FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 83-W-227 (fx83w227-il) Reynolds number: 500,000 Max Cl/Cd: 73.16 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx83w227-il-500000.txt Download as CSV file: xf-fx83w227-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-227
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9363 0.07941 0.07506 -0.0969 1.0000 0.0498
-19.500 -0.9428 0.07611 0.07169 -0.0978 1.0000 0.0504
-19.250 -0.9506 0.07270 0.06820 -0.0986 1.0000 0.0511
-19.000 -0.9582 0.06946 0.06485 -0.0992 1.0000 0.0517
-18.750 -0.9662 0.06627 0.06155 -0.0997 1.0000 0.0522
-18.500 -0.9731 0.06342 0.05861 -0.0998 1.0000 0.0529
-18.250 -0.9752 0.06143 0.05664 -0.0991 1.0000 0.0536
-18.000 -0.9791 0.05924 0.05444 -0.0985 1.0000 0.0542
-17.750 -0.9838 0.05705 0.05221 -0.0979 1.0000 0.0548
-17.500 -0.9888 0.05502 0.05015 -0.0970 1.0000 0.0553
-17.250 -0.9800 0.05253 0.04759 -0.0990 0.9990 0.0564
-17.000 -0.9651 0.04999 0.04495 -0.1021 0.9972 0.0575
-16.750 -0.9492 0.04758 0.04241 -0.1051 0.9951 0.0584
-16.500 -0.9324 0.04545 0.04022 -0.1078 0.9934 0.0594
-16.250 -0.9157 0.04349 0.03827 -0.1099 0.9911 0.0606
-16.000 -0.8981 0.04157 0.03632 -0.1123 0.9883 0.0618
-15.750 -0.8784 0.03980 0.03449 -0.1147 0.9858 0.0629
-15.500 -0.8568 0.03808 0.03270 -0.1174 0.9838 0.0643
-15.250 -0.8340 0.03640 0.03089 -0.1204 0.9822 0.0656
-15.000 -0.8173 0.03487 0.02937 -0.1214 0.9782 0.0669
-14.750 -0.7976 0.03338 0.02788 -0.1231 0.9745 0.0682
-14.500 -0.7736 0.03203 0.02649 -0.1254 0.9720 0.0696
-14.250 -0.7476 0.03071 0.02512 -0.1279 0.9702 0.0711
-14.000 -0.7287 0.02953 0.02386 -0.1287 0.9646 0.0724
-13.750 -0.7061 0.02827 0.02255 -0.1302 0.9607 0.0737
-13.500 -0.6826 0.02692 0.02122 -0.1321 0.9580 0.0754
-13.250 -0.6569 0.02579 0.02007 -0.1340 0.9545 0.0771
-13.000 -0.6354 0.02483 0.01906 -0.1349 0.9467 0.0789
-12.750 -0.6021 0.02388 0.01803 -0.1379 0.9432 0.0807
-12.500 -0.5745 0.02279 0.01692 -0.1401 0.9364 0.0828
-12.250 -0.5437 0.02175 0.01588 -0.1429 0.9296 0.0851
-12.000 -0.5096 0.02097 0.01504 -0.1458 0.9224 0.0879
-11.750 -0.4771 0.02028 0.01425 -0.1482 0.9124 0.0901
-11.500 -0.4540 0.01938 0.01332 -0.1493 0.9000 0.0927
-11.250 -0.4297 0.01870 0.01258 -0.1503 0.8882 0.0954
-11.000 -0.4075 0.01820 0.01199 -0.1505 0.8761 0.0983
-10.750 -0.3893 0.01782 0.01150 -0.1497 0.8639 0.1006
-10.500 -0.3777 0.01715 0.01080 -0.1481 0.8527 0.1040
-10.250 -0.3644 0.01672 0.01032 -0.1464 0.8419 0.1067
-10.000 -0.3485 0.01640 0.00991 -0.1450 0.8328 0.1099
-9.750 -0.3361 0.01600 0.00944 -0.1430 0.8234 0.1130
-9.500 -0.3250 0.01556 0.00898 -0.1408 0.8149 0.1168
-9.250 -0.3117 0.01526 0.00864 -0.1387 0.8066 0.1207
-9.000 -0.2952 0.01499 0.00827 -0.1372 0.7992 0.1247
-8.750 -0.2871 0.01459 0.00790 -0.1342 0.7915 0.1290
-8.500 -0.2728 0.01432 0.00759 -0.1322 0.7842 0.1337
-8.250 -0.2579 0.01408 0.00729 -0.1302 0.7775 0.1386
-8.000 -0.2479 0.01375 0.00699 -0.1273 0.7704 0.1440
-7.750 -0.2314 0.01356 0.00674 -0.1255 0.7639 0.1499
-7.500 -0.2202 0.01326 0.00644 -0.1227 0.7576 0.1563
-7.250 -0.2075 0.01303 0.00622 -0.1201 0.7509 0.1632
-7.000 -0.1940 0.01280 0.00596 -0.1176 0.7449 0.1705
-6.750 -0.1805 0.01260 0.00576 -0.1151 0.7391 0.1794
-6.500 -0.1704 0.01238 0.00558 -0.1119 0.7329 0.1884
-6.250 -0.1571 0.01224 0.00541 -0.1092 0.7271 0.1988
-6.000 -0.1453 0.01207 0.00526 -0.1062 0.7217 0.2114
-5.750 -0.1353 0.01189 0.00514 -0.1028 0.7159 0.2248
-5.500 -0.1219 0.01169 0.00499 -0.1002 0.7103 0.2418
-5.250 -0.1060 0.01150 0.00482 -0.0980 0.7051 0.2616
-5.000 -0.0919 0.01130 0.00470 -0.0955 0.6998 0.2831
-4.750 -0.0777 0.01110 0.00458 -0.0929 0.6943 0.3064
-4.500 -0.0625 0.01089 0.00444 -0.0906 0.6893 0.3319
-4.250 -0.0441 0.01073 0.00431 -0.0889 0.6843 0.3596
-3.750 -0.0148 0.01034 0.00413 -0.0838 0.6740 0.4119
-3.500 0.0031 0.01019 0.00404 -0.0819 0.6693 0.4399
-3.250 0.0225 0.01008 0.00397 -0.0803 0.6646 0.4671
-3.000 0.0380 0.00994 0.00394 -0.0778 0.6596 0.4932
-2.750 0.0560 0.00985 0.00390 -0.0758 0.6544 0.5176
-2.500 0.0772 0.00980 0.00386 -0.0745 0.6498 0.5394
-2.250 0.0990 0.00978 0.00386 -0.0733 0.6452 0.5584
-2.000 0.1173 0.00973 0.00386 -0.0713 0.6403 0.5743
-1.750 0.1373 0.00971 0.00386 -0.0697 0.6353 0.5893
-1.500 0.1604 0.00973 0.00383 -0.0688 0.6305 0.6033
-1.250 0.1826 0.00975 0.00386 -0.0677 0.6259 0.6159
-1.000 0.2016 0.00973 0.00388 -0.0658 0.6211 0.6270
-0.750 0.2218 0.00975 0.00387 -0.0643 0.6161 0.6383
-0.500 0.2454 0.00978 0.00388 -0.0634 0.6112 0.6484
-0.250 0.2660 0.00982 0.00391 -0.0620 0.6066 0.6588
0.000 0.2829 0.00980 0.00393 -0.0597 0.6018 0.6677
0.250 0.3009 0.00982 0.00394 -0.0577 0.5968 0.6783
0.500 0.3247 0.00988 0.00397 -0.0569 0.5919 0.6881
0.750 0.3414 0.00991 0.00402 -0.0546 0.5871 0.6976
1.000 0.3584 0.00992 0.00405 -0.0524 0.5822 0.7061
1.250 0.3784 0.00997 0.00410 -0.0509 0.5773 0.7146
1.500 0.4028 0.01009 0.00413 -0.0503 0.5722 0.7231
1.750 0.4183 0.01010 0.00423 -0.0478 0.5674 0.7305
2.000 0.4360 0.01017 0.00431 -0.0458 0.5623 0.7384
2.250 0.4566 0.01025 0.00436 -0.0445 0.5574 0.7459
2.500 0.4789 0.01035 0.00445 -0.0435 0.5525 0.7533
2.750 0.4950 0.01042 0.00456 -0.0412 0.5476 0.7614
3.000 0.5130 0.01049 0.00464 -0.0394 0.5421 0.7687
3.250 0.5340 0.01059 0.00472 -0.0382 0.5372 0.7766
3.750 0.5699 0.01076 0.00496 -0.0346 0.5275 0.7936
4.000 0.5873 0.01087 0.00506 -0.0327 0.5223 0.8031
4.250 0.6095 0.01099 0.00515 -0.0317 0.5171 0.8116
4.500 0.6242 0.01108 0.00531 -0.0294 0.5123 0.8219
4.750 0.6417 0.01117 0.00546 -0.0276 0.5073 0.8322
5.000 0.6600 0.01130 0.00558 -0.0259 0.5024 0.8438
5.250 0.6808 0.01142 0.00573 -0.0249 0.4975 0.8557
5.500 0.6993 0.01153 0.00595 -0.0234 0.4926 0.8711
5.750 0.7231 0.01167 0.00616 -0.0230 0.4874 0.8890
6.000 0.7588 0.01191 0.00640 -0.0251 0.4821 0.9076
6.250 0.8024 0.01220 0.00677 -0.0291 0.4770 0.9254
6.500 0.8480 0.01252 0.00714 -0.0335 0.4713 0.9401
6.750 0.8924 0.01289 0.00746 -0.0376 0.4655 0.9514
7.000 0.9342 0.01324 0.00782 -0.0413 0.4605 0.9598
7.250 0.9692 0.01360 0.00822 -0.0435 0.4553 0.9710
7.500 1.0023 0.01400 0.00860 -0.0453 0.4500 0.9817
7.750 1.0401 0.01440 0.00894 -0.0481 0.4445 0.9874
8.000 1.0756 0.01481 0.00940 -0.0506 0.4398 0.9946
8.250 1.1143 0.01523 0.00984 -0.0538 0.4343 0.9992
8.500 1.1280 0.01556 0.01010 -0.0519 0.4296 1.0000
8.750 1.1366 0.01584 0.01038 -0.0490 0.4255 1.0000
9.000 1.1448 0.01616 0.01073 -0.0460 0.4215 1.0000
9.250 1.1540 0.01653 0.01111 -0.0433 0.4169 1.0000
9.500 1.1654 0.01692 0.01146 -0.0410 0.4125 1.0000
9.750 1.1787 0.01732 0.01184 -0.0391 0.4082 1.0000
10.000 1.1887 0.01778 0.01236 -0.0367 0.4040 1.0000
10.250 1.1992 0.01828 0.01287 -0.0345 0.3991 1.0000
10.500 1.2113 0.01878 0.01334 -0.0325 0.3945 1.0000
10.750 1.2246 0.01929 0.01385 -0.0308 0.3900 1.0000
11.000 1.2346 0.01991 0.01454 -0.0288 0.3853 1.0000
11.250 1.2464 0.02051 0.01515 -0.0271 0.3807 1.0000
11.500 1.2586 0.02114 0.01573 -0.0254 0.3758 1.0000
11.750 1.2701 0.02182 0.01646 -0.0238 0.3713 1.0000
12.000 1.2793 0.02263 0.01732 -0.0220 0.3659 1.0000
12.250 1.2881 0.02349 0.01815 -0.0202 0.3600 1.0000
12.500 1.2955 0.02448 0.01917 -0.0183 0.3534 1.0000
12.750 1.3035 0.02550 0.02022 -0.0167 0.3468 1.0000
13.000 1.3115 0.02653 0.02121 -0.0150 0.3412 1.0000
13.250 1.3227 0.02744 0.02219 -0.0138 0.3366 1.0000
13.500 1.3312 0.02855 0.02334 -0.0125 0.3308 1.0000
13.750 1.3398 0.02965 0.02443 -0.0111 0.3257 1.0000
14.000 1.3483 0.03081 0.02562 -0.0099 0.3206 1.0000
14.250 1.3574 0.03199 0.02686 -0.0088 0.3149 1.0000
14.500 1.3632 0.03338 0.02825 -0.0074 0.3092 1.0000
14.750 1.3709 0.03467 0.02957 -0.0063 0.3040 1.0000
15.000 1.3779 0.03611 0.03106 -0.0053 0.2980 1.0000
15.250 1.3814 0.03776 0.03270 -0.0040 0.2915 1.0000
15.500 1.3870 0.03936 0.03435 -0.0030 0.2855 1.0000
15.750 1.3922 0.04099 0.03603 -0.0021 0.2792 1.0000
16.000 1.3927 0.04299 0.03800 -0.0009 0.2726 1.0000
16.250 1.3968 0.04483 0.03991 -0.0001 0.2653 1.0000
16.500 1.3955 0.04708 0.04214 0.0010 0.2579 1.0000
16.750 1.3976 0.04915 0.04427 0.0018 0.2504 1.0000
17.000 1.3924 0.05184 0.04693 0.0028 0.2417 1.0000
17.250 1.3929 0.05412 0.04926 0.0035 0.2333 1.0000
17.500 1.3863 0.05707 0.05219 0.0044 0.2250 1.0000
17.750 1.3835 0.05972 0.05488 0.0050 0.2155 1.0000
18.000 1.3761 0.06287 0.05801 0.0057 0.2061 1.0000
18.250 1.3655 0.06637 0.06150 0.0063 0.1965 1.0000
18.500 1.3572 0.06974 0.06487 0.0067 0.1858 1.0000
18.750 1.3490 0.07314 0.06827 0.0071 0.1769 1.0000
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