Airfoil: S1210 Builder: M. Allen Comment: clean Number of Reynolds #'s: 8 Average Reynolds #: 61100 Number of angles of attack: 53 alpha / Cl / Cm -6.22 -0.273 -0.2500 -5.15 -0.168 -0.2500 -4.15 0.183 -0.2500 -2.97 0.369 -0.2500 -1.98 0.504 -0.2500 -0.96 0.614 -0.2500 0.04 0.742 -0.2500 1.01 0.830 -0.2500 2.18 0.950 -0.2500 3.09 0.968 -0.2500 4.25 0.914 -0.2500 5.16 0.910 -0.2500 6.11 0.954 -0.2500 7.10 0.946 -0.2500 8.05 0.984 -0.2500 8.98 1.019 -0.2500 10.24 1.056 -0.2500 11.14 1.085 -0.2500 12.08 1.121 -0.2500 13.27 1.122 -0.2500 14.28 1.154 -0.2500 15.35 1.193 -0.2500 16.37 1.194 -0.2500 17.15 1.225 -0.2500 18.17 1.272 -0.2500 19.24 1.284 -0.2500 20.33 1.289 -0.2500 19.00 1.291 -0.2500 18.19 1.228 -0.2500 17.16 1.275 -0.2500 16.03 1.203 -0.2500 14.92 1.163 -0.2500 14.10 1.092 -0.2500 13.08 1.108 -0.2500 12.06 1.064 -0.2500 10.94 1.097 -0.2500 10.17 1.054 -0.2500 8.99 0.998 -0.2500 8.04 0.972 -0.2500 7.11 0.941 -0.2500 6.13 0.927 -0.2500 5.09 0.894 -0.2500 4.06 0.862 -0.2500 3.10 0.926 -0.2500 2.14 0.919 -0.2500 1.10 0.840 -0.2500 -0.12 0.692 -0.2500 -1.07 0.577 -0.2500 -1.97 0.503 -0.2500 -3.11 0.346 -0.2500 -4.27 0.192 -0.2500 -5.14 -0.182 -0.2500 -6.28 -0.246 -0.2500 Tabulated from data in file JG00127.DAT & reduced using program Q01.00L Average Reynolds #: 81200 Number of angles of attack: 53 alpha / Cl / Cm -6.42 -0.301 -0.2500 -5.22 -0.249 -0.2500 -4.04 0.194 -0.2500 -3.00 0.364 -0.2500 -1.94 0.560 -0.2500 -0.71 0.705 -0.2500 0.22 0.801 -0.2500 1.12 0.895 -0.2500 2.33 0.990 -0.2500 3.28 1.040 -0.2500 4.20 1.013 -0.2500 5.36 0.992 -0.2500 6.27 0.946 -0.2500 7.21 0.970 -0.2500 8.21 1.012 -0.2500 9.24 1.094 -0.2500 10.49 1.631 -0.2500 11.38 1.699 -0.2500 12.55 1.755 -0.2500 13.42 1.774 -0.2500 14.34 1.796 -0.2500 15.33 1.303 -0.2500 16.42 1.234 -0.2500 17.44 1.266 -0.2500 18.44 1.215 -0.2500 19.24 1.281 -0.2500 20.26 1.325 -0.2500 18.91 1.238 -0.2500 18.03 1.257 -0.2500 16.94 1.253 -0.2500 16.05 1.246 -0.2500 15.03 1.344 -0.2500 14.03 1.391 -0.2500 13.27 1.741 -0.2500 12.21 1.705 -0.2500 11.19 1.661 -0.2500 10.24 1.605 -0.2500 9.19 1.530 -0.2500 8.14 1.446 -0.2500 7.18 1.350 -0.2500 6.05 0.905 -0.2500 5.04 0.939 -0.2500 3.91 0.979 -0.2500 2.90 0.977 -0.2500 2.00 0.938 -0.2500 1.00 0.847 -0.2500 -0.03 0.747 -0.2500 -1.02 0.650 -0.2500 -2.11 0.512 -0.2500 -3.15 0.313 -0.2500 -4.16 0.163 -0.2500 -5.35 -0.283 -0.2500 -6.32 -0.313 -0.2500 Tabulated from data in file JG00484.DAT & reduced using program Q01.00L Average Reynolds #: 91300 Number of angles of attack: 53 alpha / Cl / Cm -6.12 -0.281 -0.2500 -5.16 -0.210 -0.2500 -3.99 0.231 -0.2500 -2.99 0.431 -0.2500 -1.91 0.601 -0.2500 -0.89 0.724 -0.2500 0.08 0.814 -0.2500 1.36 0.934 -0.2500 2.13 1.006 -0.2500 3.34 1.115 -0.2500 4.31 1.189 -0.2500 5.27 1.272 -0.2500 6.27 1.351 -0.2500 7.30 1.440 -0.2500 8.50 1.536 -0.2500 9.43 1.598 -0.2500 10.33 1.662 -0.2500 11.49 1.736 -0.2500 12.32 1.755 -0.2500 13.48 1.772 -0.2500 14.31 1.780 -0.2500 15.46 1.768 -0.2500 16.18 1.173 -0.2500 17.49 1.203 -0.2500 18.23 1.220 -0.2500 19.37 1.274 -0.2500 20.48 1.316 -0.2500 18.91 1.261 -0.2500 17.88 1.231 -0.2500 16.95 1.177 -0.2500 16.05 1.188 -0.2500 14.95 1.214 -0.2500 14.09 1.218 -0.2500 13.07 1.268 -0.2500 12.08 1.729 -0.2500 11.22 1.693 -0.2500 10.21 1.637 -0.2500 9.15 1.562 -0.2500 8.08 1.481 -0.2500 7.19 1.411 -0.2500 6.06 1.314 -0.2500 5.00 1.225 -0.2500 3.90 1.136 -0.2500 2.98 1.066 -0.2500 2.04 0.983 -0.2500 0.90 0.871 -0.2500 -0.08 0.772 -0.2500 -1.20 0.670 -0.2500 -2.19 0.541 -0.2500 -3.16 0.367 -0.2500 -4.30 0.156 -0.2500 -5.33 -0.235 -0.2500 -6.35 -0.289 -0.2500 Tabulated from data in file JG00485.DAT & reduced using program Q01.00L Average Reynolds #: 101500 Number of angles of attack: 53 alpha / Cl / Cm -6.23 -0.257 -0.2500 -5.18 -0.122 -0.2500 -3.98 0.339 -0.2500 -3.08 0.501 -0.2500 -2.03 0.664 -0.2500 -1.00 0.764 -0.2500 -0.04 0.850 -0.2500 1.05 0.955 -0.2500 2.09 1.057 -0.2500 3.14 1.159 -0.2500 4.22 1.244 -0.2500 5.23 1.332 -0.2500 6.32 1.428 -0.2500 7.17 1.500 -0.2500 8.28 1.585 -0.2500 9.39 1.663 -0.2500 10.21 1.721 -0.2500 11.19 1.772 -0.2500 12.35 1.786 -0.2500 13.34 1.812 -0.2500 14.27 1.809 -0.2500 15.17 1.797 -0.2500 16.15 1.193 -0.2500 17.38 1.237 -0.2500 18.33 1.225 -0.2500 19.32 1.323 -0.2500 20.40 1.335 -0.2500 19.21 1.268 -0.2500 18.03 1.274 -0.2500 16.99 1.228 -0.2500 15.98 1.207 -0.2500 15.09 1.196 -0.2500 14.15 1.272 -0.2500 13.11 1.260 -0.2500 12.15 1.794 -0.2500 11.21 1.758 -0.2500 10.28 1.716 -0.2500 9.27 1.647 -0.2500 8.23 1.570 -0.2500 7.19 1.486 -0.2500 6.13 1.396 -0.2500 5.10 1.306 -0.2500 4.20 1.228 -0.2500 3.17 1.149 -0.2500 2.11 1.046 -0.2500 1.01 0.936 -0.2500 -0.06 0.832 -0.2500 -1.16 0.733 -0.2500 -2.01 0.651 -0.2500 -3.18 0.461 -0.2500 -4.09 0.292 -0.2500 -5.18 -0.147 -0.2500 -6.15 -0.254 -0.2500 Tabulated from data in file JG00128.DAT & reduced using program Q01.00L Average Reynolds #: 151900 Number of angles of attack: 65 alpha / Cl / Cm -8.09 -0.241 -0.2500 -7.02 -0.248 -0.2500 -6.14 -0.187 -0.2500 -4.87 0.199 -0.2500 -3.84 0.407 -0.2500 -2.61 0.607 -0.2500 -1.69 0.701 -0.2500 -0.52 0.808 -0.2500 0.23 0.879 -0.2500 1.37 0.993 -0.2500 2.48 1.099 -0.2500 3.54 1.193 -0.2500 4.25 1.253 -0.2500 5.38 1.348 -0.2500 6.46 1.445 -0.2500 7.52 1.533 -0.2500 8.50 1.605 -0.2500 9.51 1.679 -0.2500 10.48 1.730 -0.2500 11.42 1.757 -0.2500 12.37 1.780 -0.2500 13.57 1.798 -0.2500 14.49 1.804 -0.2500 15.61 1.809 -0.2500 16.62 1.798 -0.2500 17.40 1.792 -0.2500 18.34 1.762 -0.2500 19.52 1.275 -0.2500 20.47 1.296 -0.2500 21.43 1.343 -0.2500 22.50 1.351 -0.2500 23.21 1.398 -0.2500 24.36 1.483 -0.2500 22.89 1.352 -0.2500 21.93 1.338 -0.2500 21.02 1.309 -0.2500 19.98 1.291 -0.2500 18.95 1.226 -0.2500 17.95 1.233 -0.2500 16.85 1.230 -0.2500 15.77 1.223 -0.2500 14.78 1.253 -0.2500 14.12 1.811 -0.2500 13.06 1.787 -0.2500 12.06 1.762 -0.2500 11.11 1.747 -0.2500 10.02 1.714 -0.2500 9.05 1.646 -0.2500 7.88 1.557 -0.2500 6.87 1.473 -0.2500 5.89 1.390 -0.2500 4.95 1.304 -0.2500 3.97 1.224 -0.2500 2.80 1.117 -0.2500 1.82 1.029 -0.2500 0.85 0.936 -0.2500 -0.16 0.838 -0.2500 -1.20 0.743 -0.2500 -2.26 0.645 -0.2500 -3.39 0.486 -0.2500 -4.50 0.280 -0.2500 -5.50 -0.109 -0.2500 -6.32 -0.215 -0.2500 -7.25 -0.244 -0.2500 -8.20 -0.240 -0.2500 Tabulated from data in file JG00545.DAT & reduced using program Q01.00L Average Reynolds #: 201800 Number of angles of attack: 65 alpha / Cl / Cm -8.39 -0.252 -0.2500 -6.97 -0.225 -0.2500 -5.87 -0.090 -0.2500 -5.29 0.218 -0.2500 -3.98 0.454 -0.2500 -2.97 0.582 -0.2500 -1.81 0.704 -0.2500 -0.86 0.793 -0.2500 0.18 0.895 -0.2500 1.28 1.003 -0.2500 2.33 1.110 -0.2500 3.20 1.192 -0.2500 4.41 1.302 -0.2500 5.51 1.388 -0.2500 6.33 1.460 -0.2500 7.34 1.544 -0.2500 8.60 1.645 -0.2500 9.55 1.712 -0.2500 10.61 1.770 -0.2500 11.50 1.791 -0.2500 12.61 1.816 -0.2500 13.54 1.826 -0.2500 14.73 1.835 -0.2500 15.67 1.840 -0.2500 16.66 1.829 -0.2500 17.67 1.814 -0.2500 18.51 1.806 -0.2500 19.66 1.794 -0.2500 20.69 1.768 -0.2500 21.79 1.760 -0.2500 22.58 1.748 -0.2500 23.48 1.739 -0.2500 24.33 1.709 -0.2500 22.91 1.772 -0.2500 21.83 1.763 -0.2500 20.92 1.778 -0.2500 19.97 1.778 -0.2500 18.93 1.804 -0.2500 17.94 1.815 -0.2500 17.08 1.821 -0.2500 16.13 1.832 -0.2500 15.09 1.841 -0.2500 14.08 1.834 -0.2500 12.99 1.822 -0.2500 12.08 1.802 -0.2500 10.92 1.776 -0.2500 9.81 1.725 -0.2500 8.95 1.665 -0.2500 7.76 1.564 -0.2500 6.88 1.492 -0.2500 5.79 1.401 -0.2500 4.73 1.308 -0.2500 3.96 1.245 -0.2500 2.72 1.129 -0.2500 1.75 1.036 -0.2500 0.89 0.949 -0.2500 -0.22 0.840 -0.2500 -1.10 0.755 -0.2500 -2.12 0.658 -0.2500 -3.11 0.542 -0.2500 -4.40 0.362 -0.2500 -5.23 0.202 -0.2500 -6.38 -0.177 -0.2500 -7.19 -0.236 -0.2500 -8.25 -0.242 -0.2500 Tabulated from data in file JG00544.DAT & reduced using program Q01.00L Average Reynolds #: 252100 Number of angles of attack: 53 alpha / Cl / Cm -5.98 -0.063 -0.2500 -5.30 0.234 -0.2500 -4.17 0.433 -0.2500 -3.14 0.580 -0.2500 -2.13 0.697 -0.2500 -1.07 0.800 -0.2500 -0.06 0.900 -0.2500 0.98 1.007 -0.2500 2.02 1.108 -0.2500 3.05 1.209 -0.2500 4.05 1.304 -0.2500 5.08 1.390 -0.2500 6.11 1.476 -0.2500 7.14 1.563 -0.2500 8.14 1.643 -0.2500 9.17 1.717 -0.2500 10.19 1.773 -0.2500 11.20 1.806 -0.2500 12.26 1.834 -0.2500 13.33 1.852 -0.2500 14.52 1.862 -0.2500 15.49 1.861 -0.2500 16.44 1.856 -0.2500 17.38 1.855 -0.2500 18.27 1.854 -0.2500 19.23 1.831 -0.2500 20.23 1.826 -0.2500 19.15 1.847 -0.2500 18.03 1.840 -0.2500 17.09 1.850 -0.2500 16.09 1.860 -0.2500 15.19 1.858 -0.2500 14.07 1.854 -0.2500 13.08 1.839 -0.2500 12.03 1.819 -0.2500 11.07 1.796 -0.2500 10.13 1.760 -0.2500 9.13 1.705 -0.2500 8.19 1.634 -0.2500 7.16 1.552 -0.2500 6.17 1.470 -0.2500 5.17 1.384 -0.2500 4.14 1.297 -0.2500 3.12 1.201 -0.2500 2.07 1.098 -0.2500 1.04 0.996 -0.2500 0.04 0.896 -0.2500 -0.97 0.795 -0.2500 -2.01 0.694 -0.2500 -3.03 0.576 -0.2500 -4.10 0.424 -0.2500 -5.13 0.244 -0.2500 -6.16 -0.102 -0.2500 Tabulated from data in file AB00489.DAT & reduced using program Q01.00L Average Reynolds #: 302500 Number of angles of attack: 57 alpha / Cl / Cm -8.09 -0.240 -0.2500 -7.19 -0.193 -0.2500 -6.07 -0.060 -0.2500 -5.14 0.280 -0.2500 -4.15 0.436 -0.2500 -3.08 0.575 -0.2500 -2.05 0.688 -0.2500 -1.04 0.788 -0.2500 -0.00 0.894 -0.2500 1.02 0.998 -0.2500 2.05 1.101 -0.2500 3.09 1.205 -0.2500 4.11 1.301 -0.2500 5.13 1.394 -0.2500 6.15 1.477 -0.2500 7.16 1.561 -0.2500 8.20 1.642 -0.2500 9.17 1.708 -0.2500 10.21 1.765 -0.2500 11.23 1.798 -0.2500 12.23 1.824 -0.2500 13.19 1.842 -0.2500 14.16 1.851 -0.2500 15.17 1.854 -0.2500 16.20 1.841 -0.2500 17.19 1.836 -0.2500 18.20 1.840 -0.2500 19.19 1.836 -0.2500 20.21 1.881 -0.2500 19.27 1.839 -0.2500 18.24 1.843 -0.2500 17.30 1.836 -0.2500 16.19 1.845 -0.2500 15.14 1.845 -0.2500 14.10 1.842 -0.2500 13.18 1.835 -0.2500 12.19 1.817 -0.2500 11.25 1.791 -0.2500 10.19 1.755 -0.2500 9.21 1.704 -0.2500 8.16 1.629 -0.2500 7.17 1.548 -0.2500 6.15 1.462 -0.2500 5.12 1.376 -0.2500 4.08 1.281 -0.2500 3.09 1.184 -0.2500 2.07 1.082 -0.2500 1.02 0.975 -0.2500 0.02 0.873 -0.2500 -0.99 0.771 -0.2500 -2.04 0.670 -0.2500 -3.08 0.552 -0.2500 -4.09 0.419 -0.2500 -5.14 0.249 -0.2500 -6.27 -0.107 -0.2500 -7.15 -0.199 -0.2500 -8.13 -0.256 -0.2500 Tabulated from data in file JG00494.DAT & reduced using program Q01.00L File s1210.lft created on 12-05-1997 at 15:25:51 using program FORMAT