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AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AS5046 (16%) (as5046-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.75 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5046-il-1000000.txt
Download as CSV file: xf-as5046-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5046 (16%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.3715   0.13399   0.13156  -0.0306   0.7594   0.0118
 -14.750  -0.5599   0.13751   0.13531  -0.0186   0.8289   0.0114
 -14.500  -0.5603   0.13331   0.13096  -0.0202   0.7976   0.0115
 -14.250  -0.5618   0.12824   0.12584  -0.0225   0.7862   0.0116
 -14.000  -0.5667   0.12199   0.11956  -0.0253   0.7791   0.0116
 -12.500  -0.8570   0.04555   0.04143  -0.0588   0.7619   0.0091
 -12.250  -0.8570   0.04328   0.03905  -0.0586   0.7577   0.0092
 -12.000  -0.8592   0.03998   0.03547  -0.0575   0.7541   0.0085
 -11.750  -0.8633   0.03693   0.03219  -0.0566   0.7505   0.0085
 -11.500  -0.7903   0.02182   0.01707  -0.0587   0.7439   0.0086
 -11.250  -0.7887   0.01964   0.01471  -0.0576   0.7413   0.0086
 -11.000  -0.7830   0.01727   0.01217  -0.0564   0.7388   0.0085
 -10.750  -0.7742   0.01551   0.01023  -0.0554   0.7364   0.0086
 -10.500  -0.7626   0.01409   0.00865  -0.0544   0.7341   0.0086
 -10.250  -0.7481   0.01261   0.00704  -0.0535   0.7318   0.0086
 -10.000  -0.7324   0.01142   0.00574  -0.0527   0.7303   0.0086
  -9.750  -0.7702   0.02301   0.01695  -0.0492   0.7307   0.0086
  -9.500  -0.7498   0.02202   0.01587  -0.0487   0.7291   0.0086
  -9.250  -0.7291   0.02111   0.01488  -0.0481   0.7273   0.0086
  -9.000  -0.7078   0.02031   0.01401  -0.0476   0.7255   0.0087
  -8.750  -0.6897   0.01897   0.01261  -0.0466   0.7236   0.0088
  -8.500  -0.6718   0.01788   0.01148  -0.0458   0.7217   0.0091
  -8.250  -0.6510   0.01716   0.01073  -0.0453   0.7199   0.0093
  -8.000  -0.6290   0.01654   0.01007  -0.0450   0.7181   0.0095
  -7.750  -0.6066   0.01595   0.00942  -0.0447   0.7161   0.0097
  -7.500  -0.5834   0.01536   0.00881  -0.0444   0.7148   0.0099
  -7.250  -0.5596   0.01481   0.00823  -0.0443   0.7136   0.0102
  -7.000  -0.5351   0.01430   0.00769  -0.0442   0.7122   0.0106
  -6.750  -0.5098   0.01385   0.00720  -0.0441   0.7106   0.0110
  -6.500  -0.4842   0.01342   0.00674  -0.0441   0.7089   0.0113
  -6.250  -0.4597   0.01279   0.00607  -0.0441   0.7074   0.0119
  -6.000  -0.4330   0.01243   0.00570  -0.0442   0.7059   0.0125
  -5.750  -0.4059   0.01211   0.00536  -0.0444   0.7045   0.0133
  -5.500  -0.3783   0.01186   0.00506  -0.0446   0.7030   0.0140
  -5.250  -0.3513   0.01147   0.00465  -0.0448   0.7014   0.0156
  -5.000  -0.3234   0.01122   0.00439  -0.0451   0.6994   0.0181
  -4.750  -0.2955   0.01091   0.00410  -0.0454   0.6980   0.0232
  -4.500  -0.2683   0.01036   0.00373  -0.0458   0.6969   0.0580
  -4.250  -0.2437   0.00892   0.00305  -0.0467   0.6955   0.2366
  -4.000  -0.2162   0.00775   0.00252  -0.0479   0.6938   0.3979
  -3.750  -0.1868   0.00691   0.00224  -0.0491   0.6920   0.5423
  -3.500  -0.1568   0.00686   0.00228  -0.0496   0.6901   0.5817
  -3.250  -0.1266   0.00692   0.00233  -0.0500   0.6883   0.6002
  -3.000  -0.0966   0.00703   0.00243  -0.0504   0.6864   0.6140
  -2.750  -0.0664   0.00714   0.00247  -0.0509   0.6843   0.6210
  -2.500  -0.0366   0.00723   0.00256  -0.0512   0.6818   0.6260
  -2.250  -0.0066   0.00726   0.00259  -0.0516   0.6800   0.6305
  -2.000   0.0235   0.00729   0.00259  -0.0521   0.6775   0.6341
  -1.750   0.0536   0.00730   0.00256  -0.0525   0.6745   0.6368
  -1.500   0.0832   0.00726   0.00251  -0.0529   0.6715   0.6398
  -1.250   0.1130   0.00728   0.00252  -0.0532   0.6688   0.6422
  -1.000   0.1428   0.00735   0.00256  -0.0537   0.6658   0.6445
  -0.750   0.1728   0.00735   0.00256  -0.0541   0.6636   0.6468
  -0.500   0.2027   0.00734   0.00255  -0.0545   0.6610   0.6488
  -0.250   0.2327   0.00735   0.00254  -0.0550   0.6580   0.6508
   0.000   0.2628   0.00737   0.00253  -0.0554   0.6548   0.6525
   0.250   0.2922   0.00730   0.00244  -0.0558   0.6505   0.6549
   0.500   0.3218   0.00725   0.00241  -0.0562   0.6456   0.6566
   0.750   0.3515   0.00720   0.00238  -0.0565   0.6406   0.6580
   1.000   0.3811   0.00718   0.00235  -0.0569   0.6360   0.6594
   1.250   0.4107   0.00718   0.00235  -0.0573   0.6314   0.6607
   1.500   0.4406   0.00715   0.00235  -0.0577   0.6265   0.6622
   1.750   0.4703   0.00715   0.00234  -0.0581   0.6210   0.6637
   2.000   0.4998   0.00715   0.00234  -0.0585   0.6149   0.6651
   2.250   0.5294   0.00714   0.00233  -0.0589   0.6064   0.6663
   2.500   0.5588   0.00716   0.00234  -0.0593   0.5981   0.6675
   2.750   0.5880   0.00720   0.00235  -0.0596   0.5866   0.6686
   3.000   0.6169   0.00725   0.00236  -0.0598   0.5708   0.6697
   3.250   0.6451   0.00729   0.00236  -0.0600   0.5505   0.6714
   3.500   0.6724   0.00744   0.00242  -0.0600   0.5221   0.6727
   3.750   0.6988   0.00770   0.00255  -0.0599   0.4855   0.6740
   4.000   0.7244   0.00804   0.00273  -0.0596   0.4455   0.6753
   4.250   0.7499   0.00839   0.00294  -0.0594   0.4093   0.6767
   4.500   0.7762   0.00868   0.00313  -0.0592   0.3801   0.6781
   4.750   0.8021   0.00899   0.00332  -0.0591   0.3514   0.6795
   5.000   0.8278   0.00931   0.00354  -0.0589   0.3242   0.6808
   5.250   0.8537   0.00962   0.00375  -0.0588   0.2996   0.6820
   5.500   0.8790   0.00997   0.00398  -0.0585   0.2724   0.6833
   5.750   0.9038   0.01035   0.00424  -0.0582   0.2466   0.6846
   6.000   0.9294   0.01067   0.00447  -0.0580   0.2271   0.6857
   6.250   0.9547   0.01097   0.00470  -0.0578   0.2094   0.6871
   6.500   0.9800   0.01124   0.00493  -0.0576   0.1950   0.6887
   6.750   1.0051   0.01153   0.00519  -0.0573   0.1822   0.6902
   7.250   1.0555   0.01210   0.00571  -0.0568   0.1611   0.6929
   7.500   1.0804   0.01240   0.00600  -0.0565   0.1516   0.6945
   7.750   1.1047   0.01273   0.00629  -0.0561   0.1418   0.6961
   8.000   1.1294   0.01302   0.00658  -0.0558   0.1334   0.6977
   8.250   1.1532   0.01338   0.00691  -0.0553   0.1243   0.6992
   8.500   1.1765   0.01375   0.00724  -0.0548   0.1147   0.7006
   8.750   1.1998   0.01411   0.00758  -0.0543   0.1060   0.7018
   9.000   1.2220   0.01452   0.00796  -0.0536   0.0970   0.7031
   9.500   1.2646   0.01537   0.00878  -0.0521   0.0807   0.7069
   9.750   1.2850   0.01584   0.00925  -0.0511   0.0740   0.7086
  10.000   1.3042   0.01635   0.00975  -0.0500   0.0677   0.7103
  10.250   1.3237   0.01682   0.01023  -0.0490   0.0626   0.7122
  10.500   1.3405   0.01741   0.01080  -0.0475   0.0574   0.7142
  10.750   1.3549   0.01788   0.01131  -0.0455   0.0540   0.7161
  11.000   1.3690   0.01849   0.01192  -0.0437   0.0504   0.7178
  11.250   1.3833   0.01918   0.01262  -0.0420   0.0470   0.7195
  11.500   1.3991   0.01978   0.01328  -0.0407   0.0448   0.7219
  11.750   1.4122   0.02058   0.01411  -0.0391   0.0423   0.7242
  12.000   1.4241   0.02151   0.01509  -0.0376   0.0399   0.7264
  12.250   1.4390   0.02231   0.01595  -0.0366   0.0383   0.7288
  12.500   1.4515   0.02334   0.01702  -0.0356   0.0365   0.7311
  12.750   1.4614   0.02467   0.01838  -0.0346   0.0346   0.7334
  13.000   1.4736   0.02588   0.01965  -0.0339   0.0332   0.7355
  13.250   1.4872   0.02699   0.02085  -0.0335   0.0320   0.7387
  13.500   1.4986   0.02833   0.02225  -0.0329   0.0306   0.7417
  13.750   1.5068   0.02993   0.02390  -0.0322   0.0292   0.7449
  14.000   1.5143   0.03161   0.02565  -0.0314   0.0281   0.7483
  14.250   1.5257   0.03294   0.02706  -0.0309   0.0272   0.7517
  14.500   1.5350   0.03446   0.02866  -0.0304   0.0263   0.7563
  14.750   1.5420   0.03618   0.03045  -0.0298   0.0254   0.7611
  15.000   1.5457   0.03822   0.03254  -0.0291   0.0244   0.7662
  15.250   1.5465   0.04054   0.03497  -0.0283   0.0235   0.7722
  15.500   1.5536   0.04230   0.03684  -0.0279   0.0231   0.7804
  15.750   1.5593   0.04422   0.03888  -0.0275   0.0224   0.7911
  16.000   1.5639   0.04628   0.04107  -0.0272   0.0218   0.8085
  16.250   1.5660   0.04861   0.04362  -0.0269   0.0212   0.8545
  16.500   1.5567   0.05065   0.04592  -0.0243   0.0207   1.0000
  16.750   1.5530   0.05388   0.04922  -0.0243   0.0200   1.0000
  17.000   1.5480   0.05735   0.05278  -0.0245   0.0195   1.0000
  17.250   1.5500   0.06011   0.05563  -0.0247   0.0192   1.0000
  17.500   1.5498   0.06321   0.05882  -0.0251   0.0188   1.0000
  17.750   1.5481   0.06659   0.06229  -0.0257   0.0184   1.0000
  18.000   1.5444   0.07028   0.06608  -0.0265   0.0180   1.0000
  18.250   1.5383   0.07437   0.07025  -0.0274   0.0176   1.0000
  18.500   1.5305   0.07880   0.07478  -0.0286   0.0173   1.0000
  18.750   1.5195   0.08380   0.07987  -0.0301   0.0169   1.0000
  19.000   1.5044   0.08950   0.08567  -0.0320   0.0166   1.0000
  19.250   1.4855   0.09588   0.09218  -0.0342   0.0163   1.0000
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