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S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: S1048 14% (Danny Howell) (s1048-il)
Reynolds number: 50,000
Max Cl/Cd: 28.26 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1048-il-50000-n5.txt
Download as CSV file: xf-s1048-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1048 14% (Danny Howell)                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7333   0.12351   0.11638  -0.0009   1.0000   0.0536
 -14.250  -0.7618   0.11175   0.10457  -0.0074   1.0000   0.0528
 -14.000  -0.7901   0.10115   0.09382  -0.0134   1.0000   0.0523
 -13.750  -0.8129   0.09255   0.08501  -0.0182   1.0000   0.0521
 -13.500  -0.8311   0.08539   0.07762  -0.0220   1.0000   0.0527
 -13.250  -0.8456   0.07921   0.07117  -0.0250   1.0000   0.0537
 -13.000  -0.8557   0.07392   0.06558  -0.0272   1.0000   0.0548
 -12.750  -0.8548   0.07062   0.06232  -0.0277   1.0000   0.0572
 -12.500  -0.8552   0.06722   0.05885  -0.0284   1.0000   0.0598
 -12.250  -0.8576   0.06355   0.05501  -0.0293   1.0000   0.0629
 -12.000  -0.8606   0.05974   0.05091  -0.0300   1.0000   0.0669
 -11.750  -0.8605   0.05694   0.04823  -0.0302   1.0000   0.0713
 -11.500  -0.8607   0.05388   0.04502  -0.0304   1.0000   0.0767
 -11.250  -0.8602   0.05105   0.04216  -0.0302   1.0000   0.0822
 -11.000  -0.8614   0.04822   0.03925  -0.0300   1.0000   0.0897
 -10.750  -0.8634   0.04556   0.03663  -0.0297   1.0000   0.0975
 -10.500  -0.8653   0.04300   0.03405  -0.0290   1.0000   0.1074
 -10.250  -0.8678   0.04065   0.03168  -0.0279   1.0000   0.1193
 -10.000  -0.8704   0.03857   0.02962  -0.0263   1.0000   0.1323
  -9.750  -0.8734   0.03677   0.02788  -0.0241   1.0000   0.1468
  -9.500  -0.8744   0.03520   0.02640  -0.0217   1.0000   0.1632
  -9.250  -0.8722   0.03380   0.02500  -0.0195   1.0000   0.1829
  -9.000  -0.8670   0.03256   0.02377  -0.0173   1.0000   0.2037
  -8.750  -0.8591   0.03154   0.02278  -0.0152   1.0000   0.2248
  -8.500  -0.8490   0.03062   0.02181  -0.0132   1.0000   0.2462
  -8.250  -0.8365   0.02990   0.02108  -0.0112   1.0000   0.2667
  -8.000  -0.8236   0.02914   0.02021  -0.0094   1.0000   0.2878
  -7.750  -0.8075   0.02863   0.01971  -0.0076   1.0000   0.3067
  -7.500  -0.7912   0.02809   0.01907  -0.0059   1.0000   0.3254
  -7.250  -0.7746   0.02752   0.01839  -0.0042   1.0000   0.3437
  -7.000  -0.7572   0.02700   0.01778  -0.0026   1.0000   0.3611
  -6.750  -0.7385   0.02659   0.01732  -0.0010   1.0000   0.3774
  -6.500  -0.7199   0.02616   0.01683   0.0005   1.0000   0.3931
  -6.250  -0.7013   0.02576   0.01634   0.0021   1.0000   0.4086
  -6.000  -0.6828   0.02535   0.01587   0.0037   1.0000   0.4236
  -5.750  -0.6645   0.02496   0.01542   0.0054   1.0000   0.4382
  -5.500  -0.6465   0.02458   0.01499   0.0070   1.0000   0.4525
  -5.250  -0.6289   0.02422   0.01458   0.0086   1.0000   0.4665
  -5.000  -0.6119   0.02388   0.01419   0.0104   1.0000   0.4804
  -4.750  -0.5956   0.02356   0.01380   0.0122   1.0000   0.4941
  -4.500  -0.5801   0.02328   0.01347   0.0140   1.0000   0.5077
  -4.250  -0.5645   0.02308   0.01327   0.0159   1.0000   0.5201
  -4.000  -0.5497   0.02290   0.01307   0.0178   1.0000   0.5327
  -3.750  -0.5266   0.02276   0.01287   0.0181   0.9954   0.5467
  -3.500  -0.4849   0.02267   0.01271   0.0150   0.9805   0.5634
  -3.250  -0.4444   0.02258   0.01254   0.0122   0.9654   0.5797
  -3.000  -0.4036   0.02248   0.01235   0.0095   0.9510   0.5958
  -2.750  -0.3621   0.02239   0.01221   0.0067   0.9373   0.6117
  -2.500  -0.3198   0.02230   0.01208   0.0040   0.9243   0.6271
  -2.250  -0.2804   0.02221   0.01195   0.0019   0.9102   0.6423
  -2.000  -0.2431   0.02211   0.01182   0.0003   0.8955   0.6572
  -1.750  -0.2075   0.02202   0.01170  -0.0009   0.8806   0.6720
  -1.500  -0.1735   0.02194   0.01158  -0.0017   0.8656   0.6867
  -1.250  -0.1418   0.02187   0.01149  -0.0020   0.8502   0.7013
  -1.000  -0.1118   0.02182   0.01142  -0.0020   0.8346   0.7156
  -0.750  -0.0829   0.02178   0.01138  -0.0017   0.8191   0.7298
  -0.500  -0.0548   0.02176   0.01135  -0.0012   0.8038   0.7443
  -0.250  -0.0273   0.02174   0.01132  -0.0006   0.7885   0.7588
   0.000   0.0000   0.02174   0.01132   0.0000   0.7736   0.7736
   0.250   0.0273   0.02174   0.01132   0.0006   0.7588   0.7885
   0.500   0.0548   0.02176   0.01134   0.0012   0.7443   0.8037
   0.750   0.0829   0.02178   0.01137   0.0017   0.7298   0.8190
   1.000   0.1119   0.02182   0.01142   0.0020   0.7156   0.8346
   1.250   0.1418   0.02187   0.01149   0.0020   0.7013   0.8502
   1.500   0.1735   0.02194   0.01158   0.0017   0.6867   0.8656
   1.750   0.2075   0.02202   0.01171   0.0009   0.6720   0.8807
   2.000   0.2432   0.02211   0.01182  -0.0003   0.6572   0.8955
   2.250   0.2804   0.02221   0.01195  -0.0019   0.6423   0.9102
   2.500   0.3198   0.02230   0.01209  -0.0040   0.6271   0.9243
   2.750   0.3621   0.02239   0.01221  -0.0067   0.6117   0.9373
   3.000   0.4037   0.02248   0.01235  -0.0095   0.5958   0.9510
   3.250   0.4445   0.02258   0.01254  -0.0122   0.5797   0.9655
   3.500   0.4850   0.02267   0.01271  -0.0150   0.5633   0.9805
   3.750   0.5266   0.02276   0.01290  -0.0181   0.5467   0.9954
   4.000   0.5497   0.02289   0.01307  -0.0178   0.5327   1.0000
   4.250   0.5645   0.02308   0.01327  -0.0159   0.5202   1.0000
   4.500   0.5801   0.02328   0.01347  -0.0140   0.5077   1.0000
   4.750   0.5956   0.02356   0.01380  -0.0122   0.4941   1.0000
   5.000   0.6119   0.02388   0.01419  -0.0104   0.4804   1.0000
   5.250   0.6289   0.02422   0.01458  -0.0086   0.4665   1.0000
   5.500   0.6465   0.02458   0.01499  -0.0070   0.4525   1.0000
   5.750   0.6646   0.02496   0.01542  -0.0054   0.4382   1.0000
   6.000   0.6828   0.02535   0.01587  -0.0037   0.4236   1.0000
   6.250   0.7013   0.02575   0.01633  -0.0021   0.4086   1.0000
   6.500   0.7199   0.02616   0.01683  -0.0006   0.3931   1.0000
   6.750   0.7386   0.02658   0.01731   0.0010   0.3773   1.0000
   7.000   0.7573   0.02701   0.01779   0.0026   0.3612   1.0000
   7.250   0.7746   0.02752   0.01839   0.0042   0.3437   1.0000
   7.500   0.7912   0.02809   0.01907   0.0059   0.3255   1.0000
   7.750   0.8076   0.02863   0.01970   0.0076   0.3067   1.0000
   8.000   0.8236   0.02914   0.02021   0.0094   0.2877   1.0000
   8.250   0.8365   0.02989   0.02108   0.0112   0.2667   1.0000
   8.500   0.8490   0.03062   0.02181   0.0132   0.2462   1.0000
   8.750   0.8591   0.03154   0.02278   0.0152   0.2247   1.0000
   9.000   0.8670   0.03256   0.02377   0.0173   0.2037   1.0000
   9.250   0.8722   0.03379   0.02499   0.0195   0.1828   1.0000
   9.500   0.8745   0.03520   0.02640   0.0217   0.1631   1.0000
   9.750   0.8734   0.03677   0.02788   0.0241   0.1466   1.0000
  10.000   0.8704   0.03857   0.02961   0.0263   0.1322   1.0000
  10.250   0.8679   0.04066   0.03168   0.0279   0.1191   1.0000
  10.500   0.8653   0.04301   0.03404   0.0289   0.1072   1.0000
  10.750   0.8639   0.04554   0.03662   0.0296   0.0975   1.0000
  11.000   0.8618   0.04822   0.03925   0.0300   0.0896   1.0000
  11.250   0.8608   0.05103   0.04214   0.0301   0.0822   1.0000
  11.500   0.8613   0.05387   0.04501   0.0303   0.0766   1.0000
  11.750   0.8611   0.05693   0.04821   0.0302   0.0712   1.0000
  12.000   0.8617   0.05969   0.05086   0.0300   0.0670   1.0000
  12.250   0.8580   0.06355   0.05502   0.0291   0.0628   1.0000
  12.500   0.8561   0.06720   0.05883   0.0284   0.0598   1.0000
  12.750   0.8559   0.07059   0.06229   0.0277   0.0573   1.0000
  13.000   0.8565   0.07393   0.06560   0.0271   0.0547   1.0000
  13.250   0.8461   0.07927   0.07124   0.0249   0.0536   1.0000
  13.500   0.8309   0.08556   0.07779   0.0217   0.0525   1.0000
  13.750   0.8130   0.09273   0.08519   0.0180   0.0520   1.0000
  14.000   0.7901   0.10137   0.09404   0.0132   0.0523   1.0000
  14.250   0.7618   0.11202   0.10484   0.0071   0.0528   1.0000
  14.500   0.7336   0.12374   0.11662   0.0007   0.0536   1.0000
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