Name = AH 79-100 C 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 -0.080 0.29940 -0.152 0.942 0.003 0.955 0.004 -0.268 0.392 -1.641 -14.5 -0.060 0.26788 -0.155 0.941 0.003 0.955 0.004 -0.223 0.384 -2.336 -14.0 -0.037 0.24062 -0.158 0.939 0.003 0.954 0.004 -0.153 0.371 -4.037 -13.5 -0.012 0.21550 -0.161 0.938 0.003 0.954 0.003 -0.054 0.236 -13.590 -13.0 -0.463 0.19170 -0.163 0.936 0.003 0.953 0.003 -2.415 0.236 -0.103 -12.5 -0.423 0.18526 -0.166 0.935 0.002 0.953 0.003 -2.285 0.321 -0.143 -12.0 -0.380 0.16373 -0.169 0.933 0.002 0.952 0.003 -2.319 0.315 -0.196 -11.5 -0.332 0.14401 -0.172 0.930 0.002 0.952 0.003 -2.307 0.311 -0.269 -11.0 -0.281 0.13226 -0.175 0.925 0.002 0.951 0.003 -2.128 0.307 -0.373 -10.5 -0.227 0.11781 -0.178 0.921 0.002 0.951 0.003 -1.930 0.304 -0.535 -10.0 -0.171 0.10719 -0.181 0.917 0.002 0.950 0.003 -1.591 0.302 -0.814 -9.5 -0.111 0.09366 -0.184 0.888 0.002 0.952 0.003 -1.188 0.300 -1.407 -9.0 -0.050 0.08558 -0.187 0.876 0.002 0.952 0.003 -0.585 0.299 -3.493 -8.5 0.013 0.07793 -0.190 0.861 0.003 0.952 0.003 0.162 0.298 15.290 -8.0 0.076 0.07099 -0.194 0.846 0.003 0.952 0.004 1.078 0.298 2.780 -7.5 0.141 0.06552 -0.197 0.831 0.003 0.952 0.004 2.152 0.297 1.644 -7.0 0.206 0.06034 -0.200 0.801 0.003 0.954 0.007 3.410 0.296 1.220 -6.5 0.270 0.05581 -0.203 0.787 0.004 0.953 0.011 4.845 0.297 0.999 -6.0 0.335 0.05378 -0.206 0.770 0.011 0.953 0.012 6.223 0.298 0.864 -5.5 0.398 0.05007 -0.209 0.748 0.011 0.953 0.012 7.959 0.299 0.774 -5.0 0.461 0.04661 -0.212 0.733 0.011 0.953 0.013 9.897 0.300 0.709 -4.5 0.523 0.04337 -0.215 0.719 0.012 0.952 0.014 12.064 0.301 0.661 -4.0 0.584 0.04067 -0.218 0.707 0.012 0.951 0.014 14.348 0.302 0.624 -3.5 0.643 0.03829 -0.221 0.696 0.013 0.950 0.015 16.784 0.304 0.594 -3.0 0.701 0.03611 -0.224 0.685 0.013 0.948 0.016 19.401 0.304 0.570 -2.5 0.757 0.03426 -0.227 0.676 0.015 0.944 0.023 22.105 0.305 0.550 -2.0 0.812 0.03290 -0.230 0.667 0.032 0.940 0.046 24.693 0.398 0.534 -1.5 0.846 0.03094 -0.240 0.658 0.036 0.936 0.999 27.329 0.369 0.534 -1.0 0.905 0.03181 -0.241 0.651 0.156 0.929 0.999 28.439 0.266 0.517 -0.5 0.964 0.02957 -0.242 0.643 0.720 0.920 0.999 32.600 0.322 0.501 0.0 0.932 0.03067 -0.243 0.636 0.787 0.900 0.999 30.384 0.476 0.511 0.5 0.976 0.03125 -0.245 0.629 0.841 0.882 0.999 31.217 0.287 0.501 1.0 1.025 0.03190 -0.247 0.617 0.927 0.872 0.999 32.115 0.289 0.491 1.5 1.072 0.03238 -0.249 0.606 0.999 0.859 0.999 33.098 0.294 0.482 2.0 1.117 0.03342 -0.251 0.596 0.999 0.845 0.999 33.436 0.299 0.475 2.5 1.162 0.03459 -0.253 0.587 0.999 0.830 1.000 33.587 0.306 0.468 3.0 1.203 0.03586 -0.256 0.578 1.000 0.810 1.000 33.534 0.312 0.463 3.5 1.245 0.03726 -0.258 0.569 1.000 0.794 1.000 33.412 0.307 0.457 4.0 1.292 0.03863 -0.261 0.555 1.000 0.784 1.000 33.442 0.235 0.452 4.5 1.489 0.03546 -0.255 0.004 1.000 0.954 1.000 42.000 0.231 0.421 5.0 1.539 0.03642 -0.256 0.004 1.000 0.951 1.000 42.260 -0.027 0.416 5.5 1.405 0.03337 -0.278 0.003 1.000 0.004 1.000 42.097 0.001 0.448 6.0 1.438 0.03653 -0.281 0.003 1.000 0.004 1.000 39.376 0.347 0.446 6.5 1.470 0.04011 -0.284 0.002 1.000 0.003 1.000 36.639 0.353 0.444 7.0 1.500 0.04410 -0.288 0.002 1.000 0.003 1.000 34.004 0.360 0.442 7.5 1.527 0.04913 -0.291 0.002 1.000 0.003 1.000 31.077 0.370 0.440 8.0 1.552 0.05457 -0.294 0.002 1.000 0.003 1.000 28.436 0.381 0.439 8.5 1.574 0.05893 -0.297 0.002 1.000 0.003 1.000 26.718 0.397 0.439 9.0 1.594 0.06625 -0.300 0.002 1.000 0.003 1.000 24.067 0.417 0.438 9.5 1.612 0.07360 -0.303 0.002 1.000 0.002 1.000 21.902 0.445 0.438 10.0 1.626 0.08218 -0.306 0.002 1.000 0.002 1.000 19.790 0.487 0.438 10.5 1.638 0.09103 -0.309 0.002 1.000 0.002 1.000 17.995 0.553 0.439 11.0 1.647 0.10104 -0.313 0.002 1.000 0.002 1.000 16.298 0.774 0.440 11.5 1.650 0.10928 -0.316 0.002 1.000 0.002 1.000 15.098 -3.144 0.441 12.0 1.645 0.12185 -0.319 0.002 1.000 0.002 1.000 13.500 -0.191 0.444 12.5 1.636 0.13451 -0.322 0.001 1.000 0.002 1.000 12.162 -0.021 0.447 13.0 1.622 0.15122 -0.325 0.001 1.000 0.002 1.000 10.728 0.056 0.450 13.5 1.604 0.15798 -0.328 0.002 1.000 0.002 1.000 10.156 0.097 0.454 14.0 1.582 0.17820 -0.331 0.002 1.000 0.002 1.000 8.880 0.123 0.459 14.5 1.557 0.19015 -0.334 0.001 1.000 0.002 1.000 8.187 0.140 0.465 15.0 1.527 0.21556 -0.337 0.001 1.000 0.002 1.000 7.085 0.147 0.471 Name = AH 79-100 C 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 -0.080 0.22709 -0.152 0.942 0.003 0.956 0.004 -0.353 0.392 -1.644 -14.5 -0.060 0.20652 -0.155 0.941 0.003 0.956 0.004 -0.289 0.384 -2.343 -14.0 -0.037 0.18485 -0.158 0.939 0.003 0.955 0.004 -0.198 0.371 -4.058 -13.5 -0.011 0.16845 -0.161 0.938 0.003 0.955 0.004 -0.068 0.236 -13.814 -13.0 -0.463 0.15231 -0.163 0.936 0.003 0.954 0.003 -3.040 0.236 -0.103 -12.5 -0.423 0.13645 -0.166 0.935 0.002 0.954 0.003 -3.102 0.321 -0.143 -12.0 -0.380 0.12310 -0.169 0.933 0.002 0.953 0.003 -3.084 0.315 -0.196 -11.5 -0.332 0.11624 -0.172 0.930 0.002 0.953 0.003 -2.858 0.311 -0.269 -11.0 -0.281 0.10470 -0.175 0.925 0.002 0.953 0.003 -2.687 0.307 -0.373 -10.5 -0.227 0.09412 -0.178 0.921 0.002 0.952 0.003 -2.415 0.304 -0.535 -10.0 -0.171 0.08654 -0.181 0.917 0.002 0.952 0.003 -1.970 0.302 -0.814 -9.5 -0.111 0.07785 -0.184 0.888 0.002 0.955 0.003 -1.429 0.300 -1.407 -9.0 -0.050 0.07105 -0.187 0.876 0.002 0.956 0.003 -0.705 0.299 -3.493 -8.5 0.013 0.06486 -0.190 0.861 0.003 0.957 0.004 0.195 0.298 15.290 -8.0 0.076 0.05911 -0.193 0.846 0.003 0.958 0.004 1.294 0.298 2.780 -7.5 0.141 0.05453 -0.197 0.831 0.003 0.958 0.004 2.586 0.296 1.644 -7.0 0.206 0.05066 -0.199 0.801 0.003 0.961 0.010 4.060 0.296 1.220 -6.5 0.270 0.04708 -0.202 0.787 0.004 0.961 0.012 5.742 0.298 0.999 -6.0 0.335 0.04506 -0.206 0.770 0.011 0.962 0.012 7.428 0.299 0.864 -5.5 0.398 0.04192 -0.209 0.748 0.011 0.963 0.013 9.504 0.299 0.774 -5.0 0.461 0.03894 -0.212 0.733 0.011 0.963 0.013 11.848 0.300 0.709 -4.5 0.523 0.03617 -0.215 0.719 0.012 0.962 0.014 14.466 0.301 0.661 -4.0 0.584 0.03383 -0.218 0.707 0.012 0.962 0.015 17.247 0.302 0.624 -3.5 0.643 0.03162 -0.221 0.696 0.013 0.961 0.016 20.321 0.304 0.594 -3.0 0.701 0.02960 -0.224 0.685 0.013 0.960 0.017 23.672 0.304 0.570 -2.5 0.757 0.02788 -0.227 0.676 0.015 0.959 0.032 27.152 0.427 0.550 -2.0 0.786 0.02419 -0.240 0.667 0.032 0.958 0.999 32.510 0.398 0.555 -1.5 0.846 0.02473 -0.240 0.658 0.036 0.956 0.999 34.192 0.266 0.534 -1.0 0.905 0.02482 -0.241 0.651 0.156 0.954 0.999 36.448 0.266 0.517 -0.5 0.964 0.02212 -0.242 0.643 0.720 0.952 0.999 43.576 0.279 0.501 0.0 0.973 0.02242 -0.243 0.636 0.787 0.951 0.999 43.388 0.285 0.500 0.5 1.028 0.02272 -0.245 0.629 0.841 0.948 0.999 45.260 0.274 0.488 1.0 1.084 0.02283 -0.246 0.617 0.927 0.946 0.999 47.479 0.275 0.477 1.5 1.138 0.02298 -0.247 0.606 0.999 0.943 0.999 49.544 0.276 0.467 2.0 1.192 0.02361 -0.249 0.596 0.999 0.939 0.999 50.480 0.277 0.459 2.5 1.245 0.02431 -0.250 0.587 0.999 0.934 1.000 51.198 0.281 0.451 3.0 1.294 0.02505 -0.252 0.578 1.000 0.926 1.000 51.656 0.286 0.445 3.5 1.341 0.02587 -0.254 0.569 1.000 0.917 1.000 51.845 0.292 0.439 4.0 1.387 0.02681 -0.256 0.555 1.000 0.905 1.000 51.716 0.253 0.434 4.5 1.501 0.02974 -0.254 0.004 1.000 0.964 1.000 50.469 0.249 0.419 5.0 1.551 0.03080 -0.256 0.004 1.000 0.961 1.000 50.357 0.002 0.415 5.5 1.404 0.02976 -0.278 0.003 1.000 0.004 1.000 47.186 0.022 0.448 6.0 1.438 0.03250 -0.281 0.003 1.000 0.004 1.000 44.247 0.347 0.446 6.5 1.469 0.03559 -0.284 0.002 1.000 0.004 1.000 41.283 0.353 0.444 7.0 1.499 0.03900 -0.288 0.002 1.000 0.003 1.000 38.440 0.360 0.442 7.5 1.526 0.04318 -0.291 0.002 1.000 0.003 1.000 35.349 0.370 0.440 8.0 1.551 0.04767 -0.294 0.002 1.000 0.003 1.000 32.543 0.381 0.439 8.5 1.574 0.05162 -0.297 0.002 1.000 0.003 1.000 30.494 0.395 0.439 9.0 1.594 0.05571 -0.300 0.002 1.000 0.003 1.000 28.616 0.415 0.438 9.5 1.612 0.06143 -0.303 0.002 1.000 0.002 1.000 26.238 0.445 0.438 10.0 1.626 0.06755 -0.306 0.002 1.000 0.002 1.000 24.076 0.487 0.438 10.5 1.638 0.07439 -0.309 0.002 1.000 0.002 1.000 22.021 0.553 0.439 11.0 1.647 0.08138 -0.313 0.002 1.000 0.002 1.000 20.235 0.782 0.440 11.5 1.650 0.09006 -0.316 0.002 1.000 0.002 1.000 18.318 -3.144 0.441 12.0 1.645 0.09687 -0.319 0.002 1.000 0.002 1.000 16.981 -0.196 0.444 12.5 1.636 0.10566 -0.322 0.001 1.000 0.002 1.000 15.483 -0.021 0.447 13.0 1.622 0.11740 -0.325 0.001 1.000 0.002 1.000 13.818 0.057 0.450 13.5 1.604 0.13167 -0.328 0.002 1.000 0.002 1.000 12.183 0.097 0.454 14.0 1.582 0.13763 -0.331 0.002 1.000 0.002 1.000 11.498 0.123 0.459 14.5 1.556 0.15514 -0.334 0.001 1.000 0.002 1.000 10.032 0.140 0.465 15.0 1.527 0.16295 -0.337 0.001 1.000 0.002 1.000 9.373 0.146 0.471 Name = AH 79-100 C 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 -0.080 0.18506 -0.152 0.942 0.003 0.956 0.004 -0.433 0.391 -1.644 -14.5 -0.059 0.18021 -0.155 0.941 0.003 0.956 0.004 -0.330 0.383 -2.350 -14.0 -0.036 0.16092 -0.158 0.939 0.003 0.956 0.004 -0.226 0.371 -4.078 -13.5 -0.011 0.14842 -0.161 0.938 0.003 0.955 0.004 -0.076 0.236 -14.046 -13.0 -0.463 0.13575 -0.163 0.936 0.003 0.955 0.004 -3.410 0.236 -0.103 -12.5 -0.423 0.12141 -0.166 0.935 0.002 0.954 0.004 -3.486 0.321 -0.143 -12.0 -0.380 0.11070 -0.169 0.933 0.002 0.954 0.003 -3.429 0.315 -0.196 -11.5 -0.332 0.10191 -0.172 0.930 0.002 0.954 0.003 -3.260 0.311 -0.269 -11.0 -0.281 0.09280 -0.175 0.925 0.002 0.954 0.003 -3.032 0.307 -0.373 -10.5 -0.227 0.08389 -0.178 0.921 0.002 0.954 0.003 -2.710 0.304 -0.535 -10.0 -0.171 0.07586 -0.181 0.917 0.002 0.953 0.003 -2.248 0.302 -0.814 -9.5 -0.111 0.06985 -0.184 0.888 0.002 0.958 0.003 -1.593 0.300 -1.407 -9.0 -0.050 0.06383 -0.187 0.876 0.002 0.959 0.004 -0.784 0.299 -3.493 -8.5 0.013 0.05847 -0.190 0.861 0.003 0.961 0.004 0.217 0.298 15.290 -8.0 0.076 0.05401 -0.193 0.846 0.003 0.962 0.004 1.416 0.297 2.780 -7.5 0.141 0.05026 -0.196 0.831 0.003 0.963 0.008 2.804 0.296 1.644 -7.0 0.206 0.04644 -0.199 0.801 0.003 0.965 0.012 4.429 0.297 1.220 -6.5 0.270 0.04325 -0.202 0.787 0.004 0.965 0.013 6.250 0.298 0.999 -6.0 0.335 0.04088 -0.206 0.770 0.011 0.966 0.012 8.187 0.299 0.864 -5.5 0.398 0.03834 -0.209 0.748 0.011 0.967 0.013 10.391 0.299 0.774 -5.0 0.461 0.03555 -0.212 0.733 0.011 0.967 0.014 12.978 0.300 0.709 -4.5 0.523 0.03298 -0.215 0.719 0.012 0.967 0.014 15.867 0.301 0.661 -4.0 0.584 0.03074 -0.218 0.707 0.012 0.967 0.015 18.982 0.302 0.624 -3.5 0.643 0.02864 -0.221 0.696 0.013 0.966 0.016 22.437 0.304 0.594 -3.0 0.701 0.02671 -0.224 0.685 0.013 0.966 0.017 26.229 0.303 0.570 -2.5 0.756 0.02481 -0.227 0.676 0.015 0.965 0.049 30.487 0.427 0.550 -2.0 0.786 0.02126 -0.240 0.667 0.032 0.964 0.999 36.985 0.399 0.555 -1.5 0.846 0.02183 -0.240 0.658 0.036 0.963 0.999 38.741 0.266 0.534 -1.0 0.905 0.02175 -0.241 0.651 0.156 0.962 0.999 41.590 0.266 0.517 -0.5 0.964 0.01885 -0.242 0.643 0.720 0.961 0.999 51.139 0.275 0.501 0.0 0.981 0.01901 -0.243 0.636 0.787 0.959 0.999 51.607 0.280 0.498 0.5 1.037 0.01900 -0.245 0.629 0.841 0.958 0.999 54.591 0.272 0.486 1.0 1.094 0.01904 -0.246 0.617 0.927 0.956 0.999 57.474 0.272 0.475 1.5 1.151 0.01910 -0.247 0.606 0.999 0.955 0.999 60.262 0.273 0.465 2.0 1.207 0.01962 -0.248 0.596 0.999 0.954 0.999 61.522 0.273 0.456 2.5 1.262 0.02015 -0.250 0.587 0.999 0.952 1.000 62.662 0.274 0.448 3.0 1.317 0.02072 -0.251 0.578 1.000 0.950 1.000 63.573 0.275 0.441 3.5 1.372 0.02136 -0.253 0.569 1.000 0.947 1.000 64.211 0.277 0.434 4.0 1.425 0.02207 -0.254 0.555 1.000 0.944 1.000 64.568 0.260 0.428 4.5 1.509 0.02682 -0.254 0.004 1.000 0.970 1.000 56.262 0.259 0.418 5.0 1.558 0.02778 -0.255 0.004 1.000 0.967 1.000 56.102 0.018 0.414 5.5 1.404 0.02820 -0.278 0.003 1.000 0.004 1.000 49.799 0.034 0.448 6.0 1.438 0.03076 -0.281 0.003 1.000 0.004 1.000 46.743 0.347 0.446 6.5 1.469 0.03364 -0.284 0.002 1.000 0.004 1.000 43.663 0.353 0.444 7.0 1.499 0.03682 -0.288 0.002 1.000 0.003 1.000 40.706 0.359 0.442 7.5 1.526 0.03998 -0.291 0.002 1.000 0.003 1.000 38.173 0.369 0.440 8.0 1.551 0.04386 -0.294 0.002 1.000 0.003 1.000 35.372 0.381 0.439 8.5 1.574 0.04749 -0.297 0.002 1.000 0.003 1.000 33.146 0.397 0.439 9.0 1.594 0.05239 -0.300 0.002 1.000 0.003 1.000 30.425 0.415 0.438 9.5 1.612 0.05609 -0.303 0.002 1.000 0.002 1.000 28.739 0.442 0.438 10.0 1.626 0.06115 -0.306 0.002 1.000 0.002 1.000 26.594 0.487 0.438 10.5 1.638 0.06708 -0.309 0.002 1.000 0.002 1.000 24.420 0.559 0.439 11.0 1.646 0.07615 -0.313 0.002 1.000 0.002 1.000 21.620 0.791 0.440 11.5 1.650 0.08191 -0.316 0.002 1.000 0.002 1.000 20.139 -3.543 0.441 12.0 1.645 0.08824 -0.319 0.002 1.000 0.002 1.000 18.640 -0.191 0.444 12.5 1.636 0.09816 -0.322 0.001 1.000 0.002 1.000 16.663 -0.019 0.447 13.0 1.622 0.10876 -0.325 0.001 1.000 0.002 1.000 14.914 0.055 0.450 13.5 1.604 0.11413 -0.328 0.002 1.000 0.002 1.000 14.055 0.097 0.454 14.0 1.582 0.12705 -0.331 0.002 1.000 0.002 1.000 12.453 0.123 0.459 14.5 1.556 0.13279 -0.334 0.001 1.000 0.002 1.000 11.721 0.140 0.465 15.0 1.527 0.14835 -0.337 0.001 1.000 0.002 1.000 10.293 0.147 0.471 Name = AH 79-100 C 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 -0.080 0.16857 -0.152 0.942 0.003 0.957 0.004 -0.474 0.390 -1.648 -14.5 -0.059 0.16480 -0.155 0.941 0.003 0.957 0.004 -0.360 0.383 -2.357 -14.0 -0.036 0.14686 -0.158 0.939 0.003 0.956 0.004 -0.247 0.371 -4.099 -13.5 -0.011 0.13682 -0.161 0.938 0.003 0.956 0.004 -0.081 0.236 -14.285 -13.0 -0.463 0.12017 -0.163 0.936 0.003 0.955 0.004 -3.853 0.236 -0.103 -12.5 -0.423 0.11280 -0.166 0.935 0.002 0.955 0.004 -3.752 0.321 -0.143 -12.0 -0.380 0.10373 -0.169 0.933 0.002 0.955 0.004 -3.660 0.315 -0.196 -11.5 -0.332 0.09346 -0.172 0.930 0.002 0.955 0.003 -3.555 0.311 -0.269 -11.0 -0.281 0.08582 -0.175 0.925 0.002 0.955 0.003 -3.279 0.307 -0.373 -10.5 -0.227 0.07790 -0.178 0.921 0.002 0.955 0.003 -2.918 0.304 -0.535 -10.0 -0.171 0.07093 -0.181 0.917 0.002 0.954 0.003 -2.404 0.302 -0.814 -9.5 -0.111 0.06516 -0.184 0.888 0.002 0.960 0.003 -1.708 0.300 -1.407 -9.0 -0.050 0.05960 -0.187 0.876 0.002 0.962 0.004 -0.840 0.299 -3.493 -8.5 0.013 0.05470 -0.190 0.861 0.003 0.963 0.004 0.231 0.298 15.290 -8.0 0.076 0.05052 -0.193 0.846 0.003 0.964 0.004 1.514 0.296 2.780 -7.5 0.141 0.04755 -0.196 0.831 0.003 0.965 0.010 2.963 0.296 1.644 -7.0 0.206 0.04420 -0.199 0.801 0.003 0.968 0.013 4.652 0.297 1.220 -6.5 0.270 0.04086 -0.202 0.787 0.004 0.969 0.014 6.615 0.298 0.999 -6.0 0.335 0.03869 -0.206 0.770 0.011 0.969 0.013 8.650 0.299 0.864 -5.5 0.398 0.03600 -0.209 0.748 0.011 0.970 0.013 11.067 0.299 0.774 -5.0 0.461 0.03336 -0.212 0.733 0.011 0.970 0.014 13.827 0.300 0.709 -4.5 0.523 0.03107 -0.215 0.719 0.012 0.970 0.014 16.839 0.301 0.661 -4.0 0.583 0.02892 -0.218 0.707 0.012 0.970 0.015 20.176 0.302 0.624 -3.5 0.643 0.02687 -0.221 0.696 0.013 0.970 0.016 23.918 0.304 0.594 -3.0 0.701 0.02499 -0.224 0.685 0.013 0.969 0.017 28.033 0.457 0.570 -2.5 0.726 0.01939 -0.239 0.676 0.015 0.969 0.999 37.466 0.427 0.578 -2.0 0.786 0.01968 -0.240 0.667 0.032 0.968 0.999 39.945 0.266 0.555 -1.5 0.846 0.02016 -0.240 0.658 0.036 0.967 1.000 41.944 0.266 0.534 -1.0 0.905 0.01999 -0.241 0.651 0.156 0.966 1.000 45.260 0.266 0.517 -0.5 0.964 0.01690 -0.242 0.643 0.720 0.965 0.999 57.047 0.274 0.502 0.0 0.986 0.01690 -0.243 0.636 0.787 0.964 0.999 58.348 0.277 0.497 0.5 1.043 0.01687 -0.245 0.629 0.841 0.963 0.999 61.843 0.271 0.484 1.0 1.100 0.01683 -0.246 0.617 0.927 0.963 0.999 65.389 0.271 0.473 1.5 1.157 0.01681 -0.247 0.606 0.999 0.962 0.999 68.853 0.272 0.463 2.0 1.214 0.01724 -0.248 0.596 0.999 0.960 0.999 70.407 0.273 0.455 2.5 1.270 0.01775 -0.250 0.587 0.999 0.959 1.000 71.528 0.273 0.447 3.0 1.325 0.01825 -0.251 0.578 1.000 0.957 1.000 72.595 0.274 0.439 3.5 1.380 0.01880 -0.252 0.569 1.000 0.955 1.000 73.408 0.274 0.433 4.0 1.435 0.01943 -0.254 0.555 1.000 0.954 1.000 73.887 0.261 0.427 4.5 1.514 0.02487 -0.254 0.004 1.000 0.974 1.000 60.869 0.261 0.418 5.0 1.564 0.02584 -0.255 0.004 1.000 0.972 1.000 60.527 0.277 0.413 5.5 1.612 0.02693 -0.256 0.003 1.000 0.968 1.000 59.866 0.043 0.409 6.0 1.437 0.02974 -0.281 0.003 1.000 0.004 1.000 48.330 0.055 0.446 6.5 1.468 0.03251 -0.284 0.002 1.000 0.004 1.000 45.172 0.352 0.444 7.0 1.499 0.03515 -0.288 0.002 1.000 0.003 1.000 42.633 0.359 0.442 7.5 1.526 0.03862 -0.291 0.002 1.000 0.003 1.000 39.512 0.370 0.441 8.0 1.551 0.04232 -0.294 0.002 1.000 0.003 1.000 36.649 0.381 0.439 8.5 1.574 0.04593 -0.297 0.002 1.000 0.003 1.000 34.259 0.395 0.439 9.0 1.594 0.04936 -0.300 0.002 1.000 0.003 1.000 32.289 0.415 0.438 9.5 1.612 0.05429 -0.303 0.002 1.000 0.003 1.000 29.682 0.445 0.438 10.0 1.626 0.05911 -0.306 0.002 1.000 0.003 1.000 27.507 0.484 0.438 10.5 1.638 0.06276 -0.309 0.002 1.000 0.002 1.000 26.102 0.553 0.439 11.0 1.646 0.07031 -0.313 0.002 1.000 0.002 1.000 23.417 0.791 0.440 11.5 1.650 0.07546 -0.316 0.002 1.000 0.002 1.000 21.859 -3.543 0.441 12.0 1.645 0.08126 -0.319 0.002 1.000 0.002 1.000 20.240 -0.191 0.444 12.5 1.636 0.08954 -0.322 0.001 1.000 0.002 1.000 18.266 -0.019 0.447 13.0 1.622 0.09863 -0.325 0.001 1.000 0.002 1.000 16.446 0.055 0.450 13.5 1.604 0.10382 -0.328 0.002 1.000 0.002 1.000 15.451 0.097 0.454 14.0 1.582 0.11489 -0.331 0.002 1.000 0.002 1.000 13.771 0.123 0.459 14.5 1.556 0.12625 -0.334 0.001 1.000 0.002 1.000 12.326 0.140 0.465 15.0 1.527 0.13283 -0.337 0.001 1.000 0.002 1.000 11.496 0.146 0.471