MUE 139 (mue139-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: MUE 139 (mue139-il) Reynolds number: 100,000 Max Cl/Cd: 44.91 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mue139-il-100000-n5.txt Download as CSV file: xf-mue139-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.250 -0.2558 0.11612 0.11087 -0.0247 1.0000 0.0815
-10.000 -0.2573 0.11331 0.10812 -0.0264 1.0000 0.0819
-9.750 -0.2581 0.11033 0.10519 -0.0280 1.0000 0.0820
-9.500 -0.2573 0.10729 0.10221 -0.0291 1.0000 0.0821
-9.250 -0.2580 0.10426 0.09924 -0.0304 1.0000 0.0822
-9.000 -0.2595 0.10117 0.09623 -0.0316 1.0000 0.0823
-8.750 -0.2601 0.09813 0.09325 -0.0324 1.0000 0.0823
-8.250 -0.2547 0.08858 0.08378 -0.0322 1.0000 0.0652
-8.000 -0.2535 0.08619 0.08150 -0.0316 1.0000 0.0646
-7.750 -0.2362 0.08171 0.07703 -0.0367 0.9629 0.0639
-7.500 -0.2153 0.07628 0.07156 -0.0449 0.9246 0.0634
-7.250 -0.1974 0.06995 0.06511 -0.0551 0.8888 0.0641
-7.000 -0.1824 0.06378 0.05875 -0.0637 0.8574 0.0643
-6.750 -0.1727 0.05811 0.05287 -0.0694 0.8302 0.0642
-6.500 -0.1664 0.05243 0.04692 -0.0735 0.8079 0.0641
-6.250 -0.1629 0.04634 0.04043 -0.0763 0.7893 0.0643
-6.000 -0.1646 0.03914 0.03249 -0.0779 0.7738 0.0659
-5.750 -0.1421 0.03836 0.03165 -0.0774 0.7562 0.0668
-5.500 -0.1227 0.03668 0.02975 -0.0770 0.7400 0.0679
-5.250 -0.1048 0.03434 0.02705 -0.0765 0.7250 0.0690
-5.000 -0.0864 0.03199 0.02426 -0.0758 0.7107 0.0702
-4.750 -0.0678 0.02970 0.02147 -0.0749 0.6961 0.0721
-4.500 -0.0471 0.02806 0.01941 -0.0739 0.6810 0.0742
-4.250 -0.0234 0.02740 0.01865 -0.0730 0.6651 0.0757
-4.000 -0.0001 0.02651 0.01754 -0.0721 0.6495 0.0775
-3.750 0.0233 0.02543 0.01613 -0.0711 0.6341 0.0794
-3.500 0.0469 0.02435 0.01458 -0.0700 0.6185 0.0824
-3.250 0.0713 0.02383 0.01403 -0.0692 0.6020 0.0844
-3.000 0.0961 0.02329 0.01336 -0.0684 0.5862 0.0867
-2.750 0.1212 0.02266 0.01251 -0.0675 0.5712 0.0894
-2.500 0.1465 0.02209 0.01165 -0.0666 0.5571 0.0928
-2.250 0.1716 0.02168 0.01120 -0.0659 0.5438 0.0956
-2.000 0.1972 0.02128 0.01069 -0.0651 0.5304 0.0988
-1.750 0.2230 0.02093 0.01014 -0.0643 0.5184 0.1027
-1.250 0.2740 0.02028 0.00939 -0.0629 0.4966 0.1102
-1.000 0.2998 0.02007 0.00901 -0.0621 0.4870 0.1149
-0.750 0.3251 0.01980 0.00873 -0.0614 0.4769 0.1195
-0.500 0.3504 0.01961 0.00850 -0.0606 0.4683 0.1246
-0.250 0.3760 0.01949 0.00829 -0.0598 0.4593 0.1306
0.000 0.4009 0.01932 0.00810 -0.0591 0.4521 0.1370
0.250 0.4264 0.01923 0.00800 -0.0583 0.4440 0.1445
0.500 0.4515 0.01913 0.00789 -0.0576 0.4370 0.1533
0.750 0.4773 0.01909 0.00784 -0.0569 0.4297 0.1644
1.250 0.5298 0.01895 0.00779 -0.0559 0.4160 0.2118
1.500 0.5558 0.01872 0.00798 -0.0556 0.4086 0.3219
2.000 0.6617 0.01764 0.00828 -0.0650 0.3936 1.0000
2.250 0.6856 0.01792 0.00844 -0.0640 0.3876 1.0000
2.500 0.7095 0.01821 0.00857 -0.0631 0.3825 1.0000
2.750 0.7334 0.01853 0.00877 -0.0621 0.3772 1.0000
3.000 0.7570 0.01883 0.00901 -0.0612 0.3713 1.0000
3.250 0.7808 0.01914 0.00920 -0.0603 0.3664 1.0000
3.500 0.8052 0.01948 0.00939 -0.0594 0.3626 1.0000
3.750 0.8285 0.01984 0.00976 -0.0585 0.3577 1.0000
4.000 0.8520 0.02020 0.01008 -0.0576 0.3530 1.0000
4.250 0.8758 0.02054 0.01034 -0.0567 0.3488 1.0000
4.500 0.9001 0.02089 0.01056 -0.0559 0.3452 1.0000
4.750 0.9226 0.02130 0.01102 -0.0549 0.3405 1.0000
5.000 0.9456 0.02171 0.01143 -0.0540 0.3362 1.0000
5.250 0.9690 0.02211 0.01178 -0.0532 0.3326 1.0000
5.500 0.9930 0.02249 0.01207 -0.0524 0.3294 1.0000
5.750 1.0157 0.02294 0.01252 -0.0515 0.3258 1.0000
6.000 1.0373 0.02342 0.01307 -0.0504 0.3215 1.0000
6.250 1.0595 0.02387 0.01352 -0.0495 0.3177 1.0000
6.500 1.0824 0.02427 0.01389 -0.0486 0.3142 1.0000
6.750 1.1063 0.02466 0.01418 -0.0479 0.3111 1.0000
7.000 1.1253 0.02523 0.01487 -0.0466 0.3066 1.0000
7.250 1.1454 0.02572 0.01542 -0.0454 0.3022 1.0000
7.500 1.1668 0.02612 0.01580 -0.0444 0.2983 1.0000
7.750 1.1897 0.02649 0.01609 -0.0436 0.2949 1.0000
8.000 1.2075 0.02712 0.01683 -0.0422 0.2909 1.0000
8.250 1.2252 0.02772 0.01753 -0.0408 0.2868 1.0000
8.500 1.2445 0.02822 0.01805 -0.0396 0.2829 1.0000
8.750 1.2656 0.02864 0.01843 -0.0386 0.2796 1.0000
9.000 1.2842 0.02923 0.01905 -0.0374 0.2763 1.0000
9.250 1.2973 0.03002 0.02000 -0.0355 0.2722 1.0000
9.500 1.3126 0.03067 0.02072 -0.0339 0.2683 1.0000
9.750 1.3303 0.03119 0.02125 -0.0326 0.2649 1.0000
10.000 1.3514 0.03163 0.02162 -0.0317 0.2618 1.0000
10.250 1.3573 0.03265 0.02284 -0.0291 0.2579 1.0000
10.500 1.3640 0.03355 0.02387 -0.0266 0.2540 1.0000
10.750 1.3736 0.03427 0.02464 -0.0244 0.2504 1.0000
11.000 1.3883 0.03482 0.02517 -0.0229 0.2472 1.0000
11.250 1.3963 0.03575 0.02615 -0.0208 0.2440 1.0000
11.500 1.3904 0.03733 0.02795 -0.0178 0.2401 1.0000
11.750 1.3912 0.03872 0.02944 -0.0157 0.2363 1.0000
12.000 1.3995 0.03972 0.03048 -0.0143 0.2329 1.0000
12.250 1.4163 0.04029 0.03097 -0.0134 0.2298 1.0000
12.500 1.3946 0.04354 0.03453 -0.0115 0.2258 1.0000
12.750 1.3821 0.04653 0.03770 -0.0105 0.2218 1.0000
13.000 1.3829 0.04855 0.03978 -0.0100 0.2182 1.0000
13.250 1.3982 0.04926 0.04043 -0.0093 0.2151 1.0000
13.500 1.3541 0.05615 0.04764 -0.0102 0.2107 1.0000
13.750 1.3031 0.06492 0.05666 -0.0127 0.2055 1.0000
14.000 1.3114 0.06655 0.05830 -0.0126 0.2021 1.0000
14.500 1.1443 0.09803 0.09017 -0.0256 0.1844 1.0000
14.750 1.2022 0.09165 0.08374 -0.0219 0.1855 1.0000
|
Polar data table (+)
Polar graphs
<< Back to MUE 139 (mue139-il)