Name = NACA M12 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 -0.790 0.19723 0.076 0.879 0.014 1.000 0.015 -4.004 0.429 0.346 -14.5 -0.772 0.18551 0.073 0.874 0.014 1.000 0.015 -4.162 0.408 0.344 -14.0 -0.750 0.17065 0.070 0.863 0.014 1.000 0.016 -4.394 0.388 0.343 -13.5 -0.726 0.16051 0.066 0.858 0.014 1.000 0.016 -4.525 0.381 0.341 -13.0 -0.701 0.16140 0.063 0.853 0.014 1.000 0.016 -4.346 0.376 0.340 -12.5 -0.676 0.13826 0.060 0.847 0.015 1.000 0.016 -4.886 0.373 0.339 -12.0 -0.648 0.13368 0.057 0.842 0.014 1.000 0.016 -4.851 0.366 0.338 -11.5 -0.620 0.11638 0.054 0.837 0.015 1.000 0.017 -5.326 0.362 0.336 -11.0 -0.590 0.11254 0.050 0.832 0.015 1.000 0.017 -5.245 0.361 0.335 -10.5 -0.560 0.10745 0.047 0.826 0.014 1.000 0.016 -5.213 0.359 0.334 -10.0 -0.529 0.09767 0.044 0.821 0.015 1.000 0.016 -5.415 0.355 0.332 -9.5 -0.497 0.09373 0.040 0.821 0.015 1.000 0.016 -5.297 0.352 0.331 -9.0 -0.463 0.08703 0.037 0.816 0.015 1.000 0.017 -5.323 0.350 0.330 -8.5 -0.429 0.07894 0.034 0.811 0.016 0.950 0.017 -5.437 0.348 0.328 -8.0 -0.394 0.07446 0.030 0.789 0.016 1.000 0.018 -5.298 0.347 0.326 -7.5 -0.359 0.07004 0.027 0.768 0.016 1.000 0.018 -5.127 0.347 0.324 -7.0 -0.324 0.06559 0.023 0.748 0.015 1.000 0.018 -4.933 0.346 0.322 -6.5 -0.287 0.06061 0.020 0.733 0.016 1.000 0.018 -4.739 0.344 0.319 -6.0 -0.250 0.05612 0.016 0.721 0.016 1.000 0.018 -4.461 0.343 0.315 -5.5 -0.213 0.05240 0.013 0.709 0.016 0.937 0.018 -4.062 0.342 0.311 -5.0 -0.175 0.04876 0.009 0.691 0.016 0.937 0.019 -3.590 0.342 0.304 -4.5 -0.137 0.04515 0.006 0.679 0.016 0.903 0.019 -3.032 0.341 0.293 -4.0 -0.098 0.04211 0.002 0.664 0.017 0.897 0.020 -2.333 0.341 0.274 -3.5 -0.059 0.03945 -0.001 0.645 0.017 0.894 0.020 -1.502 0.340 0.231 -3.0 -0.020 0.03700 -0.005 0.633 0.018 0.885 0.021 -0.536 0.166 0.014 -2.5 -0.143 0.03486 -0.008 0.621 0.019 0.876 0.023 -4.111 0.134 0.193 -2.0 -0.081 0.03288 -0.012 0.609 0.021 0.867 0.025 -2.471 0.355 0.105 -1.5 -0.020 0.02854 -0.021 0.594 0.023 0.858 0.957 -0.685 0.337 -0.837 -1.0 0.040 0.02936 -0.022 0.570 0.743 0.858 0.908 1.352 0.276 0.812 -0.5 0.099 0.02947 -0.024 0.542 0.765 0.858 0.914 3.358 0.312 0.495 0.0 0.102 0.02992 -0.026 0.518 0.792 0.855 0.908 3.422 0.321 0.506 0.5 0.158 0.03026 -0.028 0.494 0.808 0.852 0.911 5.205 0.293 0.431 1.0 0.210 0.03059 -0.031 0.473 0.814 0.842 0.931 6.866 0.295 0.397 1.5 0.264 0.03165 -0.033 0.452 0.819 0.836 0.950 8.326 0.298 0.376 2.0 0.314 0.03225 -0.036 0.433 0.824 0.824 0.951 9.737 0.305 0.364 2.5 0.363 0.03260 -0.039 0.415 0.830 0.809 0.951 11.121 0.313 0.357 3.0 0.408 0.03330 -0.042 0.400 0.838 0.788 0.951 12.248 0.319 0.352 3.5 0.454 0.03431 -0.045 0.379 0.843 0.770 0.951 13.231 0.322 0.349 4.0 0.499 0.03581 -0.048 0.358 0.851 0.752 0.952 13.937 0.329 0.347 4.5 0.542 0.03668 -0.052 0.339 0.859 0.730 0.952 14.770 0.347 0.346 5.0 0.578 0.03874 -0.056 0.324 0.868 0.700 0.952 14.931 0.356 0.347 5.5 0.618 0.04079 -0.060 0.306 0.876 0.676 0.952 15.151 0.235 0.347 6.0 0.780 0.03630 -0.053 0.024 0.886 0.864 0.952 21.498 0.232 0.318 6.5 0.824 0.03720 -0.056 0.022 0.897 0.845 0.955 22.144 0.358 0.319 7.0 0.856 0.03896 -0.061 0.020 0.953 0.812 0.954 21.974 0.075 0.321 7.5 0.684 0.05691 -0.081 0.019 0.953 0.024 0.955 12.014 0.074 0.368 8.0 0.723 0.06025 -0.085 0.018 0.953 0.023 0.955 11.995 0.346 0.367 8.5 0.759 0.06482 -0.088 0.018 0.956 0.023 0.957 11.717 0.348 0.366 9.0 0.797 0.06720 -0.092 0.018 0.956 0.021 0.957 11.859 0.348 0.365 9.5 0.834 0.07413 -0.095 0.017 0.956 0.021 0.958 11.243 0.350 0.365 10.0 0.869 0.07739 -0.099 0.016 0.956 0.020 0.957 11.231 0.352 0.364 10.5 0.904 0.08440 -0.103 0.016 0.956 0.019 0.957 10.713 0.356 0.364 11.0 0.938 0.09134 -0.106 0.016 0.956 0.019 0.958 10.266 0.358 0.363 11.5 0.971 0.09931 -0.110 0.016 0.957 0.019 0.958 9.780 0.359 0.363 12.0 1.004 0.10615 -0.114 0.016 0.951 0.018 0.953 9.455 0.363 0.363 12.5 1.035 0.11668 -0.117 0.015 0.952 0.018 0.953 8.870 0.373 0.363 13.0 1.062 0.12219 -0.121 0.015 0.952 0.018 0.953 8.691 0.390 0.364 13.5 1.086 0.13074 -0.124 0.014 0.957 0.018 0.959 8.306 0.403 0.364 14.0 1.108 0.13663 -0.128 0.014 0.957 0.017 0.959 8.112 0.419 0.365 14.5 1.128 0.14875 -0.131 0.014 0.957 0.017 0.959 7.583 0.441 0.367 15.0 1.146 0.15455 -0.135 0.013 0.957 0.016 0.959 7.413 0.449 0.368 Name = NACA M12 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 -0.790 0.15946 0.076 0.879 0.014 1.000 0.016 -4.952 0.429 0.346 -14.5 -0.772 0.15127 0.073 0.874 0.014 1.000 0.016 -5.104 0.408 0.344 -14.0 -0.750 0.13903 0.070 0.863 0.014 1.000 0.016 -5.393 0.388 0.343 -13.5 -0.726 0.13184 0.066 0.858 0.014 1.000 0.016 -5.509 0.382 0.342 -13.0 -0.701 0.12360 0.063 0.853 0.014 1.000 0.016 -5.675 0.376 0.340 -12.5 -0.675 0.11416 0.060 0.847 0.015 1.000 0.016 -5.917 0.372 0.339 -12.0 -0.648 0.11008 0.057 0.842 0.014 1.000 0.016 -5.890 0.366 0.338 -11.5 -0.620 0.10092 0.054 0.837 0.015 1.000 0.017 -6.140 0.362 0.336 -11.0 -0.590 0.08986 0.050 0.832 0.015 1.000 0.017 -6.569 0.361 0.335 -10.5 -0.560 0.08572 0.047 0.826 0.014 1.000 0.016 -6.534 0.358 0.334 -10.0 -0.529 0.08175 0.044 0.821 0.015 1.000 0.016 -6.468 0.355 0.332 -9.5 -0.497 0.07650 0.040 0.821 0.015 1.000 0.016 -6.491 0.352 0.331 -9.0 -0.463 0.07060 0.037 0.816 0.015 1.000 0.017 -6.562 0.349 0.330 -8.5 -0.429 0.06727 0.034 0.811 0.016 1.000 0.018 -6.377 0.348 0.328 -8.0 -0.394 0.06183 0.030 0.789 0.016 1.000 0.018 -6.380 0.347 0.326 -7.5 -0.359 0.05782 0.027 0.768 0.016 1.000 0.018 -6.209 0.347 0.324 -7.0 -0.324 0.05477 0.023 0.748 0.015 1.000 0.018 -5.906 0.346 0.322 -6.5 -0.287 0.05109 0.020 0.733 0.016 1.000 0.018 -5.622 0.344 0.319 -6.0 -0.250 0.04861 0.016 0.721 0.016 1.000 0.018 -5.144 0.343 0.315 -5.5 -0.213 0.04506 0.013 0.709 0.016 1.000 0.019 -4.718 0.342 0.311 -5.0 -0.175 0.04217 0.009 0.691 0.016 1.000 0.019 -4.144 0.342 0.304 -4.5 -0.137 0.03940 0.006 0.679 0.016 1.000 0.019 -3.467 0.341 0.293 -4.0 -0.098 0.03709 0.002 0.664 0.017 1.000 0.020 -2.637 0.340 0.274 -3.5 -0.059 0.03453 -0.001 0.645 0.017 1.000 0.021 -1.703 0.340 0.231 -3.0 -0.019 0.03209 -0.005 0.633 0.018 1.000 0.022 -0.599 0.166 0.007 -2.5 -0.143 0.03045 -0.008 0.621 0.019 1.000 0.024 -4.706 -0.174 0.193 -2.0 -0.055 0.02202 -0.020 0.609 0.021 1.000 0.960 -2.486 0.356 -0.110 -1.5 -0.020 0.02410 -0.021 0.594 0.023 1.000 0.959 -0.811 0.283 -0.839 -1.0 0.040 0.02238 -0.023 0.570 0.743 1.000 0.951 1.772 0.277 0.825 -0.5 0.099 0.02216 -0.025 0.542 0.765 1.000 0.951 4.465 0.279 0.498 0.0 0.158 0.02258 -0.026 0.518 0.792 1.000 0.951 7.006 0.276 0.416 0.5 0.218 0.02285 -0.028 0.494 0.808 1.000 0.951 9.519 0.273 0.377 1.0 0.277 0.02352 -0.029 0.473 0.814 1.000 0.951 11.774 0.274 0.355 1.5 0.336 0.02335 -0.030 0.452 0.819 1.000 0.951 14.399 0.274 0.340 2.0 0.396 0.02368 -0.032 0.433 0.824 1.000 0.952 16.705 0.274 0.330 2.5 0.455 0.02417 -0.033 0.415 0.830 1.000 0.952 18.822 0.274 0.323 3.0 0.514 0.02513 -0.035 0.400 0.838 1.000 0.952 20.462 0.359 0.317 3.5 0.520 0.02562 -0.040 0.379 0.843 0.900 0.952 20.302 0.397 0.328 4.0 0.571 0.02601 -0.043 0.358 0.851 0.888 0.952 21.934 0.303 0.325 4.5 0.620 0.02702 -0.046 0.339 0.859 0.876 0.953 22.959 0.312 0.324 5.0 0.666 0.02770 -0.049 0.324 0.868 0.858 0.953 24.042 0.319 0.323 5.5 0.712 0.02896 -0.052 0.306 0.876 0.842 0.953 24.597 0.263 0.323 6.0 0.803 0.03075 -0.051 0.024 0.886 0.900 0.953 26.106 0.265 0.313 6.5 0.847 0.03068 -0.054 0.022 0.897 0.882 0.956 27.603 0.334 0.314 7.0 0.888 0.03208 -0.058 0.020 0.953 0.861 0.954 27.681 0.345 0.315 7.5 0.928 0.03385 -0.062 0.019 0.953 0.839 0.955 27.408 0.088 0.316 8.0 0.721 0.05315 -0.085 0.018 0.953 0.024 0.955 13.570 0.092 0.367 8.5 0.759 0.05592 -0.088 0.018 0.956 0.023 0.957 13.568 0.348 0.366 9.0 0.796 0.06000 -0.092 0.018 0.956 0.023 0.957 13.259 0.348 0.366 9.5 0.833 0.06377 -0.096 0.017 0.956 0.021 0.958 13.060 0.350 0.365 10.0 0.868 0.06912 -0.099 0.016 0.956 0.021 0.957 12.555 0.352 0.364 10.5 0.903 0.07280 -0.103 0.016 0.956 0.020 0.957 12.410 0.354 0.364 11.0 0.937 0.07758 -0.106 0.016 0.956 0.020 0.958 12.079 0.356 0.364 11.5 0.971 0.08043 -0.110 0.016 0.957 0.019 0.958 12.076 0.358 0.363 12.0 1.004 0.08641 -0.114 0.016 0.951 0.018 0.953 11.615 0.363 0.363 12.5 1.035 0.09261 -0.117 0.015 0.952 0.018 0.953 11.175 0.374 0.363 13.0 1.062 0.10000 -0.121 0.015 0.952 0.018 0.953 10.616 0.390 0.364 13.5 1.086 0.10250 -0.124 0.014 0.957 0.018 0.959 10.595 0.403 0.364 14.0 1.108 0.11098 -0.128 0.014 0.957 0.017 0.959 9.985 0.422 0.365 14.5 1.127 0.12502 -0.131 0.014 0.957 0.018 0.959 9.018 0.442 0.367 15.0 1.145 0.13003 -0.135 0.013 0.957 0.017 0.959 8.807 0.449 0.368 Name = NACA M12 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 -0.790 0.14413 0.076 0.879 0.014 1.000 0.016 -5.478 0.430 0.346 -14.5 -0.772 0.13045 0.073 0.874 0.014 1.000 0.016 -5.919 0.408 0.344 -14.0 -0.750 0.12600 0.070 0.863 0.014 1.000 0.016 -5.951 0.388 0.343 -13.5 -0.726 0.11467 0.066 0.858 0.014 1.000 0.016 -6.334 0.382 0.342 -13.0 -0.701 0.10739 0.063 0.853 0.014 1.000 0.016 -6.532 0.376 0.340 -12.5 -0.675 0.10442 0.060 0.847 0.015 1.000 0.016 -6.468 0.372 0.339 -12.0 -0.648 0.09627 0.057 0.842 0.014 1.000 0.016 -6.735 0.366 0.338 -11.5 -0.620 0.08886 0.054 0.837 0.015 1.000 0.017 -6.974 0.362 0.336 -11.0 -0.590 0.08483 0.050 0.832 0.015 1.000 0.017 -6.956 0.361 0.335 -10.5 -0.560 0.08111 0.047 0.826 0.014 1.000 0.017 -6.903 0.359 0.334 -10.0 -0.529 0.07513 0.044 0.821 0.015 1.000 0.017 -7.037 0.355 0.332 -9.5 -0.496 0.07251 0.040 0.821 0.015 1.000 0.017 -6.845 0.352 0.331 -9.0 -0.463 0.06676 0.037 0.816 0.015 1.000 0.017 -6.936 0.350 0.330 -8.5 -0.429 0.06074 0.034 0.811 0.016 1.000 0.018 -7.063 0.348 0.328 -8.0 -0.394 0.05806 0.030 0.789 0.016 1.000 0.018 -6.791 0.347 0.326 -7.5 -0.359 0.05431 0.027 0.768 0.016 1.000 0.018 -6.607 0.347 0.325 -7.0 -0.323 0.05103 0.023 0.748 0.015 1.000 0.018 -6.335 0.346 0.322 -6.5 -0.287 0.04766 0.020 0.733 0.016 1.000 0.018 -6.021 0.344 0.319 -6.0 -0.250 0.04442 0.016 0.721 0.016 1.000 0.018 -5.627 0.343 0.316 -5.5 -0.212 0.04154 0.013 0.709 0.016 1.000 0.019 -5.115 0.342 0.311 -5.0 -0.174 0.03913 0.009 0.691 0.016 1.000 0.019 -4.459 0.342 0.304 -4.5 -0.136 0.03644 0.006 0.679 0.016 1.000 0.020 -3.740 0.341 0.293 -4.0 -0.098 0.03410 0.002 0.664 0.017 1.000 0.021 -2.861 0.340 0.275 -3.5 -0.058 0.03174 -0.001 0.645 0.017 1.000 0.021 -1.838 0.340 0.231 -3.0 -0.019 0.02987 -0.005 0.633 0.018 1.000 0.023 -0.628 0.167 0.001 -2.5 -0.143 0.02822 -0.008 0.621 0.019 1.000 0.024 -5.079 -0.163 0.193 -2.0 -0.055 0.01954 -0.020 0.609 0.021 1.000 0.962 -2.827 0.356 -0.107 -1.5 -0.020 0.02141 -0.021 0.594 0.023 1.000 0.961 -0.913 0.283 -0.841 -1.0 0.040 0.01920 -0.023 0.570 0.743 1.000 0.952 2.066 0.277 0.826 -0.5 0.099 0.01986 -0.025 0.542 0.765 1.000 0.952 4.982 0.278 0.498 0.0 0.158 0.01995 -0.026 0.518 0.792 1.000 0.952 7.931 0.276 0.416 0.5 0.218 0.01987 -0.028 0.494 0.808 1.000 0.951 10.947 0.273 0.377 1.0 0.277 0.01961 -0.029 0.473 0.814 1.000 0.952 14.121 0.274 0.355 1.5 0.336 0.02028 -0.030 0.452 0.819 1.000 0.952 16.578 0.274 0.340 2.0 0.396 0.02042 -0.032 0.433 0.824 1.000 0.952 19.369 0.274 0.330 2.5 0.455 0.02068 -0.033 0.415 0.830 1.000 0.953 21.998 0.274 0.323 3.0 0.514 0.02111 -0.035 0.400 0.838 1.000 0.953 24.364 0.274 0.317 3.5 0.573 0.02159 -0.036 0.379 0.843 1.000 0.953 26.558 0.274 0.313 4.0 0.632 0.02212 -0.038 0.358 0.851 1.000 0.953 28.580 0.274 0.309 4.5 0.691 0.02321 -0.039 0.339 0.859 1.000 0.953 29.783 0.274 0.306 5.0 0.750 0.02338 -0.040 0.324 0.868 1.000 0.953 32.068 0.275 0.304 5.5 0.808 0.02493 -0.042 0.306 0.876 1.000 0.953 32.408 0.275 0.302 6.0 0.866 0.02759 -0.043 0.024 0.886 1.000 0.953 31.387 0.452 0.300 6.5 0.860 0.02825 -0.052 0.022 0.897 0.903 0.956 30.458 0.584 0.311 7.0 0.904 0.02975 -0.056 0.020 0.953 0.885 0.954 30.372 0.338 0.312 7.5 0.944 0.03058 -0.060 0.019 0.953 0.864 0.955 30.866 0.093 0.313 8.0 0.720 0.05004 -0.085 0.018 0.953 0.025 0.955 14.387 0.097 0.368 8.5 0.757 0.05308 -0.088 0.018 0.956 0.024 0.957 14.268 0.347 0.367 9.0 0.795 0.05564 -0.092 0.018 0.956 0.023 0.957 14.285 0.347 0.366 9.5 0.832 0.05922 -0.096 0.017 0.956 0.022 0.958 14.050 0.350 0.365 10.0 0.867 0.06363 -0.099 0.016 0.956 0.022 0.957 13.626 0.352 0.364 10.5 0.903 0.06772 -0.103 0.016 0.956 0.021 0.957 13.331 0.354 0.364 11.0 0.936 0.07164 -0.106 0.016 0.956 0.021 0.958 13.071 0.356 0.364 11.5 0.971 0.07514 -0.110 0.016 0.957 0.019 0.958 12.918 0.357 0.363 12.0 1.003 0.08106 -0.114 0.016 0.951 0.019 0.953 12.374 0.363 0.363 12.5 1.034 0.08629 -0.117 0.015 0.952 0.019 0.953 11.987 0.374 0.363 13.0 1.061 0.09299 -0.121 0.015 0.952 0.018 0.953 11.410 0.390 0.364 13.5 1.085 0.09547 -0.124 0.014 0.957 0.018 0.959 11.369 0.403 0.365 14.0 1.108 0.10319 -0.128 0.014 0.957 0.018 0.959 10.734 0.419 0.365 14.5 1.127 0.10688 -0.131 0.014 0.957 0.018 0.959 10.549 0.440 0.367 15.0 1.145 0.11541 -0.135 0.013 0.957 0.017 0.959 9.920 0.453 0.368 Name = NACA M12 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 -0.790 0.12892 0.076 0.879 0.014 1.000 0.016 -6.125 0.429 0.346 -14.5 -0.772 0.12351 0.073 0.874 0.014 1.000 0.016 -6.251 0.408 0.344 -14.0 -0.750 0.11351 0.070 0.863 0.014 1.000 0.016 -6.605 0.388 0.343 -13.5 -0.726 0.10863 0.066 0.858 0.014 1.000 0.016 -6.686 0.381 0.342 -13.0 -0.701 0.10564 0.063 0.853 0.014 1.000 0.017 -6.638 0.376 0.340 -12.5 -0.675 0.09516 0.060 0.847 0.015 1.000 0.016 -7.098 0.373 0.339 -12.0 -0.648 0.09123 0.057 0.842 0.014 1.000 0.016 -7.106 0.366 0.338 -11.5 -0.620 0.08712 0.054 0.837 0.015 1.000 0.017 -7.111 0.362 0.336 -11.0 -0.590 0.07791 0.050 0.832 0.015 1.000 0.017 -7.575 0.361 0.335 -10.5 -0.560 0.07445 0.047 0.826 0.014 1.000 0.017 -7.521 0.358 0.334 -10.0 -0.529 0.07126 0.044 0.821 0.015 1.000 0.017 -7.418 0.355 0.333 -9.5 -0.496 0.06710 0.040 0.821 0.015 1.000 0.017 -7.397 0.352 0.331 -9.0 -0.463 0.06181 0.037 0.816 0.015 1.000 0.017 -7.491 0.350 0.330 -8.5 -0.429 0.05684 0.034 0.811 0.016 1.000 0.018 -7.548 0.348 0.328 -8.0 -0.394 0.05440 0.030 0.789 0.016 1.000 0.018 -7.247 0.346 0.326 -7.5 -0.359 0.05205 0.027 0.768 0.016 1.000 0.019 -6.889 0.346 0.325 -7.0 -0.323 0.04919 0.023 0.748 0.015 1.000 0.018 -6.567 0.346 0.322 -6.5 -0.287 0.04600 0.020 0.733 0.016 1.000 0.018 -6.233 0.344 0.319 -6.0 -0.250 0.04269 0.016 0.721 0.016 1.000 0.019 -5.849 0.343 0.316 -5.5 -0.212 0.03984 0.013 0.709 0.016 1.000 0.019 -5.327 0.342 0.311 -5.0 -0.174 0.03741 0.009 0.691 0.016 1.000 0.020 -4.657 0.342 0.304 -4.5 -0.136 0.03502 0.006 0.679 0.016 1.000 0.020 -3.880 0.341 0.294 -4.0 -0.097 0.03264 0.002 0.664 0.017 1.000 0.021 -2.975 0.340 0.275 -3.5 -0.058 0.03074 -0.001 0.645 0.017 1.000 0.022 -1.883 0.339 0.231 -3.0 -0.018 0.02846 -0.005 0.633 0.018 1.000 0.023 -0.638 0.167 -0.007 -2.5 -0.143 0.02670 -0.008 0.621 0.019 1.000 0.025 -5.368 -0.152 0.193 -2.0 -0.056 0.01883 -0.020 0.609 0.021 1.000 0.963 -2.962 0.356 -0.105 -1.5 -0.020 0.01969 -0.021 0.594 0.023 1.000 0.962 -0.993 0.282 -0.842 -1.0 0.040 0.01773 -0.023 0.570 0.743 1.000 0.953 2.237 0.277 0.826 -0.5 0.099 0.01743 -0.025 0.542 0.765 1.000 0.953 5.678 0.278 0.498 0.0 0.158 0.01766 -0.026 0.518 0.792 1.000 0.952 8.961 0.276 0.416 0.5 0.218 0.01773 -0.028 0.494 0.808 1.000 0.952 12.268 0.273 0.377 1.0 0.277 0.01824 -0.029 0.473 0.814 1.000 0.952 15.182 0.274 0.355 1.5 0.336 0.01812 -0.030 0.452 0.819 1.000 0.953 18.551 0.274 0.340 2.0 0.396 0.01903 -0.032 0.433 0.824 1.000 0.953 20.782 0.274 0.330 2.5 0.455 0.01924 -0.033 0.415 0.830 1.000 0.953 23.650 0.274 0.323 3.0 0.514 0.01952 -0.035 0.400 0.838 1.000 0.953 26.341 0.274 0.317 3.5 0.573 0.01994 -0.036 0.379 0.843 1.000 0.954 28.756 0.274 0.313 4.0 0.632 0.02039 -0.038 0.358 0.851 1.000 0.954 31.019 0.274 0.309 4.5 0.691 0.02097 -0.039 0.339 0.859 1.000 0.954 32.964 0.274 0.306 5.0 0.750 0.02204 -0.040 0.324 0.868 1.000 0.954 34.014 0.275 0.304 5.5 0.808 0.02194 -0.042 0.306 0.876 1.000 0.954 36.830 0.275 0.302 6.0 0.866 0.02212 -0.043 0.024 0.886 1.000 0.954 39.148 0.275 0.300 6.5 0.924 0.02294 -0.045 0.022 0.897 1.000 0.956 40.260 0.506 0.298 7.0 0.912 0.02739 -0.055 0.020 0.953 0.897 0.954 33.277 0.702 0.310 7.5 0.954 0.02863 -0.059 0.019 0.953 0.879 0.955 33.321 0.338 0.311 8.0 0.995 0.03022 -0.062 0.018 0.953 0.861 0.955 32.940 0.099 0.313 8.5 0.757 0.05047 -0.088 0.018 0.956 0.025 0.957 14.992 0.103 0.367 9.0 0.794 0.05410 -0.092 0.018 0.956 0.024 0.957 14.667 0.347 0.366 9.5 0.831 0.05649 -0.096 0.017 0.956 0.022 0.958 14.718 0.349 0.365 10.0 0.866 0.06036 -0.099 0.016 0.956 0.023 0.957 14.354 0.352 0.365 10.5 0.902 0.06469 -0.103 0.016 0.956 0.021 0.957 13.946 0.354 0.364 11.0 0.936 0.06811 -0.106 0.016 0.956 0.021 0.958 13.739 0.356 0.364 11.5 0.970 0.07204 -0.110 0.016 0.957 0.020 0.958 13.463 0.357 0.363 12.0 1.002 0.07808 -0.114 0.016 0.951 0.020 0.953 12.838 0.363 0.363 12.5 1.034 0.08271 -0.117 0.015 0.952 0.019 0.953 12.498 0.373 0.363 13.0 1.061 0.08668 -0.121 0.015 0.952 0.019 0.953 12.236 0.390 0.364 13.5 1.085 0.09158 -0.124 0.014 0.957 0.019 0.959 11.846 0.403 0.365 14.0 1.107 0.09588 -0.128 0.014 0.957 0.018 0.959 11.548 0.419 0.366 14.5 1.127 0.10252 -0.131 0.014 0.957 0.018 0.959 10.992 0.440 0.367 15.0 1.145 0.10681 -0.135 0.013 0.957 0.018 0.959 10.717 0.449 0.368