Name = WORTMANN FX 60-126 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 -0.432 0.21169 -0.045 0.888 0.002 0.938 0.003 -2.041 0.426 0.146 -14.5 -0.418 0.20518 -0.047 0.879 0.002 0.938 0.003 -2.036 0.416 0.136 -14.0 -0.402 0.17981 -0.050 0.872 0.002 0.939 0.003 -2.233 0.397 0.125 -13.5 -0.383 0.17279 -0.053 0.864 0.002 0.938 0.003 -2.217 0.382 0.113 -13.0 -0.363 0.14879 -0.055 0.857 0.002 0.938 0.003 -2.438 0.370 0.098 -12.5 -0.340 0.13647 -0.058 0.848 0.002 0.938 0.003 -2.493 0.360 0.080 -12.0 -0.316 0.12485 -0.060 0.836 0.002 0.939 0.003 -2.529 0.353 0.059 -11.5 -0.289 0.11008 -0.063 0.827 0.002 0.939 0.003 -2.630 0.346 0.032 -11.0 -0.261 0.10001 -0.066 0.820 0.002 0.938 0.003 -2.611 0.340 -0.001 -10.5 -0.231 0.09230 -0.068 0.814 0.002 0.936 0.003 -2.505 0.336 -0.045 -10.0 -0.200 0.08446 -0.071 0.808 0.002 0.935 0.003 -2.365 0.333 -0.105 -9.5 -0.167 0.07522 -0.074 0.799 0.002 0.934 0.003 -2.219 0.330 -0.191 -9.0 -0.133 0.06909 -0.076 0.789 0.002 0.933 0.003 -1.924 0.327 -0.323 -8.5 -0.097 0.06404 -0.079 0.780 0.002 0.931 0.003 -1.520 0.324 -0.560 -8.0 -0.060 0.05841 -0.082 0.773 0.002 0.927 0.003 -1.035 0.322 -1.099 -7.5 -0.023 0.05315 -0.084 0.767 0.003 0.922 0.003 -0.433 0.228 -3.413 -7.0 -0.309 0.04909 -0.087 0.761 0.003 0.916 0.003 -6.294 0.225 -0.032 -6.5 -0.244 0.04522 -0.090 0.755 0.003 0.911 0.004 -5.390 0.292 -0.118 -6.0 -0.178 0.04214 -0.092 0.747 0.003 0.907 0.004 -4.234 0.291 -0.268 -5.5 -0.113 0.03929 -0.095 0.732 0.004 0.907 0.007 -2.881 0.287 -0.590 -5.0 -0.048 0.04095 -0.097 0.719 0.031 0.904 0.038 -1.178 0.321 -1.766 -4.5 0.015 0.02626 -0.104 0.709 0.033 0.900 0.637 0.580 0.346 7.096 -4.0 0.076 0.02449 -0.109 0.701 0.034 0.891 0.724 3.099 0.333 1.689 -3.5 0.136 0.02355 -0.114 0.692 0.037 0.877 0.817 5.770 0.349 1.091 -3.0 0.194 0.02377 -0.121 0.660 0.066 0.894 0.967 8.177 0.229 0.872 -2.5 0.260 0.02772 -0.112 0.648 0.296 0.882 0.478 9.385 0.200 0.679 -2.0 0.320 0.02664 -0.115 0.637 0.303 0.870 0.500 12.003 0.298 0.609 -1.5 0.379 0.02655 -0.117 0.590 0.343 0.896 0.485 14.284 0.298 0.559 -1.0 0.438 0.02582 -0.120 0.528 0.349 0.914 0.506 16.955 0.300 0.525 -0.5 0.496 0.02503 -0.123 0.518 0.355 0.904 0.542 19.813 0.340 0.498 0.0 0.500 0.02452 -0.126 0.507 0.361 0.890 0.565 20.389 0.309 0.502 0.5 0.563 0.02481 -0.127 0.459 0.368 0.901 0.607 22.702 0.275 0.476 1.0 0.609 0.02536 -0.129 0.451 0.388 0.878 0.621 24.020 0.285 0.461 1.5 0.654 0.02615 -0.130 0.442 0.406 0.856 0.666 25.020 0.278 0.449 2.0 0.717 0.02674 -0.132 0.398 0.412 0.866 1.000 26.802 0.283 0.434 2.5 0.759 0.02634 -0.134 0.389 0.419 0.840 1.000 28.803 0.280 0.426 3.0 0.825 0.02625 -0.135 0.339 0.426 0.856 1.000 31.418 0.285 0.414 3.5 0.863 0.02690 -0.137 0.330 0.434 0.827 1.000 32.094 0.250 0.409 4.0 0.981 0.02613 -0.135 0.083 0.477 0.923 1.000 37.538 0.246 0.388 4.5 1.028 0.02704 -0.137 0.082 0.486 0.908 1.000 38.035 0.296 0.383 5.0 1.073 0.02826 -0.139 0.080 0.495 0.889 1.000 37.958 0.298 0.380 5.5 1.120 0.02932 -0.141 0.049 0.537 0.876 1.000 38.197 0.310 0.376 6.0 1.158 0.03104 -0.144 0.047 0.547 0.852 1.000 37.322 0.338 0.375 6.5 1.193 0.03302 -0.148 0.046 0.557 0.823 1.000 36.120 0.373 0.374 7.0 1.220 0.03554 -0.152 0.044 0.600 0.787 1.000 34.325 0.628 0.374 7.5 1.221 0.03974 -0.158 0.042 0.617 0.715 1.000 30.723 0.033 0.380 8.0 1.127 0.05258 -0.172 0.041 1.000 0.477 1.000 21.427 0.031 0.403 8.5 1.136 0.05867 -0.177 0.026 1.000 0.399 1.000 19.356 0.519 0.406 9.0 1.151 0.06939 -0.179 0.022 1.000 0.049 1.000 16.594 0.332 0.405 9.5 1.189 0.07399 -0.181 0.018 1.000 0.044 1.000 16.070 0.325 0.403 10.0 1.225 0.07921 -0.184 0.016 1.000 0.039 1.000 15.469 0.315 0.400 10.5 1.269 0.08350 -0.187 0.015 1.000 0.026 1.000 15.191 0.319 0.397 11.0 1.301 0.08971 -0.189 0.014 1.000 0.023 1.000 14.498 0.410 0.396 11.5 1.309 0.09419 -0.193 0.004 1.000 0.044 1.000 13.902 0.375 0.398 12.0 1.348 0.09726 -0.195 0.001 1.000 0.027 1.000 13.857 0.288 0.395 12.5 1.410 0.09707 -0.197 0.001 1.000 0.003 1.000 14.529 0.302 0.390 13.0 1.434 0.10462 -0.200 0.001 1.000 0.002 1.000 13.706 0.381 0.389 13.5 1.452 0.11364 -0.203 0.001 1.000 0.001 1.000 12.781 0.426 0.389 14.0 1.466 0.12349 -0.205 0.001 1.000 0.001 1.000 11.869 0.502 0.390 14.5 1.475 0.13358 -0.208 0.001 1.000 0.001 1.000 11.039 0.620 0.391 15.0 1.481 0.14499 -0.211 0.001 1.000 0.001 1.000 10.213 0.710 0.392 Name = WORTMANN FX 60-126 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 -0.432 0.16845 -0.045 0.888 0.002 0.944 0.003 -2.564 0.426 0.146 -14.5 -0.418 0.16448 -0.047 0.879 0.002 0.945 0.003 -2.539 0.416 0.136 -14.0 -0.401 0.14700 -0.050 0.872 0.002 0.946 0.003 -2.730 0.398 0.125 -13.5 -0.383 0.12995 -0.053 0.864 0.002 0.947 0.003 -2.948 0.382 0.113 -13.0 -0.362 0.12485 -0.055 0.857 0.002 0.948 0.003 -2.903 0.370 0.098 -12.5 -0.340 0.10908 -0.058 0.848 0.002 0.949 0.003 -3.117 0.361 0.080 -12.0 -0.316 0.10107 -0.060 0.836 0.002 0.950 0.003 -3.123 0.353 0.059 -11.5 -0.289 0.09010 -0.063 0.827 0.002 0.951 0.003 -3.211 0.346 0.032 -11.0 -0.261 0.08295 -0.066 0.820 0.002 0.951 0.003 -3.147 0.340 -0.001 -10.5 -0.231 0.07676 -0.068 0.814 0.002 0.951 0.003 -3.011 0.336 -0.045 -10.0 -0.200 0.06854 -0.071 0.808 0.002 0.950 0.003 -2.915 0.333 -0.105 -9.5 -0.167 0.06362 -0.074 0.799 0.002 0.951 0.003 -2.622 0.330 -0.191 -9.0 -0.133 0.05867 -0.076 0.789 0.002 0.951 0.003 -2.264 0.327 -0.324 -8.5 -0.097 0.05444 -0.079 0.780 0.002 0.951 0.003 -1.786 0.324 -0.562 -8.0 -0.060 0.04985 -0.082 0.773 0.002 0.951 0.003 -1.210 0.322 -1.103 -7.5 -0.023 0.04555 -0.084 0.767 0.003 0.950 0.003 -0.502 0.228 -3.438 -7.0 -0.309 0.04254 -0.087 0.761 0.003 0.948 0.004 -7.261 0.225 -0.032 -6.5 -0.244 0.03920 -0.090 0.755 0.003 0.945 0.004 -6.217 0.292 -0.118 -6.0 -0.178 0.03647 -0.092 0.747 0.003 0.943 0.005 -4.892 0.291 -0.268 -5.5 -0.113 0.03443 -0.095 0.732 0.004 0.946 0.009 -3.288 0.339 -0.590 -5.0 -0.046 0.02065 -0.104 0.719 0.031 0.946 0.701 -2.212 0.363 -2.031 -4.5 0.015 0.01935 -0.110 0.709 0.033 0.944 0.786 0.778 0.373 7.531 -4.0 0.074 0.01882 -0.119 0.701 0.034 0.941 0.960 3.956 0.343 1.847 -3.5 0.134 0.01847 -0.121 0.692 0.037 0.938 0.979 7.276 0.272 1.148 -3.0 0.194 0.01833 -0.122 0.660 0.066 0.948 0.984 10.604 0.193 0.876 -2.5 0.259 0.01888 -0.114 0.648 0.296 0.945 0.620 13.694 0.215 0.689 -2.0 0.317 0.01781 -0.117 0.637 0.303 0.942 0.713 17.823 0.291 0.620 -1.5 0.378 0.01833 -0.118 0.590 0.343 0.956 0.619 20.615 0.288 0.563 -1.0 0.434 0.01768 -0.122 0.528 0.349 0.969 0.735 24.555 0.308 0.531 -0.5 0.494 0.01864 -0.125 0.518 0.355 0.966 0.991 26.498 0.291 0.503 0.0 0.535 0.02003 -0.126 0.507 0.361 0.962 0.994 26.739 0.265 0.485 0.5 0.597 0.02153 -0.127 0.459 0.368 0.968 0.999 27.753 0.265 0.462 1.0 0.654 0.02259 -0.128 0.451 0.388 0.962 1.000 28.929 0.268 0.445 1.5 0.707 0.02087 -0.129 0.442 0.406 0.953 1.000 33.887 0.266 0.432 2.0 0.769 0.01977 -0.130 0.398 0.412 0.958 1.000 38.905 0.268 0.418 2.5 0.821 0.01922 -0.131 0.389 0.419 0.946 1.000 42.712 0.268 0.409 3.0 0.883 0.01944 -0.132 0.339 0.426 0.952 1.000 45.423 0.271 0.399 3.5 0.932 0.01961 -0.133 0.330 0.434 0.938 1.000 47.549 0.262 0.393 4.0 1.006 0.02306 -0.133 0.083 0.477 0.962 1.000 43.628 0.263 0.382 4.5 1.055 0.02392 -0.135 0.082 0.486 0.948 1.000 44.121 0.285 0.378 5.0 1.104 0.02488 -0.137 0.080 0.495 0.935 1.000 44.371 0.292 0.374 5.5 1.150 0.02613 -0.139 0.049 0.537 0.918 1.000 43.992 0.297 0.371 6.0 1.196 0.02726 -0.141 0.047 0.547 0.904 1.000 43.865 0.306 0.368 6.5 1.237 0.02825 -0.144 0.046 0.557 0.884 1.000 43.790 0.325 0.366 7.0 1.275 0.02928 -0.147 0.044 0.600 0.860 1.000 43.530 0.352 0.365 7.5 1.306 0.03026 -0.151 0.042 0.617 0.830 1.000 43.168 0.385 0.365 8.0 1.334 0.03293 -0.155 0.041 1.000 0.798 1.000 40.525 0.378 0.366 8.5 1.368 0.03540 -0.158 0.026 1.000 0.774 1.000 38.655 0.484 0.366 9.0 1.377 0.03917 -0.165 0.022 1.000 0.719 1.000 35.147 -0.141 0.370 9.5 1.323 0.04740 -0.176 0.018 1.000 0.578 1.000 27.913 0.125 0.383 10.0 1.217 0.06917 -0.185 0.016 1.000 0.051 1.000 17.599 0.091 0.402 10.5 1.252 0.07365 -0.187 0.015 1.000 0.045 1.000 17.005 0.329 0.400 11.0 1.286 0.07831 -0.190 0.014 1.000 0.039 1.000 16.417 0.514 0.398 11.5 1.287 0.08245 -0.197 0.004 1.000 0.162 1.000 15.614 0.481 0.403 12.0 1.318 0.08763 -0.198 0.001 1.000 0.084 1.000 15.045 0.286 0.400 12.5 1.356 0.09254 -0.199 0.001 1.000 0.046 1.000 14.649 0.271 0.397 13.0 1.427 0.08947 -0.200 0.001 1.000 0.004 1.000 15.949 0.288 0.390 13.5 1.449 0.09553 -0.203 0.001 1.000 0.002 1.000 15.164 0.397 0.390 14.0 1.464 0.10260 -0.205 0.001 1.000 0.001 1.000 14.273 0.471 0.390 14.5 1.474 0.10860 -0.208 0.001 1.000 0.001 1.000 13.571 0.610 0.391 15.0 1.480 0.11763 -0.211 0.001 1.000 0.001 1.000 12.581 0.709 0.393 Name = WORTMANN FX 60-126 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 -0.432 0.15060 -0.045 0.888 0.002 0.948 0.004 -2.867 0.429 0.146 -14.5 -0.418 0.13617 -0.047 0.879 0.002 0.950 0.003 -3.066 0.418 0.136 -14.0 -0.401 0.12393 -0.050 0.872 0.002 0.951 0.003 -3.238 0.397 0.125 -13.5 -0.383 0.11989 -0.053 0.864 0.002 0.952 0.003 -3.193 0.382 0.113 -13.0 -0.362 0.10708 -0.055 0.857 0.002 0.953 0.003 -3.385 0.370 0.098 -12.5 -0.340 0.09738 -0.058 0.848 0.002 0.954 0.003 -3.491 0.360 0.080 -12.0 -0.316 0.09095 -0.060 0.836 0.002 0.956 0.003 -3.469 0.353 0.059 -11.5 -0.289 0.08158 -0.063 0.827 0.002 0.958 0.003 -3.545 0.346 0.032 -11.0 -0.261 0.07575 -0.066 0.820 0.002 0.958 0.003 -3.444 0.341 -0.001 -10.5 -0.231 0.06818 -0.068 0.814 0.002 0.958 0.003 -3.390 0.336 -0.045 -10.0 -0.200 0.06313 -0.071 0.808 0.002 0.959 0.003 -3.162 0.332 -0.105 -9.5 -0.167 0.05868 -0.074 0.799 0.002 0.959 0.003 -2.840 0.330 -0.191 -9.0 -0.133 0.05417 -0.076 0.789 0.002 0.961 0.003 -2.449 0.327 -0.325 -8.5 -0.097 0.05028 -0.079 0.780 0.002 0.962 0.003 -1.930 0.324 -0.563 -8.0 -0.060 0.04612 -0.082 0.773 0.002 0.962 0.003 -1.304 0.322 -1.106 -7.5 -0.023 0.04265 -0.084 0.767 0.003 0.961 0.004 -0.528 0.228 -3.490 -7.0 -0.309 0.03940 -0.087 0.761 0.003 0.960 0.004 -7.841 0.225 -0.032 -6.5 -0.244 0.03657 -0.090 0.755 0.003 0.959 0.004 -6.664 0.291 -0.118 -6.0 -0.178 0.03416 -0.092 0.747 0.003 0.959 0.006 -5.222 0.333 -0.268 -5.5 -0.068 0.01796 -0.104 0.732 0.004 0.962 0.750 -3.813 0.351 -1.273 -5.0 -0.025 0.01740 -0.108 0.719 0.031 0.963 0.787 -1.451 0.411 -4.023 -4.5 0.015 0.01676 -0.118 0.709 0.033 0.963 0.952 0.883 0.369 8.200 -4.0 0.074 0.01638 -0.120 0.701 0.034 0.962 0.976 4.547 0.276 1.858 -3.5 0.134 0.01603 -0.121 0.692 0.037 0.961 0.984 8.380 0.266 1.149 -3.0 0.194 0.01586 -0.122 0.660 0.066 0.967 0.986 12.257 0.262 0.876 -2.5 0.254 0.01510 -0.122 0.648 0.296 0.967 0.984 16.842 0.262 0.731 -2.0 0.314 0.01504 -0.123 0.637 0.303 0.967 0.988 20.890 0.263 0.642 -1.5 0.374 0.01509 -0.124 0.590 0.343 0.975 0.989 24.791 0.262 0.581 -1.0 0.434 0.01621 -0.125 0.528 0.349 0.980 0.992 26.777 0.262 0.537 -0.5 0.494 0.01722 -0.125 0.518 0.355 0.980 0.994 28.678 0.262 0.503 0.0 0.544 0.01819 -0.126 0.507 0.361 0.980 0.996 29.919 0.263 0.481 0.5 0.605 0.01942 -0.127 0.459 0.368 0.983 0.999 31.169 0.262 0.459 1.0 0.665 0.01988 -0.127 0.451 0.388 0.983 1.000 33.431 0.263 0.442 1.5 0.723 0.01784 -0.128 0.442 0.406 0.982 1.000 40.559 0.258 0.427 2.0 0.793 0.01749 -0.128 0.398 0.412 1.000 1.000 45.350 0.257 0.412 2.5 0.853 0.01441 -0.129 0.389 0.419 1.000 1.000 59.167 0.261 0.401 3.0 0.912 0.01179 -0.130 0.339 0.426 1.000 1.000 77.346 0.261 0.392 3.5 0.972 0.00968 -0.130 0.330 0.434 1.000 1.000 100.393 0.261 0.384 4.0 1.031 0.00909 -0.131 0.083 0.477 1.000 1.000 113.433 0.261 0.377 4.5 1.090 0.00827 -0.132 0.082 0.486 1.000 1.000 131.803 0.295 0.371 5.0 1.121 0.02395 -0.135 0.080 0.495 0.958 1.000 46.791 0.321 0.371 5.5 1.166 0.02521 -0.137 0.049 0.537 0.941 1.000 46.272 0.297 0.368 6.0 1.211 0.02630 -0.139 0.047 0.547 0.925 1.000 46.063 0.301 0.365 6.5 1.256 0.02733 -0.142 0.046 0.557 0.909 1.000 45.953 0.306 0.363 7.0 1.299 0.02842 -0.144 0.044 0.600 0.892 1.000 45.711 0.325 0.361 7.5 1.335 0.02947 -0.148 0.042 0.617 0.867 1.000 45.295 0.351 0.361 8.0 1.369 0.03069 -0.151 0.041 1.000 0.842 1.000 44.610 0.356 0.361 8.5 1.403 0.03201 -0.155 0.026 1.000 0.818 1.000 43.836 0.381 0.360 9.0 1.430 0.03351 -0.159 0.022 1.000 0.787 1.000 42.677 0.470 0.361 9.5 1.447 0.03658 -0.164 0.018 1.000 0.748 1.000 39.558 -73.401 0.364 10.0 1.430 0.04174 -0.173 0.016 1.000 0.668 1.000 34.256 0.083 0.371 10.5 1.299 0.05847 -0.189 0.015 1.000 0.399 1.000 22.211 0.133 0.396 11.0 1.280 0.07292 -0.190 0.014 1.000 0.048 1.000 17.548 0.291 0.399 11.5 1.400 0.06160 -0.193 0.004 1.000 0.453 1.000 22.719 0.362 0.388 12.0 1.364 0.07293 -0.200 0.001 1.000 0.329 1.000 18.705 0.113 0.397 12.5 1.338 0.08726 -0.202 0.001 1.000 0.121 1.000 15.330 0.503 0.401 13.0 1.373 0.09219 -0.202 0.001 1.000 0.050 1.000 14.896 0.259 0.397 13.5 1.442 0.08847 -0.203 0.001 1.000 0.004 1.000 16.302 0.287 0.391 14.0 1.460 0.09422 -0.205 0.001 1.000 0.002 1.000 15.498 0.437 0.391 14.5 1.472 0.10001 -0.208 0.001 1.000 0.002 1.000 14.713 0.552 0.391 15.0 1.479 0.10745 -0.211 0.001 1.000 0.001 1.000 13.761 0.642 0.393 Name = WORTMANN FX 60-126 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 -0.432 0.14060 -0.045 0.888 0.002 0.951 0.004 -3.069 0.429 0.146 -14.5 -0.417 0.12840 -0.047 0.879 0.002 0.953 0.004 -3.250 0.418 0.136 -14.0 -0.401 0.11792 -0.050 0.872 0.002 0.954 0.003 -3.401 0.398 0.125 -13.5 -0.383 0.10689 -0.053 0.864 0.002 0.955 0.003 -3.581 0.383 0.113 -13.0 -0.362 0.09678 -0.055 0.857 0.002 0.956 0.003 -3.746 0.370 0.098 -12.5 -0.340 0.09055 -0.058 0.848 0.002 0.958 0.003 -3.752 0.360 0.080 -12.0 -0.316 0.08258 -0.060 0.836 0.002 0.961 0.003 -3.820 0.353 0.059 -11.5 -0.289 0.07666 -0.063 0.827 0.002 0.963 0.003 -3.771 0.346 0.032 -11.0 -0.261 0.06967 -0.066 0.820 0.002 0.963 0.003 -3.744 0.341 -0.001 -10.5 -0.231 0.06471 -0.068 0.814 0.002 0.963 0.003 -3.569 0.336 -0.045 -10.0 -0.200 0.06003 -0.071 0.808 0.002 0.964 0.003 -3.323 0.333 -0.105 -9.5 -0.167 0.05476 -0.074 0.799 0.002 0.964 0.003 -3.043 0.330 -0.191 -9.0 -0.132 0.05156 -0.076 0.789 0.002 0.965 0.003 -2.570 0.327 -0.325 -8.5 -0.097 0.04720 -0.079 0.780 0.002 0.966 0.003 -2.056 0.324 -0.563 -8.0 -0.060 0.04346 -0.082 0.773 0.002 0.967 0.003 -1.384 0.322 -1.106 -7.5 -0.022 0.04061 -0.084 0.767 0.003 0.967 0.004 -0.551 0.228 -3.517 -7.0 -0.309 0.03780 -0.087 0.761 0.003 0.967 0.004 -8.172 0.225 -0.032 -6.5 -0.244 0.03502 -0.090 0.755 0.003 0.966 0.004 -6.959 0.291 -0.118 -6.0 -0.178 0.03278 -0.092 0.747 0.003 0.967 0.007 -5.441 0.353 -0.268 -5.5 -0.081 0.01623 -0.106 0.732 0.004 0.969 0.792 -5.011 0.420 -1.058 -5.0 -0.045 0.01565 -0.115 0.719 0.031 0.970 0.924 -2.844 0.377 -2.336 -4.5 0.015 0.01524 -0.119 0.709 0.033 0.970 0.968 0.972 0.291 8.261 -4.0 0.074 0.01487 -0.120 0.701 0.034 0.971 0.981 5.008 0.269 1.861 -3.5 0.134 0.01459 -0.121 0.692 0.037 0.970 0.985 9.212 0.264 1.150 -3.0 0.194 0.01436 -0.122 0.660 0.066 0.975 0.987 13.530 0.262 0.876 -2.5 0.254 0.01339 -0.122 0.648 0.296 0.976 0.988 18.999 0.262 0.731 -2.0 0.314 0.01353 -0.123 0.637 0.303 0.976 0.991 23.233 0.262 0.642 -1.5 0.374 0.01407 -0.124 0.590 0.343 0.981 0.991 26.603 0.262 0.581 -1.0 0.434 0.01525 -0.125 0.528 0.349 0.984 0.993 28.470 0.262 0.537 -0.5 0.494 0.01608 -0.125 0.518 0.355 0.985 0.995 30.719 0.262 0.503 0.0 0.547 0.01701 -0.126 0.507 0.361 0.985 0.997 32.153 0.262 0.480 0.5 0.608 0.01821 -0.127 0.459 0.368 0.988 0.999 33.372 0.261 0.458 1.0 0.669 0.01809 -0.127 0.451 0.388 0.991 1.000 36.956 0.261 0.440 1.5 0.730 0.01656 -0.128 0.442 0.406 0.995 1.000 44.109 0.259 0.425 2.0 0.793 0.01671 -0.128 0.398 0.412 1.000 1.000 47.450 0.260 0.412 2.5 0.853 0.01337 -0.129 0.389 0.419 1.000 1.000 63.793 0.261 0.401 3.0 0.912 0.01074 -0.130 0.339 0.426 1.000 1.000 84.910 0.261 0.392 3.5 0.972 0.00882 -0.130 0.330 0.434 1.000 1.000 110.141 0.261 0.384 4.0 1.031 0.00846 -0.131 0.083 0.477 1.000 1.000 121.926 0.261 0.377 4.5 1.090 0.00770 -0.132 0.082 0.486 1.000 1.000 141.560 0.261 0.371 5.0 1.149 0.00675 -0.132 0.080 0.495 1.000 1.000 170.361 0.285 0.365 5.5 1.187 0.02497 -0.135 0.049 0.537 0.971 1.000 47.548 0.326 0.364 6.0 1.224 0.02579 -0.138 0.047 0.547 0.943 1.000 47.483 0.317 0.363 6.5 1.268 0.02671 -0.141 0.046 0.557 0.925 1.000 47.459 0.307 0.361 7.0 1.311 0.02782 -0.143 0.044 0.600 0.908 1.000 47.140 0.312 0.359 7.5 1.353 0.02892 -0.146 0.042 0.617 0.890 1.000 46.775 0.330 0.358 8.0 1.389 0.03018 -0.149 0.041 1.000 0.866 1.000 46.014 0.352 0.357 8.5 1.422 0.03147 -0.153 0.026 1.000 0.842 1.000 45.200 0.369 0.357 9.0 1.453 0.03256 -0.157 0.022 1.000 0.815 1.000 44.638 0.409 0.358 9.5 1.476 0.03350 -0.161 0.018 1.000 0.784 1.000 44.063 0.513 0.359 10.0 1.491 0.03627 -0.167 0.016 1.000 0.746 1.000 41.106 -17.724 0.362 10.5 1.475 0.04120 -0.175 0.015 1.000 0.672 1.000 35.812 0.061 0.369 11.0 1.366 0.05512 -0.190 0.014 1.000 0.455 1.000 24.785 -4.121 0.389 11.5 1.472 0.05205 -0.188 0.004 1.000 0.564 1.000 28.290 0.328 0.377 12.0 1.437 0.06124 -0.196 0.001 1.000 0.462 1.000 23.467 0.072 0.386 12.5 1.385 0.07456 -0.203 0.001 1.000 0.315 1.000 18.577 0.135 0.397 13.0 1.359 0.08871 -0.205 0.001 1.000 0.120 1.000 15.318 0.629 0.401 13.5 1.390 0.09370 -0.205 0.001 1.000 0.050 1.000 14.836 0.258 0.398 14.0 1.454 0.09009 -0.205 0.001 1.000 0.004 1.000 16.138 0.292 0.391 14.5 1.466 0.09531 -0.208 0.001 1.000 0.003 1.000 15.383 0.489 0.392 15.0 1.477 0.10073 -0.211 0.001 1.000 0.002 1.000 14.662 0.502 0.393