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S8064 (s8064-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S8064 (s8064-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.27 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8064-il-1000000-n5.txt
Download as CSV file: xf-s8064-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8481   0.06760   0.06522  -0.0539   0.9789   0.0029
 -14.250  -0.8740   0.05092   0.04807  -0.0696   0.9450   0.0028
 -13.750  -0.9036   0.04179   0.03852  -0.0728   0.9203   0.0029
 -13.500  -0.9106   0.03887   0.03544  -0.0727   0.9133   0.0029
 -13.250  -0.9140   0.03651   0.03295  -0.0722   0.9072   0.0029
 -13.000  -0.9281   0.03343   0.02964  -0.0707   0.9016   0.0029
 -12.750  -0.9323   0.03128   0.02734  -0.0692   0.8975   0.0029
 -12.500  -0.9395   0.02906   0.02492  -0.0669   0.8932   0.0029
 -12.250  -0.9349   0.02783   0.02358  -0.0651   0.8899   0.0029
 -12.000  -0.9385   0.02604   0.02159  -0.0622   0.8867   0.0029
 -11.750  -0.9377   0.02456   0.01997  -0.0594   0.8838   0.0030
 -11.500  -0.9315   0.02349   0.01877  -0.0569   0.8810   0.0030
 -11.250  -0.9265   0.02238   0.01752  -0.0540   0.8781   0.0030
 -11.000  -0.9171   0.02150   0.01653  -0.0515   0.8760   0.0030
 -10.750  -0.9045   0.02054   0.01543  -0.0497   0.8741   0.0031
 -10.500  -0.8896   0.01965   0.01443  -0.0482   0.8725   0.0031
 -10.250  -0.8728   0.01884   0.01354  -0.0469   0.8710   0.0032
 -10.000  -0.8552   0.01804   0.01263  -0.0457   0.8692   0.0032
  -9.750  -0.8357   0.01739   0.01190  -0.0447   0.8675   0.0033
  -9.500  -0.8163   0.01668   0.01111  -0.0437   0.8660   0.0034
  -9.250  -0.7957   0.01607   0.01042  -0.0428   0.8645   0.0035
  -9.000  -0.7745   0.01550   0.00978  -0.0420   0.8629   0.0035
  -8.750  -0.7530   0.01494   0.00914  -0.0412   0.8612   0.0037
  -8.500  -0.7308   0.01444   0.00856  -0.0405   0.8595   0.0038
  -8.250  -0.7082   0.01396   0.00801  -0.0399   0.8579   0.0040
  -8.000  -0.6848   0.01350   0.00751  -0.0394   0.8566   0.0041
  -7.750  -0.6611   0.01307   0.00702  -0.0389   0.8550   0.0042
  -7.500  -0.6369   0.01268   0.00659  -0.0385   0.8534   0.0044
  -7.250  -0.6124   0.01231   0.00617  -0.0381   0.8517   0.0045
  -7.000  -0.5882   0.01192   0.00573  -0.0377   0.8500   0.0047
  -6.750  -0.5638   0.01153   0.00528  -0.0373   0.8483   0.0050
  -6.500  -0.5389   0.01120   0.00492  -0.0369   0.8467   0.0053
  -6.250  -0.5136   0.01092   0.00459  -0.0366   0.8451   0.0057
  -6.000  -0.4881   0.01066   0.00429  -0.0364   0.8434   0.0061
  -5.750  -0.4619   0.01041   0.00403  -0.0362   0.8419   0.0067
  -5.500  -0.4365   0.01008   0.00372  -0.0360   0.8400   0.0104
  -5.250  -0.4112   0.00976   0.00345  -0.0357   0.8381   0.0193
  -5.000  -0.3854   0.00949   0.00322  -0.0355   0.8361   0.0285
  -4.750  -0.3593   0.00924   0.00301  -0.0354   0.8342   0.0386
  -4.500  -0.3334   0.00898   0.00281  -0.0352   0.8322   0.0525
  -4.250  -0.3074   0.00874   0.00262  -0.0350   0.8303   0.0686
  -4.000  -0.2814   0.00849   0.00244  -0.0349   0.8284   0.0906
  -3.750  -0.2557   0.00817   0.00227  -0.0347   0.8262   0.1227
  -3.500  -0.2303   0.00784   0.00210  -0.0345   0.8237   0.1640
  -3.250  -0.2047   0.00752   0.00194  -0.0343   0.8211   0.2066
  -3.000  -0.1796   0.00717   0.00177  -0.0340   0.8185   0.2611
  -2.750  -0.1541   0.00686   0.00163  -0.0338   0.8160   0.3114
  -2.500  -0.1288   0.00654   0.00150  -0.0335   0.8135   0.3685
  -2.250  -0.1030   0.00625   0.00140  -0.0334   0.8104   0.4227
  -2.000  -0.0768   0.00601   0.00131  -0.0332   0.8071   0.4693
  -1.750  -0.0504   0.00580   0.00123  -0.0331   0.8037   0.5127
  -1.500  -0.0238   0.00561   0.00115  -0.0330   0.8006   0.5502
  -1.250   0.0031   0.00545   0.00110  -0.0329   0.7969   0.5858
  -1.000   0.0300   0.00529   0.00106  -0.0328   0.7923   0.6199
  -0.750   0.0567   0.00515   0.00103  -0.0327   0.7876   0.6567
  -0.500   0.0839   0.00506   0.00103  -0.0326   0.7824   0.6887
  -0.250   0.1117   0.00502   0.00103  -0.0326   0.7756   0.7087
   0.000   0.1397   0.00499   0.00102  -0.0327   0.7679   0.7226
   0.250   0.1677   0.00499   0.00100  -0.0327   0.7576   0.7333
   0.500   0.1953   0.00499   0.00099  -0.0327   0.7446   0.7412
   0.750   0.2230   0.00504   0.00098  -0.0327   0.7292   0.7479
   1.000   0.2502   0.00509   0.00099  -0.0326   0.7121   0.7536
   1.250   0.2772   0.00517   0.00102  -0.0325   0.6930   0.7594
   1.500   0.3039   0.00529   0.00106  -0.0324   0.6719   0.7644
   1.750   0.3302   0.00541   0.00112  -0.0321   0.6477   0.7691
   2.000   0.3562   0.00556   0.00118  -0.0319   0.6214   0.7740
   2.250   0.3817   0.00575   0.00126  -0.0315   0.5905   0.7784
   2.500   0.4058   0.00599   0.00138  -0.0310   0.5504   0.7825
   2.750   0.4291   0.00630   0.00151  -0.0302   0.5021   0.7869
   3.000   0.4519   0.00665   0.00166  -0.0295   0.4517   0.7914
   3.250   0.4744   0.00702   0.00183  -0.0287   0.3980   0.7954
   3.500   0.4971   0.00736   0.00202  -0.0279   0.3524   0.7998
   3.750   0.5189   0.00776   0.00222  -0.0270   0.3008   0.8044
   4.250   0.5616   0.00861   0.00267  -0.0251   0.2007   0.8135
   4.500   0.5836   0.00899   0.00291  -0.0243   0.1626   0.8187
   5.000   0.6295   0.00957   0.00333  -0.0228   0.1148   0.8300
   5.250   0.6524   0.00985   0.00356  -0.0221   0.0960   0.8371
   5.750   0.6970   0.01042   0.00405  -0.0204   0.0644   0.8515
   6.000   0.7191   0.01070   0.00430  -0.0196   0.0521   0.8578
   6.250   0.7418   0.01094   0.00454  -0.0188   0.0456   0.8651
   6.500   0.7640   0.01118   0.00479  -0.0179   0.0395   0.8730
   6.750   0.7855   0.01144   0.00506  -0.0170   0.0341   0.8821
   7.000   0.8070   0.01167   0.00533  -0.0159   0.0302   0.8927
   7.250   0.8274   0.01193   0.00562  -0.0147   0.0262   0.9063
   7.500   0.8485   0.01215   0.00592  -0.0136   0.0241   0.9254
   7.750   0.8755   0.01248   0.00630  -0.0139   0.0201   0.9507
   8.250   0.9459   0.01346   0.00725  -0.0185   0.0110   0.9937
   8.500   0.9657   0.01388   0.00768  -0.0174   0.0091   1.0000
   8.750   0.9806   0.01425   0.00806  -0.0152   0.0082   1.0000
   9.000   0.9959   0.01467   0.00851  -0.0132   0.0075   1.0000
   9.250   1.0121   0.01510   0.00897  -0.0114   0.0070   1.0000
   9.500   1.0288   0.01553   0.00943  -0.0098   0.0069   1.0000
   9.750   1.0455   0.01599   0.00993  -0.0082   0.0065   1.0000
  10.000   1.0617   0.01650   0.01050  -0.0066   0.0063   1.0000
  10.250   1.0780   0.01701   0.01106  -0.0051   0.0061   1.0000
  10.500   1.0938   0.01758   0.01167  -0.0036   0.0058   1.0000
  10.750   1.1091   0.01820   0.01233  -0.0020   0.0057   1.0000
  11.000   1.1231   0.01892   0.01310  -0.0003   0.0053   1.0000
  11.250   1.1358   0.01973   0.01398   0.0015   0.0052   1.0000
  11.500   1.1484   0.02055   0.01487   0.0032   0.0050   1.0000
  11.750   1.1643   0.02113   0.01550   0.0045   0.0049   1.0000
  12.000   1.1770   0.02196   0.01641   0.0061   0.0049   1.0000
  12.250   1.1902   0.02275   0.01728   0.0076   0.0048   1.0000
  12.500   1.2021   0.02364   0.01824   0.0092   0.0047   1.0000
  12.750   1.2135   0.02458   0.01925   0.0107   0.0045   1.0000
  13.000   1.2240   0.02559   0.02035   0.0123   0.0044   1.0000
  13.250   1.2334   0.02669   0.02153   0.0139   0.0044   1.0000
  13.500   1.2426   0.02784   0.02277   0.0154   0.0044   1.0000
  13.750   1.2508   0.02907   0.02408   0.0169   0.0042   1.0000
  14.000   1.2579   0.03041   0.02552   0.0183   0.0041   1.0000
  14.250   1.2649   0.03180   0.02700   0.0197   0.0040   1.0000
  14.500   1.2692   0.03343   0.02873   0.0211   0.0040   1.0000
  14.750   1.2752   0.03498   0.03036   0.0222   0.0039   1.0000
  15.000   1.2777   0.03689   0.03238   0.0233   0.0038   1.0000
  15.250   1.2801   0.03887   0.03446   0.0242   0.0038   1.0000
  15.500   1.2820   0.04100   0.03668   0.0249   0.0037   1.0000
  15.750   1.2819   0.04343   0.03922   0.0255   0.0037   1.0000
  16.000   1.2787   0.04633   0.04223   0.0258   0.0036   1.0000
  16.250   1.2747   0.04949   0.04551   0.0258   0.0036   1.0000
  16.500   1.2673   0.05325   0.04941   0.0253   0.0036   1.0000
  16.750   1.2604   0.05717   0.05344   0.0244   0.0035   1.0000
  17.000   1.2491   0.06195   0.05837   0.0230   0.0035   1.0000
  17.250   1.2330   0.06777   0.06432   0.0208   0.0033   1.0000
  17.500   1.2199   0.07350   0.07021   0.0183   0.0034   1.0000
  17.750   1.1999   0.08075   0.07761   0.0147   0.0034   1.0000
  18.000   1.1774   0.08894   0.08596   0.0103   0.0033   1.0000
  18.250   1.1600   0.09657   0.09373   0.0061   0.0034   1.0000
  18.500   1.1353   0.10597   0.10329   0.0009   0.0034   1.0000
  18.750   1.1126   0.11527   0.11272  -0.0043   0.0034   1.0000
  19.000   1.0845   0.12588   0.12349  -0.0101   0.0035   1.0000
  19.250   1.0516   0.13786   0.13561  -0.0168   0.0035   1.0000
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