MUE 139 (mue139-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: MUE 139 (mue139-il) Reynolds number: 1,000,000 Max Cl/Cd: 115.26 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mue139-il-1000000-n5.txt Download as CSV file: xf-mue139-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.500 -1.1558 0.03218 0.02890 -0.0892 1.0000 0.0260
-15.250 -1.1561 0.03009 0.02669 -0.0877 1.0000 0.0261
-15.000 -1.1489 0.02862 0.02513 -0.0862 1.0000 0.0264
-14.750 -1.1399 0.02728 0.02370 -0.0845 1.0000 0.0265
-14.500 -1.1276 0.02619 0.02253 -0.0829 1.0000 0.0267
-14.250 -1.1147 0.02515 0.02140 -0.0813 1.0000 0.0269
-14.000 -1.1001 0.02423 0.02040 -0.0796 1.0000 0.0272
-13.750 -1.0851 0.02333 0.01942 -0.0780 1.0000 0.0273
-13.500 -1.0690 0.02250 0.01852 -0.0763 1.0000 0.0275
-13.250 -1.0518 0.02177 0.01771 -0.0747 1.0000 0.0278
-13.000 -1.0339 0.02102 0.01689 -0.0732 0.9999 0.0279
-12.750 -1.0002 0.02031 0.01609 -0.0747 0.9979 0.0283
-12.500 -0.9682 0.01955 0.01525 -0.0759 0.9936 0.0284
-12.250 -0.9410 0.01887 0.01450 -0.0760 0.9864 0.0286
-12.000 -0.9147 0.01806 0.01362 -0.0760 0.9744 0.0290
-11.750 -0.8760 0.01727 0.01277 -0.0784 0.9578 0.0293
-11.500 -0.8082 0.01639 0.01180 -0.0868 0.9348 0.0297
-11.250 -0.7646 0.01596 0.01108 -0.0900 0.8571 0.0300
-11.000 -0.7451 0.01576 0.01063 -0.0882 0.7985 0.0303
-10.750 -0.7234 0.01548 0.01018 -0.0868 0.7674 0.0306
-10.500 -0.7002 0.01518 0.00976 -0.0857 0.7481 0.0309
-10.250 -0.6763 0.01487 0.00935 -0.0847 0.7322 0.0312
-10.000 -0.6520 0.01455 0.00894 -0.0838 0.7183 0.0315
-9.750 -0.6275 0.01425 0.00854 -0.0829 0.7060 0.0318
-9.500 -0.6027 0.01395 0.00816 -0.0820 0.6949 0.0321
-9.250 -0.5773 0.01366 0.00778 -0.0812 0.6859 0.0323
-9.000 -0.5519 0.01339 0.00743 -0.0805 0.6763 0.0325
-8.750 -0.5268 0.01303 0.00702 -0.0797 0.6675 0.0330
-8.500 -0.5015 0.01275 0.00667 -0.0789 0.6564 0.0334
-8.250 -0.4755 0.01249 0.00636 -0.0782 0.6469 0.0338
-7.750 -0.4232 0.01204 0.00581 -0.0768 0.6273 0.0347
-7.500 -0.3970 0.01185 0.00555 -0.0761 0.6161 0.0352
-7.250 -0.3706 0.01166 0.00529 -0.0755 0.6029 0.0356
-7.000 -0.3442 0.01149 0.00505 -0.0748 0.5872 0.0362
-6.750 -0.3182 0.01138 0.00482 -0.0740 0.5641 0.0366
-6.500 -0.2925 0.01125 0.00458 -0.0733 0.5376 0.0372
-6.250 -0.2666 0.01113 0.00436 -0.0725 0.5132 0.0380
-6.000 -0.2403 0.01102 0.00417 -0.0719 0.4944 0.0387
-5.750 -0.2138 0.01092 0.00400 -0.0712 0.4771 0.0394
-5.500 -0.1871 0.01083 0.00384 -0.0706 0.4618 0.0401
-5.250 -0.1604 0.01075 0.00368 -0.0700 0.4489 0.0409
-5.000 -0.1334 0.01067 0.00353 -0.0694 0.4382 0.0415
-4.750 -0.1064 0.01054 0.00338 -0.0689 0.4304 0.0425
-4.500 -0.0793 0.01044 0.00325 -0.0683 0.4228 0.0436
-4.250 -0.0521 0.01036 0.00314 -0.0678 0.4159 0.0446
-4.000 -0.0246 0.01028 0.00302 -0.0673 0.4103 0.0458
-3.750 0.0028 0.01021 0.00292 -0.0668 0.4041 0.0467
-3.500 0.0299 0.01013 0.00282 -0.0663 0.3980 0.0482
-3.250 0.0574 0.01005 0.00273 -0.0659 0.3928 0.0497
-3.000 0.0848 0.00999 0.00264 -0.0654 0.3863 0.0510
-2.750 0.1121 0.00997 0.00257 -0.0649 0.3801 0.0522
-2.500 0.1397 0.00989 0.00249 -0.0644 0.3755 0.0537
-2.250 0.1671 0.00983 0.00243 -0.0640 0.3702 0.0554
-2.000 0.1945 0.00981 0.00238 -0.0635 0.3644 0.0571
-1.750 0.2221 0.00978 0.00233 -0.0630 0.3599 0.0587
-1.500 0.2495 0.00973 0.00228 -0.0626 0.3547 0.0611
-1.250 0.2769 0.00971 0.00225 -0.0621 0.3489 0.0632
-1.000 0.3043 0.00971 0.00222 -0.0617 0.3437 0.0652
-0.750 0.3317 0.00969 0.00220 -0.0612 0.3381 0.0678
-0.500 0.3590 0.00969 0.00219 -0.0608 0.3316 0.0707
-0.250 0.3862 0.00971 0.00218 -0.0603 0.3254 0.0731
0.000 0.4135 0.00970 0.00218 -0.0599 0.3196 0.0761
0.250 0.4406 0.00973 0.00219 -0.0594 0.3135 0.0793
0.500 0.4679 0.00976 0.00220 -0.0590 0.3084 0.0819
0.750 0.4951 0.00977 0.00221 -0.0585 0.3033 0.0857
1.000 0.5220 0.00981 0.00224 -0.0580 0.2976 0.0894
1.250 0.5491 0.00986 0.00227 -0.0576 0.2929 0.0922
1.500 0.5761 0.00987 0.00230 -0.0571 0.2887 0.0972
1.750 0.6030 0.00992 0.00234 -0.0566 0.2841 0.1020
2.000 0.6296 0.00999 0.00239 -0.0561 0.2789 0.1069
2.250 0.6565 0.01002 0.00245 -0.0557 0.2753 0.1137
2.500 0.6833 0.01005 0.00250 -0.0552 0.2718 0.1227
2.750 0.7099 0.01010 0.00256 -0.0547 0.2685 0.1335
3.000 0.7360 0.01013 0.00264 -0.0542 0.2651 0.1567
3.250 0.7604 0.01000 0.00276 -0.0534 0.2618 0.2614
3.500 0.7864 0.00997 0.00286 -0.0528 0.2599 0.3169
3.750 0.8123 0.00996 0.00295 -0.0522 0.2575 0.3570
4.000 0.8197 0.00889 0.00312 -0.0481 0.2553 0.8268
4.500 0.9665 0.00916 0.00354 -0.0675 0.2436 1.0000
4.750 0.9913 0.00928 0.00365 -0.0667 0.2406 1.0000
5.000 1.0160 0.00942 0.00376 -0.0658 0.2382 1.0000
5.250 1.0405 0.00956 0.00389 -0.0650 0.2360 1.0000
5.500 1.0648 0.00973 0.00402 -0.0641 0.2332 1.0000
5.750 1.0888 0.00991 0.00417 -0.0632 0.2301 1.0000
6.000 1.1135 0.01004 0.00430 -0.0624 0.2286 1.0000
6.250 1.1382 0.01017 0.00444 -0.0617 0.2269 1.0000
6.500 1.1627 0.01031 0.00458 -0.0609 0.2250 1.0000
6.750 1.1870 0.01047 0.00473 -0.0601 0.2228 1.0000
7.000 1.2110 0.01064 0.00489 -0.0592 0.2202 1.0000
7.250 1.2346 0.01084 0.00507 -0.0583 0.2171 1.0000
7.500 1.2582 0.01104 0.00525 -0.0574 0.2142 1.0000
7.750 1.2825 0.01119 0.00542 -0.0567 0.2124 1.0000
8.000 1.3065 0.01136 0.00559 -0.0559 0.2101 1.0000
8.250 1.3301 0.01154 0.00578 -0.0550 0.2073 1.0000
8.500 1.3531 0.01176 0.00598 -0.0541 0.2039 1.0000
8.750 1.3755 0.01201 0.00621 -0.0531 0.1998 1.0000
9.000 1.3989 0.01220 0.00641 -0.0523 0.1970 1.0000
9.250 1.4215 0.01242 0.00663 -0.0513 0.1930 1.0000
9.500 1.4432 0.01270 0.00688 -0.0503 0.1884 1.0000
9.750 1.4646 0.01297 0.00715 -0.0492 0.1840 1.0000
10.000 1.4857 0.01325 0.00742 -0.0481 0.1781 1.0000
10.250 1.5048 0.01364 0.00776 -0.0467 0.1714 1.0000
10.500 1.5243 0.01398 0.00809 -0.0453 0.1648 1.0000
10.750 1.5414 0.01443 0.00850 -0.0436 0.1577 1.0000
11.000 1.5590 0.01483 0.00889 -0.0420 0.1519 1.0000
11.250 1.5721 0.01530 0.00933 -0.0397 0.1464 1.0000
11.500 1.5868 0.01569 0.00974 -0.0376 0.1425 1.0000
11.750 1.6007 0.01614 0.01019 -0.0355 0.1384 1.0000
12.000 1.6135 0.01668 0.01072 -0.0333 0.1345 1.0000
12.250 1.6280 0.01718 0.01124 -0.0315 0.1316 1.0000
12.500 1.6422 0.01771 0.01179 -0.0298 0.1286 1.0000
12.750 1.6546 0.01836 0.01246 -0.0280 0.1254 1.0000
13.000 1.6657 0.01914 0.01325 -0.0263 0.1222 1.0000
13.250 1.6783 0.01986 0.01401 -0.0248 0.1200 1.0000
13.500 1.6910 0.02064 0.01482 -0.0235 0.1181 1.0000
13.750 1.7024 0.02154 0.01577 -0.0223 0.1160 1.0000
14.000 1.7115 0.02267 0.01693 -0.0211 0.1134 1.0000
14.250 1.7190 0.02400 0.01829 -0.0200 0.1109 1.0000
14.500 1.7274 0.02535 0.01968 -0.0191 0.1083 1.0000
14.750 1.7360 0.02677 0.02115 -0.0185 0.1063 1.0000
15.000 1.7436 0.02832 0.02276 -0.0179 0.1048 1.0000
15.250 1.7474 0.03028 0.02476 -0.0175 0.1024 1.0000
15.500 1.7471 0.03269 0.02721 -0.0171 0.0994 1.0000
15.750 1.7509 0.03477 0.02935 -0.0168 0.0982 1.0000
16.000 1.7530 0.03706 0.03171 -0.0166 0.0962 1.0000
16.250 1.7514 0.03975 0.03446 -0.0166 0.0942 1.0000
16.500 1.7496 0.04253 0.03732 -0.0166 0.0932 1.0000
16.750 1.7409 0.04611 0.04096 -0.0168 0.0909 1.0000
17.000 1.7301 0.05007 0.04500 -0.0173 0.0892 1.0000
17.250 1.7239 0.05361 0.04863 -0.0178 0.0883 1.0000
17.500 1.7155 0.05750 0.05260 -0.0185 0.0867 1.0000
17.750 1.7054 0.06169 0.05689 -0.0193 0.0859 1.0000
18.000 1.6916 0.06640 0.06168 -0.0204 0.0842 1.0000
18.250 1.6772 0.07124 0.06661 -0.0215 0.0831 1.0000
18.500 1.6569 0.07691 0.07235 -0.0230 0.0812 1.0000
18.750 1.6376 0.08250 0.07803 -0.0245 0.0797 1.0000
19.000 1.6232 0.08751 0.08313 -0.0259 0.0786 1.0000
|
Polar data table (+)
Polar graphs
<< Back to MUE 139 (mue139-il)