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FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: FX 61-184 AIRFOIL (fx61184-il)
Reynolds number: 50,000
Max Cl/Cd: 15.16 at α=12°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx61184-il-50000-n5.txt
Download as CSV file: xf-fx61184-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 61-184 AIRFOIL                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.3853   0.11538   0.10829  -0.0665   1.0000   0.0523
 -13.000  -0.3945   0.10928   0.10226  -0.0690   1.0000   0.0520
 -12.750  -0.4107   0.10232   0.09534  -0.0722   1.0000   0.0516
 -12.500  -0.4312   0.09555   0.08861  -0.0753   1.0000   0.0512
 -12.250  -0.4562   0.08932   0.08243  -0.0779   1.0000   0.0507
 -12.000  -0.4834   0.08425   0.07738  -0.0792   1.0000   0.0503
 -11.750  -0.5134   0.08077   0.07395  -0.0785   1.0000   0.0499
 -11.500  -0.5478   0.07906   0.07230  -0.0751   1.0000   0.0495
 -11.250  -0.5681   0.07433   0.06739  -0.0778   0.9916   0.0493
 -11.000  -0.5798   0.06938   0.06216  -0.0817   0.9797   0.0493
 -10.750  -0.5890   0.06517   0.05763  -0.0844   0.9682   0.0495
 -10.500  -0.5928   0.06147   0.05358  -0.0866   0.9585   0.0498
 -10.250  -0.5961   0.05840   0.05016  -0.0872   0.9480   0.0503
 -10.000  -0.5918   0.05545   0.04682  -0.0879   0.9394   0.0511
  -9.750  -0.5812   0.05262   0.04348  -0.0888   0.9322   0.0525
  -9.500  -0.5559   0.05022   0.04100  -0.0901   0.9279   0.0552
  -9.250  -0.5359   0.04846   0.03908  -0.0900   0.9216   0.0574
  -9.000  -0.4999   0.04651   0.03685  -0.0908   0.9184   0.0602
  -8.750  -0.4508   0.04493   0.03499  -0.0921   0.9171   0.0651
  -8.500  -0.4003   0.04394   0.03396  -0.0935   0.9158   0.0718
  -8.250  -0.3573   0.04305   0.03297  -0.0945   0.9138   0.0793
  -8.000  -0.3420   0.04242   0.03232  -0.0930   0.9064   0.0858
  -7.750  -0.3201   0.04138   0.03127  -0.0931   0.9014   0.0951
  -7.500  -0.3057   0.04038   0.03026  -0.0925   0.8956   0.1059
  -7.250  -0.3040   0.03947   0.02942  -0.0902   0.8875   0.1175
  -7.000  -0.2996   0.03805   0.02821  -0.0891   0.8815   0.1363
  -6.750  -0.3131   0.03725   0.02759  -0.0848   0.8719   0.1522
  -6.500  -0.3179   0.03530   0.02613  -0.0834   0.8655   0.2014
  -6.250  -0.3355   0.03426   0.02568  -0.0789   0.8560   0.2651
  -6.000  -0.2941   0.03799   0.03032  -0.0735   0.8532   0.4557
  -5.750  -0.2933   0.03802   0.03016  -0.0711   0.8460   0.4933
  -5.500  -0.2823   0.03898   0.03093  -0.0684   0.8394   0.5263
  -5.250  -0.2431   0.04265   0.03437  -0.0650   0.8362   0.5681
  -5.000  -0.2240   0.04430   0.03584  -0.0613   0.8308   0.5900
  -4.750  -0.2184   0.04448   0.03587  -0.0583   0.8237   0.6040
  -4.500  -0.1825   0.04482   0.03594  -0.0583   0.8205   0.6114
  -4.250  -0.1793   0.04463   0.03562  -0.0557   0.8139   0.6222
  -4.000  -0.1663   0.04472   0.03555  -0.0534   0.8076   0.6299
  -3.750  -0.1426   0.04433   0.03496  -0.0536   0.8036   0.6393
  -3.500  -0.1396   0.04443   0.03496  -0.0502   0.7965   0.6467
  -3.250  -0.1295   0.04417   0.03457  -0.0485   0.7903   0.6550
  -3.000  -0.0987   0.04395   0.03415  -0.0492   0.7870   0.6612
  -2.750  -0.1087   0.04387   0.03401  -0.0450   0.7782   0.6697
  -2.500  -0.0869   0.04381   0.03382  -0.0441   0.7734   0.6746
  -2.250  -0.0570   0.04337   0.03319  -0.0456   0.7701   0.6821
  -2.000  -0.0664   0.04362   0.03342  -0.0409   0.7608   0.6874
  -1.750  -0.0421   0.04348   0.03314  -0.0408   0.7564   0.6925
  -1.500  -0.0089   0.04302   0.03249  -0.0431   0.7534   0.6993
  -1.250  -0.0187   0.04347   0.03295  -0.0382   0.7435   0.7037
  -1.000   0.0083   0.04332   0.03268  -0.0386   0.7395   0.7081
  -0.750   0.0245   0.04333   0.03259  -0.0383   0.7334   0.7138
  -0.500   0.0362   0.04349   0.03269  -0.0372   0.7263   0.7181
  -0.250   0.0646   0.04338   0.03248  -0.0376   0.7226   0.7218
   0.000   0.0735   0.04373   0.03279  -0.0362   0.7151   0.7263
   0.250   0.0965   0.04382   0.03279  -0.0372   0.7093   0.7309
   0.500   0.1272   0.04369   0.03258  -0.0380   0.7058   0.7342
   0.750   0.1318   0.04432   0.03320  -0.0360   0.6973   0.7377
   1.000   0.1570   0.04443   0.03326  -0.0365   0.6923   0.7414
   1.250   0.1923   0.04431   0.03306  -0.0385   0.6891   0.7452
   1.500   0.1980   0.04515   0.03389  -0.0375   0.6797   0.7489
   1.750   0.2240   0.04522   0.03394  -0.0376   0.6753   0.7518
   2.250   0.2603   0.04617   0.03486  -0.0375   0.6619   0.7585
   2.500   0.2951   0.04620   0.03486  -0.0394   0.6583   0.7621
   2.750   0.3046   0.04716   0.03583  -0.0388   0.6496   0.7651
   3.000   0.3303   0.04736   0.03605  -0.0391   0.6445   0.7678
   3.250   0.3641   0.04731   0.03600  -0.0403   0.6414   0.7709
   3.500   0.3687   0.04862   0.03734  -0.0395   0.6310   0.7743
   3.750   0.4037   0.04869   0.03742  -0.0412   0.6272   0.7777
   4.000   0.4134   0.04991   0.03869  -0.0410   0.6180   0.7805
   4.250   0.4406   0.05010   0.03891  -0.0414   0.6130   0.7832
   4.750   0.4789   0.05156   0.04048  -0.0417   0.5988   0.7897
   5.000   0.5156   0.05150   0.04046  -0.0433   0.5953   0.7932
   5.250   0.5215   0.05310   0.04213  -0.0429   0.5845   0.7962
   5.500   0.5531   0.05303   0.04214  -0.0435   0.5805   0.7990
   5.750   0.5588   0.05461   0.04380  -0.0429   0.5701   0.8021
   6.000   0.5910   0.05463   0.04390  -0.0438   0.5656   0.8058
   6.250   0.6009   0.05622   0.04558  -0.0439   0.5553   0.8094
   6.500   0.6316   0.05619   0.04565  -0.0444   0.5504   0.8129
   6.750   0.6392   0.05768   0.04724  -0.0438   0.5398   0.8162
   7.000   0.6708   0.05757   0.04725  -0.0443   0.5348   0.8199
   7.250   0.6797   0.05924   0.04902  -0.0443   0.5238   0.8235
   7.500   0.7131   0.05898   0.04888  -0.0449   0.5189   0.8277
   7.750   0.7174   0.06080   0.05081  -0.0442   0.5074   0.8315
   8.000   0.7514   0.06024   0.05040  -0.0445   0.5027   0.8363
   8.250   0.7584   0.06211   0.05239  -0.0444   0.4906   0.8406
   8.500   0.7946   0.06111   0.05155  -0.0444   0.4864   0.8454
   8.750   0.7982   0.06308   0.05367  -0.0438   0.4734   0.8498
   9.250   0.8390   0.06399   0.05488  -0.0435   0.4565   0.8608
   9.750   0.8793   0.06467   0.05590  -0.0427   0.4397   0.8742
  10.000   0.8805   0.06690   0.05828  -0.0420   0.4265   0.8809
  10.500   0.9198   0.06713   0.05887  -0.0407   0.4092   0.8998
  11.000   0.9608   0.06666   0.05879  -0.0391   0.3918   0.9381
  11.250   0.9651   0.06864   0.06093  -0.0393   0.3779   1.0000
  11.500   0.9759   0.07079   0.06322  -0.0402   0.3645   1.0000
  12.000   1.0450   0.06895   0.06171  -0.0411   0.3456   1.0000
  12.250   1.0537   0.07117   0.06405  -0.0418   0.3316   1.0000
  12.500   1.0650   0.07305   0.06605  -0.0423   0.3178   1.0000
  12.750   1.0799   0.07439   0.06752  -0.0427   0.3042   1.0000
  13.000   1.0978   0.07521   0.06843  -0.0429   0.2901   1.0000
  13.250   1.1141   0.07618   0.06945  -0.0431   0.2755   1.0000
  13.500   1.1274   0.07756   0.07088  -0.0433   0.2605   1.0000
  13.750   1.1380   0.07930   0.07264  -0.0435   0.2454   1.0000
  14.000   1.1462   0.08139   0.07477  -0.0439   0.2302   1.0000
  14.250   1.1510   0.08396   0.07735  -0.0444   0.2150   1.0000
  14.500   1.1537   0.08690   0.08029  -0.0450   0.2004   1.0000
  14.750   1.1557   0.09001   0.08341  -0.0458   0.1864   1.0000
  15.000   1.1577   0.09318   0.08657  -0.0466   0.1733   1.0000
  15.250   1.1597   0.09638   0.08973  -0.0475   0.1609   1.0000
  15.500   1.1618   0.09959   0.09293  -0.0484   0.1493   1.0000
  15.750   1.1569   0.10425   0.09771  -0.0501   0.1387   1.0000
  16.000   1.1559   0.10824   0.10175  -0.0515   0.1292   1.0000
  16.250   1.1611   0.11102   0.10443  -0.0525   0.1205   1.0000
  16.500   1.1556   0.11608   0.10970  -0.0546   0.1128   1.0000
  16.750   1.1595   0.11921   0.11277  -0.0558   0.1059   1.0000
  17.000   1.1545   0.12437   0.11813  -0.0582   0.1000   1.0000
  17.250   1.1642   0.12635   0.11997  -0.0590   0.0942   1.0000
  17.500   1.1520   0.13321   0.12715  -0.0625   0.0902   1.0000
  17.750   1.1473   0.13850   0.13259  -0.0653   0.0862   1.0000
  18.000   1.1626   0.13935   0.13330  -0.0655   0.0818   1.0000
  18.250   1.1397   0.14897   0.14327  -0.0711   0.0799   1.0000
  18.500   1.1026   0.16271   0.15729  -0.0796   0.0785   1.0000
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