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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=50,000 Ncrit=9


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 50,000
Max Cl/Cd: 30.02 at α=9.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx83w160-il-50000.txt
Download as CSV file: xf-fx83w160-il-50000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.3539   0.12467   0.11848  -0.0109   1.0000   0.3597
  -8.250  -0.6375   0.09104   0.08459  -0.0348   1.0000   0.1876
  -8.000  -0.6628   0.08480   0.07836  -0.0361   1.0000   0.1845
  -7.750  -0.6916   0.07802   0.07155  -0.0377   1.0000   0.1819
  -7.500  -0.7288   0.06874   0.06201  -0.0414   1.0000   0.1780
  -7.250  -0.7420   0.06191   0.05477  -0.0439   1.0000   0.1787
  -7.000  -0.7413   0.05638   0.04876  -0.0458   1.0000   0.1813
  -6.750  -0.7332   0.05115   0.04272  -0.0482   1.0000   0.1859
  -6.500  -0.7176   0.04930   0.04095  -0.0472   1.0000   0.1924
  -6.250  -0.7008   0.04655   0.03779  -0.0478   1.0000   0.2001
  -6.000  -0.6830   0.04439   0.03545  -0.0477   1.0000   0.2088
  -5.750  -0.6629   0.04230   0.03294  -0.0481   1.0000   0.2191
  -5.500  -0.6442   0.04096   0.03167  -0.0473   1.0000   0.2300
  -5.250  -0.6237   0.03942   0.02993  -0.0472   1.0000   0.2426
  -5.000  -0.6031   0.03821   0.02858  -0.0469   1.0000   0.2577
  -4.750  -0.5826   0.03721   0.02754  -0.0464   1.0000   0.2747
  -4.500  -0.5627   0.03642   0.02683  -0.0456   1.0000   0.2933
  -4.250  -0.5433   0.03584   0.02638  -0.0446   1.0000   0.3155
  -4.000  -0.5223   0.03517   0.02570  -0.0441   1.0000   0.3432
  -3.750  -0.5043   0.03500   0.02582  -0.0423   1.0000   0.3707
  -3.500  -0.4864   0.03505   0.02609  -0.0405   1.0000   0.4044
  -3.250  -0.4701   0.03551   0.02678  -0.0380   1.0000   0.4410
  -3.000  -0.4551   0.03629   0.02771  -0.0349   1.0000   0.4789
  -2.750  -0.4406   0.03715   0.02863  -0.0318   1.0000   0.5177
  -2.500  -0.4275   0.03794   0.02945  -0.0283   1.0000   0.5526
  -2.250  -0.4180   0.03871   0.03031  -0.0236   1.0000   0.5797
  -2.000  -0.4056   0.03913   0.03070  -0.0203   1.0000   0.6106
  -1.750  -0.3953   0.03949   0.03106  -0.0164   1.0000   0.6371
  -1.500  -0.3830   0.03967   0.03117  -0.0134   1.0000   0.6644
  -1.250  -0.3736   0.03981   0.03130  -0.0095   1.0000   0.6880
  -1.000  -0.3613   0.03987   0.03129  -0.0068   1.0000   0.7135
  -0.750  -0.3506   0.03984   0.03122  -0.0036   1.0000   0.7368
  -0.500  -0.3415   0.03976   0.03110  -0.0001   1.0000   0.7589
  -0.250  -0.3309   0.03968   0.03097   0.0028   1.0000   0.7821
   0.000  -0.3189   0.03961   0.03084   0.0052   1.0000   0.8059
   0.250  -0.3089   0.03944   0.03064   0.0082   1.0000   0.8276
   0.500  -0.2975   0.03932   0.03046   0.0107   1.0000   0.8506
   0.750  -0.2837   0.03927   0.03036   0.0124   1.0000   0.8738
   1.000  -0.2680   0.03921   0.03029   0.0136   1.0000   0.8960
   1.250  -0.2457   0.03936   0.03043   0.0132   1.0000   0.9200
   1.500  -0.2110   0.03987   0.03093   0.0098   1.0000   0.9438
   1.750  -0.1675   0.04061   0.03165   0.0040   1.0000   0.9675
   2.000  -0.1363   0.04085   0.03187   0.0000   1.0000   1.0000
   2.250  -0.1191   0.04104   0.03198  -0.0015   1.0000   1.0000
   2.500  -0.0969   0.04162   0.03248  -0.0038   1.0000   1.0000
   2.750  -0.0722   0.04247   0.03324  -0.0066   1.0000   1.0000
   3.000  -0.0466   0.04350   0.03419  -0.0094   1.0000   1.0000
   3.250  -0.0209   0.04466   0.03528  -0.0123   1.0000   1.0000
   3.500   0.0045   0.04592   0.03648  -0.0150   1.0000   1.0000
   3.750   0.0293   0.04727   0.03777  -0.0176   1.0000   1.0000
   4.000   0.0683   0.04988   0.04029  -0.0229   0.9949   1.0000
   4.250   0.1095   0.05275   0.04309  -0.0285   0.9860   1.0000
   4.500   0.1454   0.05516   0.04546  -0.0331   0.9754   1.0000
   4.750   0.1772   0.05725   0.04753  -0.0369   0.9626   1.0000
   5.000   0.2089   0.05946   0.04973  -0.0405   0.9486   1.0000
   5.250   0.2398   0.06170   0.05196  -0.0439   0.9338   1.0000
   5.500   0.2697   0.06378   0.05406  -0.0470   0.9155   1.0000
   5.750   0.3038   0.06611   0.05640  -0.0505   0.8949   1.0000
   6.000   0.3451   0.06899   0.05929  -0.0547   0.8718   1.0000
   6.250   0.4550   0.06747   0.05777  -0.0616   0.7667   1.0000
   6.500   0.4938   0.06808   0.05843  -0.0633   0.7404   1.0000
   6.750   0.5367   0.06855   0.05894  -0.0651   0.7160   1.0000
   7.000   0.5677   0.06891   0.05938  -0.0655   0.6919   1.0000
   7.250   0.6180   0.06861   0.05917  -0.0673   0.6702   1.0000
   7.500   0.6525   0.06850   0.05917  -0.0675   0.6481   1.0000
   7.750   0.6806   0.06843   0.05919  -0.0670   0.6248   1.0000
   8.000   0.7280   0.06699   0.05788  -0.0673   0.6038   1.0000
   8.250   0.7845   0.06431   0.05538  -0.0674   0.5844   1.0000
   8.500   0.8038   0.06407   0.05525  -0.0656   0.5588   1.0000
   8.750   0.8568   0.06062   0.05200  -0.0646   0.5380   1.0000
   9.000   0.9257   0.05462   0.04621  -0.0631   0.5195   1.0000
   9.250   1.0207   0.04561   0.03741  -0.0623   0.4942   1.0000
   9.500   1.1105   0.03918   0.03071  -0.0629   0.4419   1.0000
   9.750   1.1568   0.03853   0.02955  -0.0630   0.3917   1.0000
  10.000   1.1864   0.03957   0.03029  -0.0625   0.3545   1.0000
  10.250   1.2194   0.04088   0.03129  -0.0627   0.3229   1.0000
  10.500   1.2417   0.04253   0.03284  -0.0620   0.2990   1.0000
  10.750   1.2838   0.04425   0.03428  -0.0639   0.2742   1.0000
  11.000   1.3078   0.04628   0.03630  -0.0636   0.2567   1.0000
  11.250   1.3344   0.04844   0.03843  -0.0637   0.2406   1.0000
  11.500   1.3354   0.05067   0.04095  -0.0606   0.2308   1.0000
  11.750   1.3520   0.05319   0.04356  -0.0596   0.2197   1.0000
  12.000   1.3819   0.05574   0.04604  -0.0604   0.2072   1.0000
  12.250   1.3654   0.05842   0.04912  -0.0554   0.2028   1.0000
  12.500   1.3987   0.06110   0.05168  -0.0566   0.1914   1.0000
  12.750   1.3730   0.06409   0.05508  -0.0512   0.1891   1.0000
  13.000   1.3482   0.06751   0.05885  -0.0467   0.1867   1.0000
  13.250   1.3237   0.07133   0.06297  -0.0430   0.1844   1.0000
  13.500   1.3020   0.07540   0.06728  -0.0401   0.1819   1.0000
  13.750   1.2689   0.08050   0.07265  -0.0376   0.1811   1.0000
  14.000   1.2439   0.08567   0.07800  -0.0361   0.1793   1.0000
  14.250   1.2176   0.09149   0.08399  -0.0354   0.1778   1.0000
  14.500   1.1925   0.09799   0.09062  -0.0355   0.1766   1.0000
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