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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 200,000
Max Cl/Cd: 69.58 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w160-il-200000-n5.txt
Download as CSV file: xf-fx83w160-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6953   0.09438   0.08976  -0.0797   1.0000   0.0306
 -15.750  -0.7310   0.08543   0.08063  -0.0839   1.0000   0.0306
 -15.500  -0.7575   0.07874   0.07379  -0.0866   1.0000   0.0308
 -15.250  -0.7781   0.07359   0.06851  -0.0880   1.0000   0.0309
 -15.000  -0.7982   0.06897   0.06376  -0.0890   1.0000   0.0312
 -14.750  -0.8048   0.06360   0.05818  -0.0935   0.9983   0.0317
 -14.500  -0.8066   0.05871   0.05305  -0.0982   0.9955   0.0323
 -14.250  -0.8021   0.05516   0.04940  -0.1015   0.9925   0.0328
 -14.000  -0.7944   0.05218   0.04636  -0.1046   0.9894   0.0333
 -13.750  -0.7852   0.04925   0.04334  -0.1078   0.9866   0.0340
 -13.500  -0.7774   0.04653   0.04052  -0.1104   0.9824   0.0347
 -13.250  -0.7672   0.04389   0.03776  -0.1132   0.9785   0.0356
 -13.000  -0.7544   0.04143   0.03514  -0.1159   0.9753   0.0364
 -12.750  -0.7458   0.03928   0.03281  -0.1173   0.9694   0.0374
 -12.500  -0.7305   0.03721   0.03070  -0.1198   0.9660   0.0383
 -12.250  -0.7194   0.03543   0.02886  -0.1211   0.9603   0.0392
 -12.000  -0.7040   0.03369   0.02704  -0.1229   0.9554   0.0405
 -11.750  -0.6838   0.03197   0.02519  -0.1253   0.9525   0.0419
 -11.500  -0.6747   0.03061   0.02371  -0.1251   0.9451   0.0430
 -11.250  -0.6583   0.02907   0.02213  -0.1265   0.9407   0.0442
 -11.000  -0.6367   0.02768   0.02067  -0.1287   0.9378   0.0460
 -10.750  -0.6326   0.02677   0.01967  -0.1268   0.9285   0.0475
 -10.500  -0.6080   0.02570   0.01846  -0.1281   0.9252   0.0496
 -10.250  -0.5810   0.02457   0.01731  -0.1301   0.9230   0.0518
 -10.000  -0.5726   0.02396   0.01664  -0.1278   0.9151   0.0537
  -9.750  -0.5481   0.02320   0.01577  -0.1285   0.9115   0.0565
  -9.500  -0.5208   0.02234   0.01489  -0.1299   0.9090   0.0594
  -9.250  -0.4904   0.02162   0.01409  -0.1315   0.9070   0.0632
  -9.000  -0.4795   0.02118   0.01358  -0.1291   0.8995   0.0659
  -8.750  -0.4551   0.02052   0.01292  -0.1295   0.8956   0.0698
  -8.500  -0.4254   0.01996   0.01225  -0.1306   0.8930   0.0746
  -8.250  -0.3954   0.01929   0.01159  -0.1320   0.8909   0.0798
  -8.000  -0.3789   0.01897   0.01121  -0.1303   0.8851   0.0844
  -7.750  -0.3568   0.01849   0.01074  -0.1299   0.8804   0.0899
  -7.250  -0.2970   0.01752   0.00971  -0.1319   0.8749   0.1041
  -7.000  -0.2685   0.01712   0.00926  -0.1325   0.8721   0.1117
  -6.750  -0.2531   0.01686   0.00901  -0.1306   0.8659   0.1184
  -6.500  -0.2262   0.01649   0.00861  -0.1308   0.8622   0.1266
  -6.250  -0.1960   0.01610   0.00820  -0.1317   0.8594   0.1371
  -6.000  -0.1644   0.01567   0.00777  -0.1329   0.8571   0.1488
  -5.750  -0.1436   0.01542   0.00754  -0.1319   0.8526   0.1602
  -5.500  -0.1216   0.01516   0.00731  -0.1311   0.8480   0.1742
  -5.250  -0.0944   0.01480   0.00700  -0.1314   0.8447   0.1939
  -5.000  -0.0642   0.01442   0.00668  -0.1323   0.8420   0.2194
  -4.750  -0.0325   0.01401   0.00636  -0.1335   0.8397   0.2492
  -4.500  -0.0136   0.01380   0.00626  -0.1320   0.8347   0.2787
  -4.250   0.0099   0.01357   0.00614  -0.1315   0.8305   0.3113
  -4.000   0.0379   0.01335   0.00599  -0.1317   0.8274   0.3449
  -3.750   0.0681   0.01313   0.00588  -0.1324   0.8248   0.3797
  -3.500   0.1003   0.01298   0.00578  -0.1333   0.8226   0.4130
  -3.250   0.1209   0.01300   0.00589  -0.1319   0.8178   0.4379
  -3.000   0.1452   0.01303   0.00593  -0.1312   0.8135   0.4595
  -2.750   0.1741   0.01302   0.00592  -0.1314   0.8102   0.4768
  -2.500   0.2054   0.01301   0.00589  -0.1320   0.8075   0.4913
  -2.250   0.2387   0.01300   0.00584  -0.1331   0.8052   0.5045
  -2.000   0.2588   0.01313   0.00593  -0.1315   0.8003   0.5164
  -1.750   0.2832   0.01321   0.00603  -0.1308   0.7962   0.5269
  -1.500   0.3118   0.01325   0.00604  -0.1309   0.7930   0.5380
  -1.250   0.3425   0.01329   0.00606  -0.1314   0.7905   0.5494
  -1.000   0.3746   0.01330   0.00607  -0.1322   0.7883   0.5583
  -0.750   0.3962   0.01343   0.00621  -0.1310   0.7842   0.5664
  -0.500   0.4189   0.01352   0.00630  -0.1300   0.7798   0.5731
  -0.250   0.4466   0.01354   0.00634  -0.1299   0.7763   0.5785
   0.000   0.4772   0.01355   0.00632  -0.1304   0.7735   0.5848
   0.250   0.5096   0.01355   0.00629  -0.1314   0.7714   0.5909
   0.500   0.5309   0.01366   0.00646  -0.1301   0.7671   0.5959
   0.750   0.5528   0.01374   0.00656  -0.1289   0.7621   0.6010
   1.000   0.5819   0.01374   0.00653  -0.1291   0.7581   0.6061
   1.250   0.6137   0.01371   0.00652  -0.1298   0.7552   0.6105
   1.500   0.6419   0.01375   0.00660  -0.1299   0.7521   0.6151
   1.750   0.6593   0.01391   0.00681  -0.1279   0.7466   0.6204
   2.000   0.6860   0.01394   0.00684  -0.1276   0.7419   0.6260
   2.250   0.7181   0.01387   0.00681  -0.1283   0.7380   0.6307
   2.500   0.7394   0.01393   0.00693  -0.1270   0.7318   0.6355
   2.750   0.7622   0.01395   0.00697  -0.1259   0.7249   0.6401
   3.000   0.7966   0.01380   0.00679  -0.1270   0.7186   0.6445
   3.250   0.8096   0.01379   0.00686  -0.1238   0.7067   0.6485
   3.500   0.8301   0.01372   0.00680  -0.1221   0.6947   0.6534
   3.750   0.8570   0.01363   0.00669  -0.1216   0.6839   0.6587
   4.000   0.8730   0.01369   0.00680  -0.1192   0.6735   0.6635
   4.250   0.8943   0.01370   0.00685  -0.1177   0.6638   0.6684
   4.500   0.9144   0.01374   0.00693  -0.1161   0.6537   0.6741
   4.750   0.9312   0.01385   0.00709  -0.1138   0.6430   0.6802
   5.000   0.9510   0.01391   0.00720  -0.1121   0.6311   0.6857
   5.250   0.9689   0.01402   0.00732  -0.1100   0.6158   0.6918
   5.750   0.9991   0.01436   0.00766  -0.1049   0.5747   0.7046
   6.000   1.0130   0.01461   0.00783  -0.1021   0.5465   0.7126
   6.250   1.0233   0.01497   0.00810  -0.0988   0.5137   0.7209
   6.500   1.0287   0.01553   0.00849  -0.0947   0.4744   0.7309
   6.750   1.0310   0.01625   0.00904  -0.0903   0.4342   0.7418
   7.000   1.0320   0.01712   0.00974  -0.0859   0.3968   0.7547
   7.500   1.0387   0.01892   0.01133  -0.0784   0.3297   0.7910
   7.750   1.0435   0.01984   0.01220  -0.0751   0.2986   0.8221
   8.000   1.0550   0.02075   0.01315  -0.0735   0.2673   0.9159
   8.500   1.0674   0.02276   0.01489  -0.0681   0.2209   1.0000
   8.750   1.0779   0.02376   0.01580  -0.0662   0.2037   1.0000
   9.000   1.0888   0.02475   0.01672  -0.0643   0.1889   1.0000
   9.250   1.1001   0.02576   0.01766  -0.0626   0.1766   1.0000
   9.500   1.1129   0.02669   0.01857  -0.0611   0.1655   1.0000
   9.750   1.1252   0.02767   0.01953  -0.0596   0.1566   1.0000
  10.000   1.1374   0.02868   0.02052  -0.0581   0.1480   1.0000
  10.250   1.1502   0.02967   0.02151  -0.0567   0.1402   1.0000
  10.500   1.1620   0.03075   0.02257  -0.0553   0.1325   1.0000
  10.750   1.1747   0.03178   0.02362  -0.0540   0.1256   1.0000
  11.000   1.1863   0.03291   0.02474  -0.0527   0.1189   1.0000
  11.250   1.1983   0.03402   0.02587  -0.0515   0.1126   1.0000
  11.500   1.2101   0.03519   0.02704  -0.0502   0.1063   1.0000
  11.750   1.2211   0.03643   0.02829  -0.0490   0.1010   1.0000
  12.000   1.2334   0.03759   0.02949  -0.0479   0.0956   1.0000
  12.250   1.2425   0.03901   0.03090  -0.0467   0.0909   1.0000
  12.500   1.2552   0.04019   0.03215  -0.0457   0.0865   1.0000
  12.750   1.2650   0.04161   0.03359  -0.0447   0.0821   1.0000
  13.000   1.2744   0.04310   0.03510  -0.0436   0.0787   1.0000
  13.250   1.2853   0.04449   0.03658  -0.0427   0.0749   1.0000
  13.500   1.2937   0.04611   0.03822  -0.0417   0.0717   1.0000
  13.750   1.3016   0.04780   0.03995  -0.0408   0.0688   1.0000
  14.000   1.3112   0.04938   0.04162  -0.0399   0.0657   1.0000
  14.250   1.3189   0.05117   0.04345  -0.0391   0.0629   1.0000
  14.500   1.3243   0.05321   0.04552  -0.0383   0.0607   1.0000
  14.750   1.3333   0.05494   0.04737  -0.0377   0.0581   1.0000
  15.000   1.3401   0.05691   0.04941  -0.0371   0.0557   1.0000
  15.250   1.3449   0.05912   0.05167  -0.0365   0.0538   1.0000
  15.500   1.3497   0.06139   0.05400  -0.0360   0.0520   1.0000
  15.750   1.3555   0.06358   0.05632  -0.0356   0.0501   1.0000
  16.000   1.3601   0.06596   0.05878  -0.0353   0.0482   1.0000
  16.250   1.3620   0.06868   0.06155  -0.0351   0.0467   1.0000
  16.500   1.3636   0.07149   0.06442  -0.0350   0.0454   1.0000
  16.750   1.3673   0.07411   0.06718  -0.0350   0.0440   1.0000
  17.000   1.3693   0.07699   0.07017  -0.0351   0.0425   1.0000
  17.250   1.3701   0.08009   0.07337  -0.0354   0.0413   1.0000
  17.500   1.3690   0.08349   0.07683  -0.0358   0.0402   1.0000
  17.750   1.3678   0.08695   0.08038  -0.0364   0.0392   1.0000
  18.000   1.3681   0.09029   0.08387  -0.0370   0.0381   1.0000
  18.250   1.3670   0.09387   0.08758  -0.0378   0.0370   1.0000
  18.500   1.3650   0.09765   0.09147  -0.0389   0.0361   1.0000
  18.750   1.3622   0.10162   0.09554  -0.0402   0.0353   1.0000
  19.000   1.3579   0.10586   0.09985  -0.0417   0.0345   1.0000
  19.250   1.3543   0.11003   0.10413  -0.0432   0.0338   1.0000
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