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S8052 (11.88%) (s8052-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S8052 (11.88%) (s8052-il)
Reynolds number: 500,000
Max Cl/Cd: 73.47 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8052-il-500000-n5.txt
Download as CSV file: xf-s8052-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8052 (11.88%)                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.6647   0.08878   0.08633  -0.0240   1.0000   0.0079
 -12.500  -0.6467   0.08897   0.08657  -0.0241   1.0000   0.0081
 -12.250  -0.7861   0.05182   0.04862  -0.0502   1.0000   0.0074
 -11.750  -0.8137   0.04316   0.03961  -0.0543   1.0000   0.0075
 -11.500  -0.8297   0.03952   0.03575  -0.0543   1.0000   0.0075
 -11.250  -0.8407   0.03680   0.03285  -0.0529   1.0000   0.0075
 -11.000  -0.8512   0.03442   0.03027  -0.0502   1.0000   0.0075
 -10.750  -0.8579   0.03199   0.02762  -0.0473   1.0000   0.0076
 -10.500  -0.8530   0.03008   0.02552  -0.0454   1.0000   0.0076
 -10.250  -0.8458   0.02817   0.02340  -0.0436   1.0000   0.0077
 -10.000  -0.8316   0.02650   0.02153  -0.0427   0.9887   0.0077
  -9.750  -0.8037   0.02464   0.01947  -0.0446   0.9598   0.0079
  -9.500  -0.7773   0.02318   0.01782  -0.0456   0.9376   0.0080
  -9.250  -0.7570   0.02206   0.01651  -0.0449   0.9158   0.0081
  -9.000  -0.7383   0.02108   0.01536  -0.0437   0.8980   0.0082
  -8.750  -0.7190   0.02020   0.01430  -0.0426   0.8838   0.0084
  -8.500  -0.6988   0.01934   0.01330  -0.0416   0.8719   0.0085
  -8.250  -0.6779   0.01855   0.01237  -0.0406   0.8615   0.0087
  -7.750  -0.6343   0.01710   0.01067  -0.0389   0.8427   0.0091
  -7.500  -0.6118   0.01645   0.00991  -0.0381   0.8348   0.0092
  -7.250  -0.5886   0.01583   0.00918  -0.0375   0.8273   0.0095
  -7.000  -0.5652   0.01527   0.00852  -0.0368   0.8204   0.0097
  -6.750  -0.5412   0.01473   0.00790  -0.0362   0.8134   0.0099
  -6.500  -0.5170   0.01425   0.00733  -0.0357   0.8070   0.0101
  -6.250  -0.4927   0.01373   0.00673  -0.0351   0.8010   0.0103
  -6.000  -0.4684   0.01320   0.00614  -0.0346   0.7950   0.0107
  -5.750  -0.4432   0.01282   0.00570  -0.0342   0.7899   0.0112
  -5.500  -0.4173   0.01246   0.00531  -0.0339   0.7846   0.0119
  -5.250  -0.3913   0.01215   0.00493  -0.0336   0.7795   0.0127
  -4.750  -0.3389   0.01152   0.00420  -0.0330   0.7704   0.0144
  -4.500  -0.3124   0.01123   0.00388  -0.0327   0.7656   0.0163
  -4.250  -0.2860   0.01096   0.00358  -0.0324   0.7613   0.0203
  -4.000  -0.2596   0.01064   0.00331  -0.0322   0.7569   0.0328
  -3.750  -0.2333   0.01031   0.00307  -0.0320   0.7521   0.0535
  -3.500  -0.2071   0.00999   0.00284  -0.0317   0.7474   0.0822
  -3.250  -0.1815   0.00959   0.00262  -0.0315   0.7431   0.1291
  -3.000  -0.1557   0.00916   0.00244  -0.0313   0.7382   0.1878
  -2.750  -0.1301   0.00875   0.00226  -0.0311   0.7336   0.2549
  -2.500  -0.1049   0.00831   0.00209  -0.0308   0.7295   0.3359
  -2.250  -0.0796   0.00785   0.00195  -0.0305   0.7247   0.4216
  -2.000  -0.0539   0.00750   0.00184  -0.0302   0.7194   0.4931
  -1.750  -0.0280   0.00726   0.00178  -0.0298   0.7145   0.5589
  -1.500  -0.0009   0.00712   0.00176  -0.0296   0.7092   0.6029
  -1.250   0.0266   0.00705   0.00174  -0.0294   0.7036   0.6324
  -1.000   0.0543   0.00702   0.00172  -0.0292   0.6981   0.6540
  -0.750   0.0823   0.00698   0.00170  -0.0291   0.6912   0.6716
  -0.500   0.1101   0.00697   0.00168  -0.0289   0.6842   0.6871
  -0.250   0.1381   0.00695   0.00167  -0.0289   0.6759   0.7008
   0.000   0.1661   0.00696   0.00165  -0.0287   0.6675   0.7130
   0.250   0.1940   0.00695   0.00165  -0.0286   0.6578   0.7241
   0.500   0.2219   0.00695   0.00165  -0.0285   0.6473   0.7340
   0.750   0.2498   0.00697   0.00164  -0.0284   0.6358   0.7439
   1.000   0.2775   0.00698   0.00165  -0.0283   0.6226   0.7534
   1.250   0.3050   0.00701   0.00165  -0.0281   0.6046   0.7626
   1.500   0.3320   0.00708   0.00166  -0.0278   0.5824   0.7726
   1.750   0.3588   0.00717   0.00170  -0.0275   0.5612   0.7821
   2.000   0.3855   0.00728   0.00175  -0.0273   0.5391   0.7917
   2.250   0.4118   0.00742   0.00182  -0.0269   0.5131   0.8008
   2.500   0.4381   0.00758   0.00190  -0.0266   0.4878   0.8086
   2.750   0.4643   0.00775   0.00201  -0.0263   0.4619   0.8166
   3.000   0.4900   0.00796   0.00213  -0.0260   0.4328   0.8246
   3.250   0.5156   0.00820   0.00226  -0.0256   0.4023   0.8333
   3.500   0.5410   0.00841   0.00242  -0.0252   0.3759   0.8420
   3.750   0.5662   0.00865   0.00258  -0.0247   0.3486   0.8520
   4.000   0.5908   0.00892   0.00275  -0.0242   0.3194   0.8631
   4.250   0.6149   0.00920   0.00295  -0.0236   0.2901   0.8748
   4.500   0.6389   0.00948   0.00316  -0.0229   0.2637   0.8887
   4.750   0.6632   0.00971   0.00336  -0.0223   0.2430   0.9055
   5.000   0.6888   0.00994   0.00357  -0.0219   0.2262   0.9251
   5.250   0.7186   0.01023   0.00382  -0.0225   0.2078   0.9454
   5.500   0.7530   0.01054   0.00407  -0.0242   0.1913   0.9660
   5.750   0.7872   0.01085   0.00433  -0.0259   0.1764   0.9878
   6.000   0.8172   0.01118   0.00460  -0.0267   0.1623   1.0000
   6.250   0.8405   0.01148   0.00485  -0.0261   0.1508   1.0000
   6.500   0.8641   0.01177   0.00511  -0.0255   0.1406   1.0000
   6.750   0.8875   0.01208   0.00539  -0.0248   0.1311   1.0000
   7.000   0.9107   0.01242   0.00569  -0.0242   0.1223   1.0000
   7.250   0.9343   0.01272   0.00599  -0.0236   0.1139   1.0000
   7.500   0.9573   0.01308   0.00631  -0.0230   0.1051   1.0000
   7.750   0.9801   0.01344   0.00665  -0.0223   0.0967   1.0000
   8.000   1.0030   0.01379   0.00701  -0.0217   0.0895   1.0000
   8.250   1.0249   0.01421   0.00739  -0.0209   0.0819   1.0000
   8.500   1.0471   0.01460   0.00778  -0.0202   0.0754   1.0000
   8.750   1.0682   0.01506   0.00822  -0.0194   0.0689   1.0000
   9.000   1.0894   0.01549   0.00866  -0.0185   0.0634   1.0000
   9.250   1.1096   0.01598   0.00915  -0.0175   0.0586   1.0000
   9.500   1.1303   0.01640   0.00961  -0.0166   0.0551   1.0000
   9.750   1.1495   0.01691   0.01012  -0.0155   0.0511   1.0000
  10.000   1.1679   0.01744   0.01067  -0.0143   0.0476   1.0000
  10.250   1.1863   0.01793   0.01121  -0.0131   0.0446   1.0000
  10.500   1.2014   0.01851   0.01179  -0.0114   0.0413   1.0000
  10.750   1.2151   0.01911   0.01241  -0.0095   0.0388   1.0000
  11.000   1.2298   0.01966   0.01302  -0.0078   0.0370   1.0000
  11.250   1.2436   0.02029   0.01369  -0.0062   0.0351   1.0000
  11.500   1.2564   0.02101   0.01445  -0.0045   0.0334   1.0000
  11.750   1.2675   0.02187   0.01535  -0.0028   0.0315   1.0000
  12.000   1.2810   0.02261   0.01616  -0.0014   0.0303   1.0000
  12.250   1.2938   0.02341   0.01703  -0.0001   0.0291   1.0000
  12.500   1.3057   0.02430   0.01798   0.0012   0.0278   1.0000
  12.750   1.3166   0.02531   0.01904   0.0024   0.0266   1.0000
  13.000   1.3261   0.02645   0.02023   0.0037   0.0255   1.0000
  13.250   1.3346   0.02771   0.02155   0.0049   0.0245   1.0000
  13.500   1.3455   0.02881   0.02276   0.0058   0.0237   1.0000
  13.750   1.3549   0.03006   0.02410   0.0067   0.0228   1.0000
  14.000   1.3639   0.03139   0.02550   0.0076   0.0216   1.0000
  14.250   1.3712   0.03291   0.02707   0.0083   0.0205   1.0000
  14.500   1.3770   0.03460   0.02883   0.0091   0.0197   1.0000
  14.750   1.3823   0.03638   0.03070   0.0096   0.0188   1.0000
  15.000   1.3886   0.03813   0.03254   0.0101   0.0178   1.0000
  15.250   1.3928   0.04012   0.03463   0.0104   0.0168   1.0000
  15.500   1.3954   0.04235   0.03693   0.0106   0.0157   1.0000
  15.750   1.3962   0.04486   0.03951   0.0107   0.0143   1.0000
  16.000   1.3967   0.04747   0.04225   0.0105   0.0135   1.0000
  16.250   1.3951   0.05046   0.04532   0.0101   0.0121   1.0000
  16.500   1.3908   0.05395   0.04889   0.0094   0.0109   1.0000
  16.750   1.3852   0.05778   0.05283   0.0083   0.0094   1.0000
  17.000   1.3784   0.06199   0.05715   0.0069   0.0088   1.0000
  17.250   1.3683   0.06687   0.06214   0.0049   0.0080   1.0000
  17.500   1.3565   0.07225   0.06764   0.0026   0.0073   1.0000
  17.750   1.3454   0.07776   0.07330   0.0000   0.0072   1.0000
  18.000   1.3303   0.08412   0.07980  -0.0031   0.0070   1.0000
  18.250   1.3134   0.09102   0.08684  -0.0067   0.0068   1.0000
  18.500   1.2924   0.09890   0.09487  -0.0109   0.0065   1.0000
  18.750   1.2738   0.10654   0.10267  -0.0150   0.0066   1.0000
  19.000   1.2517   0.11505   0.11133  -0.0198   0.0065   1.0000
  19.250   1.2294   0.12375   0.12018  -0.0247   0.0065   1.0000
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