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S1014 (s1014-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S1014 (s1014-il)
Reynolds number: 200,000
Max Cl/Cd: 30.33 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1014-il-200000-n5.txt
Download as CSV file: xf-s1014-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1014                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.8752   0.13774   0.13360  -0.0204   1.0000   0.0281
 -19.500  -0.9217   0.12346   0.11904  -0.0290   1.0000   0.0282
 -19.250  -0.9478   0.11401   0.10938  -0.0347   1.0000   0.0284
 -19.000  -0.9677   0.10612   0.10129  -0.0394   1.0000   0.0286
 -18.750  -0.9824   0.09943   0.09445  -0.0434   1.0000   0.0289
 -18.500  -0.9918   0.09394   0.08888  -0.0465   1.0000   0.0293
 -18.250  -1.0010   0.08854   0.08337  -0.0495   1.0000   0.0296
 -18.000  -1.0095   0.08339   0.07811  -0.0523   1.0000   0.0301
 -17.750  -1.0166   0.07862   0.07322  -0.0548   1.0000   0.0306
 -17.500  -1.0226   0.07415   0.06863  -0.0570   1.0000   0.0310
 -17.250  -1.0274   0.07000   0.06435  -0.0588   1.0000   0.0316
 -16.750  -1.0335   0.06272   0.05674  -0.0618   0.9473   0.0330
 -16.500  -1.0294   0.05930   0.05305  -0.0641   0.9293   0.0339
 -16.250  -1.0270   0.05636   0.04999  -0.0652   0.9174   0.0346
 -16.000  -1.0248   0.05374   0.04726  -0.0659   0.9085   0.0354
 -15.750  -1.0220   0.05136   0.04475  -0.0661   0.9016   0.0363
 -15.500  -1.0180   0.04922   0.04247  -0.0661   0.8958   0.0374
 -15.250  -1.0128   0.04723   0.04032  -0.0660   0.8911   0.0385
 -15.000  -1.0060   0.04542   0.03833  -0.0657   0.8870   0.0397
 -14.750  -1.0004   0.04360   0.03643  -0.0652   0.8833   0.0408
 -14.500  -0.9944   0.04192   0.03468  -0.0647   0.8802   0.0419
 -14.000  -0.9763   0.03910   0.03164  -0.0636   0.8750   0.0449
 -13.750  -0.9649   0.03787   0.03026  -0.0630   0.8726   0.0468
 -13.500  -0.9562   0.03651   0.02887  -0.0622   0.8702   0.0483
 -13.250  -0.9458   0.03534   0.02765  -0.0614   0.8679   0.0499
 -13.000  -0.9341   0.03430   0.02651  -0.0606   0.8658   0.0519
 -12.750  -0.9206   0.03338   0.02546  -0.0598   0.8640   0.0542
 -12.500  -0.9089   0.03237   0.02439  -0.0588   0.8622   0.0562
 -12.250  -0.8967   0.03142   0.02340  -0.0579   0.8606   0.0584
 -12.000  -0.8819   0.03059   0.02251  -0.0572   0.8590   0.0611
 -11.750  -0.8652   0.02986   0.02165  -0.0565   0.8573   0.0638
 -11.500  -0.8521   0.02894   0.02074  -0.0556   0.8557   0.0664
 -11.250  -0.8367   0.02819   0.01996  -0.0548   0.8541   0.0695
 -11.000  -0.8198   0.02754   0.01923  -0.0540   0.8524   0.0729
 -10.750  -0.8043   0.02682   0.01847  -0.0531   0.8507   0.0760
 -10.500  -0.7889   0.02613   0.01777  -0.0521   0.8492   0.0797
 -10.250  -0.7714   0.02557   0.01713  -0.0513   0.8479   0.0837
 -10.000  -0.7545   0.02497   0.01649  -0.0504   0.8467   0.0875
  -9.750  -0.7385   0.02436   0.01588  -0.0494   0.8456   0.0920
  -9.500  -0.7200   0.02387   0.01532  -0.0486   0.8446   0.0970
  -9.250  -0.7027   0.02328   0.01475  -0.0478   0.8434   0.1018
  -9.000  -0.6845   0.02277   0.01423  -0.0470   0.8422   0.1077
  -8.750  -0.6659   0.02229   0.01373  -0.0462   0.8411   0.1137
  -8.500  -0.6483   0.02177   0.01324  -0.0454   0.8399   0.1206
  -8.250  -0.6293   0.02134   0.01278  -0.0446   0.8388   0.1275
  -8.000  -0.6116   0.02086   0.01234  -0.0436   0.8376   0.1357
  -7.750  -0.5933   0.02042   0.01191  -0.0427   0.8365   0.1446
  -7.500  -0.5750   0.02000   0.01151  -0.0418   0.8353   0.1551
  -7.250  -0.5579   0.01955   0.01110  -0.0407   0.8340   0.1665
  -7.000  -0.5408   0.01912   0.01071  -0.0395   0.8327   0.1793
  -6.750  -0.5239   0.01869   0.01033  -0.0382   0.8316   0.1946
  -6.500  -0.5078   0.01825   0.00996  -0.0369   0.8306   0.2122
  -6.250  -0.4925   0.01781   0.00960  -0.0353   0.8297   0.2334
  -6.000  -0.4788   0.01734   0.00924  -0.0335   0.8288   0.2574
  -5.500  -0.4575   0.01641   0.00862  -0.0290   0.8262   0.3202
  -5.250  -0.4529   0.01600   0.00841  -0.0255   0.8244   0.3576
  -5.000  -0.4503   0.01561   0.00825  -0.0215   0.8222   0.4007
  -4.750  -0.4460   0.01517   0.00809  -0.0177   0.8205   0.4545
  -4.500  -0.4392   0.01475   0.00804  -0.0141   0.8190   0.5214
  -4.250  -0.4093   0.01505   0.00891  -0.0136   0.8183   0.6091
  -4.000  -0.3512   0.01643   0.01048  -0.0173   0.8185   0.6550
  -3.750  -0.3353   0.01664   0.01066  -0.0151   0.8170   0.6781
  -3.250  -0.3139   0.01656   0.01043  -0.0095   0.8139   0.7113
  -3.000  -0.2889   0.01689   0.01071  -0.0088   0.8131   0.7198
  -2.750  -0.2724   0.01694   0.01068  -0.0069   0.8119   0.7305
  -2.500  -0.2437   0.01748   0.01124  -0.0070   0.8100   0.7359
  -2.250  -0.2307   0.01762   0.01132  -0.0048   0.8075   0.7459
  -2.000  -0.1980   0.01823   0.01196  -0.0052   0.8059   0.7501
  -1.750  -0.1743   0.01865   0.01237  -0.0043   0.8040   0.7582
  -1.500  -0.1469   0.01915   0.01288  -0.0038   0.8024   0.7653
  -1.250  -0.1140   0.01971   0.01345  -0.0041   0.8010   0.7704
  -1.000  -0.1001   0.01963   0.01333  -0.0019   0.7989   0.7792
  -0.750  -0.0683   0.01988   0.01357  -0.0023   0.7977   0.7811
  -0.500  -0.0386   0.02000   0.01370  -0.0025   0.7966   0.7831
  -0.250  -0.0104   0.02005   0.01373  -0.0024   0.7954   0.7854
   0.000   0.0000   0.02033   0.01405   0.0000   0.7894   0.7894
   0.250   0.0104   0.02005   0.01373   0.0024   0.7854   0.7954
   0.500   0.0386   0.02000   0.01370   0.0025   0.7831   0.7966
   0.750   0.0683   0.01988   0.01357   0.0023   0.7811   0.7977
   1.000   0.1001   0.01963   0.01332   0.0019   0.7792   0.7989
   1.250   0.1140   0.01971   0.01345   0.0041   0.7704   0.8010
   1.500   0.1469   0.01915   0.01288   0.0038   0.7653   0.8024
   1.750   0.1744   0.01865   0.01237   0.0043   0.7583   0.8040
   2.000   0.1979   0.01823   0.01196   0.0052   0.7502   0.8059
   2.250   0.2307   0.01761   0.01132   0.0048   0.7459   0.8075
   2.500   0.2437   0.01749   0.01124   0.0070   0.7360   0.8100
   2.750   0.2724   0.01694   0.01068   0.0069   0.7305   0.8119
   3.000   0.2889   0.01689   0.01072   0.0088   0.7198   0.8131
   3.250   0.3134   0.01657   0.01045   0.0096   0.7110   0.8139
   3.750   0.3351   0.01664   0.01066   0.0152   0.6779   0.8170
   4.000   0.3514   0.01643   0.01048   0.0173   0.6549   0.8185
   4.250   0.4094   0.01505   0.00890   0.0135   0.6088   0.8183
   4.500   0.4394   0.01475   0.00804   0.0141   0.5224   0.8190
   4.750   0.4461   0.01517   0.00808   0.0177   0.4547   0.8205
   5.000   0.4504   0.01561   0.00824   0.0215   0.4009   0.8222
   5.250   0.4530   0.01600   0.00841   0.0255   0.3575   0.8244
   5.500   0.4576   0.01640   0.00862   0.0290   0.3206   0.8262
   5.750   0.4666   0.01686   0.00890   0.0315   0.2869   0.8276
   6.000   0.4789   0.01734   0.00924   0.0335   0.2575   0.8288
   6.250   0.4926   0.01781   0.00960   0.0353   0.2331   0.8297
   6.500   0.5080   0.01824   0.00996   0.0369   0.2125   0.8307
   6.750   0.5240   0.01869   0.01033   0.0382   0.1943   0.8316
   7.000   0.5409   0.01911   0.01071   0.0395   0.1791   0.8327
   7.250   0.5581   0.01954   0.01110   0.0406   0.1664   0.8340
   7.500   0.5752   0.02000   0.01150   0.0418   0.1550   0.8354
   7.750   0.5935   0.02042   0.01190   0.0427   0.1446   0.8365
   8.000   0.6119   0.02085   0.01233   0.0436   0.1359   0.8376
   8.250   0.6295   0.02134   0.01278   0.0445   0.1275   0.8388
   8.500   0.6486   0.02177   0.01323   0.0453   0.1203   0.8399
   8.750   0.6661   0.02228   0.01372   0.0462   0.1136   0.8411
   9.000   0.6849   0.02276   0.01422   0.0469   0.1077   0.8423
   9.250   0.7030   0.02328   0.01474   0.0477   0.1018   0.8434
   9.500   0.7203   0.02386   0.01531   0.0485   0.0969   0.8446
   9.750   0.7388   0.02436   0.01587   0.0493   0.0920   0.8456
  10.000   0.7550   0.02496   0.01648   0.0503   0.0876   0.8467
  10.250   0.7719   0.02555   0.01711   0.0512   0.0836   0.8479
  10.500   0.7893   0.02613   0.01776   0.0521   0.0795   0.8492
  10.750   0.8047   0.02682   0.01846   0.0530   0.0759   0.8507
  11.000   0.8204   0.02752   0.01920   0.0539   0.0727   0.8525
  11.250   0.8373   0.02817   0.01994   0.0547   0.0694   0.8541
  11.500   0.8525   0.02893   0.02073   0.0555   0.0664   0.8558
  11.750   0.8661   0.02982   0.02162   0.0564   0.0636   0.8574
  12.000   0.8825   0.03057   0.02249   0.0571   0.0609   0.8590
  12.250   0.8974   0.03139   0.02338   0.0578   0.0583   0.8607
  12.500   0.9096   0.03235   0.02437   0.0587   0.0561   0.8623
  12.750   0.9215   0.03335   0.02543   0.0597   0.0540   0.8640
  13.000   0.9348   0.03428   0.02649   0.0605   0.0519   0.8659
  13.250   0.9466   0.03531   0.02762   0.0613   0.0499   0.8680
  13.500   0.9567   0.03650   0.02885   0.0622   0.0481   0.8702
  13.750   0.9658   0.03783   0.03023   0.0629   0.0467   0.8727
  14.000   0.9774   0.03905   0.03159   0.0635   0.0448   0.8752
  14.500   0.9954   0.04188   0.03463   0.0646   0.0418   0.8804
  14.750   1.0015   0.04354   0.03637   0.0651   0.0408   0.8835
  15.000   1.0072   0.04536   0.03827   0.0655   0.0397   0.8872
  15.250   1.0140   0.04717   0.04027   0.0658   0.0385   0.8914
  15.500   1.0193   0.04916   0.04240   0.0660   0.0374   0.8961
  15.750   1.0233   0.05131   0.04470   0.0660   0.0363   0.9019
  16.000   1.0265   0.05365   0.04716   0.0658   0.0355   0.9090
  16.250   1.0286   0.05629   0.04991   0.0651   0.0345   0.9182
  16.500   1.0313   0.05927   0.05304   0.0638   0.0338   0.9306
  16.750   1.0359   0.06266   0.05669   0.0615   0.0330   0.9495
  17.250   1.0293   0.06990   0.06424   0.0586   0.0315   1.0000
  17.500   1.0248   0.07400   0.06847   0.0568   0.0311   1.0000
  17.750   1.0188   0.07848   0.07307   0.0546   0.0305   1.0000
  18.000   1.0117   0.08325   0.07796   0.0522   0.0300   1.0000
  18.250   1.0031   0.08841   0.08323   0.0494   0.0296   1.0000
  18.500   0.9939   0.09379   0.08873   0.0464   0.0293   1.0000
  18.750   0.9848   0.09923   0.09423   0.0432   0.0289   1.0000
  19.000   0.9706   0.10581   0.10096   0.0394   0.0286   1.0000
  19.250   0.9490   0.11410   0.10947   0.0344   0.0283   1.0000
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