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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 50,000
Max Cl/Cd: 24.51 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w160-il-50000-n5.txt
Download as CSV file: xf-fx83w160-il-50000-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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.5100   0.10677   0.09930  -0.0578   1.0000   0.0848
 -11.250  -0.5535   0.09649   0.08909  -0.0615   1.0000   0.0849
 -11.000  -0.6009   0.08739   0.08000  -0.0645   1.0000   0.0846
 -10.750  -0.6495   0.08005   0.07264  -0.0662   1.0000   0.0842
 -10.500  -0.6909   0.07486   0.06742  -0.0661   1.0000   0.0836
 -10.250  -0.7327   0.07040   0.06288  -0.0655   0.9991   0.0832
 -10.000  -0.7612   0.06447   0.05660  -0.0693   0.9915   0.0837
  -9.750  -0.7753   0.05919   0.05080  -0.0719   0.9848   0.0852
  -9.500  -0.7571   0.05796   0.04964  -0.0722   0.9805   0.0878
  -9.250  -0.7446   0.05541   0.04685  -0.0737   0.9759   0.0908
  -9.000  -0.7388   0.05247   0.04353  -0.0741   0.9702   0.0940
  -8.750  -0.7246   0.04977   0.04045  -0.0753   0.9658   0.0979
  -8.500  -0.7067   0.04850   0.03917  -0.0752   0.9616   0.1017
  -8.250  -0.6903   0.04662   0.03698  -0.0755   0.9569   0.1065
  -8.000  -0.6679   0.04495   0.03508  -0.0765   0.9531   0.1119
  -7.750  -0.6482   0.04382   0.03387  -0.0764   0.9490   0.1171
  -7.500  -0.6297   0.04233   0.03201  -0.0763   0.9445   0.1239
  -7.250  -0.6059   0.04145   0.03121  -0.0766   0.9409   0.1301
  -7.000  -0.5784   0.04030   0.02976  -0.0777   0.9378   0.1389
  -6.750  -0.5621   0.03954   0.02908  -0.0765   0.9330   0.1457
  -6.500  -0.5402   0.03865   0.02800  -0.0764   0.9289   0.1551
  -6.250  -0.5154   0.03795   0.02730  -0.0768   0.9255   0.1653
  -6.000  -0.4874   0.03724   0.02657  -0.0777   0.9226   0.1779
  -5.750  -0.4714   0.03659   0.02587  -0.0765   0.9176   0.1897
  -5.500  -0.4493   0.03597   0.02523  -0.0764   0.9133   0.2048
  -5.250  -0.4239   0.03538   0.02467  -0.0768   0.9099   0.2224
  -5.000  -0.3957   0.03483   0.02423  -0.0778   0.9071   0.2437
  -4.750  -0.3781   0.03435   0.02383  -0.0769   0.9025   0.2655
  -4.500  -0.3570   0.03392   0.02353  -0.0765   0.8980   0.2935
  -4.250  -0.3313   0.03364   0.02344  -0.0768   0.8943   0.3301
  -4.000  -0.3029   0.03363   0.02364  -0.0772   0.8912   0.3724
  -3.750  -0.2840   0.03383   0.02393  -0.0758   0.8867   0.4093
  -3.500  -0.2652   0.03417   0.02433  -0.0742   0.8817   0.4418
  -3.250  -0.2403   0.03461   0.02474  -0.0736   0.8777   0.4730
  -3.000  -0.2112   0.03506   0.02507  -0.0738   0.8745   0.5017
  -2.750  -0.1928   0.03550   0.02544  -0.0722   0.8697   0.5232
  -2.500  -0.1743   0.03588   0.02575  -0.0707   0.8647   0.5432
  -2.250  -0.1507   0.03629   0.02607  -0.0699   0.8609   0.5628
  -2.000  -0.1235   0.03668   0.02639  -0.0697   0.8578   0.5819
  -1.750  -0.1052   0.03704   0.02670  -0.0681   0.8533   0.5985
  -1.500  -0.0888   0.03735   0.02696  -0.0662   0.8479   0.6141
  -1.250  -0.0657   0.03766   0.02721  -0.0655   0.8439   0.6304
  -1.000  -0.0382   0.03793   0.02741  -0.0655   0.8408   0.6463
  -0.750  -0.0198   0.03820   0.02763  -0.0642   0.8360   0.6596
  -0.500  -0.0034   0.03844   0.02785  -0.0625   0.8302   0.6706
  -0.250   0.0233   0.03864   0.02797  -0.0627   0.8260   0.6828
   0.000   0.0541   0.03883   0.02809  -0.0634   0.8228   0.6944
   0.250   0.0670   0.03912   0.02836  -0.0614   0.8161   0.7038
   0.500   0.0907   0.03937   0.02855  -0.0614   0.8110   0.7147
   0.750   0.1190   0.03957   0.02872  -0.0617   0.8072   0.7238
   1.000   0.1444   0.03989   0.02898  -0.0620   0.8027   0.7342
   1.250   0.1581   0.04023   0.02935  -0.0602   0.7959   0.7426
   1.500   0.1864   0.04050   0.02958  -0.0608   0.7914   0.7532
   1.750   0.2180   0.04069   0.02978  -0.0616   0.7880   0.7632
   2.000   0.2282   0.04117   0.03028  -0.0597   0.7795   0.7727
   2.250   0.2559   0.04140   0.03052  -0.0600   0.7743   0.7827
   2.500   0.2905   0.04154   0.03067  -0.0613   0.7707   0.7929
   2.750   0.2995   0.04211   0.03128  -0.0593   0.7612   0.8032
   3.000   0.3288   0.04230   0.03153  -0.0598   0.7562   0.8143
   3.250   0.3502   0.04267   0.03196  -0.0593   0.7496   0.8266
   3.500   0.3711   0.04302   0.03238  -0.0588   0.7418   0.8404
   3.750   0.4059   0.04300   0.03246  -0.0599   0.7372   0.8567
   4.000   0.4182   0.04351   0.03309  -0.0584   0.7267   0.8758
   4.250   0.4562   0.04351   0.03322  -0.0602   0.7212   0.9032
   4.500   0.4770   0.04390   0.03376  -0.0606   0.7103   1.0000
   4.750   0.5164   0.04408   0.03393  -0.0630   0.7042   1.0000
   5.000   0.5368   0.04475   0.03461  -0.0632   0.6929   1.0000
   5.250   0.5773   0.04467   0.03456  -0.0652   0.6866   1.0000
   5.500   0.5954   0.04533   0.03523  -0.0648   0.6740   1.0000
   5.750   0.6400   0.04482   0.03476  -0.0667   0.6683   1.0000
   6.000   0.6568   0.04533   0.03532  -0.0658   0.6541   1.0000
   6.250   0.6784   0.04555   0.03559  -0.0651   0.6405   1.0000
   6.500   0.7060   0.04535   0.03544  -0.0648   0.6279   1.0000
   6.750   0.7451   0.04432   0.03450  -0.0652   0.6182   1.0000
   7.000   0.7653   0.04434   0.03458  -0.0640   0.6027   1.0000
   7.250   0.7865   0.04425   0.03459  -0.0628   0.5872   1.0000
   7.500   0.8084   0.04407   0.03450  -0.0616   0.5715   1.0000
   7.750   0.8313   0.04373   0.03425  -0.0604   0.5554   1.0000
   8.000   0.8547   0.04332   0.03393  -0.0591   0.5380   1.0000
   8.250   0.8781   0.04292   0.03363  -0.0578   0.5191   1.0000
   8.500   0.9047   0.04225   0.03302  -0.0566   0.4987   1.0000
   8.750   0.9252   0.04217   0.03300  -0.0551   0.4729   1.0000
   9.000   0.9557   0.04126   0.03205  -0.0540   0.4448   1.0000
   9.250   0.9828   0.04071   0.03134  -0.0526   0.4109   1.0000
   9.500   1.0031   0.04092   0.03133  -0.0511   0.3756   1.0000
   9.750   1.0184   0.04165   0.03180  -0.0494   0.3432   1.0000
  10.000   1.0288   0.04292   0.03291  -0.0477   0.3149   1.0000
  10.250   1.0396   0.04424   0.03402  -0.0462   0.2914   1.0000
  10.500   1.0502   0.04569   0.03537  -0.0448   0.2710   1.0000
  10.750   1.0611   0.04717   0.03678  -0.0435   0.2528   1.0000
  11.000   1.0730   0.04863   0.03815  -0.0424   0.2371   1.0000
  11.250   1.0853   0.05008   0.03952  -0.0413   0.2229   1.0000
  11.500   1.0978   0.05157   0.04097  -0.0403   0.2096   1.0000
  11.750   1.1104   0.05312   0.04259  -0.0394   0.1972   1.0000
  12.000   1.1239   0.05462   0.04410  -0.0385   0.1864   1.0000
  12.250   1.1391   0.05599   0.04540  -0.0377   0.1766   1.0000
  12.500   1.1515   0.05772   0.04729  -0.0370   0.1671   1.0000
  12.750   1.1686   0.05906   0.04858  -0.0363   0.1588   1.0000
  13.000   1.1796   0.06095   0.05068  -0.0356   0.1508   1.0000
  13.250   1.1968   0.06235   0.05202  -0.0350   0.1439   1.0000
  13.500   1.2039   0.06466   0.05459  -0.0342   0.1372   1.0000
  13.750   1.2187   0.06618   0.05605  -0.0336   0.1311   1.0000
  14.000   1.2231   0.06886   0.05902  -0.0329   0.1257   1.0000
  14.250   1.2278   0.07134   0.06166  -0.0322   0.1207   1.0000
  14.500   1.2421   0.07296   0.06319  -0.0317   0.1159   1.0000
  14.750   1.2349   0.07678   0.06740  -0.0312   0.1121   1.0000
  15.000   1.2324   0.08013   0.07098  -0.0309   0.1083   1.0000
  15.250   1.2394   0.08235   0.07320  -0.0306   0.1046   1.0000
  15.500   1.2362   0.08599   0.07704  -0.0305   0.1017   1.0000
  15.750   1.2178   0.09152   0.08292  -0.0312   0.0995   1.0000
  16.000   1.1992   0.09735   0.08905  -0.0324   0.0974   1.0000
  16.250   1.1816   0.10326   0.09520  -0.0341   0.0955   1.0000
  16.500   1.1705   0.10844   0.10052  -0.0358   0.0934   1.0000
  16.750   1.1813   0.11025   0.10227  -0.0358   0.0907   1.0000
  17.000   1.1361   0.12166   0.11402  -0.0415   0.0904   1.0000
  17.250   1.0632   0.14103   0.13367  -0.0531   0.0905   1.0000
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