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S8064 (s8064-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S8064 (s8064-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.95 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8064-il-1000000.txt
Download as CSV file: xf-s8064-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.6911   0.06751   0.06564  -0.0580   1.0000   0.0070
 -12.750  -0.7289   0.05647   0.05440  -0.0664   0.9870   0.0067
 -12.500  -0.7351   0.04968   0.04738  -0.0743   0.9698   0.0068
 -12.250  -0.7523   0.04396   0.04139  -0.0781   0.9532   0.0068
 -12.000  -0.7640   0.04096   0.03820  -0.0777   0.9422   0.0068
 -11.750  -0.7926   0.03686   0.03381  -0.0753   0.9325   0.0065
 -11.500  -0.8122   0.03371   0.03039  -0.0721   0.9256   0.0064
 -11.250  -0.8310   0.03069   0.02706  -0.0679   0.9197   0.0063
 -11.000  -0.8326   0.02925   0.02545  -0.0647   0.9156   0.0063
 -10.750  -0.8312   0.02794   0.02399  -0.0615   0.9124   0.0064
 -10.500  -0.8326   0.02566   0.02143  -0.0580   0.9089   0.0063
 -10.250  -0.8210   0.02452   0.02014  -0.0562   0.9064   0.0065
 -10.000  -0.8108   0.02281   0.01820  -0.0541   0.9042   0.0065
  -9.750  -0.7971   0.02145   0.01665  -0.0524   0.9018   0.0065
  -9.500  -0.7816   0.02004   0.01508  -0.0509   0.9000   0.0065
  -9.250  -0.7647   0.01881   0.01370  -0.0496   0.8981   0.0065
  -9.000  -0.7470   0.01772   0.01248  -0.0482   0.8960   0.0066
  -8.750  -0.7282   0.01682   0.01147  -0.0471   0.8939   0.0067
  -8.500  -0.7086   0.01601   0.01056  -0.0459   0.8920   0.0069
  -8.250  -0.6884   0.01531   0.00976  -0.0449   0.8902   0.0070
  -8.000  -0.6668   0.01476   0.00913  -0.0440   0.8884   0.0072
  -7.750  -0.6445   0.01425   0.00855  -0.0433   0.8867   0.0073
  -7.500  -0.6271   0.01316   0.00734  -0.0418   0.8849   0.0080
  -7.250  -0.6042   0.01265   0.00678  -0.0411   0.8830   0.0083
  -7.000  -0.5805   0.01223   0.00632  -0.0406   0.8811   0.0088
  -6.750  -0.5563   0.01186   0.00591  -0.0401   0.8792   0.0094
  -6.500  -0.5318   0.01151   0.00551  -0.0396   0.8774   0.0099
  -6.250  -0.5073   0.01117   0.00510  -0.0391   0.8757   0.0105
  -6.000  -0.4835   0.01077   0.00467  -0.0385   0.8738   0.0131
  -5.750  -0.4598   0.01032   0.00430  -0.0380   0.8720   0.0244
  -5.500  -0.4349   0.00996   0.00402  -0.0376   0.8701   0.0391
  -5.250  -0.4095   0.00968   0.00379  -0.0374   0.8681   0.0521
  -5.000  -0.3839   0.00941   0.00357  -0.0372   0.8660   0.0668
  -4.750  -0.3585   0.00912   0.00336  -0.0369   0.8640   0.0865
  -4.500  -0.3334   0.00882   0.00315  -0.0366   0.8620   0.1138
  -4.250  -0.3090   0.00846   0.00295  -0.0362   0.8600   0.1547
  -4.000  -0.2853   0.00804   0.00276  -0.0357   0.8578   0.2137
  -3.750  -0.2622   0.00752   0.00255  -0.0351   0.8554   0.2916
  -3.500  -0.2385   0.00707   0.00237  -0.0346   0.8528   0.3635
  -3.250  -0.2146   0.00665   0.00220  -0.0341   0.8503   0.4388
  -3.000  -0.1899   0.00632   0.00207  -0.0337   0.8479   0.5010
  -2.750  -0.1645   0.00608   0.00196  -0.0333   0.8456   0.5496
  -2.500  -0.1382   0.00591   0.00190  -0.0331   0.8432   0.5865
  -2.250  -0.1120   0.00571   0.00183  -0.0328   0.8404   0.6249
  -2.000  -0.0856   0.00556   0.00179  -0.0326   0.8375   0.6632
  -1.750  -0.0583   0.00547   0.00176  -0.0325   0.8346   0.6913
  -1.500  -0.0306   0.00542   0.00172  -0.0324   0.8320   0.7112
  -1.250  -0.0026   0.00541   0.00171  -0.0325   0.8292   0.7264
  -1.000   0.0255   0.00537   0.00170  -0.0326   0.8259   0.7386
  -0.750   0.0538   0.00534   0.00167  -0.0326   0.8222   0.7499
  -0.500   0.0819   0.00529   0.00164  -0.0327   0.8187   0.7598
  -0.250   0.1101   0.00528   0.00161  -0.0327   0.8153   0.7689
   0.000   0.1383   0.00525   0.00160  -0.0328   0.8106   0.7771
   0.250   0.1665   0.00519   0.00156  -0.0329   0.8055   0.7839
   0.500   0.1948   0.00517   0.00152  -0.0329   0.8008   0.7902
   0.750   0.2231   0.00513   0.00150  -0.0331   0.7939   0.7957
   1.000   0.2512   0.00508   0.00146  -0.0331   0.7873   0.8007
   1.250   0.2794   0.00505   0.00145  -0.0332   0.7783   0.8058
   1.500   0.3076   0.00503   0.00142  -0.0333   0.7685   0.8105
   1.750   0.3353   0.00501   0.00140  -0.0332   0.7562   0.8150
   2.000   0.3628   0.00503   0.00139  -0.0332   0.7406   0.8196
   2.250   0.3899   0.00509   0.00139  -0.0331   0.7222   0.8240
   2.500   0.4162   0.00517   0.00142  -0.0328   0.7002   0.8282
   2.750   0.4421   0.00529   0.00148  -0.0324   0.6750   0.8326
   3.000   0.4678   0.00544   0.00155  -0.0321   0.6487   0.8372
   3.250   0.4935   0.00557   0.00163  -0.0317   0.6251   0.8415
   3.500   0.5180   0.00576   0.00175  -0.0312   0.5930   0.8462
   3.750   0.5415   0.00602   0.00188  -0.0305   0.5546   0.8513
   4.000   0.5633   0.00634   0.00204  -0.0295   0.5041   0.8564
   4.250   0.5833   0.00677   0.00224  -0.0281   0.4430   0.8621
   4.500   0.6029   0.00726   0.00248  -0.0268   0.3795   0.8683
   4.750   0.6218   0.00773   0.00274  -0.0254   0.3185   0.8751
   5.000   0.6409   0.00823   0.00301  -0.0240   0.2611   0.8830
   5.250   0.6590   0.00872   0.00330  -0.0224   0.2066   0.8919
   5.500   0.6780   0.00915   0.00358  -0.0210   0.1643   0.9023
   5.750   0.6963   0.00959   0.00388  -0.0194   0.1253   0.9148
   6.000   0.7161   0.00994   0.00416  -0.0180   0.0993   0.9299
   6.250   0.7393   0.01029   0.00447  -0.0174   0.0786   0.9478
   6.500   0.7703   0.01072   0.00484  -0.0186   0.0620   0.9634
   6.750   0.8052   0.01113   0.00521  -0.0207   0.0512   0.9756
   7.000   0.8398   0.01151   0.00558  -0.0226   0.0439   0.9859
   7.250   0.8732   0.01198   0.00600  -0.0244   0.0363   0.9939
   7.750   0.9235   0.01270   0.00669  -0.0244   0.0275   1.0000
   8.000   0.9406   0.01293   0.00694  -0.0225   0.0250   1.0000
   8.250   0.9547   0.01334   0.00731  -0.0202   0.0201   1.0000
   8.500   0.9683   0.01371   0.00767  -0.0177   0.0167   1.0000
   8.750   0.9815   0.01416   0.00813  -0.0152   0.0141   1.0000
   9.000   0.9964   0.01459   0.00859  -0.0131   0.0128   1.0000
   9.250   1.0090   0.01524   0.00926  -0.0107   0.0112   1.0000
   9.500   1.0239   0.01579   0.00986  -0.0087   0.0106   1.0000
   9.750   1.0402   0.01627   0.01039  -0.0071   0.0102   1.0000
  10.000   1.0558   0.01682   0.01099  -0.0054   0.0096   1.0000
  10.250   1.0709   0.01741   0.01163  -0.0037   0.0092   1.0000
  10.500   1.0859   0.01803   0.01228  -0.0021   0.0087   1.0000
  10.750   1.0986   0.01882   0.01312  -0.0002   0.0084   1.0000
  11.000   1.1017   0.02029   0.01474   0.0030   0.0078   1.0000
  11.250   1.1160   0.02099   0.01551   0.0046   0.0076   1.0000
  11.500   1.1284   0.02185   0.01644   0.0063   0.0074   1.0000
  11.750   1.1398   0.02277   0.01744   0.0081   0.0073   1.0000
  12.000   1.1506   0.02377   0.01853   0.0098   0.0071   1.0000
  12.250   1.1608   0.02481   0.01965   0.0116   0.0070   1.0000
  12.500   1.1694   0.02599   0.02093   0.0134   0.0068   1.0000
  12.750   1.1788   0.02712   0.02214   0.0150   0.0066   1.0000
  13.000   1.1867   0.02839   0.02350   0.0167   0.0065   1.0000
  13.250   1.1925   0.02985   0.02507   0.0184   0.0064   1.0000
  13.500   1.1981   0.03134   0.02665   0.0199   0.0062   1.0000
  13.750   1.2049   0.03274   0.02813   0.0212   0.0060   1.0000
  14.000   1.2074   0.03457   0.03006   0.0227   0.0060   1.0000
  14.250   1.2089   0.03655   0.03214   0.0240   0.0058   1.0000
  14.500   1.2034   0.03928   0.03500   0.0254   0.0056   1.0000
  14.750   1.1952   0.04242   0.03830   0.0266   0.0055   1.0000
  15.000   1.1775   0.04684   0.04294   0.0274   0.0054   1.0000
  15.250   1.1651   0.05098   0.04727   0.0275   0.0053   1.0000
  15.500   1.1543   0.05520   0.05165   0.0271   0.0053   1.0000
  15.750   1.1663   0.05673   0.05324   0.0265   0.0052   1.0000
  16.000   1.1473   0.06245   0.05914   0.0250   0.0053   1.0000
  16.250   1.1390   0.06712   0.06395   0.0232   0.0052   1.0000
  16.500   1.1245   0.07305   0.07003   0.0207   0.0052   1.0000
  16.750   1.1156   0.07844   0.07556   0.0179   0.0052   1.0000
  17.000   1.0845   0.08807   0.08538   0.0129   0.0053   1.0000
  17.250   1.0799   0.09347   0.09089   0.0097   0.0051   1.0000
  17.500   1.0471   0.10460   0.10220   0.0034   0.0052   1.0000
  17.750   1.0207   0.11501   0.11277  -0.0026   0.0053   1.0000
  18.000   0.9929   0.12616   0.12406  -0.0090   0.0053   1.0000
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