Airfoil: S822 (B) Builder: Y. Tinel Comment: 'clean' Number of Reynolds #'s: 6 Average Reynolds #: 100027 Number of angles of attack: 61 alpha / Cl / Cm -10.26 -0.782 -0.0671 -9.26 -0.775 -0.0686 -8.23 -0.727 -0.0614 -7.19 -0.644 -0.0509 -6.21 -0.550 -0.0506 -5.16 -0.465 -0.0360 -4.09 -0.380 -0.0283 -3.10 -0.301 -0.0269 -2.07 -0.259 -0.0097 -1.06 -0.230 0.0052 -0.03 -0.140 0.0056 1.05 -0.015 0.0032 2.01 0.035 0.0098 3.01 0.122 -0.0034 4.08 0.226 -0.0187 5.11 0.318 -0.0197 6.10 0.483 -0.0302 7.16 0.858 -0.0484 8.18 0.957 -0.0445 9.19 1.022 -0.0416 10.21 1.035 -0.0319 11.27 1.034 -0.0237 12.24 1.053 -0.0117 13.25 1.074 -0.0100 14.23 1.086 -0.0195 15.23 1.048 -0.0227 16.10 0.804 -0.1096 17.07 0.806 -0.1233 18.10 0.833 -0.1276 19.07 0.813 -0.1435 20.07 0.825 -0.1523 19.54 0.788 -0.1628 18.56 0.800 -0.1521 17.54 0.809 -0.1470 16.55 0.799 -0.1346 15.55 0.806 -0.1213 14.77 1.070 -0.0194 13.73 1.081 -0.0317 12.77 1.064 -0.0229 11.76 1.044 -0.0238 10.73 1.033 -0.0344 9.74 1.039 -0.0316 8.71 0.989 -0.0415 7.70 0.925 -0.0491 6.65 0.745 -0.0423 5.55 0.390 -0.0245 4.52 0.278 -0.0142 3.52 0.192 -0.0123 2.55 0.098 -0.0031 1.47 0.028 -0.0057 0.42 -0.063 0.0044 -0.53 -0.186 0.0146 -1.61 -0.241 0.0043 -2.56 -0.274 -0.0108 -3.63 -0.325 -0.0306 -4.65 -0.410 -0.0312 -5.72 -0.499 -0.0419 -6.67 -0.574 -0.0408 -7.74 -0.680 -0.0404 -8.79 -0.748 -0.0590 -9.77 -0.777 -0.0762 Tabulated from data in file bm05016.dat & reduced using program C10.20 Average Reynolds #: 149914 Number of angles of attack: 61 alpha / Cl / Cm -10.24 -0.814 -0.0534 -9.26 -0.794 -0.0435 -8.24 -0.719 -0.0449 -7.21 -0.617 -0.0468 -6.18 -0.512 -0.0522 -5.19 -0.411 -0.0537 -4.11 -0.316 -0.0473 -3.09 -0.224 -0.0502 -2.06 -0.147 -0.0418 -1.09 -0.089 -0.0330 -0.01 -0.035 -0.0251 1.01 0.025 -0.0170 2.01 0.118 -0.0209 3.08 0.261 -0.0297 4.11 0.453 -0.0418 5.17 0.782 -0.0666 6.20 0.868 -0.0604 7.21 0.932 -0.0552 8.21 0.990 -0.0475 9.19 1.031 -0.0394 10.20 1.052 -0.0341 11.25 1.063 -0.0264 12.27 1.075 -0.0191 13.25 1.095 -0.0185 14.31 1.104 -0.0177 15.29 1.089 -0.0215 16.08 0.844 -0.1136 17.09 0.822 -0.1223 18.11 0.828 -0.1279 19.05 0.818 -0.1327 20.06 0.808 -0.1375 19.53 0.837 -0.1372 18.60 0.822 -0.1312 17.57 0.844 -0.1323 16.57 0.816 -0.1171 15.66 0.879 -0.1150 14.73 1.100 -0.0176 13.74 1.090 -0.0152 12.73 1.080 -0.0164 11.74 1.062 -0.0242 10.72 1.052 -0.0304 9.70 1.048 -0.0365 8.65 1.008 -0.0469 7.67 0.961 -0.0519 6.65 0.890 -0.0582 5.58 0.819 -0.0665 4.60 0.698 -0.0658 3.51 0.333 -0.0343 2.55 0.190 -0.0266 1.47 0.063 -0.0206 0.49 -0.010 -0.0212 -0.56 -0.060 -0.0313 -1.62 -0.121 -0.0395 -2.59 -0.189 -0.0463 -3.63 -0.267 -0.0539 -4.66 -0.354 -0.0557 -5.66 -0.460 -0.0492 -6.71 -0.560 -0.0480 -7.69 -0.659 -0.0455 -8.74 -0.762 -0.0443 -9.73 -0.809 -0.0541 Tabulated from data in file bm05018.dat & reduced using program C10.20 Average Reynolds #: 199832 Number of angles of attack: 61 alpha / Cl / Cm -10.30 -0.787 -0.0593 -9.24 -0.705 -0.0647 -8.21 -0.619 -0.0638 -7.19 -0.511 -0.0710 -6.16 -0.416 -0.0708 -5.18 -0.324 -0.0689 -4.11 -0.222 -0.0685 -3.08 -0.125 -0.0661 -2.09 -0.039 -0.0626 -1.03 0.044 -0.0591 -0.02 0.135 -0.0557 1.02 0.230 -0.0521 2.05 0.327 -0.0484 3.04 0.429 -0.0452 4.11 0.564 -0.0473 5.12 0.719 -0.0565 6.14 0.869 -0.0657 7.19 0.928 -0.0581 8.25 0.982 -0.0504 9.24 1.019 -0.0431 10.26 1.031 -0.0338 11.24 1.047 -0.0268 12.29 1.062 -0.0218 13.26 1.088 -0.0201 14.28 1.098 -0.0198 15.25 1.100 -0.0225 16.08 0.851 -0.1164 17.09 0.823 -0.1196 18.04 0.814 -0.1237 19.07 0.811 -0.1286 20.07 0.857 -0.1433 19.60 0.830 -0.1339 18.57 0.815 -0.1272 17.51 0.818 -0.1259 16.60 0.900 -0.1250 15.81 1.089 -0.0282 14.74 1.101 -0.0225 13.78 1.089 -0.0207 12.72 1.078 -0.0216 11.71 1.051 -0.0244 10.74 1.042 -0.0311 9.70 1.034 -0.0400 8.73 1.001 -0.0468 7.64 0.949 -0.0534 6.66 0.911 -0.0650 5.57 0.793 -0.0617 4.57 0.644 -0.0519 3.58 0.499 -0.0455 2.52 0.379 -0.0458 1.49 0.276 -0.0494 0.54 0.196 -0.0547 -0.53 0.093 -0.0571 -1.63 0.004 -0.0604 -2.61 -0.078 -0.0635 -3.70 -0.178 -0.0655 -4.64 -0.267 -0.0682 -5.66 -0.364 -0.0673 -6.72 -0.464 -0.0681 -7.75 -0.568 -0.0663 -8.71 -0.660 -0.0609 -9.73 -0.744 -0.0616 Tabulated from data in file bm05020.dat & reduced using program C10.20 Average Reynolds #: 349869 Number of angles of attack: 53 alpha / Cl / Cm -10.30 -0.660 -0.0860 -9.21 -0.604 -0.0814 -8.11 -0.532 -0.0768 -7.15 -0.458 -0.0743 -6.15 -0.372 -0.0721 -5.13 -0.272 -0.0703 -4.07 -0.177 -0.0693 -3.09 -0.086 -0.0680 -2.08 0.020 -0.0682 -1.01 0.123 -0.0683 0.03 0.229 -0.0684 1.01 0.330 -0.0686 2.03 0.438 -0.0687 3.09 0.542 -0.0682 4.12 0.646 -0.0673 5.15 0.743 -0.0651 6.14 0.831 -0.0603 7.15 0.899 -0.0548 8.18 0.958 -0.0496 9.23 1.001 -0.0427 10.25 1.025 -0.0352 11.24 1.055 -0.0303 12.26 1.081 -0.0264 13.25 1.102 -0.0246 14.25 1.128 -0.0257 15.28 1.125 -0.0286 16.26 1.120 -0.0363 15.72 1.126 -0.0327 14.76 1.130 -0.0277 13.71 1.115 -0.0257 12.76 1.094 -0.0265 11.68 1.063 -0.0293 10.72 1.037 -0.0337 9.71 1.016 -0.0397 8.67 0.975 -0.0474 7.65 0.931 -0.0534 6.62 0.865 -0.0588 5.62 0.790 -0.0649 4.56 0.689 -0.0678 3.61 0.597 -0.0693 2.55 0.490 -0.0697 1.53 0.388 -0.0698 0.47 0.273 -0.0692 -0.56 0.167 -0.0693 -1.60 0.063 -0.0687 -2.57 -0.031 -0.0690 -3.68 -0.139 -0.0696 -4.65 -0.236 -0.0708 -5.66 -0.330 -0.0714 -6.67 -0.420 -0.0738 -7.73 -0.505 -0.0760 -8.75 -0.580 -0.0789 -9.80 -0.637 -0.0843 Tabulated from data in file bm05022.dat & reduced using program C10.20 Average Reynolds #: 349855 Number of angles of attack: 21 alpha / Cl / Cm 10.33 1.036 -0.0167 11.20 1.064 -0.0171 12.25 1.090 -0.0175 13.27 1.122 -0.0180 14.35 1.134 -0.0182 15.15 1.157 -0.0186 16.19 1.136 -0.0183 17.24 0.910 -0.0146 18.24 0.829 -0.0133 19.24 0.822 -0.0132 20.24 0.839 -0.0135 19.73 0.832 -0.0134 18.60 0.838 -0.0135 17.60 0.857 -0.0138 16.80 0.922 -0.0148 15.69 1.141 -0.0183 14.85 1.147 -0.0184 13.78 1.129 -0.0182 12.76 1.105 -0.0178 11.67 1.080 -0.0174 10.59 1.048 -0.0168 Tabulated from data in file bm05125.dat & reduced using program C10.20 Average Reynolds #: 499698 Number of angles of attack: 53 alpha / Cl / Cm -10.20 -0.697 -0.0797 -9.21 -0.642 -0.0757 -8.20 -0.574 -0.0726 -7.21 -0.485 -0.0705 -6.10 -0.386 -0.0688 -5.07 -0.290 -0.0687 -4.16 -0.202 -0.0684 -3.09 -0.092 -0.0682 -2.07 0.016 -0.0687 -1.06 0.117 -0.0693 0.01 0.226 -0.0698 1.03 0.333 -0.0705 2.00 0.442 -0.0707 3.06 0.550 -0.0712 4.14 0.660 -0.0709 5.12 0.762 -0.0697 6.13 0.846 -0.0657 7.17 0.902 -0.0557 8.20 0.957 -0.0479 9.21 0.994 -0.0401 10.21 1.036 -0.0343 11.28 1.079 -0.0298 12.28 1.109 -0.0271 13.25 1.136 -0.0267 14.26 1.165 -0.0279 15.25 1.169 -0.0322 16.25 1.152 -0.0406 15.76 1.168 -0.0374 14.75 1.166 -0.0312 13.73 1.147 -0.0281 12.76 1.126 -0.0276 11.77 1.090 -0.0290 10.68 1.051 -0.0332 9.71 1.018 -0.0381 8.66 0.975 -0.0452 7.64 0.921 -0.0523 6.64 0.878 -0.0620 5.63 0.803 -0.0689 4.59 0.707 -0.0716 3.56 0.599 -0.0719 2.56 0.494 -0.0721 1.51 0.383 -0.0715 0.53 0.278 -0.0713 -0.52 0.170 -0.0707 -1.59 0.061 -0.0699 -2.58 -0.043 -0.0692 -3.59 -0.148 -0.0692 -4.63 -0.250 -0.0689 -5.69 -0.348 -0.0691 -6.64 -0.435 -0.0704 -7.70 -0.529 -0.0717 -8.77 -0.612 -0.0743 -9.80 -0.677 -0.0787 Tabulated from data in file bm05024.dat & reduced using program C10.20 File S822_c.lft created using program C10.20 on Thu May 22 17:01:21 2003