FX 84-W-140 (fx84w140-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 84-W-140 (fx84w140-il) Reynolds number: 100,000 Max Cl/Cd: 50.62 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w140-il-100000-n5.txt Download as CSV file: xf-fx84w140-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-140
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
------ -------- --------- --------- -------- -------- --------
-10.500 -0.2397 0.09606 0.09106 -0.0769 0.9606 0.0389
-10.250 -0.2340 0.09079 0.08578 -0.0815 0.9534 0.0388
-10.000 -0.2304 0.08508 0.08006 -0.0865 0.9461 0.0387
-9.750 -0.2309 0.07914 0.07412 -0.0914 0.9372 0.0386
-9.500 -0.2360 0.07207 0.06704 -0.0976 0.9285 0.0384
-9.250 -0.2672 0.05997 0.05489 -0.1087 0.9143 0.0376
-9.000 -0.3093 0.05250 0.04715 -0.1121 0.8986 0.0371
-8.750 -0.3301 0.04788 0.04223 -0.1120 0.8866 0.0371
-8.500 -0.3380 0.04408 0.03806 -0.1112 0.8778 0.0376
-8.250 -0.3372 0.04101 0.03459 -0.1102 0.8699 0.0386
-8.000 -0.3342 0.03788 0.03095 -0.1090 0.8627 0.0402
-7.750 -0.3285 0.03471 0.02706 -0.1074 0.8554 0.0418
-7.500 -0.3091 0.03323 0.02547 -0.1069 0.8511 0.0430
-7.250 -0.2926 0.03194 0.02400 -0.1059 0.8440 0.0443
-7.000 -0.2728 0.03055 0.02234 -0.1052 0.8386 0.0464
-6.750 -0.2511 0.02897 0.02027 -0.1045 0.8348 0.0494
-6.500 -0.2320 0.02791 0.01911 -0.1036 0.8277 0.0514
-6.250 -0.2089 0.02696 0.01805 -0.1031 0.8228 0.0538
-6.000 -0.1839 0.02599 0.01682 -0.1027 0.8192 0.0576
-5.750 -0.1627 0.02514 0.01582 -0.1018 0.8126 0.0608
-5.500 -0.1389 0.02441 0.01507 -0.1014 0.8076 0.0641
-5.250 -0.1129 0.02369 0.01416 -0.1010 0.8040 0.0692
-5.000 -0.0906 0.02305 0.01350 -0.1003 0.7982 0.0734
-4.750 -0.0669 0.02252 0.01292 -0.0997 0.7929 0.0789
-4.500 -0.0413 0.02189 0.01220 -0.0993 0.7890 0.0855
-4.250 -0.0172 0.02143 0.01172 -0.0988 0.7844 0.0928
-4.000 0.0052 0.02103 0.01132 -0.0980 0.7784 0.1015
-3.750 0.0308 0.02057 0.01082 -0.0976 0.7742 0.1128
-3.500 0.0576 0.02009 0.01032 -0.0974 0.7711 0.1276
-3.250 0.0782 0.01988 0.01018 -0.0965 0.7640 0.1444
-3.000 0.1033 0.01948 0.00985 -0.0961 0.7594 0.1692
-2.750 0.1299 0.01901 0.00947 -0.0959 0.7560 0.2058
-2.500 0.1511 0.01874 0.00941 -0.0951 0.7498 0.2553
-2.250 0.1740 0.01822 0.00923 -0.0945 0.7447 0.3407
-2.000 0.1967 0.01748 0.00908 -0.0936 0.7411 0.4908
-1.750 0.2150 0.01722 0.00933 -0.0913 0.7358 0.6306
-1.500 0.2346 0.01724 0.00952 -0.0891 0.7303 0.7161
-1.250 0.2578 0.01721 0.00951 -0.0873 0.7264 0.7723
-1.000 0.2808 0.01724 0.00951 -0.0856 0.7225 0.8141
-0.750 0.2993 0.01746 0.00971 -0.0834 0.7160 0.8473
-0.500 0.3244 0.01746 0.00966 -0.0822 0.7118 0.8779
-0.250 0.3557 0.01739 0.00948 -0.0821 0.7088 0.9055
0.000 0.3878 0.01760 0.00966 -0.0828 0.7026 0.9352
0.250 0.4418 0.01761 0.00958 -0.0876 0.6984 0.9638
0.500 0.4945 0.01750 0.00933 -0.0924 0.6949 0.9777
0.750 0.5372 0.01747 0.00920 -0.0957 0.6908 0.9873
1.000 0.5752 0.01761 0.00930 -0.0984 0.6845 0.9985
1.250 0.5968 0.01762 0.00923 -0.0976 0.6799 1.0000
1.500 0.6151 0.01768 0.00922 -0.0961 0.6755 1.0000
1.750 0.6256 0.01799 0.00952 -0.0935 0.6685 1.0000
2.000 0.6464 0.01802 0.00948 -0.0923 0.6640 1.0000
2.250 0.6660 0.01817 0.00957 -0.0911 0.6591 1.0000
2.500 0.6825 0.01846 0.00987 -0.0894 0.6525 1.0000
2.750 0.7083 0.01850 0.00984 -0.0891 0.6482 1.0000
3.000 0.7303 0.01872 0.01003 -0.0883 0.6429 1.0000
3.250 0.7505 0.01901 0.01033 -0.0873 0.6366 1.0000
3.500 0.7783 0.01906 0.01035 -0.0873 0.6325 1.0000
3.750 0.8002 0.01935 0.01065 -0.0866 0.6267 1.0000
4.000 0.8222 0.01964 0.01095 -0.0858 0.6206 1.0000
4.250 0.8513 0.01967 0.01097 -0.0860 0.6165 1.0000
4.500 0.8710 0.02007 0.01142 -0.0850 0.6099 1.0000
4.750 0.8948 0.02029 0.01167 -0.0845 0.6040 1.0000
5.000 0.9258 0.02027 0.01164 -0.0849 0.6000 1.0000
5.250 0.9411 0.02082 0.01229 -0.0833 0.5921 1.0000
5.500 0.9684 0.02092 0.01241 -0.0833 0.5867 1.0000
5.750 0.9915 0.02120 0.01273 -0.0827 0.5806 1.0000
6.000 1.0118 0.02155 0.01317 -0.0817 0.5735 1.0000
6.250 1.0438 0.02149 0.01313 -0.0822 0.5689 1.0000
6.500 1.0563 0.02214 0.01390 -0.0802 0.5604 1.0000
6.750 1.0854 0.02216 0.01397 -0.0804 0.5548 1.0000
7.000 1.1006 0.02266 0.01458 -0.0787 0.5462 1.0000
7.250 1.1289 0.02266 0.01461 -0.0786 0.5393 1.0000
7.500 1.1424 0.02319 0.01527 -0.0767 0.5302 1.0000
7.750 1.1712 0.02319 0.01532 -0.0767 0.5233 1.0000
8.000 1.1816 0.02382 0.01609 -0.0744 0.5137 1.0000
8.250 1.2079 0.02386 0.01618 -0.0740 0.5057 1.0000
8.500 1.2177 0.02431 0.01674 -0.0714 0.4943 1.0000
8.750 1.2258 0.02472 0.01720 -0.0685 0.4802 1.0000
9.000 1.2350 0.02509 0.01758 -0.0658 0.4637 1.0000
9.250 1.2452 0.02549 0.01795 -0.0634 0.4457 1.0000
9.500 1.2488 0.02638 0.01889 -0.0605 0.4281 1.0000
9.750 1.2531 0.02737 0.01994 -0.0580 0.4103 1.0000
10.000 1.2575 0.02845 0.02103 -0.0556 0.3911 1.0000
10.250 1.2624 0.02956 0.02210 -0.0534 0.3699 1.0000
10.500 1.2637 0.03103 0.02356 -0.0511 0.3464 1.0000
10.750 1.2644 0.03263 0.02509 -0.0489 0.3210 1.0000
11.000 1.2629 0.03450 0.02686 -0.0468 0.2932 1.0000
11.250 1.2594 0.03667 0.02890 -0.0448 0.2649 1.0000
11.500 1.2535 0.03917 0.03128 -0.0429 0.2354 1.0000
11.750 1.2466 0.04192 0.03389 -0.0412 0.2074 1.0000
12.000 1.2391 0.04492 0.03676 -0.0398 0.1802 1.0000
12.250 1.2319 0.04806 0.03978 -0.0387 0.1551 1.0000
12.500 1.2241 0.05142 0.04302 -0.0378 0.1327 1.0000
12.750 1.2184 0.05472 0.04624 -0.0372 0.1141 1.0000
13.000 1.2139 0.05804 0.04951 -0.0367 0.1001 1.0000
13.250 1.2105 0.06132 0.05277 -0.0364 0.0894 1.0000
13.500 1.2071 0.06469 0.05613 -0.0362 0.0813 1.0000
13.750 1.2058 0.06792 0.05942 -0.0361 0.0741 1.0000
14.000 1.2047 0.07116 0.06269 -0.0361 0.0689 1.0000
14.250 1.2052 0.07427 0.06588 -0.0362 0.0641 1.0000
14.500 1.2033 0.07773 0.06932 -0.0364 0.0603 1.0000
14.750 1.2068 0.08053 0.07226 -0.0365 0.0565 1.0000
15.000 1.2088 0.08356 0.07536 -0.0367 0.0534 1.0000
15.250 1.2097 0.08667 0.07846 -0.0370 0.0510 1.0000
15.500 1.2156 0.08920 0.08114 -0.0371 0.0483 1.0000
15.750 1.2202 0.09192 0.08397 -0.0373 0.0458 1.0000
16.000 1.2242 0.09474 0.08684 -0.0377 0.0438 1.0000
16.250 1.2298 0.09718 0.08926 -0.0378 0.0421 1.0000
16.500 1.2367 0.09965 0.09193 -0.0380 0.0402 1.0000
16.750 1.2424 0.10229 0.09471 -0.0384 0.0385 1.0000
17.000 1.2468 0.10516 0.09766 -0.0390 0.0370 1.0000
17.250 1.2515 0.10791 0.10043 -0.0397 0.0356 1.0000
17.500 1.2592 0.11016 0.10276 -0.0399 0.0345 1.0000
17.750 1.2623 0.11343 0.10627 -0.0407 0.0334 1.0000
18.000 1.2636 0.11700 0.11004 -0.0418 0.0324 1.0000
18.250 1.2634 0.12084 0.11406 -0.0433 0.0313 1.0000
18.500 1.2641 0.12451 0.11787 -0.0448 0.0305 1.0000
18.750 1.2650 0.12809 0.12152 -0.0464 0.0296 1.0000
19.000 1.2692 0.13101 0.12447 -0.0476 0.0288 1.0000
19.250 1.2649 0.13579 0.12945 -0.0499 0.0283 1.0000
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