Name = AG04 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 -0.302 0.35270 0.030 1.000 0.002 1.000 0.003 -0.856 0.086 0.350 -14.5 -0.315 0.32708 0.028 1.000 0.001 1.000 0.003 -0.963 0.084 0.339 -14.0 -0.327 0.41449 0.026 1.000 0.001 1.000 0.003 -0.790 0.076 0.329 -13.5 -0.339 0.38027 0.024 1.000 0.001 1.000 0.003 -0.892 0.064 0.320 -13.0 -0.350 0.25455 0.022 1.000 0.002 1.000 0.003 -1.375 0.043 0.312 -12.5 -0.360 0.28324 0.020 1.000 0.002 1.000 0.003 -1.271 0.009 0.304 -12.0 -0.368 0.26056 0.017 1.000 0.002 1.000 0.003 -1.412 -0.055 0.297 -11.5 -0.374 0.24676 0.015 1.000 0.001 1.000 0.003 -1.516 -0.190 0.291 -11.0 -0.378 0.20777 0.013 1.000 0.001 1.000 0.003 -1.818 -0.685 0.284 -10.5 -0.379 0.18768 0.011 1.000 0.002 1.000 0.003 -2.018 3.296 0.279 -10.0 -0.376 0.17276 0.009 1.000 0.002 1.000 0.003 -2.179 0.815 0.273 -9.5 -0.371 0.14670 0.006 1.000 0.002 1.000 0.002 -2.528 0.525 0.267 -9.0 -0.360 0.13141 0.004 1.000 0.001 1.000 0.002 -2.742 0.431 0.262 -8.5 -0.346 0.11928 0.002 1.000 0.001 1.000 0.002 -2.905 0.394 0.256 -8.0 -0.329 0.10137 -0.000 1.000 0.001 1.000 0.002 -3.250 0.368 0.249 -7.5 -0.309 0.09608 -0.002 1.000 0.001 1.000 0.002 -3.213 0.352 0.242 -7.0 -0.285 0.07988 -0.005 1.000 0.002 1.000 0.002 -3.573 0.341 0.234 -6.5 -0.259 0.07244 -0.007 1.000 0.001 1.000 0.002 -3.579 0.332 0.223 -6.0 -0.230 0.06134 -0.009 1.000 0.001 1.000 0.002 -3.754 0.326 0.210 -5.5 -0.200 0.05497 -0.011 1.000 0.001 1.000 0.002 -3.635 0.322 0.193 -5.0 -0.167 0.04836 -0.014 1.000 0.001 1.000 0.002 -3.454 0.318 0.168 -4.5 -0.132 0.04279 -0.016 1.000 0.002 1.000 0.002 -3.095 0.315 0.129 -4.0 -0.097 0.03807 -0.018 1.000 0.002 1.000 0.002 -2.536 0.313 0.061 -3.5 -0.060 0.03348 -0.021 1.000 0.002 1.000 0.003 -1.786 0.311 -0.094 -3.0 -0.022 0.03071 -0.023 0.918 0.003 1.000 0.004 -0.705 0.146 -0.805 -2.5 -0.104 0.02818 -0.025 0.891 0.004 1.000 0.009 -3.673 -0.546 0.007 -2.0 -0.038 0.03563 -0.036 0.863 0.075 1.000 0.997 -1.077 0.343 -0.692 -1.5 0.016 0.02636 -0.036 0.833 0.995 1.000 0.996 0.612 0.253 2.502 -1.0 0.074 0.02656 -0.036 0.787 0.996 1.000 0.996 2.786 0.253 0.743 -0.5 0.132 0.02763 -0.037 0.712 0.995 1.000 0.996 4.774 0.253 0.528 0.0 0.190 0.02810 -0.037 0.645 0.995 1.000 0.996 6.754 0.253 0.444 0.5 0.248 0.02901 -0.037 0.592 0.995 1.000 0.996 8.535 0.253 0.399 1.0 0.305 0.02918 -0.037 0.542 0.995 1.000 0.996 10.467 0.253 0.372 1.5 0.363 0.03000 -0.037 0.487 0.995 1.000 0.996 12.106 0.253 0.353 2.0 0.421 0.03131 -0.038 0.413 0.996 1.000 0.996 13.441 0.253 0.339 2.5 0.478 0.03208 -0.038 0.329 0.995 1.000 0.996 14.913 0.253 0.329 3.0 0.536 0.03239 -0.038 0.257 0.995 1.000 0.996 16.544 0.253 0.321 3.5 0.593 0.03299 -0.038 0.193 0.996 1.000 0.996 17.979 0.253 0.314 4.0 0.650 0.03334 -0.038 0.144 0.995 1.000 0.996 19.496 0.254 0.309 4.5 0.706 0.03275 -0.038 0.102 0.995 1.000 0.996 21.565 0.254 0.304 5.0 0.761 0.03158 -0.039 0.060 0.996 1.000 0.996 24.109 0.092 0.301 5.5 0.533 0.04465 -0.066 0.019 0.996 0.229 0.996 11.941 0.085 0.373 6.0 0.599 0.04568 -0.066 0.005 0.996 0.011 0.996 13.112 0.267 0.359 6.5 0.643 0.04810 -0.068 0.001 0.996 0.003 0.996 13.373 0.310 0.355 7.0 0.675 0.05307 -0.070 0.001 0.997 0.002 0.997 12.716 0.332 0.354 7.5 0.701 0.06063 -0.072 0.001 0.997 0.001 0.997 11.565 0.348 0.353 8.0 0.724 0.06973 -0.075 0.001 0.997 0.001 0.997 10.378 0.368 0.353 8.5 0.742 0.07609 -0.077 0.001 0.997 0.001 0.997 9.748 0.402 0.354 9.0 0.755 0.08729 -0.080 0.001 0.997 0.001 0.997 8.652 0.464 0.355 9.5 0.764 0.10316 -0.082 0.000 0.997 0.001 0.997 7.408 0.624 0.357 10.0 0.768 0.10650 -0.084 0.001 0.997 0.001 0.997 7.212 1.781 0.360 10.5 0.767 0.11965 -0.087 0.001 0.997 0.001 0.997 6.413 -0.579 0.363 11.0 0.762 0.13445 -0.089 0.001 0.997 0.001 0.997 5.670 -0.076 0.367 11.5 0.753 0.15525 -0.092 0.001 0.997 0.001 0.997 4.847 0.040 0.372 12.0 0.739 0.17062 -0.094 0.001 0.997 0.001 0.997 4.333 0.092 0.377 12.5 0.722 0.19332 -0.097 0.001 0.997 0.001 0.997 3.735 0.121 0.384 13.0 0.702 0.20522 -0.099 0.001 0.997 0.001 0.997 3.420 0.138 0.391 13.5 0.679 0.23510 -0.101 0.001 0.997 0.001 0.997 2.887 0.149 0.399 14.0 0.654 0.26957 -0.104 0.001 0.997 0.001 0.997 2.427 0.155 0.409 14.5 0.628 0.28700 -0.106 0.001 0.996 0.001 0.996 2.189 0.160 0.419 15.0 0.601 0.31383 -0.109 0.001 0.997 0.002 0.997 1.914 0.162 0.431 Name = AG04 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 -0.302 0.26361 0.030 1.000 0.002 1.000 0.003 -1.145 0.086 0.350 -14.5 -0.315 0.25950 0.028 1.000 0.001 1.000 0.003 -1.213 0.084 0.339 -14.0 -0.327 0.23891 0.026 1.000 0.001 1.000 0.003 -1.370 0.076 0.329 -13.5 -0.339 0.20867 0.024 1.000 0.001 1.000 0.003 -1.625 0.064 0.320 -13.0 -0.350 0.19457 0.022 1.000 0.002 1.000 0.003 -1.799 0.043 0.312 -12.5 -0.360 0.17107 0.020 1.000 0.002 1.000 0.003 -2.103 0.009 0.304 -12.0 -0.368 0.15988 0.017 1.000 0.002 1.000 0.003 -2.301 -0.056 0.297 -11.5 -0.374 0.18731 0.015 1.000 0.001 1.000 0.003 -1.996 -0.193 0.291 -11.0 -0.378 0.16058 0.013 1.000 0.001 1.000 0.003 -2.352 -0.699 0.285 -10.5 -0.378 0.14760 0.011 1.000 0.002 1.000 0.003 -2.564 3.723 0.279 -10.0 -0.376 0.12830 0.009 1.000 0.002 1.000 0.003 -2.934 0.813 0.273 -9.5 -0.371 0.11798 0.006 1.000 0.002 1.000 0.003 -3.142 0.521 0.267 -9.0 -0.360 0.10558 0.004 1.000 0.001 1.000 0.003 -3.411 0.433 0.262 -8.5 -0.346 0.09098 0.002 1.000 0.001 1.000 0.002 -3.808 0.394 0.256 -8.0 -0.329 0.08319 -0.000 1.000 0.001 1.000 0.002 -3.957 0.368 0.249 -7.5 -0.309 0.07408 -0.002 1.000 0.001 1.000 0.002 -4.168 0.352 0.242 -7.0 -0.285 0.06687 -0.005 1.000 0.002 1.000 0.002 -4.264 0.341 0.234 -6.5 -0.259 0.05837 -0.007 1.000 0.001 1.000 0.002 -4.439 0.332 0.223 -6.0 -0.230 0.05131 -0.009 1.000 0.001 1.000 0.002 -4.485 0.326 0.210 -5.5 -0.200 0.04517 -0.011 1.000 0.001 1.000 0.002 -4.419 0.322 0.193 -5.0 -0.167 0.04039 -0.014 1.000 0.001 1.000 0.002 -4.131 0.318 0.168 -4.5 -0.132 0.03529 -0.016 1.000 0.002 1.000 0.002 -3.753 0.315 0.129 -4.0 -0.097 0.03148 -0.018 1.000 0.002 1.000 0.002 -3.067 0.313 0.061 -3.5 -0.060 0.02781 -0.021 1.000 0.002 1.000 0.003 -2.151 0.311 -0.094 -3.0 -0.022 0.02583 -0.023 0.918 0.003 1.000 0.004 -0.839 0.148 -0.805 -2.5 -0.103 0.02447 -0.025 0.891 0.004 1.000 0.016 -4.228 -0.543 0.008 -2.0 -0.038 0.03184 -0.036 0.863 0.075 1.000 0.997 -1.208 0.344 -0.691 -1.5 0.016 0.01975 -0.036 0.833 0.995 1.000 0.996 0.816 0.253 2.502 -1.0 0.074 0.02054 -0.036 0.787 0.996 1.000 0.996 3.604 0.253 0.743 -0.5 0.132 0.02152 -0.037 0.712 0.995 1.000 0.996 6.130 0.253 0.528 0.0 0.190 0.02255 -0.037 0.645 0.995 1.000 0.996 8.415 0.253 0.444 0.5 0.248 0.02317 -0.037 0.592 0.995 1.000 0.996 10.688 0.253 0.399 1.0 0.305 0.02394 -0.037 0.542 0.995 1.000 0.996 12.759 0.253 0.372 1.5 0.363 0.02533 -0.037 0.487 0.995 1.000 0.996 14.336 0.253 0.353 2.0 0.421 0.02621 -0.038 0.413 0.996 1.000 0.996 16.055 0.253 0.339 2.5 0.478 0.02729 -0.038 0.329 0.995 1.000 0.996 17.528 0.253 0.329 3.0 0.536 0.02790 -0.038 0.257 0.995 1.000 0.996 19.207 0.253 0.321 3.5 0.593 0.02873 -0.038 0.193 0.996 1.000 0.996 20.647 0.253 0.314 4.0 0.650 0.02939 -0.038 0.144 0.995 1.000 0.996 22.120 0.254 0.309 4.5 0.706 0.02953 -0.038 0.102 0.995 1.000 0.996 23.922 0.254 0.304 5.0 0.761 0.02971 -0.039 0.060 0.996 1.000 0.996 25.628 0.254 0.301 5.5 0.815 0.02972 -0.039 0.019 0.996 1.000 0.996 27.412 0.095 0.298 6.0 0.585 0.04095 -0.066 0.005 0.996 0.025 0.996 14.297 0.083 0.363 6.5 0.642 0.04148 -0.068 0.001 0.996 0.004 0.996 15.474 0.297 0.356 7.0 0.674 0.04537 -0.070 0.001 0.997 0.002 0.997 14.868 0.330 0.354 7.5 0.701 0.05057 -0.072 0.001 0.997 0.001 0.997 13.867 0.347 0.353 8.0 0.724 0.05722 -0.075 0.001 0.997 0.001 0.997 12.647 0.369 0.353 8.5 0.741 0.06517 -0.077 0.001 0.997 0.001 0.997 11.376 0.404 0.354 9.0 0.755 0.07407 -0.080 0.001 0.997 0.001 0.997 10.191 0.464 0.356 9.5 0.764 0.08202 -0.082 0.000 0.997 0.001 0.997 9.312 0.623 0.357 10.0 0.768 0.08882 -0.084 0.001 0.997 0.001 0.997 8.644 1.766 0.360 10.5 0.767 0.09837 -0.087 0.001 0.997 0.001 0.997 7.797 -0.584 0.363 11.0 0.762 0.11047 -0.089 0.001 0.997 0.001 0.997 6.898 -0.083 0.367 11.5 0.753 0.11821 -0.092 0.001 0.997 0.001 0.997 6.366 0.039 0.372 12.0 0.739 0.13666 -0.094 0.001 0.997 0.001 0.997 5.408 0.093 0.377 12.5 0.722 0.15233 -0.097 0.001 0.997 0.001 0.997 4.738 0.121 0.384 13.0 0.702 0.16053 -0.099 0.001 0.997 0.001 0.997 4.370 0.138 0.391 13.5 0.678 0.18097 -0.101 0.001 0.997 0.002 0.997 3.749 0.148 0.399 14.0 0.654 0.19549 -0.104 0.001 0.997 0.001 0.997 3.347 0.155 0.409 14.5 0.628 0.21975 -0.106 0.001 0.996 0.001 0.996 2.857 0.160 0.419 15.0 0.601 0.23689 -0.109 0.001 0.997 0.002 0.997 2.535 0.162 0.431 Name = AG04 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 -0.302 0.22480 0.030 1.000 0.002 1.000 0.004 -1.343 0.086 0.350 -14.5 -0.315 0.21841 0.028 1.000 0.001 1.000 0.004 -1.441 0.083 0.339 -14.0 -0.327 0.20372 0.026 1.000 0.001 1.000 0.003 -1.606 0.076 0.329 -13.5 -0.339 0.18017 0.024 1.000 0.001 1.000 0.003 -1.882 0.063 0.320 -13.0 -0.350 0.16887 0.022 1.000 0.002 1.000 0.003 -2.072 0.043 0.312 -12.5 -0.360 0.15011 0.020 1.000 0.002 1.000 0.003 -2.396 0.009 0.304 -12.0 -0.368 0.14104 0.017 1.000 0.002 1.000 0.003 -2.607 -0.054 0.297 -11.5 -0.374 0.15285 0.015 1.000 0.001 1.000 0.003 -2.446 -0.194 0.291 -11.0 -0.378 0.14041 0.013 1.000 0.001 1.000 0.003 -2.689 -0.699 0.285 -10.5 -0.378 0.12359 0.011 1.000 0.002 1.000 0.003 -3.063 3.544 0.279 -10.0 -0.376 0.11481 0.009 1.000 0.002 1.000 0.003 -3.277 0.813 0.273 -9.5 -0.371 0.10045 0.006 1.000 0.002 1.000 0.003 -3.690 0.525 0.267 -9.0 -0.360 0.08994 0.004 1.000 0.001 1.000 0.003 -4.004 0.431 0.262 -8.5 -0.346 0.08253 0.002 1.000 0.001 1.000 0.003 -4.195 0.394 0.256 -8.0 -0.329 0.07223 -0.000 1.000 0.001 1.000 0.002 -4.558 0.369 0.249 -7.5 -0.309 0.06454 -0.002 1.000 0.001 1.000 0.002 -4.784 0.352 0.242 -7.0 -0.285 0.05875 -0.005 1.000 0.002 1.000 0.002 -4.854 0.341 0.234 -6.5 -0.259 0.05164 -0.007 1.000 0.001 1.000 0.002 -5.018 0.332 0.223 -6.0 -0.230 0.04615 -0.009 1.000 0.001 1.000 0.002 -4.983 0.326 0.210 -5.5 -0.200 0.04053 -0.011 1.000 0.001 1.000 0.002 -4.926 0.322 0.193 -5.0 -0.167 0.03605 -0.014 1.000 0.001 1.000 0.002 -4.629 0.318 0.168 -4.5 -0.132 0.03249 -0.016 1.000 0.002 1.000 0.002 -4.071 0.315 0.129 -4.0 -0.097 0.02857 -0.018 1.000 0.002 1.000 0.002 -3.379 0.313 0.061 -3.5 -0.060 0.02549 -0.021 1.000 0.002 1.000 0.003 -2.339 0.311 -0.095 -3.0 -0.021 0.02379 -0.023 0.918 0.003 1.000 0.004 -0.898 -0.175 -0.820 -2.5 -0.096 0.02936 -0.036 0.891 0.004 1.000 0.997 -3.269 -0.528 -0.125 -2.0 -0.038 0.02977 -0.036 0.863 0.075 1.000 0.997 -1.293 0.252 -0.690 -1.5 0.016 0.01703 -0.036 0.833 0.995 1.000 0.996 0.947 0.253 2.502 -1.0 0.074 0.01764 -0.036 0.787 0.996 1.000 0.996 4.195 0.253 0.743 -0.5 0.132 0.01893 -0.037 0.712 0.995 1.000 0.996 6.969 0.253 0.528 0.0 0.190 0.01999 -0.037 0.645 0.995 1.000 0.996 9.495 0.253 0.444 0.5 0.248 0.02074 -0.037 0.592 0.995 1.000 0.996 11.936 0.253 0.399 1.0 0.305 0.02141 -0.037 0.542 0.995 1.000 0.996 14.265 0.253 0.372 1.5 0.363 0.02281 -0.037 0.487 0.995 1.000 0.996 15.924 0.253 0.353 2.0 0.421 0.02382 -0.038 0.413 0.996 1.000 0.996 17.671 0.253 0.339 2.5 0.478 0.02507 -0.038 0.329 0.995 1.000 0.996 19.081 0.253 0.329 3.0 0.536 0.02583 -0.038 0.257 0.995 1.000 0.996 20.743 0.253 0.321 3.5 0.593 0.02679 -0.038 0.193 0.996 1.000 0.996 22.142 0.253 0.314 4.0 0.650 0.02764 -0.038 0.144 0.995 1.000 0.996 23.517 0.254 0.309 4.5 0.706 0.02783 -0.038 0.102 0.995 1.000 0.996 25.377 0.254 0.304 5.0 0.761 0.02812 -0.039 0.060 0.996 1.000 0.996 27.071 0.254 0.301 5.5 0.815 0.02840 -0.039 0.019 0.996 1.000 0.996 28.683 0.254 0.298 6.0 0.866 0.02761 -0.039 0.005 0.996 1.000 0.996 31.367 0.085 0.295 6.5 0.640 0.03883 -0.068 0.001 0.996 0.005 0.996 16.474 0.089 0.356 7.0 0.674 0.04223 -0.070 0.001 0.997 0.002 0.997 15.954 0.327 0.354 7.5 0.701 0.04695 -0.072 0.001 0.997 0.001 0.997 14.928 0.345 0.353 8.0 0.724 0.05173 -0.075 0.001 0.997 0.001 0.997 13.988 0.368 0.353 8.5 0.741 0.05838 -0.077 0.001 0.997 0.001 0.997 12.698 0.404 0.354 9.0 0.755 0.06578 -0.080 0.001 0.997 0.001 0.997 11.475 0.464 0.356 9.5 0.764 0.07183 -0.082 0.000 0.997 0.001 0.997 10.633 0.623 0.357 10.0 0.768 0.07786 -0.084 0.001 0.997 0.001 0.997 9.860 1.766 0.360 10.5 0.767 0.08534 -0.087 0.001 0.997 0.001 0.997 8.987 -0.584 0.363 11.0 0.762 0.09555 -0.089 0.001 0.997 0.001 0.997 7.975 -0.077 0.367 11.5 0.752 0.10714 -0.092 0.001 0.997 0.001 0.997 7.021 0.039 0.372 12.0 0.739 0.11623 -0.094 0.001 0.997 0.001 0.997 6.359 0.092 0.377 12.5 0.722 0.12793 -0.097 0.001 0.997 0.001 0.997 5.641 0.122 0.384 13.0 0.701 0.14142 -0.099 0.001 0.997 0.001 0.997 4.959 0.139 0.391 13.5 0.678 0.15781 -0.101 0.001 0.997 0.002 0.997 4.298 0.148 0.399 14.0 0.654 0.17155 -0.104 0.001 0.997 0.001 0.997 3.812 0.155 0.409 14.5 0.628 0.19072 -0.106 0.001 0.996 0.002 0.996 3.291 0.160 0.419 15.0 0.600 0.20360 -0.109 0.001 0.997 0.002 0.997 2.949 0.161 0.431 Name = AG04 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 -0.302 0.21246 0.030 1.000 0.002 1.000 0.004 -1.420 0.086 0.350 -14.5 -0.315 0.19408 0.028 1.000 0.001 1.000 0.004 -1.621 0.083 0.339 -14.0 -0.327 0.18287 0.026 1.000 0.001 1.000 0.004 -1.789 0.076 0.329 -13.5 -0.339 0.16330 0.024 1.000 0.001 1.000 0.003 -2.076 0.063 0.320 -13.0 -0.350 0.15381 0.022 1.000 0.002 1.000 0.004 -2.274 0.043 0.312 -12.5 -0.360 0.13788 0.020 1.000 0.002 1.000 0.003 -2.608 0.008 0.304 -12.0 -0.368 0.13020 0.017 1.000 0.002 1.000 0.003 -2.823 -0.055 0.297 -11.5 -0.374 0.11411 0.015 1.000 0.001 1.000 0.003 -3.276 -0.195 0.291 -11.0 -0.377 0.10657 0.013 1.000 0.001 1.000 0.003 -3.541 -0.703 0.285 -10.5 -0.378 0.11480 0.011 1.000 0.002 1.000 0.003 -3.296 3.938 0.279 -10.0 -0.376 0.10194 0.009 1.000 0.002 1.000 0.003 -3.690 0.809 0.273 -9.5 -0.370 0.09450 0.006 1.000 0.002 1.000 0.003 -3.920 0.521 0.267 -9.0 -0.360 0.08452 0.004 1.000 0.001 1.000 0.003 -4.259 0.433 0.262 -8.5 -0.346 0.07430 0.002 1.000 0.001 1.000 0.003 -4.660 0.394 0.256 -8.0 -0.329 0.06861 -0.000 1.000 0.001 1.000 0.003 -4.794 0.368 0.249 -7.5 -0.308 0.06160 -0.002 1.000 0.001 1.000 0.003 -5.007 0.352 0.242 -7.0 -0.285 0.05395 -0.005 1.000 0.002 1.000 0.002 -5.285 0.341 0.234 -6.5 -0.259 0.04767 -0.007 1.000 0.001 1.000 0.002 -5.436 0.332 0.223 -6.0 -0.230 0.04268 -0.009 1.000 0.001 1.000 0.002 -5.388 0.326 0.210 -5.5 -0.199 0.03909 -0.011 1.000 0.001 1.000 0.002 -5.099 0.322 0.193 -5.0 -0.167 0.03446 -0.014 1.000 0.001 1.000 0.002 -4.836 0.318 0.168 -4.5 -0.132 0.03042 -0.016 1.000 0.002 1.000 0.002 -4.348 0.315 0.129 -4.0 -0.096 0.02712 -0.018 1.000 0.002 1.000 0.002 -3.553 0.313 0.060 -3.5 -0.060 0.02396 -0.021 1.000 0.002 1.000 0.003 -2.488 0.311 -0.095 -3.0 -0.021 0.02239 -0.023 0.918 0.003 1.000 0.004 -0.955 -0.175 -0.820 -2.5 -0.096 0.02867 -0.036 0.891 0.004 1.000 0.997 -3.349 -0.527 -0.125 -2.0 -0.039 0.02911 -0.036 0.863 0.075 1.000 0.997 -1.324 0.252 -0.689 -1.5 0.016 0.01533 -0.036 0.833 0.995 1.000 0.996 1.051 0.253 2.502 -1.0 0.074 0.01606 -0.036 0.787 0.996 1.000 0.996 4.608 0.253 0.743 -0.5 0.132 0.01747 -0.037 0.712 0.995 1.000 0.996 7.551 0.253 0.528 0.0 0.190 0.01857 -0.037 0.645 0.995 1.000 0.996 10.219 0.253 0.444 0.5 0.248 0.01925 -0.037 0.592 0.995 1.000 0.996 12.860 0.253 0.399 1.0 0.305 0.02035 -0.037 0.542 0.995 1.000 0.996 15.005 0.253 0.372 1.5 0.363 0.02127 -0.037 0.487 0.995 1.000 0.996 17.070 0.253 0.353 2.0 0.421 0.02237 -0.038 0.413 0.996 1.000 0.996 18.813 0.253 0.339 2.5 0.478 0.02312 -0.038 0.329 0.995 1.000 0.996 20.689 0.253 0.329 3.0 0.536 0.02460 -0.038 0.257 0.995 1.000 0.996 21.784 0.253 0.321 3.5 0.593 0.02495 -0.038 0.193 0.996 1.000 0.996 23.768 0.253 0.314 4.0 0.650 0.02586 -0.038 0.144 0.995 1.000 0.996 25.137 0.254 0.309 4.5 0.706 0.02646 -0.038 0.102 0.995 1.000 0.996 26.690 0.254 0.304 5.0 0.761 0.02720 -0.039 0.060 0.996 1.000 0.996 27.986 0.254 0.301 5.5 0.815 0.02689 -0.039 0.019 0.996 1.000 0.996 30.296 0.254 0.298 6.0 0.866 0.02698 -0.039 0.005 0.996 1.000 0.996 32.100 0.088 0.295 6.5 0.637 0.03746 -0.068 0.001 0.996 0.006 0.996 16.993 0.089 0.357 7.0 0.673 0.04000 -0.070 0.001 0.997 0.002 0.997 16.834 0.322 0.354 7.5 0.701 0.04413 -0.072 0.001 0.997 0.001 0.997 15.881 0.345 0.353 8.0 0.724 0.04849 -0.075 0.001 0.997 0.001 0.997 14.923 0.368 0.353 8.5 0.741 0.05437 -0.077 0.001 0.997 0.001 0.997 13.635 0.404 0.354 9.0 0.755 0.06089 -0.080 0.001 0.997 0.001 0.997 12.396 0.464 0.356 9.5 0.764 0.06590 -0.082 0.000 0.997 0.001 0.997 11.590 0.623 0.357 10.0 0.768 0.07144 -0.084 0.001 0.997 0.001 0.997 10.747 1.950 0.360 10.5 0.767 0.08097 -0.087 0.001 0.997 0.001 0.997 9.468 -0.584 0.363 11.0 0.762 0.08681 -0.089 0.001 0.997 0.001 0.997 8.777 -0.084 0.367 11.5 0.752 0.09638 -0.092 0.001 0.997 0.001 0.997 7.805 0.042 0.372 12.0 0.739 0.10890 -0.094 0.001 0.997 0.001 0.997 6.784 0.093 0.377 12.5 0.721 0.11888 -0.097 0.001 0.997 0.001 0.997 6.069 0.122 0.384 13.0 0.701 0.13029 -0.099 0.001 0.997 0.002 0.997 5.381 0.139 0.391 13.5 0.678 0.14426 -0.101 0.001 0.997 0.002 0.997 4.700 0.148 0.400 14.0 0.654 0.15753 -0.104 0.001 0.997 0.002 0.997 4.150 0.155 0.409 14.5 0.628 0.17356 -0.106 0.001 0.996 0.002 0.996 3.616 0.160 0.419 15.0 0.600 0.16504 -0.109 0.001 0.997 0.002 0.997 3.637 0.161 0.431