Airfoil: SD2030 (B) Builder: Y. Tinel Comment: 'clean' Number of Reynolds #'s: 5 Average Reynolds #: 99958 Number of angles of attack: 61 alpha / Cl / Cm -9.97 -0.568 0.0171 -9.01 -0.571 0.0153 -8.03 -0.561 0.0039 -7.07 -0.517 -0.0176 -6.08 -0.449 -0.0430 -5.03 -0.361 -0.0320 -3.98 -0.275 -0.0355 -2.97 -0.183 -0.0331 -1.94 -0.095 -0.0406 -0.92 -0.015 -0.0249 0.06 0.088 -0.0360 1.13 0.194 -0.0207 2.18 0.352 -0.0368 3.21 0.525 -0.0649 4.25 0.634 -0.0561 5.26 0.725 -0.0522 6.27 0.805 -0.0303 7.30 0.878 -0.0424 8.31 0.931 -0.0183 9.33 0.999 -0.0330 10.34 1.046 -0.0300 11.34 1.074 -0.0282 12.29 1.048 -0.0896 13.23 0.959 -0.1253 14.20 0.914 -0.1396 15.22 0.900 -0.1466 16.18 0.970 -0.1678 17.20 0.926 -0.1649 18.15 0.957 -0.1735 19.16 0.966 -0.1832 20.14 0.946 -0.1844 19.65 0.954 -0.1882 18.62 0.949 -0.1828 17.66 0.978 -0.1803 16.62 0.924 -0.1716 15.64 0.921 -0.1612 14.71 0.914 -0.1514 13.70 0.970 -0.1421 12.76 1.023 -0.1177 11.83 1.108 -0.0514 10.83 1.071 -0.0307 9.78 1.025 -0.0230 8.79 0.971 -0.0292 7.80 0.912 -0.0330 6.78 0.862 -0.0605 5.71 0.767 -0.0452 4.72 0.675 -0.0568 3.70 0.589 -0.0740 2.61 0.438 -0.0653 1.63 0.281 -0.0575 0.61 0.156 -0.0520 -0.43 0.050 -0.0300 -1.45 -0.047 -0.0403 -2.50 -0.125 -0.0598 -3.52 -0.222 -0.0622 -4.54 -0.309 -0.0454 -5.55 -0.385 -0.0726 -6.56 -0.482 -0.0519 -7.58 -0.550 -0.0216 -8.56 -0.571 -0.0048 -9.56 -0.585 -0.0019 Tabulated from data in file bm05094.dat & reduced using program C10.20 Average Reynolds #: 199941 Number of angles of attack: 61 alpha / Cl / Cm -9.99 -0.589 0.0367 -8.95 -0.586 0.0282 -8.02 -0.590 0.0096 -7.07 -0.554 -0.0147 -6.08 -0.479 -0.0408 -5.06 -0.374 -0.0525 -3.99 -0.272 -0.0461 -2.97 -0.157 -0.0531 -1.98 -0.037 -0.0581 -0.92 0.076 -0.0617 0.10 0.214 -0.0693 1.16 0.350 -0.0766 2.13 0.453 -0.0751 3.15 0.546 -0.0703 4.19 0.658 -0.0683 5.25 0.753 -0.0634 6.22 0.835 -0.0591 7.37 0.917 -0.0542 8.29 0.985 -0.0489 9.36 1.043 -0.0429 10.35 1.095 -0.0371 11.40 1.127 -0.0314 12.30 1.148 -0.0868 13.24 1.079 -0.1345 14.17 0.991 -0.1556 15.22 0.969 -0.1588 16.17 0.979 -0.1630 17.19 0.949 -0.1622 18.17 0.931 -0.1606 19.20 0.939 -0.1691 20.13 0.954 -0.1737 19.71 0.924 -0.1661 18.67 0.927 -0.1635 17.68 0.937 -0.1643 16.69 0.974 -0.1678 15.71 0.969 -0.1617 14.63 0.983 -0.1604 13.68 1.043 -0.1485 12.76 1.102 -0.1203 11.86 1.110 -0.0494 10.89 1.110 -0.0364 9.83 1.071 -0.0416 8.77 1.013 -0.0471 7.81 0.958 -0.0532 6.74 0.882 -0.0577 5.72 0.797 -0.0620 4.74 0.718 -0.0684 3.65 0.609 -0.0719 2.63 0.507 -0.0755 1.58 0.405 -0.0779 0.61 0.292 -0.0778 -0.44 0.145 -0.0669 -1.45 0.033 -0.0638 -2.49 -0.089 -0.0568 -3.50 -0.207 -0.0504 -4.55 -0.316 -0.0488 -5.55 -0.416 -0.0507 -6.54 -0.511 -0.0306 -7.57 -0.561 -0.0063 -8.56 -0.583 0.0139 -9.50 -0.591 0.0305 Tabulated from data in file bm05078.dat & reduced using program C10.20 Average Reynolds #: 349542 Number of angles of attack: 33 alpha / Cl / Cm -6.03 -0.446 -0.0483 -5.02 -0.310 -0.0606 -3.97 -0.189 -0.0660 -2.99 -0.062 -0.0734 -1.94 0.071 -0.0807 -0.90 0.173 -0.0815 0.11 0.260 -0.0746 1.12 0.378 -0.0763 2.19 0.488 -0.0749 3.17 0.584 -0.0733 4.18 0.692 -0.0712 5.23 0.785 -0.0672 6.29 0.876 -0.0637 7.26 0.951 -0.0600 8.29 1.028 -0.0551 9.33 1.094 -0.0493 10.37 1.145 -0.0429 9.85 1.120 -0.0473 8.78 1.062 -0.0533 7.82 0.990 -0.0585 6.76 0.910 -0.0626 5.75 0.823 -0.0660 4.70 0.735 -0.0697 3.69 0.637 -0.0730 2.64 0.537 -0.0757 1.67 0.431 -0.0764 0.62 0.321 -0.0756 -0.41 0.214 -0.0782 -1.47 0.122 -0.0827 -2.47 0.006 -0.0781 -3.45 -0.126 -0.0699 -4.54 -0.259 -0.0622 -5.57 -0.381 -0.0580 Tabulated from data in file bm05080.dat & reduced using program C10.20 Average Reynolds #: 350076 Number of angles of attack: 21 alpha / Cl / Cm 10.40 1.155 -0.0186 11.46 1.186 -0.0191 12.35 1.174 -0.0189 13.34 1.149 -0.0185 14.37 1.117 -0.0180 15.34 1.034 -0.0166 16.38 0.982 -0.0158 17.20 0.965 -0.0155 18.42 0.954 -0.0153 19.34 0.949 -0.0153 20.34 0.978 -0.0157 19.81 0.952 -0.0153 18.85 0.941 -0.0151 17.71 0.958 -0.0154 16.76 0.974 -0.0157 15.79 1.021 -0.0164 14.79 1.043 -0.0168 13.82 1.119 -0.0180 12.98 1.157 -0.0186 11.87 1.189 -0.0191 10.92 1.173 -0.0189 Tabulated from data in file bm05132.dat & reduced using program C10.20 Average Reynolds #: 500252 Number of angles of attack: 35 alpha / Cl / Cm -6.06 -0.384 -0.0634 -4.96 -0.250 -0.0722 -3.99 -0.132 -0.0768 -2.97 -0.021 -0.0786 -1.94 0.081 -0.0784 -0.91 0.170 -0.0755 0.11 0.263 -0.0712 1.13 0.383 -0.0716 2.14 0.494 -0.0723 3.19 0.599 -0.0704 4.22 0.698 -0.0677 5.25 0.788 -0.0646 6.25 0.876 -0.0616 7.34 0.963 -0.0579 8.30 1.042 -0.0537 9.37 1.106 -0.0479 10.31 1.160 -0.0420 11.38 1.189 -0.0363 10.84 1.187 -0.0401 9.83 1.131 -0.0458 8.74 1.072 -0.0517 7.76 1.005 -0.0566 6.73 0.917 -0.0605 5.71 0.829 -0.0636 4.73 0.739 -0.0665 3.68 0.645 -0.0698 2.65 0.550 -0.0727 1.65 0.440 -0.0726 0.59 0.320 -0.0708 -0.40 0.216 -0.0736 -1.43 0.131 -0.0785 -2.48 0.029 -0.0792 -3.55 -0.084 -0.0781 -4.52 -0.194 -0.0745 -5.55 -0.316 -0.0706 Tabulated from data in file bm05082.dat & reduced using program C10.20 File sd2030_c.lft created using program C10.20 on Thu May 22 17:01:22 2003