FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 83-W-160 (fx83w160-il) Reynolds number: 500,000 Max Cl/Cd: 96.44 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx83w160-il-500000-n5.txt Download as CSV file: xf-fx83w160-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-160
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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.7400 0.12437 0.12099 -0.0670 1.0000 0.0187
-18.750 -0.7570 0.11794 0.11448 -0.0699 1.0000 0.0189
-18.500 -0.7743 0.11157 0.10802 -0.0728 1.0000 0.0191
-18.250 -0.7911 0.10544 0.10180 -0.0755 1.0000 0.0193
-18.000 -0.8084 0.09947 0.09574 -0.0780 1.0000 0.0194
-17.750 -0.8245 0.09384 0.09003 -0.0803 1.0000 0.0195
-17.500 -0.8417 0.08823 0.08433 -0.0825 1.0000 0.0196
-17.250 -0.8582 0.08291 0.07891 -0.0845 1.0000 0.0198
-17.000 -0.8730 0.07786 0.07376 -0.0864 1.0000 0.0200
-16.750 -0.8776 0.07240 0.06816 -0.0908 0.9992 0.0202
-16.500 -0.8825 0.06695 0.06261 -0.0953 0.9981 0.0205
-16.250 -0.8850 0.06196 0.05753 -0.0995 0.9966 0.0208
-16.000 -0.8864 0.05727 0.05274 -0.1036 0.9946 0.0209
-15.750 -0.8858 0.05321 0.04859 -0.1071 0.9925 0.0212
-15.500 -0.8828 0.04954 0.04484 -0.1104 0.9901 0.0216
-15.250 -0.8773 0.04619 0.04140 -0.1137 0.9879 0.0219
-15.000 -0.8687 0.04320 0.03830 -0.1169 0.9861 0.0224
-14.750 -0.8636 0.04051 0.03553 -0.1188 0.9820 0.0227
-14.500 -0.8528 0.03810 0.03302 -0.1213 0.9789 0.0232
-14.000 -0.8298 0.03371 0.02844 -0.1255 0.9713 0.0239
-13.750 -0.8180 0.03142 0.02610 -0.1279 0.9674 0.0246
-13.500 -0.8003 0.02949 0.02412 -0.1306 0.9649 0.0253
-13.250 -0.7878 0.02785 0.02241 -0.1318 0.9585 0.0259
-13.000 -0.7668 0.02629 0.02078 -0.1342 0.9547 0.0267
-12.750 -0.7412 0.02478 0.01917 -0.1374 0.9521 0.0275
-12.500 -0.7239 0.02341 0.01773 -0.1389 0.9452 0.0282
-12.250 -0.6974 0.02203 0.01630 -0.1421 0.9412 0.0293
-12.000 -0.6662 0.02083 0.01503 -0.1457 0.9382 0.0305
-11.750 -0.6468 0.01985 0.01397 -0.1467 0.9306 0.0317
-11.500 -0.6222 0.01887 0.01290 -0.1486 0.9248 0.0328
-11.250 -0.6039 0.01809 0.01207 -0.1488 0.9180 0.0341
-11.000 -0.5827 0.01745 0.01137 -0.1490 0.9117 0.0355
-10.750 -0.5558 0.01690 0.01073 -0.1500 0.9072 0.0372
-10.500 -0.5388 0.01637 0.01015 -0.1490 0.9006 0.0384
-10.250 -0.5171 0.01586 0.00960 -0.1488 0.8949 0.0403
-10.000 -0.4910 0.01541 0.00907 -0.1493 0.8903 0.0425
-9.750 -0.4727 0.01501 0.00864 -0.1482 0.8840 0.0443
-9.500 -0.4505 0.01460 0.00821 -0.1478 0.8785 0.0469
-9.250 -0.4249 0.01425 0.00779 -0.1480 0.8741 0.0495
-9.000 -0.4037 0.01389 0.00742 -0.1472 0.8692 0.0523
-8.750 -0.3810 0.01359 0.00708 -0.1467 0.8640 0.0557
-8.500 -0.3563 0.01327 0.00673 -0.1466 0.8594 0.0591
-8.250 -0.3309 0.01298 0.00641 -0.1465 0.8552 0.0632
-8.000 -0.3083 0.01272 0.00613 -0.1458 0.8503 0.0670
-7.750 -0.2841 0.01244 0.00584 -0.1455 0.8458 0.0717
-7.500 -0.2581 0.01220 0.00555 -0.1454 0.8416 0.0762
-7.250 -0.2328 0.01194 0.00529 -0.1453 0.8376 0.0818
-7.000 -0.2088 0.01171 0.00506 -0.1448 0.8331 0.0875
-6.750 -0.1837 0.01148 0.00483 -0.1445 0.8289 0.0947
-6.500 -0.1575 0.01125 0.00460 -0.1445 0.8252 0.1022
-6.250 -0.1301 0.01107 0.00439 -0.1446 0.8219 0.1093
-6.000 -0.1058 0.01085 0.00420 -0.1441 0.8179 0.1175
-5.750 -0.0802 0.01068 0.00402 -0.1439 0.8137 0.1249
-5.500 -0.0540 0.01048 0.00383 -0.1437 0.8097 0.1346
-5.250 -0.0269 0.01029 0.00365 -0.1438 0.8062 0.1461
-5.000 -0.0006 0.01011 0.00349 -0.1437 0.8029 0.1577
-4.750 0.0249 0.00992 0.00334 -0.1434 0.7992 0.1724
-4.500 0.0506 0.00969 0.00319 -0.1432 0.7954 0.1936
-4.250 0.0771 0.00947 0.00303 -0.1431 0.7919 0.2191
-4.000 0.1042 0.00925 0.00287 -0.1432 0.7885 0.2468
-3.750 0.1298 0.00904 0.00276 -0.1430 0.7847 0.2771
-3.500 0.1554 0.00885 0.00266 -0.1427 0.7804 0.3059
-3.250 0.1819 0.00869 0.00256 -0.1425 0.7764 0.3329
-3.000 0.2093 0.00857 0.00248 -0.1425 0.7729 0.3579
-2.750 0.2368 0.00845 0.00243 -0.1426 0.7698 0.3863
-2.500 0.2628 0.00834 0.00242 -0.1423 0.7664 0.4163
-2.250 0.2894 0.00828 0.00243 -0.1421 0.7630 0.4400
-2.000 0.3169 0.00825 0.00242 -0.1420 0.7596 0.4560
-1.750 0.3449 0.00825 0.00242 -0.1420 0.7566 0.4696
-1.500 0.3736 0.00826 0.00242 -0.1422 0.7538 0.4814
-1.250 0.4003 0.00827 0.00246 -0.1419 0.7505 0.4919
-1.000 0.4270 0.00828 0.00250 -0.1417 0.7468 0.5036
-0.750 0.4543 0.00832 0.00254 -0.1415 0.7431 0.5151
-0.500 0.4820 0.00835 0.00257 -0.1415 0.7396 0.5241
0.000 0.5368 0.00843 0.00264 -0.1412 0.7326 0.5381
0.250 0.5632 0.00845 0.00269 -0.1409 0.7288 0.5438
0.500 0.5903 0.00848 0.00272 -0.1407 0.7250 0.5483
1.000 0.6441 0.00855 0.00279 -0.1402 0.7164 0.5574
1.250 0.6688 0.00858 0.00284 -0.1395 0.7102 0.5621
1.500 0.6949 0.00862 0.00287 -0.1391 0.7045 0.5660
1.750 0.7200 0.00867 0.00290 -0.1384 0.6983 0.5693
2.000 0.7425 0.00870 0.00292 -0.1372 0.6878 0.5726
2.250 0.7633 0.00874 0.00295 -0.1356 0.6749 0.5763
2.500 0.7839 0.00881 0.00299 -0.1340 0.6614 0.5803
2.750 0.8055 0.00890 0.00305 -0.1326 0.6505 0.5845
3.000 0.8280 0.00897 0.00312 -0.1315 0.6407 0.5886
3.250 0.8496 0.00904 0.00320 -0.1301 0.6324 0.5921
3.500 0.8694 0.00911 0.00329 -0.1284 0.6215 0.5955
3.750 0.8882 0.00921 0.00338 -0.1265 0.6090 0.5988
4.000 0.9033 0.00938 0.00349 -0.1238 0.5897 0.6021
4.250 0.9156 0.00963 0.00366 -0.1206 0.5664 0.6057
4.500 0.9283 0.00992 0.00387 -0.1175 0.5421 0.6091
4.750 0.9371 0.01032 0.00415 -0.1137 0.5105 0.6127
5.000 0.9405 0.01089 0.00454 -0.1090 0.4706 0.6163
5.250 0.9466 0.01147 0.00496 -0.1050 0.4340 0.6207
5.500 0.9522 0.01212 0.00544 -0.1009 0.3983 0.6251
5.750 0.9591 0.01276 0.00595 -0.0973 0.3633 0.6294
6.000 0.9682 0.01337 0.00645 -0.0941 0.3345 0.6339
6.250 0.9776 0.01402 0.00698 -0.0911 0.3045 0.6386
6.500 0.9859 0.01474 0.00755 -0.0879 0.2756 0.6432
6.750 0.9957 0.01542 0.00814 -0.0851 0.2466 0.6480
7.000 1.0055 0.01614 0.00874 -0.0824 0.2215 0.6537
7.250 1.0173 0.01680 0.00933 -0.0801 0.2006 0.6599
7.500 1.0305 0.01741 0.00990 -0.0780 0.1851 0.6664
7.750 1.0444 0.01800 0.01047 -0.0760 0.1725 0.6746
8.000 1.0584 0.01859 0.01106 -0.0741 0.1618 0.6833
8.250 1.0738 0.01913 0.01162 -0.0724 0.1529 0.6935
8.500 1.0875 0.01976 0.01226 -0.0706 0.1444 0.7047
8.750 1.1028 0.02032 0.01287 -0.0689 0.1364 0.7183
9.250 1.1307 0.02155 0.01419 -0.0654 0.1217 0.7569
9.500 1.1436 0.02218 0.01491 -0.0635 0.1144 0.7902
9.750 1.1609 0.02270 0.01567 -0.0625 0.1072 0.8816
10.000 1.1901 0.02347 0.01649 -0.0644 0.0994 1.0000
10.250 1.2049 0.02425 0.01726 -0.0630 0.0938 1.0000
10.500 1.2192 0.02507 0.01807 -0.0617 0.0887 1.0000
10.750 1.2339 0.02589 0.01889 -0.0604 0.0840 1.0000
11.000 1.2474 0.02679 0.01977 -0.0591 0.0794 1.0000
11.250 1.2616 0.02765 0.02065 -0.0578 0.0755 1.0000
11.500 1.2749 0.02860 0.02160 -0.0565 0.0716 1.0000
11.750 1.2882 0.02957 0.02258 -0.0553 0.0682 1.0000
12.000 1.3016 0.03054 0.02357 -0.0541 0.0644 1.0000
12.250 1.3137 0.03162 0.02465 -0.0528 0.0612 1.0000
12.500 1.3268 0.03264 0.02570 -0.0517 0.0585 1.0000
12.750 1.3391 0.03374 0.02682 -0.0506 0.0552 1.0000
13.000 1.3503 0.03495 0.02804 -0.0494 0.0524 1.0000
13.250 1.3625 0.03610 0.02923 -0.0483 0.0503 1.0000
13.500 1.3734 0.03737 0.03051 -0.0472 0.0476 1.0000
13.750 1.3832 0.03874 0.03191 -0.0461 0.0456 1.0000
14.000 1.3945 0.04002 0.03323 -0.0451 0.0437 1.0000
14.250 1.4042 0.04146 0.03471 -0.0441 0.0418 1.0000
14.500 1.4129 0.04300 0.03627 -0.0431 0.0401 1.0000
14.750 1.4225 0.04450 0.03782 -0.0422 0.0384 1.0000
15.000 1.4318 0.04605 0.03943 -0.0413 0.0366 1.0000
15.250 1.4393 0.04778 0.04119 -0.0405 0.0350 1.0000
15.500 1.4467 0.04955 0.04301 -0.0397 0.0338 1.0000
15.750 1.4549 0.05129 0.04482 -0.0390 0.0325 1.0000
16.000 1.4623 0.05313 0.04672 -0.0383 0.0313 1.0000
16.250 1.4681 0.05517 0.04881 -0.0377 0.0301 1.0000
16.500 1.4730 0.05734 0.05103 -0.0371 0.0292 1.0000
16.750 1.4791 0.05942 0.05320 -0.0366 0.0283 1.0000
17.000 1.4841 0.06165 0.05550 -0.0362 0.0274 1.0000
17.250 1.4880 0.06405 0.05797 -0.0359 0.0266 1.0000
17.500 1.4907 0.06663 0.06061 -0.0357 0.0257 1.0000
17.750 1.4916 0.06950 0.06353 -0.0356 0.0250 1.0000
18.000 1.4947 0.07215 0.06629 -0.0356 0.0243 1.0000
18.250 1.4960 0.07505 0.06928 -0.0357 0.0237 1.0000
18.500 1.4967 0.07808 0.07240 -0.0359 0.0231 1.0000
18.750 1.4964 0.08132 0.07573 -0.0363 0.0226 1.0000
19.000 1.4939 0.08493 0.07942 -0.0369 0.0220 1.0000
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