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WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il)
Reynolds number: 200,000
Max Cl/Cd: 55.65 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx05191-il-200000.txt
Download as CSV file: xf-fx05191-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-191 AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.2958   0.12635   0.12265  -0.0884   0.9759   0.0732
 -13.500  -0.2871   0.12237   0.11866  -0.0913   0.9745   0.0757
 -13.250  -0.3633   0.10345   0.09977  -0.1111   0.9723   0.0812
 -13.000  -0.3176   0.10477   0.10112  -0.1056   0.9719   0.0830
 -12.750  -0.3005   0.10383   0.10017  -0.1045   0.9694   0.0843
 -12.500  -0.2087   0.08479   0.08125  -0.1215   0.9593   0.0964
 -12.250  -0.1768   0.08446   0.08089  -0.1210   0.9587   0.0981
 -11.500  -0.5047   0.03749   0.03219  -0.1275   0.9446   0.0486
 -11.250  -0.5684   0.05371   0.04850  -0.1244   0.9435   0.0604
 -11.000  -0.6118   0.04908   0.04334  -0.1143   0.9337   0.0480
 -10.750  -0.6030   0.04551   0.03947  -0.1143   0.9312   0.0469
 -10.500  -0.6254   0.04503   0.03887  -0.1069   0.9241   0.0466
 -10.250  -0.6321   0.04332   0.03693  -0.1025   0.9188   0.0462
 -10.000  -0.6166   0.04057   0.03383  -0.1022   0.9164   0.0457
  -9.750  -0.5898   0.03838   0.03135  -0.1035   0.9150   0.0465
  -9.500  -0.6222   0.03883   0.03176  -0.0933   0.9058   0.0464
  -9.250  -0.6032   0.03726   0.02997  -0.0926   0.9026   0.0471
  -9.000  -0.5724   0.03552   0.02796  -0.0938   0.9008   0.0479
  -8.750  -0.5334   0.03378   0.02599  -0.0962   0.8999   0.0486
  -8.500  -0.4901   0.03233   0.02432  -0.0994   0.8992   0.0494
  -8.250  -0.4854   0.03174   0.02370  -0.0952   0.8935   0.0501
  -8.000  -0.4601   0.03082   0.02286  -0.0947   0.8899   0.0519
  -7.750  -0.4211   0.02989   0.02195  -0.0969   0.8880   0.0545
  -7.500  -0.3731   0.02888   0.02089  -0.1006   0.8872   0.0573
  -7.250  -0.3287   0.02768   0.01971  -0.1038   0.8863   0.0603
  -7.000  -0.2987   0.02674   0.01882  -0.1050   0.8843   0.0643
  -6.750  -0.3388   0.02737   0.01942  -0.0933   0.8725   0.0636
  -6.500  -0.3164   0.02669   0.01870  -0.0931   0.8691   0.0680
  -6.250  -0.2938   0.02551   0.01756  -0.0933   0.8667   0.0741
  -6.000  -0.2701   0.02452   0.01656  -0.0938   0.8645   0.0835
  -5.750  -0.3027   0.02499   0.01698  -0.0833   0.8513   0.0828
  -5.500  -0.3063   0.02465   0.01668  -0.0785   0.8437   0.0918
  -4.750  -0.2919   0.02031   0.01463  -0.0718   0.8240   0.5303
  -4.500  -0.2615   0.02024   0.01467  -0.0722   0.8205   0.5812
  -4.250  -0.2240   0.02024   0.01469  -0.0736   0.8187   0.6131
  -4.000  -0.1840   0.02037   0.01480  -0.0753   0.8174   0.6399
  -3.750  -0.1810   0.02098   0.01542  -0.0707   0.8079   0.6553
  -3.500  -0.1561   0.02162   0.01607  -0.0690   0.8038   0.6728
  -3.250  -0.1237   0.02251   0.01696  -0.0680   0.8019   0.6886
  -3.000  -0.0883   0.02346   0.01790  -0.0672   0.8007   0.6964
  -2.750  -0.0696   0.02372   0.01810  -0.0655   0.7950   0.7048
  -2.500  -0.0142   0.02360   0.01787  -0.0696   0.7975   0.7071
  -2.000   0.0199   0.02366   0.01782  -0.0666   0.7844   0.7201
  -1.750   0.0574   0.02364   0.01775  -0.0677   0.7832   0.7222
  -1.500   0.0962   0.02358   0.01762  -0.0692   0.7822   0.7251
  -1.250   0.0882   0.02375   0.01776  -0.0642   0.7695   0.7356
  -1.000   0.1242   0.02370   0.01768  -0.0651   0.7682   0.7377
  -0.750   0.1138   0.02433   0.01834  -0.0581   0.7571   0.7419
  -0.500   0.1500   0.02407   0.01802  -0.0597   0.7550   0.7472
  -0.250   0.1911   0.02366   0.01754  -0.0625   0.7536   0.7534
   0.000   0.2269   0.02352   0.01738  -0.0633   0.7523   0.7559
   0.250   0.2644   0.02331   0.01714  -0.0647   0.7512   0.7592
   0.500   0.3060   0.02294   0.01672  -0.0674   0.7502   0.7646
   0.750   0.2907   0.02339   0.01721  -0.0602   0.7379   0.7717
   1.000   0.3278   0.02312   0.01692  -0.0614   0.7366   0.7749
   1.250   0.3307   0.02343   0.01723  -0.0580   0.7278   0.7837
   1.500   0.3563   0.02325   0.01704  -0.0575   0.7241   0.7876
   1.750   0.3897   0.02294   0.01673  -0.0580   0.7224   0.7908
   2.000   0.4298   0.02255   0.01633  -0.0600   0.7212   0.7951
   2.250   0.4800   0.02208   0.01581  -0.0648   0.7202   0.8019
   2.500   0.5173   0.02170   0.01545  -0.0660   0.7190   0.8042
   2.750   0.4917   0.02234   0.01615  -0.0566   0.7072   0.8108
   3.000   0.5409   0.02188   0.01567  -0.0610   0.7059   0.8170
   3.250   0.5815   0.02144   0.01524  -0.0630   0.7045   0.8199
   3.500   0.5595   0.02207   0.01594  -0.0543   0.6939   0.8262
   3.750   0.6029   0.02167   0.01554  -0.0574   0.6920   0.8312
   4.000   0.6473   0.02120   0.01508  -0.0605   0.6903   0.8349
   4.250   0.6889   0.02081   0.01471  -0.0626   0.6886   0.8378
   4.500   0.6721   0.02141   0.01538  -0.0553   0.6786   0.8454
   4.750   0.7188   0.02102   0.01499  -0.0591   0.6762   0.8495
   5.000   0.7585   0.02060   0.01461  -0.0609   0.6740   0.8522
   5.250   0.7578   0.02091   0.01498  -0.0561   0.6667   0.8580
   5.500   0.7909   0.02080   0.01490  -0.0576   0.6618   0.8628
   5.750   0.8422   0.02025   0.01437  -0.0617   0.6585   0.8657
   6.000   0.8507   0.02025   0.01442  -0.0581   0.6517   0.8701
   6.250   0.8783   0.01998   0.01418  -0.0581   0.6445   0.8746
   6.500   0.9331   0.01957   0.01376  -0.0631   0.6387   0.8777
   6.750   0.9293   0.01966   0.01394  -0.0576   0.6297   0.8829
   7.000   0.9647   0.01923   0.01349  -0.0586   0.6209   0.8864
   7.250   0.9854   0.01896   0.01322  -0.0573   0.6095   0.8909
   7.500   0.9966   0.01911   0.01345  -0.0549   0.5995   0.8957
   7.750   1.0294   0.01874   0.01304  -0.0555   0.5908   0.8988
   8.000   1.0248   0.01903   0.01346  -0.0503   0.5806   0.9042
   8.250   1.0485   0.01903   0.01349  -0.0500   0.5706   0.9081
   8.500   1.0618   0.01908   0.01359  -0.0478   0.5601   0.9120
   8.750   1.0672   0.01931   0.01391  -0.0444   0.5495   0.9164
   9.000   1.0817   0.01945   0.01408  -0.0427   0.5369   0.9206
   9.250   1.0936   0.01973   0.01439  -0.0408   0.5220   0.9242
   9.500   1.0987   0.01999   0.01468  -0.0375   0.5071   0.9283
   9.750   1.1025   0.02053   0.01527  -0.0345   0.4895   0.9328
  10.000   1.1066   0.02131   0.01609  -0.0321   0.4678   0.9366
  10.250   1.1072   0.02196   0.01670  -0.0286   0.4442   0.9407
  10.500   1.1052   0.02297   0.01766  -0.0253   0.4127   0.9453
  10.750   1.1000   0.02448   0.01898  -0.0221   0.3678   0.9493
  11.000   1.0836   0.02649   0.02071  -0.0176   0.3169   0.9539
  11.250   1.0651   0.02906   0.02297  -0.0136   0.2643   0.9590
  11.500   1.0466   0.03205   0.02565  -0.0103   0.2136   0.9636
  11.750   1.0323   0.03505   0.02839  -0.0078   0.1739   0.9684
  12.000   1.0256   0.03782   0.03099  -0.0063   0.1457   0.9740
  12.250   1.0250   0.04034   0.03341  -0.0057   0.1282   0.9815
  12.500   1.0264   0.04263   0.03564  -0.0053   0.1160   1.0000
  12.750   1.0341   0.04486   0.03787  -0.0055   0.1062   1.0000
  13.000   1.0404   0.04722   0.04022  -0.0056   0.0984   1.0000
  13.250   1.0481   0.04951   0.04250  -0.0059   0.0914   1.0000
  13.500   1.0570   0.05165   0.04466  -0.0061   0.0851   1.0000
  13.750   1.0670   0.05375   0.04676  -0.0065   0.0794   1.0000
  14.000   1.0783   0.05564   0.04864  -0.0066   0.0742   1.0000
  14.250   1.0914   0.05752   0.05058  -0.0071   0.0697   1.0000
  14.500   1.1065   0.05892   0.05186  -0.0070   0.0650   1.0000
  14.750   1.1194   0.06093   0.05405  -0.0078   0.0618   1.0000
  15.000   1.1333   0.06276   0.05591  -0.0084   0.0585   1.0000
  15.250   1.1531   0.06378   0.05682  -0.0084   0.0551   1.0000
  15.500   1.1646   0.06599   0.05922  -0.0092   0.0529   1.0000
  15.750   1.1775   0.06799   0.06133  -0.0099   0.0504   1.0000
  16.000   1.1910   0.06988   0.06321  -0.0106   0.0483   1.0000
  16.250   1.2089   0.07130   0.06466  -0.0108   0.0460   1.0000
  16.500   1.2186   0.07375   0.06731  -0.0116   0.0443   1.0000
  16.750   1.2290   0.07609   0.06978  -0.0123   0.0426   1.0000
  17.000   1.2403   0.07830   0.07204  -0.0131   0.0411   1.0000
  17.250   1.2605   0.07956   0.07324  -0.0134   0.0393   1.0000
  17.500   1.2617   0.08303   0.07698  -0.0144   0.0382   1.0000
  17.750   1.2650   0.08630   0.08046  -0.0154   0.0370   1.0000
  18.000   1.2696   0.08945   0.08378  -0.0164   0.0359   1.0000
  18.250   1.2746   0.09254   0.08700  -0.0176   0.0350   1.0000
  18.500   1.2833   0.09511   0.08960  -0.0188   0.0341   1.0000
  18.750   1.2943   0.09762   0.09216  -0.0193   0.0330   1.0000
  19.000   1.2835   0.10283   0.09768  -0.0213   0.0326   1.0000
  19.250   1.2717   0.10838   0.10353  -0.0237   0.0321   1.0000
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