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NACA 64-210 (naca64210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64-210 (naca64210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.87 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca64210-il-1000000-n5.txt
Download as CSV file: xf-naca64210-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64-210                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -1.0280   0.05482   0.05277  -0.0422   1.0000   0.0043
 -14.250  -1.0734   0.04498   0.04264  -0.0484   1.0000   0.0043
 -14.000  -1.0832   0.04110   0.03862  -0.0499   1.0000   0.0043
 -13.750  -1.1009   0.03686   0.03417  -0.0506   1.0000   0.0043
 -13.500  -1.1001   0.03486   0.03207  -0.0502   1.0000   0.0044
 -13.250  -1.1074   0.03243   0.02947  -0.0489   1.0000   0.0045
 -13.000  -1.1125   0.03054   0.02743  -0.0466   1.0000   0.0046
 -12.750  -1.1076   0.02896   0.02570  -0.0450   1.0000   0.0046
 -12.500  -1.0997   0.02726   0.02381  -0.0437   1.0000   0.0047
 -12.250  -1.0870   0.02591   0.02232  -0.0427   1.0000   0.0049
 -12.000  -1.0721   0.02469   0.02096  -0.0418   1.0000   0.0050
 -11.750  -1.0569   0.02338   0.01949  -0.0409   1.0000   0.0051
 -11.500  -1.0398   0.02223   0.01819  -0.0401   1.0000   0.0053
 -11.250  -1.0213   0.02119   0.01702  -0.0394   1.0000   0.0054
 -11.000  -1.0009   0.02039   0.01611  -0.0388   1.0000   0.0055
 -10.750  -0.9826   0.01919   0.01477  -0.0381   1.0000   0.0058
 -10.500  -0.9599   0.01869   0.01424  -0.0377   1.0000   0.0061
 -10.250  -0.9372   0.01818   0.01367  -0.0373   1.0000   0.0063
 -10.000  -0.9145   0.01765   0.01308  -0.0368   1.0000   0.0066
  -9.750  -0.8920   0.01707   0.01243  -0.0364   1.0000   0.0069
  -9.500  -0.8696   0.01646   0.01174  -0.0358   1.0000   0.0072
  -9.250  -0.8472   0.01587   0.01107  -0.0352   1.0000   0.0074
  -9.000  -0.8181   0.01522   0.01033  -0.0361   0.9929   0.0077
  -8.750  -0.7859   0.01469   0.00971  -0.0375   0.9842   0.0080
  -8.500  -0.7539   0.01390   0.00881  -0.0390   0.9739   0.0083
  -8.250  -0.7225   0.01327   0.00812  -0.0403   0.9624   0.0089
  -8.000  -0.6931   0.01293   0.00773  -0.0410   0.9489   0.0093
  -7.750  -0.6664   0.01265   0.00740  -0.0410   0.9343   0.0098
  -7.500  -0.6411   0.01235   0.00702  -0.0407   0.9204   0.0103
  -7.250  -0.6162   0.01197   0.00653  -0.0403   0.9075   0.0107
  -7.000  -0.5909   0.01163   0.00610  -0.0400   0.8954   0.0110
  -6.750  -0.5654   0.01130   0.00569  -0.0397   0.8838   0.0113
  -6.500  -0.5396   0.01098   0.00529  -0.0394   0.8730   0.0115
  -6.250  -0.5145   0.01050   0.00472  -0.0391   0.8621   0.0124
  -6.000  -0.4882   0.01021   0.00437  -0.0390   0.8513   0.0131
  -5.750  -0.4616   0.00994   0.00405  -0.0389   0.8412   0.0136
  -5.500  -0.4349   0.00970   0.00374  -0.0388   0.8314   0.0142
  -5.250  -0.4080   0.00948   0.00346  -0.0387   0.8215   0.0149
  -5.000  -0.3808   0.00929   0.00320  -0.0387   0.8122   0.0157
  -4.750  -0.3537   0.00905   0.00290  -0.0386   0.8032   0.0166
  -4.500  -0.3264   0.00882   0.00264  -0.0386   0.7941   0.0184
  -4.250  -0.2989   0.00865   0.00244  -0.0387   0.7858   0.0202
  -4.000  -0.2713   0.00851   0.00225  -0.0387   0.7766   0.0219
  -3.750  -0.2436   0.00835   0.00206  -0.0388   0.7676   0.0244
  -3.500  -0.2159   0.00820   0.00189  -0.0388   0.7590   0.0280
  -3.250  -0.1880   0.00809   0.00175  -0.0389   0.7503   0.0308
  -3.000  -0.1601   0.00795   0.00160  -0.0390   0.7424   0.0373
  -2.750  -0.1323   0.00781   0.00147  -0.0391   0.7340   0.0486
  -2.500  -0.1045   0.00758   0.00133  -0.0392   0.7259   0.0797
  -2.000  -0.0500   0.00674   0.00101  -0.0397   0.7090   0.2479
  -1.750  -0.0229   0.00629   0.00085  -0.0399   0.7011   0.3501
  -1.500   0.0045   0.00586   0.00076  -0.0401   0.6933   0.4586
  -1.250   0.0324   0.00569   0.00073  -0.0403   0.6860   0.5106
  -1.000   0.0602   0.00549   0.00072  -0.0404   0.6785   0.5758
  -0.750   0.0882   0.00540   0.00073  -0.0405   0.6713   0.6154
  -0.500   0.1166   0.00538   0.00072  -0.0406   0.6634   0.6286
  -0.250   0.1451   0.00538   0.00072  -0.0408   0.6561   0.6385
   0.000   0.1736   0.00540   0.00073  -0.0409   0.6488   0.6466
   0.250   0.2021   0.00541   0.00074  -0.0410   0.6422   0.6540
   0.500   0.2306   0.00543   0.00076  -0.0412   0.6339   0.6617
   0.750   0.2589   0.00545   0.00078  -0.0413   0.6247   0.6700
   1.000   0.2872   0.00549   0.00082  -0.0414   0.6145   0.6777
   1.250   0.3152   0.00555   0.00085  -0.0415   0.5957   0.6858
   1.500   0.3426   0.00568   0.00089  -0.0414   0.5661   0.6934
   1.750   0.3697   0.00587   0.00095  -0.0413   0.5254   0.7017
   2.000   0.3968   0.00604   0.00103  -0.0413   0.4882   0.7100
   2.250   0.4223   0.00649   0.00117  -0.0411   0.4026   0.7190
   2.500   0.4464   0.00714   0.00143  -0.0407   0.2968   0.7280
   2.750   0.4716   0.00766   0.00167  -0.0406   0.2182   0.7366
   3.000   0.4965   0.00822   0.00194  -0.0403   0.1376   0.7456
   3.250   0.5220   0.00868   0.00219  -0.0401   0.0803   0.7542
   3.750   0.5750   0.00925   0.00262  -0.0399   0.0352   0.7731
   4.000   0.6019   0.00943   0.00281  -0.0398   0.0303   0.7827
   4.500   0.6558   0.00979   0.00323  -0.0397   0.0240   0.8020
   4.750   0.6824   0.01000   0.00347  -0.0396   0.0210   0.8116
   5.250   0.7351   0.01044   0.00399  -0.0392   0.0166   0.8326
   5.500   0.7611   0.01069   0.00426  -0.0390   0.0151   0.8435
   5.750   0.7866   0.01098   0.00460  -0.0386   0.0136   0.8547
   6.000   0.8118   0.01129   0.00498  -0.0382   0.0129   0.8669
   6.500   0.8612   0.01186   0.00570  -0.0372   0.0120   0.8942
   6.750   0.8851   0.01215   0.00606  -0.0366   0.0115   0.9095
   7.000   0.9080   0.01246   0.00645  -0.0357   0.0111   0.9265
   7.250   0.9301   0.01278   0.00685  -0.0347   0.0107   0.9480
   7.500   0.9574   0.01317   0.00730  -0.0349   0.0104   1.0000
   7.750   0.9818   0.01365   0.00782  -0.0346   0.0101   1.0000
   8.000   1.0052   0.01426   0.00849  -0.0341   0.0095   1.0000
   8.250   1.0272   0.01503   0.00933  -0.0334   0.0092   1.0000
   8.500   1.0509   0.01553   0.00989  -0.0330   0.0090   1.0000
   8.750   1.0744   0.01605   0.01046  -0.0325   0.0089   1.0000
   9.000   1.0974   0.01661   0.01109  -0.0320   0.0087   1.0000
   9.250   1.1201   0.01718   0.01172  -0.0315   0.0085   1.0000
   9.500   1.1425   0.01776   0.01237  -0.0309   0.0082   1.0000
   9.750   1.1647   0.01833   0.01301  -0.0304   0.0079   1.0000
  10.000   1.1868   0.01887   0.01361  -0.0298   0.0076   1.0000
  10.250   1.2087   0.01939   0.01417  -0.0292   0.0073   1.0000
  10.500   1.2297   0.02000   0.01483  -0.0285   0.0071   1.0000
  10.750   1.2498   0.02065   0.01554  -0.0277   0.0069   1.0000
  11.000   1.2681   0.02147   0.01643  -0.0267   0.0067   1.0000
  11.250   1.2810   0.02285   0.01794  -0.0251   0.0063   1.0000
  11.500   1.2983   0.02364   0.01884  -0.0240   0.0062   1.0000
  11.750   1.3144   0.02447   0.01977  -0.0227   0.0061   1.0000
  12.000   1.3274   0.02534   0.02074  -0.0210   0.0060   1.0000
  12.250   1.3391   0.02614   0.02164  -0.0191   0.0059   1.0000
  12.500   1.3478   0.02718   0.02278  -0.0170   0.0057   1.0000
  12.750   1.3558   0.02829   0.02401  -0.0150   0.0056   1.0000
  13.000   1.3679   0.02907   0.02485  -0.0136   0.0053   1.0000
  13.250   1.3761   0.03024   0.02610  -0.0121   0.0052   1.0000
  13.500   1.3833   0.03154   0.02750  -0.0106   0.0050   1.0000
  13.750   1.3896   0.03298   0.02904  -0.0094   0.0049   1.0000
  14.000   1.3956   0.03450   0.03066  -0.0083   0.0048   1.0000
  14.250   1.4000   0.03626   0.03253  -0.0073   0.0047   1.0000
  14.500   1.4024   0.03831   0.03469  -0.0066   0.0046   1.0000
  14.750   1.4065   0.04026   0.03672  -0.0061   0.0045   1.0000
  15.000   1.4056   0.04288   0.03946  -0.0058   0.0045   1.0000
  15.250   1.4066   0.04540   0.04207  -0.0058   0.0043   1.0000
  15.500   1.4000   0.04897   0.04578  -0.0063   0.0043   1.0000
  15.750   1.3901   0.05320   0.05017  -0.0072   0.0042   1.0000
  16.000   1.3784   0.05796   0.05507  -0.0088   0.0042   1.0000
  16.250   1.3616   0.06382   0.06110  -0.0113   0.0041   1.0000
  16.500   1.3481   0.06962   0.06705  -0.0141   0.0041   1.0000
  16.750   1.3221   0.07821   0.07584  -0.0189   0.0041   1.0000
  17.000   1.2936   0.08830   0.08611  -0.0251   0.0041   1.0000
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