Airfoil: S834 Builder: Y. Tinel Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' Number of Reynolds #'s: 7 Average Reynolds #: 99954 Number of angles of attack: 61 alpha / Cl / Cm -10.25 -0.775 -0.0908 -9.19 -0.772 -0.0614 -8.23 -0.737 -0.0604 -7.21 -0.685 -0.0250 -6.15 -0.592 -0.0313 -5.13 -0.492 -0.0159 -4.13 -0.374 -0.0162 -3.02 -0.246 -0.0268 -2.06 -0.171 -0.0206 -1.03 -0.130 0.0039 0.02 -0.067 -0.0023 1.05 0.028 0.0004 2.05 0.108 -0.0111 3.08 0.241 -0.0020 4.13 0.603 -0.0553 5.10 0.706 -0.0540 6.18 0.770 -0.0359 7.20 0.802 -0.0225 8.18 0.838 -0.0199 9.17 0.877 0.0028 10.26 0.957 -0.0080 11.24 1.010 -0.0153 12.30 1.038 -0.0137 13.31 1.045 -0.0044 14.24 1.036 -0.0101 15.10 0.773 -0.1017 16.06 0.835 -0.1172 17.11 0.774 -0.1260 18.05 0.790 -0.1324 19.07 0.829 -0.1492 20.02 0.860 -0.1592 19.55 0.824 -0.1642 18.50 0.791 -0.1503 17.54 0.764 -0.1351 16.56 0.802 -0.1277 15.60 0.844 -0.1256 14.60 0.805 -0.1059 13.79 1.044 -0.0033 12.75 1.036 -0.0011 11.77 1.025 -0.0089 10.74 0.982 -0.0039 9.70 0.916 -0.0043 8.69 0.856 -0.0061 7.65 0.826 -0.0218 6.67 0.791 -0.0294 5.65 0.747 -0.0584 4.61 0.670 -0.0478 3.57 0.368 -0.0233 2.53 0.171 -0.0060 1.53 0.083 0.0059 0.51 0.003 0.0080 -0.53 -0.079 0.0035 -1.56 -0.133 -0.0074 -2.55 -0.189 -0.0183 -3.66 -0.295 -0.0300 -4.65 -0.412 -0.0224 -5.62 -0.520 -0.0319 -6.70 -0.626 -0.0257 -7.72 -0.688 -0.0618 -8.74 -0.741 -0.0460 -9.73 -0.765 -0.0644 Tabulated from data in file bm05046.dat & reduced using program C10.20 Average Reynolds #: 149902 Number of angles of attack: 61 alpha / Cl / Cm -10.20 -0.816 -0.0508 -9.25 -0.808 -0.0464 -8.19 -0.762 -0.0373 -7.15 -0.685 -0.0276 -6.16 -0.594 -0.0301 -5.11 -0.487 -0.0304 -4.16 -0.387 -0.0337 -3.13 -0.280 -0.0371 -2.10 -0.185 -0.0397 -1.03 -0.082 -0.0417 -0.04 0.053 -0.0410 1.02 0.233 -0.0513 2.04 0.336 -0.0446 3.10 0.487 -0.0495 4.08 0.623 -0.0588 5.19 0.630 -0.0372 6.16 0.661 -0.0283 7.16 0.743 -0.0283 8.19 0.828 -0.0270 9.26 0.898 -0.0216 10.22 0.975 -0.0230 11.28 1.028 -0.0184 12.25 1.048 -0.0184 13.26 1.056 -0.0166 14.25 1.057 -0.0193 15.15 1.023 -0.1017 16.07 0.848 -0.1217 17.11 0.782 -0.1240 18.12 0.780 -0.1306 19.09 0.815 -0.1431 20.06 0.859 -0.1536 19.56 0.848 -0.1551 18.57 0.792 -0.1378 17.58 0.786 -0.1296 16.60 0.795 -0.1250 15.63 0.850 -0.1173 14.78 1.055 -0.0263 13.75 1.055 -0.0163 12.76 1.056 -0.0158 11.73 1.044 -0.0242 10.69 1.002 -0.0208 9.72 0.937 -0.0281 8.65 0.861 -0.0238 7.66 0.787 -0.0297 6.64 0.704 -0.0326 5.65 0.640 -0.0316 4.66 0.640 -0.0494 3.55 0.564 -0.0565 2.60 0.409 -0.0496 1.50 0.296 -0.0555 0.50 0.147 -0.0508 -0.53 -0.029 -0.0405 -1.58 -0.128 -0.0391 -2.63 -0.230 -0.0383 -3.63 -0.333 -0.0322 -4.62 -0.432 -0.0289 -5.68 -0.546 -0.0287 -6.68 -0.636 -0.0384 -7.64 -0.725 -0.0300 -8.69 -0.784 -0.0385 -9.74 -0.817 -0.0496 Tabulated from data in file bm05048.dat & reduced using program C10.20 Average Reynolds #: 200072 Number of angles of attack: 61 alpha / Cl / Cm -10.23 -0.857 -0.0559 -9.22 -0.840 -0.0399 -8.23 -0.785 -0.0360 -7.16 -0.688 -0.0347 -6.16 -0.580 -0.0385 -5.14 -0.460 -0.0410 -4.13 -0.334 -0.0462 -3.08 -0.210 -0.0534 -2.09 -0.099 -0.0582 -1.04 0.042 -0.0649 0.02 0.211 -0.0739 1.08 0.290 -0.0652 2.05 0.337 -0.0511 3.08 0.391 -0.0367 4.12 0.511 -0.0382 5.14 0.609 -0.0400 6.14 0.658 -0.0309 7.17 0.755 -0.0288 8.18 0.837 -0.0278 9.22 0.923 -0.0285 10.28 0.988 -0.0258 11.24 1.040 -0.0220 12.30 1.083 -0.0195 13.27 1.098 -0.0193 14.24 1.101 -0.0208 15.26 1.096 -0.0302 16.08 0.916 -0.1236 17.14 0.834 -0.1236 18.10 0.814 -0.1294 19.10 0.819 -0.1346 20.04 0.839 -0.1406 19.55 0.832 -0.1420 18.55 0.826 -0.1388 17.59 0.820 -0.1297 16.58 0.887 -0.1287 15.65 0.998 -0.1126 14.71 1.105 -0.0258 13.74 1.096 -0.0198 12.77 1.097 -0.0212 11.72 1.061 -0.0215 10.74 1.018 -0.0262 9.70 0.949 -0.0274 8.67 0.878 -0.0279 7.69 0.801 -0.0301 6.64 0.706 -0.0313 5.60 0.621 -0.0311 4.63 0.591 -0.0429 3.57 0.440 -0.0324 2.59 0.374 -0.0446 1.52 0.316 -0.0568 0.51 0.259 -0.0681 -0.52 0.139 -0.0715 -1.58 -0.025 -0.0618 -2.61 -0.152 -0.0539 -3.64 -0.268 -0.0513 -4.65 -0.397 -0.0411 -5.65 -0.524 -0.0350 -6.69 -0.635 -0.0348 -7.72 -0.744 -0.0321 -8.75 -0.817 -0.0330 -9.79 -0.861 -0.0431 Tabulated from data in file bm05050.dat & reduced using program C10.20 Average Reynolds #: 349875 Number of angles of attack: 53 alpha / Cl / Cm -10.25 -0.855 -0.0522 -9.21 -0.802 -0.0517 -8.18 -0.672 -0.0593 -7.20 -0.539 -0.0676 -6.19 -0.412 -0.0744 -5.17 -0.294 -0.0784 -4.11 -0.172 -0.0810 -3.04 -0.064 -0.0772 -2.04 0.003 -0.0682 -1.03 0.071 -0.0613 0.01 0.168 -0.0603 1.01 0.257 -0.0579 2.06 0.352 -0.0560 3.11 0.445 -0.0545 4.07 0.537 -0.0529 5.09 0.623 -0.0511 6.16 0.712 -0.0485 7.15 0.771 -0.0392 8.21 0.848 -0.0346 9.20 0.924 -0.0323 10.22 0.987 -0.0301 11.25 1.043 -0.0274 12.30 1.063 -0.0254 13.27 1.063 -0.0276 14.24 1.059 -0.0396 15.17 1.027 -0.0542 16.18 1.013 -0.0644 15.70 1.021 -0.0594 14.71 1.048 -0.0488 13.71 1.059 -0.0324 12.71 1.062 -0.0259 11.76 1.053 -0.0265 10.71 1.017 -0.0288 9.69 0.954 -0.0316 8.68 0.882 -0.0339 7.65 0.804 -0.0367 6.65 0.743 -0.0455 5.60 0.665 -0.0505 4.56 0.570 -0.0521 3.55 0.482 -0.0539 2.55 0.394 -0.0553 1.56 0.300 -0.0573 0.46 0.205 -0.0588 -0.52 0.119 -0.0608 -1.56 0.033 -0.0636 -2.58 -0.032 -0.0743 -3.60 -0.118 -0.0805 -4.67 -0.231 -0.0799 -5.68 -0.353 -0.0769 -6.62 -0.474 -0.0713 -7.73 -0.614 -0.0638 -8.72 -0.744 -0.0554 -9.74 -0.838 -0.0493 Tabulated from data in file bm05052.dat & reduced using program C10.20 Average Reynolds #: 349892 Number of angles of attack: 21 alpha / Cl / Cm 10.31 1.016 -0.0163 11.33 1.060 -0.0171 12.20 1.073 -0.0173 13.24 1.068 -0.0172 14.23 1.054 -0.0169 15.22 1.033 -0.0166 16.34 1.001 -0.0161 17.22 0.872 -0.0140 18.28 0.828 -0.0133 19.17 0.836 -0.0134 20.24 0.870 -0.0140 19.76 0.837 -0.0135 18.61 0.838 -0.0135 17.78 0.841 -0.0135 16.65 0.938 -0.0151 15.86 1.014 -0.0163 14.73 1.043 -0.0168 13.88 1.059 -0.0170 12.75 1.077 -0.0173 11.69 1.070 -0.0172 10.69 1.039 -0.0167 Tabulated from data in file bm05128.dat & reduced using program C10.20 Average Reynolds #: 500141 Number of angles of attack: 53 alpha / Cl / Cm -10.22 -0.792 -0.0672 -9.20 -0.690 -0.0741 -8.19 -0.574 -0.0817 -7.17 -0.454 -0.0850 -6.13 -0.350 -0.0850 -5.13 -0.261 -0.0789 -4.10 -0.182 -0.0718 -3.04 -0.102 -0.0663 -2.04 -0.012 -0.0637 -1.03 0.077 -0.0621 0.01 0.171 -0.0600 1.00 0.263 -0.0582 2.10 0.361 -0.0563 3.05 0.454 -0.0549 4.07 0.549 -0.0533 5.11 0.642 -0.0512 6.17 0.731 -0.0490 7.21 0.816 -0.0461 8.16 0.892 -0.0427 9.17 0.949 -0.0349 10.20 1.009 -0.0306 11.29 1.056 -0.0259 12.28 1.064 -0.0230 13.26 1.076 -0.0277 14.20 1.057 -0.0477 15.22 1.024 -0.0661 16.12 1.002 -0.0762 15.71 1.010 -0.0700 14.74 1.027 -0.0577 13.73 1.065 -0.0371 12.77 1.074 -0.0244 11.71 1.056 -0.0245 10.74 1.032 -0.0286 9.72 0.982 -0.0334 8.68 0.925 -0.0400 7.67 0.854 -0.0452 6.62 0.769 -0.0478 5.67 0.688 -0.0501 4.59 0.597 -0.0526 3.60 0.503 -0.0545 2.57 0.410 -0.0563 1.54 0.305 -0.0578 0.53 0.218 -0.0594 -0.63 0.114 -0.0614 -1.56 0.035 -0.0633 -2.58 -0.063 -0.0655 -3.62 -0.146 -0.0693 -4.65 -0.227 -0.0765 -5.66 -0.308 -0.0836 -6.66 -0.402 -0.0854 -7.71 -0.516 -0.0836 -8.69 -0.636 -0.0785 -9.74 -0.750 -0.0709 Tabulated from data in file bm05054.dat & reduced using program C10.20 Average Reynolds #: 499789 Number of angles of attack: 21 alpha / Cl / Cm 10.28 1.020 -0.0164 11.16 1.044 -0.0168 12.29 1.063 -0.0171 13.29 1.071 -0.0172 14.33 1.039 -0.0167 15.37 1.003 -0.0161 16.30 0.993 -0.0160 17.12 0.934 -0.0150 18.26 0.867 -0.0139 19.15 0.899 -0.0145 20.22 0.868 -0.0140 19.65 0.871 -0.0140 18.68 0.860 -0.0138 17.74 0.892 -0.0144 16.85 0.968 -0.0156 15.79 1.002 -0.0161 14.73 1.024 -0.0165 13.75 1.048 -0.0169 12.81 1.071 -0.0172 11.69 1.055 -0.0170 10.70 1.036 -0.0167 Tabulated from data in file bm05127.dat & reduced using program C10.20 File s834_tf.lft created using program C10.20 on Thu May 22 17:01:22 2003