Name = EPPLER 793 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 -0.459 0.14781 -0.054 0.966 0.007 0.976 0.008 -3.106 0.349 0.133 -14.5 -0.432 0.14512 -0.056 0.964 0.006 0.976 0.008 -2.973 0.346 0.119 -14.0 -0.402 0.12979 -0.059 0.962 0.006 0.976 0.008 -3.100 0.339 0.103 -13.5 -0.371 0.12185 -0.062 0.961 0.007 0.975 0.008 -3.043 0.337 0.083 -13.0 -0.339 0.11476 -0.065 0.960 0.006 0.975 0.008 -2.958 0.335 0.059 -12.5 -0.306 0.10358 -0.067 0.959 0.007 0.974 0.008 -2.952 0.331 0.029 -12.0 -0.271 0.09722 -0.070 0.957 0.007 0.974 0.009 -2.789 0.330 -0.009 -11.5 -0.236 0.09111 -0.073 0.956 0.007 0.973 0.009 -2.589 0.328 -0.060 -11.0 -0.199 0.08529 -0.076 0.954 0.007 0.971 0.009 -2.337 0.326 -0.131 -10.5 -0.162 0.08009 -0.079 0.950 0.008 0.971 0.009 -2.021 0.326 -0.236 -10.0 -0.124 0.07459 -0.082 0.891 0.007 0.974 0.009 -1.668 0.324 -0.406 -9.5 -0.085 0.06943 -0.084 0.843 0.008 0.976 0.010 -1.220 0.322 -0.746 -9.0 -0.045 0.06469 -0.087 0.798 0.008 0.978 0.010 -0.699 0.322 -1.681 -8.5 -0.005 0.06102 -0.090 0.765 0.009 0.978 0.011 -0.078 0.232 -18.687 -8.0 -0.362 0.05718 -0.093 0.734 0.009 0.979 0.012 -6.329 0.230 -0.007 -7.5 -0.293 0.05410 -0.096 0.701 0.009 0.979 0.013 -5.407 0.292 -0.078 -7.0 -0.224 0.05103 -0.099 0.672 0.010 0.979 0.013 -4.381 0.292 -0.192 -6.5 -0.155 0.04807 -0.102 0.645 0.011 0.978 0.016 -3.226 0.289 -0.406 -6.0 -0.087 0.04676 -0.104 0.617 0.013 0.977 0.041 -1.859 0.318 -0.948 -5.5 -0.019 0.02980 -0.111 0.590 0.014 0.977 0.600 -0.636 0.287 -5.609 -5.0 0.045 0.03727 -0.109 0.566 0.141 0.976 0.378 1.210 0.260 2.669 -4.5 0.109 0.03623 -0.112 0.542 0.176 0.975 0.380 3.011 0.302 1.280 -4.0 0.172 0.03474 -0.116 0.516 0.199 0.974 0.397 4.959 0.304 0.921 -3.5 0.235 0.03321 -0.119 0.492 0.220 0.973 0.419 7.069 0.305 0.757 -3.0 0.297 0.03189 -0.122 0.470 0.238 0.969 0.445 9.297 0.306 0.663 -2.5 0.357 0.03072 -0.126 0.449 0.256 0.966 0.474 11.633 0.307 0.602 -2.0 0.417 0.02934 -0.129 0.431 0.269 0.960 0.522 14.226 0.309 0.560 -1.5 0.477 0.02817 -0.133 0.416 0.280 0.954 0.587 16.921 0.308 0.529 -1.0 0.536 0.02736 -0.136 0.400 0.292 0.932 0.668 19.582 0.304 0.504 -0.5 0.594 0.02698 -0.139 0.388 0.305 0.889 0.772 22.000 0.433 0.485 0.0 0.564 0.02860 -0.141 0.376 0.324 0.847 0.884 19.716 1.345 0.501 0.5 0.597 0.03001 -0.143 0.366 0.343 0.801 0.995 19.911 0.315 0.490 1.0 0.632 0.03186 -0.146 0.356 0.365 0.759 0.997 19.844 0.320 0.481 1.5 0.670 0.03366 -0.148 0.343 0.388 0.724 0.997 19.904 0.326 0.472 2.0 0.706 0.03572 -0.151 0.331 0.414 0.689 0.997 19.766 0.336 0.464 2.5 0.741 0.03788 -0.155 0.321 0.444 0.653 0.997 19.562 0.343 0.459 3.0 0.777 0.04004 -0.158 0.310 0.476 0.619 0.997 19.395 0.343 0.453 3.5 0.814 0.04241 -0.161 0.299 0.509 0.591 0.997 19.191 0.341 0.448 4.0 0.852 0.04471 -0.165 0.289 0.544 0.564 0.998 19.052 0.346 0.443 4.5 0.888 0.04718 -0.168 0.280 0.584 0.535 0.998 18.815 0.353 0.440 5.0 0.923 0.05000 -0.172 0.272 0.632 0.507 0.998 18.462 0.348 0.436 5.5 0.962 0.05236 -0.176 0.262 0.686 0.487 0.998 18.374 0.341 0.433 6.0 1.002 0.05487 -0.179 0.252 0.773 0.468 0.997 18.256 0.343 0.429 6.5 1.039 0.05686 -0.183 0.243 0.997 0.449 0.997 18.280 0.344 0.426 7.0 1.079 0.05986 -0.187 0.234 0.997 0.433 0.997 18.022 0.343 0.423 7.5 1.117 0.06311 -0.190 0.225 0.997 0.416 0.997 17.697 0.344 0.420 8.0 1.155 0.06627 -0.194 0.215 0.997 0.402 0.997 17.435 0.343 0.418 8.5 1.194 0.06962 -0.197 0.205 0.996 0.389 0.997 17.151 0.342 0.415 9.0 1.233 0.07326 -0.201 0.196 0.996 0.377 0.997 16.824 0.344 0.413 9.5 1.270 0.07687 -0.204 0.186 0.996 0.365 0.997 16.518 0.343 0.411 10.0 1.308 0.08049 -0.208 0.172 0.996 0.358 0.997 16.250 0.344 0.409 10.5 1.344 0.08445 -0.211 0.160 0.996 0.348 0.997 15.914 0.318 0.407 11.0 1.399 0.08609 -0.214 0.123 0.997 0.378 0.997 16.257 0.305 0.403 11.5 1.447 0.08906 -0.217 0.088 0.997 0.392 0.997 16.243 0.327 0.400 12.0 1.481 0.09283 -0.220 0.063 0.997 0.389 0.997 15.950 0.374 0.399 12.5 1.504 0.09816 -0.224 0.048 0.997 0.373 0.997 15.322 0.444 0.399 13.0 1.520 0.10420 -0.228 0.037 0.997 0.349 0.997 14.588 0.557 0.400 13.5 1.530 0.11134 -0.232 0.027 0.997 0.316 0.997 13.738 0.646 0.402 14.0 1.539 0.11837 -0.236 0.017 0.997 0.285 0.997 13.005 -1.413 0.403 14.5 1.526 0.13103 -0.238 0.014 0.997 0.168 0.997 11.644 0.359 0.406 15.0 1.561 0.13524 -0.238 0.011 0.997 0.065 0.997 11.543 0.242 0.402 Name = EPPLER 793 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 -0.459 0.11734 -0.054 0.966 0.007 0.977 0.008 -3.912 0.349 0.133 -14.5 -0.432 0.11405 -0.056 0.964 0.006 0.976 0.008 -3.783 0.345 0.119 -14.0 -0.402 0.10792 -0.059 0.962 0.006 0.976 0.008 -3.725 0.338 0.103 -13.5 -0.370 0.10119 -0.062 0.961 0.007 0.976 0.009 -3.661 0.337 0.083 -13.0 -0.339 0.09599 -0.065 0.960 0.006 0.975 0.008 -3.533 0.335 0.059 -12.5 -0.305 0.08730 -0.067 0.959 0.007 0.974 0.009 -3.498 0.331 0.029 -12.0 -0.271 0.08177 -0.070 0.957 0.007 0.974 0.009 -3.312 0.330 -0.009 -11.5 -0.236 0.07730 -0.073 0.956 0.007 0.974 0.009 -3.047 0.328 -0.060 -11.0 -0.199 0.07221 -0.076 0.954 0.007 0.973 0.009 -2.755 0.326 -0.131 -10.5 -0.161 0.06803 -0.079 0.950 0.008 0.973 0.010 -2.373 0.326 -0.237 -10.0 -0.124 0.06462 -0.082 0.891 0.007 0.977 0.010 -1.913 0.324 -0.409 -9.5 -0.084 0.05933 -0.084 0.843 0.008 0.981 0.010 -1.421 0.322 -0.751 -9.0 -0.044 0.05632 -0.087 0.798 0.008 0.983 0.011 -0.788 0.322 -1.715 -8.5 -0.004 0.05307 -0.090 0.765 0.009 0.984 0.012 -0.074 0.232 -22.634 -8.0 -0.362 0.04964 -0.093 0.734 0.009 0.985 0.012 -7.289 0.230 -0.007 -7.5 -0.293 0.04697 -0.096 0.701 0.009 0.987 0.013 -6.227 0.292 -0.078 -7.0 -0.224 0.04430 -0.099 0.672 0.010 0.987 0.014 -5.047 0.288 -0.192 -6.5 -0.148 0.02997 -0.101 0.645 0.011 0.987 0.469 -4.935 0.335 -0.436 -6.0 -0.082 0.02356 -0.111 0.617 0.013 0.987 0.666 -3.472 0.369 -1.106 -5.5 -0.019 0.02183 -0.117 0.590 0.014 0.987 0.742 -0.856 0.276 -5.995 -5.0 0.044 0.02356 -0.114 0.566 0.141 0.986 0.615 1.878 0.252 2.832 -4.5 0.107 0.02289 -0.117 0.542 0.176 0.985 0.618 4.680 0.301 1.342 -4.0 0.169 0.02186 -0.121 0.516 0.199 0.985 0.653 7.747 0.310 0.962 -3.5 0.231 0.02084 -0.124 0.492 0.220 0.984 0.702 11.077 0.314 0.789 -3.0 0.292 0.02015 -0.128 0.470 0.238 0.983 0.765 14.478 0.315 0.690 -2.5 0.352 0.01986 -0.132 0.449 0.256 0.982 0.837 17.715 0.320 0.626 -2.0 0.411 0.01996 -0.137 0.431 0.269 0.981 0.955 20.569 0.303 0.583 -1.5 0.472 0.02052 -0.139 0.416 0.280 0.979 0.996 22.979 0.273 0.544 -1.0 0.533 0.02133 -0.140 0.400 0.292 0.977 0.997 24.968 0.265 0.512 -0.5 0.594 0.02202 -0.140 0.388 0.305 0.975 0.997 26.959 0.268 0.487 0.0 0.635 0.02272 -0.141 0.376 0.324 0.973 0.997 27.949 0.270 0.473 0.5 0.691 0.02337 -0.142 0.366 0.343 0.967 0.997 29.577 0.270 0.456 1.0 0.747 0.02399 -0.144 0.356 0.365 0.961 0.998 31.151 0.272 0.442 1.5 0.803 0.02470 -0.145 0.343 0.388 0.956 0.998 32.510 0.276 0.430 2.0 0.853 0.02526 -0.146 0.331 0.414 0.941 0.998 33.753 0.291 0.422 2.5 0.892 0.02606 -0.149 0.321 0.444 0.912 0.998 34.241 0.313 0.417 3.0 0.928 0.02707 -0.151 0.310 0.476 0.878 0.998 34.290 0.325 0.413 3.5 0.965 0.02825 -0.154 0.299 0.509 0.846 0.998 34.155 0.333 0.410 4.0 1.000 0.02950 -0.157 0.289 0.544 0.814 0.998 33.903 0.350 0.407 4.5 1.032 0.03118 -0.161 0.280 0.584 0.777 0.998 33.097 0.368 0.406 5.0 1.063 0.03283 -0.165 0.272 0.632 0.741 0.998 32.361 0.368 0.405 5.5 1.096 0.03460 -0.168 0.262 0.686 0.710 0.998 31.668 0.364 0.404 6.0 1.129 0.03636 -0.172 0.252 0.773 0.681 0.998 31.052 0.370 0.402 6.5 1.161 0.03770 -0.176 0.243 0.997 0.651 0.997 30.791 0.377 0.402 7.0 1.192 0.04034 -0.180 0.234 0.997 0.622 0.997 29.555 0.382 0.401 7.5 1.223 0.04326 -0.184 0.225 0.997 0.593 0.997 28.265 0.374 0.401 8.0 1.257 0.04598 -0.188 0.215 0.997 0.571 0.997 27.335 0.370 0.400 8.5 1.289 0.04908 -0.192 0.205 0.996 0.548 0.997 26.265 0.374 0.399 9.0 1.322 0.05222 -0.196 0.196 0.996 0.526 0.997 25.306 0.370 0.398 9.5 1.354 0.05545 -0.200 0.186 0.996 0.507 0.997 24.426 0.358 0.398 10.0 1.391 0.05851 -0.204 0.172 0.996 0.495 0.997 23.771 0.353 0.396 10.5 1.425 0.06182 -0.207 0.160 0.996 0.482 0.997 23.059 0.306 0.395 11.0 1.489 0.06314 -0.209 0.123 0.997 0.512 0.997 23.576 0.293 0.390 11.5 1.533 0.06627 -0.212 0.088 0.997 0.516 0.997 23.131 0.339 0.388 12.0 1.562 0.07034 -0.216 0.063 0.997 0.506 0.997 22.206 0.403 0.388 12.5 1.583 0.07513 -0.220 0.048 0.997 0.487 0.997 21.070 0.470 0.389 13.0 1.600 0.08013 -0.224 0.037 0.997 0.466 0.997 19.962 0.534 0.390 13.5 1.613 0.08577 -0.228 0.027 0.997 0.444 0.997 18.803 0.558 0.391 14.0 1.626 0.09120 -0.232 0.017 0.997 0.426 0.997 17.832 0.876 0.393 14.5 1.626 0.09846 -0.237 0.014 0.997 0.393 0.997 16.517 10.430 0.395 15.0 1.627 0.10535 -0.241 0.011 0.997 0.364 0.997 15.444 5.455 0.398 Name = EPPLER 793 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 -0.459 0.10828 -0.054 0.966 0.007 0.977 0.008 -4.236 0.349 0.133 -14.5 -0.431 0.10462 -0.056 0.964 0.006 0.976 0.008 -4.122 0.345 0.119 -14.0 -0.402 0.09867 -0.059 0.962 0.006 0.976 0.008 -4.071 0.339 0.103 -13.5 -0.370 0.08903 -0.062 0.961 0.007 0.976 0.009 -4.161 0.338 0.083 -13.0 -0.339 0.08511 -0.065 0.960 0.006 0.976 0.008 -3.985 0.335 0.059 -12.5 -0.305 0.08033 -0.067 0.959 0.007 0.975 0.009 -3.797 0.330 0.029 -12.0 -0.270 0.07506 -0.070 0.957 0.007 0.974 0.009 -3.603 0.330 -0.009 -11.5 -0.235 0.07131 -0.073 0.956 0.007 0.974 0.009 -3.298 0.328 -0.060 -11.0 -0.199 0.06651 -0.076 0.954 0.007 0.973 0.010 -2.986 0.326 -0.132 -10.5 -0.161 0.06276 -0.079 0.950 0.008 0.973 0.010 -2.567 0.326 -0.238 -10.0 -0.123 0.05935 -0.082 0.891 0.007 0.979 0.010 -2.077 0.324 -0.411 -9.5 -0.084 0.05566 -0.084 0.843 0.008 0.984 0.011 -1.501 0.322 -0.760 -9.0 -0.044 0.05210 -0.087 0.798 0.008 0.987 0.011 -0.844 0.322 -1.733 -8.5 -0.004 0.04907 -0.090 0.765 0.009 0.989 0.012 -0.072 0.232 -25.296 -8.0 -0.362 0.04637 -0.093 0.734 0.009 0.989 0.013 -7.803 0.230 -0.007 -7.5 -0.292 0.04379 -0.096 0.701 0.009 0.989 0.014 -6.680 0.291 -0.078 -7.0 -0.223 0.04208 -0.099 0.672 0.010 0.990 0.022 -5.308 0.300 -0.192 -6.5 -0.039 0.02174 -0.108 0.645 0.011 0.990 0.666 -1.807 0.327 -2.511 -6.0 -0.017 0.01991 -0.114 0.617 0.013 0.990 0.740 -0.856 0.810 -6.469 -5.5 -0.019 0.01879 -0.120 0.590 0.014 0.990 0.808 -0.989 0.360 -6.212 -5.0 0.044 0.01814 -0.121 0.566 0.141 0.989 0.791 2.402 0.287 3.031 -4.5 0.105 0.01757 -0.125 0.542 0.176 0.989 0.825 6.000 0.314 1.432 -4.0 0.167 0.01715 -0.129 0.516 0.199 0.989 0.886 9.718 0.323 1.024 -3.5 0.227 0.01708 -0.134 0.492 0.220 0.989 0.958 13.272 0.307 0.839 -3.0 0.288 0.01727 -0.136 0.470 0.238 0.988 0.995 16.685 0.278 0.722 -2.5 0.349 0.01786 -0.137 0.449 0.256 0.987 0.996 19.556 0.265 0.642 -2.0 0.411 0.01837 -0.138 0.431 0.269 0.986 0.997 22.343 0.264 0.586 -1.5 0.472 0.01890 -0.139 0.416 0.280 0.985 0.997 24.955 0.265 0.544 -1.0 0.533 0.01944 -0.140 0.400 0.292 0.984 0.997 27.401 0.265 0.512 -0.5 0.594 0.01994 -0.140 0.388 0.305 0.982 0.998 29.770 0.267 0.487 0.0 0.640 0.02042 -0.141 0.376 0.324 0.980 0.998 31.361 0.268 0.471 0.5 0.699 0.02077 -0.142 0.366 0.343 0.978 0.997 33.667 0.268 0.454 1.0 0.758 0.02134 -0.143 0.356 0.365 0.976 0.998 35.511 0.268 0.439 1.5 0.816 0.02170 -0.145 0.343 0.388 0.974 0.998 37.615 0.269 0.427 2.0 0.874 0.02230 -0.146 0.331 0.414 0.971 0.998 39.178 0.271 0.417 2.5 0.929 0.02267 -0.147 0.321 0.444 0.965 0.998 40.984 0.274 0.408 3.0 0.984 0.02327 -0.148 0.310 0.476 0.959 0.998 42.304 0.276 0.401 3.5 1.038 0.02370 -0.150 0.299 0.509 0.953 0.998 43.818 0.287 0.394 4.0 1.082 0.02440 -0.152 0.289 0.544 0.933 0.998 44.340 0.312 0.390 4.5 1.119 0.02523 -0.155 0.280 0.584 0.904 0.998 44.376 0.334 0.388 5.0 1.155 0.02623 -0.158 0.272 0.632 0.874 0.998 44.016 0.345 0.387 5.5 1.190 0.02730 -0.162 0.262 0.686 0.844 0.998 43.572 0.352 0.386 6.0 1.224 0.02830 -0.165 0.252 0.773 0.814 0.998 43.240 0.363 0.385 6.5 1.256 0.02886 -0.169 0.243 0.997 0.785 0.997 43.517 0.375 0.385 7.0 1.287 0.03083 -0.173 0.234 0.997 0.754 0.997 41.752 0.385 0.384 7.5 1.317 0.03310 -0.177 0.225 0.997 0.724 0.997 39.806 0.385 0.385 8.0 1.349 0.03543 -0.181 0.215 0.997 0.698 0.997 38.068 0.387 0.385 8.5 1.379 0.03799 -0.186 0.205 0.996 0.671 0.997 36.292 0.394 0.385 9.0 1.408 0.04078 -0.190 0.196 0.996 0.645 0.997 34.522 0.393 0.385 9.5 1.438 0.04361 -0.194 0.186 0.996 0.621 0.997 32.972 0.380 0.385 10.0 1.470 0.04648 -0.198 0.172 0.996 0.603 0.997 31.636 0.377 0.385 10.5 1.501 0.04959 -0.202 0.160 0.996 0.584 0.997 30.265 0.328 0.385 11.0 1.552 0.05205 -0.204 0.123 0.997 0.593 0.997 29.812 0.319 0.382 11.5 1.586 0.05597 -0.208 0.088 0.997 0.583 0.997 28.331 0.385 0.381 12.0 1.609 0.06028 -0.212 0.063 0.997 0.564 0.997 26.691 0.463 0.382 12.5 1.626 0.06497 -0.217 0.048 0.997 0.542 0.997 25.026 0.530 0.383 13.0 1.640 0.06974 -0.221 0.037 0.997 0.519 0.997 23.523 0.594 0.385 13.5 1.652 0.07502 -0.225 0.027 0.997 0.495 0.997 22.020 0.640 0.386 14.0 1.663 0.08040 -0.230 0.017 0.997 0.474 0.997 20.681 0.906 0.388 14.5 1.665 0.08652 -0.234 0.014 0.997 0.447 0.997 19.249 1.541 0.391 15.0 1.670 0.09237 -0.239 0.011 0.997 0.424 0.997 18.076 1.243 0.393 Name = EPPLER 793 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 -0.459 0.09932 -0.054 0.966 0.007 0.977 0.008 -4.619 0.349 0.133 -14.5 -0.431 0.09566 -0.056 0.964 0.006 0.977 0.008 -4.508 0.344 0.119 -14.0 -0.401 0.09332 -0.059 0.962 0.006 0.976 0.008 -4.301 0.338 0.103 -13.5 -0.370 0.08436 -0.062 0.961 0.007 0.976 0.009 -4.387 0.338 0.083 -13.0 -0.339 0.08080 -0.065 0.960 0.006 0.976 0.008 -4.194 0.335 0.059 -12.5 -0.305 0.07624 -0.067 0.959 0.007 0.975 0.009 -3.997 0.330 0.029 -12.0 -0.270 0.07112 -0.070 0.957 0.007 0.975 0.010 -3.798 0.331 -0.010 -11.5 -0.235 0.06643 -0.073 0.956 0.007 0.974 0.009 -3.540 0.328 -0.060 -11.0 -0.198 0.06316 -0.076 0.954 0.007 0.974 0.010 -3.138 0.326 -0.132 -10.5 -0.161 0.05966 -0.079 0.950 0.008 0.974 0.010 -2.694 0.326 -0.239 -10.0 -0.123 0.05623 -0.081 0.891 0.007 0.982 0.010 -2.185 0.324 -0.413 -9.5 -0.083 0.05287 -0.084 0.843 0.008 0.987 0.011 -1.572 0.322 -0.765 -9.0 -0.043 0.05008 -0.087 0.798 0.008 0.989 0.012 -0.862 0.322 -1.770 -8.5 -0.003 0.04711 -0.090 0.765 0.009 0.990 0.013 -0.057 0.232 -33.049 -8.0 -0.362 0.04452 -0.093 0.734 0.009 0.991 0.014 -8.126 0.231 -0.007 -7.5 -0.292 0.04308 -0.096 0.701 0.009 0.992 0.026 -6.780 0.287 -0.077 -7.0 -0.070 0.02235 -0.104 0.672 0.010 0.992 0.619 -3.120 0.318 -1.238 -6.5 -0.063 0.01952 -0.111 0.645 0.011 0.992 0.719 -3.228 0.624 -1.514 -6.0 -0.034 0.01838 -0.117 0.617 0.013 0.992 0.786 -1.874 0.505 -3.146 -5.5 -0.019 0.01734 -0.122 0.590 0.014 0.992 0.851 -1.067 0.379 -6.368 -5.0 0.043 0.01630 -0.127 0.566 0.141 0.992 0.903 2.647 0.323 3.192 -4.5 0.104 0.01601 -0.131 0.542 0.176 0.992 0.960 6.495 0.309 1.514 -4.0 0.165 0.01579 -0.134 0.516 0.199 0.991 0.992 10.471 0.281 1.061 -3.5 0.227 0.01635 -0.135 0.492 0.220 0.991 0.996 13.867 0.266 0.846 -3.0 0.288 0.01660 -0.136 0.470 0.238 0.990 0.997 17.359 0.264 0.722 -2.5 0.349 0.01696 -0.137 0.449 0.256 0.989 0.997 20.598 0.264 0.642 -2.0 0.411 0.01741 -0.138 0.431 0.269 0.989 0.997 23.584 0.264 0.586 -1.5 0.472 0.01776 -0.139 0.416 0.280 0.988 0.997 26.553 0.265 0.544 -1.0 0.533 0.01809 -0.140 0.400 0.292 0.987 0.997 29.438 0.265 0.512 -0.5 0.594 0.01866 -0.140 0.388 0.305 0.985 0.998 31.817 0.266 0.487 0.0 0.643 0.01907 -0.141 0.376 0.324 0.984 0.998 33.721 0.267 0.470 0.5 0.702 0.01926 -0.142 0.366 0.343 0.982 0.997 36.478 0.267 0.453 1.0 0.761 0.01955 -0.143 0.356 0.365 0.980 0.998 38.937 0.268 0.438 1.5 0.820 0.02011 -0.144 0.343 0.388 0.979 0.998 40.774 0.268 0.426 2.0 0.878 0.02046 -0.146 0.331 0.414 0.976 0.998 42.945 0.269 0.416 2.5 0.937 0.02075 -0.147 0.321 0.444 0.974 0.998 45.140 0.270 0.407 3.0 0.994 0.02120 -0.148 0.310 0.476 0.972 0.998 46.914 0.272 0.399 3.5 1.049 0.02170 -0.149 0.299 0.509 0.966 0.998 48.355 0.275 0.392 4.0 1.104 0.02213 -0.151 0.289 0.544 0.961 0.998 49.882 0.277 0.386 4.5 1.158 0.02268 -0.152 0.280 0.584 0.955 0.998 51.058 0.287 0.381 5.0 1.203 0.02319 -0.154 0.272 0.632 0.938 0.998 51.881 0.310 0.378 5.5 1.243 0.02388 -0.157 0.262 0.686 0.915 0.998 52.042 0.330 0.377 6.0 1.279 0.02461 -0.160 0.252 0.773 0.889 0.998 51.991 0.345 0.375 6.5 1.314 0.02458 -0.164 0.243 0.997 0.861 0.997 53.486 0.361 0.375 7.0 1.347 0.02610 -0.168 0.234 0.997 0.832 0.997 51.608 0.373 0.375 7.5 1.379 0.02789 -0.172 0.225 0.997 0.804 0.997 49.440 0.377 0.375 8.0 1.411 0.02979 -0.176 0.215 0.997 0.777 0.997 47.353 0.385 0.375 8.5 1.440 0.03192 -0.180 0.205 0.996 0.749 0.997 45.135 0.396 0.375 9.0 1.470 0.03429 -0.185 0.196 0.996 0.722 0.997 42.863 0.403 0.376 9.5 1.498 0.03680 -0.189 0.186 0.996 0.696 0.997 40.693 0.397 0.376 10.0 1.528 0.03945 -0.193 0.172 0.996 0.674 0.997 38.727 0.396 0.376 10.5 1.556 0.04237 -0.198 0.160 0.996 0.652 0.997 36.713 0.360 0.377 11.0 1.595 0.04560 -0.201 0.123 0.997 0.646 0.997 34.985 0.363 0.376 11.5 1.621 0.04992 -0.205 0.088 0.997 0.626 0.997 32.469 0.453 0.376 12.0 1.639 0.05441 -0.210 0.063 0.997 0.601 0.997 30.124 0.527 0.378 12.5 1.654 0.05893 -0.214 0.048 0.997 0.576 0.997 28.073 0.590 0.379 13.0 1.666 0.06357 -0.219 0.037 0.997 0.551 0.997 26.215 0.653 0.381 13.5 1.677 0.06851 -0.224 0.027 0.997 0.527 0.997 24.483 0.733 0.383 14.0 1.685 0.07407 -0.228 0.017 0.997 0.503 0.997 22.753 0.963 0.385 14.5 1.690 0.07972 -0.233 0.014 0.997 0.478 0.997 21.201 1.412 0.388 15.0 1.693 0.08527 -0.237 0.011 0.997 0.455 0.997 19.855 1.777 0.390