Airfoil: SD2030 (B) Builder: Y. Tinel Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' Number of Reynolds #'s: 5 Average Reynolds #: 99923 Number of angles of attack: 61 alpha / Cl / Cm -10.01 -0.509 0.0151 -9.05 -0.520 0.0041 -8.07 -0.518 0.0029 -7.03 -0.478 -0.0203 -6.05 -0.396 -0.0475 -4.99 -0.303 -0.0512 -4.01 -0.234 -0.0533 -2.95 -0.150 -0.0382 -1.93 -0.066 -0.0473 -0.89 0.001 -0.0394 0.13 0.092 -0.0302 1.15 0.238 -0.0509 2.18 0.428 -0.0567 3.17 0.560 -0.0591 4.22 0.660 -0.0570 5.24 0.732 -0.0327 6.29 0.803 -0.0353 7.32 0.880 -0.0395 8.29 0.960 -0.0371 9.35 1.025 -0.0263 10.33 1.071 -0.0303 11.36 1.097 -0.0276 12.27 1.026 -0.0856 13.21 0.975 -0.1296 14.21 0.939 -0.1350 15.22 0.956 -0.1499 16.18 0.942 -0.1559 17.20 0.964 -0.1602 18.20 0.959 -0.1671 19.14 1.004 -0.1807 20.18 1.022 -0.1937 19.66 0.985 -0.1858 18.69 0.987 -0.1802 17.64 0.960 -0.1714 16.67 0.997 -0.1736 15.66 0.948 -0.1589 14.65 0.940 -0.1479 13.67 0.944 -0.1356 12.75 1.063 -0.1094 11.79 1.086 -0.0464 10.83 1.091 -0.0179 9.83 1.055 -0.0274 8.83 1.000 -0.0251 7.83 0.924 -0.0351 6.70 0.845 -0.0417 5.79 0.790 -0.0552 4.70 0.710 -0.0424 3.67 0.620 -0.0526 2.72 0.528 -0.0691 1.61 0.345 -0.0596 0.59 0.153 -0.0299 -0.42 0.049 -0.0247 -1.44 -0.027 -0.0402 -2.51 -0.101 -0.0468 -3.48 -0.185 -0.0491 -4.56 -0.265 -0.0571 -5.57 -0.347 -0.0540 -6.58 -0.426 -0.0493 -7.53 -0.484 -0.0158 -8.53 -0.505 -0.0020 -9.56 -0.496 0.0073 Tabulated from data in file bm05095.dat & reduced using program C10.20 Average Reynolds #: 199981 Number of angles of attack: 61 alpha / Cl / Cm -10.03 -0.582 0.0323 -9.01 -0.569 0.0244 -8.03 -0.560 0.0075 -7.03 -0.533 -0.0186 -6.01 -0.459 -0.0433 -5.05 -0.360 -0.0525 -3.98 -0.264 -0.0525 -3.02 -0.161 -0.0524 -1.94 -0.004 -0.0651 -0.98 0.136 -0.0735 0.11 0.234 -0.0676 1.18 0.316 -0.0599 2.18 0.416 -0.0582 3.15 0.511 -0.0581 4.22 0.613 -0.0574 5.23 0.708 -0.0557 6.25 0.802 -0.0529 7.27 0.895 -0.0516 8.33 0.986 -0.0482 9.30 1.045 -0.0429 10.32 1.097 -0.0379 11.35 1.139 -0.0324 12.26 1.142 -0.0654 13.26 1.077 -0.1320 14.21 1.006 -0.1557 15.20 0.978 -0.1594 16.17 0.977 -0.1610 17.20 0.964 -0.1624 18.17 0.926 -0.1560 19.16 0.944 -0.1643 20.16 0.946 -0.1678 19.71 0.942 -0.1700 18.63 0.936 -0.1652 17.65 0.947 -0.1614 16.68 0.948 -0.1608 15.66 0.970 -0.1603 14.65 0.962 -0.1537 13.71 1.053 -0.1508 12.75 1.091 -0.1240 11.89 1.147 -0.0321 10.86 1.119 -0.0363 9.81 1.070 -0.0422 8.83 1.015 -0.0459 7.83 0.939 -0.0492 6.79 0.848 -0.0517 5.68 0.754 -0.0551 4.70 0.659 -0.0546 3.68 0.565 -0.0559 2.68 0.472 -0.0571 1.63 0.371 -0.0580 0.65 0.280 -0.0615 -0.48 0.194 -0.0733 -1.49 0.066 -0.0675 -2.46 -0.086 -0.0530 -3.47 -0.205 -0.0537 -4.55 -0.314 -0.0467 -5.57 -0.406 -0.0491 -6.56 -0.500 -0.0285 -7.55 -0.548 -0.0014 -8.53 -0.565 0.0152 -9.50 -0.571 0.0292 Tabulated from data in file bm05086.dat & reduced using program C10.20 Average Reynolds #: 349925 Number of angles of attack: 37 alpha / Cl / Cm -6.05 -0.415 -0.0557 -5.07 -0.280 -0.0666 -3.99 -0.148 -0.0694 -2.95 -0.061 -0.0668 -1.92 0.043 -0.0665 -0.97 0.137 -0.0664 0.11 0.247 -0.0661 1.10 0.347 -0.0658 2.14 0.448 -0.0649 3.22 0.554 -0.0642 4.20 0.660 -0.0630 5.20 0.758 -0.0615 6.26 0.855 -0.0598 7.30 0.948 -0.0571 8.28 1.032 -0.0540 9.33 1.103 -0.0485 10.36 1.145 -0.0410 11.34 1.161 -0.0345 12.39 1.159 -0.0762 11.86 1.169 -0.0337 10.84 1.152 -0.0386 9.81 1.124 -0.0462 8.78 1.070 -0.0530 7.78 0.990 -0.0563 6.73 0.902 -0.0597 5.74 0.805 -0.0618 4.69 0.706 -0.0634 3.69 0.608 -0.0648 2.68 0.504 -0.0655 1.61 0.393 -0.0660 0.60 0.292 -0.0667 -0.44 0.189 -0.0668 -1.50 0.086 -0.0669 -2.49 -0.013 -0.0668 -3.46 -0.104 -0.0678 -4.54 -0.195 -0.0719 -5.59 -0.344 -0.0636 Tabulated from data in file bm05088.dat & reduced using program C10.20 Average Reynolds #: 350116 Number of angles of attack: 21 alpha / Cl / Cm 10.41 1.159 -0.0186 11.45 1.176 -0.0189 12.32 1.188 -0.0191 13.32 1.139 -0.0183 14.30 1.105 -0.0178 15.31 1.029 -0.0166 16.28 0.997 -0.0160 17.19 0.976 -0.0157 18.42 0.944 -0.0152 19.26 0.963 -0.0155 20.34 0.975 -0.0157 19.73 0.985 -0.0158 18.85 0.950 -0.0153 17.82 0.963 -0.0155 16.72 0.981 -0.0158 15.89 1.014 -0.0163 14.76 1.073 -0.0173 13.96 1.118 -0.0180 12.89 1.153 -0.0185 11.91 1.181 -0.0190 10.85 1.166 -0.0187 Tabulated from data in file bm05131.dat & reduced using program C10.20 Average Reynolds #: 500249 Number of angles of attack: 37 alpha / Cl / Cm -6.07 -0.354 -0.0698 -4.98 -0.250 -0.0688 -4.00 -0.161 -0.0682 -2.92 -0.058 -0.0671 -1.91 0.039 -0.0668 -0.93 0.140 -0.0667 0.12 0.243 -0.0658 1.13 0.355 -0.0654 2.19 0.463 -0.0644 3.23 0.569 -0.0639 4.19 0.665 -0.0625 5.22 0.768 -0.0611 6.25 0.862 -0.0591 7.29 0.962 -0.0569 8.34 1.044 -0.0532 9.37 1.098 -0.0460 10.34 1.141 -0.0398 11.36 1.165 -0.0345 12.38 1.169 -0.0360 11.87 1.175 -0.0334 10.78 1.159 -0.0379 9.82 1.119 -0.0435 8.81 1.072 -0.0506 7.77 0.993 -0.0554 6.72 0.911 -0.0584 5.74 0.810 -0.0604 4.72 0.714 -0.0620 3.69 0.614 -0.0634 2.65 0.507 -0.0647 1.64 0.406 -0.0656 0.61 0.303 -0.0659 -0.42 0.188 -0.0664 -1.42 0.089 -0.0670 -2.49 -0.016 -0.0672 -3.52 -0.119 -0.0680 -4.54 -0.211 -0.0684 -5.60 -0.305 -0.0713 Tabulated from data in file bm05090.dat & reduced using program C10.20 File sd2030_tf.lft created using program C10.20 on Thu May 22 17:01:22 2003