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S8064 (s8064-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S8064 (s8064-il)
Reynolds number: 500,000
Max Cl/Cd: 65.38 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8064-il-500000-n5.txt
Download as CSV file: xf-s8064-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8064                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.6925   0.09296   0.09047  -0.0400   1.0000   0.0047
 -14.000  -0.7034   0.08525   0.08268  -0.0443   1.0000   0.0046
 -13.750  -0.7278   0.07444   0.07170  -0.0513   1.0000   0.0045
 -13.500  -0.7448   0.06623   0.06336  -0.0572   1.0000   0.0045
 -13.250  -0.7665   0.05834   0.05531  -0.0627   1.0000   0.0045
 -13.000  -0.7829   0.05233   0.04912  -0.0666   1.0000   0.0045
 -12.750  -0.7948   0.04617   0.04270  -0.0719   0.9671   0.0045
 -12.500  -0.8009   0.04165   0.03789  -0.0750   0.9533   0.0045
 -12.250  -0.8070   0.03857   0.03460  -0.0753   0.9421   0.0045
 -12.000  -0.8156   0.03585   0.03162  -0.0740   0.9333   0.0045
 -11.750  -0.8204   0.03367   0.02921  -0.0723   0.9269   0.0045
 -11.500  -0.8233   0.03172   0.02706  -0.0701   0.9213   0.0045
 -11.250  -0.8237   0.03007   0.02519  -0.0677   0.9168   0.0045
 -11.000  -0.8208   0.02858   0.02352  -0.0654   0.9127   0.0045
 -10.750  -0.8206   0.02674   0.02146  -0.0624   0.9084   0.0046
 -10.500  -0.8160   0.02532   0.01984  -0.0596   0.9051   0.0046
 -10.250  -0.8093   0.02401   0.01835  -0.0570   0.9025   0.0047
 -10.000  -0.7982   0.02268   0.01687  -0.0551   0.9002   0.0048
  -9.750  -0.7837   0.02164   0.01571  -0.0536   0.8977   0.0049
  -9.500  -0.7682   0.02065   0.01460  -0.0522   0.8952   0.0050
  -9.250  -0.7510   0.01980   0.01365  -0.0510   0.8932   0.0052
  -9.000  -0.7327   0.01903   0.01277  -0.0498   0.8912   0.0053
  -8.750  -0.7141   0.01828   0.01191  -0.0486   0.8893   0.0055
  -8.500  -0.6945   0.01762   0.01115  -0.0476   0.8875   0.0057
  -8.250  -0.6740   0.01695   0.01039  -0.0467   0.8855   0.0059
  -8.000  -0.6528   0.01634   0.00970  -0.0459   0.8833   0.0061
  -7.750  -0.6311   0.01577   0.00906  -0.0452   0.8812   0.0063
  -7.500  -0.6089   0.01526   0.00846  -0.0444   0.8792   0.0066
  -7.250  -0.5865   0.01475   0.00787  -0.0437   0.8773   0.0068
  -7.000  -0.5643   0.01423   0.00729  -0.0430   0.8755   0.0075
  -6.750  -0.5411   0.01382   0.00682  -0.0424   0.8738   0.0082
  -6.500  -0.5171   0.01346   0.00640  -0.0419   0.8721   0.0092
  -6.250  -0.4932   0.01304   0.00596  -0.0414   0.8700   0.0106
  -6.000  -0.4692   0.01264   0.00554  -0.0409   0.8678   0.0140
  -5.750  -0.4452   0.01227   0.00518  -0.0404   0.8655   0.0213
  -5.500  -0.4210   0.01190   0.00486  -0.0400   0.8634   0.0323
  -5.250  -0.3963   0.01161   0.00458  -0.0396   0.8614   0.0421
  -5.000  -0.3719   0.01128   0.00431  -0.0392   0.8596   0.0583
  -4.750  -0.3476   0.01093   0.00406  -0.0387   0.8577   0.0813
  -4.500  -0.3232   0.01057   0.00383  -0.0384   0.8553   0.1114
  -4.250  -0.2988   0.01021   0.00361  -0.0380   0.8527   0.1458
  -4.000  -0.2744   0.00985   0.00338  -0.0377   0.8501   0.1849
  -3.750  -0.2506   0.00945   0.00316  -0.0372   0.8477   0.2349
  -3.500  -0.2275   0.00899   0.00294  -0.0366   0.8455   0.3013
  -3.250  -0.2041   0.00857   0.00274  -0.0360   0.8434   0.3678
  -3.000  -0.1805   0.00820   0.00260  -0.0354   0.8403   0.4319
  -2.750  -0.1561   0.00790   0.00249  -0.0350   0.8372   0.4865
  -2.500  -0.1312   0.00765   0.00238  -0.0345   0.8343   0.5327
  -2.250  -0.1059   0.00743   0.00227  -0.0341   0.8316   0.5741
  -2.000  -0.0805   0.00723   0.00219  -0.0336   0.8292   0.6145
  -1.750  -0.0550   0.00708   0.00219  -0.0332   0.8257   0.6513
  -1.500  -0.0287   0.00700   0.00220  -0.0329   0.8220   0.6830
  -1.250  -0.0016   0.00695   0.00218  -0.0327   0.8186   0.7068
  -1.000   0.0257   0.00691   0.00215  -0.0325   0.8157   0.7253
  -0.750   0.0532   0.00689   0.00215  -0.0324   0.8121   0.7395
  -0.500   0.0807   0.00688   0.00215  -0.0324   0.8075   0.7507
  -0.250   0.1084   0.00684   0.00213  -0.0324   0.8033   0.7599
   0.000   0.1365   0.00681   0.00208  -0.0324   0.7996   0.7670
   0.250   0.1641   0.00680   0.00210  -0.0324   0.7935   0.7739
   0.500   0.1920   0.00676   0.00206  -0.0324   0.7879   0.7802
   0.750   0.2197   0.00673   0.00206  -0.0324   0.7810   0.7858
   1.000   0.2474   0.00670   0.00202  -0.0324   0.7731   0.7917
   1.250   0.2750   0.00667   0.00201  -0.0323   0.7630   0.7966
   1.500   0.3024   0.00664   0.00198  -0.0322   0.7514   0.8016
   1.750   0.3297   0.00664   0.00195  -0.0321   0.7373   0.8068
   2.000   0.3565   0.00665   0.00192  -0.0319   0.7202   0.8112
   2.250   0.3827   0.00671   0.00192  -0.0315   0.7003   0.8159
   2.500   0.4086   0.00681   0.00196  -0.0311   0.6768   0.8209
   2.750   0.4337   0.00695   0.00201  -0.0306   0.6498   0.8254
   3.000   0.4575   0.00714   0.00210  -0.0298   0.6168   0.8302
   3.250   0.4802   0.00739   0.00221  -0.0289   0.5763   0.8356
   3.500   0.5021   0.00768   0.00236  -0.0278   0.5343   0.8407
   3.750   0.5230   0.00801   0.00254  -0.0266   0.4884   0.8464
   4.000   0.5424   0.00843   0.00276  -0.0252   0.4343   0.8530
   4.250   0.5608   0.00889   0.00301  -0.0236   0.3766   0.8596
   4.500   0.5783   0.00944   0.00331  -0.0220   0.3132   0.8675
   4.750   0.5963   0.00993   0.00361  -0.0204   0.2587   0.8755
   5.000   0.6145   0.01044   0.00391  -0.0189   0.2074   0.8844
   5.250   0.6334   0.01089   0.00422  -0.0175   0.1661   0.8936
   5.500   0.6534   0.01128   0.00453  -0.0163   0.1356   0.9030
   5.750   0.6743   0.01164   0.00483  -0.0152   0.1127   0.9144
   6.250   0.7228   0.01242   0.00554  -0.0146   0.0766   0.9417
   6.500   0.7536   0.01287   0.00596  -0.0158   0.0626   0.9544
   6.750   0.7860   0.01334   0.00639  -0.0174   0.0513   0.9673
   7.000   0.8174   0.01382   0.00683  -0.0188   0.0416   0.9829
   7.250   0.8487   0.01426   0.00727  -0.0202   0.0355   0.9962
   7.500   0.8703   0.01465   0.00768  -0.0195   0.0320   1.0000
   7.750   0.8849   0.01497   0.00801  -0.0172   0.0286   1.0000
   8.000   0.8990   0.01536   0.00839  -0.0150   0.0256   1.0000
   8.250   0.9146   0.01574   0.00880  -0.0130   0.0229   1.0000
   8.500   0.9298   0.01620   0.00926  -0.0111   0.0194   1.0000
   8.750   0.9459   0.01667   0.00977  -0.0094   0.0166   1.0000
   9.000   0.9612   0.01723   0.01032  -0.0076   0.0140   1.0000
   9.250   0.9770   0.01779   0.01091  -0.0059   0.0121   1.0000
   9.500   0.9926   0.01838   0.01153  -0.0043   0.0110   1.0000
   9.750   1.0073   0.01906   0.01224  -0.0026   0.0100   1.0000
  10.000   1.0224   0.01971   0.01297  -0.0011   0.0094   1.0000
  10.250   1.0373   0.02040   0.01374   0.0005   0.0091   1.0000
  10.500   1.0519   0.02112   0.01453   0.0021   0.0086   1.0000
  10.750   1.0654   0.02192   0.01540   0.0037   0.0083   1.0000
  11.000   1.0785   0.02277   0.01631   0.0053   0.0079   1.0000
  11.250   1.0895   0.02377   0.01739   0.0071   0.0077   1.0000
  11.500   1.0992   0.02488   0.01858   0.0089   0.0074   1.0000
  11.750   1.1082   0.02607   0.01986   0.0107   0.0073   1.0000
  12.000   1.1180   0.02720   0.02110   0.0124   0.0072   1.0000
  12.250   1.1277   0.02836   0.02238   0.0140   0.0070   1.0000
  12.500   1.1370   0.02957   0.02371   0.0155   0.0068   1.0000
  12.750   1.1444   0.03095   0.02520   0.0170   0.0066   1.0000
  13.000   1.1532   0.03223   0.02658   0.0183   0.0063   1.0000
  13.250   1.1577   0.03390   0.02838   0.0198   0.0063   1.0000
  13.500   1.1637   0.03548   0.03006   0.0211   0.0062   1.0000
  13.750   1.1673   0.03731   0.03201   0.0223   0.0059   1.0000
  14.000   1.1700   0.03929   0.03411   0.0234   0.0059   1.0000
  14.250   1.1716   0.04143   0.03637   0.0243   0.0057   1.0000
  14.500   1.1711   0.04388   0.03895   0.0250   0.0057   1.0000
  14.750   1.1702   0.04648   0.04167   0.0254   0.0055   1.0000
  15.000   1.1668   0.04948   0.04481   0.0256   0.0055   1.0000
  15.250   1.1620   0.05286   0.04835   0.0255   0.0055   1.0000
  15.500   1.1556   0.05661   0.05225   0.0249   0.0054   1.0000
  15.750   1.1476   0.06081   0.05658   0.0238   0.0053   1.0000
  16.000   1.1346   0.06603   0.06196   0.0220   0.0053   1.0000
  16.250   1.1256   0.07096   0.06706   0.0201   0.0053   1.0000
  16.500   1.1105   0.07717   0.07342   0.0172   0.0052   1.0000
  16.750   1.0979   0.08338   0.07979   0.0140   0.0052   1.0000
  17.000   1.0800   0.09092   0.08749   0.0099   0.0052   1.0000
  17.250   1.0633   0.09861   0.09535   0.0056   0.0052   1.0000
  17.500   1.0420   0.10761   0.10451   0.0005   0.0052   1.0000
  17.750   1.0203   0.11706   0.11411  -0.0049   0.0052   1.0000
  18.000   0.9995   0.12661   0.12382  -0.0102   0.0053   1.0000
  18.250   0.9726   0.13800   0.13535  -0.0166   0.0054   1.0000
  18.500   0.9348   0.15274   0.15027  -0.0246   0.0055   1.0000
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