Airfoil: S822 (B) Builder: Y. Tinel Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' Number of Reynolds #'s: 6 Average Reynolds #: 100074 Number of angles of attack: 61 alpha / Cl / Cm -10.27 -0.781 -0.0687 -9.26 -0.784 -0.0563 -8.16 -0.729 -0.0434 -7.20 -0.660 -0.0359 -6.17 -0.578 -0.0215 -5.14 -0.482 -0.0298 -4.10 -0.382 -0.0409 -3.14 -0.290 -0.0363 -2.10 -0.217 -0.0252 -1.04 -0.160 -0.0147 -0.03 -0.102 -0.0106 1.04 -0.034 -0.0044 2.08 0.035 0.0009 3.02 0.128 -0.0118 4.08 0.286 -0.0160 5.15 0.662 -0.0406 6.18 0.827 -0.0487 7.21 0.902 -0.0410 8.22 0.946 -0.0164 9.24 0.972 -0.0264 10.31 1.007 -0.0129 11.21 1.062 -0.0109 12.26 1.099 -0.0195 13.28 1.112 -0.0184 14.28 1.115 -0.0080 15.25 1.100 -0.0258 16.13 0.863 -0.1127 17.06 0.830 -0.1202 18.08 0.833 -0.1328 19.05 0.870 -0.1415 20.06 0.857 -0.1419 19.54 0.835 -0.1457 18.59 0.884 -0.1473 17.61 0.827 -0.1253 16.58 0.841 -0.1239 15.60 0.908 -0.1205 14.74 1.121 -0.0211 13.76 1.123 -0.0279 12.70 1.105 -0.0201 11.75 1.081 -0.0098 10.75 1.041 -0.0304 9.70 0.987 -0.0203 8.71 0.962 -0.0276 7.66 0.929 -0.0292 6.65 0.879 -0.0546 5.65 0.779 -0.0448 4.57 0.394 -0.0185 3.55 0.218 -0.0109 2.57 0.082 0.0041 1.53 0.010 -0.0060 0.52 -0.079 0.0059 -0.54 -0.123 -0.0093 -1.55 -0.188 -0.0164 -2.57 -0.243 -0.0270 -3.63 -0.348 -0.0260 -4.67 -0.437 -0.0278 -5.71 -0.533 -0.0488 -6.75 -0.624 -0.0306 -7.73 -0.696 -0.0353 -8.74 -0.755 -0.0542 -9.76 -0.784 -0.0556 Tabulated from data in file bm05026.dat & reduced using program C10.20 Average Reynolds #: 150091 Number of angles of attack: 61 alpha / Cl / Cm -10.26 -0.839 -0.0549 -9.17 -0.814 -0.0397 -8.30 -0.754 -0.0406 -7.25 -0.638 -0.0402 -6.20 -0.526 -0.0423 -5.14 -0.421 -0.0502 -4.17 -0.329 -0.0445 -3.11 -0.230 -0.0478 -2.09 -0.140 -0.0469 -1.08 -0.067 -0.0413 -0.04 0.028 -0.0455 1.04 0.235 -0.0542 2.04 0.346 -0.0489 3.11 0.446 -0.0393 4.12 0.571 -0.0425 5.16 0.714 -0.0555 6.14 0.715 -0.0373 7.14 0.768 -0.0349 8.20 0.844 -0.0280 9.17 0.903 -0.0301 10.22 0.968 -0.0234 11.25 1.027 -0.0219 12.27 1.048 -0.0198 13.27 1.066 -0.0175 14.24 1.088 -0.0202 15.28 1.074 -0.0214 16.15 0.842 -0.1177 17.08 0.808 -0.1245 18.13 0.791 -0.1290 19.08 0.793 -0.1333 20.04 0.798 -0.1382 19.50 0.805 -0.1380 18.57 0.794 -0.1314 17.56 0.793 -0.1271 16.61 0.825 -0.1248 15.58 0.881 -0.1127 14.74 1.083 -0.0201 13.75 1.075 -0.0219 12.69 1.054 -0.0187 11.75 1.040 -0.0264 10.72 1.003 -0.0272 9.72 0.937 -0.0259 8.62 0.867 -0.0341 7.65 0.804 -0.0328 6.60 0.733 -0.0355 5.61 0.713 -0.0455 4.62 0.678 -0.0597 3.55 0.494 -0.0380 2.56 0.394 -0.0460 1.54 0.300 -0.0527 0.46 0.093 -0.0454 -0.56 -0.014 -0.0460 -1.59 -0.097 -0.0455 -2.66 -0.180 -0.0522 -3.64 -0.274 -0.0483 -4.62 -0.372 -0.0469 -5.65 -0.478 -0.0442 -6.76 -0.575 -0.0445 -7.71 -0.675 -0.0433 -8.75 -0.784 -0.0374 -9.80 -0.827 -0.0530 Tabulated from data in file bm05028.dat & reduced using program C10.20 Average Reynolds #: 200131 Number of angles of attack: 61 alpha / Cl / Cm -10.23 -0.805 -0.0596 -9.22 -0.724 -0.0630 -8.20 -0.628 -0.0670 -7.17 -0.511 -0.0671 -6.19 -0.402 -0.0719 -5.19 -0.304 -0.0720 -4.12 -0.208 -0.0683 -3.10 -0.112 -0.0700 -2.07 -0.028 -0.0653 -1.03 0.077 -0.0685 0.04 0.199 -0.0662 1.04 0.296 -0.0613 2.04 0.353 -0.0487 3.06 0.412 -0.0388 4.08 0.474 -0.0276 5.12 0.587 -0.0320 6.10 0.656 -0.0307 7.17 0.746 -0.0312 8.18 0.825 -0.0286 9.16 0.899 -0.0281 10.24 0.972 -0.0265 11.29 1.030 -0.0241 12.22 1.060 -0.0213 13.29 1.082 -0.0186 14.26 1.101 -0.0181 15.27 1.103 -0.0199 16.05 0.893 -0.1111 17.05 0.818 -0.1168 18.09 0.805 -0.1212 19.10 0.805 -0.1294 20.06 0.813 -0.1337 19.55 0.794 -0.1327 18.60 0.788 -0.1275 17.53 0.829 -0.1286 16.57 0.839 -0.1211 15.72 1.104 -0.0276 14.76 1.103 -0.0230 13.75 1.082 -0.0225 12.78 1.062 -0.0235 11.77 1.042 -0.0273 10.70 0.995 -0.0298 9.64 0.928 -0.0323 8.65 0.862 -0.0344 7.64 0.783 -0.0333 6.62 0.701 -0.0329 5.62 0.624 -0.0360 4.58 0.521 -0.0325 3.57 0.441 -0.0364 2.48 0.376 -0.0471 1.51 0.325 -0.0603 0.47 0.249 -0.0659 -0.54 0.131 -0.0697 -1.58 0.016 -0.0687 -2.62 -0.069 -0.0714 -3.58 -0.151 -0.0741 -4.69 -0.249 -0.0737 -5.67 -0.347 -0.0751 -6.72 -0.457 -0.0726 -7.73 -0.574 -0.0688 -8.77 -0.683 -0.0663 -9.76 -0.774 -0.0587 Tabulated from data in file bm05030.dat & reduced using program C10.20 Average Reynolds #: 350098 Number of angles of attack: 53 alpha / Cl / Cm -10.22 -0.652 -0.0875 -9.23 -0.615 -0.0823 -8.20 -0.534 -0.0797 -7.16 -0.446 -0.0767 -6.19 -0.360 -0.0754 -5.11 -0.264 -0.0745 -4.05 -0.169 -0.0718 -3.07 -0.084 -0.0668 -2.05 -0.016 -0.0597 -0.98 0.068 -0.0571 0.02 0.166 -0.0571 1.02 0.251 -0.0556 2.00 0.342 -0.0539 3.10 0.442 -0.0530 4.09 0.533 -0.0515 5.11 0.617 -0.0495 6.13 0.700 -0.0475 7.16 0.777 -0.0441 8.12 0.836 -0.0379 9.19 0.904 -0.0345 10.19 0.968 -0.0316 11.24 1.041 -0.0299 12.22 1.087 -0.0283 13.29 1.129 -0.0277 14.25 1.155 -0.0306 15.24 1.156 -0.0375 16.18 1.146 -0.0415 15.75 1.148 -0.0410 14.73 1.158 -0.0347 13.73 1.143 -0.0297 12.72 1.104 -0.0283 11.70 1.063 -0.0298 10.70 1.002 -0.0314 9.71 0.942 -0.0338 8.70 0.875 -0.0367 7.63 0.808 -0.0413 6.62 0.738 -0.0473 5.59 0.654 -0.0497 4.59 0.570 -0.0513 3.51 0.477 -0.0530 2.53 0.391 -0.0546 1.54 0.304 -0.0559 0.45 0.205 -0.0571 -0.52 0.114 -0.0583 -1.57 0.023 -0.0586 -2.59 -0.053 -0.0640 -3.61 -0.126 -0.0714 -4.62 -0.216 -0.0742 -5.64 -0.313 -0.0752 -6.68 -0.405 -0.0768 -7.72 -0.499 -0.0787 -8.72 -0.587 -0.0811 -9.81 -0.632 -0.0864 Tabulated from data in file bm05032.dat & reduced using program C10.20 Average Reynolds #: 349951 Number of angles of attack: 21 alpha / Cl / Cm 10.26 0.984 -0.0158 11.33 1.048 -0.0168 12.27 1.099 -0.0177 13.33 1.139 -0.0183 14.20 1.162 -0.0187 15.26 1.159 -0.0186 16.29 1.137 -0.0183 17.35 1.108 -0.0178 18.32 1.088 -0.0175 19.24 0.828 -0.0133 20.10 0.858 -0.0138 19.61 0.843 -0.0136 18.60 0.843 -0.0136 17.73 0.859 -0.0138 16.55 0.920 -0.0148 15.80 1.148 -0.0185 14.68 1.164 -0.0187 13.67 1.147 -0.0184 12.74 1.114 -0.0179 11.66 1.071 -0.0172 10.78 1.017 -0.0163 Tabulated from data in file bm05124.dat & reduced using program C10.20 Average Reynolds #: 499891 Number of angles of attack: 53 alpha / Cl / Cm -10.22 -0.660 -0.0807 -9.19 -0.614 -0.0768 -8.15 -0.543 -0.0736 -7.17 -0.454 -0.0734 -6.16 -0.355 -0.0717 -5.10 -0.264 -0.0678 -4.09 -0.185 -0.0629 -3.07 -0.100 -0.0603 -2.02 -0.000 -0.0590 -1.04 0.084 -0.0571 -0.05 0.177 -0.0563 1.06 0.268 -0.0543 2.10 0.367 -0.0533 3.06 0.459 -0.0519 4.09 0.549 -0.0498 5.10 0.630 -0.0475 6.14 0.713 -0.0448 7.19 0.791 -0.0417 8.18 0.865 -0.0388 9.15 0.928 -0.0352 10.19 0.997 -0.0313 11.23 1.049 -0.0288 12.24 1.083 -0.0272 13.29 1.103 -0.0265 14.24 1.110 -0.0292 15.22 1.122 -0.0363 16.23 1.092 -0.0476 15.75 1.105 -0.0462 14.71 1.111 -0.0336 13.77 1.115 -0.0286 12.71 1.099 -0.0272 11.75 1.071 -0.0283 10.71 1.022 -0.0306 9.68 0.960 -0.0336 8.66 0.896 -0.0379 7.67 0.828 -0.0407 6.61 0.749 -0.0438 5.57 0.671 -0.0467 4.59 0.585 -0.0491 3.59 0.504 -0.0513 2.51 0.411 -0.0532 1.50 0.315 -0.0548 0.45 0.223 -0.0558 -0.52 0.132 -0.0571 -1.57 0.037 -0.0587 -2.63 -0.055 -0.0604 -3.56 -0.143 -0.0619 -4.62 -0.226 -0.0654 -5.66 -0.308 -0.0705 -6.69 -0.408 -0.0730 -7.80 -0.506 -0.0738 -8.76 -0.592 -0.0748 -9.77 -0.643 -0.0797 Tabulated from data in file bm05034.dat & reduced using program C10.20 File s822_tf.lft created using program C10.20 on Thu May 22 17:01:22 2003