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S1016 (s1016-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S1016 (s1016-il)
Reynolds number: 200,000
Max Cl/Cd: 30.19 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1016-il-200000-n5.txt
Download as CSV file: xf-s1016-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1016                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.9721   0.10514   0.10004  -0.0471   1.0000   0.0365
 -19.250  -0.9815   0.09968   0.09448  -0.0502   1.0000   0.0371
 -19.000  -0.9902   0.09443   0.08912  -0.0531   1.0000   0.0378
 -18.750  -0.9987   0.08933   0.08389  -0.0559   1.0000   0.0385
 -18.500  -1.0062   0.08447   0.07889  -0.0584   1.0000   0.0394
 -18.250  -1.0123   0.07993   0.07419  -0.0607   1.0000   0.0403
 -18.000  -1.0168   0.07577   0.06990  -0.0627   1.0000   0.0411
 -17.500  -1.0240   0.06808   0.06205  -0.0666   0.9575   0.0427
 -17.250  -1.0214   0.06440   0.05824  -0.0692   0.9472   0.0440
 -16.750  -1.0142   0.05821   0.05169  -0.0726   0.9331   0.0467
 -16.500  -1.0116   0.05541   0.04877  -0.0736   0.9279   0.0479
 -16.250  -1.0095   0.05273   0.04602  -0.0744   0.9236   0.0491
 -16.000  -1.0057   0.05040   0.04358  -0.0748   0.9198   0.0505
 -15.750  -1.0000   0.04833   0.04139  -0.0750   0.9164   0.0522
 -15.500  -0.9930   0.04645   0.03936  -0.0751   0.9134   0.0539
 -15.250  -0.9881   0.04450   0.03734  -0.0749   0.9107   0.0555
 -14.750  -0.9742   0.04114   0.03382  -0.0744   0.9062   0.0592
 -14.500  -0.9643   0.03976   0.03232  -0.0740   0.9039   0.0615
 -14.250  -0.9556   0.03834   0.03083  -0.0735   0.9014   0.0635
 -14.000  -0.9475   0.03697   0.02942  -0.0728   0.8992   0.0656
 -13.750  -0.9372   0.03577   0.02815  -0.0721   0.8972   0.0680
 -13.500  -0.9247   0.03476   0.02701  -0.0715   0.8955   0.0708
 -13.250  -0.9148   0.03364   0.02585  -0.0705   0.8939   0.0733
 -12.750  -0.8910   0.03171   0.02381  -0.0688   0.8910   0.0791
 -12.500  -0.8761   0.03090   0.02290  -0.0682   0.8896   0.0824
 -12.250  -0.8644   0.02994   0.02195  -0.0673   0.8882   0.0855
 -12.000  -0.8501   0.02915   0.02111  -0.0665   0.8868   0.0891
 -11.750  -0.8335   0.02849   0.02036  -0.0658   0.8855   0.0931
 -11.500  -0.8205   0.02766   0.01955  -0.0648   0.8841   0.0967
 -11.250  -0.8052   0.02699   0.01883  -0.0639   0.8829   0.1010
 -11.000  -0.7877   0.02643   0.01819  -0.0632   0.8817   0.1055
 -10.750  -0.7737   0.02572   0.01751  -0.0621   0.8805   0.1099
 -10.500  -0.7573   0.02515   0.01690  -0.0612   0.8793   0.1151
 -10.250  -0.7405   0.02463   0.01632  -0.0602   0.8779   0.1202
 -10.000  -0.7253   0.02405   0.01575  -0.0591   0.8766   0.1256
  -9.750  -0.7071   0.02361   0.01525  -0.0582   0.8756   0.1317
  -9.500  -0.6904   0.02305   0.01473  -0.0574   0.8746   0.1381
  -9.250  -0.6720   0.02259   0.01425  -0.0566   0.8735   0.1452
  -9.000  -0.6543   0.02212   0.01379  -0.0558   0.8724   0.1519
  -8.750  -0.6358   0.02169   0.01337  -0.0550   0.8713   0.1599
  -8.500  -0.6180   0.02125   0.01296  -0.0541   0.8702   0.1684
  -8.250  -0.5991   0.02087   0.01258  -0.0533   0.8691   0.1781
  -8.000  -0.5820   0.02044   0.01220  -0.0523   0.8678   0.1879
  -7.750  -0.5639   0.02008   0.01185  -0.0512   0.8663   0.1987
  -7.500  -0.5460   0.01971   0.01150  -0.0502   0.8649   0.2113
  -7.250  -0.5293   0.01933   0.01117  -0.0489   0.8638   0.2243
  -7.000  -0.5124   0.01896   0.01087  -0.0477   0.8627   0.2387
  -6.750  -0.4959   0.01860   0.01057  -0.0463   0.8616   0.2548
  -6.500  -0.4799   0.01826   0.01028  -0.0449   0.8605   0.2722
  -6.250  -0.4650   0.01792   0.01001  -0.0431   0.8593   0.2918
  -6.000  -0.4500   0.01758   0.00979  -0.0416   0.8574   0.3143
  -5.750  -0.4370   0.01724   0.00957  -0.0397   0.8558   0.3376
  -5.500  -0.4252   0.01693   0.00938  -0.0375   0.8537   0.3633
  -5.250  -0.4164   0.01662   0.00921  -0.0346   0.8512   0.3909
  -4.750  -0.4055   0.01616   0.00903  -0.0272   0.8468   0.4518
  -4.500  -0.4004   0.01593   0.00896  -0.0231   0.8446   0.4879
  -4.250  -0.3897   0.01572   0.00895  -0.0200   0.8431   0.5276
  -4.000  -0.3757   0.01568   0.00917  -0.0175   0.8405   0.5717
  -3.750  -0.3439   0.01593   0.00972  -0.0179   0.8388   0.6196
  -3.500  -0.2735   0.01672   0.01067  -0.0246   0.8400   0.6545
  -3.250  -0.2310   0.01751   0.01151  -0.0265   0.8389   0.6725
  -3.000  -0.2067   0.01803   0.01206  -0.0255   0.8363   0.6872
  -2.750  -0.1939   0.01831   0.01233  -0.0227   0.8332   0.7015
  -2.500  -0.1920   0.01834   0.01234  -0.0180   0.8298   0.7171
  -2.250  -0.1840   0.01833   0.01229  -0.0143   0.8274   0.7308
  -2.000  -0.1839   0.01844   0.01236  -0.0095   0.8229   0.7438
  -1.750  -0.1634   0.01893   0.01286  -0.0079   0.8184   0.7498
  -1.500  -0.1533   0.01891   0.01280  -0.0047   0.8144   0.7601
  -1.250  -0.1187   0.01926   0.01314  -0.0054   0.8125   0.7641
  -1.000  -0.1056   0.01906   0.01287  -0.0026   0.8100   0.7749
  -0.750  -0.0653   0.01939   0.01321  -0.0042   0.8088   0.7775
  -0.500  -0.0517   0.01993   0.01381  -0.0015   0.8004   0.7819
  -0.250  -0.0409   0.01963   0.01346   0.0016   0.7958   0.7918
   0.000   0.0000   0.01970   0.01353   0.0000   0.7938   0.7938
   0.250   0.0409   0.01963   0.01346  -0.0016   0.7918   0.7958
   0.500   0.0518   0.01993   0.01380   0.0015   0.7819   0.8004
   0.750   0.0654   0.01938   0.01321   0.0042   0.7775   0.8088
   1.000   0.1055   0.01906   0.01287   0.0026   0.7749   0.8100
   1.250   0.1188   0.01925   0.01314   0.0054   0.7641   0.8125
   1.500   0.1531   0.01892   0.01281   0.0047   0.7601   0.8144
   1.750   0.1634   0.01893   0.01286   0.0079   0.7498   0.8184
   2.000   0.1837   0.01844   0.01237   0.0095   0.7439   0.8229
   2.250   0.1840   0.01833   0.01228   0.0143   0.7308   0.8273
   2.500   0.1920   0.01834   0.01233   0.0180   0.7170   0.8298
   2.750   0.1941   0.01831   0.01234   0.0227   0.7017   0.8332
   3.000   0.2067   0.01804   0.01207   0.0255   0.6875   0.8363
   3.250   0.2309   0.01751   0.01152   0.0265   0.6728   0.8389
   3.500   0.2727   0.01673   0.01069   0.0247   0.6549   0.8401
   3.750   0.3455   0.01592   0.00969   0.0177   0.6179   0.8386
   4.000   0.3758   0.01568   0.00917   0.0175   0.5716   0.8406
   4.250   0.3899   0.01571   0.00895   0.0199   0.5280   0.8431
   4.500   0.4002   0.01593   0.00896   0.0231   0.4872   0.8446
   4.750   0.4057   0.01616   0.00902   0.0272   0.4519   0.8468
   5.250   0.4163   0.01662   0.00920   0.0347   0.3904   0.8512
   5.500   0.4255   0.01693   0.00938   0.0375   0.3636   0.8538
   5.750   0.4371   0.01724   0.00957   0.0397   0.3375   0.8558
   6.000   0.4502   0.01758   0.00978   0.0416   0.3143   0.8574
   6.250   0.4652   0.01791   0.01001   0.0431   0.2917   0.8593
   6.500   0.4802   0.01825   0.01028   0.0448   0.2724   0.8605
   6.750   0.4961   0.01860   0.01056   0.0463   0.2545   0.8616
   7.000   0.5126   0.01896   0.01086   0.0476   0.2385   0.8627
   7.250   0.5296   0.01932   0.01117   0.0489   0.2243   0.8638
   7.500   0.5464   0.01971   0.01150   0.0501   0.2110   0.8650
   7.750   0.5643   0.02007   0.01184   0.0512   0.1988   0.8664
   8.000   0.5823   0.02044   0.01219   0.0522   0.1879   0.8679
   8.250   0.5995   0.02087   0.01257   0.0532   0.1780   0.8691
   8.500   0.6185   0.02124   0.01294   0.0540   0.1686   0.8702
   8.750   0.6362   0.02168   0.01336   0.0549   0.1601   0.8713
   9.000   0.6546   0.02211   0.01379   0.0557   0.1518   0.8724
   9.250   0.6725   0.02258   0.01425   0.0565   0.1449   0.8735
   9.500   0.6909   0.02304   0.01472   0.0573   0.1379   0.8746
   9.750   0.7077   0.02360   0.01524   0.0581   0.1317   0.8756
  10.000   0.7258   0.02404   0.01574   0.0590   0.1256   0.8766
  10.250   0.7411   0.02462   0.01631   0.0601   0.1202   0.8779
  10.500   0.7579   0.02514   0.01689   0.0611   0.1149   0.8793
  10.750   0.7744   0.02571   0.01749   0.0620   0.1099   0.8805
  11.000   0.7884   0.02642   0.01817   0.0631   0.1054   0.8817
  11.250   0.8059   0.02697   0.01882   0.0638   0.1008   0.8829
  11.500   0.8212   0.02765   0.01953   0.0647   0.0966   0.8842
  11.750   0.8343   0.02847   0.02034   0.0657   0.0929   0.8855
  12.000   0.8509   0.02913   0.02109   0.0663   0.0891   0.8868
  12.250   0.8652   0.02992   0.02193   0.0672   0.0854   0.8882
  12.500   0.8768   0.03088   0.02289   0.0681   0.0822   0.8897
  12.750   0.8920   0.03169   0.02379   0.0687   0.0791   0.8911
  13.250   0.9157   0.03362   0.02582   0.0704   0.0732   0.8939
  13.500   0.9258   0.03473   0.02698   0.0713   0.0708   0.8955
  13.750   0.9383   0.03575   0.02812   0.0720   0.0680   0.8972
  14.000   0.9486   0.03694   0.02938   0.0726   0.0655   0.8992
  14.250   0.9567   0.03831   0.03079   0.0733   0.0634   0.9016
  14.500   0.9657   0.03971   0.03227   0.0739   0.0613   0.9040
  14.750   0.9755   0.04111   0.03378   0.0742   0.0591   0.9063
  15.250   0.9895   0.04445   0.03728   0.0747   0.0554   0.9109
  15.500   0.9947   0.04639   0.03929   0.0749   0.0539   0.9136
  15.750   1.0020   0.04824   0.04130   0.0748   0.0521   0.9166
  16.000   1.0075   0.05033   0.04351   0.0746   0.0505   0.9201
  16.250   1.0114   0.05266   0.04594   0.0742   0.0491   0.9239
  16.500   1.0138   0.05532   0.04868   0.0734   0.0478   0.9283
  16.750   1.0165   0.05812   0.05161   0.0724   0.0467   0.9337
  17.250   1.0242   0.06432   0.05816   0.0689   0.0439   0.9482
  17.500   1.0270   0.06799   0.06197   0.0662   0.0428   0.9593
  18.000   1.0194   0.07564   0.06976   0.0625   0.0411   1.0000
  18.250   1.0148   0.07984   0.07410   0.0605   0.0402   1.0000
  18.500   1.0092   0.08430   0.07871   0.0582   0.0394   1.0000
  18.750   1.0019   0.08913   0.08368   0.0557   0.0386   1.0000
  19.000   0.9934   0.09423   0.08891   0.0529   0.0378   1.0000
  19.250   0.9842   0.09959   0.09438   0.0499   0.0371   1.0000
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