3.203 0.503 0.237 -12.5 -0.403 0.11661 -0.009 0.695 0.002 0.745 0.003 -3.456 0.445 0.229 -12.0 -0.385 0.10711 -0.012 0.694 0.002 0.742 0.003 -3.597 0.412 0.220 -11.5 -0.365 0.09495 -0.015 0.693 0.002 0.739 0.003 -3.847 0.393 0.210 -11.0 -0.342 0.08723 -0.018 0.692 0.002 0.736 0.003 -3.922 0.378 0.198 -10.5 -0.317 0.07868 -0.021 0.692 0.002 0.733 0.003 -4.027 0.369 0.184 -10.0 -0.290 0.07254 -0.024 0.689 0.002 0.733 0.003 -3.993 0.358 0.167 -9.5 -0.259 0.06646 -0.027 0.687 0.002 0.732 0.004 -3.900 0.351 0.145 -9.0 -0.227 0.06087 -0.030 0.684 0.003 0.731 0.004 -3.736 0.348 0.117 -8.5 -0.194 0.05504 -0.034 0.682 0.003 0.731 0.004 -3.527 0.343 0.077 -8.0 -0.159 0.05060 -0.037 0.680 0.003 0.729 0.005 -3.144 0.339 0.019 -7.5 -0.122 0.04679 -0.040 0.677 0.003 0.728 0.006 -2.618 0.337 -0.076 -7.0 -0.085 0.04245 -0.043 0.675 0.004 0.727 0.006 -2.001 0.335 -0.258 -6.5 -0.046 0.03938 -0.046 0.673 0.004 0.726 0.007 -1.179 0.334 -0.749 -6.0 -0.007 0.03603 -0.050 0.671 0.005 0.724 0.007 -0.199 0.214 -6.676 -5.5 -0.229 0.03310 -0.053 0.669 0.006 0.723 0.008 -6.905 0.208 0.018 -5.0 -0.163 0.03057 -0.056 0.667 0.006 0.721 0.009 -5.336 0.298 -0.095 -4.5 -0.098 0.02914 -0.059 0.665 0.007 0.720 0.028 -3.357 0.433 -0.356 -4.0 -0.031 0.01658 -0.080 0.664 0.008 0.718 0.999 -1.851 0.427 -2.373 -3.5 0.029 0.01678 -0.082 0.662 0.024 0.717 0.999 1.729 0.270 3.065 -3.0 0.089 0.01716 -0.083 0.659 0.029 0.716 0.999 5.205 0.270 1.178 -2.5 0.150 0.01751 -0.084 0.656 0.035 0.716 1.000 8.549 0.270 0.812 -2.0 0.210 0.01792 -0.085 0.652 0.055 0.715 1.000 11.731 0.270 0.656 -1.5 0.271 0.01814 -0.087 0.649 0.059 0.715 1.000 14.924 0.270 0.570 -1.0 0.331 0.01841 -0.088 0.645 0.062 0.714 1.000 17.981 0.264 0.515 -0.5 0.392 0.01305 -0.088 0.642 0.769 0.713 0.866 30.011 0.163 0.475 0.0 0.302 0.01660 -0.090 0.639 0.774 0.711 0.868 18.212 0.116 0.549 0.5 0.356 0.01686 -0.093 0.635 0.808 0.710 0.849 21.094 0.303 0.512 1.0 0.409 0.01723 -0.096 0.632 0.810 0.709 0.852 23.732 0.301 0.484 1.5 0.465 0.01754 -0.099 0.623 0.811 0.711 0.855 26.494 0.298 0.462 2.0 0.524 0.01777 -0.101 0.606 0.813 0.718 0.858 29.491 0.295 0.443 2.5 0.583 0.01804 -0.104 0.588 0.814 0.725 0.861 32.338 0.295 0.428 3.0 0.642 0.01836 -0.107 0.570 0.816 0.730 0.863 34.955 0.294 0.416 3.5 0.701 0.01873 -0.109 0.550 0.817 0.736 0.865 37.432 0.293 0.406 4.0 0.760 0.01914 -0.112 0.527 0.818 0.742 0.868 39.715 0.292 0.397 4.5 0.820 0.01962 -0.114 0.497 0.820 0.749 0.870 41.805 0.294 0.389 5.0 0.876 0.02025 -0.117 0.475 0.821 0.751 0.873 43.247 0.298 0.383 5.5 0.930 0.02100 -0.120 0.448 0.822 0.752 0.876 44.312 0.299 0.378 6.0 0.984 0.02186 -0.122 0.416 0.823 0.754 0.878 45.005 0.277 0.374 6.5 1.062 0.02568 -0.123 0.003 0.825 0.783 0.880 41.343 0.284 0.366 7.0 1.103 0.02723 -0.126 0.002 0.826 0.775 0.881 40.491 -0.083 0.364 7.5 1.002 0.03663 -0.143 0.001 0.827 0.004 0.883 27.361 -0.049 0.393 8.0 1.035 0.03928 -0.146 0.001 0.829 0.002 0.885 26.354 0.363 0.391 8.5 1.064 0.04270 -0.150 0.001 0.830 0.002 0.887 24.922 0.378 0.391 9.0 1.090 0.04650 -0.153 0.001 0.832 0.001 0.889 23.440 0.402 0.391 9.5 1.111 0.05110 -0.157 0.000 0.833 0.001 0.891 21.737 0.437 0.391 10.0 1.128 0.05601 -0.160 0.000 0.835 0.001 0.892 20.133 0.488 0.392 10.5 1.140 0.06119 -0.164 0.000 0.837 0.001 0.894 18.638 0.607 0.394 11.0 1.147 0.06697 -0.168 0.000 0.839 0.001 0.895 17.135 0.907 0.396 11.5 1.151 0.07272 -0.171 0.001 0.842 0.001 0.896 15.830 2.938 0.399 12.0 1.150 0.08046 -0.175 0.001 0.844 0.001 0.909 14.294 -0.842 0.402 12.5 1.145 0.09100 -0.178 0.000 0.846 0.001 0.922 12.579 -0.208 0.406 13.0 1.135 0.09836 -0.182 0.001 0.849 0.001 1.000 11.537 -0.045 0.410 13.5 1.121 0.11076 -0.185 0.001 0.851 0.001 1.000 10.120 0.029 0.415 14.0 1.103 0.11970 -0.189 0.001 0.854 0.001 1.000 9.213 0.071 0.421 14.5 1.082 0.11159 -0.192 0.001 0.855 0.001 1.000 9.691 0.096 0.428 15.0 1.057 0.12273 -0.196 0.001 0.857 0.001 1.000 8.615 0.105 0.435