XFOIL Version 6.96 Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -10.750 -0.3181 0.09401 0.08995 -0.0535 -0.0001 4.4567 -10.500 -0.3243 0.08757 0.08354 -0.0562 0.0000 4.4562 -10.250 -0.3271 0.08344 0.07943 -0.0575 0.0000 4.4560 -10.000 -0.3335 0.07851 0.07453 -0.0596 0.0001 4.4557 -9.750 -0.3497 0.07148 0.06750 -0.0637 0.0001 4.4552 -9.500 -0.3849 0.06416 0.06004 -0.0688 0.0000 4.4546 -9.250 -0.4021 0.06074 0.05653 -0.0705 -0.0001 4.4545 -9.000 -0.4208 0.05808 0.05378 -0.0706 -0.0003 4.4544 -8.750 -0.4343 0.05530 0.05089 -0.0700 -0.0008 4.4542 -8.500 -0.4416 0.05219 0.04761 -0.0698 -0.0012 4.4540 -8.250 -0.4426 0.04876 0.04394 -0.0699 -0.0015 4.4537 -8.000 -0.4414 0.04556 0.04046 -0.0694 -0.0016 4.4533 -7.750 -0.4423 0.04271 0.03735 -0.0677 -0.0015 4.4530 -7.500 -0.4365 0.03963 0.03389 -0.0666 -0.0013 4.4525 -7.250 -0.4253 0.03680 0.03059 -0.0656 -0.0011 4.4520 -7.000 -0.4106 0.03488 0.02838 -0.0648 -0.0008 4.4518 -6.750 -0.4039 0.03327 0.02657 -0.0627 -0.0004 4.4518 -6.500 -0.3894 0.03169 0.02475 -0.0615 -0.0002 4.4517 -6.250 -0.3717 0.03030 0.02311 -0.0605 0.0000 4.4517 -6.000 -0.3506 0.02911 0.02170 -0.0599 0.0000 4.4517 -5.750 -0.3396 0.02807 0.02053 -0.0579 -0.0001 4.4518 -5.500 -0.3234 0.02714 0.01948 -0.0566 -0.0003 4.4519 -5.250 -0.3047 0.02638 0.01864 -0.0558 -0.0004 4.4522 -5.000 -0.2839 0.02578 0.01795 -0.0552 -0.0004 4.4527 -4.750 -0.2753 0.02509 0.01721 -0.0532 -0.0003 4.4531 -4.500 -0.2587 0.02456 0.01659 -0.0521 0.0002 4.4536 -4.250 -0.2391 0.02417 0.01606 -0.0514 0.0007 4.4543 -4.000 -0.2277 0.02372 0.01554 -0.0497 0.0023 4.4550 -3.750 -0.2116 0.02336 0.01509 -0.0486 0.0043 4.4558 -3.500 -0.1908 0.02313 0.01476 -0.0479 0.0058 4.4568 -3.250 -0.1773 0.02281 0.01441 -0.0465 0.0088 4.4573 -3.000 -0.1623 0.02210 0.01405 -0.0453 0.0123 4.3932 -2.750 -0.0991 0.02283 0.01714 -0.0455 0.0120 2.4061 -2.500 -0.0404 0.02508 0.01915 -0.0460 0.0124 2.2208 -2.250 -0.0071 0.02576 0.01963 -0.0462 0.0140 2.1575 -2.000 0.0259 0.02601 0.01969 -0.0466 0.0154 2.1268 -1.750 0.0422 0.02611 0.01969 -0.0454 0.0204 2.0936 -1.500 0.0661 0.02628 0.01973 -0.0450 0.0236 2.0631 -1.250 0.0952 0.02637 0.01969 -0.0453 0.0257 2.0363 -1.000 0.1255 0.02657 0.01976 -0.0458 0.0272 2.0077 -0.750 0.1300 0.02641 0.01954 -0.0437 0.0349 2.0009 -0.500 0.1463 0.02616 0.01919 -0.0433 0.0382 2.0009 -0.250 0.1503 0.02591 0.01890 -0.0413 0.0463 2.0009 0.000 0.1652 0.02571 0.01861 -0.0406 0.0511 2.0009 0.250 0.1719 0.02549 0.01834 -0.0389 0.0604 2.0009 0.500 0.1857 0.02528 0.01807 -0.0380 0.0674 2.0009 0.750 0.1948 0.02512 0.01786 -0.0366 0.0775 2.0009 1.000 0.2068 0.02492 0.01762 -0.0354 0.0878 2.0009 1.250 0.2260 0.02472 0.01733 -0.0350 0.0931 2.0009 1.500 0.2281 0.02459 0.01720 -0.0327 0.1121 2.0009 1.750 0.2470 0.02438 0.01694 -0.0322 0.1186 2.0009 2.000 0.2500 0.02427 0.01683 -0.0300 0.1394 2.0009 2.250 0.2686 0.02406 0.01658 -0.0294 0.1474 2.0009 2.500 0.2729 0.02393 0.01645 -0.0273 0.1684 2.0009 2.750 0.2906 0.02369 0.01619 -0.0266 0.1778 2.0009 3.000 0.2961 0.02359 0.01609 -0.0246 0.1986 2.0009 3.250 0.3129 0.02337 0.01586 -0.0237 0.2093 2.0009 3.500 0.3186 0.02329 0.01579 -0.0218 0.2313 2.0009 3.750 0.3357 0.02307 0.01556 -0.0209 0.2428 2.0009 4.000 0.3413 0.02302 0.01553 -0.0189 0.2675 2.0009 4.250 0.3593 0.02276 0.01530 -0.0181 0.2795 2.0009 4.500 0.3649 0.02273 0.01529 -0.0162 0.3072 2.0009 4.750 0.3834 0.02244 0.01500 -0.0153 0.3202 2.0009 5.000 0.3894 0.02241 0.01502 -0.0134 0.3503 2.0009 5.250 0.4078 0.02209 0.01474 -0.0125 0.3648 2.0009 5.500 0.4303 0.02168 0.01435 -0.0119 0.3730 2.0009 5.750 0.4311 0.02178 0.01451 -0.0096 0.4126 2.0009 6.000 0.4532 0.02136 0.01412 -0.0089 0.4214 2.0009 6.250 0.4534 0.02153 0.01437 -0.0066 0.4625 2.0009 6.500 0.4749 0.02109 0.01397 -0.0058 0.4723 2.0009 6.750 0.4754 0.02129 0.01425 -0.0036 0.5142 2.0009 7.000 0.4966 0.02082 0.01384 -0.0027 0.5247 2.0009 7.250 0.4977 0.02103 0.01413 -0.0006 0.5678 2.0009 7.500 0.5187 0.02050 0.01368 0.0003 0.5788 2.0009 7.750 0.5200 0.02071 0.01397 0.0024 0.6235 2.0009 8.000 0.5415 0.02012 0.01347 0.0034 0.6348 2.0009 8.250 0.5429 0.02032 0.01375 0.0054 0.6816 2.0009 8.500 0.5655 0.01964 0.01317 0.0064 0.6934 2.0009 8.750 0.5670 0.01981 0.01343 0.0084 0.7426 2.0009 9.000 0.5753 0.01973 0.01344 0.0101 0.7813 2.0009 9.250 0.5926 0.01922 0.01305 0.0114 0.8069 2.0009 9.500 0.5990 0.01923 0.01316 0.0131 0.8511 2.0009 9.750 0.6194 0.01859 0.01265 0.0143 0.8745 2.0009 10.000 0.6239 0.01868 0.01286 0.0161 0.9240 2.0009 10.250 0.6466 0.01690 0.01108 0.0181 1.0255 2.0009 10.500 0.6506 0.01644 0.01059 0.0205 1.1614 2.0009 10.750 0.6504 0.01628 0.01034 0.0230 1.3438 2.0009 11.000 0.6533 0.01626 0.01022 0.0250 1.5166 2.0009 11.250 0.6528 0.01647 0.01031 0.0271 1.7035 2.0009 11.500 0.6473 0.01696 0.01065 0.0292 1.9305 2.0009 11.750 0.6394 0.01764 0.01118 0.0311 2.1859 2.0009 12.000 0.6266 0.01864 0.01195 0.0330 2.5052 2.0009 12.250 0.6140 0.01977 0.01286 0.0345 2.8345 2.0009 12.500 0.5965 0.02129 0.01405 0.0359 3.3084 2.0009 12.750 0.5765 0.02312 0.01550 0.0371 3.9971 2.0009 13.000 0.5686 0.02427 0.01663 0.0381 4.0951 2.0009 13.250 0.5655 0.02513 0.01760 0.0390 4.1173 2.0009 13.500 0.5623 0.02601 0.01859 0.0398 4.1363 2.0009 13.750 0.5590 0.02693 0.01965 0.0405 4.1463 2.0009 14.000 0.5556 0.02789 0.02075 0.0412 4.1547 2.0009 14.250 0.5527 0.02884 0.02185 0.0417 4.1582 2.0009 14.500 0.5488 0.02990 0.02305 0.0422 4.1635 2.0009 14.750 0.5444 0.03104 0.02433 0.0425 4.1676 2.0009 15.000 0.5400 0.03220 0.02564 0.0428 4.1696 2.0009 15.250 0.5346 0.03350 0.02708 0.0429 4.1724 2.0009 15.500 0.5293 0.03485 0.02856 0.0429 4.1739 2.0009 15.750 0.5232 0.03633 0.03018 0.0428 4.1761 2.0009 16.000 0.5173 0.03783 0.03180 0.0427 4.1777 2.0009 16.250 0.5121 0.03932 0.03342 0.0425 4.1792 2.0009 16.500 0.5070 0.04084 0.03507 0.0422 4.1798 2.0009 16.750 0.5022 0.04234 0.03670 0.0420 4.1807 2.0009 17.000 0.4976 0.04383 0.03830 0.0417 4.1820 2.0009 17.250 0.4935 0.04534 0.03992 0.0414 4.1834 2.0009 17.500 0.4902 0.04671 0.04140 0.0411 4.1837 2.0009 17.750 0.4876 0.04799 0.04278 0.0409 4.1845 2.0009 18.000 0.4858 0.04922 0.04412 0.0408 4.1850 2.0009 18.250 0.4849 0.05029 0.04528 0.0408 4.1862 2.0009 18.500 0.4848 0.05126 0.04635 0.0408 4.1872 2.0009 18.750 0.4853 0.05216 0.04735 0.0409 4.1876 2.0009 19.000 0.4862 0.05302 0.04831 0.0410 4.1882 2.0009 19.250 0.4874 0.05390 0.04929 0.0412 4.1888 2.0009