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S9026 (9.5%) (s9026-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S9026 (9.5%) (s9026-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.57 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s9026-il-1000000-n5.txt
Download as CSV file: xf-s9026-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S9026 (9.5%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1235   0.11262   0.11011   0.0103   1.0000   0.0049
 -17.500  -1.1857   0.09614   0.09344   0.0004   1.0000   0.0046
 -17.250  -1.2479   0.08048   0.07754  -0.0090   1.0000   0.0043
 -17.000  -1.2947   0.06805   0.06490  -0.0167   1.0000   0.0042
 -16.750  -1.3282   0.05830   0.05496  -0.0229   1.0000   0.0041
 -16.500  -1.3507   0.05091   0.04740  -0.0277   1.0000   0.0042
 -16.250  -1.3672   0.04501   0.04135  -0.0312   1.0000   0.0042
 -16.000  -1.3780   0.04054   0.03673  -0.0334   1.0000   0.0042
 -15.750  -1.3868   0.03685   0.03290  -0.0346   1.0000   0.0043
 -15.500  -1.3923   0.03397   0.02991  -0.0347   1.0000   0.0044
 -15.250  -1.3947   0.03173   0.02756  -0.0341   1.0000   0.0046
 -15.000  -1.3958   0.02986   0.02559  -0.0329   1.0000   0.0047
 -14.750  -1.3953   0.02831   0.02393  -0.0311   1.0000   0.0049
 -14.500  -1.3925   0.02705   0.02259  -0.0289   1.0000   0.0050
 -14.250  -1.3885   0.02597   0.02140  -0.0264   1.0000   0.0052
 -14.000  -1.3815   0.02506   0.02040  -0.0239   1.0000   0.0053
 -13.750  -1.3705   0.02408   0.01933  -0.0221   1.0000   0.0056
 -13.500  -1.3568   0.02316   0.01836  -0.0207   1.0000   0.0060
 -13.250  -1.3412   0.02234   0.01748  -0.0194   1.0000   0.0064
 -13.000  -1.3241   0.02158   0.01666  -0.0182   1.0000   0.0067
 -12.750  -1.3059   0.02088   0.01589  -0.0172   1.0000   0.0072
 -12.500  -1.2865   0.02025   0.01519  -0.0163   1.0000   0.0076
 -12.250  -1.2667   0.01961   0.01448  -0.0153   1.0000   0.0079
 -12.000  -1.2469   0.01892   0.01374  -0.0144   1.0000   0.0085
 -11.750  -1.2259   0.01835   0.01313  -0.0137   1.0000   0.0091
 -11.500  -1.2042   0.01781   0.01255  -0.0129   1.0000   0.0096
 -11.250  -1.1821   0.01731   0.01199  -0.0122   1.0000   0.0101
 -11.000  -1.1597   0.01681   0.01144  -0.0115   1.0000   0.0105
 -10.750  -1.1367   0.01638   0.01095  -0.0109   1.0000   0.0108
 -10.500  -1.1143   0.01584   0.01035  -0.0102   1.0000   0.0113
 -10.250  -1.0918   0.01528   0.00975  -0.0095   1.0000   0.0120
 -10.000  -1.0685   0.01484   0.00929  -0.0089   1.0000   0.0127
  -9.750  -1.0448   0.01442   0.00883  -0.0083   1.0000   0.0134
  -9.500  -1.0210   0.01402   0.00838  -0.0077   1.0000   0.0139
  -9.250  -0.9969   0.01365   0.00798  -0.0071   1.0000   0.0144
  -9.000  -0.9725   0.01332   0.00761  -0.0065   1.0000   0.0148
  -8.750  -0.9489   0.01287   0.00710  -0.0059   1.0000   0.0156
  -8.500  -0.9251   0.01246   0.00667  -0.0052   1.0000   0.0168
  -8.250  -0.9011   0.01209   0.00630  -0.0045   1.0000   0.0178
  -8.000  -0.8769   0.01176   0.00595  -0.0038   1.0000   0.0188
  -7.750  -0.8527   0.01147   0.00562  -0.0032   1.0000   0.0197
  -7.500  -0.8287   0.01116   0.00527  -0.0024   1.0000   0.0208
  -7.250  -0.8050   0.01082   0.00494  -0.0016   1.0000   0.0229
  -7.000  -0.7812   0.01053   0.00465  -0.0008   1.0000   0.0252
  -6.750  -0.7573   0.01025   0.00437   0.0000   1.0000   0.0278
  -6.500  -0.7337   0.00996   0.00411   0.0008   1.0000   0.0322
  -6.250  -0.7099   0.00972   0.00386   0.0017   1.0000   0.0358
  -6.000  -0.6809   0.00943   0.00361   0.0013   0.9986   0.0422
  -5.750  -0.6477   0.00920   0.00339   0.0002   0.9959   0.0469
  -5.500  -0.6141   0.00894   0.00317  -0.0012   0.9930   0.0530
  -5.250  -0.5820   0.00873   0.00296  -0.0021   0.9886   0.0584
  -5.000  -0.5487   0.00849   0.00277  -0.0033   0.9838   0.0664
  -4.750  -0.5175   0.00826   0.00258  -0.0040   0.9762   0.0763
  -4.500  -0.4851   0.00802   0.00239  -0.0050   0.9670   0.0887
  -4.250  -0.4538   0.00777   0.00221  -0.0057   0.9510   0.1054
  -4.000  -0.4248   0.00757   0.00204  -0.0058   0.9272   0.1225
  -3.750  -0.3987   0.00744   0.00189  -0.0052   0.9018   0.1355
  -3.500  -0.3729   0.00733   0.00175  -0.0046   0.8787   0.1492
  -3.250  -0.3468   0.00723   0.00163  -0.0041   0.8554   0.1636
  -3.000  -0.3209   0.00710   0.00151  -0.0036   0.8311   0.1831
  -2.750  -0.2946   0.00702   0.00139  -0.0031   0.8053   0.2019
  -2.500  -0.2681   0.00695   0.00130  -0.0027   0.7789   0.2197
  -2.250  -0.2414   0.00688   0.00121  -0.0024   0.7533   0.2385
  -2.000  -0.2149   0.00675   0.00112  -0.0021   0.7287   0.2698
  -1.750  -0.1883   0.00664   0.00104  -0.0018   0.7037   0.3017
  -1.500  -0.1614   0.00658   0.00098  -0.0015   0.6772   0.3251
  -1.250  -0.1345   0.00656   0.00093  -0.0012   0.6459   0.3474
  -1.000  -0.1077   0.00654   0.00088  -0.0009   0.6122   0.3738
  -0.750  -0.0808   0.00653   0.00085  -0.0007   0.5790   0.3988
  -0.500  -0.0538   0.00649   0.00083  -0.0005   0.5509   0.4285
  -0.250  -0.0269   0.00644   0.00081  -0.0002   0.5259   0.4644
   0.000   0.0000   0.00642   0.00080   0.0000   0.4971   0.4971
   0.250   0.0269   0.00644   0.00081   0.0002   0.4646   0.5262
   0.500   0.0538   0.00649   0.00083   0.0005   0.4286   0.5509
   0.750   0.0808   0.00653   0.00085   0.0007   0.3985   0.5788
   1.000   0.1077   0.00654   0.00088   0.0009   0.3737   0.6122
   1.250   0.1345   0.00656   0.00093   0.0012   0.3469   0.6463
   1.500   0.1614   0.00658   0.00098   0.0015   0.3251   0.6771
   1.750   0.1884   0.00663   0.00104   0.0018   0.3021   0.7036
   2.000   0.2149   0.00675   0.00112   0.0021   0.2693   0.7281
   2.250   0.2414   0.00688   0.00121   0.0024   0.2386   0.7533
   2.500   0.2681   0.00695   0.00130   0.0027   0.2197   0.7789
   2.750   0.2946   0.00702   0.00139   0.0031   0.2021   0.8053
   3.000   0.3208   0.00710   0.00151   0.0036   0.1830   0.8312
   3.250   0.3468   0.00723   0.00163   0.0041   0.1635   0.8555
   3.500   0.3728   0.00733   0.00175   0.0046   0.1492   0.8789
   3.750   0.3986   0.00744   0.00189   0.0052   0.1356   0.9018
   4.000   0.4247   0.00757   0.00204   0.0058   0.1225   0.9271
   4.250   0.4538   0.00777   0.00221   0.0057   0.1056   0.9509
   4.500   0.4851   0.00802   0.00239   0.0050   0.0886   0.9668
   4.750   0.5174   0.00825   0.00258   0.0040   0.0765   0.9761
   5.000   0.5485   0.00849   0.00277   0.0033   0.0665   0.9837
   5.250   0.5819   0.00873   0.00296   0.0021   0.0585   0.9886
   5.500   0.6140   0.00894   0.00317   0.0012   0.0530   0.9930
   5.750   0.6476   0.00920   0.00339  -0.0001   0.0469   0.9958
   6.000   0.6808   0.00943   0.00361  -0.0013   0.0422   0.9985
   6.250   0.7101   0.00972   0.00386  -0.0017   0.0359   1.0000
   6.500   0.7340   0.00996   0.00411  -0.0009   0.0322   1.0000
   6.750   0.7575   0.01026   0.00437   0.0000   0.0278   1.0000
   7.000   0.7814   0.01053   0.00465   0.0008   0.0251   1.0000
   7.250   0.8052   0.01082   0.00494   0.0016   0.0230   1.0000
   7.500   0.8288   0.01116   0.00527   0.0024   0.0207   1.0000
   7.750   0.8528   0.01147   0.00562   0.0031   0.0197   1.0000
   8.000   0.8770   0.01176   0.00595   0.0038   0.0188   1.0000
   8.250   0.9011   0.01209   0.00630   0.0045   0.0178   1.0000
   8.500   0.9251   0.01246   0.00667   0.0052   0.0168   1.0000
   8.750   0.9488   0.01287   0.00711   0.0059   0.0156   1.0000
   9.000   0.9724   0.01331   0.00760   0.0066   0.0148   1.0000
   9.250   0.9967   0.01365   0.00798   0.0071   0.0144   1.0000
   9.500   1.0208   0.01402   0.00838   0.0077   0.0139   1.0000
   9.750   1.0447   0.01442   0.00883   0.0083   0.0133   1.0000
  10.000   1.0683   0.01483   0.00928   0.0089   0.0127   1.0000
  10.250   1.0915   0.01529   0.00975   0.0095   0.0120   1.0000
  10.500   1.1140   0.01583   0.01034   0.0103   0.0113   1.0000
  10.750   1.1364   0.01637   0.01093   0.0110   0.0108   1.0000
  11.000   1.1592   0.01683   0.01145   0.0116   0.0105   1.0000
  11.250   1.1817   0.01731   0.01199   0.0123   0.0101   1.0000
  11.500   1.2039   0.01781   0.01255   0.0130   0.0096   1.0000
  11.750   1.2255   0.01834   0.01312   0.0137   0.0091   1.0000
  12.000   1.2465   0.01892   0.01374   0.0145   0.0086   1.0000
  12.250   1.2663   0.01961   0.01448   0.0154   0.0079   1.0000
  12.500   1.2860   0.02024   0.01518   0.0164   0.0076   1.0000
  12.750   1.3053   0.02088   0.01589   0.0173   0.0072   1.0000
  13.000   1.3236   0.02157   0.01665   0.0184   0.0068   1.0000
  13.250   1.3406   0.02233   0.01747   0.0195   0.0064   1.0000
  13.500   1.3562   0.02316   0.01835   0.0208   0.0060   1.0000
  13.750   1.3699   0.02405   0.01931   0.0223   0.0056   1.0000
  14.000   1.3808   0.02504   0.02038   0.0241   0.0054   1.0000
  14.250   1.3875   0.02597   0.02140   0.0265   0.0052   1.0000
  14.500   1.3918   0.02704   0.02258   0.0290   0.0051   1.0000
  14.750   1.3945   0.02831   0.02394   0.0312   0.0049   1.0000
  15.000   1.3959   0.02980   0.02553   0.0329   0.0047   1.0000
  15.250   1.3950   0.03166   0.02749   0.0342   0.0046   1.0000
  15.500   1.3920   0.03395   0.02990   0.0348   0.0045   1.0000
  15.750   1.3867   0.03682   0.03288   0.0346   0.0044   1.0000
  16.000   1.3792   0.04036   0.03655   0.0335   0.0043   1.0000
  16.250   1.3664   0.04510   0.04143   0.0312   0.0041   1.0000
  16.500   1.3510   0.05083   0.04732   0.0277   0.0041   1.0000
  16.750   1.3297   0.05806   0.05472   0.0231   0.0042   1.0000
  17.000   1.2962   0.06779   0.06464   0.0168   0.0042   1.0000
  17.250   1.2490   0.08031   0.07738   0.0091   0.0044   1.0000
  17.500   1.1855   0.09622   0.09352  -0.0005   0.0046   1.0000
  17.750   1.1247   0.11243   0.10992  -0.0102   0.0049   1.0000
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