Airfoil: S1223 RTL Builder: C. Richardson Comment: clean Number of Reynolds #'s: 5 Average Reynolds #: 100700 Number of angles of attack: 61 alpha / Cl / Cm -6.75 -0.464 -0.2480 -5.15 -0.285 -0.2480 -4.02 -0.041 -0.2480 -2.94 0.105 -0.2480 -1.91 0.458 -0.2480 -0.93 0.589 -0.2480 0.19 0.716 -0.2480 1.30 0.823 -0.2480 2.07 0.887 -0.2480 3.21 0.980 -0.2480 4.33 1.060 -0.2480 5.11 1.109 -0.2480 6.30 1.170 -0.2480 6.98 0.787 -0.2480 8.34 0.756 -0.2480 9.13 0.772 -0.2480 10.27 0.824 -0.2480 11.08 0.860 -0.2480 12.20 0.885 -0.2480 13.30 0.923 -0.2480 14.06 0.947 -0.2480 15.32 0.981 -0.2480 16.02 1.018 -0.2480 17.13 1.020 -0.2480 18.17 1.061 -0.2480 19.16 1.097 -0.2480 19.95 1.145 -0.2480 21.07 1.167 -0.2480 22.11 1.213 -0.2480 23.20 1.237 -0.2480 24.08 1.208 -0.2480 22.46 1.185 -0.2480 21.62 1.125 -0.2480 20.39 1.122 -0.2480 19.53 1.084 -0.2480 18.39 1.045 -0.2480 17.43 1.030 -0.2480 16.31 0.992 -0.2480 15.47 0.951 -0.2480 14.42 0.949 -0.2480 13.37 0.937 -0.2480 12.43 0.891 -0.2480 11.50 0.839 -0.2480 10.46 0.836 -0.2480 9.42 0.797 -0.2480 8.37 0.815 -0.2480 7.41 0.771 -0.2480 6.52 0.897 -0.2480 5.54 1.112 -0.2480 4.49 1.051 -0.2480 3.33 0.962 -0.2480 2.53 0.899 -0.2480 1.51 0.816 -0.2480 0.46 0.706 -0.2480 -0.71 0.577 -0.2480 -1.66 0.461 -0.2480 -2.78 0.154 -0.2480 -3.75 -0.053 -0.2480 -4.94 -0.249 -0.2480 -5.95 -0.394 -0.2480 -6.89 -0.447 -0.2480 Tabulated from data in file CL00970.DAT & reduced using program Q02.00L Average Reynolds #: 150100 Number of angles of attack: 61 alpha / Cl / Cm -6.03 0.031 -0.2480 -5.12 0.129 -0.2480 -3.97 0.247 -0.2480 -3.00 0.343 -0.2480 -2.14 0.731 -0.2480 -0.79 0.914 -0.2480 0.31 1.035 -0.2480 1.07 1.118 -0.2480 2.49 1.248 -0.2480 3.34 1.316 -0.2480 4.48 1.399 -0.2480 5.37 1.455 -0.2480 6.16 1.501 -0.2480 7.32 1.556 -0.2480 8.20 1.035 -0.2480 9.04 1.043 -0.2480 10.08 1.075 -0.2480 11.44 1.098 -0.2480 12.26 1.154 -0.2480 13.27 1.201 -0.2480 14.27 1.207 -0.2480 15.37 1.227 -0.2480 16.23 1.261 -0.2480 17.24 1.290 -0.2480 18.27 1.319 -0.2480 19.36 1.353 -0.2480 20.36 1.359 -0.2480 21.07 1.404 -0.2480 22.39 1.449 -0.2480 23.41 1.506 -0.2480 24.13 1.521 -0.2480 22.56 1.477 -0.2480 21.52 1.458 -0.2480 20.70 1.396 -0.2480 19.51 1.325 -0.2480 18.66 1.304 -0.2480 17.54 1.265 -0.2480 16.70 1.231 -0.2480 15.60 1.180 -0.2480 14.47 1.196 -0.2480 13.64 1.164 -0.2480 12.57 1.105 -0.2480 11.25 1.094 -0.2480 10.45 1.081 -0.2480 9.45 1.063 -0.2480 8.56 1.008 -0.2480 7.49 1.023 -0.2480 6.50 1.484 -0.2480 5.59 1.433 -0.2480 4.42 1.366 -0.2480 3.59 1.314 -0.2480 2.46 1.224 -0.2480 1.35 1.131 -0.2480 0.31 1.018 -0.2480 -0.50 0.927 -0.2480 -1.75 0.779 -0.2480 -2.61 0.478 -0.2480 -3.77 0.266 -0.2480 -4.72 0.170 -0.2480 -5.76 0.055 -0.2480 -6.71 -0.016 -0.2480 Tabulated from data in file CL00971.DAT & reduced using program Q02.00L Average Reynolds #: 200200 Number of angles of attack: 61 alpha / Cl / Cm -6.75 0.044 -0.2480 -4.98 0.163 -0.2480 -4.15 0.228 -0.2480 -3.05 0.355 -0.2480 -2.24 0.753 -0.2480 -0.90 0.929 -0.2480 0.24 1.058 -0.2480 1.15 1.153 -0.2480 2.32 1.252 -0.2480 3.23 1.327 -0.2480 4.18 1.399 -0.2480 5.21 1.465 -0.2480 6.42 1.547 -0.2480 7.44 1.621 -0.2480 8.44 1.679 -0.2480 9.36 1.721 -0.2480 10.31 1.765 -0.2480 11.26 1.804 -0.2480 12.09 1.134 -0.2480 13.08 1.156 -0.2480 14.09 1.183 -0.2480 15.06 1.217 -0.2480 16.04 1.244 -0.2480 17.27 1.263 -0.2480 18.13 1.302 -0.2480 19.10 1.310 -0.2480 20.28 1.402 -0.2480 21.20 1.453 -0.2480 22.16 1.474 -0.2480 23.23 1.535 -0.2480 23.99 1.549 -0.2480 22.74 1.479 -0.2480 21.66 1.440 -0.2480 20.68 1.388 -0.2480 19.44 1.330 -0.2480 18.57 1.272 -0.2480 17.55 1.283 -0.2480 16.65 1.233 -0.2480 15.65 1.235 -0.2480 14.48 1.173 -0.2480 13.51 1.155 -0.2480 12.64 1.154 -0.2480 11.47 1.123 -0.2480 10.50 1.091 -0.2480 9.60 1.095 -0.2480 8.42 1.064 -0.2480 7.67 1.059 -0.2480 6.73 1.551 -0.2480 5.49 1.473 -0.2480 4.70 1.428 -0.2480 3.60 1.342 -0.2480 2.51 1.253 -0.2480 1.56 1.172 -0.2480 0.55 1.077 -0.2480 -0.46 0.961 -0.2480 -1.46 0.844 -0.2480 -2.39 0.603 -0.2480 -3.70 0.259 -0.2480 -4.94 0.159 -0.2480 -5.73 0.145 -0.2480 -6.71 0.039 -0.2480 Tabulated from data in file CL00972.DAT & reduced using program Q02.00L Average Reynolds #: 250000 Number of angles of attack: 61 alpha / Cl / Cm -6.05 0.101 -0.2480 -5.05 0.176 -0.2480 -3.93 0.249 -0.2480 -3.09 0.369 -0.2480 -2.10 0.794 -0.2480 -0.99 0.930 -0.2480 -0.08 1.029 -0.2480 1.03 1.151 -0.2480 1.97 1.233 -0.2480 3.10 1.330 -0.2480 4.22 1.421 -0.2480 5.14 1.495 -0.2480 6.24 1.569 -0.2480 7.23 1.643 -0.2480 8.24 1.711 -0.2480 9.29 1.773 -0.2480 10.37 1.845 -0.2480 11.52 1.922 -0.2480 12.46 1.974 -0.2480 13.36 2.022 -0.2480 14.60 2.068 -0.2480 15.37 2.093 -0.2480 16.59 2.107 -0.2480 17.33 2.119 -0.2480 17.65 1.269 -0.2480 18.89 1.324 -0.2480 19.82 1.415 -0.2480 20.82 1.438 -0.2480 21.83 1.489 -0.2480 22.86 1.518 -0.2480 23.89 1.516 -0.2480 22.98 1.530 -0.2480 21.83 1.473 -0.2480 20.71 1.431 -0.2480 19.76 1.401 -0.2480 18.67 1.312 -0.2480 17.66 1.289 -0.2480 16.64 1.258 -0.2480 15.65 1.207 -0.2480 14.71 1.178 -0.2480 13.58 1.184 -0.2480 12.65 1.182 -0.2480 11.65 1.125 -0.2480 10.68 1.108 -0.2480 9.64 1.076 -0.2480 8.52 1.082 -0.2480 7.71 1.108 -0.2480 6.99 1.615 -0.2480 5.72 1.511 -0.2480 4.48 1.429 -0.2480 3.53 1.356 -0.2480 2.63 1.283 -0.2480 1.60 1.194 -0.2480 0.61 1.099 -0.2480 -0.36 0.989 -0.2480 -1.47 0.860 -0.2480 -2.53 0.651 -0.2480 -3.27 0.334 -0.2480 -4.63 0.179 -0.2480 -5.63 0.123 -0.2480 -6.71 0.064 -0.2480 Tabulated from data in file CL00973.DAT & reduced using program Q02.00L Average Reynolds #: 299700 Number of angles of attack: 61 alpha / Cl / Cm -5.94 0.131 -0.2480 -5.23 0.154 -0.2480 -4.06 0.255 -0.2480 -3.12 0.421 -0.2480 -2.33 0.773 -0.2480 -1.27 0.910 -0.2480 -0.25 1.023 -0.2480 0.80 1.141 -0.2480 1.84 1.239 -0.2480 2.85 1.327 -0.2480 3.89 1.417 -0.2480 4.97 1.507 -0.2480 6.02 1.583 -0.2480 7.01 1.659 -0.2480 8.20 1.738 -0.2480 9.10 1.803 -0.2480 10.26 1.878 -0.2480 11.31 1.966 -0.2480 12.26 2.022 -0.2480 13.30 2.069 -0.2480 14.37 2.112 -0.2480 15.48 2.148 -0.2480 16.49 2.174 -0.2480 17.44 2.185 -0.2480 18.44 2.207 -0.2480 19.40 2.230 -0.2480 20.43 2.225 -0.2480 18.29 1.311 -0.2480 22.12 1.519 -0.2480 22.91 1.551 -0.2480 23.94 1.555 -0.2480 22.95 1.544 -0.2480 21.94 1.493 -0.2480 20.96 1.473 -0.2480 19.97 1.403 -0.2480 18.95 1.388 -0.2480 17.90 1.318 -0.2480 16.93 1.272 -0.2480 15.88 1.226 -0.2480 14.92 1.215 -0.2480 13.95 1.169 -0.2480 12.90 1.158 -0.2480 11.87 1.150 -0.2480 10.83 1.126 -0.2480 9.89 1.102 -0.2480 8.90 1.118 -0.2480 7.91 1.281 -0.2480 6.79 1.641 -0.2480 5.78 1.560 -0.2480 4.66 1.475 -0.2480 3.65 1.389 -0.2480 2.72 1.310 -0.2480 1.67 1.216 -0.2480 0.79 1.132 -0.2480 -0.25 1.013 -0.2480 -1.38 0.884 -0.2480 -2.29 0.766 -0.2480 -3.36 0.356 -0.2480 -4.69 0.173 -0.2480 -5.61 0.152 -0.2480 -6.81 0.046 -0.2480 Tabulated from data in file CL00974.DAT & reduced using program Q02.00L File s1223rtl.lft created on 09-12-1997 at 13:46:18 using program FORMAT