MUE 139 (mue139-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: MUE 139 (mue139-il) Reynolds number: 500,000 Max Cl/Cd: 90.93 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mue139-il-500000-n5.txt Download as CSV file: xf-mue139-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.8596 0.03752 0.03410 -0.0780 1.0000 0.0320
-12.500 -0.8783 0.03299 0.02924 -0.0773 1.0000 0.0322
-12.250 -0.8797 0.03041 0.02641 -0.0756 1.0000 0.0323
-12.000 -0.8744 0.02849 0.02428 -0.0738 1.0000 0.0325
-11.750 -0.8650 0.02702 0.02270 -0.0719 1.0000 0.0327
-11.500 -0.8478 0.02583 0.02144 -0.0710 0.9991 0.0330
-11.250 -0.8164 0.02465 0.02017 -0.0727 0.9922 0.0332
-10.750 -0.7573 0.02273 0.01809 -0.0746 0.9631 0.0339
-10.500 -0.7110 0.02175 0.01700 -0.0789 0.9438 0.0344
-10.250 -0.6545 0.02060 0.01566 -0.0852 0.9173 0.0350
-10.000 -0.6134 0.01968 0.01447 -0.0883 0.8706 0.0355
-9.750 -0.5900 0.01908 0.01358 -0.0875 0.8255 0.0359
-9.500 -0.5691 0.01852 0.01278 -0.0862 0.7938 0.0363
-8.750 -0.5031 0.01701 0.01076 -0.0826 0.7345 0.0374
-8.500 -0.4794 0.01661 0.01027 -0.0816 0.7214 0.0378
-8.250 -0.4551 0.01627 0.00983 -0.0807 0.7100 0.0382
-8.000 -0.4304 0.01592 0.00940 -0.0799 0.6986 0.0386
-7.750 -0.4056 0.01558 0.00897 -0.0791 0.6876 0.0392
-7.500 -0.3807 0.01526 0.00855 -0.0782 0.6758 0.0398
-7.250 -0.3552 0.01494 0.00813 -0.0775 0.6652 0.0405
-7.000 -0.3299 0.01464 0.00770 -0.0767 0.6547 0.0412
-6.750 -0.3044 0.01430 0.00728 -0.0759 0.6430 0.0417
-6.500 -0.2791 0.01399 0.00691 -0.0752 0.6311 0.0424
-6.250 -0.2536 0.01376 0.00660 -0.0744 0.6169 0.0430
-6.000 -0.2279 0.01356 0.00631 -0.0736 0.5995 0.0437
-5.750 -0.2023 0.01337 0.00602 -0.0728 0.5792 0.0446
-5.500 -0.1766 0.01318 0.00572 -0.0720 0.5589 0.0454
-5.250 -0.1508 0.01301 0.00542 -0.0713 0.5397 0.0463
-5.000 -0.1251 0.01283 0.00514 -0.0705 0.5210 0.0472
-4.750 -0.0992 0.01269 0.00494 -0.0698 0.5035 0.0482
-4.500 -0.0731 0.01260 0.00476 -0.0691 0.4869 0.0494
-4.000 -0.0205 0.01240 0.00438 -0.0678 0.4594 0.0520
-3.750 0.0058 0.01227 0.00419 -0.0672 0.4493 0.0532
-3.500 0.0324 0.01217 0.00406 -0.0666 0.4402 0.0545
-3.250 0.0590 0.01209 0.00393 -0.0660 0.4325 0.0560
-3.000 0.0860 0.01200 0.00380 -0.0654 0.4252 0.0576
-2.750 0.1126 0.01193 0.00367 -0.0648 0.4181 0.0592
-2.500 0.1395 0.01184 0.00359 -0.0643 0.4122 0.0611
-2.250 0.1665 0.01179 0.00351 -0.0638 0.4054 0.0631
-1.750 0.2202 0.01167 0.00333 -0.0626 0.3928 0.0671
-1.500 0.2472 0.01163 0.00328 -0.0621 0.3864 0.0695
-1.250 0.2739 0.01163 0.00323 -0.0616 0.3808 0.0720
-1.000 0.3011 0.01158 0.00317 -0.0611 0.3757 0.0744
-0.750 0.3280 0.01154 0.00314 -0.0606 0.3700 0.0772
-0.500 0.3547 0.01154 0.00311 -0.0600 0.3642 0.0803
-0.250 0.3817 0.01153 0.00307 -0.0595 0.3593 0.0830
0.000 0.4086 0.01149 0.00306 -0.0590 0.3536 0.0865
0.250 0.4352 0.01151 0.00305 -0.0585 0.3474 0.0902
0.500 0.4620 0.01152 0.00304 -0.0579 0.3419 0.0935
0.750 0.4887 0.01151 0.00304 -0.0574 0.3357 0.0978
1.000 0.5152 0.01156 0.00305 -0.0569 0.3297 0.1023
1.250 0.5418 0.01157 0.00307 -0.0563 0.3249 0.1072
1.500 0.5684 0.01159 0.00310 -0.0558 0.3195 0.1129
1.750 0.5946 0.01163 0.00314 -0.0552 0.3142 0.1198
2.000 0.6207 0.01168 0.00319 -0.0547 0.3095 0.1290
2.250 0.6471 0.01169 0.00324 -0.0541 0.3050 0.1422
2.500 0.6727 0.01168 0.00331 -0.0535 0.3003 0.1724
2.750 0.6965 0.01153 0.00345 -0.0526 0.2955 0.2896
3.000 0.7217 0.01151 0.00354 -0.0519 0.2915 0.3440
3.250 0.7427 0.01112 0.00368 -0.0506 0.2878 0.5315
3.750 0.8700 0.01065 0.00414 -0.0656 0.2777 1.0000
4.000 0.8947 0.01079 0.00426 -0.0647 0.2751 1.0000
4.250 0.9191 0.01094 0.00439 -0.0639 0.2720 1.0000
4.500 0.9432 0.01111 0.00452 -0.0629 0.2688 1.0000
4.750 0.9670 0.01130 0.00467 -0.0620 0.2656 1.0000
5.000 0.9902 0.01154 0.00485 -0.0609 0.2615 1.0000
5.250 1.0148 0.01168 0.00498 -0.0601 0.2581 1.0000
5.500 1.0389 0.01185 0.00514 -0.0593 0.2542 1.0000
5.750 1.0626 0.01205 0.00532 -0.0583 0.2513 1.0000
6.000 1.0858 0.01227 0.00551 -0.0573 0.2482 1.0000
6.250 1.1087 0.01252 0.00572 -0.0563 0.2456 1.0000
6.500 1.1328 0.01269 0.00591 -0.0555 0.2438 1.0000
6.750 1.1568 0.01287 0.00610 -0.0546 0.2413 1.0000
7.000 1.1802 0.01307 0.00630 -0.0537 0.2386 1.0000
7.250 1.2032 0.01329 0.00652 -0.0528 0.2359 1.0000
7.500 1.2257 0.01354 0.00675 -0.0517 0.2333 1.0000
7.750 1.2476 0.01381 0.00701 -0.0506 0.2308 1.0000
8.000 1.2703 0.01404 0.00725 -0.0497 0.2287 1.0000
8.250 1.2933 0.01424 0.00749 -0.0487 0.2262 1.0000
8.500 1.3157 0.01447 0.00774 -0.0477 0.2232 1.0000
8.750 1.3373 0.01473 0.00800 -0.0466 0.2201 1.0000
9.000 1.3579 0.01502 0.00829 -0.0454 0.2172 1.0000
9.250 1.3779 0.01534 0.00861 -0.0441 0.2144 1.0000
9.500 1.3997 0.01557 0.00888 -0.0431 0.2119 1.0000
9.750 1.4204 0.01583 0.00917 -0.0419 0.2085 1.0000
10.000 1.4397 0.01615 0.00950 -0.0405 0.2045 1.0000
10.250 1.4564 0.01652 0.00986 -0.0387 0.2007 1.0000
10.500 1.4735 0.01683 0.01020 -0.0369 0.1976 1.0000
10.750 1.4901 0.01716 0.01056 -0.0351 0.1934 1.0000
11.000 1.5047 0.01758 0.01099 -0.0332 0.1888 1.0000
11.250 1.5188 0.01805 0.01146 -0.0312 0.1841 1.0000
11.500 1.5340 0.01851 0.01194 -0.0295 0.1787 1.0000
11.750 1.5464 0.01912 0.01255 -0.0276 0.1734 1.0000
12.000 1.5594 0.01975 0.01320 -0.0258 0.1683 1.0000
12.250 1.5708 0.02051 0.01396 -0.0241 0.1624 1.0000
12.500 1.5804 0.02142 0.01488 -0.0224 0.1576 1.0000
12.750 1.5915 0.02231 0.01581 -0.0210 0.1532 1.0000
13.000 1.6001 0.02344 0.01696 -0.0196 0.1488 1.0000
13.250 1.6071 0.02477 0.01831 -0.0184 0.1450 1.0000
13.500 1.6162 0.02603 0.01963 -0.0175 0.1417 1.0000
13.750 1.6233 0.02753 0.02118 -0.0167 0.1385 1.0000
14.000 1.6274 0.02937 0.02306 -0.0160 0.1354 1.0000
14.250 1.6306 0.03139 0.02513 -0.0155 0.1326 1.0000
14.500 1.6361 0.03324 0.02706 -0.0151 0.1302 1.0000
14.750 1.6389 0.03541 0.02929 -0.0148 0.1275 1.0000
15.000 1.6389 0.03791 0.03185 -0.0146 0.1252 1.0000
15.250 1.6343 0.04094 0.03494 -0.0146 0.1227 1.0000
15.500 1.6299 0.04402 0.03809 -0.0147 0.1208 1.0000
15.750 1.6295 0.04672 0.04089 -0.0148 0.1193 1.0000
16.000 1.6264 0.04978 0.04404 -0.0151 0.1177 1.0000
16.250 1.6208 0.05322 0.04757 -0.0155 0.1159 1.0000
16.500 1.6131 0.05700 0.05142 -0.0162 0.1142 1.0000
16.750 1.6009 0.06143 0.05592 -0.0171 0.1121 1.0000
17.000 1.5894 0.06586 0.06044 -0.0181 0.1108 1.0000
17.250 1.5792 0.07017 0.06483 -0.0191 0.1088 1.0000
17.500 1.5733 0.07395 0.06870 -0.0200 0.1074 1.0000
17.750 1.5659 0.07798 0.07282 -0.0209 0.1061 1.0000
18.000 1.5541 0.08262 0.07754 -0.0222 0.1037 1.0000
18.250 1.5428 0.08726 0.08224 -0.0235 0.1021 1.0000
18.500 1.5316 0.09191 0.08695 -0.0249 0.1006 1.0000
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