Name = AG45c-03f 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 -0.293 0.42232 0.032 0.696 0.002 0.700 0.004 -0.695 0.090 0.358 -14.5 -0.305 0.41424 0.030 0.696 0.002 0.700 0.004 -0.736 0.088 0.348 -14.0 -0.317 0.36973 0.028 0.695 0.002 0.700 0.004 -0.856 0.083 0.338 -13.5 -0.328 0.33608 0.026 0.695 0.003 0.700 0.004 -0.975 0.074 0.329 -13.0 -0.338 0.30015 0.024 0.694 0.002 0.700 0.004 -1.127 0.060 0.321 -12.5 -0.348 0.26577 0.022 0.694 0.002 0.700 0.004 -1.309 0.039 0.314 -12.0 -0.357 0.25376 0.020 0.693 0.002 0.700 0.004 -1.405 0.005 0.307 -11.5 -0.364 0.23818 0.018 0.692 0.002 0.699 0.003 -1.528 -0.057 0.300 -11.0 -0.369 0.20252 0.016 0.692 0.002 0.700 0.004 -1.824 -0.195 0.294 -10.5 -0.373 0.19508 0.014 0.692 0.002 0.700 0.004 -1.912 -0.598 0.288 -10.0 -0.374 0.25354 0.012 0.690 0.002 0.700 0.003 -1.476 29.188 0.283 -9.5 -0.373 0.21965 0.010 0.688 0.002 0.699 0.003 -1.697 0.945 0.277 -9.0 -0.368 0.19404 0.008 0.687 0.002 0.699 0.003 -1.898 0.583 0.272 -8.5 -0.360 0.13624 0.006 0.685 0.002 0.699 0.003 -2.646 0.471 0.267 -8.0 -0.350 0.15093 0.004 0.683 0.002 0.699 0.003 -2.317 0.415 0.261 -7.5 -0.335 0.13884 0.002 0.681 0.002 0.699 0.003 -2.414 0.382 0.256 -7.0 -0.318 0.11772 -0.000 0.680 0.002 0.699 0.003 -2.699 0.361 0.249 -6.5 -0.297 0.10338 -0.002 0.678 0.002 0.699 0.003 -2.872 0.345 0.242 -6.0 -0.273 0.08717 -0.004 0.674 0.002 0.699 0.003 -3.133 0.335 0.234 -5.5 -0.247 0.07622 -0.007 0.670 0.002 0.698 0.003 -3.235 0.327 0.223 -5.0 -0.217 0.06650 -0.009 0.666 0.002 0.697 0.003 -3.264 0.321 0.210 -4.5 -0.185 0.05634 -0.011 0.660 0.003 0.697 0.003 -3.286 0.318 0.191 -4.0 -0.152 0.05026 -0.013 0.653 0.002 0.696 0.003 -3.031 0.316 0.164 -3.5 -0.118 0.04334 -0.015 0.645 0.002 0.696 0.003 -2.726 0.313 0.120 -3.0 -0.082 0.03680 -0.018 0.635 0.002 0.696 0.003 -2.235 0.312 0.036 -2.5 -0.046 0.03196 -0.020 0.624 0.003 0.696 0.003 -1.433 0.311 -0.183 -2.0 -0.009 0.02864 -0.022 0.610 0.003 0.696 0.003 -0.302 0.125 -2.301 -1.5 -0.082 0.02533 -0.024 0.593 0.003 0.696 0.005 -3.238 -0.072 -0.047 -1.0 -0.023 0.02294 -0.027 0.570 0.004 0.697 0.006 -0.991 0.307 -0.921 -0.5 0.036 0.02327 -0.031 0.544 0.995 0.698 0.995 1.527 0.312 1.124 0.0 0.052 0.02461 -0.031 0.511 0.995 0.699 0.995 2.104 0.277 0.853 0.5 0.104 0.02511 -0.033 0.473 0.995 0.699 0.995 4.132 0.283 0.567 1.0 0.156 0.02574 -0.035 0.435 0.995 0.700 0.995 6.052 0.283 0.472 1.5 0.207 0.02594 -0.036 0.414 0.995 0.699 0.995 7.998 0.284 0.425 2.0 0.259 0.02612 -0.038 0.396 0.995 0.699 0.995 9.918 0.284 0.397 2.5 0.311 0.02624 -0.040 0.368 0.995 0.698 0.995 11.837 0.285 0.379 3.0 0.362 0.02664 -0.042 0.336 0.995 0.698 0.995 13.590 0.285 0.365 3.5 0.413 0.02705 -0.044 0.304 0.995 0.697 0.995 15.277 0.286 0.355 4.0 0.464 0.02756 -0.045 0.272 0.995 0.695 0.995 16.835 0.287 0.348 4.5 0.515 0.02859 -0.047 0.235 0.995 0.694 0.995 18.003 0.287 0.342 5.0 0.565 0.02964 -0.049 0.194 0.995 0.692 0.995 19.063 0.290 0.337 5.5 0.614 0.03078 -0.051 0.149 0.995 0.688 0.996 19.941 0.295 0.333 6.0 0.660 0.03209 -0.053 0.105 0.995 0.679 0.996 20.563 0.327 0.331 6.5 0.691 0.03433 -0.057 0.072 0.995 0.642 0.996 20.131 1.860 0.333 7.0 0.667 0.04055 -0.065 0.048 0.995 0.491 0.996 16.452 0.095 0.347 7.5 0.604 0.05398 -0.071 0.025 0.995 0.145 0.996 11.195 0.850 0.367 8.0 0.676 0.05370 -0.070 0.006 0.996 0.016 0.996 12.585 0.266 0.354 8.5 0.721 0.05585 -0.072 0.003 0.996 0.006 0.996 12.903 0.310 0.350 9.0 0.753 0.06153 -0.075 0.002 0.996 0.004 0.996 12.237 0.331 0.349 9.5 0.781 0.06795 -0.077 0.001 0.996 0.003 0.996 11.494 0.345 0.349 10.0 0.805 0.07543 -0.080 0.001 0.996 0.002 0.996 10.672 0.368 0.349 10.5 0.823 0.08542 -0.082 0.001 0.996 0.002 0.996 9.639 0.406 0.350 11.0 0.837 0.09289 -0.085 0.001 0.996 0.001 0.996 9.015 0.466 0.351 11.5 0.847 0.10578 -0.087 0.001 0.996 0.001 0.996 8.005 0.625 0.353 12.0 0.851 0.11858 -0.090 0.001 0.996 0.001 0.996 7.176 1.788 0.356 12.5 0.850 0.13534 -0.092 0.001 0.996 0.001 0.996 6.282 -0.620 0.359 13.0 0.845 0.15081 -0.095 0.001 0.996 0.001 0.996 5.604 -0.095 0.362 13.5 0.835 0.17265 -0.098 0.001 0.996 0.001 0.996 4.838 0.032 0.367 14.0 0.821 0.18698 -0.100 0.001 0.996 0.001 0.996 4.393 0.086 0.372 14.5 0.804 0.21254 -0.103 0.001 0.996 0.001 0.996 3.782 0.116 0.378 15.0 0.783 0.22285 -0.105 0.001 0.996 0.001 0.996 3.512 0.127 0.385 Name = AG45c-03f 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 -0.293 0.33344 0.032 0.696 0.002 0.700 0.005 -0.879 0.089 0.358 -14.5 -0.305 0.30476 0.030 0.696 0.002 0.700 0.004 -1.001 0.088 0.348 -14.0 -0.316 0.27768 0.028 0.695 0.002 0.700 0.004 -1.140 0.083 0.338 -13.5 -0.328 0.25518 0.026 0.695 0.003 0.700 0.004 -1.284 0.074 0.329 -13.0 -0.338 0.22582 0.024 0.694 0.002 0.700 0.004 -1.497 0.060 0.321 -12.5 -0.348 0.20391 0.022 0.694 0.002 0.700 0.004 -1.706 0.039 0.314 -12.0 -0.356 0.19583 0.020 0.693 0.002 0.700 0.004 -1.820 0.005 0.307 -11.5 -0.364 0.18563 0.018 0.692 0.002 0.700 0.004 -1.960 -0.058 0.300 -11.0 -0.369 0.15810 0.016 0.692 0.002 0.700 0.004 -2.336 -0.196 0.294 -10.5 -0.373 0.15341 0.014 0.692 0.002 0.700 0.004 -2.430 -0.602 0.288 -10.0 -0.374 0.13756 0.012 0.690 0.002 0.700 0.004 -2.719 25.086 0.283 -9.5 -0.373 0.12703 0.010 0.688 0.002 0.699 0.003 -2.933 0.943 0.277 -9.0 -0.368 0.11553 0.008 0.687 0.002 0.699 0.003 -3.186 0.588 0.272 -8.5 -0.360 0.10223 0.006 0.685 0.002 0.699 0.003 -3.526 0.471 0.267 -8.0 -0.349 0.09405 0.004 0.683 0.002 0.699 0.003 -3.715 0.415 0.262 -7.5 -0.335 0.10286 0.002 0.681 0.002 0.699 0.003 -3.259 0.382 0.256 -7.0 -0.318 0.09289 -0.000 0.680 0.002 0.699 0.003 -3.420 0.361 0.249 -6.5 -0.297 0.07914 -0.002 0.678 0.002 0.699 0.003 -3.752 0.345 0.242 -6.0 -0.273 0.07023 -0.004 0.674 0.002 0.699 0.003 -3.887 0.335 0.234 -5.5 -0.246 0.06225 -0.007 0.670 0.002 0.699 0.003 -3.958 0.327 0.223 -5.0 -0.217 0.05480 -0.009 0.666 0.002 0.699 0.003 -3.958 0.321 0.210 -4.5 -0.185 0.04562 -0.011 0.660 0.003 0.699 0.003 -4.058 0.318 0.191 -4.0 -0.152 0.04093 -0.013 0.653 0.002 0.699 0.003 -3.722 0.316 0.164 -3.5 -0.118 0.03571 -0.015 0.645 0.002 0.699 0.003 -3.308 0.313 0.120 -3.0 -0.082 0.03066 -0.018 0.635 0.002 0.699 0.003 -2.683 0.312 0.036 -2.5 -0.046 0.02735 -0.020 0.624 0.003 0.699 0.003 -1.669 0.311 -0.184 -2.0 -0.009 0.02416 -0.022 0.610 0.003 0.699 0.003 -0.358 0.126 -2.301 -1.5 -0.082 0.02170 -0.024 0.593 0.003 0.699 0.005 -3.779 -0.072 -0.047 -1.0 -0.023 0.01960 -0.027 0.570 0.004 0.700 0.007 -1.160 0.307 -0.921 -0.5 0.036 0.01780 -0.031 0.544 0.995 0.701 0.995 1.997 0.312 1.124 0.0 0.052 0.01906 -0.031 0.511 0.995 0.701 0.995 2.745 0.252 0.847 0.5 0.152 0.02529 -0.031 0.473 0.995 1.000 0.995 5.996 0.252 0.457 1.0 0.210 0.02604 -0.032 0.435 0.995 1.000 0.995 8.051 0.253 0.400 1.5 0.268 0.02625 -0.032 0.414 0.995 1.000 0.995 10.194 0.253 0.368 2.0 0.326 0.02649 -0.032 0.396 0.995 1.000 0.995 12.291 0.253 0.348 2.5 0.383 0.02682 -0.032 0.368 0.995 1.000 0.995 14.299 0.253 0.334 3.0 0.441 0.02725 -0.032 0.336 0.995 1.000 0.995 16.193 0.254 0.323 3.5 0.499 0.02757 -0.032 0.304 0.995 1.000 0.995 18.100 0.254 0.315 4.0 0.557 0.02783 -0.033 0.272 0.995 1.000 0.995 20.004 0.254 0.309 4.5 0.614 0.02841 -0.033 0.235 0.995 1.000 0.995 21.615 1.526 0.304 5.0 0.569 0.02514 -0.049 0.194 0.995 0.702 0.995 22.646 3.213 0.336 5.5 0.620 0.02568 -0.051 0.149 0.995 0.702 0.996 24.145 0.286 0.332 6.0 0.670 0.02627 -0.052 0.105 0.995 0.701 0.996 25.519 0.288 0.328 6.5 0.719 0.02661 -0.054 0.072 0.995 0.700 0.996 27.026 0.289 0.326 7.0 0.767 0.02754 -0.056 0.048 0.995 0.699 0.996 27.861 0.296 0.323 7.5 0.811 0.02896 -0.059 0.025 0.995 0.692 0.996 27.991 0.457 0.322 8.0 0.810 0.03265 -0.065 0.006 0.996 0.607 0.996 24.813 0.101 0.330 8.5 0.717 0.04868 -0.072 0.003 0.996 0.008 0.996 14.728 0.084 0.351 9.0 0.752 0.05234 -0.075 0.002 0.996 0.004 0.996 14.362 0.326 0.350 9.5 0.780 0.05715 -0.077 0.001 0.996 0.003 0.996 13.657 0.344 0.349 10.0 0.805 0.06341 -0.080 0.001 0.996 0.002 0.996 12.688 0.368 0.349 10.5 0.823 0.07125 -0.082 0.001 0.996 0.002 0.996 11.549 0.406 0.350 11.0 0.837 0.07751 -0.085 0.001 0.996 0.001 0.996 10.797 0.461 0.351 11.5 0.847 0.08480 -0.087 0.001 0.996 0.001 0.996 9.987 0.625 0.353 12.0 0.850 0.09906 -0.090 0.001 0.996 0.001 0.996 8.585 1.788 0.356 12.5 0.850 0.10501 -0.092 0.001 0.996 0.001 0.996 8.096 -0.630 0.359 13.0 0.845 0.12095 -0.095 0.001 0.996 0.001 0.996 6.983 -0.086 0.363 13.5 0.835 0.13530 -0.098 0.001 0.996 0.001 0.996 6.171 0.029 0.367 14.0 0.821 0.14168 -0.100 0.001 0.996 0.001 0.996 5.798 0.086 0.372 14.5 0.803 0.15914 -0.103 0.001 0.996 0.001 0.996 5.049 0.117 0.378 15.0 0.782 0.17688 -0.105 0.001 0.996 0.001 0.996 4.423 0.127 0.385 Name = AG45c-03f 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 -0.293 0.27719 0.032 0.696 0.002 0.700 0.005 -1.058 0.089 0.358 -14.5 -0.305 0.25719 0.030 0.696 0.002 0.700 0.005 -1.185 0.087 0.348 -14.0 -0.316 0.23770 0.028 0.695 0.002 0.700 0.004 -1.331 0.082 0.338 -13.5 -0.328 0.20536 0.026 0.695 0.003 0.700 0.004 -1.595 0.074 0.329 -13.0 -0.338 0.19396 0.024 0.694 0.002 0.700 0.005 -1.743 0.060 0.321 -12.5 -0.348 0.17741 0.022 0.694 0.002 0.700 0.004 -1.960 0.038 0.314 -12.0 -0.356 0.17140 0.020 0.693 0.002 0.700 0.004 -2.079 0.004 0.307 -11.5 -0.364 0.16350 0.018 0.692 0.002 0.700 0.004 -2.225 -0.059 0.300 -11.0 -0.369 0.13938 0.016 0.692 0.002 0.700 0.004 -2.649 -0.192 0.294 -10.5 -0.373 0.12650 0.014 0.692 0.002 0.700 0.004 -2.947 -0.584 0.288 -10.0 -0.374 0.11518 0.012 0.690 0.002 0.700 0.004 -3.247 25.086 0.283 -9.5 -0.373 0.10752 0.010 0.688 0.002 0.699 0.003 -3.466 0.943 0.277 -9.0 -0.368 0.09821 0.008 0.687 0.002 0.699 0.003 -3.748 0.583 0.272 -8.5 -0.360 0.09360 0.006 0.685 0.002 0.699 0.004 -3.849 0.471 0.267 -8.0 -0.349 0.08071 0.004 0.683 0.002 0.699 0.003 -4.330 0.415 0.262 -7.5 -0.335 0.07510 0.002 0.681 0.002 0.699 0.004 -4.461 0.382 0.256 -7.0 -0.318 0.07945 -0.000 0.680 0.002 0.699 0.003 -3.998 0.361 0.249 -6.5 -0.297 0.07075 -0.002 0.678 0.002 0.699 0.003 -4.195 0.345 0.242 -6.0 -0.273 0.06316 -0.004 0.674 0.002 0.699 0.003 -4.320 0.335 0.234 -5.5 -0.246 0.05471 -0.007 0.670 0.002 0.699 0.003 -4.503 0.327 0.223 -5.0 -0.217 0.04843 -0.009 0.666 0.002 0.699 0.003 -4.478 0.321 0.210 -4.5 -0.185 0.04188 -0.011 0.660 0.003 0.699 0.003 -4.417 0.318 0.191 -4.0 -0.152 0.03676 -0.013 0.653 0.002 0.699 0.003 -4.145 0.316 0.164 -3.5 -0.118 0.03240 -0.015 0.645 0.002 0.699 0.003 -3.646 0.313 0.120 -3.0 -0.082 0.02798 -0.018 0.635 0.002 0.699 0.003 -2.940 0.312 0.036 -2.5 -0.046 0.02499 -0.020 0.624 0.003 0.700 0.003 -1.827 0.311 -0.184 -2.0 -0.008 0.02236 -0.022 0.610 0.003 0.700 0.004 -0.373 0.126 -2.395 -1.5 -0.082 0.01995 -0.024 0.593 0.003 0.701 0.005 -4.109 -0.065 -0.047 -1.0 -0.023 0.01829 -0.027 0.570 0.004 0.701 0.007 -1.243 0.307 -0.921 -0.5 0.036 0.01517 -0.031 0.544 0.995 0.702 0.995 2.343 0.290 1.124 0.0 0.094 0.02195 -0.031 0.511 0.995 1.000 0.995 4.262 0.252 0.584 0.5 0.152 0.02256 -0.031 0.473 0.995 1.000 0.995 6.723 0.252 0.457 1.0 0.210 0.02331 -0.032 0.435 0.995 1.000 0.995 8.992 0.253 0.400 1.5 0.268 0.02351 -0.032 0.414 0.995 1.000 0.995 11.384 0.253 0.368 2.0 0.326 0.02398 -0.032 0.396 0.995 1.000 0.995 13.574 0.253 0.348 2.5 0.383 0.02428 -0.032 0.368 0.995 1.000 0.995 15.792 0.253 0.334 3.0 0.441 0.02482 -0.032 0.336 0.995 1.000 0.995 17.778 0.254 0.323 3.5 0.499 0.02545 -0.032 0.304 0.995 1.000 0.995 19.609 0.254 0.315 4.0 0.557 0.02613 -0.033 0.272 0.995 1.000 0.995 21.301 0.254 0.309 4.5 0.614 0.02678 -0.033 0.235 0.995 1.000 0.995 22.933 0.254 0.304 5.0 0.671 0.02702 -0.033 0.194 0.995 1.000 0.995 24.853 0.254 0.299 5.5 0.728 0.02778 -0.033 0.149 0.995 1.000 0.996 26.220 0.255 0.296 6.0 0.785 0.02835 -0.034 0.105 0.995 1.000 0.996 27.680 -2.312 0.293 6.5 0.720 0.02507 -0.054 0.072 0.995 0.702 0.996 28.726 -1.109 0.325 7.0 0.768 0.02536 -0.056 0.048 0.995 0.701 0.996 30.294 0.290 0.323 7.5 0.815 0.02570 -0.058 0.025 0.995 0.700 0.996 31.703 0.295 0.321 8.0 0.858 0.02714 -0.060 0.006 0.996 0.696 0.996 31.606 0.115 0.320 8.5 0.706 0.04656 -0.073 0.003 0.996 0.016 0.996 15.172 0.114 0.353 9.0 0.750 0.04864 -0.075 0.002 0.996 0.005 0.996 15.410 0.313 0.350 9.5 0.780 0.05312 -0.077 0.001 0.996 0.003 0.996 14.675 0.340 0.349 10.0 0.804 0.05816 -0.080 0.001 0.996 0.002 0.996 13.826 0.365 0.349 10.5 0.823 0.06335 -0.082 0.001 0.996 0.002 0.996 12.989 0.406 0.350 11.0 0.836 0.07104 -0.085 0.001 0.996 0.002 0.996 11.773 0.465 0.351 11.5 0.846 0.07847 -0.087 0.001 0.996 0.001 0.996 10.786 0.611 0.353 12.0 0.850 0.08618 -0.090 0.001 0.996 0.001 0.996 9.868 1.788 0.356 12.5 0.850 0.09740 -0.092 0.001 0.996 0.001 0.996 8.723 -0.630 0.359 13.0 0.845 0.10415 -0.095 0.001 0.996 0.001 0.996 8.109 -0.096 0.363 13.5 0.835 0.11561 -0.098 0.001 0.996 0.001 0.996 7.222 0.032 0.367 14.0 0.821 0.12898 -0.100 0.001 0.996 0.001 0.996 6.366 0.086 0.372 14.5 0.803 0.13506 -0.103 0.001 0.996 0.001 0.996 5.949 0.116 0.378 15.0 0.782 0.14802 -0.105 0.001 0.996 0.001 0.996 5.286 0.127 0.385 Name = AG45c-03f 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 -0.293 0.26018 0.032 0.696 0.002 0.700 0.005 -1.127 0.088 0.358 -14.5 -0.305 0.22871 0.030 0.696 0.002 0.700 0.005 -1.333 0.087 0.348 -14.0 -0.316 0.21381 0.028 0.695 0.002 0.700 0.005 -1.480 0.082 0.338 -13.5 -0.327 0.18719 0.026 0.695 0.003 0.700 0.005 -1.749 0.074 0.329 -13.0 -0.338 0.17508 0.024 0.694 0.002 0.700 0.005 -1.930 0.060 0.321 -12.5 -0.348 0.16188 0.022 0.694 0.002 0.700 0.005 -2.148 0.038 0.314 -12.0 -0.356 0.14710 0.020 0.693 0.002 0.700 0.004 -2.423 0.005 0.307 -11.5 -0.364 0.14127 0.018 0.692 0.002 0.700 0.004 -2.575 -0.060 0.300 -11.0 -0.369 0.12873 0.016 0.692 0.002 0.700 0.004 -2.867 -0.197 0.294 -10.5 -0.373 0.11792 0.014 0.692 0.002 0.700 0.004 -3.160 -0.588 0.288 -10.0 -0.374 0.10822 0.012 0.690 0.002 0.700 0.004 -3.455 22.004 0.283 -9.5 -0.372 0.10179 0.010 0.688 0.002 0.700 0.004 -3.659 0.940 0.277 -9.0 -0.368 0.09328 0.008 0.687 0.002 0.699 0.004 -3.945 0.588 0.272 -8.5 -0.360 0.08339 0.006 0.685 0.002 0.699 0.004 -4.321 0.471 0.267 -8.0 -0.349 0.07694 0.004 0.683 0.002 0.699 0.004 -4.540 0.415 0.262 -7.5 -0.335 0.06772 0.002 0.681 0.002 0.699 0.004 -4.947 0.382 0.256 -7.0 -0.317 0.06282 -0.000 0.680 0.002 0.699 0.003 -5.054 0.360 0.249 -6.5 -0.297 0.05737 -0.002 0.678 0.002 0.699 0.003 -5.169 0.346 0.242 -6.0 -0.273 0.05742 -0.004 0.674 0.002 0.699 0.003 -4.752 0.335 0.234 -5.5 -0.246 0.05160 -0.007 0.670 0.002 0.699 0.003 -4.772 0.327 0.223 -5.0 -0.217 0.04468 -0.009 0.666 0.002 0.699 0.003 -4.854 0.321 0.210 -4.5 -0.185 0.03887 -0.011 0.660 0.003 0.699 0.003 -4.760 0.318 0.191 -4.0 -0.152 0.03502 -0.013 0.653 0.002 0.699 0.003 -4.345 0.316 0.164 -3.5 -0.118 0.03093 -0.015 0.645 0.002 0.700 0.003 -3.813 0.313 0.120 -3.0 -0.082 0.02672 -0.018 0.635 0.002 0.700 0.003 -3.072 0.312 0.036 -2.5 -0.046 0.02351 -0.020 0.624 0.003 0.700 0.003 -1.942 0.311 -0.184 -2.0 -0.008 0.02113 -0.022 0.610 0.003 0.701 0.004 -0.395 0.126 -2.395 -1.5 -0.082 0.01900 -0.024 0.593 0.003 0.701 0.005 -4.316 -0.065 -0.047 -1.0 -0.023 0.01733 -0.027 0.570 0.004 0.702 0.008 -1.312 0.307 -0.920 -0.5 0.036 0.02015 -0.031 0.544 0.995 1.000 0.995 1.764 0.290 1.124 0.0 0.094 0.02052 -0.031 0.511 0.995 1.000 0.995 4.561 0.252 0.584 0.5 0.152 0.02114 -0.031 0.473 0.995 1.000 0.995 7.175 0.252 0.457 1.0 0.210 0.02194 -0.032 0.435 0.995 1.000 0.995 9.557 0.253 0.400 1.5 0.268 0.02218 -0.032 0.414 0.995 1.000 0.995 12.067 0.253 0.368 2.0 0.326 0.02238 -0.032 0.396 0.995 1.000 0.995 14.547 0.253 0.348 2.5 0.383 0.02302 -0.032 0.368 0.995 1.000 0.995 16.657 0.253 0.334 3.0 0.441 0.02364 -0.032 0.336 0.995 1.000 0.995 18.667 0.254 0.323 3.5 0.499 0.02423 -0.032 0.304 0.995 1.000 0.995 20.595 0.254 0.315 4.0 0.557 0.02453 -0.033 0.272 0.995 1.000 0.995 22.693 0.254 0.309 4.5 0.614 0.02520 -0.033 0.235 0.995 1.000 0.995 24.368 0.254 0.304 5.0 0.671 0.02589 -0.033 0.194 0.995 1.000 0.995 25.930 0.254 0.299 5.5 0.728 0.02667 -0.033 0.149 0.995 1.000 0.996 27.308 0.255 0.296 6.0 0.785 0.02689 -0.034 0.105 0.995 1.000 0.996 29.188 0.255 0.293 6.5 0.840 0.02719 -0.034 0.072 0.995 1.000 0.996 30.901 -1.152 0.290 7.0 0.769 0.02433 -0.056 0.048 0.995 0.702 0.996 31.602 -0.722 0.323 7.5 0.815 0.02472 -0.058 0.025 0.995 0.701 0.996 32.980 0.293 0.321 8.0 0.860 0.02517 -0.060 0.006 0.996 0.700 0.996 34.148 0.307 0.320 8.5 0.896 0.02682 -0.063 0.003 0.996 0.688 0.996 33.399 0.117 0.320 9.0 0.747 0.04661 -0.075 0.002 0.996 0.006 0.996 16.029 0.124 0.350 9.5 0.779 0.05013 -0.077 0.001 0.996 0.003 0.996 15.540 0.336 0.349 10.0 0.804 0.05487 -0.080 0.001 0.996 0.002 0.996 14.647 0.365 0.349 10.5 0.822 0.06009 -0.082 0.001 0.996 0.002 0.996 13.687 0.404 0.350 11.0 0.836 0.06527 -0.085 0.001 0.996 0.002 0.996 12.814 0.461 0.351 11.5 0.846 0.07230 -0.087 0.001 0.996 0.001 0.996 11.706 0.611 0.353 12.0 0.850 0.07870 -0.090 0.001 0.996 0.001 0.996 10.806 1.788 0.356 12.5 0.850 0.08820 -0.092 0.001 0.996 0.001 0.996 9.634 -0.571 0.359 13.0 0.844 0.09948 -0.095 0.001 0.996 0.001 0.996 8.486 -0.096 0.363 13.5 0.835 0.10415 -0.098 0.001 0.996 0.001 0.996 8.016 0.028 0.367 14.0 0.821 0.11550 -0.100 0.001 0.996 0.001 0.996 7.108 0.087 0.372 14.5 0.803 0.12718 -0.103 0.001 0.996 0.001 0.996 6.315 0.117 0.378 15.0 0.782 0.13820 -0.105 0.001 0.996 0.001 0.996 5.659 0.127 0.385