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NACA 63012A AIRFOIL (n63012a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63012A AIRFOIL (n63012a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 64.66 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n63012a-il-1000000.txt
Download as CSV file: xf-n63012a-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63012A AIRFOIL                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.9546   0.11497   0.11307   0.0090   1.0000   0.0096
 -16.000  -0.9749   0.10506   0.10305   0.0032   1.0000   0.0095
 -15.750  -0.9925   0.09625   0.09412  -0.0022   1.0000   0.0095
 -15.500  -1.0092   0.08811   0.08586  -0.0073   1.0000   0.0095
 -15.250  -1.0250   0.08073   0.07836  -0.0120   1.0000   0.0094
 -15.000  -1.0437   0.07336   0.07084  -0.0165   1.0000   0.0094
 -14.750  -1.0630   0.06655   0.06387  -0.0204   1.0000   0.0094
 -14.500  -1.0826   0.06018   0.05732  -0.0237   1.0000   0.0094
 -14.250  -1.1066   0.05369   0.05061  -0.0264   1.0000   0.0094
 -14.000  -1.1303   0.04772   0.04439  -0.0280   1.0000   0.0095
 -13.750  -1.1513   0.04249   0.03891  -0.0285   1.0000   0.0096
 -13.500  -1.1658   0.03830   0.03449  -0.0281   1.0000   0.0097
 -13.250  -1.1714   0.03530   0.03133  -0.0272   1.0000   0.0098
 -13.000  -1.1706   0.03312   0.02902  -0.0262   1.0000   0.0100
 -12.750  -1.1663   0.03140   0.02721  -0.0250   1.0000   0.0101
 -12.500  -1.1597   0.02998   0.02569  -0.0237   1.0000   0.0103
 -12.250  -1.1517   0.02874   0.02436  -0.0221   1.0000   0.0104
 -12.000  -1.1426   0.02759   0.02312  -0.0205   1.0000   0.0106
 -11.750  -1.1322   0.02652   0.02195  -0.0187   1.0000   0.0108
 -11.500  -1.1203   0.02548   0.02081  -0.0170   1.0000   0.0110
 -11.250  -1.1055   0.02444   0.01968  -0.0157   1.0000   0.0113
 -11.000  -1.0892   0.02348   0.01862  -0.0145   1.0000   0.0115
 -10.750  -1.0715   0.02263   0.01767  -0.0134   1.0000   0.0118
 -10.500  -1.0527   0.02186   0.01681  -0.0125   1.0000   0.0121
 -10.250  -1.0334   0.02110   0.01596  -0.0115   1.0000   0.0123
 -10.000  -1.0133   0.02040   0.01517  -0.0107   1.0000   0.0124
  -9.750  -0.9966   0.01911   0.01378  -0.0093   1.0000   0.0126
  -9.500  -0.9829   0.01756   0.01212  -0.0075   1.0000   0.0131
  -9.250  -0.9643   0.01672   0.01123  -0.0063   1.0000   0.0135
  -9.000  -0.9440   0.01610   0.01058  -0.0053   1.0000   0.0138
  -8.750  -0.9233   0.01555   0.00999  -0.0043   1.0000   0.0142
  -8.500  -0.9028   0.01502   0.00943  -0.0033   1.0000   0.0146
  -8.250  -0.8823   0.01456   0.00894  -0.0021   1.0000   0.0151
  -8.000  -0.8621   0.01414   0.00847  -0.0008   1.0000   0.0156
  -7.750  -0.8425   0.01372   0.00801   0.0005   1.0000   0.0160
  -7.500  -0.8232   0.01334   0.00759   0.0020   1.0000   0.0162
  -7.250  -0.8064   0.01258   0.00677   0.0038   0.9996   0.0169
  -7.000  -0.7731   0.01196   0.00612   0.0022   0.9967   0.0180
  -6.750  -0.7381   0.01154   0.00568   0.0003   0.9941   0.0190
  -6.500  -0.7049   0.01117   0.00529  -0.0011   0.9897   0.0202
  -6.250  -0.6708   0.01075   0.00484  -0.0027   0.9852   0.0217
  -6.000  -0.6390   0.01033   0.00443  -0.0039   0.9781   0.0249
  -5.750  -0.6061   0.00996   0.00404  -0.0052   0.9704   0.0290
  -5.500  -0.5770   0.00963   0.00373  -0.0056   0.9579   0.0354
  -5.250  -0.5500   0.00929   0.00342  -0.0055   0.9429   0.0466
  -5.000  -0.5249   0.00898   0.00315  -0.0050   0.9259   0.0628
  -4.750  -0.5006   0.00864   0.00289  -0.0044   0.9086   0.0892
  -4.500  -0.4769   0.00822   0.00261  -0.0038   0.8914   0.1327
  -4.250  -0.4539   0.00770   0.00231  -0.0031   0.8753   0.1969
  -4.000  -0.4310   0.00714   0.00202  -0.0024   0.8603   0.2769
  -3.750  -0.4082   0.00658   0.00177  -0.0017   0.8465   0.3657
  -3.500  -0.3841   0.00618   0.00160  -0.0012   0.8336   0.4395
  -3.250  -0.3584   0.00595   0.00149  -0.0008   0.8215   0.4868
  -3.000  -0.3316   0.00583   0.00141  -0.0006   0.8105   0.5145
  -2.750  -0.3046   0.00574   0.00134  -0.0005   0.8001   0.5367
  -2.500  -0.2775   0.00567   0.00128  -0.0003   0.7897   0.5596
  -2.250  -0.2502   0.00559   0.00123  -0.0002   0.7801   0.5805
  -2.000  -0.2230   0.00554   0.00119  -0.0001   0.7707   0.6008
  -1.750  -0.1953   0.00549   0.00116   0.0000   0.7612   0.6172
  -1.500  -0.1676   0.00546   0.00113   0.0000   0.7521   0.6323
  -1.250  -0.1400   0.00544   0.00110   0.0001   0.7430   0.6457
  -1.000  -0.1121   0.00541   0.00109   0.0001   0.7338   0.6584
  -0.750  -0.0842   0.00541   0.00107   0.0001   0.7251   0.6702
  -0.500  -0.0560   0.00540   0.00106   0.0000   0.7160   0.6804
  -0.250  -0.0281   0.00538   0.00105   0.0000   0.7074   0.6893
   0.000   0.0000   0.00540   0.00105   0.0000   0.6983   0.6983
   0.250   0.0281   0.00538   0.00105   0.0000   0.6893   0.7074
   0.500   0.0561   0.00540   0.00106  -0.0001   0.6804   0.7159
   0.750   0.0843   0.00541   0.00107  -0.0001   0.6702   0.7251
   1.000   0.1121   0.00541   0.00109  -0.0001   0.6584   0.7338
   1.250   0.1400   0.00544   0.00110  -0.0001   0.6457   0.7430
   1.500   0.1677   0.00546   0.00113   0.0000   0.6323   0.7521
   1.750   0.1954   0.00549   0.00116   0.0000   0.6170   0.7612
   2.000   0.2230   0.00554   0.00119   0.0001   0.6007   0.7707
   2.250   0.2503   0.00559   0.00123   0.0002   0.5804   0.7800
   2.500   0.2776   0.00567   0.00128   0.0003   0.5598   0.7897
   2.750   0.3048   0.00574   0.00134   0.0004   0.5367   0.8001
   3.000   0.3318   0.00583   0.00141   0.0006   0.5145   0.8105
   3.250   0.3586   0.00595   0.00149   0.0008   0.4867   0.8215
   3.750   0.4084   0.00658   0.00177   0.0017   0.3651   0.8465
   4.000   0.4314   0.00714   0.00203   0.0023   0.2763   0.8602
   4.250   0.4542   0.00771   0.00232   0.0030   0.1961   0.8752
   4.500   0.4773   0.00823   0.00261   0.0037   0.1322   0.8913
   4.750   0.5011   0.00865   0.00289   0.0043   0.0887   0.9084
   5.000   0.5254   0.00898   0.00315   0.0049   0.0626   0.9258
   5.250   0.5505   0.00930   0.00342   0.0054   0.0465   0.9427
   5.500   0.5773   0.00963   0.00373   0.0055   0.0353   0.9578
   5.750   0.6063   0.00996   0.00405   0.0051   0.0289   0.9703
   6.000   0.6391   0.01033   0.00442   0.0038   0.0248   0.9782
   6.250   0.6710   0.01075   0.00483   0.0027   0.0217   0.9853
   6.500   0.7050   0.01117   0.00529   0.0011   0.0202   0.9898
   6.750   0.7383   0.01154   0.00568  -0.0004   0.0190   0.9942
   7.000   0.7733   0.01196   0.00612  -0.0022   0.0179   0.9968
   7.250   0.8065   0.01258   0.00677  -0.0039   0.0169   0.9997
   7.500   0.8228   0.01333   0.00759  -0.0019   0.0162   1.0000
   7.750   0.8422   0.01371   0.00801  -0.0005   0.0160   1.0000
   8.000   0.8619   0.01414   0.00846   0.0009   0.0156   1.0000
   8.250   0.8822   0.01456   0.00893   0.0021   0.0151   1.0000
   8.500   0.9029   0.01503   0.00943   0.0032   0.0146   1.0000
   8.750   0.9236   0.01555   0.00999   0.0043   0.0142   1.0000
   9.000   0.9444   0.01610   0.01058   0.0052   0.0138   1.0000
   9.250   0.9649   0.01673   0.01124   0.0062   0.0135   1.0000
   9.500   0.9836   0.01758   0.01214   0.0074   0.0131   1.0000
   9.750   0.9973   0.01916   0.01383   0.0092   0.0126   1.0000
  10.000   1.0144   0.02040   0.01518   0.0104   0.0124   1.0000
  10.250   1.0345   0.02112   0.01598   0.0113   0.0123   1.0000
  10.500   1.0541   0.02187   0.01682   0.0122   0.0121   1.0000
  10.750   1.0730   0.02265   0.01770   0.0131   0.0118   1.0000
  11.000   1.0909   0.02350   0.01864   0.0142   0.0115   1.0000
  11.250   1.1073   0.02448   0.01972   0.0153   0.0112   1.0000
  11.500   1.1223   0.02551   0.02085   0.0166   0.0110   1.0000
  11.750   1.1345   0.02655   0.02199   0.0182   0.0108   1.0000
  12.000   1.1450   0.02763   0.02316   0.0200   0.0106   1.0000
  12.250   1.1542   0.02878   0.02440   0.0216   0.0104   1.0000
  12.500   1.1624   0.03003   0.02574   0.0231   0.0103   1.0000
  12.750   1.1689   0.03148   0.02730   0.0245   0.0101   1.0000
  13.000   1.1733   0.03319   0.02910   0.0256   0.0100   1.0000
  13.250   1.1738   0.03543   0.03146   0.0267   0.0098   1.0000
  13.500   1.1678   0.03850   0.03470   0.0275   0.0097   1.0000
  13.750   1.1522   0.04284   0.03928   0.0279   0.0096   1.0000
  14.000   1.1308   0.04815   0.04485   0.0273   0.0095   1.0000
  14.250   1.1060   0.05429   0.05124   0.0255   0.0094   1.0000
  14.500   1.0841   0.06054   0.05770   0.0229   0.0094   1.0000
  14.750   1.0669   0.06659   0.06392   0.0197   0.0094   1.0000
  15.000   1.0447   0.07391   0.07140   0.0155   0.0094   1.0000
  15.250   1.0254   0.08144   0.07909   0.0108   0.0094   1.0000
  15.500   1.0094   0.08894   0.08671   0.0061   0.0094   1.0000
  15.750   0.9941   0.09686   0.09474   0.0011   0.0095   1.0000
  16.000   0.9769   0.10562   0.10362  -0.0043   0.0095   1.0000
  16.250   0.9549   0.11600   0.11411  -0.0103   0.0096   1.0000
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