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NACA 2414 (n2414-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 2414 (n2414-il)
Reynolds number: 100,000
Max Cl/Cd: 48.11 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n2414-il-100000-n5.txt
Download as CSV file: xf-n2414-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 2414                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.7162   0.08156   0.07545  -0.0513   1.0000   0.0501
 -13.000  -0.7866   0.06543   0.05900  -0.0639   1.0000   0.0493
 -12.750  -0.8221   0.05769   0.05097  -0.0690   1.0000   0.0492
 -12.500  -0.8474   0.05262   0.04563  -0.0708   1.0000   0.0495
 -12.250  -0.8683   0.04892   0.04166  -0.0701   1.0000   0.0500
 -12.000  -0.8872   0.04610   0.03855  -0.0673   1.0000   0.0505
 -11.750  -0.8932   0.04407   0.03638  -0.0646   1.0000   0.0512
 -11.500  -0.8885   0.04270   0.03499  -0.0625   1.0000   0.0520
 -11.250  -0.8851   0.04125   0.03347  -0.0602   1.0000   0.0530
 -11.000  -0.8816   0.03975   0.03184  -0.0577   1.0000   0.0540
 -10.750  -0.8778   0.03818   0.03009  -0.0551   1.0000   0.0554
 -10.500  -0.8739   0.03650   0.02811  -0.0524   1.0000   0.0571
 -10.250  -0.8654   0.03518   0.02668  -0.0501   1.0000   0.0585
 -10.000  -0.8542   0.03422   0.02573  -0.0480   1.0000   0.0600
  -9.750  -0.8434   0.03315   0.02457  -0.0458   1.0000   0.0617
  -9.500  -0.8324   0.03199   0.02321  -0.0435   1.0000   0.0639
  -9.250  -0.8205   0.03084   0.02189  -0.0414   1.0000   0.0661
  -9.000  -0.8070   0.03003   0.02111  -0.0394   1.0000   0.0680
  -8.750  -0.7932   0.02917   0.02019  -0.0375   1.0000   0.0705
  -8.500  -0.7787   0.02826   0.01909  -0.0355   1.0000   0.0735
  -8.250  -0.7639   0.02744   0.01826  -0.0337   1.0000   0.0761
  -8.000  -0.7484   0.02675   0.01755  -0.0320   1.0000   0.0792
  -7.750  -0.7320   0.02602   0.01668  -0.0303   1.0000   0.0829
  -7.500  -0.7158   0.02532   0.01598  -0.0287   1.0000   0.0863
  -7.250  -0.6961   0.02472   0.01535  -0.0277   0.9993   0.0907
  -7.000  -0.6621   0.02397   0.01453  -0.0295   0.9949   0.0967
  -6.750  -0.6285   0.02335   0.01387  -0.0312   0.9901   0.1037
  -6.500  -0.5945   0.02271   0.01322  -0.0330   0.9850   0.1111
  -6.250  -0.5600   0.02216   0.01260  -0.0347   0.9800   0.1203
  -6.000  -0.5268   0.02161   0.01208  -0.0362   0.9739   0.1301
  -5.750  -0.4901   0.02108   0.01158  -0.0384   0.9693   0.1417
  -5.500  -0.4594   0.02060   0.01111  -0.0393   0.9617   0.1539
  -5.250  -0.4224   0.02013   0.01067  -0.0414   0.9566   0.1689
  -5.000  -0.3913   0.01970   0.01028  -0.0423   0.9488   0.1845
  -4.750  -0.3553   0.01928   0.00990  -0.0441   0.9428   0.2032
  -4.500  -0.3218   0.01889   0.00956  -0.0454   0.9360   0.2233
  -4.250  -0.2886   0.01852   0.00922  -0.0466   0.9286   0.2454
  -4.000  -0.2511   0.01809   0.00890  -0.0486   0.9238   0.2702
  -3.750  -0.2243   0.01778   0.00866  -0.0484   0.9135   0.2938
  -3.500  -0.1886   0.01739   0.00836  -0.0499   0.9078   0.3220
  -3.250  -0.1617   0.01709   0.00815  -0.0496   0.8974   0.3497
  -3.000  -0.1277   0.01669   0.00787  -0.0507   0.8909   0.3823
  -2.750  -0.1012   0.01639   0.00770  -0.0503   0.8801   0.4149
  -2.500  -0.0682   0.01601   0.00747  -0.0510   0.8731   0.4551
  -2.250  -0.0426   0.01574   0.00736  -0.0503   0.8614   0.4963
  -2.000  -0.0124   0.01542   0.00721  -0.0503   0.8526   0.5421
  -1.750   0.0149   0.01518   0.00711  -0.0497   0.8416   0.5879
  -1.500   0.0424   0.01495   0.00703  -0.0491   0.8305   0.6334
  -1.250   0.0726   0.01472   0.00692  -0.0488   0.8209   0.6795
  -1.000   0.0990   0.01460   0.00691  -0.0479   0.8080   0.7218
  -0.750   0.1274   0.01449   0.00688  -0.0471   0.7964   0.7627
  -0.500   0.1582   0.01439   0.00682  -0.0468   0.7853   0.8016
  -0.250   0.1879   0.01439   0.00685  -0.0464   0.7715   0.8367
   0.000   0.2206   0.01441   0.00685  -0.0466   0.7584   0.8685
   0.250   0.2572   0.01443   0.00683  -0.0476   0.7453   0.8956
   0.500   0.2936   0.01446   0.00678  -0.0487   0.7320   0.9204
   0.750   0.3328   0.01453   0.00678  -0.0506   0.7169   0.9403
   1.000   0.3733   0.01459   0.00677  -0.0529   0.7017   0.9579
   1.250   0.4164   0.01465   0.00674  -0.0558   0.6864   0.9726
   1.500   0.4606   0.01470   0.00671  -0.0591   0.6707   0.9860
   1.750   0.5063   0.01474   0.00667  -0.0627   0.6548   0.9985
   2.000   0.5309   0.01481   0.00664  -0.0622   0.6405   1.0000
   2.250   0.5526   0.01491   0.00665  -0.0610   0.6264   1.0000
   2.500   0.5739   0.01504   0.00672  -0.0598   0.6118   1.0000
   2.750   0.5955   0.01518   0.00680  -0.0586   0.5976   1.0000
   3.000   0.6173   0.01534   0.00689  -0.0574   0.5840   1.0000
   3.250   0.6395   0.01552   0.00699  -0.0563   0.5707   1.0000
   3.500   0.6613   0.01571   0.00713  -0.0551   0.5568   1.0000
   3.750   0.6830   0.01591   0.00730  -0.0538   0.5428   1.0000
   4.000   0.7047   0.01613   0.00748  -0.0526   0.5290   1.0000
   4.250   0.7266   0.01636   0.00766  -0.0514   0.5151   1.0000
   4.500   0.7484   0.01660   0.00784  -0.0501   0.5011   1.0000
   4.750   0.7698   0.01686   0.00807  -0.0489   0.4863   1.0000
   5.000   0.7912   0.01712   0.00832  -0.0476   0.4709   1.0000
   5.250   0.8126   0.01740   0.00858  -0.0463   0.4554   1.0000
   5.500   0.8338   0.01769   0.00886  -0.0450   0.4395   1.0000
   5.750   0.8547   0.01800   0.00914  -0.0437   0.4230   1.0000
   6.000   0.8754   0.01832   0.00944  -0.0424   0.4057   1.0000
   6.250   0.8957   0.01866   0.00976  -0.0410   0.3877   1.0000
   6.500   0.9155   0.01903   0.01010  -0.0396   0.3690   1.0000
   6.750   0.9347   0.01944   0.01046  -0.0381   0.3498   1.0000
   7.000   0.9534   0.01989   0.01086  -0.0365   0.3302   1.0000
   7.250   0.9718   0.02037   0.01132  -0.0350   0.3097   1.0000
   7.500   0.9894   0.02090   0.01180  -0.0334   0.2890   1.0000
   7.750   1.0060   0.02150   0.01233  -0.0316   0.2686   1.0000
   8.000   1.0214   0.02216   0.01292  -0.0298   0.2489   1.0000
   8.250   1.0370   0.02284   0.01356  -0.0280   0.2296   1.0000
   8.500   1.0514   0.02358   0.01425  -0.0261   0.2112   1.0000
   8.750   1.0648   0.02437   0.01500  -0.0241   0.1942   1.0000
   9.000   1.0770   0.02521   0.01581  -0.0220   0.1787   1.0000
   9.250   1.0871   0.02608   0.01666  -0.0196   0.1650   1.0000
   9.500   1.0964   0.02704   0.01758  -0.0172   0.1528   1.0000
  10.000   1.1145   0.02915   0.01969  -0.0128   0.1319   1.0000
  10.250   1.1231   0.03031   0.02087  -0.0107   0.1234   1.0000
  10.500   1.1297   0.03163   0.02216  -0.0087   0.1161   1.0000
  10.750   1.1386   0.03289   0.02349  -0.0070   0.1089   1.0000
  11.000   1.1437   0.03442   0.02500  -0.0052   0.1035   1.0000
  11.250   1.1520   0.03583   0.02652  -0.0037   0.0977   1.0000
  11.500   1.1570   0.03749   0.02820  -0.0023   0.0931   1.0000
  11.750   1.1630   0.03918   0.02995  -0.0009   0.0889   1.0000
  12.000   1.1688   0.04093   0.03179   0.0002   0.0848   1.0000
  12.250   1.1719   0.04293   0.03379   0.0013   0.0816   1.0000
  12.500   1.1778   0.04483   0.03583   0.0022   0.0781   1.0000
  12.750   1.1823   0.04688   0.03796   0.0029   0.0750   1.0000
  13.000   1.1851   0.04910   0.04021   0.0036   0.0726   1.0000
  13.250   1.1890   0.05134   0.04253   0.0042   0.0701   1.0000
  13.500   1.1925   0.05367   0.04501   0.0046   0.0675   1.0000
  13.750   1.1948   0.05613   0.04754   0.0049   0.0653   1.0000
  14.000   1.1969   0.05862   0.05005   0.0051   0.0635   1.0000
  14.250   1.1988   0.06128   0.05286   0.0052   0.0617   1.0000
  14.500   1.1995   0.06415   0.05590   0.0052   0.0598   1.0000
  14.750   1.1996   0.06711   0.05897   0.0049   0.0580   1.0000
  15.000   1.2000   0.07004   0.06195   0.0046   0.0566   1.0000
  15.250   1.2022   0.07272   0.06461   0.0045   0.0553   1.0000
  15.500   1.1979   0.07659   0.06874   0.0036   0.0540   1.0000
  15.750   1.1931   0.08059   0.07295   0.0026   0.0527   1.0000
  16.000   1.1880   0.08467   0.07719   0.0014   0.0515   1.0000
  16.250   1.1836   0.08871   0.08135   0.0001   0.0505   1.0000
  16.500   1.1811   0.09245   0.08516  -0.0011   0.0495   1.0000
  16.750   1.1834   0.09538   0.08808  -0.0018   0.0486   1.0000
  17.000   1.1690   0.10147   0.09443  -0.0046   0.0479   1.0000
  17.250   1.1515   0.10834   0.10156  -0.0080   0.0473   1.0000
  17.500   1.1305   0.11619   0.10967  -0.0122   0.0467   1.0000
  17.750   1.1028   0.12586   0.11961  -0.0178   0.0464   1.0000
  18.000   1.0395   0.14467   0.13878  -0.0297   0.0465   1.0000
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