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NACA 65(1)-212 (naca651212-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 65(1)-212 (naca651212-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.8 at α=2.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca651212-il-1000000-n5.txt
Download as CSV file: xf-naca651212-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 65(1)-212                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -1.0431   0.06366   0.06131  -0.0497   1.0000   0.0064
 -16.000  -1.0659   0.05661   0.05409  -0.0539   1.0000   0.0064
 -15.750  -1.0848   0.05087   0.04818  -0.0567   1.0000   0.0064
 -15.500  -1.0991   0.04624   0.04338  -0.0584   1.0000   0.0064
 -15.250  -1.1058   0.04282   0.03981  -0.0592   1.0000   0.0065
 -15.000  -1.1154   0.03930   0.03612  -0.0596   1.0000   0.0065
 -14.750  -1.1178   0.03670   0.03339  -0.0595   1.0000   0.0066
 -14.500  -1.1160   0.03465   0.03120  -0.0592   1.0000   0.0066
 -14.250  -1.1186   0.03229   0.02869  -0.0584   1.0000   0.0066
 -14.000  -1.1175   0.03039   0.02668  -0.0574   1.0000   0.0069
 -13.750  -1.1127   0.02889   0.02508  -0.0563   1.0000   0.0070
 -13.500  -1.1031   0.02786   0.02400  -0.0553   1.0000   0.0071
 -13.250  -1.0985   0.02644   0.02246  -0.0537   1.0000   0.0072
 -13.000  -1.0873   0.02565   0.02162  -0.0524   1.0000   0.0073
 -12.750  -1.0758   0.02494   0.02085  -0.0509   1.0000   0.0075
 -12.500  -1.0668   0.02411   0.01995  -0.0490   1.0000   0.0076
 -12.250  -1.0563   0.02345   0.01923  -0.0470   1.0000   0.0078
 -12.000  -1.0440   0.02262   0.01829  -0.0453   1.0000   0.0080
 -11.750  -1.0291   0.02186   0.01746  -0.0439   1.0000   0.0082
 -11.500  -1.0129   0.02121   0.01672  -0.0426   1.0000   0.0084
 -11.250  -0.9834   0.02040   0.01582  -0.0442   0.9819   0.0087
 -11.000  -0.9510   0.01964   0.01495  -0.0462   0.9698   0.0090
 -10.750  -0.9213   0.01891   0.01410  -0.0476   0.9568   0.0091
 -10.500  -0.8988   0.01807   0.01312  -0.0475   0.9413   0.0094
 -10.250  -0.8796   0.01732   0.01226  -0.0466   0.9272   0.0097
 -10.000  -0.8593   0.01680   0.01165  -0.0458   0.9153   0.0099
  -9.750  -0.8380   0.01637   0.01114  -0.0450   0.9042   0.0101
  -9.500  -0.8157   0.01598   0.01068  -0.0444   0.8940   0.0104
  -9.250  -0.7935   0.01554   0.01016  -0.0437   0.8849   0.0107
  -9.000  -0.7709   0.01515   0.00969  -0.0431   0.8757   0.0110
  -8.750  -0.7482   0.01468   0.00913  -0.0426   0.8670   0.0113
  -8.500  -0.7246   0.01435   0.00872  -0.0421   0.8589   0.0117
  -8.250  -0.7009   0.01394   0.00824  -0.0417   0.8510   0.0120
  -8.000  -0.6774   0.01354   0.00774  -0.0412   0.8435   0.0122
  -7.750  -0.6531   0.01316   0.00730  -0.0408   0.8356   0.0123
  -7.500  -0.6304   0.01261   0.00665  -0.0402   0.8282   0.0127
  -7.250  -0.6064   0.01216   0.00616  -0.0398   0.8210   0.0132
  -6.750  -0.5559   0.01155   0.00547  -0.0394   0.8080   0.0141
  -6.500  -0.5306   0.01126   0.00511  -0.0392   0.8011   0.0145
  -6.250  -0.5049   0.01097   0.00478  -0.0390   0.7947   0.0149
  -6.000  -0.4790   0.01070   0.00445  -0.0389   0.7880   0.0153
  -5.750  -0.4529   0.01044   0.00414  -0.0387   0.7822   0.0159
  -5.500  -0.4264   0.01021   0.00386  -0.0387   0.7761   0.0162
  -5.250  -0.4002   0.00995   0.00355  -0.0386   0.7702   0.0169
  -5.000  -0.3736   0.00969   0.00327  -0.0385   0.7644   0.0182
  -4.750  -0.3468   0.00949   0.00305  -0.0385   0.7582   0.0192
  -4.500  -0.3198   0.00932   0.00284  -0.0385   0.7526   0.0203
  -4.250  -0.2924   0.00916   0.00265  -0.0386   0.7470   0.0214
  -4.000  -0.2652   0.00899   0.00245  -0.0386   0.7417   0.0230
  -3.750  -0.2378   0.00881   0.00227  -0.0387   0.7368   0.0256
  -3.500  -0.2102   0.00867   0.00212  -0.0388   0.7313   0.0279
  -3.250  -0.1826   0.00856   0.00197  -0.0389   0.7259   0.0311
  -3.000  -0.1550   0.00840   0.00183  -0.0390   0.7211   0.0374
  -2.750  -0.1276   0.00819   0.00170  -0.0391   0.7162   0.0572
  -2.500  -0.1007   0.00790   0.00154  -0.0392   0.7113   0.1037
  -2.250  -0.0748   0.00739   0.00135  -0.0393   0.7068   0.2001
  -2.000  -0.0494   0.00671   0.00113  -0.0395   0.7018   0.3348
  -1.750  -0.0250   0.00589   0.00093  -0.0395   0.6971   0.5150
  -1.500   0.0024   0.00567   0.00091  -0.0396   0.6929   0.5813
  -1.250   0.0305   0.00557   0.00091  -0.0397   0.6882   0.6158
  -0.750   0.0873   0.00553   0.00091  -0.0401   0.6792   0.6504
  -0.500   0.1161   0.00552   0.00091  -0.0404   0.6749   0.6569
  -0.250   0.1449   0.00552   0.00091  -0.0406   0.6703   0.6616
   0.000   0.1736   0.00555   0.00091  -0.0409   0.6660   0.6661
   0.250   0.2024   0.00555   0.00092  -0.0411   0.6619   0.6704
   0.500   0.2312   0.00555   0.00094  -0.0414   0.6575   0.6751
   0.750   0.2599   0.00558   0.00095  -0.0416   0.6530   0.6798
   1.000   0.2885   0.00560   0.00098  -0.0419   0.6489   0.6842
   1.250   0.3171   0.00561   0.00102  -0.0421   0.6420   0.6888
   1.500   0.3452   0.00567   0.00104  -0.0422   0.6276   0.6938
   1.750   0.3733   0.00573   0.00108  -0.0423   0.6137   0.6983
   2.000   0.4006   0.00583   0.00112  -0.0423   0.5912   0.7030
   2.250   0.4269   0.00603   0.00118  -0.0421   0.5476   0.7082
   2.500   0.4517   0.00640   0.00131  -0.0418   0.4799   0.7131
   2.750   0.4715   0.00729   0.00165  -0.0407   0.3430   0.7182
   3.250   0.5145   0.00879   0.00232  -0.0393   0.1363   0.7285
   3.500   0.5377   0.00933   0.00262  -0.0388   0.0721   0.7341
   3.750   0.5626   0.00969   0.00286  -0.0385   0.0411   0.7400
   4.000   0.5888   0.00992   0.00306  -0.0383   0.0321   0.7453
   4.250   0.6150   0.01012   0.00326  -0.0382   0.0280   0.7511
   4.500   0.6413   0.01033   0.00348  -0.0380   0.0246   0.7569
   4.750   0.6675   0.01051   0.00369  -0.0379   0.0227   0.7628
   5.000   0.6933   0.01074   0.00393  -0.0377   0.0205   0.7695
   5.250   0.7187   0.01099   0.00421  -0.0374   0.0184   0.7757
   5.500   0.7444   0.01121   0.00447  -0.0372   0.0175   0.7824
   6.000   0.7946   0.01172   0.00502  -0.0366   0.0152   0.7953
   6.250   0.8186   0.01208   0.00541  -0.0361   0.0140   0.8025
   6.500   0.8430   0.01235   0.00574  -0.0357   0.0137   0.8097
   6.750   0.8671   0.01267   0.00610  -0.0352   0.0133   0.8174
   7.000   0.8907   0.01298   0.00648  -0.0347   0.0129   0.8247
   7.250   0.9140   0.01333   0.00689  -0.0341   0.0125   0.8324
   7.500   0.9367   0.01369   0.00730  -0.0334   0.0122   0.8403
   8.000   0.9808   0.01444   0.00817  -0.0318   0.0116   0.8582
   8.250   1.0019   0.01486   0.00865  -0.0309   0.0114   0.8675
   8.500   1.0221   0.01532   0.00917  -0.0298   0.0110   0.8776
   8.750   1.0407   0.01583   0.00976  -0.0285   0.0108   0.8890
   9.000   1.0559   0.01654   0.01058  -0.0266   0.0104   0.9023
   9.250   1.0736   0.01699   0.01111  -0.0250   0.0102   0.9164
   9.500   1.0895   0.01745   0.01166  -0.0232   0.0101   0.9332
   9.750   1.1044   0.01790   0.01224  -0.0212   0.0100   0.9606
  10.000   1.1251   0.01849   0.01290  -0.0206   0.0098   1.0000
  10.250   1.1401   0.01916   0.01363  -0.0189   0.0097   1.0000
  10.500   1.1553   0.01980   0.01434  -0.0174   0.0095   1.0000
  10.750   1.1699   0.02052   0.01512  -0.0158   0.0093   1.0000
  11.000   1.1840   0.02129   0.01596  -0.0143   0.0092   1.0000
  11.250   1.1982   0.02205   0.01678  -0.0128   0.0090   1.0000
  11.500   1.2136   0.02269   0.01748  -0.0116   0.0087   1.0000
  11.750   1.2262   0.02360   0.01846  -0.0101   0.0086   1.0000
  12.000   1.2402   0.02438   0.01929  -0.0089   0.0084   1.0000
  12.250   1.2532   0.02526   0.02023  -0.0077   0.0083   1.0000
  12.500   1.2641   0.02634   0.02139  -0.0063   0.0082   1.0000
  12.750   1.2750   0.02743   0.02255  -0.0050   0.0081   1.0000
  13.000   1.2841   0.02869   0.02388  -0.0037   0.0079   1.0000
  13.250   1.2926   0.03002   0.02529  -0.0025   0.0078   1.0000
  13.500   1.2961   0.03188   0.02727  -0.0010   0.0076   1.0000
  13.750   1.3012   0.03363   0.02914   0.0002   0.0075   1.0000
  14.000   1.3058   0.03547   0.03111   0.0012   0.0074   1.0000
  14.250   1.3110   0.03727   0.03303   0.0021   0.0074   1.0000
  14.500   1.3219   0.03851   0.03435   0.0026   0.0072   1.0000
  14.750   1.3250   0.04061   0.03657   0.0032   0.0072   1.0000
  15.000   1.3236   0.04328   0.03938   0.0038   0.0072   1.0000
  15.250   1.3303   0.04510   0.04129   0.0040   0.0070   1.0000
  15.500   1.3306   0.04771   0.04402   0.0042   0.0069   1.0000
  15.750   1.3269   0.05088   0.04734   0.0041   0.0068   1.0000
  16.000   1.3244   0.05407   0.05065   0.0037   0.0067   1.0000
  16.250   1.3192   0.05776   0.05448   0.0030   0.0067   1.0000
  16.500   1.3102   0.06216   0.05903   0.0018   0.0066   1.0000
  16.750   1.3056   0.06620   0.06318   0.0004   0.0065   1.0000
  17.000   1.2962   0.07116   0.06829  -0.0016   0.0065   1.0000
  17.250   1.2833   0.07701   0.07429  -0.0043   0.0064   1.0000
  17.500   1.2675   0.08381   0.08124  -0.0078   0.0064   1.0000
  17.750   1.2435   0.09270   0.09032  -0.0129   0.0064   1.0000
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