Airfoil: SG6040 Builder: M. Allen Comment: Zigzag trip Type C (h = 0.023") @ 2% u.s. & 5% l.s. Number of Reynolds #'s: 6 Average Reynolds #: 100006 Number of angles of attack: 59 alpha / Cl / Cm -8.99 -0.635 -0.0479 -7.96 -0.624 -0.0414 -6.90 -0.569 -0.0398 -5.83 -0.478 -0.0449 -4.71 -0.326 -0.0557 -3.59 -0.211 -0.0626 -2.82 -0.158 -0.0641 -1.84 -0.047 -0.0730 -0.70 0.078 -0.0792 0.63 0.206 -0.0817 1.61 0.322 -0.0782 2.30 0.438 -0.0659 3.53 0.549 -0.0505 4.38 0.620 -0.0484 5.56 0.707 -0.0520 6.44 0.768 -0.0516 7.45 0.823 -0.0489 8.57 0.883 -0.0447 9.32 0.931 -0.0425 10.71 0.971 -0.0378 11.46 0.990 -0.0368 12.46 1.020 -0.0372 13.49 1.045 -0.0385 14.57 1.054 -0.0406 15.71 1.075 -0.0443 16.40 1.080 -0.0487 17.25 0.864 -0.1339 18.75 0.891 -0.1550 19.28 0.930 -0.1580 20.50 0.976 -0.1663 19.28 0.934 -0.1716 18.47 0.895 -0.1583 17.56 0.947 -0.1464 16.50 0.961 -0.1395 15.62 0.849 -0.1082 14.86 1.069 -0.0524 13.85 1.048 -0.0441 12.83 1.031 -0.0416 11.81 1.013 -0.0405 10.76 0.987 -0.0418 9.79 0.964 -0.0447 8.77 0.918 -0.0483 7.75 0.870 -0.0520 6.56 0.797 -0.0548 5.73 0.739 -0.0558 4.63 0.658 -0.0530 3.72 0.593 -0.0539 2.55 0.498 -0.0655 1.52 0.334 -0.0834 0.48 0.217 -0.0839 -0.47 0.134 -0.0820 -1.51 0.022 -0.0769 -2.59 -0.108 -0.0676 -3.53 -0.203 -0.0619 -4.69 -0.317 -0.0551 -5.53 -0.426 -0.0457 -6.55 -0.524 -0.0401 -7.68 -0.603 -0.0370 -8.68 -0.633 -0.0425 Tabulated from data in file pg02507.dat & reduced using program C06.01 Average Reynolds #: 150010 Number of angles of attack: 57 alpha / Cl / Cm -7.82 -0.477 -0.0486 -6.77 -0.424 -0.0559 -5.83 -0.335 -0.0696 -4.75 -0.202 -0.0815 -3.70 -0.071 -0.0899 -2.67 0.036 -0.0931 -1.64 0.128 -0.0927 -0.66 0.228 -0.0916 0.77 0.368 -0.0851 1.22 0.412 -0.0834 2.27 0.499 -0.0792 3.37 0.578 -0.0721 4.36 0.635 -0.0642 5.84 0.723 -0.0526 6.32 0.763 -0.0522 7.56 0.851 -0.0500 8.27 0.888 -0.0475 9.48 0.936 -0.0429 10.37 0.961 -0.0400 11.48 0.992 -0.0399 12.49 1.017 -0.0423 13.70 1.027 -0.0457 14.44 1.037 -0.0498 15.48 1.052 -0.0558 16.81 1.076 -0.0614 17.48 1.087 -0.0661 18.41 0.894 -0.1521 19.53 0.879 -0.1643 20.55 0.935 -0.1719 19.48 0.909 -0.1726 18.38 0.905 -0.1489 17.52 0.919 -0.1417 16.55 0.876 -0.1311 15.67 1.073 -0.0617 14.81 1.060 -0.0552 13.73 1.046 -0.0506 12.83 1.020 -0.0485 11.79 1.007 -0.0455 10.75 0.981 -0.0435 9.68 0.953 -0.0457 8.80 0.915 -0.0495 7.73 0.864 -0.0525 6.72 0.806 -0.0544 5.76 0.734 -0.0549 4.71 0.665 -0.0617 3.55 0.596 -0.0719 2.47 0.523 -0.0781 1.59 0.450 -0.0813 0.39 0.340 -0.0866 -0.58 0.249 -0.0911 -1.61 0.148 -0.0926 -2.65 0.033 -0.0926 -3.64 -0.071 -0.0893 -4.76 -0.212 -0.0801 -5.70 -0.341 -0.0696 -6.79 -0.457 -0.0545 -7.58 -0.485 -0.0467 Tabulated from data in file pg02504.dat & reduced using program C06.01 Average Reynolds #: 199946 Number of angles of attack: 59 alpha / Cl / Cm -8.71 -0.667 -0.0522 -7.75 -0.560 -0.0619 -6.72 -0.398 -0.0791 -5.63 -0.241 -0.0902 -4.56 -0.120 -0.0942 -3.48 -0.016 -0.0931 -2.44 0.082 -0.0910 -1.70 0.155 -0.0907 -0.52 0.267 -0.0865 0.36 0.349 -0.0840 1.48 0.446 -0.0800 2.50 0.531 -0.0758 3.42 0.602 -0.0720 4.38 0.677 -0.0688 5.62 0.764 -0.0627 6.92 0.839 -0.0532 7.41 0.871 -0.0516 8.47 0.925 -0.0474 9.48 0.966 -0.0434 10.40 0.994 -0.0418 11.45 1.022 -0.0422 12.48 1.041 -0.0452 13.66 1.061 -0.0502 14.56 1.078 -0.0546 15.71 1.080 -0.0605 16.45 1.085 -0.0664 17.48 1.086 -0.0733 18.34 0.905 -0.1518 19.48 0.890 -0.1531 20.54 0.929 -0.1767 19.42 0.934 -0.1621 18.13 0.900 -0.1612 17.30 0.920 -0.1471 16.53 1.095 -0.0701 15.78 1.100 -0.0632 14.61 1.073 -0.0576 13.80 1.054 -0.0545 12.76 1.062 -0.0483 11.82 1.032 -0.0454 10.74 1.006 -0.0427 9.83 0.981 -0.0433 8.62 0.935 -0.0472 7.51 0.879 -0.0514 6.68 0.832 -0.0552 5.69 0.774 -0.0629 4.36 0.675 -0.0693 3.64 0.617 -0.0714 2.36 0.518 -0.0755 1.48 0.446 -0.0791 0.50 0.361 -0.0824 -0.56 0.266 -0.0858 -1.63 0.165 -0.0893 -2.69 0.063 -0.0902 -3.65 -0.025 -0.0919 -4.78 -0.141 -0.0927 -5.68 -0.243 -0.0885 -6.72 -0.384 -0.0779 -7.78 -0.555 -0.0602 -9.06 -0.686 -0.0486 Tabulated from data in file pg02508.dat & reduced using program C06.01 Average Reynolds #: 299965 Number of angles of attack: 59 alpha / Cl / Cm -9.13 -0.665 -0.0672 -8.00 -0.492 -0.0849 -7.09 -0.370 -0.0942 -5.89 -0.251 -0.0953 -4.87 -0.156 -0.0927 -4.03 -0.076 -0.0907 -2.86 0.036 -0.0883 -1.76 0.131 -0.0839 -0.73 0.233 -0.0830 0.31 0.337 -0.0805 1.53 0.446 -0.0765 2.56 0.539 -0.0738 3.66 0.638 -0.0709 4.67 0.722 -0.0680 5.78 0.814 -0.0637 6.52 0.864 -0.0603 7.63 0.924 -0.0538 8.57 0.963 -0.0479 9.53 0.999 -0.0439 10.54 1.030 -0.0425 11.46 1.059 -0.0455 12.56 1.075 -0.0492 13.62 1.100 -0.0545 14.51 1.106 -0.0599 15.58 1.095 -0.0672 16.58 1.112 -0.0765 17.75 1.105 -0.0858 18.37 1.006 -0.1512 19.16 1.025 -0.1621 20.05 0.996 -0.1714 19.68 0.973 -0.1671 18.71 1.003 -0.1551 17.69 1.073 -0.1478 16.90 1.109 -0.0778 15.73 1.114 -0.0710 14.79 1.105 -0.0630 13.84 1.104 -0.0570 12.73 1.084 -0.0514 11.81 1.065 -0.0472 10.76 1.042 -0.0433 9.56 1.004 -0.0441 8.76 0.975 -0.0471 7.78 0.936 -0.0530 6.61 0.873 -0.0594 5.41 0.787 -0.0648 4.42 0.707 -0.0684 3.26 0.606 -0.0722 2.45 0.537 -0.0745 1.18 0.427 -0.0782 0.30 0.344 -0.0813 -0.69 0.237 -0.0830 -1.87 0.127 -0.0836 -2.63 0.063 -0.0869 -3.71 -0.041 -0.0896 -4.72 -0.138 -0.0913 -5.63 -0.221 -0.0932 -6.84 -0.339 -0.0943 -7.65 -0.438 -0.0886 -8.76 -0.602 -0.0734 Tabulated from data in file pg02509.dat & reduced using program C06.01 Average Reynolds #: 400026 Number of angles of attack: 49 alpha / Cl / Cm -7.08 -0.373 -0.0945 -5.98 -0.275 -0.0924 -5.00 -0.179 -0.0906 -3.99 -0.084 -0.0878 -2.91 0.011 -0.0833 -1.97 0.108 -0.0825 -0.93 0.216 -0.0805 0.19 0.319 -0.0770 1.22 0.423 -0.0748 2.24 0.517 -0.0726 3.33 0.617 -0.0698 4.42 0.709 -0.0668 5.52 0.798 -0.0630 6.71 0.880 -0.0580 8.07 0.952 -0.0513 8.53 0.973 -0.0492 9.66 1.016 -0.0456 10.52 1.040 -0.0475 11.65 1.065 -0.0519 12.79 1.095 -0.0555 13.97 1.100 -0.0594 14.71 1.108 -0.0641 15.78 1.124 -0.0695 16.60 1.126 -0.0773 17.43 1.110 -0.0868 16.48 1.114 -0.0779 15.58 1.126 -0.0699 14.65 1.120 -0.0664 13.78 1.104 -0.0613 12.56 1.091 -0.0560 11.65 1.068 -0.0538 10.73 1.046 -0.0514 9.79 1.017 -0.0501 8.48 0.974 -0.0486 7.67 0.935 -0.0521 6.48 0.869 -0.0579 5.54 0.803 -0.0611 4.32 0.706 -0.0652 3.37 0.624 -0.0681 2.38 0.533 -0.0705 1.46 0.445 -0.0726 0.53 0.356 -0.0746 -0.49 0.266 -0.0774 -1.44 0.170 -0.0805 -2.78 0.025 -0.0809 -3.58 -0.044 -0.0837 -4.74 -0.151 -0.0873 -5.60 -0.235 -0.0879 -6.53 -0.318 -0.0897 Tabulated from data in file cf02511.dat & reduced using program C06.01 Average Reynolds #: 499355 Number of angles of attack: 49 alpha / Cl / Cm -7.00 -0.380 -0.0919 -5.92 -0.287 -0.0910 -5.00 -0.192 -0.0895 -3.99 -0.096 -0.0871 -2.98 0.002 -0.0853 -1.92 0.113 -0.0829 -0.91 0.223 -0.0799 0.15 0.324 -0.0765 1.13 0.428 -0.0754 2.17 0.528 -0.0732 3.17 0.620 -0.0710 4.27 0.715 -0.0662 5.29 0.796 -0.0617 6.41 0.873 -0.0569 7.68 0.943 -0.0510 8.77 0.992 -0.0481 10.15 1.037 -0.0466 10.94 1.063 -0.0476 11.91 1.086 -0.0558 12.58 1.095 -0.0592 13.89 1.115 -0.0640 14.53 1.112 -0.0690 15.33 1.123 -0.0745 16.26 1.123 -0.0818 17.25 1.136 -0.0930 16.69 1.126 -0.0880 15.49 1.122 -0.0774 14.48 1.117 -0.0692 13.51 1.111 -0.0640 12.70 1.096 -0.0609 11.65 1.079 -0.0574 10.68 1.052 -0.0547 9.80 1.028 -0.0481 8.82 0.995 -0.0460 7.74 0.952 -0.0504 6.59 0.888 -0.0546 5.15 0.791 -0.0609 4.27 0.720 -0.0643 3.46 0.654 -0.0655 2.67 0.580 -0.0687 1.62 0.481 -0.0729 0.63 0.379 -0.0747 -0.40 0.282 -0.0762 -1.42 0.174 -0.0782 -2.45 0.065 -0.0810 -3.48 -0.045 -0.0824 -4.60 -0.152 -0.0861 -5.53 -0.244 -0.0894 -6.61 -0.351 -0.0895 Tabulated from data in file cf02512.dat & reduced using program C06.01 File sg6040t.lft created using program C06.01 on Mon Feb 02 15:11:35 1998