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NACA 2414 (n2414-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 2414 (n2414-il)
Reynolds number: 500,000
Max Cl/Cd: 87.57 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n2414-il-500000.txt
Download as CSV file: xf-n2414-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.9646   0.10148   0.09806  -0.0372   1.0000   0.0265
 -17.500  -0.9974   0.09157   0.08796  -0.0433   1.0000   0.0265
 -17.250  -1.0183   0.08419   0.08045  -0.0478   1.0000   0.0266
 -17.000  -1.0353   0.07772   0.07386  -0.0517   1.0000   0.0267
 -16.750  -1.0497   0.07185   0.06787  -0.0553   1.0000   0.0269
 -16.500  -1.0622   0.06632   0.06223  -0.0587   1.0000   0.0270
 -16.250  -1.0723   0.06125   0.05705  -0.0619   1.0000   0.0272
 -16.000  -1.0805   0.05654   0.05222  -0.0648   1.0000   0.0274
 -15.750  -1.0871   0.05218   0.04774  -0.0675   1.0000   0.0277
 -15.500  -1.0920   0.04820   0.04363  -0.0699   1.0000   0.0279
 -15.250  -1.0954   0.04460   0.03990  -0.0718   1.0000   0.0282
 -15.000  -1.0974   0.04139   0.03655  -0.0733   1.0000   0.0285
 -14.750  -1.0978   0.03859   0.03361  -0.0742   1.0000   0.0288
 -14.500  -1.0969   0.03617   0.03105  -0.0745   1.0000   0.0292
 -14.250  -1.0946   0.03411   0.02884  -0.0743   1.0000   0.0295
 -14.000  -1.0911   0.03239   0.02698  -0.0736   1.0000   0.0298
 -13.750  -1.0905   0.03042   0.02493  -0.0721   1.0000   0.0302
 -13.500  -1.0874   0.02895   0.02342  -0.0702   1.0000   0.0306
 -13.250  -1.0832   0.02788   0.02230  -0.0679   1.0000   0.0311
 -13.000  -1.0806   0.02702   0.02140  -0.0647   1.0000   0.0315
 -12.750  -1.0759   0.02623   0.02057  -0.0615   1.0000   0.0320
 -12.500  -1.0688   0.02549   0.01976  -0.0587   1.0000   0.0326
 -12.250  -1.0609   0.02480   0.01898  -0.0558   1.0000   0.0332
 -12.000  -1.0521   0.02417   0.01826  -0.0529   1.0000   0.0339
 -11.750  -1.0443   0.02341   0.01741  -0.0499   1.0000   0.0345
 -11.500  -1.0382   0.02248   0.01647  -0.0467   1.0000   0.0352
 -11.250  -1.0279   0.02187   0.01585  -0.0440   1.0000   0.0360
 -11.000  -1.0161   0.02132   0.01527  -0.0415   1.0000   0.0368
 -10.750  -1.0033   0.02080   0.01468  -0.0391   1.0000   0.0377
 -10.500  -0.9895   0.02031   0.01411  -0.0368   1.0000   0.0386
 -10.250  -0.9760   0.01971   0.01344  -0.0346   1.0000   0.0395
 -10.000  -0.9485   0.01889   0.01265  -0.0353   0.9984   0.0410
  -9.750  -0.9149   0.01839   0.01211  -0.0369   0.9963   0.0428
  -9.500  -0.8800   0.01798   0.01161  -0.0387   0.9944   0.0446
  -9.250  -0.8488   0.01715   0.01080  -0.0400   0.9922   0.0467
  -9.000  -0.8164   0.01669   0.01031  -0.0413   0.9893   0.0488
  -8.750  -0.7818   0.01632   0.00986  -0.0428   0.9868   0.0509
  -8.500  -0.7482   0.01562   0.00920  -0.0445   0.9846   0.0539
  -8.250  -0.7114   0.01526   0.00881  -0.0466   0.9830   0.0570
  -8.000  -0.6802   0.01470   0.00826  -0.0476   0.9795   0.0603
  -7.750  -0.6467   0.01432   0.00786  -0.0489   0.9759   0.0639
  -7.500  -0.6109   0.01382   0.00737  -0.0508   0.9734   0.0684
  -7.250  -0.5727   0.01346   0.00701  -0.0530   0.9716   0.0734
  -7.000  -0.5345   0.01296   0.00655  -0.0554   0.9702   0.0796
  -6.750  -0.5041   0.01263   0.00621  -0.0559   0.9651   0.0854
  -6.500  -0.4712   0.01223   0.00586  -0.0570   0.9611   0.0927
  -6.250  -0.4374   0.01183   0.00549  -0.0583   0.9579   0.1011
  -6.000  -0.4042   0.01148   0.00517  -0.0594   0.9546   0.1102
  -5.750  -0.3781   0.01122   0.00492  -0.0589   0.9471   0.1193
  -5.500  -0.3478   0.01086   0.00462  -0.0594   0.9421   0.1312
  -5.250  -0.3209   0.01057   0.00438  -0.0591   0.9352   0.1433
  -5.000  -0.2935   0.01028   0.00414  -0.0588   0.9279   0.1571
  -4.750  -0.2659   0.01002   0.00391  -0.0586   0.9210   0.1723
  -4.500  -0.2397   0.00977   0.00372  -0.0581   0.9121   0.1886
  -4.250  -0.2123   0.00953   0.00352  -0.0579   0.9043   0.2068
  -4.000  -0.1858   0.00932   0.00335  -0.0574   0.8945   0.2256
  -3.750  -0.1587   0.00912   0.00319  -0.0571   0.8853   0.2455
  -3.500  -0.1318   0.00891   0.00304  -0.0568   0.8751   0.2666
  -3.250  -0.1051   0.00872   0.00291  -0.0564   0.8642   0.2892
  -3.000  -0.0778   0.00856   0.00277  -0.0561   0.8539   0.3134
  -2.750  -0.0511   0.00838   0.00266  -0.0557   0.8416   0.3383
  -2.500  -0.0242   0.00822   0.00256  -0.0554   0.8295   0.3659
  -2.250   0.0026   0.00806   0.00245  -0.0550   0.8173   0.3957
  -2.000   0.0291   0.00789   0.00236  -0.0546   0.8039   0.4302
  -1.750   0.0554   0.00772   0.00230  -0.0542   0.7901   0.4708
  -1.500   0.0818   0.00758   0.00225  -0.0537   0.7760   0.5153
  -1.250   0.1079   0.00744   0.00221  -0.0532   0.7618   0.5581
  -1.000   0.1340   0.00734   0.00218  -0.0527   0.7472   0.6001
  -0.750   0.1601   0.00725   0.00217  -0.0521   0.7322   0.6405
  -0.500   0.1861   0.00718   0.00217  -0.0515   0.7166   0.6796
  -0.250   0.2121   0.00712   0.00219  -0.0509   0.7012   0.7170
   0.000   0.2379   0.00708   0.00221  -0.0501   0.6856   0.7533
   0.250   0.2635   0.00706   0.00225  -0.0494   0.6703   0.7882
   0.500   0.2890   0.00707   0.00230  -0.0486   0.6551   0.8215
   0.750   0.3143   0.00710   0.00237  -0.0477   0.6400   0.8528
   1.000   0.3396   0.00718   0.00244  -0.0467   0.6251   0.8816
   1.250   0.3655   0.00726   0.00252  -0.0459   0.6103   0.9066
   1.500   0.3929   0.00738   0.00262  -0.0455   0.5958   0.9282
   1.750   0.4224   0.00751   0.00271  -0.0455   0.5818   0.9455
   2.000   0.4544   0.00767   0.00281  -0.0462   0.5679   0.9594
   2.250   0.4881   0.00785   0.00291  -0.0472   0.5539   0.9707
   2.500   0.5264   0.00802   0.00301  -0.0494   0.5392   0.9781
   2.750   0.5660   0.00818   0.00312  -0.0518   0.5245   0.9839
   3.000   0.6069   0.00833   0.00321  -0.0546   0.5097   0.9887
   3.250   0.6460   0.00850   0.00332  -0.0570   0.4953   0.9938
   3.500   0.6874   0.00865   0.00341  -0.0600   0.4804   0.9977
   3.750   0.7207   0.00881   0.00350  -0.0613   0.4660   1.0000
   4.000   0.7426   0.00892   0.00357  -0.0601   0.4525   1.0000
   4.250   0.7645   0.00905   0.00365  -0.0590   0.4387   1.0000
   4.500   0.7862   0.00919   0.00376  -0.0578   0.4248   1.0000
   4.750   0.8077   0.00936   0.00387  -0.0565   0.4105   1.0000
   5.000   0.8291   0.00954   0.00399  -0.0553   0.3950   1.0000
   5.250   0.8505   0.00974   0.00413  -0.0540   0.3785   1.0000
   5.500   0.8719   0.00996   0.00429  -0.0527   0.3612   1.0000
   5.750   0.8932   0.01020   0.00446  -0.0514   0.3434   1.0000
   6.000   0.9143   0.01046   0.00465  -0.0501   0.3248   1.0000
   6.250   0.9352   0.01075   0.00487  -0.0488   0.3050   1.0000
   6.500   0.9559   0.01109   0.00511  -0.0475   0.2846   1.0000
   6.750   0.9765   0.01146   0.00538  -0.0462   0.2639   1.0000
   7.000   0.9977   0.01183   0.00567  -0.0450   0.2432   1.0000
   7.250   1.0185   0.01224   0.00598  -0.0438   0.2225   1.0000
   7.500   1.0388   0.01270   0.00633  -0.0426   0.2025   1.0000
   7.750   1.0593   0.01315   0.00670  -0.0414   0.1839   1.0000
   8.000   1.0796   0.01362   0.00709  -0.0402   0.1657   1.0000
   8.250   1.0994   0.01412   0.00750  -0.0389   0.1488   1.0000
   8.500   1.1187   0.01464   0.00795  -0.0376   0.1336   1.0000
   8.750   1.1377   0.01518   0.00841  -0.0362   0.1203   1.0000
   9.000   1.1563   0.01572   0.00890  -0.0348   0.1086   1.0000
   9.250   1.1743   0.01627   0.00941  -0.0333   0.0987   1.0000
   9.500   1.1908   0.01687   0.00996  -0.0316   0.0902   1.0000
   9.750   1.2059   0.01744   0.01051  -0.0296   0.0831   1.0000
  10.000   1.2215   0.01801   0.01108  -0.0277   0.0772   1.0000
  10.250   1.2339   0.01876   0.01180  -0.0255   0.0717   1.0000
  10.500   1.2504   0.01931   0.01239  -0.0239   0.0675   1.0000
  10.750   1.2618   0.02017   0.01322  -0.0218   0.0633   1.0000
  11.000   1.2775   0.02080   0.01391  -0.0202   0.0601   1.0000
  11.250   1.2898   0.02165   0.01476  -0.0184   0.0570   1.0000
  11.500   1.3009   0.02259   0.01574  -0.0166   0.0543   1.0000
  11.750   1.3145   0.02341   0.01661  -0.0151   0.0518   1.0000
  12.000   1.3239   0.02453   0.01774  -0.0133   0.0496   1.0000
  12.250   1.3325   0.02577   0.01902  -0.0116   0.0477   1.0000
  12.500   1.3442   0.02682   0.02015  -0.0103   0.0459   1.0000
  12.750   1.3537   0.02807   0.02145  -0.0090   0.0443   1.0000
  13.000   1.3570   0.02986   0.02325  -0.0074   0.0427   1.0000
  13.250   1.3659   0.03129   0.02477  -0.0063   0.0414   1.0000
  13.500   1.3747   0.03277   0.02633  -0.0054   0.0400   1.0000
  13.750   1.3818   0.03446   0.02808  -0.0046   0.0388   1.0000
  14.000   1.3844   0.03661   0.03027  -0.0037   0.0378   1.0000
  14.250   1.3829   0.03924   0.03296  -0.0030   0.0368   1.0000
  14.500   1.3895   0.04118   0.03501  -0.0026   0.0359   1.0000
  14.750   1.3935   0.04342   0.03734  -0.0022   0.0350   1.0000
  15.000   1.3964   0.04585   0.03985  -0.0021   0.0342   1.0000
  15.250   1.3977   0.04853   0.04260  -0.0021   0.0335   1.0000
  15.500   1.3954   0.05165   0.04577  -0.0022   0.0328   1.0000
  15.750   1.3883   0.05533   0.04950  -0.0023   0.0321   1.0000
  16.000   1.3906   0.05815   0.05245  -0.0027   0.0315   1.0000
  16.250   1.3909   0.06125   0.05565  -0.0032   0.0309   1.0000
  16.500   1.3898   0.06454   0.05904  -0.0038   0.0303   1.0000
  16.750   1.3880   0.06799   0.06258  -0.0046   0.0297   1.0000
  17.000   1.3855   0.07161   0.06626  -0.0054   0.0292   1.0000
  17.250   1.3817   0.07539   0.07012  -0.0064   0.0287   1.0000
  17.500   1.3763   0.07935   0.07413  -0.0074   0.0283   1.0000
  17.750   1.3698   0.08328   0.07809  -0.0081   0.0278   1.0000
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