XFOIL Version 6.96 Calculated polar for: GOE 433 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 = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -17.500 -0.8592 0.09142 0.08807 -0.0640 1.0000 0.0558 -17.250 -0.9327 0.07590 0.07221 -0.0753 1.0000 0.0563 -17.000 -0.9521 0.06960 0.06578 -0.0797 1.0000 0.0570 -16.750 -0.9461 0.06719 0.06340 -0.0810 1.0000 0.0577 -16.500 -0.9437 0.06413 0.06034 -0.0831 1.0000 0.0584 -16.250 -0.9469 0.06027 0.05643 -0.0860 1.0000 0.0590 -16.000 -0.9536 0.05610 0.05217 -0.0892 1.0000 0.0597 -15.750 -0.9614 0.05183 0.04781 -0.0926 1.0000 0.0603 -15.500 -0.9688 0.04767 0.04353 -0.0960 1.0000 0.0610 -15.250 -0.9749 0.04378 0.03951 -0.0994 1.0000 0.0617 -15.000 -0.9786 0.04025 0.03584 -0.1026 1.0000 0.0623 -14.750 -0.9804 0.03716 0.03263 -0.1052 1.0000 0.0628 -14.500 -0.9773 0.03528 0.03078 -0.1053 1.0000 0.0637 -14.250 -0.9883 0.03370 0.02921 -0.1036 1.0000 0.0641 -14.000 -0.9729 0.03189 0.02739 -0.1065 0.9953 0.0649 -13.750 -0.9388 0.02981 0.02524 -0.1128 0.9903 0.0661 -13.500 -0.9051 0.02773 0.02304 -0.1193 0.9834 0.0674 -13.250 -0.8704 0.02606 0.02120 -0.1247 0.9783 0.0686 -13.000 -0.8435 0.02490 0.01987 -0.1273 0.9688 0.0695 -12.750 -0.8181 0.02361 0.01860 -0.1286 0.9614 0.0708 -12.500 -0.7941 0.02287 0.01784 -0.1291 0.9515 0.0718 -12.250 -0.7703 0.02220 0.01713 -0.1295 0.9420 0.0730 -12.000 -0.7469 0.02153 0.01637 -0.1297 0.9328 0.0742 -11.750 -0.7232 0.02088 0.01561 -0.1299 0.9231 0.0753 -11.500 -0.6987 0.02031 0.01490 -0.1300 0.9145 0.0763 -11.250 -0.6751 0.01943 0.01397 -0.1301 0.9056 0.0776 -11.000 -0.6505 0.01879 0.01331 -0.1302 0.8976 0.0790 -10.750 -0.6245 0.01830 0.01278 -0.1303 0.8900 0.0803 -10.500 -0.5981 0.01782 0.01224 -0.1305 0.8820 0.0816 -10.250 -0.5714 0.01737 0.01168 -0.1306 0.8749 0.0830 -10.000 -0.5439 0.01699 0.01120 -0.1308 0.8671 0.0843 -9.750 -0.5180 0.01631 0.01047 -0.1309 0.8595 0.0860 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0.1441 -4.750 0.0535 0.01106 0.00426 -0.1341 0.6745 0.1500 -4.500 0.0828 0.01088 0.00408 -0.1344 0.6674 0.1571 -4.250 0.1121 0.01086 0.00398 -0.1345 0.6612 0.1634 -4.000 0.1418 0.01070 0.00384 -0.1348 0.6558 0.1700 -3.750 0.1714 0.01061 0.00374 -0.1351 0.6500 0.1765 -3.500 0.2008 0.01059 0.00365 -0.1352 0.6444 0.1823 -3.250 0.2303 0.01049 0.00357 -0.1355 0.6395 0.1902 -3.000 0.2601 0.01043 0.00350 -0.1357 0.6349 0.1970 -2.750 0.2898 0.01032 0.00343 -0.1360 0.6299 0.2064 -2.500 0.3192 0.01030 0.00338 -0.1361 0.6249 0.2160 -2.250 0.3488 0.01027 0.00337 -0.1364 0.6201 0.2290 -2.000 0.3786 0.01017 0.00335 -0.1366 0.6157 0.2447 -1.750 0.4083 0.01011 0.00334 -0.1369 0.6111 0.2622 -1.500 0.4377 0.01010 0.00333 -0.1371 0.6064 0.2795 -1.250 0.4672 0.01014 0.00336 -0.1373 0.6013 0.2962 -1.000 0.4968 0.01007 0.00336 -0.1375 0.5969 0.3131 -0.750 0.5263 0.01002 0.00337 -0.1376 0.5920 0.3312 -0.500 0.5556 0.01001 0.00339 -0.1378 0.5873 0.3496 0.000 0.6142 0.01001 0.00349 -0.1381 0.5773 0.3883 0.250 0.6435 0.01000 0.00355 -0.1382 0.5718 0.4094 0.500 0.6726 0.01005 0.00361 -0.1383 0.5665 0.4289 0.750 0.7016 0.01016 0.00371 -0.1383 0.5612 0.4461 1.000 0.7307 0.01016 0.00379 -0.1384 0.5556 0.4606 1.250 0.7596 0.01021 0.00385 -0.1384 0.5494 0.4730 1.500 0.7881 0.01035 0.00391 -0.1383 0.5428 0.4854 1.750 0.8169 0.01034 0.00399 -0.1383 0.5353 0.4959 2.000 0.8452 0.01043 0.00403 -0.1382 0.5274 0.5059 2.250 0.8734 0.01047 0.00410 -0.1381 0.5191 0.5145 2.500 0.9015 0.01056 0.00416 -0.1380 0.5095 0.5236 2.750 0.9293 0.01063 0.00424 -0.1378 0.4997 0.5325 3.000 0.9566 0.01076 0.00433 -0.1376 0.4894 0.5419 3.250 0.9843 0.01086 0.00443 -0.1375 0.4792 0.5499 3.750 1.0385 0.01117 0.00468 -0.1370 0.4592 0.5663 4.000 1.0647 0.01133 0.00482 -0.1366 0.4493 0.5739 4.250 1.0918 0.01148 0.00497 -0.1364 0.4402 0.5810 4.500 1.1178 0.01171 0.00514 -0.1361 0.4317 0.5873 4.750 1.1448 0.01183 0.00531 -0.1359 0.4237 0.5939 5.250 1.1969 0.01222 0.00569 -0.1352 0.4068 0.6091 5.500 1.2218 0.01246 0.00591 -0.1346 0.3977 0.6174 6.000 1.2728 0.01285 0.00635 -0.1338 0.3810 0.6364 6.250 1.2981 0.01304 0.00658 -0.1334 0.3733 0.6502 6.500 1.3226 0.01325 0.00684 -0.1328 0.3643 0.6692 6.750 1.3466 0.01345 0.00713 -0.1322 0.3549 0.6986 7.000 1.3692 0.01361 0.00746 -0.1313 0.3452 0.7633 7.250 1.3869 0.01350 0.00767 -0.1292 0.3364 1.0000 7.500 1.4085 0.01391 0.00800 -0.1283 0.3250 1.0000 7.750 1.4309 0.01427 0.00832 -0.1274 0.3126 1.0000 8.000 1.4509 0.01472 0.00871 -0.1263 0.2988 1.0000 8.250 1.4670 0.01525 0.00916 -0.1244 0.2832 1.0000 8.500 1.4811 0.01592 0.00973 -0.1224 0.2647 1.0000 8.750 1.4921 0.01677 0.01045 -0.1201 0.2432 1.0000 9.000 1.5007 0.01780 0.01135 -0.1176 0.2195 1.0000 9.250 1.5050 0.01914 0.01251 -0.1147 0.1940 1.0000 9.500 1.5120 0.02039 0.01366 -0.1124 0.1767 1.0000 9.750 1.5201 0.02163 0.01484 -0.1103 0.1645 1.0000 10.000 1.5298 0.02283 0.01600 -0.1086 0.1549 1.0000 10.250 1.5398 0.02406 0.01721 -0.1070 0.1469 1.0000 10.500 1.5479 0.02547 0.01860 -0.1053 0.1389 1.0000 10.750 1.5583 0.02676 0.01989 -0.1040 0.1315 1.0000 11.000 1.5651 0.02836 0.02146 -0.1024 0.1228 1.0000 11.250 1.5712 0.03007 0.02315 -0.1010 0.1143 1.0000 11.500 1.5765 0.03189 0.02494 -0.0996 0.1043 1.0000 11.750 1.5774 0.03412 0.02713 -0.0980 0.0910 1.0000 12.000 1.5701 0.03718 0.03008 -0.0963 0.0737 1.0000 12.250 1.5693 0.03974 0.03264 -0.0950 0.0686 1.0000 12.500 1.5720 0.04207 0.03500 -0.0940 0.0669 1.0000 12.750 1.5746 0.04448 0.03747 -0.0931 0.0656 1.0000 13.000 1.5766 0.04702 0.04005 -0.0924 0.0645 1.0000 13.250 1.5781 0.04967 0.04276 -0.0917 0.0636 1.0000 13.500 1.5787 0.05247 0.04562 -0.0910 0.0629 1.0000 13.750 1.5789 0.05535 0.04856 -0.0905 0.0622 1.0000 14.000 1.5784 0.05835 0.05163 -0.0900 0.0617 1.0000 14.250 1.5784 0.06133 0.05468 -0.0896 0.0614 1.0000 14.500 1.5786 0.06431 0.05774 -0.0892 0.0611 1.0000 14.750 1.5783 0.06739 0.06090 -0.0890 0.0608 1.0000 15.000 1.5768 0.07064 0.06423 -0.0887 0.0605 1.0000 15.250 1.5756 0.07387 0.06754 -0.0885 0.0603 1.0000 15.500 1.5734 0.07730 0.07106 -0.0885 0.0600 1.0000 15.750 1.5711 0.08078 0.07461 -0.0885 0.0598 1.0000 16.000 1.5688 0.08424 0.07814 -0.0885 0.0596 1.0000 16.250 1.5657 0.08787 0.08185 -0.0887 0.0593 1.0000 16.500 1.5633 0.09142 0.08548 -0.0888 0.0589 1.0000