MUE 139 (mue139-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: MUE 139 (mue139-il) Reynolds number: 200,000 Max Cl/Cd: 63.52 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mue139-il-200000-n5.txt Download as CSV file: xf-mue139-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MUE 139
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.2692 0.09604 0.09234 -0.0286 1.0000 0.0430
-9.250 -0.2709 0.09231 0.08865 -0.0299 1.0000 0.0428
-9.000 -0.2732 0.08866 0.08505 -0.0311 1.0000 0.0428
-8.750 -0.2670 0.08436 0.08078 -0.0343 0.9737 0.0429
-8.500 -0.2325 0.07821 0.07453 -0.0456 0.9171 0.0436
-8.250 -0.2001 0.07099 0.06714 -0.0588 0.8698 0.0447
-7.750 -0.3393 0.03093 0.02537 -0.0841 0.8034 0.0472
-7.500 -0.3170 0.03033 0.02462 -0.0835 0.7811 0.0477
-7.250 -0.2973 0.02931 0.02341 -0.0826 0.7628 0.0483
-7.000 -0.2801 0.02769 0.02148 -0.0816 0.7472 0.0491
-6.750 -0.2635 0.02576 0.01916 -0.0804 0.7327 0.0501
-6.500 -0.2464 0.02375 0.01669 -0.0792 0.7191 0.0512
-6.250 -0.2275 0.02195 0.01436 -0.0779 0.7063 0.0524
-5.750 -0.1790 0.02117 0.01346 -0.0762 0.6794 0.0540
-5.500 -0.1547 0.02072 0.01288 -0.0754 0.6658 0.0551
-5.250 -0.1307 0.02009 0.01205 -0.0744 0.6518 0.0564
-5.000 -0.1070 0.01931 0.01099 -0.0734 0.6368 0.0579
-4.750 -0.0826 0.01867 0.01014 -0.0725 0.6203 0.0591
-4.500 -0.0576 0.01835 0.00978 -0.0717 0.6031 0.0601
-4.250 -0.0325 0.01806 0.00939 -0.0709 0.5859 0.0614
-4.000 -0.0073 0.01774 0.00891 -0.0700 0.5687 0.0632
-3.750 0.0180 0.01733 0.00828 -0.0692 0.5519 0.0654
-3.500 0.0432 0.01704 0.00792 -0.0684 0.5356 0.0669
-3.250 0.0686 0.01684 0.00764 -0.0676 0.5207 0.0684
-3.000 0.0940 0.01663 0.00731 -0.0668 0.5068 0.0704
-2.750 0.1199 0.01641 0.00692 -0.0661 0.4934 0.0730
-2.500 0.1454 0.01620 0.00667 -0.0654 0.4814 0.0750
-2.250 0.1709 0.01608 0.00648 -0.0646 0.4705 0.0772
-2.000 0.1970 0.01593 0.00625 -0.0639 0.4603 0.0800
-1.750 0.2227 0.01579 0.00599 -0.0632 0.4518 0.0828
-1.500 0.2487 0.01564 0.00586 -0.0626 0.4435 0.0855
-1.250 0.2744 0.01557 0.00571 -0.0619 0.4360 0.0885
-1.000 0.3008 0.01547 0.00556 -0.0612 0.4288 0.0920
-0.750 0.3264 0.01534 0.00543 -0.0605 0.4214 0.0953
-0.500 0.3521 0.01530 0.00535 -0.0598 0.4146 0.0991
-0.250 0.3784 0.01524 0.00525 -0.0592 0.4074 0.1033
0.000 0.4036 0.01517 0.00517 -0.0585 0.4007 0.1077
0.250 0.4296 0.01513 0.00513 -0.0578 0.3947 0.1126
0.500 0.4556 0.01510 0.00508 -0.0572 0.3883 0.1179
0.750 0.4809 0.01507 0.00506 -0.0565 0.3826 0.1244
1.000 0.5069 0.01509 0.00504 -0.0559 0.3771 0.1314
1.250 0.5326 0.01504 0.00505 -0.0552 0.3712 0.1410
1.500 0.5578 0.01504 0.00506 -0.0545 0.3655 0.1539
1.750 0.5829 0.01501 0.00510 -0.0538 0.3602 0.1786
2.000 0.6066 0.01477 0.00523 -0.0529 0.3543 0.2811
2.250 0.6299 0.01462 0.00531 -0.0519 0.3489 0.3748
2.750 0.7483 0.01371 0.00573 -0.0645 0.3358 1.0000
3.000 0.7721 0.01392 0.00584 -0.0635 0.3313 1.0000
3.250 0.7956 0.01416 0.00596 -0.0625 0.3275 1.0000
3.500 0.8200 0.01435 0.00613 -0.0616 0.3231 1.0000
3.750 0.8439 0.01455 0.00629 -0.0607 0.3185 1.0000
4.000 0.8675 0.01479 0.00645 -0.0597 0.3144 1.0000
4.250 0.8907 0.01506 0.00662 -0.0586 0.3111 1.0000
4.500 0.9149 0.01529 0.00685 -0.0578 0.3077 1.0000
4.750 0.9388 0.01553 0.00708 -0.0569 0.3041 1.0000
5.000 0.9623 0.01578 0.00729 -0.0559 0.3004 1.0000
5.250 0.9854 0.01605 0.00750 -0.0550 0.2971 1.0000
5.500 1.0083 0.01637 0.00774 -0.0540 0.2941 1.0000
5.750 1.0320 0.01663 0.00803 -0.0531 0.2909 1.0000
6.000 1.0552 0.01689 0.00830 -0.0522 0.2871 1.0000
6.250 1.0778 0.01716 0.00855 -0.0511 0.2829 1.0000
6.500 1.0997 0.01747 0.00879 -0.0501 0.2790 1.0000
6.750 1.1222 0.01778 0.00910 -0.0491 0.2756 1.0000
7.000 1.1448 0.01807 0.00943 -0.0481 0.2720 1.0000
7.250 1.1668 0.01837 0.00975 -0.0471 0.2686 1.0000
7.500 1.1884 0.01871 0.01007 -0.0460 0.2654 1.0000
7.750 1.2096 0.01909 0.01040 -0.0449 0.2625 1.0000
8.000 1.2310 0.01944 0.01078 -0.0438 0.2597 1.0000
8.250 1.2522 0.01978 0.01119 -0.0427 0.2565 1.0000
8.500 1.2727 0.02013 0.01158 -0.0415 0.2532 1.0000
8.750 1.2924 0.02050 0.01196 -0.0403 0.2499 1.0000
9.000 1.3116 0.02092 0.01235 -0.0389 0.2470 1.0000
9.250 1.3307 0.02135 0.01280 -0.0376 0.2442 1.0000
9.500 1.3493 0.02174 0.01330 -0.0362 0.2411 1.0000
9.750 1.3670 0.02216 0.01378 -0.0347 0.2378 1.0000
10.000 1.3829 0.02259 0.01424 -0.0330 0.2344 1.0000
10.250 1.3967 0.02306 0.01469 -0.0309 0.2314 1.0000
10.500 1.4102 0.02356 0.01524 -0.0289 0.2283 1.0000
10.750 1.4235 0.02407 0.01586 -0.0269 0.2248 1.0000
11.000 1.4362 0.02462 0.01648 -0.0250 0.2214 1.0000
11.250 1.4476 0.02523 0.01712 -0.0230 0.2180 1.0000
11.500 1.4580 0.02594 0.01782 -0.0211 0.2149 1.0000
11.750 1.4692 0.02669 0.01870 -0.0194 0.2110 1.0000
12.000 1.4793 0.02752 0.01963 -0.0178 0.2070 1.0000
12.250 1.4875 0.02848 0.02063 -0.0162 0.2032 1.0000
12.500 1.4944 0.02959 0.02175 -0.0148 0.1998 1.0000
12.750 1.5029 0.03076 0.02306 -0.0136 0.1956 1.0000
13.000 1.5091 0.03212 0.02451 -0.0126 0.1912 1.0000
13.250 1.5130 0.03372 0.02613 -0.0117 0.1873 1.0000
13.500 1.5173 0.03544 0.02793 -0.0109 0.1834 1.0000
13.750 1.5206 0.03733 0.02993 -0.0104 0.1790 1.0000
14.000 1.5215 0.03950 0.03216 -0.0100 0.1751 1.0000
14.250 1.5201 0.04195 0.03463 -0.0098 0.1714 1.0000
14.500 1.5200 0.04445 0.03725 -0.0097 0.1674 1.0000
14.750 1.5167 0.04729 0.04017 -0.0097 0.1636 1.0000
15.000 1.5111 0.05046 0.04337 -0.0100 0.1603 1.0000
15.250 1.5055 0.05372 0.04671 -0.0104 0.1572 1.0000
15.500 1.4994 0.05722 0.05033 -0.0109 0.1538 1.0000
15.750 1.4920 0.06096 0.05415 -0.0117 0.1507 1.0000
16.000 1.4836 0.06487 0.05810 -0.0126 0.1478 1.0000
16.250 1.4761 0.06875 0.06201 -0.0135 0.1452 1.0000
16.500 1.4679 0.07292 0.06632 -0.0146 0.1426 1.0000
16.750 1.4587 0.07726 0.07077 -0.0159 0.1398 1.0000
17.000 1.4506 0.08147 0.07503 -0.0171 0.1372 1.0000
17.250 1.4450 0.08531 0.07889 -0.0182 0.1349 1.0000
17.500 1.4416 0.08883 0.08242 -0.0192 0.1325 1.0000
17.750 1.4299 0.09381 0.08756 -0.0209 0.1302 1.0000
18.000 1.4182 0.09884 0.09271 -0.0228 0.1276 1.0000
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Polar data table (+)
Polar graphs
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