NACA 4424 1.000000, 0.000000 0.951960, 0.022400 0.903200, 0.040990 0.804640, 0.074470 0.704870, 0.103120 0.604050, 0.126740 0.502350, 0.144740 0.400000, 0.156060 0.294010, 0.157380 0.241110, 0.152870 0.188580, 0.144160 0.136740, 0.130450 0.086110, 0.110120 0.061530, 0.096510 0.037750, 0.079420 0.015360, 0.056240 0.005300, 0.039640 0.000000, 0.000000 0.019700, -0.034720 0.034640, -0.046560 0.062250, -0.060660 0.088470, -0.069310 0.113890, -0.075120 0.163260, -0.081690 0.211420, -0.084160 0.258890, -0.084110 0.305990, -0.082380 0.400000, -0.076060 0.497650, -0.066980 0.595950, -0.055620 0.695130, -0.043120 0.795360, -0.030030 0.896800, -0.016550 0.948040, -0.009640 1.000000, 0.000000

Name = NACA 4424Mach = 0; Re = 25000; T.U. = 1.0; T.L. = 1.0Surface 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 -0.630 0.12759 0.009 0.810 0.045 0.876 0.085 -4.934 0.338 0.265-14.5 -0.587 0.11754 0.006 0.799 0.048 0.887 0.085 -4.995 0.335 0.260-14.0 -0.543 0.11437 0.002 0.782 0.052 0.892 0.088 -4.752 0.335 0.254-13.5 -0.500 0.11164 -0.002 0.771 0.055 0.881 0.088 -4.478 0.336 0.246-13.0 -0.456 0.10627 -0.005 0.760 0.059 0.876 0.093 -4.291 0.334 0.238-12.5 -0.412 0.10204 -0.009 0.749 0.062 0.876 0.097 -4.033 0.334 0.228-12.0 -0.366 0.09841 -0.013 0.738 0.066 0.870 0.101 -3.724 0.331 0.214-11.5 -0.320 0.09322 -0.017 0.733 0.070 0.865 0.114 -3.437 0.331 0.198-11.0 -0.276 0.09056 -0.020 0.721 0.074 0.859 0.121 -3.042 0.335 0.176-10.5 -0.230 0.08637 -0.024 0.716 0.077 0.854 0.129 -2.664 0.335 0.144-10.0 -0.184 0.08266 -0.028 0.710 0.081 0.843 0.140 -2.231 0.335 0.097-9.5 -0.138 0.07885 -0.032 0.688 0.085 0.854 0.152 -1.752 0.336 0.017-9.0 -0.093 0.07645 -0.036 0.677 0.088 0.848 0.171 -1.219 0.338 -0.137-8.5 -0.047 0.07356 -0.040 0.660 0.097 0.848 0.179 -0.636 0.340 -0.609-8.0 -0.002 0.06917 -0.044 0.643 0.101 0.843 0.195 -0.023 0.229 -27.555-7.5 -0.434 0.06702 -0.048 0.632 0.105 0.837 0.215 -6.477 0.226 0.138-7.0 -0.359 0.06345 -0.053 0.616 0.114 0.835 0.239 -5.658 0.308 0.103-6.5 -0.286 0.06086 -0.057 0.604 0.125 0.831 0.251 -4.691 0.310 0.050-6.0 -0.213 0.05853 -0.061 0.581 0.137 0.831 0.263 -3.638 0.311 -0.039-5.5 -0.141 0.05642 -0.066 0.557 0.144 0.835 0.290 -2.501 0.313 -0.217-5.0 -0.070 0.05397 -0.070 0.538 0.156 0.831 0.306 -1.306 0.315 -0.750-4.5 -0.001 0.05190 -0.075 0.522 0.167 0.827 0.337 -0.015 0.318 0.250-4.0 0.068 0.04933 -0.080 0.502 0.179 0.824 0.376 1.376 0.322 1.426-3.5 0.135 0.04639 -0.085 0.491 0.191 0.816 0.439 2.917 0.335 0.877-3.0 0.201 0.04107 -0.091 0.479 0.199 0.801 0.580 4.894 0.338 0.704-2.5 0.266 0.03934 -0.096 0.467 0.211 0.789 0.653 6.773 0.328 0.612-2.0 0.331 0.03752 -0.101 0.455 0.227 0.774 0.726 8.831 0.323 0.556-1.5 0.396 0.03652 -0.106 0.443 0.243 0.759 0.792 10.844 0.314 0.517-1.0 0.461 0.03613 -0.110 0.435 0.259 0.739 0.834 12.753 0.305 0.488-0.5 0.526 0.03602 -0.113 0.431 0.275 0.716 0.873 14.591 0.189 0.4650.0 0.357 0.04181 -0.116 0.420 0.290 0.705 0.950 8.543 0.193 0.5750.5 0.405 0.04324 -0.120 0.412 0.306 0.685 0.952 9.379 0.342 0.5451.0 0.444 0.04551 -0.124 0.408 0.376 0.651 0.952 9.754 0.339 0.5291.5 0.497 0.04621 -0.128 0.396 0.470 0.643 0.893 10.760 0.325 0.5072.0 0.553 0.04741 -0.132 0.380 0.509 0.639 0.893 11.657 0.332 0.4892.5 0.600 0.04936 -0.136 0.369 0.529 0.623 0.951 12.159 0.331 0.4773.0 0.657 0.05054 -0.140 0.353 0.553 0.623 0.952 13.006 0.330 0.4643.5 0.706 0.05219 -0.145 0.341 0.572 0.612 0.952 13.534 0.350 0.4554.0 0.748 0.05462 -0.150 0.333 0.596 0.588 0.953 13.703 0.365 0.450

4.5 0.790 0.05666 -0.154 0.325 0.630 0.565 0.953 13.947 0.352 0.4455.0 0.841 0.05837 -0.159 0.314 0.661 0.557 0.953 14.404 0.352 0.4395.5 0.883 0.06133 -0.164 0.306 0.695 0.538 0.953 14.402 0.368 0.4366.0 0.925 0.06433 -0.169 0.298 0.722 0.518 0.954 14.376 0.358 0.4336.5 0.973 0.06662 -0.174 0.286 0.749 0.510 0.954 14.609 0.348 0.4287.0 1.021 0.06930 -0.178 0.274 0.780 0.502 0.954 14.736 0.356 0.4257.5 1.065 0.07234 -0.183 0.266 0.799 0.487 0.954 14.722 0.353 0.4228.0 1.115 0.07580 -0.188 0.253 0.811 0.483 0.954 14.711 0.344 0.4198.5 1.165 0.07886 -0.193 0.241 0.819 0.479 0.954 14.768 0.346 0.4169.0 1.214 0.07928 -0.197 0.225 0.830 0.475 0.958 15.306 0.350 0.4139.5 1.260 0.08323 -0.202 0.213 0.843 0.468 0.960 15.141 0.355 0.41110.0 1.306 0.08603 -0.207 0.196 0.854 0.461 0.960 15.175 0.359 0.40910.5 1.350 0.08918 -0.212 0.185 0.870 0.453 0.960 15.139 0.366 0.40711.0 1.391 0.09320 -0.217 0.174 0.881 0.442 0.961 14.929 0.368 0.40611.5 1.435 0.09939 -0.222 0.163 0.897 0.434 0.961 14.433 0.371 0.40512.0 1.474 0.10452 -0.227 0.152 0.951 0.423 0.953 14.103 0.387 0.40412.5 1.510 0.10722 -0.232 0.140 0.957 0.408 0.959 14.080 0.384 0.40413.0 1.549 0.11324 -0.237 0.130 0.957 0.400 0.959 13.683 0.378 0.40313.5 1.588 0.11878 -0.242 0.119 0.957 0.388 0.959 13.366 0.364 0.40314.0 1.634 0.12188 -0.247 0.101 0.957 0.392 0.959 13.408 0.361 0.40114.5 1.673 0.12913 -0.252 0.090 0.958 0.384 0.959 12.953 0.408 0.40115.0 1.700 0.13426 -0.257 0.083 0.958 0.361 0.959 12.659 0.451 0.401

Name = NACA 4424Mach = 0; Re = 50000; T.U. = 1.0; T.L. = 1.0Surface 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 -0.631 0.10356 0.010 0.810 0.045 0.903 0.114 -6.093 0.336 0.267-14.5 -0.590 0.10142 0.007 0.799 0.048 1.000 0.121 -5.819 0.336 0.262-14.0 -0.547 0.09595 0.003 0.782 0.052 1.000 0.125 -5.705 0.337 0.256-13.5 -0.502 0.09159 -0.001 0.771 0.055 1.000 0.118 -5.476 0.336 0.248-13.0 -0.460 0.09001 -0.004 0.760 0.059 1.000 0.130 -5.107 0.335 0.241-12.5 -0.415 0.08515 -0.008 0.749 0.062 1.000 0.135 -4.877 0.336 0.230-12.0 -0.371 0.08256 -0.012 0.738 0.066 1.000 0.143 -4.495 0.335 0.218-11.5 -0.330 0.07785 -0.015 0.733 0.070 0.909 0.167 -4.235 0.339 0.203-11.0 -0.288 0.07405 -0.019 0.721 0.074 0.909 0.183 -3.889 0.342 0.183-10.5 -0.245 0.07069 -0.023 0.716 0.077 0.898 0.199 -3.471 0.344 0.155-10.0 -0.204 0.06772 -0.027 0.710 0.081 0.887 0.219 -3.012 0.352 0.117-9.5 -0.166 0.06392 -0.031 0.688 0.085 0.903 0.247 -2.597 0.360 0.061-9.0 -0.128 0.05952 -0.036 0.677 0.088 0.898 0.275 -2.150 0.353 -0.028-8.5 -0.083 0.05732 -0.040 0.660 0.097 0.903 0.286 -1.444 0.360 -0.232-8.0 -0.048 0.05356 -0.044 0.643 0.101 0.903 0.322 -0.892 0.401 -0.680-7.5 -0.020 0.04915 -0.049 0.632 0.105 0.898 0.373 -0.404 0.216 -2.234-7.0 -0.351 0.04450 -0.055 0.616 0.114 0.896 0.435 -7.892 0.208 0.094-6.5 -0.279 0.04102 -0.060 0.604 0.125 0.892 0.486 -6.790 0.326 0.034

-6.0 -0.207 0.03808 -0.066 0.581 0.137 0.896 0.537 -5.444 0.335 -0.067-5.5 -0.137 0.03454 -0.072 0.557 0.144 0.899 0.615 -3.966 0.339 -0.277-5.0 -0.068 0.03210 -0.078 0.538 0.156 0.899 0.672 -2.129 0.336 -0.892-4.5 -0.001 0.03040 -0.084 0.522 0.167 0.896 0.734 -0.025 0.334 0.250-4.0 0.066 0.02871 -0.089 0.502 0.179 0.892 0.788 2.299 0.326 1.604-3.5 0.132 0.02769 -0.094 0.491 0.191 0.884 0.830 4.773 0.319 0.962-3.0 0.198 0.02697 -0.098 0.479 0.199 0.877 0.873 7.340 0.323 0.747-2.5 0.263 0.02508 -0.104 0.467 0.211 0.873 0.954 10.485 0.308 0.644-2.0 0.329 0.02715 -0.106 0.455 0.227 0.865 0.951 12.110 0.287 0.572-1.5 0.394 0.02699 -0.108 0.443 0.243 0.858 0.952 14.608 0.288 0.525-1.0 0.460 0.02734 -0.111 0.435 0.259 0.846 0.954 16.818 0.288 0.491-0.5 0.525 0.02768 -0.113 0.431 0.275 0.835 0.955 18.974 -0.009 0.4660.0 0.441 0.02958 -0.116 0.420 0.290 0.827 0.955 14.898 0.068 0.5130.5 0.494 0.03009 -0.119 0.412 0.306 0.816 0.956 16.399 0.320 0.4911.0 0.538 0.03106 -0.123 0.408 0.376 0.793 0.956 17.312 0.318 0.4781.5 0.596 0.03225 -0.126 0.396 0.470 0.789 0.955 18.481 0.312 0.4622.0 0.651 0.03256 -0.130 0.380 0.509 0.782 0.955 19.992 0.319 0.4492.5 0.703 0.03366 -0.133 0.369 0.529 0.770 0.956 20.882 0.315 0.4403.0 0.763 0.03467 -0.137 0.353 0.553 0.770 0.956 22.008 0.317 0.4303.5 0.814 0.03574 -0.141 0.341 0.572 0.759 0.956 22.766 0.333 0.4234.0 0.861 0.03755 -0.145 0.333 0.596 0.743 0.956 22.919 0.345 0.4194.5 0.904 0.03884 -0.150 0.325 0.630 0.724 0.957 23.265 0.340 0.4155.0 0.956 0.04013 -0.154 0.314 0.661 0.716 0.956 23.814 0.343 0.4115.5 0.998 0.04211 -0.158 0.306 0.695 0.697 0.956 23.695 0.362 0.4096.0 1.040 0.04416 -0.163 0.298 0.722 0.678 0.956 23.555 0.349 0.4076.5 1.091 0.04613 -0.167 0.286 0.749 0.670 0.956 23.647 0.342 0.4047.0 1.138 0.04772 -0.172 0.274 0.780 0.658 0.955 23.843 0.362 0.4017.5 1.177 0.05044 -0.177 0.266 0.799 0.639 0.955 23.342 0.359 0.4008.0 1.226 0.05312 -0.182 0.253 0.811 0.631 0.956 23.080 0.345 0.3988.5 1.274 0.05540 -0.186 0.241 0.819 0.623 0.956 22.998 0.341 0.3969.0 1.325 0.05692 -0.191 0.225 0.830 0.620 0.960 23.274 0.350 0.3949.5 1.368 0.05992 -0.196 0.213 0.843 0.608 0.961 22.823 0.364 0.39310.0 1.411 0.06209 -0.201 0.196 0.854 0.597 0.961 22.725 0.358 0.39210.5 1.457 0.06569 -0.205 0.185 0.870 0.589 0.961 22.183 0.368 0.39111.0 1.496 0.06833 -0.211 0.174 0.881 0.574 0.962 21.896 0.379 0.39111.5 1.537 0.07239 -0.216 0.163 0.897 0.563 0.961 21.236 0.383 0.39012.0 1.574 0.07569 -0.221 0.152 0.951 0.548 0.953 20.801 0.387 0.39012.5 1.613 0.08056 -0.226 0.140 0.957 0.536 0.959 20.029 0.384 0.39013.0 1.651 0.08354 -0.231 0.130 0.957 0.525 0.959 19.765 0.399 0.39013.5 1.684 0.08762 -0.237 0.119 0.957 0.510 0.959 19.220 0.374 0.39114.0 1.730 0.09225 -0.241 0.101 0.957 0.510 0.959 18.759 0.369 0.38914.5 1.765 0.09628 -0.246 0.090 0.958 0.499 0.959 18.335 0.411 0.39015.0 1.796 0.10074 -0.252 0.083 0.958 0.483 0.959 17.831 0.425 0.390

Name = NACA 4424Mach = 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 -0.646 0.09332 0.012 0.810 0.045 1.000 0.163 -6.919 0.338 0.268-14.5 -0.603 0.08873 0.008 0.799 0.048 1.000 0.167 -6.802 0.339 0.264-14.0 -0.563 0.08552 0.004 0.782 0.052 1.000 0.175 -6.577 0.336 0.258-13.5 -0.514 0.08258 0.000 0.771 0.055 1.000 0.167 -6.225 0.337 0.251-13.0 -0.473 0.07898 -0.003 0.760 0.059 1.000 0.179 -5.994 0.341 0.243-12.5 -0.432 0.07654 -0.007 0.749 0.062 1.000 0.191 -5.643 0.340 0.234-12.0 -0.388 0.07240 -0.011 0.738 0.066 1.000 0.199 -5.361 0.354 0.222-11.5 -0.358 0.06666 -0.015 0.733 0.070 1.000 0.239 -5.371 0.367 0.209-11.0 -0.321 0.06298 -0.019 0.721 0.074 1.000 0.263 -5.092 0.362 0.191-10.5 -0.284 0.05921 -0.023 0.716 0.077 1.000 0.286 -4.790 0.364 0.169-10.0 -0.246 0.05528 -0.027 0.710 0.081 1.000 0.310 -4.443 0.395 0.138-9.5 -0.221 0.05036 -0.032 0.688 0.085 1.000 0.357 -4.380 0.442 0.104-9.0 -0.194 0.04573 -0.037 0.677 0.088 1.000 0.404 -4.237 0.437 0.057-8.5 -0.165 0.04196 -0.043 0.660 0.097 1.000 0.447 -3.935 0.560 -0.008-8.0 -0.155 0.03697 -0.049 0.643 0.101 1.000 0.525 -4.200 0.701 -0.068-7.5 -0.136 0.03312 -0.056 0.632 0.105 1.000 0.588 -4.103 0.569 -0.161-7.0 -0.114 0.03186 -0.062 0.616 0.114 1.000 0.649 -3.587 0.493 -0.296-6.5 -0.084 0.02761 -0.068 0.604 0.125 1.000 0.699 -3.034 0.434 -0.568-6.0 -0.050 0.02737 -0.074 0.581 0.137 1.000 0.745 -1.820 0.430 -1.241-5.5 -0.018 0.02618 -0.080 0.557 0.144 1.000 0.799 -0.689 -0.358 -4.204-5.0 -0.067 0.02321 -0.085 0.538 0.156 1.000 0.830 -2.906 0.778 -1.010-4.5 -0.001 0.02241 -0.089 0.522 0.167 1.000 0.862 -0.033 0.314 0.250-4.0 0.066 0.02216 -0.094 0.502 0.179 1.000 0.889 2.957 0.322 1.677-3.5 0.131 0.01894 -0.099 0.491 0.191 1.000 0.954 6.926 0.309 1.004-3.0 0.197 0.01892 -0.101 0.479 0.199 1.000 0.955 10.419 0.287 0.764-2.5 0.263 0.02127 -0.104 0.467 0.211 0.944 0.957 12.362 0.286 0.645-2.0 0.329 0.02326 -0.106 0.455 0.227 0.907 0.954 14.133 0.286 0.573-1.5 0.394 0.02361 -0.109 0.443 0.243 0.899 0.955 16.702 0.287 0.525-1.0 0.460 0.02291 -0.111 0.435 0.259 0.888 0.956 20.072 0.288 0.491-0.5 0.525 0.02370 -0.113 0.431 0.275 0.880 0.957 22.158 0.558 0.4660.0 0.476 0.02478 -0.116 0.420 0.290 0.873 0.957 19.198 1.498 0.4940.5 0.530 0.02505 -0.119 0.412 0.306 0.861 0.958 21.141 0.308 0.4751.0 0.583 0.02565 -0.122 0.408 0.376 0.850 0.958 22.720 0.307 0.4601.5 0.642 0.02649 -0.125 0.396 0.470 0.846 0.958 24.229 0.304 0.4452.0 0.700 0.02684 -0.129 0.380 0.509 0.843 0.957 26.103 0.308 0.4332.5 0.756 0.02767 -0.132 0.369 0.529 0.835 0.958 27.311 0.309 0.4253.0 0.814 0.02852 -0.135 0.353 0.553 0.831 0.958 28.531 0.311 0.4163.5 0.868 0.02916 -0.139 0.341 0.572 0.824 0.958 29.771 0.320 0.4104.0 0.918 0.02989 -0.143 0.333 0.596 0.812 0.958 30.723 0.326 0.4054.5 0.968 0.03178 -0.146 0.325 0.630 0.801 0.959 30.471 0.329 0.4015.0 1.019 0.03240 -0.150 0.314 0.661 0.789 0.958 31.436 0.336 0.3985.5 1.065 0.03381 -0.155 0.306 0.695 0.774 0.958 31.499 0.345 0.3956.0 1.110 0.03534 -0.159 0.298 0.722 0.759 0.958 31.416 0.338 0.393

6.5 1.162 0.03723 -0.163 0.286 0.749 0.751 0.957 31.204 0.336 0.3917.0 1.209 0.03857 -0.168 0.274 0.780 0.739 0.957 31.348 0.351 0.3897.5 1.252 0.04066 -0.172 0.266 0.799 0.724 0.957 30.789 0.348 0.3888.0 1.301 0.04314 -0.177 0.253 0.811 0.716 0.957 30.165 0.345 0.3868.5 1.346 0.04443 -0.181 0.241 0.819 0.705 0.957 30.303 0.347 0.3859.0 1.395 0.04595 -0.186 0.225 0.830 0.697 0.960 30.365 0.355 0.3839.5 1.437 0.04811 -0.191 0.213 0.843 0.682 0.962 29.866 0.365 0.38310.0 1.481 0.05105 -0.196 0.196 0.854 0.671 0.962 29.007 0.362 0.38210.5 1.524 0.05356 -0.200 0.185 0.870 0.660 0.962 28.450 0.374 0.38211.0 1.562 0.05613 -0.206 0.174 0.881 0.645 0.962 27.835 0.378 0.38211.5 1.604 0.06029 -0.211 0.163 0.897 0.634 0.962 26.601 0.383 0.38112.0 1.640 0.06370 -0.216 0.152 0.951 0.619 0.953 25.749 0.399 0.38212.5 1.676 0.06665 -0.221 0.140 0.957 0.604 0.959 25.138 0.392 0.38213.0 1.714 0.06988 -0.227 0.130 0.957 0.593 0.959 24.533 0.395 0.38213.5 1.749 0.07386 -0.232 0.119 0.957 0.578 0.959 23.675 0.389 0.38314.0 1.789 0.07794 -0.237 0.101 0.957 0.570 0.959 22.951 0.394 0.38214.5 1.820 0.08230 -0.242 0.090 0.958 0.555 0.959 22.121 0.429 0.38315.0 1.850 0.08785 -0.248 0.083 0.958 0.540 0.959 21.061 0.434 0.384

Name = NACA 4424Mach = 0; Re = 100000; T.U. = 1.0; T.L. = 1.0Surface 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 -0.667 0.08630 0.013 0.810 0.045 1.000 0.207 -7.727 0.343 0.269-14.5 -0.626 0.08304 0.009 0.799 0.048 1.000 0.215 -7.542 0.343 0.264-14.0 -0.585 0.07792 0.005 0.782 0.052 1.000 0.223 -7.512 0.337 0.259-13.5 -0.537 0.07631 0.001 0.771 0.055 1.000 0.219 -7.038 0.340 0.252-13.0 -0.499 0.07216 -0.003 0.760 0.059 1.000 0.235 -6.915 0.349 0.245-12.5 -0.458 0.06839 -0.007 0.749 0.062 1.000 0.247 -6.693 0.349 0.235-12.0 -0.418 0.06537 -0.011 0.738 0.066 1.000 0.263 -6.393 0.380 0.224-11.5 -0.393 0.05932 -0.015 0.733 0.070 1.000 0.306 -6.630 0.418 0.212-11.0 -0.365 0.05470 -0.020 0.721 0.074 1.000 0.341 -6.670 0.410 0.196-10.5 -0.335 0.05042 -0.024 0.716 0.077 1.000 0.376 -6.639 0.418 0.177-10.0 -0.306 0.04599 -0.030 0.710 0.081 1.000 0.416 -6.655 0.525 0.154-9.5 -0.294 0.04070 -0.036 0.688 0.085 1.000 0.482 -7.212 0.714 0.128-9.0 -0.278 0.03601 -0.042 0.677 0.088 1.000 0.545 -7.733 0.514 0.098-8.5 -0.247 0.03268 -0.048 0.660 0.097 1.000 0.584 -7.560 0.518 0.056-8.0 -0.231 0.02941 -0.055 0.643 0.101 1.000 0.649 -7.839 0.574 0.011-7.5 -0.205 0.02671 -0.062 0.632 0.105 1.000 0.703 -7.663 0.483 -0.052-7.0 -0.175 0.02634 -0.068 0.616 0.114 1.000 0.753 -6.643 0.435 -0.139-6.5 -0.139 0.02293 -0.074 0.604 0.125 1.000 0.795 -6.054 0.383 -0.282-6.0 -0.095 0.02323 -0.079 0.581 0.137 1.000 0.827 -4.079 0.358 -0.582-5.5 -0.049 0.02239 -0.084 0.557 0.144 1.000 0.858 -2.207 0.346 -1.442-5.0 -0.001 0.02026 -0.088 0.538 0.156 1.000 0.885 -0.035 0.469 0.250-4.5 -0.001 0.01778 -0.094 0.522 0.167 1.000 0.954 -0.042 0.382 0.250

-4.0 0.065 0.01750 -0.097 0.502 0.179 1.000 0.955 3.727 0.286 1.731-3.5 0.131 0.01709 -0.099 0.491 0.191 1.000 0.956 7.674 0.286 1.005-3.0 0.197 0.01731 -0.101 0.479 0.199 1.000 0.957 11.387 0.286 0.765-2.5 0.263 0.01698 -0.104 0.467 0.211 1.000 0.958 15.489 0.286 0.645-2.0 0.329 0.02077 -0.106 0.455 0.227 1.000 0.956 15.828 0.286 0.573-1.5 0.394 0.02190 -0.109 0.443 0.243 1.000 0.957 18.001 0.287 0.525-1.0 0.460 0.02124 -0.111 0.435 0.259 0.941 0.957 21.644 0.287 0.491-0.5 0.525 0.02103 -0.113 0.431 0.275 0.907 0.958 24.969 0.384 0.4660.0 0.496 0.02214 -0.116 0.420 0.290 0.899 0.959 22.417 0.437 0.4840.5 0.554 0.02249 -0.119 0.412 0.306 0.892 0.959 24.612 0.303 0.4651.0 0.607 0.02250 -0.122 0.408 0.376 0.880 0.959 26.994 0.305 0.4501.5 0.664 0.02271 -0.125 0.396 0.470 0.873 0.959 29.235 0.303 0.4382.0 0.723 0.02340 -0.128 0.380 0.509 0.869 0.959 30.901 0.305 0.4272.5 0.779 0.02379 -0.131 0.369 0.529 0.861 0.959 32.736 0.307 0.4183.0 0.837 0.02453 -0.134 0.353 0.553 0.858 0.959 34.144 0.308 0.4113.5 0.892 0.02534 -0.138 0.341 0.572 0.850 0.960 35.208 0.313 0.4044.0 0.947 0.02656 -0.141 0.333 0.596 0.843 0.960 35.649 0.319 0.3994.5 0.997 0.02683 -0.145 0.325 0.630 0.831 0.960 37.153 0.317 0.3965.0 1.054 0.02877 -0.149 0.314 0.661 0.827 0.960 36.639 0.320 0.3915.5 1.103 0.02944 -0.153 0.306 0.695 0.816 0.959 37.476 0.332 0.3886.0 1.152 0.03069 -0.157 0.298 0.722 0.805 0.959 37.533 0.334 0.3866.5 1.201 0.03178 -0.161 0.286 0.749 0.793 0.958 37.783 0.331 0.3847.0 1.252 0.03404 -0.165 0.274 0.780 0.785 0.958 36.794 0.340 0.3827.5 1.296 0.03550 -0.169 0.266 0.799 0.770 0.958 36.514 0.350 0.3818.0 1.343 0.03683 -0.174 0.253 0.811 0.759 0.957 36.463 0.347 0.3798.5 1.389 0.03837 -0.178 0.241 0.819 0.747 0.958 36.195 0.344 0.3789.0 1.437 0.04030 -0.183 0.225 0.830 0.739 0.961 35.670 0.349 0.3779.5 1.481 0.04249 -0.187 0.213 0.843 0.727 0.963 34.846 0.359 0.37710.0 1.524 0.04551 -0.192 0.196 0.854 0.716 0.963 33.492 0.369 0.37610.5 1.564 0.04684 -0.197 0.185 0.870 0.701 0.963 33.382 0.371 0.37611.0 1.607 0.05058 -0.202 0.174 0.881 0.690 0.963 31.764 0.374 0.37611.5 1.645 0.05315 -0.207 0.163 0.897 0.675 0.962 30.949 0.390 0.37612.0 1.682 0.05643 -0.213 0.152 0.951 0.660 0.953 29.807 0.396 0.37612.5 1.718 0.05939 -0.218 0.140 0.957 0.645 0.959 28.929 0.391 0.37713.0 1.756 0.06302 -0.223 0.130 0.957 0.634 0.959 27.872 0.411 0.37713.5 1.786 0.06582 -0.229 0.119 0.957 0.615 0.959 27.129 0.418 0.37814.0 1.822 0.06989 -0.234 0.101 0.957 0.604 0.959 26.062 0.407 0.37914.5 1.854 0.07449 -0.240 0.090 0.958 0.589 0.959 24.888 0.427 0.37915.0 1.884 0.07907 -0.245 0.083 0.958 0.574 0.959 23.830 0.433 0.380