Airfoil: SG6041 Builder: M. Allen Comment: clean Number of Reynolds #'s: 6 Average Reynolds #: 99924 Number of angles of attack: 59 alpha / Cl / Cm -8.97 -0.523 0.0188 -7.95 -0.518 0.0019 -7.02 -0.485 -0.0334 -6.02 -0.405 -0.0454 -5.01 -0.332 -0.0432 -3.99 -0.238 -0.0424 -2.98 -0.144 -0.0443 -1.94 -0.061 -0.0376 -0.82 0.034 -0.0394 0.20 0.150 -0.0508 1.17 0.303 -0.0667 2.20 0.475 -0.0776 3.23 0.618 -0.0786 4.28 0.721 -0.0712 5.28 0.815 -0.0659 6.32 0.899 -0.0622 7.44 0.969 -0.0557 8.40 1.021 -0.0505 9.37 1.083 -0.0465 10.40 1.130 -0.0410 11.37 1.152 -0.0368 12.31 1.013 -0.1218 13.23 0.924 -0.1355 14.17 0.924 -0.1420 15.36 0.982 -0.1460 16.23 0.936 -0.1470 17.29 0.983 -0.1440 18.31 0.987 -0.1554 19.21 1.006 -0.1545 20.24 1.028 -0.1750 19.64 1.005 -0.1545 18.66 0.987 -0.1658 17.58 0.928 -0.1536 16.47 0.959 -0.1590 15.71 0.954 -0.1516 14.66 0.948 -0.1463 13.59 0.934 -0.1490 12.66 0.977 -0.1391 11.77 1.048 -0.1122 10.87 1.146 -0.0411 9.71 1.099 -0.0462 8.84 1.053 -0.0499 7.83 0.991 -0.0545 6.81 0.926 -0.0591 5.78 0.855 -0.0646 4.74 0.775 -0.0703 3.69 0.675 -0.0800 2.65 0.566 -0.0860 1.65 0.393 -0.0750 0.60 0.215 -0.0583 -0.46 0.065 -0.0428 -1.40 -0.027 -0.0342 -2.45 -0.094 -0.0419 -3.47 -0.186 -0.0406 -4.50 -0.283 -0.0390 -5.58 -0.366 -0.0406 -6.55 -0.437 -0.0384 -7.53 -0.493 -0.0175 -8.53 -0.517 0.0146 Tabulated from data in file ag02330.dat & reduced using program C06.01 Average Reynolds #: 150078 Number of angles of attack: 59 alpha / Cl / Cm -8.77 -0.552 0.0154 -7.68 -0.526 -0.0114 -6.87 -0.493 -0.0310 -5.71 -0.404 -0.0459 -4.72 -0.339 -0.0426 -3.69 -0.240 -0.0441 -2.79 -0.137 -0.0479 -1.13 0.041 -0.0514 -0.71 0.084 -0.0527 0.27 0.251 -0.0689 1.55 0.425 -0.0745 2.32 0.491 -0.0722 3.42 0.580 -0.0667 4.39 0.686 -0.0664 5.48 0.796 -0.0624 6.48 0.878 -0.0584 7.57 0.946 -0.0533 8.46 1.005 -0.0495 9.56 1.079 -0.0445 10.61 1.134 -0.0390 11.56 1.163 -0.0342 12.30 0.986 -0.1277 13.63 0.921 -0.1375 14.73 0.893 -0.1411 15.48 0.910 -0.1418 16.75 0.900 -0.1498 17.49 0.921 -0.1547 18.77 0.938 -0.1507 19.88 0.960 -0.1611 20.45 0.948 -0.1609 19.55 0.960 -0.1659 18.51 0.926 -0.1587 17.42 0.898 -0.1498 16.61 0.918 -0.1538 15.52 0.910 -0.1496 14.49 0.898 -0.1455 13.56 0.935 -0.1417 12.69 0.928 -0.1344 11.85 1.167 -0.0359 10.85 1.151 -0.0381 9.81 1.102 -0.0438 8.89 1.040 -0.0481 7.80 0.971 -0.0524 6.69 0.897 -0.0565 5.78 0.833 -0.0600 4.73 0.742 -0.0642 3.74 0.629 -0.0655 2.51 0.511 -0.0675 1.48 0.422 -0.0707 0.57 0.309 -0.0689 -0.70 0.091 -0.0489 -1.41 0.010 -0.0450 -2.53 -0.089 -0.0455 -3.44 -0.195 -0.0387 -4.63 -0.317 -0.0366 -5.50 -0.386 -0.0382 -6.48 -0.454 -0.0368 -7.53 -0.525 -0.0111 -8.49 -0.537 0.0100 Tabulated from data in file pg02503.dat & reduced using program C06.01 Average Reynolds #: 199973 Number of angles of attack: 59 alpha / Cl / Cm -8.98 -0.547 0.0220 -7.93 -0.542 -0.0046 -7.04 -0.512 -0.0312 -5.99 -0.424 -0.0470 -5.00 -0.338 -0.0456 -3.92 -0.225 -0.0481 -2.92 -0.108 -0.0539 -1.83 0.030 -0.0642 -0.92 0.149 -0.0699 0.14 0.281 -0.0737 1.20 0.402 -0.0740 2.21 0.499 -0.0697 3.20 0.608 -0.0692 4.26 0.720 -0.0668 5.28 0.807 -0.0629 6.29 0.891 -0.0590 7.28 0.969 -0.0546 8.29 1.046 -0.0499 9.41 1.115 -0.0444 10.37 1.166 -0.0392 11.39 1.206 -0.0330 12.42 1.222 -0.0285 13.46 0.929 -0.1427 14.33 0.910 -0.1463 15.36 0.899 -0.1516 16.45 0.940 -0.1474 17.18 0.956 -0.1468 18.27 0.958 -0.1541 19.26 0.958 -0.1584 20.32 1.000 -0.1613 19.76 1.011 -0.1625 18.76 0.992 -0.1600 17.49 0.933 -0.1581 16.44 0.925 -0.1539 15.54 0.928 -0.1495 14.35 0.902 -0.1498 13.57 0.917 -0.1468 12.60 0.953 -0.1413 11.92 1.220 -0.0301 10.80 1.190 -0.0362 9.85 1.143 -0.0418 8.89 1.085 -0.0470 7.85 1.011 -0.0517 6.76 0.925 -0.0568 5.64 0.836 -0.0606 4.68 0.756 -0.0644 3.75 0.670 -0.0679 2.66 0.556 -0.0698 1.63 0.447 -0.0738 0.44 0.327 -0.0758 -0.39 0.209 -0.0718 -1.41 0.079 -0.0652 -2.44 -0.050 -0.0586 -3.49 -0.181 -0.0484 -4.53 -0.294 -0.0438 -5.53 -0.383 -0.0440 -6.54 -0.470 -0.0422 -7.49 -0.533 -0.0198 -8.53 -0.553 0.0091 Tabulated from data in file ag02332.dat & reduced using program C06.01 Average Reynolds #: 300019 Number of angles of attack: 59 alpha / Cl / Cm -9.00 -0.575 0.0131 -7.85 -0.556 -0.0159 -6.95 -0.510 -0.0379 -5.86 -0.387 -0.0551 -4.97 -0.288 -0.0582 -3.77 -0.134 -0.0671 -2.70 0.017 -0.0782 -1.72 0.135 -0.0820 -0.83 0.218 -0.0770 0.59 0.341 -0.0658 1.43 0.452 -0.0705 2.35 0.550 -0.0707 3.25 0.646 -0.0696 4.29 0.744 -0.0668 5.29 0.833 -0.0636 6.28 0.920 -0.0607 7.54 1.026 -0.0562 8.34 1.085 -0.0527 9.33 1.159 -0.0483 10.39 1.218 -0.0422 11.42 1.262 -0.0357 12.42 1.284 -0.0303 13.50 1.292 -0.0307 14.20 0.975 -0.1511 15.23 0.938 -0.1519 16.17 0.936 -0.1542 17.20 0.928 -0.1574 18.22 0.936 -0.1665 19.24 1.005 -0.1756 20.17 1.028 -0.1830 19.71 1.020 -0.1715 18.75 0.975 -0.1638 17.77 0.956 -0.1604 16.70 0.933 -0.1560 15.76 0.917 -0.1533 14.75 0.912 -0.1484 13.78 0.976 -0.1508 12.80 1.038 -0.1336 11.97 1.280 -0.0304 10.84 1.246 -0.0370 9.89 1.196 -0.0426 8.82 1.124 -0.0480 7.78 1.047 -0.0526 6.73 0.962 -0.0571 5.81 0.884 -0.0605 4.47 0.760 -0.0648 3.70 0.690 -0.0676 2.55 0.573 -0.0698 1.51 0.459 -0.0698 0.59 0.341 -0.0653 -0.44 0.249 -0.0734 -1.37 0.165 -0.0801 -2.58 0.031 -0.0787 -3.45 -0.094 -0.0681 -4.60 -0.245 -0.0584 -5.55 -0.353 -0.0534 -6.77 -0.495 -0.0426 -7.74 -0.551 -0.0154 -8.54 -0.568 0.0054 Tabulated from data in file ag02334.dat & reduced using program C06.01 Average Reynolds #: 399591 Number of angles of attack: 47 alpha / Cl / Cm -9.00 -0.573 0.0182 -7.71 -0.558 -0.0171 -7.00 -0.498 -0.0430 -6.03 -0.363 -0.0654 -4.96 -0.242 -0.0687 -3.93 -0.111 -0.0761 -2.95 0.008 -0.0810 -1.88 0.115 -0.0801 -0.70 0.230 -0.0746 0.45 0.339 -0.0694 1.32 0.427 -0.0666 2.36 0.549 -0.0693 3.40 0.656 -0.0679 4.61 0.770 -0.0647 5.54 0.856 -0.0627 6.70 0.960 -0.0594 7.60 1.038 -0.0564 8.59 1.117 -0.0521 9.56 1.190 -0.0478 10.46 1.240 -0.0425 11.48 1.289 -0.0363 12.48 1.317 -0.0311 13.52 1.334 -0.0316 14.39 1.340 -0.0458 13.93 1.334 -0.0366 12.83 1.322 -0.0276 11.95 1.305 -0.0309 10.82 1.260 -0.0369 9.85 1.206 -0.0428 8.79 1.134 -0.0481 7.86 1.064 -0.0525 6.84 0.972 -0.0563 5.69 0.868 -0.0601 4.41 0.749 -0.0634 3.30 0.646 -0.0667 2.57 0.572 -0.0680 1.46 0.440 -0.0665 0.45 0.337 -0.0693 -0.56 0.242 -0.0742 -1.69 0.131 -0.0794 -2.66 0.038 -0.0815 -3.63 -0.076 -0.0779 -4.76 -0.218 -0.0700 -5.78 -0.333 -0.0656 -6.57 -0.437 -0.0581 -7.73 -0.553 -0.0174 -8.74 -0.575 0.0070 Tabulated from data in file ag02338.dat & reduced using program C06.01 Average Reynolds #: 500033 Number of angles of attack: 47 alpha / Cl / Cm -8.87 -0.564 0.0083 -8.31 -0.563 -0.0035 -7.06 -0.466 -0.0552 -5.94 -0.315 -0.0730 -4.92 -0.208 -0.0769 -3.96 -0.099 -0.0784 -2.82 0.018 -0.0778 -1.92 0.112 -0.0776 -0.89 0.217 -0.0743 0.16 0.325 -0.0711 1.42 0.452 -0.0671 2.29 0.551 -0.0668 3.24 0.652 -0.0671 4.27 0.747 -0.0636 5.36 0.853 -0.0615 6.54 0.964 -0.0587 7.76 1.074 -0.0547 8.84 1.157 -0.0497 9.72 1.220 -0.0456 10.73 1.273 -0.0427 11.65 1.310 -0.0385 12.64 1.337 -0.0355 13.52 1.355 -0.0391 14.67 1.347 -0.0579 13.98 1.363 -0.0427 12.89 1.357 -0.0249 11.91 1.334 -0.0294 10.87 1.286 -0.0345 9.78 1.226 -0.0419 8.68 1.145 -0.0473 7.74 1.069 -0.0513 6.59 0.966 -0.0562 5.44 0.858 -0.0598 4.46 0.764 -0.0620 3.55 0.676 -0.0642 2.53 0.573 -0.0660 1.44 0.452 -0.0663 0.23 0.331 -0.0704 -0.46 0.263 -0.0732 -1.52 0.149 -0.0758 -2.41 0.061 -0.0780 -3.46 -0.050 -0.0782 -4.48 -0.156 -0.0780 -5.47 -0.268 -0.0744 -6.54 -0.388 -0.0701 -7.52 -0.532 -0.0334 -8.58 -0.586 0.0015 Tabulated from data in file ag02339.dat & reduced using program C06.01 File sg6041.lft created using program C06.01 on Mon Feb 02 15:11:35 1998