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N-13 (n13-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: N-13 (n13-il)
Reynolds number: 200,000
Max Cl/Cd: 45.78 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n13-il-200000-n5.txt
Download as CSV file: xf-n13-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-13                                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8156   0.12069   0.11655  -0.0153   1.0000   0.0133
 -16.000  -0.8432   0.11007   0.10582  -0.0209   1.0000   0.0131
 -15.750  -0.8721   0.09946   0.09505  -0.0268   1.0000   0.0131
 -15.500  -0.8936   0.09097   0.08641  -0.0316   1.0000   0.0130
 -15.250  -0.9154   0.08285   0.07812  -0.0363   1.0000   0.0130
 -15.000  -0.9338   0.07585   0.07094  -0.0402   1.0000   0.0129
 -14.750  -0.9500   0.06959   0.06450  -0.0435   1.0000   0.0130
 -14.500  -0.9633   0.06417   0.05890  -0.0461   1.0000   0.0130
 -14.250  -0.9755   0.05927   0.05381  -0.0481   1.0000   0.0131
 -14.000  -0.9851   0.05502   0.04936  -0.0494   1.0000   0.0132
 -13.750  -0.9934   0.05120   0.04536  -0.0502   1.0000   0.0132
 -13.500  -0.9997   0.04783   0.04181  -0.0504   1.0000   0.0134
 -13.250  -1.0063   0.04467   0.03850  -0.0501   1.0000   0.0135
 -13.000  -1.0121   0.04179   0.03549  -0.0494   1.0000   0.0138
 -12.750  -1.0157   0.03934   0.03291  -0.0482   1.0000   0.0140
 -12.500  -1.0179   0.03722   0.03068  -0.0466   1.0000   0.0144
 -12.250  -1.0172   0.03546   0.02879  -0.0448   1.0000   0.0147
 -12.000  -1.0160   0.03385   0.02707  -0.0426   1.0000   0.0152
 -11.750  -1.0140   0.03236   0.02546  -0.0402   1.0000   0.0156
 -11.500  -1.0089   0.03121   0.02417  -0.0378   1.0000   0.0165
 -11.250  -1.0059   0.02992   0.02275  -0.0348   1.0000   0.0170
 -11.000  -1.0020   0.02879   0.02148  -0.0317   1.0000   0.0176
 -10.750  -0.9995   0.02770   0.02029  -0.0281   1.0000   0.0182
 -10.500  -0.9984   0.02666   0.01920  -0.0241   1.0000   0.0190
 -10.250  -0.9938   0.02581   0.01828  -0.0205   1.0000   0.0198
 -10.000  -0.9854   0.02497   0.01738  -0.0175   1.0000   0.0210
  -9.750  -0.9755   0.02418   0.01649  -0.0147   1.0000   0.0225
  -9.500  -0.9650   0.02340   0.01566  -0.0119   1.0000   0.0245
  -9.250  -0.9522   0.02278   0.01501  -0.0095   1.0000   0.0273
  -9.000  -0.9397   0.02212   0.01428  -0.0069   1.0000   0.0305
  -8.750  -0.9261   0.02156   0.01369  -0.0045   1.0000   0.0343
  -8.500  -0.9123   0.02102   0.01306  -0.0021   1.0000   0.0386
  -8.250  -0.8990   0.02048   0.01248   0.0003   1.0000   0.0426
  -8.000  -0.8834   0.02011   0.01198   0.0025   1.0000   0.0467
  -7.750  -0.8732   0.01941   0.01126   0.0055   1.0000   0.0502
  -7.500  -0.8610   0.01887   0.01065   0.0082   1.0000   0.0539
  -7.250  -0.8473   0.01845   0.01013   0.0107   1.0000   0.0574
  -7.000  -0.8344   0.01795   0.00962   0.0133   1.0000   0.0618
  -6.750  -0.8206   0.01749   0.00919   0.0157   1.0000   0.0671
  -6.500  -0.7945   0.01706   0.00887   0.0156   0.9980   0.0782
  -6.250  -0.7627   0.01676   0.00856   0.0144   0.9950   0.0939
  -6.000  -0.7319   0.01643   0.00815   0.0135   0.9917   0.1049
  -5.750  -0.7030   0.01602   0.00772   0.0129   0.9882   0.1133
  -5.500  -0.6722   0.01575   0.00736   0.0120   0.9854   0.1210
  -5.250  -0.6456   0.01534   0.00696   0.0119   0.9814   0.1300
  -5.000  -0.6170   0.01501   0.00663   0.0114   0.9776   0.1396
  -4.750  -0.5862   0.01467   0.00633   0.0105   0.9746   0.1521
  -4.500  -0.5614   0.01433   0.00604   0.0108   0.9694   0.1670
  -4.250  -0.5319   0.01400   0.00575   0.0102   0.9655   0.1879
  -4.000  -0.5030   0.01364   0.00547   0.0097   0.9615   0.2138
  -3.750  -0.4782   0.01321   0.00520   0.0100   0.9561   0.2495
  -3.500  -0.4498   0.01267   0.00493   0.0095   0.9521   0.3085
  -3.250  -0.4246   0.01224   0.00474   0.0098   0.9468   0.3691
  -3.000  -0.3966   0.01189   0.00455   0.0096   0.9418   0.4136
  -2.750  -0.3651   0.01155   0.00436   0.0088   0.9385   0.4535
  -2.500  -0.3381   0.01125   0.00422   0.0089   0.9332   0.4928
  -2.250  -0.3098   0.01093   0.00411   0.0089   0.9282   0.5428
  -2.000  -0.2767   0.01066   0.00400   0.0078   0.9248   0.5872
  -1.750  -0.2449   0.01046   0.00392   0.0071   0.9195   0.6236
  -1.500  -0.2091   0.01025   0.00380   0.0057   0.9133   0.6547
  -1.250  -0.1652   0.01003   0.00365   0.0024   0.9087   0.6803
  -1.000  -0.1336   0.00989   0.00358   0.0019   0.8991   0.7024
  -0.750  -0.0954   0.00973   0.00350  -0.0001   0.8912   0.7249
  -0.500  -0.0600   0.00961   0.00346  -0.0014   0.8813   0.7493
  -0.250  -0.0287   0.00953   0.00349  -0.0018   0.8699   0.7728
   0.000   0.0039   0.00949   0.00354  -0.0025   0.8584   0.7943
   0.250   0.0382   0.00947   0.00360  -0.0036   0.8454   0.8127
   0.500   0.0731   0.00949   0.00367  -0.0048   0.8294   0.8299
   0.750   0.1098   0.00951   0.00373  -0.0063   0.8087   0.8449
   1.250   0.1905   0.00961   0.00368  -0.0106   0.7448   0.8722
   1.500   0.2262   0.00980   0.00374  -0.0119   0.7168   0.8856
   1.750   0.2616   0.01002   0.00387  -0.0132   0.6921   0.8954
   2.000   0.2935   0.01023   0.00402  -0.0138   0.6682   0.9047
   2.250   0.3206   0.01045   0.00418  -0.0134   0.6428   0.9164
   2.500   0.3539   0.01074   0.00438  -0.0143   0.6047   0.9242
   2.750   0.3799   0.01106   0.00452  -0.0136   0.5497   0.9335
   3.000   0.4052   0.01153   0.00464  -0.0130   0.4711   0.9407
   3.250   0.4288   0.01200   0.00484  -0.0122   0.4136   0.9482
   3.500   0.4592   0.01242   0.00507  -0.0129   0.3691   0.9535
   3.750   0.4841   0.01280   0.00530  -0.0125   0.3295   0.9609
   4.000   0.5169   0.01320   0.00555  -0.0138   0.2857   0.9650
   4.250   0.5450   0.01361   0.00580  -0.0142   0.2452   0.9709
   4.500   0.5752   0.01406   0.00608  -0.0150   0.2077   0.9755
   4.750   0.6062   0.01448   0.00639  -0.0161   0.1758   0.9800
   5.000   0.6352   0.01492   0.00672  -0.0167   0.1500   0.9850
   5.250   0.6677   0.01533   0.00705  -0.0181   0.1245   0.9885
   5.500   0.6982   0.01579   0.00742  -0.0191   0.1064   0.9927
   5.750   0.7297   0.01622   0.00784  -0.0202   0.0942   0.9963
   6.000   0.7617   0.01664   0.00829  -0.0215   0.0856   0.9997
   6.250   0.7783   0.01712   0.00874  -0.0195   0.0800   1.0000
   6.500   0.7946   0.01748   0.00917  -0.0174   0.0756   1.0000
   6.750   0.8104   0.01789   0.00963  -0.0152   0.0710   1.0000
   7.000   0.8243   0.01843   0.01017  -0.0127   0.0673   1.0000
   7.250   0.8397   0.01886   0.01067  -0.0105   0.0638   1.0000
   7.500   0.8556   0.01925   0.01113  -0.0084   0.0596   1.0000
   7.750   0.8696   0.01975   0.01163  -0.0060   0.0557   1.0000
   8.000   0.8830   0.02032   0.01225  -0.0034   0.0528   1.0000
   8.250   0.8983   0.02073   0.01276  -0.0012   0.0494   1.0000
   8.500   0.9125   0.02119   0.01329   0.0012   0.0462   1.0000
   8.750   0.9231   0.02187   0.01395   0.0040   0.0431   1.0000
   9.000   0.9377   0.02231   0.01454   0.0064   0.0402   1.0000
   9.250   0.9505   0.02283   0.01513   0.0089   0.0373   1.0000
   9.500   0.9604   0.02349   0.01579   0.0118   0.0347   1.0000
   9.750   0.9716   0.02413   0.01655   0.0146   0.0322   1.0000
  10.000   0.9825   0.02474   0.01725   0.0173   0.0296   1.0000
  10.250   0.9900   0.02541   0.01796   0.0206   0.0277   1.0000
  10.500   0.9942   0.02623   0.01886   0.0244   0.0262   1.0000
  10.750   0.9998   0.02703   0.01980   0.0279   0.0244   1.0000
  11.000   1.0055   0.02785   0.02071   0.0312   0.0230   1.0000
  11.250   1.0107   0.02873   0.02165   0.0343   0.0219   1.0000
  11.500   1.0133   0.02981   0.02277   0.0375   0.0207   1.0000
  11.750   1.0177   0.03099   0.02412   0.0403   0.0198   1.0000
  12.000   1.0212   0.03226   0.02553   0.0429   0.0189   1.0000
  12.250   1.0233   0.03367   0.02708   0.0454   0.0180   1.0000
  12.500   1.0243   0.03522   0.02878   0.0477   0.0175   1.0000
  12.750   1.0243   0.03694   0.03062   0.0497   0.0171   1.0000
  13.000   1.0227   0.03886   0.03266   0.0514   0.0165   1.0000
  13.250   1.0206   0.04097   0.03489   0.0526   0.0163   1.0000
  13.500   1.0131   0.04377   0.03781   0.0535   0.0158   1.0000
  13.750   1.0062   0.04681   0.04099   0.0538   0.0155   1.0000
  14.000   0.9986   0.05023   0.04461   0.0536   0.0153   1.0000
  14.250   0.9889   0.05415   0.04872   0.0527   0.0151   1.0000
  14.500   0.9788   0.05843   0.05319   0.0512   0.0149   1.0000
  14.750   0.9632   0.06386   0.05882   0.0488   0.0148   1.0000
  15.000   0.9491   0.06949   0.06461   0.0459   0.0149   1.0000
  15.250   0.9285   0.07673   0.07206   0.0417   0.0147   1.0000
  15.500   0.9047   0.08495   0.08046   0.0369   0.0147   1.0000
  15.750   0.8810   0.09355   0.08922   0.0319   0.0148   1.0000
  16.000   0.8500   0.10393   0.09974   0.0263   0.0151   1.0000
  16.250   0.8138   0.11600   0.11194   0.0198   0.0154   1.0000
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