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S8037 (16%) (s8037-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S8037 (16%) (s8037-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.53 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8037-il-1000000.txt
Download as CSV file: xf-s8037-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8037 (16%)                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.7750   0.09005   0.08751  -0.0552   1.0000   0.0081
 -16.500  -0.8148   0.07874   0.07599  -0.0618   1.0000   0.0082
 -16.250  -0.8369   0.07105   0.06814  -0.0664   1.0000   0.0081
 -16.000  -0.8504   0.06523   0.06219  -0.0698   1.0000   0.0080
 -15.750  -0.8723   0.05867   0.05549  -0.0733   1.0000   0.0081
 -15.500  -0.8828   0.05406   0.05074  -0.0755   1.0000   0.0080
 -15.250  -0.8997   0.04907   0.04560  -0.0775   1.0000   0.0081
 -15.000  -0.9061   0.04569   0.04217  -0.0786   1.0000   0.0083
 -14.750  -0.9203   0.04165   0.03796  -0.0792   1.0000   0.0083
 -14.500  -0.9255   0.03881   0.03499  -0.0792   1.0000   0.0082
 -14.250  -0.9251   0.03675   0.03288  -0.0789   1.0000   0.0083
 -14.000  -0.9284   0.03448   0.03052  -0.0781   1.0000   0.0084
 -13.750  -0.9279   0.03273   0.02871  -0.0770   1.0000   0.0085
 -13.500  -0.9328   0.03066   0.02651  -0.0752   1.0000   0.0085
 -13.250  -0.9304   0.02938   0.02516  -0.0733   1.0000   0.0086
 -13.000  -0.9281   0.02824   0.02397  -0.0711   1.0000   0.0088
 -12.750  -0.9268   0.02710   0.02275  -0.0685   1.0000   0.0088
 -12.500  -0.9261   0.02607   0.02164  -0.0654   1.0000   0.0089
 -12.250  -0.9240   0.02494   0.02043  -0.0624   0.9997   0.0089
 -12.000  -0.8921   0.02405   0.01946  -0.0648   0.9971   0.0095
 -11.750  -0.8635   0.02289   0.01819  -0.0666   0.9927   0.0096
 -11.500  -0.8394   0.02182   0.01704  -0.0672   0.9834   0.0098
 -11.250  -0.8138   0.02136   0.01649  -0.0674   0.9568   0.0101
 -10.750  -0.7096   0.01801   0.01291  -0.0810   0.9319   0.0110
 -10.500  -0.6572   0.01716   0.01191  -0.0871   0.9014   0.0114
 -10.250  -0.6395   0.01671   0.01124  -0.0856   0.8642   0.0118
 -10.000  -0.6275   0.01631   0.01070  -0.0829   0.8405   0.0120
  -9.750  -0.6142   0.01596   0.01023  -0.0803   0.8230   0.0123
  -9.500  -0.5988   0.01572   0.00987  -0.0780   0.8091   0.0126
  -9.250  -0.5890   0.01517   0.00921  -0.0748   0.7967   0.0130
  -9.000  -0.5782   0.01457   0.00854  -0.0718   0.7867   0.0133
  -8.750  -0.5615   0.01422   0.00811  -0.0698   0.7777   0.0137
  -8.500  -0.5428   0.01386   0.00772  -0.0682   0.7696   0.0143
  -8.250  -0.5237   0.01356   0.00734  -0.0666   0.7621   0.0147
  -8.000  -0.5030   0.01328   0.00701  -0.0652   0.7556   0.0152
  -7.750  -0.4823   0.01300   0.00667  -0.0639   0.7490   0.0157
  -7.500  -0.4657   0.01251   0.00612  -0.0619   0.7428   0.0166
  -7.250  -0.4444   0.01221   0.00580  -0.0606   0.7371   0.0174
  -7.000  -0.4226   0.01197   0.00551  -0.0595   0.7313   0.0181
  -6.750  -0.4003   0.01175   0.00523  -0.0584   0.7259   0.0188
  -6.500  -0.3797   0.01137   0.00483  -0.0570   0.7210   0.0199
  -6.250  -0.3577   0.01110   0.00453  -0.0558   0.7157   0.0211
  -6.000  -0.3345   0.01094   0.00431  -0.0549   0.7107   0.0225
  -5.750  -0.3119   0.01065   0.00402  -0.0538   0.7065   0.0244
  -5.500  -0.2884   0.01044   0.00379  -0.0529   0.7017   0.0268
  -5.000  -0.2445   0.00988   0.00330  -0.0506   0.6922   0.0473
  -4.750  -0.2221   0.00958   0.00311  -0.0495   0.6881   0.0671
  -4.500  -0.1990   0.00935   0.00293  -0.0486   0.6835   0.0857
  -4.250  -0.1765   0.00911   0.00277  -0.0476   0.6789   0.1098
  -4.000  -0.1539   0.00886   0.00261  -0.0465   0.6744   0.1396
  -3.750  -0.1319   0.00853   0.00245  -0.0454   0.6700   0.1801
  -3.500  -0.1111   0.00818   0.00229  -0.0441   0.6654   0.2362
  -3.250  -0.0911   0.00782   0.00214  -0.0426   0.6605   0.3025
  -3.000  -0.0707   0.00743   0.00200  -0.0412   0.6563   0.3725
  -2.750  -0.0504   0.00706   0.00190  -0.0397   0.6516   0.4452
  -2.500  -0.0292   0.00682   0.00182  -0.0383   0.6469   0.5053
  -2.250  -0.0065   0.00667   0.00178  -0.0372   0.6421   0.5487
  -2.000   0.0179   0.00656   0.00176  -0.0364   0.6375   0.5795
  -1.750   0.0432   0.00650   0.00172  -0.0358   0.6327   0.6007
  -1.500   0.0683   0.00648   0.00170  -0.0351   0.6277   0.6184
  -1.250   0.0940   0.00643   0.00168  -0.0346   0.6233   0.6367
  -1.000   0.1195   0.00639   0.00167  -0.0340   0.6182   0.6541
  -0.750   0.1449   0.00637   0.00165  -0.0334   0.6133   0.6673
  -0.500   0.1704   0.00635   0.00165  -0.0329   0.6084   0.6818
  -0.250   0.1959   0.00631   0.00165  -0.0323   0.6029   0.6981
   0.000   0.2208   0.00630   0.00164  -0.0316   0.5972   0.7132
   0.250   0.2466   0.00630   0.00165  -0.0311   0.5917   0.7258
   0.500   0.2723   0.00628   0.00165  -0.0306   0.5861   0.7386
   0.750   0.2972   0.00629   0.00166  -0.0299   0.5801   0.7514
   1.000   0.3229   0.00628   0.00168  -0.0294   0.5746   0.7641
   1.250   0.3483   0.00628   0.00169  -0.0288   0.5682   0.7771
   1.500   0.3727   0.00630   0.00171  -0.0281   0.5618   0.7909
   1.750   0.3984   0.00627   0.00174  -0.0276   0.5559   0.8053
   2.000   0.4230   0.00628   0.00177  -0.0268   0.5494   0.8212
   2.250   0.4479   0.00628   0.00182  -0.0262   0.5431   0.8393
   2.500   0.4736   0.00626   0.00186  -0.0257   0.5364   0.8592
   2.750   0.5002   0.00630   0.00192  -0.0254   0.5294   0.8803
   3.000   0.5343   0.00631   0.00201  -0.0268   0.5219   0.9007
   3.250   0.5757   0.00642   0.00212  -0.0299   0.5129   0.9177
   3.500   0.6218   0.00654   0.00224  -0.0340   0.5024   0.9297
   3.750   0.6710   0.00669   0.00237  -0.0389   0.4920   0.9350
   4.000   0.7101   0.00688   0.00252  -0.0415   0.4815   0.9430
   4.250   0.7474   0.00706   0.00268  -0.0437   0.4709   0.9484
   4.500   0.7768   0.00726   0.00285  -0.0440   0.4602   0.9570
   4.750   0.8082   0.00748   0.00302  -0.0449   0.4489   0.9627
   5.000   0.8336   0.00769   0.00321  -0.0445   0.4376   0.9717
   5.250   0.8691   0.00791   0.00339  -0.0464   0.4239   0.9744
   5.500   0.9019   0.00816   0.00358  -0.0477   0.4083   0.9785
   5.750   0.9295   0.00847   0.00382  -0.0479   0.3907   0.9838
   6.000   0.9644   0.00877   0.00402  -0.0498   0.3712   0.9858
   6.250   0.9986   0.00906   0.00424  -0.0515   0.3534   0.9884
   6.500   1.0309   0.00936   0.00447  -0.0529   0.3353   0.9915
   6.750   1.0624   0.00967   0.00472  -0.0541   0.3182   0.9941
   7.000   1.0966   0.00997   0.00493  -0.0559   0.2997   0.9960
   7.250   1.1297   0.01032   0.00519  -0.0576   0.2801   0.9983
   7.500   1.1605   0.01067   0.00546  -0.0588   0.2629   1.0000
   7.750   1.1729   0.01093   0.00568  -0.0559   0.2510   1.0000
   8.000   1.1842   0.01124   0.00594  -0.0529   0.2387   1.0000
   8.250   1.1944   0.01157   0.00622  -0.0497   0.2265   1.0000
   8.500   1.2033   0.01192   0.00652  -0.0462   0.2152   1.0000
   8.750   1.2109   0.01219   0.00677  -0.0424   0.2059   1.0000
   9.000   1.2140   0.01249   0.00704  -0.0378   0.1971   1.0000
   9.250   1.2195   0.01282   0.00735  -0.0337   0.1884   1.0000
   9.500   1.2276   0.01316   0.00768  -0.0302   0.1806   1.0000
   9.750   1.2348   0.01360   0.00809  -0.0267   0.1721   1.0000
  10.000   1.2448   0.01400   0.00848  -0.0238   0.1648   1.0000
  10.250   1.2518   0.01455   0.00900  -0.0206   0.1562   1.0000
  10.500   1.2626   0.01501   0.00947  -0.0181   0.1500   1.0000
  11.000   1.2812   0.01621   0.01066  -0.0130   0.1371   1.0000
  11.250   1.2889   0.01697   0.01140  -0.0105   0.1302   1.0000
  11.500   1.2998   0.01764   0.01209  -0.0086   0.1248   1.0000
  11.750   1.3083   0.01850   0.01294  -0.0065   0.1185   1.0000
  12.000   1.3178   0.01935   0.01380  -0.0047   0.1128   1.0000
  12.250   1.3270   0.02027   0.01473  -0.0029   0.1074   1.0000
  12.500   1.3350   0.02132   0.01578  -0.0012   0.1019   1.0000
  12.750   1.3447   0.02231   0.01678   0.0002   0.0971   1.0000
  13.000   1.3508   0.02357   0.01803   0.0019   0.0913   1.0000
  13.250   1.3606   0.02464   0.01913   0.0031   0.0876   1.0000
  13.500   1.3678   0.02590   0.02040   0.0045   0.0835   1.0000
  13.750   1.3731   0.02733   0.02185   0.0059   0.0791   1.0000
  14.000   1.3825   0.02851   0.02307   0.0069   0.0764   1.0000
  14.250   1.3877   0.03002   0.02457   0.0081   0.0723   1.0000
  14.500   1.3916   0.03167   0.02625   0.0094   0.0683   1.0000
  14.750   1.3993   0.03305   0.02768   0.0102   0.0657   1.0000
  15.000   1.4036   0.03475   0.02939   0.0112   0.0626   1.0000
  15.250   1.4062   0.03663   0.03129   0.0122   0.0586   1.0000
  15.500   1.4127   0.03824   0.03295   0.0129   0.0568   1.0000
  15.750   1.4141   0.04033   0.03503   0.0136   0.0525   1.0000
  16.000   1.4160   0.04244   0.03718   0.0143   0.0504   1.0000
  16.250   1.4221   0.04419   0.03898   0.0148   0.0483   1.0000
  16.500   1.4241   0.04638   0.04121   0.0152   0.0461   1.0000
  16.750   1.4258   0.04866   0.04354   0.0156   0.0450   1.0000
  17.000   1.4250   0.05123   0.04615   0.0160   0.0427   1.0000
  17.250   1.4290   0.05335   0.04833   0.0161   0.0416   1.0000
  17.500   1.4297   0.05584   0.05087   0.0163   0.0398   1.0000
  17.750   1.4296   0.05848   0.05356   0.0163   0.0387   1.0000
  18.000   1.4272   0.06142   0.05654   0.0163   0.0371   1.0000
  18.250   1.4255   0.06433   0.05952   0.0161   0.0358   1.0000
  18.500   1.4262   0.06701   0.06227   0.0159   0.0347   1.0000
  18.750   1.4247   0.06999   0.06534   0.0156   0.0344   1.0000
  19.000   1.4225   0.07309   0.06850   0.0152   0.0333   1.0000
  19.250   1.4168   0.07666   0.07211   0.0146   0.0318   1.0000
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