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NACA 2414 (n2414-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 2414 (n2414-il)
Reynolds number: 200,000
Max Cl/Cd: 62.15 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n2414-il-200000-n5.txt
Download as CSV file: xf-n2414-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.8947   0.08030   0.07530  -0.0498   1.0000   0.0312
 -15.250  -0.9230   0.07161   0.06639  -0.0556   1.0000   0.0313
 -15.000  -0.9424   0.06473   0.05934  -0.0601   1.0000   0.0314
 -14.750  -0.9567   0.05893   0.05336  -0.0640   1.0000   0.0317
 -14.500  -0.9674   0.05394   0.04821  -0.0672   1.0000   0.0319
 -14.250  -0.9754   0.04964   0.04374  -0.0697   1.0000   0.0322
 -14.000  -0.9813   0.04594   0.03987  -0.0714   1.0000   0.0326
 -13.750  -0.9854   0.04276   0.03652  -0.0724   1.0000   0.0331
 -13.500  -0.9881   0.04005   0.03361  -0.0727   1.0000   0.0336
 -13.250  -0.9897   0.03773   0.03109  -0.0722   1.0000   0.0341
 -13.000  -0.9886   0.03594   0.02922  -0.0711   1.0000   0.0346
 -12.750  -0.9863   0.03452   0.02776  -0.0694   1.0000   0.0351
 -12.500  -0.9846   0.03332   0.02650  -0.0670   1.0000   0.0357
 -12.250  -0.9837   0.03228   0.02539  -0.0640   1.0000   0.0363
 -12.000  -0.9796   0.03124   0.02426  -0.0612   1.0000   0.0370
 -11.750  -0.9740   0.03022   0.02313  -0.0585   1.0000   0.0379
 -11.500  -0.9670   0.02922   0.02199  -0.0558   1.0000   0.0387
 -11.250  -0.9593   0.02827   0.02095  -0.0531   1.0000   0.0395
 -11.000  -0.9506   0.02745   0.02011  -0.0505   1.0000   0.0403
 -10.750  -0.9405   0.02671   0.01933  -0.0480   1.0000   0.0412
 -10.500  -0.9295   0.02600   0.01855  -0.0456   1.0000   0.0424
 -10.250  -0.9177   0.02529   0.01774  -0.0432   1.0000   0.0437
 -10.000  -0.9055   0.02457   0.01693  -0.0409   1.0000   0.0450
  -9.750  -0.8930   0.02391   0.01626  -0.0387   1.0000   0.0462
  -9.500  -0.8791   0.02331   0.01562  -0.0366   1.0000   0.0476
  -9.250  -0.8483   0.02257   0.01478  -0.0378   0.9970   0.0498
  -9.000  -0.8171   0.02183   0.01399  -0.0392   0.9940   0.0521
  -8.750  -0.7867   0.02120   0.01332  -0.0403   0.9904   0.0546
  -8.500  -0.7552   0.02061   0.01262  -0.0415   0.9867   0.0576
  -8.250  -0.7228   0.01996   0.01199  -0.0430   0.9836   0.0606
  -8.000  -0.6917   0.01944   0.01140  -0.0440   0.9797   0.0642
  -7.750  -0.6612   0.01886   0.01081  -0.0450   0.9751   0.0678
  -7.500  -0.6276   0.01837   0.01028  -0.0465   0.9717   0.0724
  -7.250  -0.5946   0.01785   0.00976  -0.0479   0.9682   0.0771
  -7.000  -0.5650   0.01742   0.00929  -0.0484   0.9624   0.0825
  -6.750  -0.5310   0.01693   0.00881  -0.0499   0.9586   0.0885
  -6.500  -0.4949   0.01649   0.00834  -0.0518   0.9556   0.0957
  -6.250  -0.4678   0.01608   0.00796  -0.0518   0.9480   0.1030
  -6.000  -0.4349   0.01566   0.00755  -0.0529   0.9430   0.1116
  -5.750  -0.4031   0.01529   0.00717  -0.0538   0.9375   0.1213
  -5.500  -0.3747   0.01494   0.00684  -0.0539   0.9298   0.1320
  -5.250  -0.3419   0.01455   0.00650  -0.0550   0.9247   0.1447
  -5.000  -0.3152   0.01423   0.00622  -0.0547   0.9159   0.1574
  -4.750  -0.2845   0.01390   0.00592  -0.0553   0.9094   0.1722
  -4.500  -0.2564   0.01360   0.00567  -0.0553   0.9010   0.1878
  -4.250  -0.2270   0.01330   0.00541  -0.0555   0.8930   0.2050
  -4.000  -0.1990   0.01303   0.00519  -0.0555   0.8841   0.2233
  -3.750  -0.1700   0.01276   0.00496  -0.0556   0.8753   0.2433
  -3.500  -0.1425   0.01253   0.00477  -0.0554   0.8652   0.2637
  -3.250  -0.1137   0.01226   0.00456  -0.0554   0.8559   0.2860
  -3.000  -0.0871   0.01204   0.00440  -0.0551   0.8445   0.3088
  -2.750  -0.0592   0.01183   0.00423  -0.0549   0.8338   0.3335
  -2.500  -0.0320   0.01160   0.00407  -0.0546   0.8221   0.3599
  -2.000   0.0214   0.01120   0.00383  -0.0538   0.7973   0.4208
  -1.500   0.0740   0.01083   0.00365  -0.0528   0.7709   0.4980
  -1.250   0.0998   0.01066   0.00360  -0.0521   0.7570   0.5394
  -1.000   0.1257   0.01052   0.00356  -0.0515   0.7432   0.5806
  -0.750   0.1515   0.01041   0.00353  -0.0508   0.7291   0.6210
  -0.500   0.1773   0.01033   0.00352  -0.0500   0.7148   0.6604
  -0.250   0.2028   0.01026   0.00353  -0.0491   0.6999   0.6985
   0.000   0.2283   0.01022   0.00356  -0.0483   0.6854   0.7353
   0.250   0.2539   0.01021   0.00360  -0.0474   0.6709   0.7712
   0.500   0.2799   0.01023   0.00366  -0.0465   0.6569   0.8056
   0.750   0.3066   0.01029   0.00372  -0.0458   0.6426   0.8377
   1.000   0.3345   0.01038   0.00381  -0.0454   0.6280   0.8676
   1.250   0.3649   0.01049   0.00390  -0.0455   0.6136   0.8932
   1.500   0.3965   0.01063   0.00398  -0.0459   0.5993   0.9156
   1.750   0.4295   0.01077   0.00407  -0.0467   0.5851   0.9342
   2.000   0.4639   0.01093   0.00416  -0.0479   0.5708   0.9496
   2.250   0.4993   0.01110   0.00425  -0.0494   0.5564   0.9629
   2.500   0.5356   0.01125   0.00435  -0.0511   0.5419   0.9745
   2.750   0.5747   0.01142   0.00446  -0.0535   0.5274   0.9849
   3.000   0.6169   0.01160   0.00458  -0.0565   0.5125   0.9946
   3.250   0.6524   0.01176   0.00468  -0.0583   0.4981   1.0000
   3.750   0.6952   0.01208   0.00488  -0.0558   0.4713   1.0000
   4.000   0.7168   0.01225   0.00502  -0.0546   0.4578   1.0000
   4.250   0.7382   0.01245   0.00516  -0.0534   0.4443   1.0000
   4.500   0.7594   0.01266   0.00531  -0.0521   0.4300   1.0000
   4.750   0.7805   0.01288   0.00548  -0.0508   0.4150   1.0000
   5.000   0.8017   0.01311   0.00566  -0.0495   0.3991   1.0000
   5.250   0.8226   0.01335   0.00586  -0.0481   0.3824   1.0000
   5.500   0.8434   0.01363   0.00608  -0.0468   0.3648   1.0000
   5.750   0.8642   0.01392   0.00631  -0.0455   0.3467   1.0000
   6.000   0.8850   0.01424   0.00657  -0.0442   0.3277   1.0000
   6.250   0.9054   0.01459   0.00686  -0.0429   0.3079   1.0000
   6.500   0.9256   0.01498   0.00718  -0.0416   0.2879   1.0000
   6.750   0.9452   0.01541   0.00752  -0.0402   0.2679   1.0000
   7.000   0.9645   0.01588   0.00790  -0.0388   0.2484   1.0000
   7.250   0.9840   0.01635   0.00831  -0.0375   0.2291   1.0000
   7.500   1.0030   0.01685   0.00874  -0.0361   0.2104   1.0000
   7.750   1.0214   0.01739   0.00921  -0.0346   0.1924   1.0000
   8.000   1.0393   0.01797   0.00972  -0.0331   0.1753   1.0000
   8.250   1.0566   0.01856   0.01025  -0.0316   0.1596   1.0000
   8.500   1.0735   0.01918   0.01081  -0.0300   0.1454   1.0000
   8.750   1.0898   0.01981   0.01141  -0.0283   0.1328   1.0000
   9.000   1.1049   0.02045   0.01203  -0.0264   0.1219   1.0000
   9.250   1.1184   0.02113   0.01268  -0.0243   0.1126   1.0000
   9.500   1.1314   0.02186   0.01339  -0.0223   0.1040   1.0000
   9.750   1.1454   0.02257   0.01413  -0.0204   0.0965   1.0000
  10.000   1.1577   0.02340   0.01495  -0.0185   0.0902   1.0000
  10.250   1.1705   0.02423   0.01580  -0.0167   0.0842   1.0000
  10.500   1.1820   0.02516   0.01675  -0.0149   0.0793   1.0000
  10.750   1.1937   0.02611   0.01775  -0.0132   0.0746   1.0000
  11.000   1.2034   0.02722   0.01887  -0.0114   0.0709   1.0000
  11.250   1.2147   0.02826   0.01999  -0.0099   0.0671   1.0000
  11.500   1.2232   0.02954   0.02128  -0.0083   0.0639   1.0000
  11.750   1.2322   0.03083   0.02264  -0.0069   0.0611   1.0000
  12.000   1.2411   0.03217   0.02407  -0.0056   0.0583   1.0000
  12.250   1.2473   0.03378   0.02571  -0.0044   0.0561   1.0000
  12.500   1.2542   0.03540   0.02741  -0.0033   0.0539   1.0000
  12.750   1.2613   0.03706   0.02916  -0.0024   0.0518   1.0000
  13.000   1.2663   0.03896   0.03113  -0.0016   0.0500   1.0000
  13.250   1.2685   0.04121   0.03341  -0.0009   0.0485   1.0000
  13.500   1.2740   0.04320   0.03553  -0.0003   0.0469   1.0000
  13.750   1.2780   0.04541   0.03784   0.0001   0.0454   1.0000
  14.000   1.2805   0.04783   0.04034   0.0003   0.0441   1.0000
  14.250   1.2810   0.05053   0.04310   0.0004   0.0430   1.0000
  14.500   1.2807   0.05337   0.04601   0.0004   0.0420   1.0000
  14.750   1.2825   0.05607   0.04886   0.0003   0.0408   1.0000
  15.000   1.2832   0.05898   0.05188   0.0000   0.0397   1.0000
  15.250   1.2827   0.06208   0.05508  -0.0004   0.0388   1.0000
  15.500   1.2812   0.06541   0.05848  -0.0011   0.0380   1.0000
  15.750   1.2782   0.06896   0.06209  -0.0018   0.0373   1.0000
  16.000   1.2760   0.07248   0.06570  -0.0026   0.0366   1.0000
  16.250   1.2742   0.07601   0.06938  -0.0034   0.0358   1.0000
  16.500   1.2716   0.07971   0.07321  -0.0044   0.0350   1.0000
  16.750   1.2685   0.08357   0.07718  -0.0056   0.0343   1.0000
  17.000   1.2648   0.08756   0.08127  -0.0069   0.0337   1.0000
  17.250   1.2607   0.09167   0.08546  -0.0083   0.0331   1.0000
  17.500   1.2561   0.09589   0.08975  -0.0098   0.0326   1.0000
  17.750   1.2522   0.09999   0.09389  -0.0113   0.0321   1.0000
  18.000   1.2466   0.10457   0.09865  -0.0132   0.0315   1.0000
  18.250   1.2406   0.10926   0.10349  -0.0152   0.0309   1.0000
  18.500   1.2343   0.11407   0.10843  -0.0173   0.0304   1.0000
  18.750   1.2280   0.11896   0.11344  -0.0196   0.0299   1.0000
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