Airfoil: E387 (E) 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 #: 99963 Number of angles of attack: 61 alpha / Cl / Cm -10.17 -0.471 0.0533 -9.16 -0.434 0.0408 -8.15 -0.398 0.0269 -7.14 -0.386 0.0079 -6.18 -0.332 -0.0183 -5.19 -0.258 -0.0556 -4.21 -0.108 -0.0587 -3.18 0.039 -0.0865 -2.11 0.185 -0.0891 -1.11 0.280 -0.0869 -0.06 0.385 -0.1013 0.89 0.472 -0.0923 1.96 0.573 -0.0840 3.00 0.675 -0.0893 4.02 0.769 -0.0742 5.04 0.872 -0.0670 6.08 0.979 -0.0761 7.09 1.072 -0.0729 8.14 1.138 -0.0665 9.15 1.191 -0.0571 10.17 1.230 -0.0427 11.13 1.250 -0.0544 12.16 1.254 -0.0518 13.16 1.251 -0.0537 14.08 1.205 -0.1200 15.08 1.119 -0.1515 16.01 1.082 -0.1581 17.00 1.083 -0.1639 18.02 1.063 -0.1665 19.05 1.077 -0.1694 20.01 1.087 -0.1773 19.50 1.074 -0.1822 18.52 1.054 -0.1723 17.54 1.073 -0.1763 16.50 1.074 -0.1704 15.51 1.076 -0.1625 14.53 1.100 -0.1467 13.64 1.246 -0.0565 12.67 1.257 -0.0442 11.67 1.256 -0.0442 10.67 1.247 -0.0492 9.64 1.219 -0.0538 8.65 1.165 -0.0664 7.69 1.115 -0.0643 6.56 1.026 -0.0693 5.59 0.928 -0.0732 4.51 0.825 -0.0768 3.46 0.719 -0.0921 2.50 0.629 -0.1016 1.45 0.528 -0.0966 0.38 0.431 -0.1064 -0.60 0.338 -0.0973 -1.65 0.239 -0.0999 -2.71 0.114 -0.0958 -3.67 -0.036 -0.0804 -4.73 -0.187 -0.0706 -5.69 -0.322 -0.0391 -6.72 -0.372 -0.0181 -7.71 -0.415 0.0080 -8.69 -0.433 0.0246 -9.65 -0.440 0.0311 Tabulated from data in file bm04988.dat & reduced using program C10.20 Average Reynolds #: 200028 Number of angles of attack: 61 alpha / Cl / Cm -10.17 -0.477 0.0468 -9.12 -0.485 0.0408 -8.19 -0.469 0.0306 -7.14 -0.428 0.0055 -6.17 -0.368 -0.0210 -5.19 -0.169 -0.0801 -4.21 -0.036 -0.0866 -3.16 0.059 -0.0890 -2.13 0.154 -0.0875 -1.11 0.255 -0.0866 -0.08 0.350 -0.0839 0.94 0.452 -0.0793 1.97 0.550 -0.0784 3.00 0.640 -0.0765 4.02 0.734 -0.0750 5.04 0.829 -0.0734 6.10 0.925 -0.0707 7.10 1.018 -0.0696 8.13 1.105 -0.0662 9.15 1.191 -0.0637 10.19 1.237 -0.0590 11.14 1.236 -0.0549 12.17 1.240 -0.0539 13.17 1.237 -0.0564 14.19 1.225 -0.0627 15.05 1.216 -0.1529 16.04 1.110 -0.1660 17.03 1.081 -0.1718 18.00 1.047 -0.1726 18.97 1.040 -0.1741 19.98 1.035 -0.1751 19.42 1.032 -0.1784 18.49 1.063 -0.1777 17.51 1.080 -0.1785 16.55 1.127 -0.1780 15.57 1.177 -0.1614 14.63 1.238 -0.1050 13.65 1.223 -0.0592 12.60 1.230 -0.0556 11.64 1.237 -0.0560 10.63 1.240 -0.0578 9.66 1.213 -0.0630 8.56 1.138 -0.0661 7.57 1.060 -0.0698 6.57 0.968 -0.0714 5.62 0.880 -0.0726 4.52 0.780 -0.0746 3.50 0.687 -0.0753 2.46 0.596 -0.0773 1.47 0.507 -0.0786 0.46 0.413 -0.0842 -0.59 0.311 -0.0844 -1.63 0.208 -0.0879 -2.71 0.107 -0.0862 -3.65 0.018 -0.0878 -4.76 -0.090 -0.0890 -5.75 -0.270 -0.0550 -6.69 -0.401 -0.0097 -7.68 -0.454 0.0186 -8.65 -0.470 0.0344 -9.66 -0.469 0.0422 Tabulated from data in file bm04990.dat & reduced using program C10.20 Average Reynolds #: 350084 Number of angles of attack: 47 alpha / Cl / Cm -8.18 -0.487 0.0256 -7.22 -0.435 0.0009 -6.21 -0.317 -0.0466 -5.19 -0.161 -0.0805 -4.14 -0.049 -0.0831 -3.19 0.048 -0.0825 -2.15 0.153 -0.0819 -1.14 0.249 -0.0808 -0.08 0.351 -0.0797 0.94 0.451 -0.0790 1.99 0.556 -0.0785 3.02 0.664 -0.0778 4.08 0.769 -0.0768 5.04 0.862 -0.0755 6.10 0.963 -0.0740 7.10 1.047 -0.0711 8.18 1.142 -0.0687 9.11 1.205 -0.0650 10.16 1.260 -0.0604 11.15 1.274 -0.0587 12.13 1.279 -0.0625 13.15 1.269 -0.0667 14.15 1.262 -0.0748 15.19 1.249 -0.0834 14.66 1.254 -0.0786 13.66 1.275 -0.0710 12.64 1.275 -0.0648 11.66 1.287 -0.0611 10.61 1.275 -0.0580 9.61 1.236 -0.0629 8.63 1.179 -0.0671 7.63 1.092 -0.0699 6.58 1.003 -0.0727 5.57 0.909 -0.0750 4.50 0.809 -0.0768 3.52 0.710 -0.0783 2.44 0.605 -0.0791 1.46 0.502 -0.0798 0.42 0.397 -0.0804 -0.61 0.296 -0.0806 -1.61 0.208 -0.0826 -2.66 0.099 -0.0835 -3.70 -0.007 -0.0839 -4.73 -0.104 -0.0844 -5.73 -0.236 -0.0689 -6.69 -0.382 -0.0240 -7.68 -0.460 0.0131 Tabulated from data in file bm04992.dat & reduced using program C10.20 Average Reynolds #: 349956 Number of angles of attack: 21 alpha / Cl / Cm 10.25 1.270 -0.0204 11.27 1.285 -0.0207 12.29 1.281 -0.0206 13.22 1.280 -0.0206 14.18 1.278 -0.0205 15.23 1.259 -0.0202 16.22 1.197 -0.0193 17.17 1.151 -0.0185 18.21 1.061 -0.0171 19.18 1.049 -0.0169 20.13 1.054 -0.0169 19.66 1.056 -0.0170 18.66 1.058 -0.0170 17.63 1.120 -0.0180 16.57 1.192 -0.0192 15.62 1.258 -0.0202 14.60 1.270 -0.0204 13.81 1.280 -0.0206 12.81 1.281 -0.0206 11.74 1.278 -0.0205 10.70 1.281 -0.0206 Tabulated from data in file bm05120.dat & reduced using program C10.20 Average Reynolds #: 499933 Number of angles of attack: 43 alpha / Cl / Cm -7.81 -0.484 0.0165 -6.21 -0.313 -0.0495 -5.19 -0.171 -0.0784 -4.16 -0.054 -0.0807 -3.16 0.048 -0.0803 -2.13 0.150 -0.0799 -1.12 0.247 -0.0792 -0.06 0.360 -0.0789 0.97 0.459 -0.0774 1.98 0.570 -0.0770 3.03 0.677 -0.0765 4.00 0.774 -0.0752 5.04 0.877 -0.0740 6.10 0.970 -0.0720 7.11 1.056 -0.0701 8.07 1.149 -0.0681 9.18 1.216 -0.0642 10.12 1.239 -0.0597 11.15 1.235 -0.0608 12.17 1.247 -0.0633 13.13 1.246 -0.0702 14.12 1.240 -0.0807 13.62 1.251 -0.0758 12.66 1.246 -0.0679 11.61 1.245 -0.0629 10.65 1.240 -0.0599 9.60 1.233 -0.0612 8.62 1.183 -0.0657 7.60 1.102 -0.0684 6.56 1.014 -0.0710 5.53 0.922 -0.0729 4.53 0.827 -0.0745 3.55 0.732 -0.0754 2.47 0.620 -0.0767 1.43 0.516 -0.0775 0.39 0.407 -0.0785 -0.58 0.305 -0.0793 -1.64 0.196 -0.0797 -2.62 0.101 -0.0805 -3.70 -0.010 -0.0802 -4.73 -0.107 -0.0816 -5.69 -0.232 -0.0694 -6.72 -0.372 -0.0292 Tabulated from data in file bm04994.dat & reduced using program C10.20 File e387_tf.lft created using program C10.20 on Thu May 22 17:01:21 2003