XFOIL Version 6.96 Calculated polar for: GOE 16K AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -0.5226 0.11007 0.10670 -0.1483 0.9468 0.0225 -19.500 -0.5656 0.09937 0.09586 -0.1541 0.9464 0.0227 -19.250 -0.5959 0.09100 0.08735 -0.1588 0.9460 0.0228 -19.000 -0.6344 0.08551 0.08177 -0.1575 0.9403 0.0225 -18.750 -0.6719 0.07725 0.07337 -0.1614 0.9385 0.0233 -18.500 -0.6918 0.07139 0.06738 -0.1646 0.9371 0.0232 -18.250 -0.7155 0.06490 0.06077 -0.1683 0.9360 0.0234 -18.000 -0.7309 0.05942 0.05515 -0.1718 0.9350 0.0237 -17.750 -0.7448 0.05395 0.04954 -0.1754 0.9342 0.0238 -17.500 -0.7672 0.04988 0.04536 -0.1750 0.9289 0.0247 -17.250 -0.7787 0.04578 0.04112 -0.1767 0.9259 0.0251 -17.000 -0.7805 0.04252 0.03773 -0.1783 0.9240 0.0261 -16.750 -0.7859 0.03912 0.03420 -0.1796 0.9225 0.0261 -16.500 -0.7830 0.03675 0.03174 -0.1803 0.9213 0.0271 -16.250 -0.7880 0.03496 0.02986 -0.1786 0.9174 0.0278 -16.000 -0.7910 0.03339 0.02822 -0.1766 0.9132 0.0287 -15.750 -0.7846 0.03200 0.02673 -0.1757 0.9110 0.0297 -15.500 -0.7755 0.03069 0.02530 -0.1751 0.9094 0.0307 -15.250 -0.7684 0.02918 0.02366 -0.1743 0.9082 0.0308 -15.000 -0.7497 0.02838 0.02286 -0.1745 0.9072 0.0325 -14.750 -0.7305 0.02756 0.02196 -0.1748 0.9064 0.0341 -14.500 -0.7364 0.02684 0.02116 -0.1701 0.9000 0.0344 -14.250 -0.7231 0.02607 0.02028 -0.1690 0.8976 0.0353 -14.000 -0.7067 0.02530 0.01943 -0.1684 0.8959 0.0364 -13.750 -0.6888 0.02454 0.01862 -0.1681 0.8945 0.0373 -13.500 -0.6655 0.02400 0.01803 -0.1685 0.8934 0.0386 -13.250 -0.6427 0.02332 0.01725 -0.1689 0.8923 0.0393 -13.000 -0.6174 0.02277 0.01661 -0.1697 0.8913 0.0408 -12.750 -0.6188 0.02253 0.01629 -0.1646 0.8852 0.0415 -12.500 -0.6017 0.02203 0.01570 -0.1636 0.8825 0.0419 -12.250 -0.5835 0.02140 0.01499 -0.1628 0.8805 0.0426 -12.000 -0.5613 0.02090 0.01446 -0.1628 0.8788 0.0440 -11.750 -0.5366 0.02044 0.01393 -0.1631 0.8774 0.0448 -11.500 -0.5099 0.02005 0.01347 -0.1639 0.8761 0.0461 -11.250 -0.5024 0.01979 0.01316 -0.1603 0.8726 0.0468 -11.000 -0.4948 0.01950 0.01281 -0.1568 0.8691 0.0473 -10.750 -0.4770 0.01925 0.01248 -0.1554 0.8667 0.0483 -10.500 -0.4559 0.01894 0.01208 -0.1547 0.8648 0.0490 -10.250 -0.4328 0.01859 0.01166 -0.1544 0.8632 0.0496 -10.000 -0.4130 0.01793 0.01095 -0.1537 0.8617 0.0507 -9.750 -0.3877 0.01750 0.01048 -0.1539 0.8604 0.0516 -9.500 -0.3600 0.01713 0.01006 -0.1546 0.8593 0.0530 -9.250 -0.3640 0.01709 0.01001 -0.1482 0.8557 0.0535 -9.000 -0.3555 0.01690 0.00978 -0.1445 0.8531 0.0537 -8.750 -0.3417 0.01666 0.00949 -0.1420 0.8509 0.0544 -8.500 -0.3243 0.01639 0.00917 -0.1403 0.8490 0.0550 -8.250 -0.3012 0.01619 0.00892 -0.1397 0.8475 0.0563 -8.000 -0.2781 0.01587 0.00855 -0.1392 0.8461 0.0567 -7.750 -0.2520 0.01560 0.00821 -0.1394 0.8449 0.0573 -7.500 -0.2243 0.01535 0.00790 -0.1398 0.8439 0.0580 -7.250 -0.1975 0.01495 0.00747 -0.1402 0.8430 0.0593 -7.000 -0.1927 0.01487 0.00738 -0.1355 0.8408 0.0601 -6.750 -0.1899 0.01483 0.00733 -0.1303 0.8383 0.0605 -6.500 -0.1783 0.01473 0.00722 -0.1270 0.8364 0.0616 -6.250 -0.1627 0.01461 0.00709 -0.1247 0.8347 0.0629 -6.000 -0.1442 0.01448 0.00693 -0.1231 0.8332 0.0635 -5.750 -0.1235 0.01434 0.00677 -0.1218 0.8319 0.0654 -5.500 -0.1010 0.01422 0.00662 -0.1210 0.8307 0.0662 -5.250 -0.0768 0.01408 0.00645 -0.1205 0.8297 0.0675 -5.000 -0.0505 0.01389 0.00626 -0.1206 0.8288 0.0697 -4.750 -0.0222 0.01372 0.00608 -0.1211 0.8280 0.0718 -4.500 0.0071 0.01354 0.00590 -0.1218 0.8272 0.0763 -4.250 0.0390 0.01333 0.00572 -0.1231 0.8264 0.0842 -4.000 0.0515 0.01333 0.00574 -0.1200 0.8248 0.0897 -3.750 0.0385 0.01355 0.00601 -0.1111 0.8217 0.0968 -3.500 0.0461 0.01347 0.00610 -0.1071 0.8196 0.1305 -3.250 0.0611 0.01335 0.00615 -0.1047 0.8180 0.1687 -3.000 0.0799 0.01332 0.00616 -0.1030 0.8165 0.1832 -2.750 0.1016 0.01325 0.00615 -0.1020 0.8153 0.2022 -2.250 0.1524 0.01301 0.00607 -0.1016 0.8132 0.2441 -2.000 0.1783 0.01290 0.00605 -0.1016 0.8123 0.2696 -1.500 0.2328 0.01266 0.00602 -0.1021 0.8108 0.3283 -1.250 0.2621 0.01255 0.00599 -0.1028 0.8101 0.3518 -1.000 0.2188 0.01335 0.00679 -0.0872 0.8034 0.3459 -0.750 0.2286 0.01341 0.00695 -0.0836 0.8002 0.3697 -0.500 0.2558 0.01325 0.00683 -0.0837 0.7983 0.3891 -0.250 0.2832 0.01306 0.00676 -0.0839 0.7970 0.4211 0.000 0.3120 0.01288 0.00667 -0.0844 0.7959 0.4469 0.250 0.3425 0.01257 0.00652 -0.0853 0.7948 0.4929 0.500 0.3640 0.01196 0.00633 -0.0842 0.7934 0.6092 0.750 0.2964 0.01282 0.00757 -0.0636 0.7841 0.6916 1.750 0.5767 0.01458 0.01005 -0.1015 0.7834 0.9299 2.000 0.6153 0.01482 0.01031 -0.1041 0.7821 0.9331 2.250 0.6463 0.01511 0.01059 -0.1050 0.7809 0.9390 2.500 0.6716 0.01511 0.01058 -0.1046 0.7791 0.9430 2.750 0.7138 0.01503 0.01050 -0.1081 0.7778 0.9443 3.000 0.7571 0.01495 0.01042 -0.1118 0.7767 0.9457 3.250 0.7108 0.01644 0.01199 -0.0961 0.7669 0.9542 3.500 0.7536 0.01617 0.01171 -0.0995 0.7631 0.9551 3.750 0.7933 0.01614 0.01169 -0.1025 0.7618 0.9565 4.000 0.7835 0.01708 0.01270 -0.0950 0.7536 0.9597 4.250 0.8158 0.01679 0.01235 -0.0959 0.7449 0.9625 4.500 0.8044 0.01800 0.01365 -0.0885 0.7381 0.9659 4.750 0.8341 0.01820 0.01386 -0.0893 0.7267 0.9683 5.000 0.8362 0.01891 0.01457 -0.0845 0.7067 0.9708 5.250 0.8593 0.01904 0.01459 -0.0835 0.6819 0.9749 5.500 0.8904 0.01893 0.01438 -0.0847 0.6575 0.9759 5.750 0.9015 0.01947 0.01461 -0.0817 0.6106 0.9775 6.000 0.9050 0.02040 0.01537 -0.0776 0.5746 0.9796 6.250 0.8870 0.02212 0.01682 -0.0694 0.5151 0.9824 6.500 0.8711 0.02409 0.01847 -0.0622 0.4565 0.9854 6.750 0.8763 0.02513 0.01936 -0.0591 0.4266 0.9864 7.000 0.8894 0.02586 0.02000 -0.0573 0.4054 0.9876 7.250 0.9031 0.02654 0.02062 -0.0555 0.3888 0.9887 7.500 0.9167 0.02721 0.02123 -0.0538 0.3721 0.9899 7.750 0.9306 0.02789 0.02186 -0.0520 0.3532 0.9910 8.000 0.9424 0.02876 0.02262 -0.0500 0.3263 0.9926 8.500 0.9690 0.03057 0.02413 -0.0472 0.2627 0.9956 8.750 0.9832 0.03138 0.02480 -0.0461 0.2332 0.9970 9.000 0.9939 0.03230 0.02555 -0.0442 0.2022 0.9980 9.250 1.0085 0.03293 0.02615 -0.0427 0.1903 0.9985 9.500 1.0192 0.03376 0.02686 -0.0407 0.1703 0.9990 9.750 1.0323 0.03439 0.02746 -0.0390 0.1583 0.9992 10.000 1.0443 0.03509 0.02810 -0.0371 0.1446 0.9993 10.250 1.0561 0.03580 0.02876 -0.0352 0.1338 0.9994 10.500 1.0674 0.03656 0.02948 -0.0333 0.1238 0.9995 10.750 1.0801 0.03723 0.03015 -0.0316 0.1151 0.9995 11.000 1.0913 0.03801 0.03087 -0.0297 0.1043 0.9996 11.250 1.1049 0.03865 0.03152 -0.0281 0.1010 0.9997 11.500 1.1137 0.03961 0.03239 -0.0261 0.0870 0.9997 11.750 1.1272 0.04028 0.03312 -0.0245 0.0870 0.9998 12.000 1.1391 0.04105 0.03389 -0.0228 0.0823 0.9998 12.250 1.1499 0.04188 0.03470 -0.0211 0.0755 0.9998 12.500 1.1611 0.04272 0.03556 -0.0194 0.0732 0.9998 12.750 1.1718 0.04359 0.03644 -0.0176 0.0674 0.9998 13.000 1.1839 0.04439 0.03728 -0.0161 0.0664 0.9998 13.250 1.1943 0.04532 0.03824 -0.0144 0.0625 0.9999 13.500 1.2051 0.04624 0.03919 -0.0129 0.0592 0.9999 13.750 1.2137 0.04733 0.04026 -0.0111 0.0548 0.9999 14.000 1.2237 0.04832 0.04128 -0.0095 0.0505 0.9999 14.250 1.2323 0.04943 0.04240 -0.0078 0.0466 0.9999 14.750 1.2486 0.05177 0.04477 -0.0045 0.0388 0.9999 15.000 1.2554 0.05307 0.04607 -0.0028 0.0345 0.9999 15.250 1.2621 0.05441 0.04745 -0.0012 0.0320 0.9999 15.500 1.2705 0.05563 0.04873 0.0002 0.0314 0.9999 15.750 1.2745 0.05725 0.05035 0.0019 0.0280 0.9999 16.000 1.2807 0.05871 0.05186 0.0034 0.0263 0.9999 16.250 1.2857 0.06028 0.05348 0.0049 0.0249 0.9999 16.500 1.2904 0.06193 0.05518 0.0063 0.0244 0.9999 16.750 1.2955 0.06356 0.05688 0.0077 0.0232 0.9999 17.000 1.2993 0.06533 0.05871 0.0090 0.0220 0.9999 17.250 1.3036 0.06709 0.06053 0.0102 0.0210 0.9999 17.500 1.3040 0.06927 0.06276 0.0116 0.0200 0.9999 17.750 1.3070 0.07123 0.06480 0.0127 0.0192 0.9999 18.000 1.3091 0.07331 0.06696 0.0137 0.0187 0.9999 18.250 1.3123 0.07530 0.06900 0.0146 0.0179 0.9998 18.500 1.3123 0.07766 0.07145 0.0155 0.0175 0.9998 18.750 1.3101 0.08034 0.07421 0.0164 0.0167 0.9998 19.000 1.3087 0.08294 0.07688 0.0171 0.0168 0.9998 19.250 1.3075 0.08557 0.07961 0.0177 0.0167 0.9998