WORTMANN FX 057-816 (fx057816-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 057-816 (fx057816-il) Reynolds number: 1,000,000 Max Cl/Cd: 152.99 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx057816-il-1000000-n5.txt Download as CSV file: xf-fx057816-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 057-816
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 -0.8607 0.04783 0.04377 -0.0908 0.5731 0.0067
-15.250 -0.9029 0.04106 0.03678 -0.0925 0.5728 0.0066
-15.000 -0.9196 0.03743 0.03298 -0.0918 0.5724 0.0067
-14.750 -0.9303 0.03476 0.03016 -0.0903 0.5718 0.0067
-14.500 -0.9368 0.03261 0.02787 -0.0884 0.5712 0.0068
-14.250 -0.9374 0.03093 0.02606 -0.0864 0.5705 0.0068
-14.000 -0.9378 0.02943 0.02444 -0.0840 0.5702 0.0069
-13.750 -0.9353 0.02826 0.02317 -0.0813 0.5698 0.0069
-13.500 -0.9325 0.02690 0.02168 -0.0788 0.5694 0.0070
-13.250 -0.9231 0.02560 0.02027 -0.0771 0.5690 0.0072
-13.000 -0.9094 0.02453 0.01910 -0.0758 0.5686 0.0073
-12.750 -0.8939 0.02352 0.01798 -0.0746 0.5681 0.0075
-12.500 -0.8764 0.02263 0.01700 -0.0736 0.5675 0.0077
-12.250 -0.8577 0.02181 0.01609 -0.0727 0.5670 0.0078
-12.000 -0.8376 0.02107 0.01527 -0.0720 0.5664 0.0080
-11.750 -0.8168 0.02037 0.01448 -0.0712 0.5658 0.0082
-11.500 -0.7952 0.01971 0.01374 -0.0706 0.5651 0.0084
-11.250 -0.7730 0.01909 0.01304 -0.0701 0.5644 0.0086
-11.000 -0.7500 0.01852 0.01237 -0.0696 0.5637 0.0088
-10.750 -0.7266 0.01798 0.01175 -0.0691 0.5631 0.0090
-10.500 -0.7028 0.01746 0.01116 -0.0687 0.5625 0.0092
-10.250 -0.6794 0.01685 0.01048 -0.0682 0.5619 0.0096
-10.000 -0.6551 0.01633 0.00990 -0.0679 0.5614 0.0099
-9.750 -0.6304 0.01585 0.00937 -0.0676 0.5608 0.0103
-9.500 -0.6052 0.01543 0.00890 -0.0673 0.5603 0.0108
-9.250 -0.5797 0.01506 0.00847 -0.0671 0.5597 0.0113
-9.000 -0.5538 0.01471 0.00807 -0.0669 0.5592 0.0117
-8.750 -0.5280 0.01432 0.00761 -0.0667 0.5586 0.0122
-8.500 -0.5023 0.01392 0.00718 -0.0665 0.5580 0.0130
-8.250 -0.4761 0.01358 0.00680 -0.0663 0.5573 0.0137
-8.000 -0.4497 0.01328 0.00646 -0.0662 0.5567 0.0145
-7.750 -0.4229 0.01301 0.00615 -0.0662 0.5563 0.0152
-7.500 -0.3963 0.01268 0.00580 -0.0661 0.5560 0.0166
-7.250 -0.3696 0.01236 0.00548 -0.0660 0.5556 0.0182
-7.000 -0.3425 0.01210 0.00520 -0.0660 0.5552 0.0198
-6.750 -0.3155 0.01181 0.00492 -0.0660 0.5547 0.0230
-6.500 -0.2882 0.01157 0.00470 -0.0660 0.5542 0.0262
-6.250 -0.2604 0.01141 0.00458 -0.0661 0.5536 0.0322
-6.000 -0.2323 0.01128 0.00446 -0.0662 0.5531 0.0363
-5.750 -0.2041 0.01115 0.00433 -0.0663 0.5526 0.0381
-5.500 -0.1760 0.01102 0.00418 -0.0665 0.5521 0.0401
-5.250 -0.1474 0.01094 0.00412 -0.0667 0.5516 0.0430
-5.000 -0.1187 0.01090 0.00408 -0.0669 0.5511 0.0455
-4.750 -0.0900 0.01084 0.00402 -0.0671 0.5506 0.0476
-4.500 -0.0613 0.01079 0.00395 -0.0673 0.5501 0.0493
-4.250 -0.0325 0.01073 0.00388 -0.0676 0.5496 0.0504
-4.000 -0.0036 0.01073 0.00386 -0.0678 0.5491 0.0513
-3.750 0.0257 0.01076 0.00390 -0.0681 0.5486 0.0518
-3.500 0.0537 0.01058 0.00369 -0.0683 0.5482 0.0530
-3.250 0.0818 0.01037 0.00346 -0.0685 0.5477 0.0542
-3.000 0.1102 0.01022 0.00329 -0.0687 0.5472 0.0552
-2.750 0.1387 0.01010 0.00316 -0.0689 0.5467 0.0561
-2.500 0.1674 0.01000 0.00305 -0.0692 0.5461 0.0569
-2.250 0.1961 0.00990 0.00294 -0.0695 0.5455 0.0576
-2.000 0.2248 0.00983 0.00285 -0.0698 0.5449 0.0583
-1.750 0.2536 0.00976 0.00277 -0.0701 0.5444 0.0591
-1.500 0.2824 0.00970 0.00271 -0.0704 0.5439 0.0601
-1.250 0.3113 0.00966 0.00267 -0.0707 0.5433 0.0610
-1.000 0.3402 0.00963 0.00263 -0.0710 0.5427 0.0622
-0.750 0.3692 0.00959 0.00260 -0.0714 0.5424 0.0636
-0.500 0.3982 0.00955 0.00258 -0.0718 0.5421 0.0650
-0.250 0.4273 0.00953 0.00258 -0.0721 0.5417 0.0660
0.000 0.4564 0.00951 0.00257 -0.0725 0.5414 0.0665
0.250 0.4854 0.00945 0.00254 -0.0729 0.5409 0.0690
0.500 0.5145 0.00942 0.00253 -0.0733 0.5405 0.0713
0.750 0.5435 0.00939 0.00254 -0.0737 0.5399 0.0732
1.000 0.5726 0.00937 0.00255 -0.0742 0.5393 0.0751
1.250 0.6017 0.00936 0.00256 -0.0746 0.5387 0.0769
1.500 0.6308 0.00935 0.00258 -0.0750 0.5381 0.0804
1.750 0.6599 0.00934 0.00261 -0.0755 0.5376 0.0866
2.000 0.6884 0.00885 0.00265 -0.0762 0.5371 0.3004
2.250 0.7174 0.00855 0.00269 -0.0770 0.5365 0.4238
2.500 0.7456 0.00769 0.00283 -0.0778 0.5359 0.7754
2.750 0.7747 0.00774 0.00290 -0.0782 0.5350 0.7908
3.000 0.8041 0.00778 0.00295 -0.0787 0.5339 0.8011
3.250 0.8330 0.00781 0.00302 -0.0790 0.5328 0.8094
3.500 0.8624 0.00787 0.00306 -0.0795 0.5317 0.8157
3.750 0.8910 0.00791 0.00312 -0.0798 0.5303 0.8201
4.000 0.9197 0.00796 0.00320 -0.0801 0.5285 0.8249
4.250 0.9489 0.00800 0.00328 -0.0806 0.5271 0.8273
4.500 0.9781 0.00803 0.00335 -0.0811 0.5257 0.8290
4.750 1.0073 0.00808 0.00342 -0.0816 0.5243 0.8303
5.000 1.0364 0.00812 0.00349 -0.0821 0.5227 0.8321
5.250 1.0648 0.00814 0.00357 -0.0824 0.5211 0.8357
5.500 1.0936 0.00816 0.00362 -0.0828 0.5192 0.8377
5.750 1.1224 0.00817 0.00363 -0.0833 0.5164 0.8385
6.000 1.1512 0.00821 0.00372 -0.0838 0.5139 0.8394
6.250 1.1800 0.00826 0.00383 -0.0843 0.5117 0.8403
6.500 1.2089 0.00830 0.00392 -0.0848 0.5080 0.8411
6.750 1.2374 0.00832 0.00395 -0.0852 0.5036 0.8418
7.000 1.2659 0.00836 0.00404 -0.0857 0.4971 0.8426
7.250 1.2928 0.00845 0.00408 -0.0859 0.4770 0.8434
7.500 1.2978 0.01017 0.00526 -0.0831 0.3745 0.8447
7.750 1.2897 0.01259 0.00722 -0.0787 0.2863 0.8464
8.000 1.2974 0.01373 0.00824 -0.0765 0.2585 0.8475
8.250 1.3024 0.01482 0.00928 -0.0739 0.2382 0.8492
8.500 1.2957 0.01611 0.01056 -0.0696 0.2231 0.8514
8.750 1.2726 0.01980 0.01435 -0.0666 0.2139 0.8549
9.000 1.2509 0.02310 0.01766 -0.0631 0.2039 0.8578
9.250 1.2338 0.02591 0.02044 -0.0599 0.1912 0.8603
9.500 1.2149 0.02884 0.02330 -0.0567 0.1736 0.8625
9.750 1.2029 0.03135 0.02574 -0.0541 0.1544 0.8647
10.000 1.1824 0.03449 0.02874 -0.0511 0.1249 0.8672
10.250 1.1756 0.03688 0.03102 -0.0493 0.1049 0.8693
10.500 1.1797 0.03864 0.03275 -0.0483 0.0949 0.8713
10.750 1.1869 0.04020 0.03428 -0.0475 0.0868 0.8732
11.000 1.1963 0.04162 0.03569 -0.0468 0.0802 0.8751
11.250 1.2049 0.04316 0.03721 -0.0463 0.0732 0.8772
11.750 1.2254 0.04600 0.04007 -0.0453 0.0624 0.8818
12.000 1.2341 0.04755 0.04159 -0.0448 0.0530 0.8846
12.250 1.2329 0.04999 0.04387 -0.0439 0.0303 0.8875
12.500 1.2389 0.05190 0.04576 -0.0434 0.0220 0.8905
12.750 1.2481 0.05354 0.04741 -0.0431 0.0191 0.8937
13.000 1.2583 0.05507 0.04898 -0.0428 0.0166 0.8977
13.250 1.2690 0.05655 0.05050 -0.0425 0.0152 0.9029
13.500 1.2780 0.05822 0.05221 -0.0422 0.0138 0.9091
13.750 1.2861 0.05993 0.05398 -0.0418 0.0128 0.9197
14.000 1.2971 0.06143 0.05561 -0.0417 0.0120 0.9475
15.000 1.3395 0.06877 0.06308 -0.0429 0.0094 1.0000
15.250 1.3492 0.07061 0.06496 -0.0430 0.0089 1.0000
15.500 1.3587 0.07247 0.06685 -0.0431 0.0085 1.0000
15.750 1.3669 0.07453 0.06894 -0.0433 0.0081 1.0000
16.000 1.3739 0.07679 0.07124 -0.0435 0.0077 1.0000
16.250 1.3813 0.07897 0.07346 -0.0437 0.0074 1.0000
16.500 1.3901 0.08101 0.07555 -0.0440 0.0072 1.0000
16.750 1.3972 0.08331 0.07790 -0.0444 0.0070 1.0000
17.000 1.4044 0.08561 0.08025 -0.0448 0.0066 1.0000
17.250 1.4113 0.08795 0.08266 -0.0452 0.0063 1.0000
17.500 1.4172 0.09047 0.08522 -0.0457 0.0061 1.0000
17.750 1.4218 0.09319 0.08799 -0.0463 0.0059 1.0000
18.000 1.4262 0.09594 0.09080 -0.0469 0.0057 1.0000
18.250 1.4299 0.09883 0.09375 -0.0476 0.0056 1.0000
18.500 1.4348 0.10158 0.09657 -0.0483 0.0054 1.0000
18.750 1.4395 0.10437 0.09942 -0.0491 0.0053 1.0000
19.000 1.4427 0.10744 0.10256 -0.0500 0.0052 1.0000
19.250 1.4460 0.11047 0.10566 -0.0509 0.0050 1.0000
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