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S4062-095-87 (s4062-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S4062-095-87 (s4062-il)
Reynolds number: 1,000,000
Max Cl/Cd: 130.99 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s4062-il-1000000-n5.txt
Download as CSV file: xf-s4062-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S4062-095-87                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.2963   0.09152   0.08946  -0.0557   0.8825   0.0040
  -9.750  -0.2964   0.08730   0.08522  -0.0574   0.8742   0.0039
  -9.250  -0.5090   0.03268   0.03020  -0.0922   0.8367   0.0040
  -9.000  -0.5036   0.02663   0.02365  -0.0953   0.8305   0.0040
  -8.750  -0.4883   0.02328   0.01990  -0.0964   0.8258   0.0041
  -8.500  -0.4684   0.02095   0.01726  -0.0970   0.8209   0.0041
  -8.250  -0.4458   0.01939   0.01544  -0.0972   0.8164   0.0042
  -8.000  -0.4222   0.01802   0.01382  -0.0973   0.8124   0.0042
  -7.750  -0.3974   0.01686   0.01247  -0.0975   0.8082   0.0043
  -7.500  -0.3721   0.01582   0.01123  -0.0976   0.8038   0.0043
  -7.250  -0.3463   0.01497   0.01020  -0.0976   0.7997   0.0043
  -7.000  -0.3213   0.01359   0.00858  -0.0977   0.7959   0.0045
  -6.750  -0.2950   0.01273   0.00758  -0.0977   0.7916   0.0047
  -6.500  -0.2680   0.01219   0.00693  -0.0978   0.7875   0.0049
  -6.250  -0.2408   0.01170   0.00635  -0.0978   0.7837   0.0051
  -6.000  -0.2132   0.01121   0.00578  -0.0979   0.7798   0.0053
  -5.750  -0.1857   0.01074   0.00521  -0.0980   0.7755   0.0054
  -5.500  -0.1580   0.01032   0.00470  -0.0980   0.7715   0.0056
  -5.250  -0.1301   0.00994   0.00424  -0.0980   0.7677   0.0060
  -5.000  -0.1020   0.00960   0.00384  -0.0981   0.7636   0.0062
  -4.750  -0.0739   0.00932   0.00349  -0.0982   0.7594   0.0065
  -4.500  -0.0458   0.00909   0.00318  -0.0982   0.7555   0.0067
  -4.250  -0.0176   0.00873   0.00276  -0.0983   0.7516   0.0073
  -4.000   0.0107   0.00849   0.00248  -0.0984   0.7473   0.0079
  -3.750   0.0390   0.00830   0.00225  -0.0985   0.7432   0.0086
  -3.500   0.0673   0.00814   0.00204  -0.0985   0.7393   0.0096
  -3.250   0.0958   0.00794   0.00184  -0.0986   0.7351   0.0126
  -3.000   0.1241   0.00773   0.00166  -0.0987   0.7308   0.0222
  -2.750   0.1524   0.00755   0.00150  -0.0988   0.7266   0.0357
  -2.500   0.1809   0.00740   0.00139  -0.0990   0.7226   0.0492
  -2.250   0.2093   0.00723   0.00129  -0.0991   0.7182   0.0693
  -2.000   0.2376   0.00710   0.00120  -0.0992   0.7138   0.0903
  -1.500   0.2944   0.00683   0.00107  -0.0995   0.7049   0.1434
  -1.250   0.3228   0.00674   0.00102  -0.0996   0.6998   0.1651
  -1.000   0.3512   0.00666   0.00098  -0.0998   0.6949   0.1901
  -0.750   0.3796   0.00656   0.00095  -0.0999   0.6885   0.2183
  -0.500   0.4077   0.00650   0.00093  -0.1000   0.6806   0.2481
  -0.250   0.4359   0.00643   0.00091  -0.1001   0.6707   0.2818
   0.000   0.4639   0.00635   0.00091  -0.1002   0.6606   0.3209
   0.250   0.4918   0.00628   0.00091  -0.1002   0.6504   0.3678
   0.500   0.5198   0.00621   0.00093  -0.1003   0.6406   0.4161
   0.750   0.5477   0.00611   0.00096  -0.1004   0.6316   0.4715
   1.000   0.5754   0.00604   0.00100  -0.1005   0.6222   0.5308
   1.250   0.6029   0.00595   0.00106  -0.1005   0.6111   0.5982
   1.500   0.6301   0.00584   0.00112  -0.1004   0.5997   0.6766
   1.750   0.6563   0.00569   0.00120  -0.1001   0.5878   0.7724
   2.000   0.6789   0.00551   0.00129  -0.0988   0.5749   0.8861
   2.250   0.7112   0.00548   0.00133  -0.0997   0.5583   1.0000
   2.500   0.7382   0.00564   0.00141  -0.0996   0.5393   1.0000
   2.750   0.7650   0.00584   0.00151  -0.0994   0.5166   1.0000
   3.000   0.7910   0.00610   0.00164  -0.0992   0.4861   1.0000
   3.250   0.8164   0.00644   0.00181  -0.0988   0.4502   1.0000
   3.500   0.8416   0.00678   0.00199  -0.0985   0.4147   1.0000
   3.750   0.8663   0.00717   0.00220  -0.0981   0.3779   1.0000
   4.000   0.8913   0.00752   0.00242  -0.0977   0.3465   1.0000
   4.250   0.9161   0.00788   0.00264  -0.0974   0.3164   1.0000
   4.500   0.9411   0.00821   0.00285  -0.0970   0.2914   1.0000
   4.750   0.9659   0.00855   0.00309  -0.0966   0.2656   1.0000
   5.000   0.9899   0.00895   0.00334  -0.0961   0.2369   1.0000
   5.250   1.0138   0.00935   0.00361  -0.0956   0.2102   1.0000
   5.500   1.0385   0.00966   0.00385  -0.0952   0.1937   1.0000
   5.750   1.0626   0.01001   0.00412  -0.0947   0.1758   1.0000
   6.000   1.0855   0.01045   0.00444  -0.0941   0.1507   1.0000
   6.250   1.1087   0.01086   0.00474  -0.0935   0.1312   1.0000
   6.500   1.1318   0.01125   0.00506  -0.0929   0.1152   1.0000
   6.750   1.1548   0.01163   0.00539  -0.0922   0.1015   1.0000
   7.000   1.1766   0.01210   0.00577  -0.0914   0.0850   1.0000
   7.250   1.1983   0.01256   0.00615  -0.0906   0.0712   1.0000
   7.500   1.2195   0.01303   0.00655  -0.0896   0.0581   1.0000
   7.750   1.2405   0.01350   0.00697  -0.0887   0.0478   1.0000
   8.250   1.2813   0.01444   0.00785  -0.0866   0.0326   1.0000
   8.500   1.3012   0.01491   0.00831  -0.0855   0.0267   1.0000
   8.750   1.3191   0.01548   0.00884  -0.0841   0.0193   1.0000
   9.000   1.3350   0.01608   0.00941  -0.0824   0.0138   1.0000
   9.250   1.3506   0.01659   0.00994  -0.0805   0.0117   1.0000
   9.500   1.3657   0.01713   0.01050  -0.0786   0.0106   1.0000
   9.750   1.3806   0.01770   0.01110  -0.0768   0.0096   1.0000
  10.000   1.3959   0.01826   0.01171  -0.0751   0.0092   1.0000
  10.250   1.4111   0.01885   0.01235  -0.0734   0.0089   1.0000
  10.500   1.4260   0.01948   0.01304  -0.0718   0.0085   1.0000
  10.750   1.4400   0.02019   0.01379  -0.0701   0.0081   1.0000
  11.000   1.4537   0.02093   0.01459  -0.0685   0.0078   1.0000
  11.250   1.4666   0.02175   0.01546  -0.0668   0.0075   1.0000
  11.500   1.4781   0.02270   0.01647  -0.0651   0.0071   1.0000
  11.750   1.4889   0.02373   0.01757  -0.0634   0.0068   1.0000
  12.000   1.4994   0.02480   0.01871  -0.0617   0.0066   1.0000
  12.250   1.5117   0.02573   0.01972  -0.0603   0.0064   1.0000
  12.500   1.5234   0.02674   0.02079  -0.0589   0.0063   1.0000
  12.750   1.5339   0.02788   0.02201  -0.0575   0.0061   1.0000
  13.000   1.5441   0.02905   0.02325  -0.0562   0.0059   1.0000
  13.250   1.5540   0.03028   0.02455  -0.0549   0.0056   1.0000
  13.500   1.5633   0.03160   0.02593  -0.0536   0.0054   1.0000
  13.750   1.5713   0.03304   0.02744  -0.0524   0.0053   1.0000
  14.000   1.5780   0.03465   0.02913  -0.0512   0.0051   1.0000
  14.250   1.5838   0.03639   0.03095  -0.0501   0.0050   1.0000
  14.500   1.5884   0.03828   0.03293  -0.0490   0.0048   1.0000
  14.750   1.5901   0.04055   0.03530  -0.0479   0.0047   1.0000
  15.000   1.5893   0.04315   0.03801  -0.0470   0.0045   1.0000
  15.250   1.5938   0.04527   0.04022  -0.0464   0.0044   1.0000
  15.500   1.5985   0.04743   0.04247  -0.0459   0.0043   1.0000
  15.750   1.6027   0.04973   0.04486  -0.0455   0.0042   1.0000
  16.000   1.6026   0.05262   0.04787  -0.0453   0.0041   1.0000
  16.250   1.6064   0.05511   0.05044  -0.0453   0.0040   1.0000
  16.500   1.6052   0.05835   0.05379  -0.0454   0.0039   1.0000
  16.750   1.6047   0.06161   0.05715  -0.0457   0.0038   1.0000
  17.000   1.6032   0.06513   0.06078  -0.0463   0.0037   1.0000
  17.250   1.6017   0.06872   0.06447  -0.0470   0.0035   1.0000
  17.500   1.5966   0.07302   0.06889  -0.0481   0.0035   1.0000
  17.750   1.5906   0.07760   0.07358  -0.0495   0.0034   1.0000
  18.000   1.5849   0.08231   0.07841  -0.0511   0.0033   1.0000
  18.250   1.5750   0.08786   0.08408  -0.0532   0.0032   1.0000
  18.500   1.5650   0.09365   0.08999  -0.0556   0.0031   1.0000
  18.750   1.5504   0.10050   0.09699  -0.0587   0.0031   1.0000
  19.000   1.5350   0.10769   0.10432  -0.0622   0.0031   1.0000
  19.250   1.5183   0.11533   0.11210  -0.0661   0.0031   1.0000
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