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S8052 (11.88%) (s8052-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S8052 (11.88%) (s8052-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.54 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8052-il-1000000-n5.txt
Download as CSV file: xf-s8052-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8052 (11.88%)                                  
  
 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  -0.8192   0.08842   0.08627  -0.0244   1.0000   0.0053
 -14.500  -0.8402   0.07931   0.07706  -0.0297   1.0000   0.0052
 -14.250  -0.8754   0.06708   0.06464  -0.0378   1.0000   0.0052
 -14.000  -0.9036   0.05699   0.05435  -0.0453   1.0000   0.0052
 -13.750  -0.9119   0.05164   0.04889  -0.0492   1.0000   0.0052
 -13.500  -0.9296   0.04572   0.04280  -0.0529   1.0000   0.0052
 -13.250  -0.9436   0.04116   0.03808  -0.0550   1.0000   0.0052
 -13.000  -0.9536   0.03763   0.03439  -0.0558   1.0000   0.0052
 -12.750  -0.9670   0.03419   0.03077  -0.0556   1.0000   0.0052
 -12.500  -0.9753   0.03164   0.02806  -0.0544   1.0000   0.0052
 -12.250  -0.9809   0.02959   0.02586  -0.0523   1.0000   0.0052
 -12.000  -0.9828   0.02807   0.02422  -0.0496   1.0000   0.0053
 -11.750  -0.9826   0.02662   0.02263  -0.0467   1.0000   0.0053
 -11.500  -0.9757   0.02514   0.02100  -0.0447   1.0000   0.0054
 -11.250  -0.9635   0.02401   0.01977  -0.0432   1.0000   0.0054
 -11.000  -0.9346   0.02256   0.01816  -0.0451   0.9607   0.0055
 -10.750  -0.9093   0.02174   0.01721  -0.0457   0.9285   0.0057
 -10.500  -0.8934   0.02092   0.01622  -0.0442   0.9019   0.0057
 -10.250  -0.8771   0.02006   0.01519  -0.0426   0.8823   0.0058
  -9.750  -0.8392   0.01855   0.01340  -0.0404   0.8542   0.0059
  -9.500  -0.8186   0.01785   0.01257  -0.0395   0.8437   0.0060
  -9.250  -0.7976   0.01716   0.01176  -0.0386   0.8343   0.0061
  -9.000  -0.7758   0.01649   0.01099  -0.0378   0.8254   0.0062
  -8.750  -0.7533   0.01590   0.01030  -0.0371   0.8175   0.0063
  -8.500  -0.7304   0.01532   0.00961  -0.0365   0.8094   0.0064
  -8.250  -0.7069   0.01478   0.00899  -0.0359   0.8026   0.0065
  -8.000  -0.6831   0.01426   0.00839  -0.0353   0.7960   0.0067
  -7.750  -0.6588   0.01380   0.00785  -0.0348   0.7898   0.0068
  -7.500  -0.6341   0.01336   0.00733  -0.0344   0.7836   0.0069
  -7.250  -0.6091   0.01296   0.00685  -0.0339   0.7774   0.0071
  -7.000  -0.5837   0.01259   0.00643  -0.0336   0.7721   0.0072
  -6.750  -0.5581   0.01222   0.00601  -0.0332   0.7666   0.0073
  -6.500  -0.5323   0.01189   0.00562  -0.0329   0.7616   0.0074
  -6.250  -0.5069   0.01146   0.00513  -0.0325   0.7573   0.0076
  -6.000  -0.4812   0.01106   0.00468  -0.0322   0.7528   0.0079
  -5.750  -0.4549   0.01075   0.00433  -0.0319   0.7484   0.0082
  -5.500  -0.4284   0.01048   0.00402  -0.0317   0.7442   0.0085
  -5.250  -0.4015   0.01023   0.00374  -0.0315   0.7403   0.0088
  -5.000  -0.3744   0.01000   0.00348  -0.0314   0.7360   0.0091
  -4.750  -0.3473   0.00979   0.00324  -0.0312   0.7319   0.0096
  -4.500  -0.3201   0.00961   0.00302  -0.0311   0.7279   0.0101
  -4.250  -0.2928   0.00938   0.00279  -0.0310   0.7235   0.0114
  -4.000  -0.2654   0.00919   0.00258  -0.0308   0.7189   0.0129
  -3.750  -0.2381   0.00900   0.00239  -0.0307   0.7148   0.0173
  -3.500  -0.2111   0.00873   0.00220  -0.0306   0.7111   0.0326
  -3.250  -0.1839   0.00848   0.00203  -0.0305   0.7070   0.0519
  -3.000  -0.1568   0.00824   0.00187  -0.0304   0.7025   0.0765
  -2.750  -0.1299   0.00799   0.00172  -0.0303   0.6980   0.1100
  -2.500  -0.1031   0.00766   0.00158  -0.0302   0.6932   0.1592
  -2.250  -0.0765   0.00733   0.00145  -0.0301   0.6882   0.2155
  -2.000  -0.0501   0.00701   0.00133  -0.0299   0.6835   0.2803
  -1.750  -0.0237   0.00663   0.00122  -0.0298   0.6780   0.3579
  -1.500   0.0031   0.00635   0.00113  -0.0297   0.6716   0.4222
  -1.250   0.0301   0.00611   0.00106  -0.0296   0.6651   0.4792
  -1.000   0.0570   0.00588   0.00100  -0.0294   0.6567   0.5395
  -0.750   0.0845   0.00575   0.00098  -0.0293   0.6480   0.5839
  -0.500   0.1123   0.00570   0.00096  -0.0293   0.6380   0.6118
  -0.250   0.1405   0.00567   0.00095  -0.0292   0.6254   0.6324
   0.000   0.1685   0.00567   0.00094  -0.0292   0.6112   0.6499
   0.250   0.1965   0.00570   0.00095  -0.0292   0.5952   0.6653
   0.500   0.2241   0.00576   0.00096  -0.0291   0.5733   0.6779
   0.750   0.2514   0.00587   0.00099  -0.0289   0.5463   0.6890
   1.000   0.2789   0.00598   0.00103  -0.0289   0.5228   0.6991
   1.250   0.3064   0.00609   0.00108  -0.0288   0.5001   0.7089
   1.500   0.3336   0.00624   0.00115  -0.0286   0.4728   0.7179
   1.750   0.3609   0.00639   0.00122  -0.0286   0.4487   0.7272
   2.000   0.3881   0.00652   0.00130  -0.0284   0.4262   0.7362
   2.250   0.4150   0.00671   0.00139  -0.0283   0.3987   0.7454
   2.500   0.4415   0.00691   0.00150  -0.0281   0.3698   0.7555
   2.750   0.4684   0.00707   0.00161  -0.0280   0.3466   0.7648
   3.000   0.4952   0.00726   0.00173  -0.0278   0.3243   0.7733
   3.250   0.5218   0.00745   0.00185  -0.0276   0.2997   0.7803
   3.500   0.5481   0.00769   0.00200  -0.0275   0.2734   0.7874
   3.750   0.5740   0.00794   0.00215  -0.0272   0.2465   0.7944
   4.000   0.6004   0.00815   0.00230  -0.0270   0.2270   0.8020
   4.250   0.6269   0.00832   0.00244  -0.0268   0.2127   0.8093
   4.500   0.6532   0.00852   0.00260  -0.0266   0.1974   0.8180
   4.750   0.6792   0.00871   0.00276  -0.0263   0.1833   0.8270
   5.000   0.7054   0.00888   0.00293  -0.0261   0.1726   0.8364
   5.250   0.7311   0.00908   0.00311  -0.0258   0.1607   0.8470
   5.500   0.7564   0.00928   0.00330  -0.0254   0.1485   0.8590
   5.750   0.7815   0.00947   0.00349  -0.0249   0.1381   0.8733
   6.000   0.8063   0.00963   0.00368  -0.0244   0.1296   0.8901
   6.500   0.8551   0.00998   0.00411  -0.0232   0.1127   0.9423
   6.750   0.8903   0.01025   0.00437  -0.0250   0.1030   0.9737
   7.000   0.9245   0.01057   0.00464  -0.0267   0.0939   0.9995
   7.250   0.9489   0.01084   0.00489  -0.0262   0.0865   1.0000
   7.500   0.9729   0.01113   0.00515  -0.0257   0.0796   1.0000
   7.750   0.9964   0.01147   0.00545  -0.0251   0.0721   1.0000
   8.000   1.0202   0.01177   0.00574  -0.0246   0.0662   1.0000
   8.250   1.0434   0.01213   0.00606  -0.0240   0.0604   1.0000
   8.500   1.0671   0.01242   0.00636  -0.0234   0.0567   1.0000
   8.750   1.0901   0.01277   0.00671  -0.0228   0.0522   1.0000
   9.000   1.1125   0.01316   0.00707  -0.0221   0.0469   1.0000
   9.250   1.1344   0.01357   0.00745  -0.0214   0.0421   1.0000
   9.500   1.1562   0.01397   0.00784  -0.0206   0.0384   1.0000
   9.750   1.1779   0.01435   0.00823  -0.0198   0.0356   1.0000
  10.000   1.1987   0.01478   0.00867  -0.0189   0.0330   1.0000
  10.250   1.2194   0.01520   0.00910  -0.0180   0.0310   1.0000
  10.500   1.2401   0.01558   0.00951  -0.0171   0.0297   1.0000
  10.750   1.2599   0.01600   0.00996  -0.0160   0.0283   1.0000
  11.000   1.2782   0.01648   0.01045  -0.0148   0.0266   1.0000
  11.250   1.2938   0.01699   0.01097  -0.0131   0.0247   1.0000
  11.500   1.3093   0.01743   0.01146  -0.0114   0.0240   1.0000
  11.750   1.3240   0.01792   0.01198  -0.0096   0.0229   1.0000
  12.000   1.3380   0.01846   0.01256  -0.0078   0.0218   1.0000
  12.250   1.3509   0.01910   0.01321  -0.0061   0.0205   1.0000
  12.500   1.3631   0.01980   0.01395  -0.0044   0.0190   1.0000
  12.750   1.3768   0.02046   0.01465  -0.0029   0.0183   1.0000
  13.000   1.3890   0.02122   0.01546  -0.0014   0.0169   1.0000
  13.250   1.4002   0.02210   0.01636   0.0001   0.0155   1.0000
  13.500   1.4109   0.02303   0.01733   0.0015   0.0143   1.0000
  13.750   1.4218   0.02399   0.01834   0.0027   0.0133   1.0000
  14.000   1.4289   0.02526   0.01963   0.0042   0.0110   1.0000
  14.250   1.4353   0.02664   0.02103   0.0055   0.0087   1.0000
  14.500   1.4420   0.02805   0.02249   0.0067   0.0074   1.0000
  14.750   1.4427   0.03000   0.02448   0.0080   0.0053   1.0000
  15.250   1.4500   0.03361   0.02824   0.0097   0.0042   1.0000
  15.500   1.4543   0.03547   0.03019   0.0104   0.0040   1.0000
  15.750   1.4535   0.03787   0.03267   0.0109   0.0035   1.0000
  16.000   1.4574   0.03989   0.03478   0.0113   0.0036   1.0000
  16.250   1.4556   0.04258   0.03756   0.0114   0.0033   1.0000
  16.500   1.4526   0.04552   0.04060   0.0114   0.0031   1.0000
  16.750   1.4502   0.04855   0.04373   0.0110   0.0030   1.0000
  17.000   1.4477   0.05176   0.04704   0.0104   0.0030   1.0000
  17.250   1.4431   0.05538   0.05078   0.0095   0.0029   1.0000
  17.500   1.4370   0.05940   0.05492   0.0082   0.0029   1.0000
  17.750   1.4301   0.06373   0.05936   0.0066   0.0029   1.0000
  18.000   1.4202   0.06870   0.06445   0.0045   0.0029   1.0000
  18.250   1.4083   0.07418   0.07006   0.0020   0.0028   1.0000
  18.500   1.3931   0.08043   0.07645  -0.0010   0.0028   1.0000
  18.750   1.3759   0.08724   0.08341  -0.0045   0.0028   1.0000
  19.000   1.3548   0.09499   0.09130  -0.0086   0.0028   1.0000
  19.250   1.3309   0.10348   0.09995  -0.0132   0.0028   1.0000
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