Airfoil: NACA 64A010 Builder: B. Champine Comment: clean Number of Reynolds #'s: 9 Average Reynolds #: 22100 Number of angles of attack: 97 alpha / Cl / Cm -6.18 -0.588 0.0000 -5.65 -0.555 0.0000 -5.09 -0.436 0.0000 -4.63 -0.383 0.0000 -4.01 -0.311 0.0000 -3.60 -0.243 0.0000 -3.02 -0.103 0.0000 -2.58 -0.139 0.0000 -1.99 -0.049 0.0000 -1.52 -0.024 0.0000 -0.95 0.019 0.0000 -0.55 0.035 0.0000 0.04 0.044 0.0000 0.46 0.092 0.0000 1.09 0.103 0.0000 1.48 0.125 0.0000 2.01 0.143 0.0000 2.51 0.189 0.0000 3.11 0.245 0.0000 3.51 0.288 0.0000 4.04 0.325 0.0000 4.57 0.386 0.0000 5.15 0.563 0.0000 5.61 0.635 0.0000 6.15 0.660 0.0000 6.65 0.714 0.0000 7.14 0.729 0.0000 7.66 0.755 0.0000 8.19 0.779 0.0000 8.65 0.808 0.0000 9.27 0.836 0.0000 9.64 0.859 0.0000 10.22 0.837 0.0000 10.67 0.823 0.0000 11.18 0.798 0.0000 11.64 0.799 0.0000 12.28 0.756 0.0000 12.68 0.767 0.0000 13.17 0.748 0.0000 13.68 0.775 0.0000 14.18 0.763 0.0000 14.66 0.783 0.0000 15.22 0.842 0.0000 15.68 0.852 0.0000 16.27 0.826 0.0000 16.65 0.884 0.0000 17.31 0.931 0.0000 17.70 0.914 0.0000 18.26 0.989 0.0000 17.82 0.921 0.0000 17.27 0.928 0.0000 16.76 0.847 0.0000 16.29 0.884 0.0000 15.75 0.804 0.0000 15.28 0.835 0.0000 14.78 0.791 0.0000 14.25 0.809 0.0000 13.77 0.811 0.0000 13.22 0.783 0.0000 12.75 0.814 0.0000 12.25 0.817 0.0000 11.77 0.770 0.0000 11.28 0.891 0.0000 10.79 0.906 0.0000 10.31 0.913 0.0000 9.77 0.920 0.0000 9.33 0.903 0.0000 8.81 0.880 0.0000 8.30 0.855 0.0000 7.79 0.837 0.0000 7.30 0.800 0.0000 6.74 0.770 0.0000 6.29 0.738 0.0000 5.70 0.663 0.0000 5.24 0.590 0.0000 4.69 0.443 0.0000 4.13 0.377 0.0000 3.64 0.328 0.0000 3.08 0.285 0.0000 2.62 0.235 0.0000 2.11 0.212 0.0000 1.62 0.176 0.0000 1.07 0.168 0.0000 0.60 0.146 0.0000 0.14 0.138 0.0000 -0.40 0.107 0.0000 -0.91 0.090 0.0000 -1.44 0.037 0.0000 -1.95 0.017 0.0000 -2.44 -0.026 0.0000 -2.98 -0.059 0.0000 -3.48 -0.110 0.0000 -3.94 -0.173 0.0000 -4.50 -0.274 0.0000 -5.01 -0.349 0.0000 -5.59 -0.433 0.0000 -6.10 -0.483 0.0000 Tabulated from data in file MS00242.DAT & reduced using program Q01.00L Average Reynolds #: 30600 Number of angles of attack: 97 alpha / Cl / Cm -6.73 -0.591 0.0000 -5.70 -0.568 0.0000 -5.17 -0.551 0.0000 -4.67 -0.501 0.0000 -4.20 -0.421 0.0000 -3.61 -0.269 0.0000 -3.16 -0.192 0.0000 -2.54 -0.138 0.0000 -2.10 -0.096 0.0000 -1.59 -0.057 0.0000 -1.06 -0.027 0.0000 -0.52 -0.012 0.0000 -0.09 -0.004 0.0000 0.50 0.017 0.0000 0.94 0.022 0.0000 1.54 0.058 0.0000 1.95 0.082 0.0000 2.49 0.139 0.0000 2.94 0.166 0.0000 3.54 0.237 0.0000 4.08 0.356 0.0000 4.60 0.488 0.0000 5.00 0.523 0.0000 5.66 0.572 0.0000 6.05 0.584 0.0000 6.65 0.615 0.0000 7.01 0.651 0.0000 7.69 0.685 0.0000 8.07 0.713 0.0000 8.72 0.755 0.0000 9.16 0.770 0.0000 9.73 0.800 0.0000 10.07 0.840 0.0000 10.64 0.840 0.0000 11.08 0.858 0.0000 11.62 0.771 0.0000 12.13 0.761 0.0000 12.75 0.761 0.0000 13.07 0.694 0.0000 13.68 0.652 0.0000 14.03 0.666 0.0000 14.65 0.677 0.0000 15.10 0.652 0.0000 15.64 0.652 0.0000 16.12 0.673 0.0000 16.66 0.672 0.0000 17.04 0.728 0.0000 17.70 0.733 0.0000 18.16 0.743 0.0000 17.79 0.750 0.0000 17.36 0.725 0.0000 16.79 0.716 0.0000 16.39 0.688 0.0000 15.74 0.660 0.0000 15.36 0.668 0.0000 14.80 0.651 0.0000 14.36 0.650 0.0000 13.73 0.663 0.0000 13.35 0.654 0.0000 12.78 0.661 0.0000 12.35 0.710 0.0000 11.80 0.699 0.0000 11.36 0.735 0.0000 10.82 0.774 0.0000 10.34 0.767 0.0000 9.78 0.774 0.0000 9.36 0.767 0.0000 8.82 0.743 0.0000 8.38 0.707 0.0000 7.80 0.673 0.0000 7.40 0.635 0.0000 6.75 0.613 0.0000 6.38 0.594 0.0000 5.73 0.565 0.0000 5.33 0.531 0.0000 4.70 0.469 0.0000 4.26 0.395 0.0000 3.64 0.277 0.0000 3.29 0.218 0.0000 2.56 0.154 0.0000 2.10 0.115 0.0000 1.62 0.075 0.0000 1.20 0.047 0.0000 0.61 0.025 0.0000 0.21 0.018 0.0000 -0.41 0.015 0.0000 -0.86 -0.004 0.0000 -1.39 -0.026 0.0000 -1.78 -0.051 0.0000 -2.45 -0.100 0.0000 -2.86 -0.132 0.0000 -3.46 -0.200 0.0000 -3.91 -0.293 0.0000 -4.49 -0.405 0.0000 -4.95 -0.469 0.0000 -5.55 -0.514 0.0000 -5.96 -0.539 0.0000 Tabulated from data in file MS00265.DAT & reduced using program Q01.00L Average Reynolds #: 40600 Number of angles of attack: 97 alpha / Cl / Cm -5.97 -0.515 0.0000 -5.64 -0.500 0.0000 -5.05 -0.470 0.0000 -4.65 -0.456 0.0000 -4.07 -0.411 0.0000 -3.62 -0.343 0.0000 -3.06 -0.213 0.0000 -2.54 -0.137 0.0000 -1.99 -0.068 0.0000 -1.49 -0.025 0.0000 -1.03 0.002 0.0000 -0.49 0.014 0.0000 -0.06 0.026 0.0000 0.52 0.049 0.0000 1.05 0.071 0.0000 1.51 0.092 0.0000 2.00 0.125 0.0000 2.53 0.177 0.0000 3.15 0.284 0.0000 3.53 0.367 0.0000 4.08 0.467 0.0000 4.60 0.533 0.0000 5.14 0.560 0.0000 5.65 0.590 0.0000 6.14 0.618 0.0000 6.66 0.647 0.0000 7.14 0.682 0.0000 7.68 0.712 0.0000 8.23 0.751 0.0000 8.68 0.775 0.0000 9.07 0.801 0.0000 9.76 0.841 0.0000 10.20 0.859 0.0000 10.74 0.820 0.0000 11.24 0.869 0.0000 11.76 0.798 0.0000 12.17 0.793 0.0000 12.69 0.772 0.0000 13.28 0.733 0.0000 13.68 0.718 0.0000 14.14 0.714 0.0000 14.68 0.718 0.0000 15.09 0.710 0.0000 15.65 0.699 0.0000 16.25 0.738 0.0000 16.68 0.789 0.0000 17.17 0.788 0.0000 17.72 0.804 0.0000 18.26 0.866 0.0000 17.71 0.790 0.0000 17.26 0.741 0.0000 16.81 0.755 0.0000 16.22 0.756 0.0000 15.74 0.708 0.0000 15.27 0.727 0.0000 14.78 0.697 0.0000 14.38 0.691 0.0000 13.83 0.694 0.0000 13.28 0.737 0.0000 12.83 0.729 0.0000 12.39 0.777 0.0000 11.84 0.811 0.0000 11.30 0.799 0.0000 10.86 0.819 0.0000 10.27 0.801 0.0000 9.81 0.824 0.0000 9.25 0.801 0.0000 8.82 0.776 0.0000 8.29 0.751 0.0000 7.84 0.726 0.0000 7.39 0.695 0.0000 6.77 0.660 0.0000 6.41 0.645 0.0000 5.76 0.613 0.0000 5.25 0.593 0.0000 4.76 0.561 0.0000 4.21 0.505 0.0000 3.71 0.421 0.0000 3.19 0.322 0.0000 2.64 0.244 0.0000 2.10 0.179 0.0000 1.56 0.132 0.0000 1.13 0.100 0.0000 0.62 0.087 0.0000 0.12 0.072 0.0000 -0.33 0.050 0.0000 -0.78 0.025 0.0000 -1.40 -0.004 0.0000 -1.93 -0.033 0.0000 -2.43 -0.097 0.0000 -3.00 -0.180 0.0000 -3.44 -0.264 0.0000 -4.01 -0.377 0.0000 -4.50 -0.427 0.0000 -5.03 -0.468 0.0000 -5.58 -0.499 0.0000 -6.04 -0.522 0.0000 Tabulated from data in file MS00266.DAT & reduced using program Q01.00L Average Reynolds #: 50600 Number of angles of attack: 97 alpha / Cl / Cm -6.24 -0.545 0.0000 -5.65 -0.522 0.0000 -5.23 -0.506 0.0000 -4.62 -0.471 0.0000 -4.23 -0.446 0.0000 -3.67 -0.398 0.0000 -3.18 -0.340 0.0000 -2.57 -0.244 0.0000 -2.12 -0.147 0.0000 -1.50 -0.050 0.0000 -1.01 -0.006 0.0000 -0.49 0.009 0.0000 -0.10 0.020 0.0000 0.55 0.039 0.0000 1.08 0.053 0.0000 1.49 0.082 0.0000 1.96 0.126 0.0000 2.52 0.214 0.0000 2.92 0.304 0.0000 3.57 0.420 0.0000 4.05 0.469 0.0000 4.60 0.512 0.0000 5.07 0.536 0.0000 5.62 0.571 0.0000 6.08 0.591 0.0000 6.68 0.623 0.0000 7.05 0.649 0.0000 7.73 0.695 0.0000 8.08 0.716 0.0000 8.73 0.745 0.0000 9.17 0.773 0.0000 9.71 0.799 0.0000 10.10 0.817 0.0000 10.68 0.838 0.0000 11.16 0.844 0.0000 11.70 0.816 0.0000 12.18 0.851 0.0000 12.72 0.818 0.0000 13.13 0.776 0.0000 13.71 0.780 0.0000 14.05 0.740 0.0000 14.69 0.740 0.0000 15.18 0.782 0.0000 15.72 0.762 0.0000 16.14 0.755 0.0000 16.72 0.803 0.0000 17.09 0.790 0.0000 17.62 0.826 0.0000 18.14 0.852 0.0000 17.81 0.845 0.0000 17.39 0.809 0.0000 16.81 0.805 0.0000 16.45 0.817 0.0000 15.83 0.772 0.0000 15.40 0.731 0.0000 14.80 0.731 0.0000 14.38 0.730 0.0000 13.76 0.733 0.0000 13.40 0.775 0.0000 12.81 0.780 0.0000 12.43 0.810 0.0000 11.79 0.827 0.0000 11.42 0.840 0.0000 10.78 0.844 0.0000 10.25 0.817 0.0000 9.80 0.809 0.0000 9.40 0.787 0.0000 8.79 0.768 0.0000 8.42 0.749 0.0000 7.75 0.711 0.0000 7.37 0.680 0.0000 6.74 0.639 0.0000 6.35 0.613 0.0000 5.72 0.584 0.0000 5.32 0.565 0.0000 4.72 0.536 0.0000 4.30 0.507 0.0000 3.69 0.451 0.0000 3.33 0.404 0.0000 2.68 0.276 0.0000 2.23 0.178 0.0000 1.60 0.104 0.0000 1.23 0.088 0.0000 0.61 0.063 0.0000 0.20 0.044 0.0000 -0.40 0.034 0.0000 -0.87 0.024 0.0000 -1.40 -0.010 0.0000 -1.92 -0.090 0.0000 -2.44 -0.165 0.0000 -2.87 -0.252 0.0000 -3.52 -0.363 0.0000 -3.91 -0.403 0.0000 -4.49 -0.439 0.0000 -4.95 -0.476 0.0000 -5.55 -0.505 0.0000 -5.91 -0.526 0.0000 Tabulated from data in file MS00267.DAT & reduced using program Q01.00L Average Reynolds #: 60900 Number of angles of attack: 97 alpha / Cl / Cm -5.98 -0.539 0.0000 -5.71 -0.527 0.0000 -5.10 -0.498 0.0000 -4.69 -0.477 0.0000 -4.20 -0.440 0.0000 -3.66 -0.391 0.0000 -3.20 -0.361 0.0000 -2.64 -0.314 0.0000 -2.12 -0.229 0.0000 -1.58 -0.123 0.0000 -1.06 -0.025 0.0000 -0.54 0.012 0.0000 -0.08 0.013 0.0000 0.48 0.041 0.0000 0.92 0.059 0.0000 1.48 0.079 0.0000 1.99 0.170 0.0000 2.50 0.287 0.0000 3.11 0.375 0.0000 3.52 0.406 0.0000 4.07 0.462 0.0000 4.54 0.478 0.0000 5.04 0.530 0.0000 5.61 0.566 0.0000 6.07 0.595 0.0000 6.58 0.629 0.0000 7.11 0.664 0.0000 7.66 0.699 0.0000 8.12 0.726 0.0000 8.68 0.754 0.0000 9.08 0.773 0.0000 9.66 0.808 0.0000 10.12 0.825 0.0000 10.72 0.846 0.0000 11.14 0.849 0.0000 11.69 0.855 0.0000 12.15 0.840 0.0000 12.71 0.859 0.0000 13.16 0.811 0.0000 13.65 0.786 0.0000 14.20 0.748 0.0000 14.67 0.752 0.0000 15.19 0.739 0.0000 15.65 0.732 0.0000 16.17 0.740 0.0000 16.67 0.754 0.0000 17.21 0.770 0.0000 17.61 0.803 0.0000 18.18 0.814 0.0000 17.78 0.818 0.0000 17.31 0.783 0.0000 16.75 0.759 0.0000 16.31 0.752 0.0000 15.78 0.750 0.0000 15.35 0.741 0.0000 14.77 0.741 0.0000 14.39 0.781 0.0000 13.77 0.794 0.0000 13.37 0.822 0.0000 12.82 0.838 0.0000 12.37 0.853 0.0000 11.81 0.854 0.0000 11.34 0.844 0.0000 10.78 0.839 0.0000 10.37 0.829 0.0000 9.76 0.805 0.0000 9.38 0.791 0.0000 8.78 0.762 0.0000 8.33 0.738 0.0000 7.73 0.704 0.0000 7.33 0.678 0.0000 6.74 0.638 0.0000 6.37 0.613 0.0000 5.75 0.574 0.0000 5.29 0.545 0.0000 4.74 0.509 0.0000 4.30 0.477 0.0000 3.68 0.431 0.0000 3.27 0.402 0.0000 2.65 0.314 0.0000 2.22 0.224 0.0000 1.58 0.094 0.0000 1.19 0.051 0.0000 0.61 0.035 0.0000 0.16 0.020 0.0000 -0.43 0.027 0.0000 -0.76 0.017 0.0000 -1.45 -0.089 0.0000 -1.90 -0.166 0.0000 -2.50 -0.289 0.0000 -2.94 -0.342 0.0000 -3.51 -0.384 0.0000 -3.96 -0.407 0.0000 -4.55 -0.456 0.0000 -4.98 -0.488 0.0000 -5.59 -0.516 0.0000 -5.94 -0.538 0.0000 Tabulated from data in file MS00268.DAT & reduced using program Q01.00L Average Reynolds #: 80800 Number of angles of attack: 97 alpha / Cl / Cm -5.90 -0.551 0.0000 -5.73 -0.541 0.0000 -5.16 -0.511 0.0000 -4.60 -0.484 0.0000 -4.12 -0.442 0.0000 -3.64 -0.408 0.0000 -3.13 -0.375 0.0000 -2.55 -0.324 0.0000 -2.02 -0.253 0.0000 -1.55 -0.179 0.0000 -1.04 -0.097 0.0000 -0.51 -0.016 0.0000 0.06 0.018 0.0000 0.47 0.021 0.0000 0.96 0.039 0.0000 1.49 0.128 0.0000 2.09 0.245 0.0000 2.54 0.323 0.0000 3.14 0.377 0.0000 3.58 0.411 0.0000 4.08 0.450 0.0000 4.59 0.491 0.0000 5.15 0.525 0.0000 5.64 0.556 0.0000 6.08 0.587 0.0000 6.62 0.624 0.0000 7.15 0.662 0.0000 7.69 0.696 0.0000 8.20 0.728 0.0000 8.72 0.760 0.0000 9.21 0.790 0.0000 9.73 0.799 0.0000 10.19 0.809 0.0000 10.70 0.830 0.0000 11.20 0.812 0.0000 11.72 0.793 0.0000 12.18 0.808 0.0000 12.70 0.812 0.0000 13.24 0.812 0.0000 13.67 0.768 0.0000 14.25 0.771 0.0000 14.68 0.793 0.0000 15.25 0.716 0.0000 15.64 0.706 0.0000 16.10 0.728 0.0000 16.68 0.747 0.0000 17.17 0.739 0.0000 17.65 0.792 0.0000 18.20 0.780 0.0000 17.71 0.747 0.0000 17.29 0.764 0.0000 16.82 0.743 0.0000 16.26 0.734 0.0000 15.83 0.726 0.0000 15.24 0.721 0.0000 14.85 0.762 0.0000 14.29 0.772 0.0000 13.80 0.791 0.0000 13.31 0.792 0.0000 12.81 0.792 0.0000 12.24 0.774 0.0000 11.85 0.793 0.0000 11.29 0.805 0.0000 10.83 0.808 0.0000 10.42 0.802 0.0000 9.83 0.793 0.0000 9.38 0.774 0.0000 8.81 0.746 0.0000 8.29 0.716 0.0000 7.82 0.688 0.0000 7.21 0.647 0.0000 6.72 0.614 0.0000 6.32 0.585 0.0000 5.76 0.545 0.0000 5.24 0.512 0.0000 4.74 0.483 0.0000 4.30 0.447 0.0000 3.69 0.400 0.0000 3.20 0.367 0.0000 2.73 0.320 0.0000 2.29 0.255 0.0000 1.64 0.143 0.0000 1.10 0.038 0.0000 0.61 0.001 0.0000 0.05 0.000 0.0000 -0.46 -0.029 0.0000 -0.95 -0.099 0.0000 -1.45 -0.176 0.0000 -2.00 -0.268 0.0000 -2.55 -0.341 0.0000 -2.99 -0.381 0.0000 -3.49 -0.418 0.0000 -3.88 -0.447 0.0000 -4.53 -0.491 0.0000 -5.06 -0.523 0.0000 -5.51 -0.548 0.0000 -6.15 -0.590 0.0000 Tabulated from data in file MS00269.DAT & reduced using program Q01.00L Average Reynolds #: 101000 Number of angles of attack: 97 alpha / Cl / Cm -6.25 -0.584 0.0000 -5.68 -0.544 0.0000 -5.21 -0.518 0.0000 -4.62 -0.484 0.0000 -4.15 -0.455 0.0000 -3.65 -0.413 0.0000 -3.08 -0.370 0.0000 -2.66 -0.341 0.0000 -2.14 -0.300 0.0000 -1.59 -0.243 0.0000 -1.07 -0.164 0.0000 -0.54 -0.082 0.0000 -0.05 -0.002 0.0000 0.46 0.010 0.0000 0.95 0.092 0.0000 1.46 0.184 0.0000 2.04 0.283 0.0000 2.53 0.336 0.0000 3.11 0.380 0.0000 3.54 0.411 0.0000 4.06 0.452 0.0000 4.53 0.481 0.0000 5.04 0.512 0.0000 5.59 0.549 0.0000 6.04 0.581 0.0000 6.60 0.622 0.0000 7.06 0.655 0.0000 7.63 0.693 0.0000 8.15 0.726 0.0000 8.64 0.759 0.0000 9.14 0.791 0.0000 9.67 0.801 0.0000 10.15 0.793 0.0000 10.64 0.798 0.0000 11.11 0.808 0.0000 11.69 0.804 0.0000 12.16 0.785 0.0000 12.66 0.816 0.0000 13.11 0.777 0.0000 13.71 0.783 0.0000 14.20 0.778 0.0000 14.63 0.762 0.0000 15.19 0.717 0.0000 15.60 0.705 0.0000 16.14 0.738 0.0000 16.67 0.747 0.0000 17.18 0.773 0.0000 17.71 0.741 0.0000 18.13 0.745 0.0000 17.81 0.743 0.0000 17.35 0.769 0.0000 16.74 0.725 0.0000 16.37 0.728 0.0000 15.78 0.727 0.0000 15.31 0.724 0.0000 14.78 0.780 0.0000 14.34 0.779 0.0000 13.81 0.785 0.0000 13.31 0.783 0.0000 12.79 0.799 0.0000 12.35 0.785 0.0000 11.77 0.788 0.0000 11.37 0.814 0.0000 10.79 0.828 0.0000 10.37 0.807 0.0000 9.79 0.806 0.0000 9.36 0.787 0.0000 8.81 0.763 0.0000 8.32 0.730 0.0000 7.76 0.692 0.0000 7.34 0.663 0.0000 6.76 0.623 0.0000 6.32 0.591 0.0000 5.67 0.544 0.0000 5.30 0.517 0.0000 4.67 0.478 0.0000 4.27 0.458 0.0000 3.69 0.410 0.0000 3.21 0.373 0.0000 2.66 0.333 0.0000 2.27 0.298 0.0000 1.61 0.205 0.0000 1.18 0.122 0.0000 0.58 0.019 0.0000 0.19 -0.020 0.0000 -0.46 -0.076 0.0000 -0.89 -0.142 0.0000 -1.50 -0.236 0.0000 -1.87 -0.282 0.0000 -2.49 -0.334 0.0000 -2.95 -0.369 0.0000 -3.51 -0.407 0.0000 -4.01 -0.447 0.0000 -4.54 -0.481 0.0000 -4.97 -0.506 0.0000 -5.55 -0.541 0.0000 -6.08 -0.576 0.0000 Tabulated from data in file MS00270.DAT & reduced using program Q01.00L Average Reynolds #: 204000 Number of angles of attack: 33 alpha / Cl / Cm -6.03 -0.568 0.0000 -4.45 -0.459 0.0000 -2.69 -0.317 0.0000 -1.16 -0.146 0.0000 0.15 0.018 0.0000 1.63 0.183 0.0000 3.38 0.389 0.0000 4.68 0.486 0.0000 6.12 0.595 0.0000 7.70 0.713 0.0000 9.21 0.817 0.0000 10.77 0.857 0.0000 12.42 0.821 0.0000 13.78 0.778 0.0000 15.23 0.699 0.0000 16.94 0.712 0.0000 18.42 0.789 0.0000 16.62 0.717 0.0000 14.98 0.698 0.0000 13.66 0.808 0.0000 12.18 0.837 0.0000 10.70 0.859 0.0000 9.28 0.821 0.0000 7.68 0.704 0.0000 6.15 0.593 0.0000 4.61 0.473 0.0000 3.03 0.351 0.0000 1.52 0.162 0.0000 -0.01 -0.009 0.0000 -1.55 -0.210 0.0000 -3.43 -0.394 0.0000 -4.93 -0.504 0.0000 -6.28 -0.598 0.0000 Tabulated from data in file AB00247.DAT & reduced using program Q01.00L Average Reynolds #: 305400 Number of angles of attack: 33 alpha / Cl / Cm -6.25 -0.597 0.0000 -4.41 -0.460 0.0000 -2.65 -0.300 0.0000 -1.01 -0.094 0.0000 0.33 0.030 0.0000 1.66 0.157 0.0000 3.23 0.357 0.0000 4.62 0.479 0.0000 6.14 0.601 0.0000 7.72 0.717 0.0000 9.22 0.819 0.0000 10.78 0.868 0.0000 12.25 0.858 0.0000 13.80 0.786 0.0000 15.34 0.712 0.0000 17.00 0.738 0.0000 18.45 0.840 0.0000 16.49 0.720 0.0000 15.03 0.704 0.0000 13.73 0.826 0.0000 12.26 0.858 0.0000 10.77 0.860 0.0000 9.18 0.816 0.0000 7.65 0.706 0.0000 6.13 0.592 0.0000 4.65 0.475 0.0000 3.13 0.338 0.0000 1.57 0.142 0.0000 -0.15 -0.017 0.0000 -1.66 -0.179 0.0000 -3.58 -0.407 0.0000 -5.00 -0.511 0.0000 -6.32 -0.609 0.0000 Tabulated from data in file AB00249.DAT & reduced using program Q01.00L File n64a.lft created on 12-05-1997 at 15:25:50 using program FORMAT