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NACA 2414 (n2414-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NACA 2414 (n2414-il)
Reynolds number: 200,000
Max Cl/Cd: 65.07 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n2414-il-200000.txt
Download as CSV file: xf-n2414-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.7757   0.07662   0.07216  -0.0588   1.0000   0.0507
 -13.500  -0.8145   0.06684   0.06220  -0.0661   1.0000   0.0504
 -13.250  -0.8486   0.05934   0.05449  -0.0712   1.0000   0.0501
 -13.000  -0.8784   0.05381   0.04871  -0.0735   1.0000   0.0500
 -12.750  -0.9045   0.04976   0.04441  -0.0730   1.0000   0.0501
 -12.500  -0.9282   0.04681   0.04122  -0.0699   1.0000   0.0502
 -12.250  -0.9473   0.04424   0.03837  -0.0659   1.0000   0.0504
 -12.000  -0.9610   0.04191   0.03571  -0.0620   1.0000   0.0508
 -11.750  -0.9600   0.03940   0.03309  -0.0595   1.0000   0.0515
 -11.500  -0.9502   0.03806   0.03175  -0.0575   1.0000   0.0524
 -11.250  -0.9413   0.03695   0.03060  -0.0552   1.0000   0.0535
 -11.000  -0.9344   0.03568   0.02922  -0.0526   1.0000   0.0546
 -10.750  -0.9298   0.03418   0.02750  -0.0496   1.0000   0.0558
 -10.500  -0.9254   0.03267   0.02568  -0.0465   1.0000   0.0570
 -10.250  -0.9184   0.03104   0.02379  -0.0436   1.0000   0.0581
 -10.000  -0.9038   0.02973   0.02253  -0.0419   1.0000   0.0595
  -9.750  -0.8901   0.02887   0.02164  -0.0399   1.0000   0.0610
  -9.500  -0.8769   0.02799   0.02064  -0.0377   1.0000   0.0630
  -9.250  -0.8640   0.02710   0.01951  -0.0354   1.0000   0.0650
  -9.000  -0.8488   0.02582   0.01819  -0.0337   1.0000   0.0669
  -8.750  -0.8323   0.02510   0.01750  -0.0320   1.0000   0.0690
  -8.500  -0.8160   0.02440   0.01671  -0.0303   1.0000   0.0715
  -8.250  -0.7994   0.02381   0.01592  -0.0285   1.0000   0.0741
  -8.000  -0.7818   0.02279   0.01498  -0.0272   1.0000   0.0770
  -7.750  -0.7636   0.02227   0.01445  -0.0258   1.0000   0.0801
  -7.500  -0.7448   0.02182   0.01383  -0.0244   1.0000   0.0836
  -7.250  -0.7258   0.02100   0.01310  -0.0233   1.0000   0.0874
  -7.000  -0.7013   0.02057   0.01264  -0.0231   0.9991   0.0922
  -6.750  -0.6627   0.01983   0.01192  -0.0257   0.9952   0.0986
  -6.500  -0.6233   0.01944   0.01144  -0.0283   0.9910   0.1061
  -6.250  -0.5855   0.01877   0.01087  -0.0307   0.9862   0.1146
  -6.000  -0.5443   0.01822   0.01035  -0.0338   0.9826   0.1249
  -5.750  -0.5092   0.01773   0.00987  -0.0355   0.9762   0.1360
  -5.500  -0.4689   0.01728   0.00946  -0.0382   0.9717   0.1497
  -5.250  -0.4320   0.01684   0.00908  -0.0403   0.9663   0.1650
  -5.000  -0.3955   0.01638   0.00872  -0.0422   0.9603   0.1824
  -4.750  -0.3540   0.01594   0.00839  -0.0452   0.9566   0.2037
  -4.500  -0.3210   0.01559   0.00810  -0.0463   0.9492   0.2255
  -4.250  -0.2822   0.01516   0.00779  -0.0486   0.9441   0.2509
  -4.000  -0.2384   0.01475   0.00748  -0.0519   0.9410   0.2812
  -3.750  -0.2077   0.01438   0.00726  -0.0525   0.9325   0.3081
  -3.500  -0.1689   0.01395   0.00695  -0.0546   0.9275   0.3408
  -3.250  -0.1287   0.01348   0.00662  -0.0570   0.9240   0.3769
  -3.000  -0.1026   0.01314   0.00642  -0.0564   0.9133   0.4105
  -2.750  -0.0668   0.01264   0.00613  -0.0577   0.9081   0.4541
  -2.500  -0.0410   0.01231   0.00597  -0.0570   0.8974   0.4985
  -2.250  -0.0087   0.01187   0.00572  -0.0574   0.8909   0.5505
  -2.000   0.0157   0.01157   0.00562  -0.0562   0.8791   0.5989
  -1.750   0.0447   0.01123   0.00545  -0.0557   0.8708   0.6490
  -1.500   0.0699   0.01099   0.00535  -0.0545   0.8589   0.6952
  -1.250   0.0953   0.01080   0.00529  -0.0532   0.8470   0.7387
  -1.000   0.1227   0.01061   0.00518  -0.0522   0.8367   0.7793
  -0.750   0.1476   0.01052   0.00516  -0.0507   0.8231   0.8165
  -0.500   0.1732   0.01049   0.00517  -0.0493   0.8094   0.8507
  -0.250   0.2011   0.01051   0.00518  -0.0483   0.7962   0.8807
   0.000   0.2322   0.01056   0.00517  -0.0480   0.7831   0.9063
   0.250   0.2667   0.01065   0.00519  -0.0486   0.7685   0.9275
   0.500   0.3046   0.01077   0.00523  -0.0500   0.7529   0.9451
   0.750   0.3467   0.01089   0.00526  -0.0525   0.7371   0.9592
   1.000   0.3925   0.01100   0.00527  -0.0558   0.7208   0.9709
   1.250   0.4388   0.01109   0.00526  -0.0594   0.7041   0.9820
   1.500   0.4880   0.01115   0.00521  -0.0638   0.6869   0.9910
   1.750   0.5369   0.01119   0.00516  -0.0682   0.6695   0.9997
   2.000   0.5600   0.01123   0.00510  -0.0675   0.6544   1.0000
   2.250   0.5821   0.01130   0.00508  -0.0665   0.6399   1.0000
   2.500   0.6043   0.01140   0.00507  -0.0655   0.6258   1.0000
   2.750   0.6259   0.01150   0.00512  -0.0644   0.6109   1.0000
   3.000   0.6477   0.01162   0.00519  -0.0632   0.5965   1.0000
   3.250   0.6696   0.01176   0.00527  -0.0621   0.5825   1.0000
   3.500   0.6916   0.01192   0.00535  -0.0609   0.5687   1.0000
   3.750   0.7137   0.01210   0.00544  -0.0597   0.5550   1.0000
   4.000   0.7351   0.01226   0.00558  -0.0585   0.5404   1.0000
   4.250   0.7567   0.01243   0.00572  -0.0572   0.5259   1.0000
   4.500   0.7784   0.01263   0.00587  -0.0559   0.5116   1.0000
   4.750   0.8000   0.01284   0.00603  -0.0547   0.4971   1.0000
   5.000   0.8215   0.01306   0.00619  -0.0533   0.4824   1.0000
   5.250   0.8426   0.01329   0.00635  -0.0520   0.4671   1.0000
   5.500   0.8636   0.01350   0.00655  -0.0506   0.4510   1.0000
   5.750   0.8845   0.01373   0.00676  -0.0492   0.4344   1.0000
   6.000   0.9053   0.01398   0.00697  -0.0478   0.4174   1.0000
   6.250   0.9258   0.01425   0.00721  -0.0464   0.3995   1.0000
   6.500   0.9461   0.01455   0.00745  -0.0449   0.3810   1.0000
   6.750   0.9663   0.01485   0.00773  -0.0435   0.3611   1.0000
   7.000   0.9861   0.01519   0.00804  -0.0420   0.3403   1.0000
   7.250   1.0051   0.01560   0.00838  -0.0405   0.3189   1.0000
   7.500   1.0230   0.01608   0.00876  -0.0388   0.2974   1.0000
   7.750   1.0412   0.01656   0.00919  -0.0372   0.2743   1.0000
   8.000   1.0578   0.01714   0.00967  -0.0354   0.2516   1.0000
   8.250   1.0738   0.01777   0.01021  -0.0336   0.2293   1.0000
   8.500   1.0891   0.01844   0.01080  -0.0316   0.2076   1.0000
   8.750   1.1026   0.01922   0.01146  -0.0295   0.1880   1.0000
   9.000   1.1149   0.02005   0.01219  -0.0272   0.1707   1.0000
   9.250   1.1258   0.02087   0.01294  -0.0247   0.1556   1.0000
   9.500   1.1355   0.02177   0.01377  -0.0221   0.1426   1.0000
   9.750   1.1468   0.02265   0.01464  -0.0198   0.1311   1.0000
  10.000   1.1575   0.02361   0.01561  -0.0176   0.1213   1.0000
  10.250   1.1659   0.02475   0.01669  -0.0153   0.1134   1.0000
  10.500   1.1766   0.02577   0.01773  -0.0133   0.1061   1.0000
  10.750   1.1857   0.02699   0.01895  -0.0113   0.1000   1.0000
  11.000   1.1956   0.02813   0.02011  -0.0095   0.0944   1.0000
  11.250   1.2040   0.02951   0.02148  -0.0077   0.0897   1.0000
  11.500   1.2142   0.03072   0.02275  -0.0061   0.0851   1.0000
  11.750   1.2216   0.03231   0.02424  -0.0045   0.0813   1.0000
  12.000   1.2318   0.03358   0.02568  -0.0031   0.0777   1.0000
  12.250   1.2408   0.03499   0.02712  -0.0019   0.0745   1.0000
  12.500   1.2502   0.03664   0.02867  -0.0005   0.0715   1.0000
  12.750   1.2583   0.03816   0.03038   0.0006   0.0689   1.0000
  13.000   1.2666   0.03974   0.03202   0.0017   0.0663   1.0000
  13.250   1.2759   0.04133   0.03357   0.0027   0.0641   1.0000
  13.500   1.2852   0.04309   0.03540   0.0037   0.0620   1.0000
  13.750   1.2909   0.04498   0.03745   0.0046   0.0600   1.0000
  14.000   1.2975   0.04682   0.03936   0.0054   0.0581   1.0000
  14.250   1.3071   0.04848   0.04099   0.0061   0.0564   1.0000
  14.500   1.3165   0.05043   0.04299   0.0070   0.0548   1.0000
  14.750   1.3182   0.05285   0.04562   0.0076   0.0536   1.0000
  15.000   1.3203   0.05529   0.04822   0.0081   0.0523   1.0000
  15.250   1.3233   0.05764   0.05067   0.0084   0.0510   1.0000
  15.500   1.3295   0.05971   0.05275   0.0088   0.0498   1.0000
  15.750   1.3432   0.06147   0.05446   0.0096   0.0484   1.0000
  16.000   1.3345   0.06506   0.05831   0.0094   0.0477   1.0000
  16.250   1.3264   0.06881   0.06230   0.0090   0.0470   1.0000
  16.500   1.3193   0.07264   0.06634   0.0083   0.0463   1.0000
  16.750   1.3127   0.07655   0.07042   0.0075   0.0456   1.0000
  17.000   1.3058   0.08059   0.07463   0.0065   0.0449   1.0000
  17.250   1.2979   0.08487   0.07907   0.0052   0.0444   1.0000
  17.500   1.2907   0.08916   0.08349   0.0038   0.0439   1.0000
  17.750   1.2871   0.09299   0.08740   0.0026   0.0433   1.0000
  18.000   1.2906   0.09583   0.09025   0.0024   0.0426   1.0000
  18.250   1.2731   0.10199   0.09660  -0.0002   0.0423   1.0000
  18.500   1.2472   0.10983   0.10470  -0.0045   0.0423   1.0000
  18.750   1.2181   0.11873   0.11386  -0.0099   0.0422   1.0000
  19.000   1.1853   0.12890   0.12428  -0.0163   0.0423   1.0000
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