MUE 139 (mue139-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: MUE 139 (mue139-il) Reynolds number: 200,000 Max Cl/Cd: 58.32 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mue139-il-200000.txt Download as CSV file: xf-mue139-il-200000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.500 -0.2237 0.09402 0.09064 -0.0267 1.0000 0.0781
-8.250 -0.2246 0.09147 0.08817 -0.0274 1.0000 0.0800
-8.000 -0.2753 0.08923 0.08612 -0.0326 1.0000 0.0822
-7.750 -0.2571 0.08351 0.08043 -0.0383 0.9790 0.0829
-7.500 -0.2189 0.08025 0.07716 -0.0386 0.9626 0.0837
-7.250 -0.1766 0.07654 0.07340 -0.0437 0.9406 0.0855
-7.000 -0.1347 0.07136 0.06812 -0.0554 0.9089 0.0894
-6.750 -0.1225 0.06263 0.05911 -0.0740 0.8659 0.0935
-6.500 -0.0986 0.06058 0.05695 -0.0738 0.8354 0.0944
-6.250 -0.0833 0.05864 0.05487 -0.0735 0.8089 0.0958
-6.000 -0.0976 0.05364 0.04918 -0.0813 0.7892 0.1038
-5.750 -0.0841 0.04963 0.04517 -0.0806 0.7707 0.1047
-5.500 -0.0668 0.04780 0.04332 -0.0792 0.7519 0.1055
-5.250 -0.0498 0.04646 0.04193 -0.0777 0.7334 0.1068
-5.000 -0.0334 0.04496 0.04033 -0.0767 0.7159 0.1090
-4.750 -0.0255 0.04081 0.03562 -0.0784 0.7023 0.1180
-4.500 -0.0294 0.02759 0.02084 -0.0769 0.6965 0.0828
-4.250 -0.0037 0.02789 0.02146 -0.0764 0.6780 0.0856
-4.000 0.0165 0.02614 0.01939 -0.0752 0.6617 0.0864
-3.750 0.0375 0.02442 0.01731 -0.0738 0.6455 0.0871
-3.500 0.0596 0.02294 0.01548 -0.0726 0.6295 0.0880
-3.250 0.0828 0.02177 0.01395 -0.0713 0.6139 0.0896
-3.000 0.1069 0.02104 0.01280 -0.0701 0.5983 0.0920
-2.750 0.1307 0.01995 0.01156 -0.0692 0.5824 0.0944
-2.500 0.1559 0.01944 0.01098 -0.0684 0.5669 0.0967
-2.250 0.1814 0.01894 0.01031 -0.0676 0.5528 0.0995
-2.000 0.2071 0.01863 0.00973 -0.0666 0.5404 0.1030
-1.750 0.2326 0.01793 0.00891 -0.0659 0.5284 0.1061
-1.500 0.2586 0.01759 0.00853 -0.0653 0.5169 0.1095
-1.250 0.2848 0.01739 0.00816 -0.0645 0.5070 0.1137
-1.000 0.3111 0.01707 0.00773 -0.0638 0.4962 0.1176
-0.750 0.3370 0.01669 0.00732 -0.0632 0.4870 0.1219
-0.500 0.3631 0.01652 0.00712 -0.0625 0.4770 0.1273
-0.250 0.3893 0.01634 0.00682 -0.0618 0.4684 0.1324
0.000 0.4148 0.01606 0.00660 -0.0611 0.4594 0.1384
0.250 0.4411 0.01607 0.00649 -0.0605 0.4518 0.1453
0.500 0.4661 0.01579 0.00631 -0.0597 0.4435 0.1530
0.750 0.4920 0.01580 0.00624 -0.0590 0.4363 0.1623
1.000 0.5168 0.01565 0.00620 -0.0582 0.4288 0.1744
1.250 0.5418 0.01555 0.00615 -0.0574 0.4215 0.1916
1.500 0.5661 0.01544 0.00622 -0.0565 0.4149 0.2406
1.750 0.6627 0.01375 0.00642 -0.0704 0.4028 1.0000
2.000 0.6874 0.01409 0.00656 -0.0696 0.3972 1.0000
2.250 0.7112 0.01428 0.00673 -0.0685 0.3910 1.0000
2.500 0.7356 0.01452 0.00686 -0.0676 0.3855 1.0000
2.750 0.7608 0.01490 0.00705 -0.0669 0.3807 1.0000
3.000 0.7844 0.01512 0.00728 -0.0659 0.3753 1.0000
3.250 0.8085 0.01535 0.00747 -0.0649 0.3700 1.0000
3.500 0.8333 0.01563 0.00763 -0.0641 0.3655 1.0000
3.750 0.8583 0.01603 0.00792 -0.0634 0.3615 1.0000
4.000 0.8818 0.01630 0.00823 -0.0624 0.3571 1.0000
4.250 0.9060 0.01658 0.00849 -0.0616 0.3529 1.0000
4.500 0.9307 0.01686 0.00869 -0.0608 0.3490 1.0000
4.750 0.9564 0.01730 0.00899 -0.0603 0.3453 1.0000
5.000 0.9793 0.01761 0.00937 -0.0592 0.3416 1.0000
5.250 1.0028 0.01792 0.00971 -0.0583 0.3378 1.0000
5.500 1.0269 0.01819 0.00996 -0.0575 0.3338 1.0000
5.750 1.0518 0.01848 0.01015 -0.0568 0.3300 1.0000
6.000 1.0755 0.01891 0.01054 -0.0560 0.3261 1.0000
6.250 1.0974 0.01918 0.01091 -0.0549 0.3219 1.0000
6.500 1.1207 0.01946 0.01119 -0.0540 0.3179 1.0000
6.750 1.1451 0.01975 0.01142 -0.0533 0.3144 1.0000
7.000 1.1711 0.02027 0.01181 -0.0529 0.3110 1.0000
7.250 1.1912 0.02060 0.01229 -0.0516 0.3075 1.0000
7.500 1.2128 0.02095 0.01270 -0.0505 0.3036 1.0000
7.750 1.2359 0.02128 0.01304 -0.0496 0.3001 1.0000
8.000 1.2602 0.02161 0.01331 -0.0490 0.2969 1.0000
8.250 1.2841 0.02216 0.01381 -0.0484 0.2934 1.0000
8.500 1.3024 0.02254 0.01436 -0.0469 0.2896 1.0000
8.750 1.3230 0.02291 0.01478 -0.0457 0.2857 1.0000
9.000 1.3456 0.02324 0.01509 -0.0449 0.2822 1.0000
9.250 1.3705 0.02369 0.01545 -0.0445 0.2788 1.0000
9.500 1.3882 0.02423 0.01612 -0.0430 0.2751 1.0000
9.750 1.4051 0.02466 0.01666 -0.0413 0.2710 1.0000
10.000 1.4250 0.02498 0.01699 -0.0401 0.2669 1.0000
10.250 1.4483 0.02535 0.01728 -0.0395 0.2632 1.0000
10.500 1.4655 0.02600 0.01801 -0.0381 0.2594 1.0000
10.750 1.4780 0.02650 0.01866 -0.0359 0.2551 1.0000
11.000 1.4948 0.02687 0.01906 -0.0343 0.2509 1.0000
11.250 1.5166 0.02725 0.01934 -0.0336 0.2469 1.0000
11.500 1.5273 0.02794 0.02016 -0.0313 0.2428 1.0000
11.750 1.5342 0.02851 0.02087 -0.0285 0.2384 1.0000
12.000 1.5454 0.02894 0.02131 -0.0261 0.2344 1.0000
12.250 1.5675 0.02941 0.02165 -0.0255 0.2302 1.0000
12.500 1.5622 0.03027 0.02272 -0.0213 0.2265 1.0000
12.750 1.5632 0.03110 0.02366 -0.0183 0.2223 1.0000
13.000 1.5719 0.03174 0.02431 -0.0163 0.2183 1.0000
13.250 1.5896 0.03239 0.02486 -0.0154 0.2143 1.0000
13.500 1.5799 0.03395 0.02667 -0.0124 0.2105 1.0000
13.750 1.5800 0.03531 0.02813 -0.0106 0.2065 1.0000
14.000 1.5869 0.03637 0.02920 -0.0094 0.2029 1.0000
14.250 1.5977 0.03746 0.03024 -0.0085 0.1991 1.0000
14.500 1.5874 0.03992 0.03293 -0.0072 0.1955 1.0000
14.750 1.5856 0.04197 0.03509 -0.0064 0.1917 1.0000
15.000 1.5908 0.04352 0.03664 -0.0059 0.1884 1.0000
15.250 1.6005 0.04487 0.03794 -0.0052 0.1850 1.0000
15.500 1.5859 0.04844 0.04174 -0.0051 0.1818 1.0000
15.750 1.5792 0.05143 0.04484 -0.0052 0.1786 1.0000
16.000 1.5805 0.05365 0.04710 -0.0051 0.1756 1.0000
16.250 1.5985 0.05417 0.04750 -0.0044 0.1723 1.0000
16.500 1.5774 0.05896 0.05252 -0.0053 0.1697 1.0000
16.750 1.5583 0.06385 0.05760 -0.0064 0.1668 1.0000
17.000 1.5506 0.06752 0.06136 -0.0073 0.1638 1.0000
17.250 1.5564 0.06949 0.06332 -0.0074 0.1612 1.0000
17.500 1.5741 0.06996 0.06369 -0.0066 0.1582 1.0000
17.750 1.5327 0.07840 0.07244 -0.0099 0.1560 1.0000
18.000 1.4897 0.08763 0.08193 -0.0137 0.1533 1.0000
18.250 1.4668 0.09419 0.08863 -0.0163 0.1506 1.0000
18.500 1.4871 0.09413 0.08851 -0.0156 0.1483 1.0000
18.750 1.5411 0.08894 0.08310 -0.0119 0.1457 1.0000
19.000 0.9957 0.20391 0.19900 -0.0730 0.1224 1.0000
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