XFOIL Version 6.94 Calculated polar for: AH 83-150 Q 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.500 0.3582 0.01560 0.01036 -0.0409 0.6571 0.9321 1.000 0.4111 0.01542 0.01011 -0.0411 0.6506 0.9360 1.500 0.4658 0.01524 0.00987 -0.0415 0.6438 0.9394 2.000 0.5221 0.01505 0.00959 -0.0421 0.6382 0.9418 2.500 0.5791 0.01495 0.00938 -0.0428 0.6330 0.9450 3.000 0.6324 0.01512 0.00954 -0.0433 0.6258 0.9473 3.500 0.6864 0.01508 0.00956 -0.0440 0.6179 0.9493 4.000 0.7438 0.01493 0.00942 -0.0449 0.6107 0.9512 4.500 0.8056 0.01449 0.00896 -0.0463 0.6037 0.9529 5.000 0.8623 0.01456 0.00903 -0.0471 0.5958 0.9563 5.500 0.9169 0.01435 0.00894 -0.0477 0.5850 0.9586 6.000 0.9774 0.01390 0.00850 -0.0490 0.5745 0.9605 6.500 1.0363 0.01350 0.00821 -0.0499 0.5603 0.9625 7.000 1.0919 0.01330 0.00814 -0.0507 0.5444 0.9650 7.500 1.1484 0.01322 0.00814 -0.0515 0.5272 0.9679 8.000 1.2013 0.01325 0.00820 -0.0518 0.5030 0.9728 8.500 1.2522 0.01364 0.00863 -0.0523 0.4715 0.9782 9.000 1.2977 0.01448 0.00943 -0.0525 0.4304 0.9886 9.500 1.3218 0.01604 0.01085 -0.0500 0.3816 1.0000 10.000 1.3356 0.01876 0.01345 -0.0478 0.3337 1.0000 10.500 1.3477 0.02212 0.01670 -0.0464 0.2905 1.0000 11.000 1.3508 0.02633 0.02077 -0.0447 0.2494 1.0000 11.500 1.3562 0.03044 0.02480 -0.0431 0.2115 1.0000 12.000 1.3567 0.03503 0.02928 -0.0414 0.1781 1.0000 12.500 1.3604 0.03942 0.03362 -0.0398 0.1538 1.0000 13.000 1.3657 0.04404 0.03827 -0.0388 0.1312 1.0000 13.500 1.3703 0.04895 0.04319 -0.0381 0.1110 1.0000 14.000 1.3696 0.05450 0.04871 -0.0374 0.0890 1.0000 14.500 1.3665 0.06061 0.05476 -0.0371 0.0697 1.0000 15.000 1.3682 0.06643 0.06070 -0.0371 0.0595 1.0000 15.500 1.3658 0.07291 0.06724 -0.0375 0.0524 1.0000 16.000 1.3712 0.07869 0.07323 -0.0382 0.0471 1.0000 16.500 1.3756 0.08457 0.07929 -0.0393 0.0432 1.0000 17.000 1.3741 0.09138 0.08622 -0.0409 0.0365 1.0000 17.500 1.3783 0.09753 0.09255 -0.0427 0.0317 1.0000 18.000 1.3692 0.10590 0.10086 -0.0455 0.0144 1.0000 18.500 1.3535 0.11550 0.11056 -0.0489 0.0092 1.0000 19.000 1.3351 0.12588 0.12114 -0.0531 0.0071 1.0000 19.500 1.3156 0.13679 0.13229 -0.0581 0.0061 1.0000 20.000 1.2980 0.14763 0.14340 -0.0637 0.0056 1.0000 20.500 1.2796 0.15871 0.15475 -0.0701 0.0052 1.0000 21.000 1.2627 0.16959 0.16588 -0.0770 0.0049 1.0000 21.500 1.2471 0.18100 0.17753 -0.0840 0.0046 1.0000 22.000 1.2326 0.19302 0.18979 -0.0911 0.0044 1.0000 22.500 1.2207 0.20534 0.20233 -0.0983 0.0042 1.0000 23.000 1.2075 0.21903 0.21625 -0.1060 0.0042 1.0000 23.500 1.1908 0.23493 0.23238 -0.1142 0.0042 1.0000 24.000 1.1619 0.25709 0.25481 -0.1243 0.0042 1.0000 24.500 1.1308 0.28369 0.28157 -0.1345 0.0040 1.0000 25.500 1.0724 0.34836 0.34616 -0.1491 0.0040 1.0000 26.000 1.0653 0.36775 0.36552 -0.1524 0.0036 1.0000 26.500 1.0563 0.38247 0.38025 -0.1546 0.0040 1.0000 28.500 0.8257 0.35701 0.35517 -0.1264 0.0095 1.0000 29.000 0.8160 0.36002 0.35818 -0.1275 0.0093 1.0000 29.500 0.8093 0.36316 0.36135 -0.1294 0.0091 1.0000 30.000 0.8051 0.36714 0.36533 -0.1313 0.0073 1.0000 30.500 0.8001 0.36958 0.36781 -0.1326 0.0069 1.0000 31.000 0.7984 0.37145 0.36972 -0.1346 0.0058 1.0000 31.500 0.7957 0.37340 0.37170 -0.1362 0.0056 1.0000 32.000 0.7919 0.37532 0.37366 -0.1375 0.0051 1.0000 32.500 0.7903 0.37731 0.37571 -0.1397 0.0051 1.0000 33.000 0.7831 0.37685 0.37524 -0.1395 0.0043 1.0000 33.500 0.7804 0.37969 0.37809 -0.1411 0.0043 1.0000 34.000 0.7786 0.38227 0.38071 -0.1432 0.0042 1.0000 34.500 0.7762 0.38593 0.38438 -0.1450 0.0042 1.0000 35.000 0.7756 0.38805 0.38657 -0.1477 0.0042 1.0000 35.500 0.7731 0.39115 0.38970 -0.1494 0.0042 1.0000 36.000 0.7715 0.39460 0.39315 -0.1515 0.0042 1.0000 36.500 0.7705 0.39876 0.39734 -0.1540 0.0040 1.0000 37.000 0.7696 0.40281 0.40140 -0.1563 0.0039 1.0000 37.500 0.7679 0.40538 0.40401 -0.1583 0.0039 1.0000 38.000 0.7676 0.41040 0.40903 -0.1602 0.0023 1.0000 38.500 0.7662 0.41313 0.41182 -0.1627 0.0025 1.0000 39.000 0.7641 0.41667 0.41535 -0.1645 0.0023 1.0000 39.500 0.7623 0.41891 0.41765 -0.1670 0.0022 1.0000 40.000 0.7599 0.42202 0.42077 -0.1688 0.0021 1.0000 40.500 0.7583 0.42447 0.42333 -0.1717 0.0024 1.0000 41.000 0.7564 0.42803 0.42692 -0.1738 0.0021 1.0000 41.500 0.7536 0.43084 0.42973 -0.1757 0.0020 1.0000 42.000 0.7515 0.43536 0.43425 -0.1776 0.0017 1.0000 42.500 0.7484 0.43719 0.43612 -0.1800 0.0016 1.0000 43.000 0.7457 0.44109 0.44001 -0.1819 0.0014 1.0000 43.500 0.7432 0.44345 0.44245 -0.1845 0.0016 1.0000 44.000 0.7400 0.44655 0.44554 -0.1867 0.0014 1.0000 44.500 0.7371 0.44888 0.44797 -0.1896 0.0014 1.0000 45.000 0.7336 0.45286 0.45195 -0.1912 0.0017 1.0000