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NACA 0012-34 (naca001234-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0012-34 (naca001234-il)
Reynolds number: 1,000,000
Max Cl/Cd: 55.74 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001234-il-1000000-n5.txt
Download as CSV file: xf-naca001234-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0012-34                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9006   0.07344   0.07156  -0.0322   1.0000   0.0020
 -14.000  -0.9307   0.06357   0.06150  -0.0386   1.0000   0.0020
 -13.750  -0.9559   0.05608   0.05381  -0.0424   1.0000   0.0020
 -13.500  -0.9761   0.05032   0.04785  -0.0442   1.0000   0.0020
 -13.250  -0.9946   0.04542   0.04273  -0.0446   1.0000   0.0020
 -13.000  -1.0093   0.04142   0.03851  -0.0439   1.0000   0.0020
 -12.750  -1.0199   0.03815   0.03503  -0.0423   1.0000   0.0020
 -12.500  -1.0267   0.03543   0.03210  -0.0403   1.0000   0.0020
 -12.250  -1.0410   0.03209   0.02847  -0.0369   1.0000   0.0020
 -12.000  -1.0475   0.02959   0.02571  -0.0336   1.0000   0.0021
 -11.750  -1.0477   0.02774   0.02368  -0.0305   1.0000   0.0021
 -11.500  -1.0446   0.02629   0.02207  -0.0275   1.0000   0.0022
 -11.250  -1.0401   0.02515   0.02080  -0.0243   1.0000   0.0022
 -11.000  -1.0371   0.02425   0.01979  -0.0204   1.0000   0.0023
 -10.750  -1.0345   0.02352   0.01896  -0.0162   1.0000   0.0023
 -10.500  -1.0294   0.02273   0.01807  -0.0125   1.0000   0.0024
 -10.250  -1.0112   0.02181   0.01704  -0.0116   0.9989   0.0024
 -10.000  -0.9884   0.02080   0.01591  -0.0116   0.9972   0.0025
  -9.750  -0.9645   0.01984   0.01480  -0.0118   0.9957   0.0026
  -9.500  -0.9396   0.01899   0.01386  -0.0121   0.9944   0.0027
  -9.250  -0.9157   0.01818   0.01295  -0.0121   0.9921   0.0029
  -9.000  -0.8905   0.01741   0.01208  -0.0123   0.9901   0.0031
  -8.750  -0.8643   0.01666   0.01123  -0.0127   0.9884   0.0032
  -8.500  -0.8377   0.01594   0.01042  -0.0131   0.9868   0.0034
  -8.250  -0.8142   0.01515   0.00953  -0.0128   0.9839   0.0035
  -8.000  -0.7917   0.01430   0.00860  -0.0124   0.9803   0.0037
  -7.750  -0.7655   0.01375   0.00801  -0.0126   0.9777   0.0040
  -7.500  -0.7398   0.01328   0.00749  -0.0126   0.9746   0.0042
  -7.250  -0.7161   0.01284   0.00698  -0.0121   0.9701   0.0045
  -7.000  -0.6906   0.01240   0.00649  -0.0120   0.9664   0.0049
  -6.750  -0.6662   0.01200   0.00603  -0.0117   0.9622   0.0052
  -6.500  -0.6420   0.01167   0.00566  -0.0112   0.9571   0.0055
  -6.250  -0.6181   0.01121   0.00515  -0.0107   0.9526   0.0063
  -6.000  -0.5938   0.01090   0.00483  -0.0102   0.9475   0.0070
  -5.750  -0.5692   0.01061   0.00449  -0.0098   0.9420   0.0077
  -5.500  -0.5438   0.01035   0.00417  -0.0095   0.9373   0.0083
  -5.250  -0.5196   0.01003   0.00381  -0.0089   0.9313   0.0103
  -5.000  -0.4946   0.00977   0.00355  -0.0086   0.9257   0.0127
  -4.750  -0.4690   0.00955   0.00330  -0.0083   0.9200   0.0171
  -4.500  -0.4437   0.00932   0.00307  -0.0080   0.9136   0.0247
  -4.250  -0.4189   0.00903   0.00282  -0.0076   0.9075   0.0415
  -4.000  -0.3954   0.00862   0.00257  -0.0070   0.9003   0.0815
  -3.750  -0.3729   0.00813   0.00228  -0.0062   0.8933   0.1435
  -3.500  -0.3518   0.00753   0.00201  -0.0053   0.8853   0.2303
  -3.250  -0.3318   0.00686   0.00174  -0.0041   0.8774   0.3389
  -3.000  -0.3099   0.00639   0.00155  -0.0032   0.8691   0.4181
  -2.750  -0.2867   0.00603   0.00140  -0.0025   0.8605   0.4824
  -2.500  -0.2625   0.00579   0.00128  -0.0020   0.8517   0.5285
  -2.250  -0.2387   0.00554   0.00117  -0.0013   0.8418   0.5798
  -2.000  -0.2131   0.00540   0.00109  -0.0010   0.8322   0.6106
  -1.750  -0.1869   0.00530   0.00103  -0.0008   0.8233   0.6334
  -1.500  -0.1604   0.00523   0.00097  -0.0007   0.8139   0.6533
  -1.250  -0.1340   0.00515   0.00093  -0.0005   0.8047   0.6742
  -1.000  -0.1076   0.00509   0.00090  -0.0003   0.7955   0.6960
  -0.750  -0.0810   0.00505   0.00087  -0.0002   0.7856   0.7137
  -0.500  -0.0540   0.00502   0.00086  -0.0001   0.7754   0.7284
  -0.250  -0.0270   0.00501   0.00085  -0.0001   0.7649   0.7415
   0.000   0.0000   0.00500   0.00084   0.0000   0.7537   0.7537
   0.250   0.0270   0.00501   0.00085   0.0001   0.7415   0.7649
   0.500   0.0540   0.00502   0.00086   0.0001   0.7284   0.7755
   0.750   0.0810   0.00505   0.00087   0.0002   0.7137   0.7856
   1.000   0.1076   0.00509   0.00090   0.0003   0.6960   0.7956
   1.250   0.1340   0.00515   0.00093   0.0005   0.6743   0.8048
   1.500   0.1604   0.00523   0.00097   0.0007   0.6530   0.8139
   1.750   0.1870   0.00530   0.00103   0.0008   0.6334   0.8232
   2.000   0.2131   0.00540   0.00109   0.0010   0.6107   0.8322
   2.250   0.2387   0.00553   0.00117   0.0013   0.5804   0.8418
   2.500   0.2625   0.00578   0.00128   0.0020   0.5288   0.8517
   2.750   0.2868   0.00604   0.00140   0.0025   0.4819   0.8605
   3.000   0.3100   0.00639   0.00155   0.0032   0.4191   0.8691
   3.250   0.3317   0.00688   0.00175   0.0042   0.3352   0.8774
   3.500   0.3519   0.00753   0.00201   0.0053   0.2306   0.8853
   3.750   0.3730   0.00813   0.00228   0.0062   0.1436   0.8933
   4.000   0.3955   0.00862   0.00256   0.0070   0.0817   0.9002
   4.250   0.4190   0.00903   0.00282   0.0076   0.0415   0.9074
   4.500   0.4438   0.00932   0.00307   0.0080   0.0247   0.9135
   4.750   0.4691   0.00955   0.00330   0.0083   0.0170   0.9198
   5.000   0.4946   0.00977   0.00355   0.0086   0.0127   0.9255
   5.250   0.5197   0.01003   0.00381   0.0089   0.0103   0.9312
   5.500   0.5440   0.01035   0.00417   0.0095   0.0083   0.9373
   5.750   0.5694   0.01061   0.00449   0.0098   0.0077   0.9419
   6.000   0.5940   0.01090   0.00482   0.0102   0.0070   0.9474
   6.250   0.6182   0.01121   0.00515   0.0107   0.0063   0.9526
   6.500   0.6421   0.01168   0.00567   0.0112   0.0054   0.9570
   6.750   0.6664   0.01200   0.00603   0.0116   0.0052   0.9622
   7.000   0.6909   0.01240   0.00648   0.0120   0.0048   0.9664
   7.250   0.7163   0.01285   0.00699   0.0121   0.0045   0.9700
   7.500   0.7400   0.01328   0.00749   0.0126   0.0042   0.9747
   7.750   0.7657   0.01376   0.00802   0.0125   0.0040   0.9777
   8.000   0.7919   0.01431   0.00860   0.0123   0.0038   0.9804
   8.250   0.8144   0.01515   0.00953   0.0128   0.0035   0.9840
   8.500   0.8381   0.01593   0.01041   0.0130   0.0034   0.9869
   8.750   0.8647   0.01665   0.01123   0.0126   0.0032   0.9885
   9.000   0.8909   0.01741   0.01208   0.0122   0.0031   0.9901
   9.250   0.9161   0.01819   0.01296   0.0120   0.0029   0.9921
   9.500   0.9402   0.01898   0.01384   0.0119   0.0027   0.9944
   9.750   0.9652   0.01984   0.01481   0.0116   0.0026   0.9958
  10.000   0.9889   0.02082   0.01594   0.0115   0.0025   0.9973
  10.250   1.0117   0.02183   0.01706   0.0115   0.0024   0.9989
  10.500   1.0292   0.02273   0.01807   0.0126   0.0024   1.0000
  10.750   1.0347   0.02352   0.01896   0.0162   0.0023   1.0000
  11.000   1.0374   0.02427   0.01981   0.0204   0.0023   1.0000
  11.250   1.0403   0.02519   0.02084   0.0242   0.0022   1.0000
  11.500   1.0450   0.02632   0.02210   0.0274   0.0022   1.0000
  11.750   1.0483   0.02777   0.02370   0.0304   0.0021   1.0000
  12.000   1.0478   0.02965   0.02578   0.0335   0.0021   1.0000
  12.250   1.0418   0.03212   0.02850   0.0368   0.0020   1.0000
  12.500   1.0280   0.03541   0.03209   0.0401   0.0020   1.0000
  12.750   1.0198   0.03829   0.03518   0.0422   0.0020   1.0000
  13.000   1.0099   0.04150   0.03860   0.0437   0.0020   1.0000
  13.250   0.9961   0.04541   0.04272   0.0444   0.0020   1.0000
  13.500   0.9776   0.05032   0.04786   0.0440   0.0020   1.0000
  13.750   0.9557   0.05634   0.05408   0.0420   0.0020   1.0000
  14.000   0.9297   0.06406   0.06200   0.0380   0.0020   1.0000
  14.250   0.8997   0.07403   0.07216   0.0315   0.0020   1.0000
  14.500   0.8029   0.10484   0.10334   0.0156   0.0022   1.0000
  14.750   0.8285   0.10283   0.10129   0.0154   0.0021   1.0000
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