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AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AS5048 (18%) (as5048-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.54 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5048-il-1000000.txt
Download as CSV file: xf-as5048-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5048 (18%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.7696   0.11033   0.10802  -0.0397   1.0000   0.0080
 -16.750  -0.8070   0.09867   0.09618  -0.0459   1.0000   0.0080
 -16.500  -0.8368   0.08933   0.08666  -0.0506   1.0000   0.0079
 -16.250  -0.8618   0.08151   0.07866  -0.0542   1.0000   0.0079
 -16.000  -0.8836   0.07478   0.07176  -0.0568   1.0000   0.0079
 -15.750  -0.9024   0.06899   0.06580  -0.0586   1.0000   0.0078
 -15.500  -0.9193   0.06382   0.06045  -0.0597   1.0000   0.0078
 -15.250  -0.9322   0.05952   0.05600  -0.0602   1.0000   0.0079
 -15.000  -0.9444   0.05551   0.05182  -0.0602   1.0000   0.0079
 -14.750  -0.9441   0.05137   0.04750  -0.0626   0.9989   0.0079
 -14.500  -0.9371   0.04758   0.04352  -0.0655   0.9944   0.0079
 -14.250  -0.9194   0.04386   0.03958  -0.0700   0.9411   0.0080
 -14.000  -0.8620   0.03967   0.03470  -0.0837   0.8368   0.0081
 -13.750  -0.8589   0.03821   0.03292  -0.0825   0.7912   0.0081
 -13.500  -0.8573   0.03572   0.03019  -0.0807   0.7787   0.0082
 -13.250  -0.8505   0.03398   0.02829  -0.0794   0.7697   0.0083
 -13.000  -0.8408   0.03257   0.02679  -0.0785   0.7636   0.0084
 -12.750  -0.8294   0.03135   0.02550  -0.0778   0.7581   0.0086
 -12.500  -0.8171   0.03024   0.02430  -0.0771   0.7532   0.0087
 -12.250  -0.8039   0.02917   0.02318  -0.0765   0.7498   0.0088
 -12.000  -0.7899   0.02815   0.02211  -0.0759   0.7467   0.0089
 -11.750  -0.7753   0.02720   0.02109  -0.0753   0.7437   0.0091
 -11.500  -0.7599   0.02631   0.02014  -0.0747   0.7409   0.0093
 -11.250  -0.7444   0.02543   0.01919  -0.0741   0.7381   0.0096
 -11.000  -0.7283   0.02461   0.01830  -0.0735   0.7352   0.0098
 -10.750  -0.7118   0.02377   0.01740  -0.0729   0.7334   0.0101
 -10.500  -0.6950   0.02295   0.01654  -0.0723   0.7316   0.0103
 -10.250  -0.6770   0.02224   0.01577  -0.0718   0.7297   0.0104
 -10.000  -0.6666   0.02097   0.01445  -0.0704   0.7277   0.0107
  -9.750  -0.6535   0.01994   0.01339  -0.0694   0.7256   0.0110
  -9.500  -0.6372   0.01914   0.01256  -0.0687   0.7236   0.0113
  -9.250  -0.6197   0.01844   0.01183  -0.0682   0.7217   0.0116
  -9.000  -0.6022   0.01776   0.01110  -0.0675   0.7197   0.0119
  -8.750  -0.5844   0.01713   0.01042  -0.0668   0.7175   0.0123
  -8.500  -0.5667   0.01652   0.00978  -0.0660   0.7165   0.0127
  -8.250  -0.5480   0.01601   0.00925  -0.0651   0.7152   0.0131
  -8.000  -0.5380   0.01528   0.00847  -0.0627   0.7138   0.0136
  -7.750  -0.5236   0.01475   0.00792  -0.0609   0.7123   0.0141
  -7.500  -0.5035   0.01434   0.00750  -0.0600   0.7107   0.0148
  -7.250  -0.4823   0.01398   0.00711  -0.0593   0.7091   0.0155
  -7.000  -0.4590   0.01371   0.00682  -0.0588   0.7077   0.0162
  -6.750  -0.4398   0.01318   0.00626  -0.0577   0.7063   0.0173
  -6.500  -0.4165   0.01288   0.00594  -0.0572   0.7049   0.0184
  -6.250  -0.3922   0.01262   0.00566  -0.0569   0.7034   0.0194
  -6.000  -0.3688   0.01230   0.00530  -0.0565   0.7016   0.0210
  -5.750  -0.3438   0.01206   0.00505  -0.0562   0.7000   0.0228
  -5.500  -0.3192   0.01177   0.00478  -0.0559   0.6990   0.0256
  -5.250  -0.2945   0.01147   0.00451  -0.0556   0.6980   0.0318
  -5.000  -0.2789   0.01046   0.00394  -0.0541   0.6968   0.1250
  -4.750  -0.2650   0.00918   0.00332  -0.0526   0.6954   0.2762
  -4.500  -0.2469   0.00804   0.00278  -0.0517   0.6939   0.4199
  -4.250  -0.2242   0.00727   0.00252  -0.0514   0.6924   0.5483
  -4.000  -0.1951   0.00723   0.00255  -0.0517   0.6910   0.5820
  -3.750  -0.1654   0.00726   0.00257  -0.0522   0.6895   0.5974
  -3.500  -0.1356   0.00733   0.00262  -0.0526   0.6879   0.6095
  -3.250  -0.1055   0.00742   0.00267  -0.0531   0.6863   0.6168
  -3.000  -0.0752   0.00750   0.00270  -0.0537   0.6843   0.6217
  -2.750  -0.0452   0.00760   0.00281  -0.0542   0.6826   0.6276
  -2.500  -0.0155   0.00767   0.00286  -0.0547   0.6814   0.6328
  -2.250   0.0144   0.00772   0.00289  -0.0551   0.6799   0.6370
  -2.000   0.0438   0.00771   0.00289  -0.0555   0.6781   0.6404
  -1.750   0.0734   0.00772   0.00290  -0.0560   0.6759   0.6428
  -1.500   0.1030   0.00773   0.00288  -0.0564   0.6732   0.6453
  -1.250   0.1325   0.00773   0.00286  -0.0568   0.6704   0.6475
  -1.000   0.1624   0.00779   0.00287  -0.0573   0.6675   0.6496
  -0.750   0.1924   0.00785   0.00290  -0.0578   0.6651   0.6516
  -0.500   0.2218   0.00784   0.00289  -0.0582   0.6632   0.6535
  -0.250   0.2509   0.00776   0.00283  -0.0586   0.6608   0.6559
   0.000   0.2803   0.00773   0.00281  -0.0590   0.6581   0.6575
   0.250   0.3097   0.00771   0.00279  -0.0594   0.6554   0.6589
   0.500   0.3391   0.00770   0.00277  -0.0598   0.6527   0.6603
   0.750   0.3687   0.00774   0.00279  -0.0603   0.6489   0.6618
   1.000   0.3970   0.00765   0.00273  -0.0604   0.6443   0.6633
   1.250   0.4255   0.00759   0.00267  -0.0606   0.6387   0.6647
   1.500   0.4545   0.00758   0.00264  -0.0609   0.6346   0.6660
   1.750   0.4838   0.00759   0.00265  -0.0613   0.6310   0.6674
   2.000   0.5129   0.00757   0.00265  -0.0617   0.6266   0.6686
   2.250   0.5419   0.00756   0.00264  -0.0620   0.6212   0.6696
   2.500   0.5704   0.00756   0.00261  -0.0622   0.6159   0.6707
   2.750   0.5994   0.00749   0.00260  -0.0626   0.6099   0.6723
   3.000   0.6277   0.00748   0.00259  -0.0628   0.6026   0.6738
   3.250   0.6560   0.00748   0.00261  -0.0630   0.5935   0.6752
   3.500   0.6836   0.00751   0.00263  -0.0630   0.5813   0.6766
   3.750   0.7108   0.00757   0.00266  -0.0630   0.5662   0.6778
   4.000   0.7372   0.00768   0.00272  -0.0628   0.5458   0.6791
   4.250   0.7617   0.00789   0.00282  -0.0623   0.5174   0.6804
   4.500   0.7848   0.00819   0.00298  -0.0615   0.4826   0.6818
   4.750   0.8073   0.00855   0.00319  -0.0607   0.4472   0.6833
   5.000   0.8300   0.00889   0.00341  -0.0599   0.4155   0.6846
   5.250   0.8525   0.00925   0.00363  -0.0590   0.3865   0.6858
   5.500   0.8751   0.00959   0.00386  -0.0582   0.3587   0.6867
   5.750   0.8977   0.00990   0.00408  -0.0575   0.3353   0.6880
   6.000   0.9198   0.01019   0.00429  -0.0566   0.3112   0.6898
   6.250   0.9409   0.01055   0.00455  -0.0556   0.2868   0.6913
   6.500   0.9619   0.01091   0.00482  -0.0545   0.2624   0.6927
   6.750   0.9825   0.01129   0.00511  -0.0534   0.2417   0.6942
   7.000   1.0029   0.01165   0.00540  -0.0523   0.2235   0.6958
   7.250   1.0235   0.01200   0.00569  -0.0512   0.2079   0.6974
   7.500   1.0441   0.01233   0.00598  -0.0501   0.1947   0.6989
   7.750   1.0650   0.01264   0.00626  -0.0490   0.1840   0.7003
   8.000   1.0839   0.01298   0.00657  -0.0476   0.1741   0.7017
   8.250   1.1011   0.01328   0.00685  -0.0458   0.1657   0.7029
   8.500   1.1190   0.01361   0.00716  -0.0442   0.1583   0.7040
   8.750   1.1377   0.01394   0.00750  -0.0429   0.1508   0.7060
   9.000   1.1565   0.01430   0.00787  -0.0416   0.1434   0.7079
   9.250   1.1750   0.01469   0.00826  -0.0403   0.1363   0.7097
   9.500   1.1928   0.01511   0.00869  -0.0389   0.1294   0.7116
   9.750   1.2099   0.01558   0.00914  -0.0375   0.1217   0.7134
  10.000   1.2265   0.01607   0.00964  -0.0360   0.1147   0.7153
  10.250   1.2414   0.01666   0.01020  -0.0343   0.1066   0.7171
  10.500   1.2569   0.01724   0.01078  -0.0329   0.0994   0.7188
  10.750   1.2698   0.01798   0.01149  -0.0312   0.0918   0.7203
  11.000   1.2841   0.01868   0.01220  -0.0298   0.0858   0.7222
  11.250   1.2966   0.01952   0.01304  -0.0283   0.0794   0.7246
  11.500   1.3097   0.02039   0.01393  -0.0271   0.0744   0.7268
  11.750   1.3218   0.02140   0.01496  -0.0259   0.0691   0.7291
  12.000   1.3352   0.02237   0.01597  -0.0250   0.0650   0.7313
  12.250   1.3457   0.02362   0.01721  -0.0239   0.0601   0.7335
  12.500   1.3600   0.02462   0.01826  -0.0233   0.0573   0.7357
  12.750   1.3708   0.02589   0.01953  -0.0224   0.0538   0.7377
  13.000   1.3822   0.02713   0.02082  -0.0217   0.0508   0.7410
  13.250   1.3946   0.02830   0.02205  -0.0210   0.0485   0.7443
  13.500   1.4042   0.02969   0.02347  -0.0202   0.0460   0.7476
  13.750   1.4123   0.03119   0.02500  -0.0193   0.0436   0.7509
  14.000   1.4239   0.03242   0.02631  -0.0187   0.0422   0.7541
  14.250   1.4334   0.03383   0.02777  -0.0180   0.0404   0.7583
  14.500   1.4398   0.03550   0.02948  -0.0171   0.0385   0.7631
  14.750   1.4458   0.03720   0.03126  -0.0163   0.0368   0.7683
  15.000   1.4558   0.03861   0.03276  -0.0158   0.0358   0.7749
  15.250   1.4636   0.04023   0.03447  -0.0152   0.0345   0.7840
  15.500   1.4695   0.04206   0.03639  -0.0147   0.0332   0.7975
  15.750   1.4726   0.04420   0.03868  -0.0142   0.0318   0.8260
  16.000   1.4527   0.04523   0.04009  -0.0077   0.0312   0.9895
  16.250   1.4595   0.04688   0.04181  -0.0072   0.0304   1.0000
  16.500   1.4658   0.04883   0.04383  -0.0069   0.0296   1.0000
  16.750   1.4700   0.05105   0.04609  -0.0067   0.0285   1.0000
  17.000   1.4717   0.05356   0.04863  -0.0066   0.0274   1.0000
  17.250   1.4693   0.05655   0.05168  -0.0064   0.0262   1.0000
  17.500   1.4751   0.05874   0.05395  -0.0065   0.0256   1.0000
  17.750   1.4785   0.06123   0.05651  -0.0066   0.0248   1.0000
  18.000   1.4795   0.06404   0.05938  -0.0068   0.0240   1.0000
  18.250   1.4777   0.06721   0.06261  -0.0072   0.0233   1.0000
  18.500   1.4726   0.07085   0.06632  -0.0076   0.0226   1.0000
  18.750   1.4629   0.07517   0.07072  -0.0084   0.0220   1.0000
  19.000   1.4626   0.07837   0.07401  -0.0090   0.0216   1.0000
  19.250   1.4598   0.08194   0.07768  -0.0099   0.0212   1.0000
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