Airfoil: S834 Builder: Y. Tinel Comment: 'clean' Number of Reynolds #'s: 7 Average Reynolds #: 100033 Number of angles of attack: 61 alpha / Cl / Cm -10.31 -0.773 -0.0705 -9.20 -0.769 -0.0536 -8.24 -0.740 -0.0658 -7.21 -0.693 -0.0552 -6.18 -0.610 -0.0507 -5.17 -0.516 -0.0473 -4.12 -0.412 -0.0331 -3.10 -0.332 -0.0217 -2.08 -0.255 -0.0114 -1.02 -0.242 0.0099 0.01 -0.136 -0.0004 0.96 -0.035 0.0100 2.03 0.052 -0.0128 3.07 0.153 -0.0076 4.07 0.273 -0.0246 5.04 0.452 -0.0343 6.13 0.771 -0.0454 7.21 0.869 -0.0451 8.20 0.941 -0.0358 9.24 0.996 -0.0326 10.22 1.010 -0.0051 11.26 1.036 -0.0073 12.26 1.058 0.0024 13.27 1.071 0.0044 14.28 1.060 -0.0091 15.12 0.851 -0.1012 16.07 0.832 -0.1101 17.08 0.767 -0.1180 18.10 0.792 -0.1359 19.08 0.802 -0.1471 20.07 0.875 -0.1620 19.60 0.848 -0.1608 18.53 0.818 -0.1419 17.54 0.789 -0.1272 16.59 0.809 -0.1245 15.58 0.796 -0.1059 14.61 0.958 -0.1010 13.79 1.079 -0.0004 12.76 1.070 -0.0024 11.78 1.059 -0.0006 10.74 1.031 -0.0129 9.73 1.011 -0.0169 8.71 0.984 -0.0283 7.68 0.917 -0.0447 6.66 0.836 -0.0538 5.63 0.695 -0.0567 4.57 0.364 -0.0130 3.62 0.236 -0.0051 2.54 0.127 0.0025 1.49 0.035 0.0035 0.46 -0.057 0.0054 -0.56 -0.168 0.0107 -1.57 -0.237 -0.0011 -2.54 -0.278 -0.0128 -3.61 -0.351 -0.0441 -4.65 -0.440 -0.0339 -5.64 -0.537 -0.0395 -6.71 -0.629 -0.0622 -7.68 -0.693 -0.0388 -8.73 -0.740 -0.0791 -9.79 -0.758 -0.0687 Tabulated from data in file bm05036.dat & reduced using program C10.20 Average Reynolds #: 150063 Number of angles of attack: 61 alpha / Cl / Cm -10.27 -0.809 -0.0526 -9.25 -0.806 -0.0490 -8.22 -0.773 -0.0395 -7.22 -0.704 -0.0315 -6.21 -0.614 -0.0242 -5.15 -0.500 -0.0293 -4.13 -0.388 -0.0312 -3.09 -0.295 -0.0345 -2.07 -0.197 -0.0372 -1.06 -0.111 -0.0263 -0.01 -0.029 -0.0241 1.00 0.064 -0.0203 2.06 0.284 -0.0432 3.09 0.524 -0.0693 4.14 0.676 -0.0754 5.13 0.755 -0.0676 6.15 0.827 -0.0588 7.17 0.886 -0.0529 8.22 0.932 -0.0366 9.26 0.983 -0.0364 10.25 1.011 -0.0236 11.23 1.041 -0.0182 12.30 1.057 -0.0156 13.29 1.065 -0.0160 14.26 1.063 -0.0202 15.11 0.924 -0.1116 16.10 0.862 -0.1182 17.10 0.795 -0.1237 18.00 0.785 -0.1305 19.08 0.805 -0.1378 20.09 0.873 -0.1555 19.55 0.814 -0.1447 18.56 0.788 -0.1362 17.58 0.778 -0.1274 16.52 0.802 -0.1228 15.57 0.875 -0.1153 14.72 1.050 -0.0219 13.73 1.058 -0.0203 12.77 1.057 -0.0138 11.80 1.051 -0.0174 10.72 1.022 -0.0245 9.75 0.996 -0.0290 8.70 0.954 -0.0361 7.66 0.908 -0.0442 6.66 0.863 -0.0564 5.67 0.786 -0.0631 4.57 0.715 -0.0711 3.57 0.608 -0.0788 2.49 0.383 -0.0534 1.57 0.177 -0.0364 0.47 0.006 -0.0184 -0.51 -0.067 -0.0257 -1.51 -0.140 -0.0320 -2.57 -0.246 -0.0346 -3.58 -0.347 -0.0329 -4.70 -0.445 -0.0340 -5.66 -0.557 -0.0301 -6.69 -0.661 -0.0277 -7.69 -0.737 -0.0403 -8.74 -0.795 -0.0393 -9.74 -0.810 -0.0490 Tabulated from data in file bm05038.dat & reduced using program C10.20 Average Reynolds #: 199991 Number of angles of attack: 61 alpha / Cl / Cm -10.31 -0.838 -0.0572 -9.20 -0.829 -0.0406 -8.23 -0.778 -0.0372 -7.20 -0.698 -0.0358 -6.20 -0.594 -0.0403 -5.13 -0.468 -0.0457 -4.12 -0.353 -0.0477 -3.13 -0.230 -0.0555 -2.06 -0.110 -0.0584 -1.09 0.003 -0.0582 -0.01 0.115 -0.0550 1.07 0.219 -0.0515 2.05 0.310 -0.0453 3.06 0.460 -0.0542 4.04 0.617 -0.0641 5.16 0.766 -0.0732 6.15 0.853 -0.0688 7.20 0.882 -0.0537 8.19 0.927 -0.0435 9.27 0.980 -0.0375 10.23 1.016 -0.0309 11.22 1.047 -0.0240 12.23 1.064 -0.0213 13.29 1.067 -0.0185 14.27 1.073 -0.0211 15.21 1.064 -0.0296 16.09 0.912 -0.1205 17.09 0.819 -0.1254 18.04 0.798 -0.1308 19.04 0.805 -0.1362 20.06 0.857 -0.1495 19.54 0.818 -0.1417 18.56 0.801 -0.1378 17.58 0.812 -0.1310 16.57 0.838 -0.1259 15.64 0.999 -0.1082 14.70 1.066 -0.0289 13.74 1.066 -0.0216 12.73 1.064 -0.0216 11.73 1.055 -0.0270 10.75 1.031 -0.0297 9.73 0.996 -0.0372 8.70 0.950 -0.0422 7.64 0.891 -0.0498 6.67 0.872 -0.0642 5.60 0.810 -0.0740 4.65 0.708 -0.0728 3.56 0.546 -0.0618 2.57 0.380 -0.0503 1.51 0.267 -0.0529 0.47 0.174 -0.0580 -0.56 0.067 -0.0597 -1.55 -0.046 -0.0591 -2.62 -0.169 -0.0570 -3.62 -0.290 -0.0529 -4.62 -0.404 -0.0511 -5.68 -0.528 -0.0408 -6.70 -0.646 -0.0351 -7.74 -0.746 -0.0379 -8.74 -0.808 -0.0361 -9.75 -0.840 -0.0522 Tabulated from data in file bm05040.dat & reduced using program C10.20 Average Reynolds #: 350168 Number of angles of attack: 53 alpha / Cl / Cm -10.27 -0.879 -0.0475 -9.28 -0.798 -0.0498 -8.21 -0.679 -0.0581 -7.18 -0.551 -0.0666 -6.19 -0.429 -0.0724 -5.14 -0.306 -0.0766 -4.11 -0.190 -0.0783 -3.10 -0.085 -0.0786 -2.05 0.021 -0.0775 -1.02 0.122 -0.0769 -0.00 0.223 -0.0753 0.99 0.324 -0.0734 2.00 0.424 -0.0708 3.07 0.520 -0.0668 4.08 0.604 -0.0613 5.11 0.689 -0.0558 6.16 0.786 -0.0559 7.20 0.855 -0.0495 8.23 0.913 -0.0435 9.19 0.978 -0.0398 10.23 1.031 -0.0351 11.26 1.067 -0.0302 12.24 1.088 -0.0270 13.33 1.088 -0.0260 14.25 1.084 -0.0328 15.24 1.073 -0.0453 16.22 1.053 -0.0594 15.70 1.063 -0.0519 14.75 1.078 -0.0379 13.77 1.091 -0.0272 12.73 1.087 -0.0258 11.68 1.075 -0.0284 10.75 1.050 -0.0324 9.70 1.002 -0.0377 8.68 0.944 -0.0419 7.69 0.880 -0.0459 6.67 0.840 -0.0566 5.64 0.742 -0.0562 4.63 0.648 -0.0597 3.60 0.563 -0.0651 2.55 0.468 -0.0694 1.50 0.375 -0.0730 0.51 0.277 -0.0752 -0.50 0.173 -0.0769 -1.57 0.069 -0.0779 -2.56 -0.029 -0.0794 -3.61 -0.144 -0.0794 -4.63 -0.249 -0.0785 -5.69 -0.374 -0.0754 -6.68 -0.492 -0.0705 -7.70 -0.621 -0.0631 -8.74 -0.748 -0.0544 -9.77 -0.844 -0.0493 Tabulated from data in file bm05042.dat & reduced using program C10.20 Average Reynolds #: 349748 Number of angles of attack: 21 alpha / Cl / Cm 10.27 1.053 -0.0169 11.29 1.087 -0.0175 12.21 1.098 -0.0177 13.29 1.102 -0.0177 14.22 1.100 -0.0177 15.23 1.083 -0.0174 16.29 0.999 -0.0161 17.08 0.855 -0.0138 18.16 0.842 -0.0135 19.21 0.824 -0.0133 20.20 0.855 -0.0137 19.66 0.837 -0.0135 18.70 0.833 -0.0134 17.70 0.850 -0.0137 16.71 0.933 -0.0150 15.72 1.062 -0.0171 14.76 1.093 -0.0176 13.69 1.109 -0.0178 12.80 1.105 -0.0178 11.69 1.089 -0.0175 10.74 1.075 -0.0173 Tabulated from data in file bm05129.dat & reduced using program C10.20 Average Reynolds #: 499828 Number of angles of attack: 53 alpha / Cl / Cm -10.24 -0.820 -0.0663 -9.20 -0.707 -0.0735 -8.18 -0.589 -0.0800 -7.21 -0.483 -0.0822 -6.17 -0.381 -0.0811 -5.11 -0.279 -0.0792 -4.13 -0.182 -0.0784 -3.07 -0.076 -0.0776 -2.05 0.026 -0.0772 -1.01 0.134 -0.0767 -0.03 0.235 -0.0762 1.05 0.341 -0.0749 2.06 0.449 -0.0744 3.06 0.547 -0.0727 4.10 0.648 -0.0699 5.08 0.734 -0.0648 6.20 0.797 -0.0546 7.19 0.851 -0.0470 8.26 0.923 -0.0421 9.21 0.991 -0.0385 10.21 1.044 -0.0343 11.29 1.088 -0.0296 12.27 1.113 -0.0267 13.21 1.130 -0.0275 14.24 1.122 -0.0396 15.21 1.086 -0.0565 16.19 1.074 -0.0675 15.68 1.074 -0.0626 14.71 1.095 -0.0488 13.70 1.131 -0.0310 12.74 1.130 -0.0267 11.73 1.112 -0.0279 10.71 1.068 -0.0317 9.71 1.015 -0.0361 8.68 0.953 -0.0402 7.69 0.888 -0.0445 6.64 0.822 -0.0502 5.61 0.761 -0.0595 4.62 0.693 -0.0678 3.59 0.598 -0.0714 2.56 0.502 -0.0739 1.56 0.397 -0.0749 0.49 0.288 -0.0760 -0.54 0.181 -0.0762 -1.55 0.082 -0.0765 -2.59 -0.027 -0.0771 -3.57 -0.129 -0.0779 -4.64 -0.230 -0.0787 -5.67 -0.325 -0.0805 -6.73 -0.432 -0.0817 -7.72 -0.532 -0.0810 -8.72 -0.645 -0.0763 -9.75 -0.769 -0.0693 Tabulated from data in file bm05044.dat & reduced using program C10.20 Average Reynolds #: 499966 Number of angles of attack: 21 alpha / Cl / Cm 10.28 1.060 -0.0170 11.19 1.095 -0.0176 12.27 1.125 -0.0181 13.25 1.136 -0.0183 14.27 1.116 -0.0179 15.20 1.085 -0.0174 16.38 1.058 -0.0170 17.18 0.894 -0.0144 18.14 0.851 -0.0137 19.21 0.864 -0.0139 20.19 0.882 -0.0142 19.60 0.875 -0.0141 18.74 0.867 -0.0139 17.65 0.877 -0.0141 16.61 0.940 -0.0151 15.90 1.066 -0.0171 14.75 1.099 -0.0177 13.78 1.125 -0.0181 12.77 1.132 -0.0182 11.75 1.120 -0.0180 10.85 1.088 -0.0175 Tabulated from data in file bm05130.dat & reduced using program C10.20 File s834_c.lft created using program C10.20 on Thu May 22 17:01:22 2003