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NACA 2414 (n2414-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 2414 (n2414-il)
Reynolds number: 500,000
Max Cl/Cd: 79.41 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n2414-il-500000-n5.txt
Download as CSV file: xf-n2414-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -1.0317   0.08950   0.08559  -0.0404   1.0000   0.0206
 -17.250  -1.0560   0.08197   0.07794  -0.0445   1.0000   0.0206
 -17.000  -1.0803   0.07457   0.07041  -0.0486   1.0000   0.0207
 -16.750  -1.1030   0.06746   0.06316  -0.0526   1.0000   0.0208
 -16.500  -1.1230   0.06070   0.05626  -0.0566   1.0000   0.0208
 -16.250  -1.1389   0.05453   0.04994  -0.0604   1.0000   0.0209
 -16.000  -1.1506   0.04906   0.04433  -0.0639   1.0000   0.0211
 -15.750  -1.1582   0.04437   0.03950  -0.0669   1.0000   0.0212
 -15.500  -1.1625   0.04041   0.03541  -0.0693   1.0000   0.0214
 -15.250  -1.1638   0.03714   0.03200  -0.0709   1.0000   0.0217
 -15.000  -1.1631   0.03444   0.02918  -0.0718   1.0000   0.0219
 -14.750  -1.1605   0.03224   0.02685  -0.0721   1.0000   0.0221
 -14.500  -1.1584   0.03028   0.02479  -0.0716   1.0000   0.0224
 -14.250  -1.1559   0.02861   0.02305  -0.0705   1.0000   0.0227
 -14.000  -1.1517   0.02730   0.02167  -0.0688   1.0000   0.0230
 -13.750  -1.1470   0.02625   0.02055  -0.0666   1.0000   0.0233
 -13.500  -1.1431   0.02539   0.01964  -0.0636   1.0000   0.0237
 -13.250  -1.1367   0.02464   0.01882  -0.0608   1.0000   0.0241
 -13.000  -1.1282   0.02394   0.01805  -0.0582   1.0000   0.0246
 -12.750  -1.1186   0.02329   0.01733  -0.0556   1.0000   0.0251
 -12.500  -1.1084   0.02269   0.01665  -0.0530   1.0000   0.0256
 -12.250  -1.0987   0.02205   0.01596  -0.0502   1.0000   0.0261
 -12.000  -1.0889   0.02142   0.01529  -0.0475   1.0000   0.0266
 -11.750  -1.0701   0.02078   0.01461  -0.0465   0.9991   0.0272
 -11.500  -1.0420   0.02013   0.01390  -0.0473   0.9971   0.0281
 -11.250  -1.0129   0.01952   0.01323  -0.0481   0.9951   0.0290
 -11.000  -0.9829   0.01896   0.01259  -0.0491   0.9934   0.0298
 -10.750  -0.9560   0.01830   0.01191  -0.0496   0.9905   0.0308
 -10.500  -0.9269   0.01776   0.01135  -0.0503   0.9878   0.0320
 -10.250  -0.8964   0.01728   0.01081  -0.0513   0.9856   0.0334
 -10.000  -0.8650   0.01677   0.01026  -0.0524   0.9837   0.0347
  -9.750  -0.8329   0.01625   0.00972  -0.0537   0.9822   0.0362
  -9.500  -0.8055   0.01582   0.00926  -0.0539   0.9780   0.0376
  -9.250  -0.7751   0.01542   0.00881  -0.0547   0.9748   0.0392
  -9.000  -0.7444   0.01495   0.00834  -0.0556   0.9720   0.0411
  -8.750  -0.7125   0.01456   0.00792  -0.0567   0.9697   0.0434
  -8.500  -0.6864   0.01421   0.00754  -0.0564   0.9639   0.0454
  -8.250  -0.6574   0.01382   0.00716  -0.0568   0.9594   0.0478
  -8.000  -0.6264   0.01348   0.00678  -0.0576   0.9558   0.0504
  -7.750  -0.6006   0.01314   0.00645  -0.0572   0.9488   0.0533
  -7.500  -0.5718   0.01282   0.00612  -0.0574   0.9429   0.0567
  -7.250  -0.5444   0.01251   0.00580  -0.0574   0.9361   0.0602
  -7.000  -0.5172   0.01223   0.00550  -0.0572   0.9282   0.0643
  -6.750  -0.4897   0.01193   0.00521  -0.0571   0.9211   0.0687
  -6.500  -0.4630   0.01169   0.00495  -0.0568   0.9126   0.0735
  -6.250  -0.4358   0.01141   0.00468  -0.0567   0.9050   0.0789
  -6.000  -0.4089   0.01120   0.00445  -0.0564   0.8959   0.0844
  -5.750  -0.3819   0.01095   0.00420  -0.0562   0.8874   0.0914
  -5.500  -0.3550   0.01074   0.00399  -0.0559   0.8775   0.0983
  -5.250  -0.3279   0.01054   0.00378  -0.0557   0.8679   0.1060
  -5.000  -0.3009   0.01033   0.00358  -0.0554   0.8574   0.1151
  -4.750  -0.2739   0.01015   0.00340  -0.0551   0.8466   0.1248
  -4.500  -0.2467   0.00998   0.00322  -0.0549   0.8358   0.1355
  -4.250  -0.2197   0.00982   0.00306  -0.0547   0.8237   0.1479
  -4.000  -0.1926   0.00965   0.00291  -0.0544   0.8117   0.1614
  -3.750  -0.1655   0.00951   0.00277  -0.0542   0.7996   0.1756
  -3.500  -0.1385   0.00937   0.00264  -0.0539   0.7863   0.1903
  -3.250  -0.1113   0.00925   0.00253  -0.0537   0.7730   0.2061
  -3.000  -0.0841   0.00913   0.00242  -0.0534   0.7598   0.2232
  -2.750  -0.0571   0.00903   0.00233  -0.0532   0.7460   0.2411
  -2.500  -0.0301   0.00894   0.00224  -0.0529   0.7316   0.2601
  -2.250  -0.0029   0.00885   0.00217  -0.0527   0.7170   0.2796
  -2.000   0.0242   0.00877   0.00210  -0.0525   0.7021   0.2999
  -1.750   0.0512   0.00869   0.00204  -0.0522   0.6876   0.3217
  -1.500   0.0782   0.00863   0.00200  -0.0520   0.6727   0.3459
  -1.000   0.1318   0.00850   0.00192  -0.0514   0.6432   0.3987
  -0.750   0.1586   0.00841   0.00190  -0.0512   0.6287   0.4310
  -0.500   0.1852   0.00832   0.00190  -0.0509   0.6143   0.4689
  -0.250   0.2118   0.00825   0.00190  -0.0505   0.6006   0.5080
   0.000   0.2382   0.00820   0.00192  -0.0502   0.5866   0.5457
   0.250   0.2647   0.00816   0.00194  -0.0498   0.5730   0.5817
   0.500   0.2913   0.00812   0.00198  -0.0495   0.5595   0.6171
   0.750   0.3178   0.00809   0.00202  -0.0491   0.5465   0.6518
   1.000   0.3441   0.00809   0.00208  -0.0487   0.5339   0.6852
   1.500   0.3966   0.00808   0.00221  -0.0477   0.5092   0.7530
   1.750   0.4225   0.00809   0.00229  -0.0471   0.4981   0.7861
   2.000   0.4481   0.00812   0.00239  -0.0465   0.4862   0.8187
   2.250   0.4740   0.00816   0.00249  -0.0458   0.4750   0.8504
   2.500   0.4995   0.00823   0.00260  -0.0451   0.4636   0.8801
   2.750   0.5259   0.00835   0.00272  -0.0445   0.4511   0.9058
   3.000   0.5542   0.00847   0.00284  -0.0444   0.4383   0.9276
   3.250   0.5843   0.00862   0.00296  -0.0447   0.4251   0.9449
   3.500   0.6159   0.00880   0.00309  -0.0455   0.4111   0.9588
   3.750   0.6485   0.00899   0.00323  -0.0465   0.3956   0.9709
   4.000   0.6836   0.00921   0.00338  -0.0480   0.3786   0.9826
   4.250   0.7211   0.00945   0.00354  -0.0502   0.3589   0.9899
   4.500   0.7552   0.00971   0.00371  -0.0517   0.3382   0.9946
   4.750   0.7891   0.00998   0.00389  -0.0532   0.3175   0.9983
   5.000   0.8155   0.01027   0.00407  -0.0530   0.2977   1.0000
   5.250   0.8361   0.01053   0.00425  -0.0517   0.2790   1.0000
   5.500   0.8568   0.01082   0.00445  -0.0503   0.2603   1.0000
   5.750   0.8774   0.01111   0.00467  -0.0490   0.2423   1.0000
   6.000   0.8980   0.01143   0.00490  -0.0476   0.2246   1.0000
   6.250   0.9188   0.01177   0.00516  -0.0464   0.2070   1.0000
   6.500   0.9397   0.01214   0.00543  -0.0451   0.1893   1.0000
   6.750   0.9605   0.01253   0.00573  -0.0439   0.1720   1.0000
   7.000   0.9815   0.01293   0.00605  -0.0427   0.1562   1.0000
   7.250   1.0026   0.01333   0.00638  -0.0416   0.1416   1.0000
   7.500   1.0237   0.01375   0.00673  -0.0405   0.1285   1.0000
   7.750   1.0449   0.01415   0.00708  -0.0395   0.1170   1.0000
   8.000   1.0660   0.01456   0.00745  -0.0384   0.1069   1.0000
   8.250   1.0867   0.01499   0.00784  -0.0373   0.0977   1.0000
   8.500   1.1069   0.01544   0.00825  -0.0361   0.0895   1.0000
   8.750   1.1268   0.01590   0.00868  -0.0349   0.0821   1.0000
   9.000   1.1467   0.01633   0.00911  -0.0337   0.0759   1.0000
   9.250   1.1655   0.01682   0.00957  -0.0323   0.0703   1.0000
   9.500   1.1833   0.01729   0.01004  -0.0308   0.0654   1.0000
   9.750   1.1999   0.01778   0.01053  -0.0290   0.0613   1.0000
  10.000   1.2162   0.01830   0.01106  -0.0273   0.0572   1.0000
  10.250   1.2324   0.01886   0.01162  -0.0256   0.0539   1.0000
  10.500   1.2485   0.01943   0.01221  -0.0240   0.0508   1.0000
  10.750   1.2634   0.02008   0.01287  -0.0223   0.0481   1.0000
  11.000   1.2791   0.02070   0.01352  -0.0208   0.0457   1.0000
  11.250   1.2934   0.02142   0.01427  -0.0192   0.0434   1.0000
  11.500   1.3074   0.02218   0.01506  -0.0177   0.0415   1.0000
  11.750   1.3214   0.02295   0.01587  -0.0162   0.0396   1.0000
  12.000   1.3340   0.02385   0.01679  -0.0147   0.0379   1.0000
  12.250   1.3459   0.02481   0.01780  -0.0132   0.0365   1.0000
  12.500   1.3585   0.02577   0.01882  -0.0119   0.0352   1.0000
  12.750   1.3697   0.02684   0.01994  -0.0106   0.0339   1.0000
  13.000   1.3794   0.02808   0.02122  -0.0093   0.0326   1.0000
  13.250   1.3889   0.02938   0.02258  -0.0082   0.0316   1.0000
  13.500   1.3986   0.03071   0.02398  -0.0071   0.0306   1.0000
  13.750   1.4071   0.03219   0.02552  -0.0062   0.0296   1.0000
  14.000   1.4141   0.03385   0.02724  -0.0053   0.0287   1.0000
  14.250   1.4190   0.03576   0.02921  -0.0045   0.0279   1.0000
  14.500   1.4251   0.03764   0.03117  -0.0039   0.0273   1.0000
  14.750   1.4305   0.03965   0.03327  -0.0034   0.0266   1.0000
  15.000   1.4346   0.04184   0.03554  -0.0031   0.0259   1.0000
  15.250   1.4373   0.04424   0.03803  -0.0028   0.0253   1.0000
  15.500   1.4386   0.04689   0.04075  -0.0028   0.0248   1.0000
  15.750   1.4380   0.04983   0.04377  -0.0029   0.0243   1.0000
  16.000   1.4356   0.05307   0.04709  -0.0032   0.0239   1.0000
  16.250   1.4355   0.05613   0.05026  -0.0036   0.0234   1.0000
  16.500   1.4340   0.05943   0.05367  -0.0042   0.0230   1.0000
  16.750   1.4315   0.06292   0.05726  -0.0049   0.0226   1.0000
  17.000   1.4277   0.06665   0.06109  -0.0057   0.0221   1.0000
  17.250   1.4224   0.07065   0.06518  -0.0067   0.0218   1.0000
  17.500   1.4159   0.07491   0.06954  -0.0079   0.0214   1.0000
  17.750   1.4079   0.07942   0.07414  -0.0093   0.0211   1.0000
  18.000   1.3984   0.08422   0.07904  -0.0109   0.0209   1.0000
  18.250   1.3876   0.08932   0.08423  -0.0126   0.0206   1.0000
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