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S1016 (s1016-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S1016 (s1016-il)
Reynolds number: 500,000
Max Cl/Cd: 40.14 at α=10.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1016-il-500000.txt
Download as CSV file: xf-s1016-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1075   0.08686   0.08242  -0.0544   1.0000   0.0306
 -19.500  -1.1158   0.08213   0.07764  -0.0568   1.0000   0.0313
 -19.250  -1.1227   0.07784   0.07330  -0.0587   0.9690   0.0319
 -19.000  -1.1193   0.07331   0.06864  -0.0629   0.9533   0.0326
 -18.750  -1.1158   0.06907   0.06426  -0.0665   0.9433   0.0334
 -18.500  -1.1126   0.06537   0.06040  -0.0691   0.9347   0.0344
 -18.250  -1.1101   0.06221   0.05708  -0.0707   0.9275   0.0351
 -18.000  -1.1152   0.05861   0.05339  -0.0718   0.9222   0.0360
 -17.750  -1.1175   0.05544   0.05014  -0.0726   0.9180   0.0369
 -17.500  -1.1163   0.05277   0.04738  -0.0731   0.9142   0.0378
 -17.250  -1.1130   0.05045   0.04496  -0.0734   0.9110   0.0389
 -17.000  -1.1081   0.04833   0.04272  -0.0736   0.9082   0.0401
 -16.750  -1.1029   0.04627   0.04055  -0.0736   0.9058   0.0411
 -16.500  -1.1043   0.04372   0.03796  -0.0734   0.9034   0.0423
 -16.250  -1.1002   0.04177   0.03596  -0.0731   0.9010   0.0436
 -16.000  -1.0930   0.04015   0.03427  -0.0727   0.8989   0.0450
 -15.750  -1.0839   0.03872   0.03274  -0.0723   0.8971   0.0464
 -15.500  -1.0770   0.03717   0.03111  -0.0717   0.8953   0.0480
 -15.250  -1.0725   0.03551   0.02942  -0.0709   0.8936   0.0497
 -15.000  -1.0629   0.03427   0.02813  -0.0702   0.8920   0.0514
 -14.750  -1.0510   0.03319   0.02698  -0.0696   0.8909   0.0532
 -14.500  -1.0392   0.03212   0.02583  -0.0689   0.8897   0.0549
 -14.250  -1.0327   0.03073   0.02444  -0.0678   0.8884   0.0570
 -14.000  -1.0207   0.02977   0.02345  -0.0670   0.8871   0.0591
 -13.750  -1.0067   0.02894   0.02257  -0.0663   0.8859   0.0613
 -13.500  -0.9936   0.02807   0.02164  -0.0654   0.8847   0.0635
 -13.250  -0.9839   0.02703   0.02060  -0.0642   0.8835   0.0661
 -13.000  -0.9693   0.02630   0.01985  -0.0634   0.8825   0.0688
 -12.750  -0.9528   0.02570   0.01918  -0.0626   0.8814   0.0711
 -12.500  -0.9414   0.02482   0.01829  -0.0613   0.8804   0.0742
 -12.250  -0.9272   0.02413   0.01759  -0.0603   0.8794   0.0773
 -12.000  -0.9099   0.02362   0.01704  -0.0595   0.8784   0.0805
 -11.750  -0.8958   0.02297   0.01636  -0.0583   0.8772   0.0841
 -11.500  -0.8813   0.02237   0.01577  -0.0572   0.8761   0.0880
 -11.250  -0.8626   0.02194   0.01530  -0.0565   0.8754   0.0919
 -11.000  -0.8468   0.02133   0.01470  -0.0555   0.8747   0.0963
 -10.750  -0.8300   0.02079   0.01419  -0.0546   0.8740   0.1009
 -10.500  -0.8100   0.02043   0.01378  -0.0540   0.8733   0.1052
 -10.250  -0.7949   0.01982   0.01321  -0.0529   0.8725   0.1107
 -10.000  -0.7759   0.01941   0.01281  -0.0521   0.8717   0.1161
  -9.750  -0.7575   0.01899   0.01238  -0.0513   0.8709   0.1216
  -9.500  -0.7399   0.01854   0.01197  -0.0503   0.8701   0.1282
  -9.250  -0.7200   0.01821   0.01162  -0.0496   0.8693   0.1342
  -9.000  -0.7028   0.01776   0.01122  -0.0485   0.8683   0.1416
  -8.750  -0.6827   0.01745   0.01090  -0.0478   0.8672   0.1488
  -8.500  -0.6654   0.01703   0.01054  -0.0467   0.8663   0.1574
  -8.250  -0.6459   0.01672   0.01024  -0.0458   0.8655   0.1659
  -8.000  -0.6273   0.01637   0.00994  -0.0448   0.8647   0.1756
  -7.750  -0.6090   0.01603   0.00965  -0.0438   0.8639   0.1865
  -7.500  -0.5901   0.01573   0.00938  -0.0428   0.8631   0.1983
  -7.250  -0.5717   0.01544   0.00913  -0.0417   0.8621   0.2112
  -7.000  -0.5549   0.01513   0.00888  -0.0402   0.8610   0.2263
  -6.750  -0.5380   0.01485   0.00868  -0.0388   0.8601   0.2429
  -6.500  -0.5213   0.01460   0.00852  -0.0374   0.8591   0.2617
  -6.250  -0.5045   0.01424   0.00826  -0.0361   0.8582   0.2824
  -6.000  -0.4890   0.01387   0.00801  -0.0346   0.8567   0.3060
  -5.500  -0.4629   0.01317   0.00758  -0.0306   0.8537   0.3608
  -5.250  -0.4546   0.01286   0.00740  -0.0275   0.8515   0.3904
  -5.000  -0.4502   0.01264   0.00731  -0.0236   0.8495   0.4216
  -4.750  -0.4494   0.01242   0.00723  -0.0187   0.8472   0.4553
  -4.500  -0.4445   0.01215   0.00713  -0.0145   0.8454   0.4945
  -4.250  -0.4380   0.01189   0.00706  -0.0105   0.8436   0.5397
  -4.000  -0.4300   0.01169   0.00711  -0.0071   0.8413   0.5907
  -3.750  -0.4178   0.01156   0.00727  -0.0044   0.8378   0.6433
  -3.500  -0.3974   0.01170   0.00766  -0.0028   0.8352   0.6890
  -3.250  -0.3717   0.01197   0.00799  -0.0022   0.8332   0.7162
  -3.000  -0.3458   0.01215   0.00816  -0.0017   0.8314   0.7323
  -2.750  -0.3199   0.01228   0.00823  -0.0011   0.8298   0.7446
  -2.500  -0.2907   0.01248   0.00841  -0.0010   0.8284   0.7527
  -2.250  -0.2638   0.01263   0.00851  -0.0006   0.8269   0.7603
  -2.000  -0.2354   0.01300   0.00890  -0.0005   0.8243   0.7650
  -1.750  -0.2135   0.01328   0.00918   0.0004   0.8190   0.7715
  -1.500  -0.1854   0.01339   0.00927   0.0006   0.8161   0.7766
  -1.250  -0.1519   0.01352   0.00941   0.0001   0.8141   0.7797
  -1.000  -0.1185   0.01359   0.00946  -0.0003   0.8121   0.7835
  -0.750  -0.0887   0.01352   0.00935  -0.0002   0.8101   0.7886
  -0.500  -0.0633   0.01359   0.00941   0.0004   0.8061   0.7929
  -0.250  -0.0334   0.01372   0.00958   0.0004   0.8011   0.7952
   0.000   0.0000   0.01372   0.00959   0.0000   0.7978   0.7978
   0.250   0.0335   0.01371   0.00957  -0.0004   0.7952   0.8011
   0.500   0.0634   0.01358   0.00940  -0.0004   0.7929   0.8061
   0.750   0.0888   0.01352   0.00935   0.0002   0.7887   0.8101
   1.000   0.1185   0.01357   0.00945   0.0003   0.7834   0.8121
   1.250   0.1518   0.01353   0.00942  -0.0001   0.7798   0.8141
   1.500   0.1853   0.01339   0.00927  -0.0006   0.7767   0.8161
   1.750   0.2135   0.01328   0.00918  -0.0004   0.7716   0.8191
   2.000   0.2354   0.01300   0.00890   0.0005   0.7649   0.8244
   2.250   0.2638   0.01262   0.00850   0.0006   0.7602   0.8269
   2.500   0.2907   0.01248   0.00841   0.0011   0.7527   0.8284
   2.750   0.3199   0.01228   0.00823   0.0011   0.7447   0.8298
   3.000   0.3458   0.01216   0.00816   0.0017   0.7325   0.8314
   3.250   0.3717   0.01197   0.00799   0.0022   0.7159   0.8332
   3.500   0.3974   0.01170   0.00766   0.0028   0.6891   0.8352
   3.750   0.4178   0.01156   0.00727   0.0044   0.6433   0.8378
   4.000   0.4300   0.01169   0.00711   0.0071   0.5909   0.8413
   4.250   0.4381   0.01189   0.00706   0.0105   0.5399   0.8436
   4.500   0.4446   0.01215   0.00713   0.0145   0.4946   0.8454
   5.000   0.4505   0.01263   0.00731   0.0235   0.4217   0.8495
   5.250   0.4545   0.01286   0.00740   0.0276   0.3900   0.8515
   5.500   0.4631   0.01317   0.00758   0.0305   0.3609   0.8537
   5.750   0.4742   0.01354   0.00780   0.0329   0.3322   0.8554
   6.000   0.4892   0.01386   0.00801   0.0346   0.3061   0.8567
   6.250   0.5046   0.01424   0.00826   0.0361   0.2821   0.8582
   6.500   0.5215   0.01460   0.00851   0.0374   0.2610   0.8591
   6.750   0.5382   0.01484   0.00868   0.0388   0.2430   0.8601
   7.000   0.5551   0.01512   0.00888   0.0402   0.2262   0.8610
   7.250   0.5720   0.01544   0.00913   0.0416   0.2114   0.8621
   7.500   0.5903   0.01573   0.00938   0.0428   0.1982   0.8631
   7.750   0.6093   0.01603   0.00964   0.0437   0.1865   0.8639
   8.000   0.6277   0.01637   0.00993   0.0448   0.1759   0.8647
   8.250   0.6462   0.01672   0.01023   0.0458   0.1657   0.8655
   8.500   0.6658   0.01703   0.01053   0.0466   0.1574   0.8663
   8.750   0.6830   0.01745   0.01090   0.0477   0.1486   0.8672
   9.000   0.7031   0.01775   0.01121   0.0485   0.1416   0.8683
   9.250   0.7203   0.01821   0.01161   0.0496   0.1341   0.8693
   9.500   0.7404   0.01853   0.01196   0.0502   0.1282   0.8701
   9.750   0.7580   0.01898   0.01237   0.0512   0.1215   0.8709
  10.000   0.7765   0.01940   0.01279   0.0520   0.1159   0.8717
  10.250   0.7952   0.01981   0.01321   0.0528   0.1106   0.8725
  10.500   0.8107   0.02041   0.01376   0.0539   0.1051   0.8733
  10.750   0.8307   0.02077   0.01417   0.0545   0.1009   0.8740
  11.000   0.8472   0.02132   0.01469   0.0555   0.0961   0.8747
  11.250   0.8633   0.02192   0.01529   0.0564   0.0918   0.8754
  11.500   0.8819   0.02236   0.01576   0.0571   0.0878   0.8761
  11.750   0.8961   0.02298   0.01636   0.0583   0.0838   0.8772
  12.000   0.9107   0.02360   0.01701   0.0594   0.0805   0.8785
  12.250   0.9278   0.02412   0.01758   0.0602   0.0773   0.8795
  12.500   0.9421   0.02481   0.01827   0.0612   0.0741   0.8804
  12.750   0.9536   0.02568   0.01916   0.0625   0.0711   0.8815
  13.000   0.9702   0.02628   0.01982   0.0632   0.0686   0.8825
  13.250   0.9847   0.02701   0.02058   0.0641   0.0661   0.8836
  13.500   0.9946   0.02803   0.02160   0.0653   0.0635   0.8848
  13.750   1.0070   0.02895   0.02257   0.0662   0.0614   0.8860
  14.000   1.0218   0.02972   0.02340   0.0669   0.0590   0.8872
  14.250   1.0336   0.03071   0.02442   0.0677   0.0571   0.8884
  14.500   1.0398   0.03211   0.02582   0.0689   0.0547   0.8897
  14.750   1.0519   0.03316   0.02695   0.0695   0.0531   0.8909
  15.000   1.0643   0.03421   0.02806   0.0701   0.0512   0.8921
  15.250   1.0737   0.03544   0.02935   0.0707   0.0496   0.8937
  15.500   1.0785   0.03708   0.03101   0.0716   0.0480   0.8954
  15.750   1.0849   0.03867   0.03268   0.0722   0.0465   0.8972
  16.000   1.0946   0.04004   0.03416   0.0726   0.0450   0.8991
  16.250   1.1016   0.04168   0.03587   0.0730   0.0436   0.9012
  16.500   1.1061   0.04360   0.03784   0.0733   0.0424   0.9036
  16.750   1.1043   0.04617   0.04044   0.0735   0.0410   0.9061
  17.000   1.1103   0.04817   0.04255   0.0735   0.0400   0.9084
  17.250   1.1146   0.05033   0.04484   0.0733   0.0389   0.9113
  17.500   1.1182   0.05262   0.04723   0.0730   0.0377   0.9146
  17.750   1.1193   0.05530   0.05000   0.0725   0.0370   0.9185
  18.000   1.1170   0.05847   0.05324   0.0717   0.0359   0.9229
  18.250   1.1125   0.06204   0.05691   0.0706   0.0350   0.9285
  18.500   1.1152   0.06525   0.06028   0.0689   0.0344   0.9359
  18.750   1.1195   0.06892   0.06411   0.0661   0.0335   0.9449
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