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NACA 63-212 AIRFOIL (n63212-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-212 AIRFOIL (n63212-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.89 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63212-il-1000000-n5.txt
Download as CSV file: xf-n63212-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-212 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.9225   0.08473   0.08249  -0.0238   1.0000   0.0078
 -15.250  -0.9530   0.07394   0.07152  -0.0309   1.0000   0.0078
 -15.000  -0.9767   0.06556   0.06297  -0.0365   1.0000   0.0078
 -14.750  -0.9974   0.05848   0.05573  -0.0410   1.0000   0.0078
 -14.500  -1.0109   0.05306   0.05016  -0.0442   1.0000   0.0078
 -14.250  -1.0251   0.04796   0.04490  -0.0468   1.0000   0.0078
 -14.000  -1.0319   0.04415   0.04095  -0.0485   1.0000   0.0079
 -13.750  -1.0372   0.04078   0.03744  -0.0497   1.0000   0.0079
 -13.500  -1.0386   0.03805   0.03459  -0.0503   1.0000   0.0080
 -13.250  -1.0415   0.03533   0.03172  -0.0505   1.0000   0.0081
 -13.000  -1.0404   0.03320   0.02947  -0.0503   1.0000   0.0082
 -12.750  -1.0410   0.03102   0.02716  -0.0497   1.0000   0.0081
 -12.500  -1.0377   0.02938   0.02540  -0.0487   1.0000   0.0082
 -12.250  -1.0336   0.02796   0.02387  -0.0474   1.0000   0.0083
 -12.000  -1.0296   0.02674   0.02254  -0.0454   1.0000   0.0084
 -11.750  -1.0216   0.02569   0.02138  -0.0437   1.0000   0.0084
 -11.500  -1.0090   0.02458   0.02017  -0.0425   1.0000   0.0085
 -11.250  -0.9927   0.02379   0.01928  -0.0416   1.0000   0.0085
 -11.000  -0.9757   0.02295   0.01835  -0.0407   1.0000   0.0086
 -10.750  -0.9594   0.02189   0.01718  -0.0398   1.0000   0.0087
 -10.500  -0.9467   0.02020   0.01534  -0.0385   1.0000   0.0089
 -10.250  -0.9288   0.01920   0.01425  -0.0377   1.0000   0.0091
 -10.000  -0.8972   0.01816   0.01313  -0.0396   0.9730   0.0092
  -9.750  -0.8654   0.01729   0.01217  -0.0414   0.9517   0.0093
  -9.500  -0.8417   0.01661   0.01137  -0.0412   0.9294   0.0094
  -9.250  -0.8204   0.01603   0.01068  -0.0405   0.9108   0.0095
  -9.000  -0.7985   0.01548   0.01002  -0.0398   0.8956   0.0096
  -8.750  -0.7760   0.01494   0.00938  -0.0392   0.8827   0.0097
  -8.500  -0.7528   0.01444   0.00880  -0.0386   0.8706   0.0098
  -8.250  -0.7291   0.01395   0.00822  -0.0382   0.8593   0.0099
  -8.000  -0.7049   0.01348   0.00767  -0.0378   0.8489   0.0100
  -7.750  -0.6802   0.01305   0.00716  -0.0375   0.8392   0.0101
  -7.500  -0.6551   0.01263   0.00666  -0.0373   0.8296   0.0103
  -7.250  -0.6296   0.01225   0.00621  -0.0371   0.8206   0.0104
  -7.000  -0.6038   0.01190   0.00580  -0.0369   0.8116   0.0107
  -6.750  -0.5777   0.01155   0.00538  -0.0368   0.8032   0.0108
  -6.250  -0.5247   0.01093   0.00464  -0.0366   0.7867   0.0110
  -6.000  -0.4979   0.01066   0.00430  -0.0366   0.7786   0.0112
  -5.750  -0.4707   0.01040   0.00399  -0.0366   0.7706   0.0113
  -5.500  -0.4436   0.01014   0.00368  -0.0365   0.7630   0.0115
  -5.250  -0.4162   0.00990   0.00340  -0.0366   0.7552   0.0119
  -5.000  -0.3887   0.00970   0.00314  -0.0366   0.7477   0.0123
  -4.750  -0.3609   0.00950   0.00292  -0.0367   0.7403   0.0127
  -4.250  -0.3051   0.00917   0.00253  -0.0369   0.7256   0.0138
  -4.000  -0.2771   0.00903   0.00236  -0.0370   0.7181   0.0148
  -3.750  -0.2491   0.00884   0.00220  -0.0371   0.7112   0.0205
  -3.500  -0.2210   0.00868   0.00204  -0.0372   0.7037   0.0288
  -3.250  -0.1928   0.00852   0.00190  -0.0374   0.6968   0.0368
  -3.000  -0.1648   0.00833   0.00176  -0.0375   0.6894   0.0542
  -2.750  -0.1368   0.00810   0.00161  -0.0377   0.6826   0.0819
  -2.500  -0.1088   0.00783   0.00147  -0.0379   0.6750   0.1219
  -2.250  -0.0811   0.00744   0.00130  -0.0382   0.6685   0.1917
  -2.000  -0.0538   0.00687   0.00110  -0.0385   0.6612   0.3007
  -1.750  -0.0262   0.00644   0.00097  -0.0389   0.6541   0.3937
  -1.500   0.0019   0.00615   0.00091  -0.0391   0.6469   0.4637
  -1.250   0.0302   0.00600   0.00089  -0.0393   0.6398   0.5100
  -1.000   0.0591   0.00594   0.00088  -0.0395   0.6327   0.5355
  -0.750   0.0878   0.00592   0.00087  -0.0397   0.6256   0.5525
  -0.500   0.1165   0.00587   0.00087  -0.0399   0.6187   0.5714
  -0.250   0.1453   0.00586   0.00087  -0.0401   0.6112   0.5841
   0.000   0.1742   0.00586   0.00087  -0.0403   0.6042   0.5930
   0.250   0.2030   0.00588   0.00088  -0.0405   0.5962   0.6010
   0.500   0.2318   0.00589   0.00090  -0.0406   0.5886   0.6093
   0.750   0.2605   0.00592   0.00092  -0.0408   0.5798   0.6171
   1.000   0.2893   0.00594   0.00095  -0.0410   0.5711   0.6255
   1.250   0.3180   0.00599   0.00099  -0.0411   0.5618   0.6331
   1.500   0.3467   0.00602   0.00103  -0.0413   0.5515   0.6416
   1.750   0.3751   0.00608   0.00108  -0.0414   0.5375   0.6493
   2.000   0.4034   0.00618   0.00114  -0.0415   0.5198   0.6574
   2.250   0.4316   0.00627   0.00120  -0.0416   0.5022   0.6651
   2.500   0.4594   0.00643   0.00128  -0.0417   0.4738   0.6733
   2.750   0.4866   0.00665   0.00139  -0.0417   0.4348   0.6806
   3.000   0.5130   0.00700   0.00154  -0.0416   0.3818   0.6887
   3.250   0.5387   0.00745   0.00175  -0.0414   0.3186   0.6962
   3.500   0.5646   0.00786   0.00198  -0.0413   0.2664   0.7041
   3.750   0.5902   0.00832   0.00224  -0.0412   0.2126   0.7114
   4.000   0.6152   0.00886   0.00254  -0.0409   0.1531   0.7196
   4.250   0.6403   0.00936   0.00284  -0.0407   0.1039   0.7269
   4.500   0.6662   0.00975   0.00311  -0.0406   0.0741   0.7351
   4.750   0.6923   0.01008   0.00337  -0.0404   0.0538   0.7427
   5.000   0.7186   0.01037   0.00362  -0.0403   0.0409   0.7511
   5.250   0.7452   0.01062   0.00386  -0.0402   0.0343   0.7589
   5.500   0.7718   0.01085   0.00411  -0.0401   0.0300   0.7678
   5.750   0.7981   0.01111   0.00437  -0.0399   0.0263   0.7764
   6.250   0.8506   0.01159   0.00492  -0.0396   0.0214   0.7944
   6.500   0.8764   0.01188   0.00523  -0.0394   0.0191   0.8033
   6.750   0.9022   0.01213   0.00553  -0.0392   0.0177   0.8128
   7.000   0.9275   0.01243   0.00585  -0.0389   0.0162   0.8218
   7.250   0.9524   0.01278   0.00623  -0.0385   0.0149   0.8312
   7.500   0.9774   0.01307   0.00659  -0.0382   0.0143   0.8411
   7.750   1.0020   0.01338   0.00696  -0.0377   0.0137   0.8516
   8.250   1.0495   0.01408   0.00775  -0.0367   0.0124   0.8756
   8.500   1.0720   0.01447   0.00820  -0.0359   0.0120   0.8890
   8.750   1.0928   0.01496   0.00878  -0.0349   0.0114   0.9051
   9.000   1.1134   0.01532   0.00923  -0.0337   0.0113   0.9250
   9.250   1.1330   0.01567   0.00968  -0.0324   0.0111   0.9600
   9.500   1.1577   0.01615   0.01022  -0.0323   0.0109   1.0000
   9.750   1.1797   0.01666   0.01078  -0.0317   0.0107   1.0000
  10.000   1.2008   0.01722   0.01139  -0.0309   0.0105   1.0000
  10.250   1.2213   0.01779   0.01200  -0.0301   0.0103   1.0000
  10.500   1.2410   0.01838   0.01264  -0.0292   0.0101   1.0000
  10.750   1.2600   0.01898   0.01328  -0.0282   0.0099   1.0000
  11.000   1.2785   0.01957   0.01391  -0.0272   0.0097   1.0000
  11.250   1.2946   0.02020   0.01460  -0.0258   0.0095   1.0000
  11.500   1.3074   0.02088   0.01533  -0.0238   0.0093   1.0000
  11.750   1.3182   0.02167   0.01617  -0.0218   0.0092   1.0000
  12.000   1.3283   0.02255   0.01711  -0.0198   0.0090   1.0000
  12.250   1.3364   0.02362   0.01825  -0.0178   0.0089   1.0000
  12.500   1.3434   0.02482   0.01954  -0.0160   0.0087   1.0000
  12.750   1.3465   0.02641   0.02122  -0.0141   0.0085   1.0000
  13.000   1.3563   0.02757   0.02245  -0.0129   0.0085   1.0000
  13.250   1.3642   0.02894   0.02392  -0.0117   0.0085   1.0000
  13.500   1.3725   0.03033   0.02539  -0.0107   0.0084   1.0000
  13.750   1.3803   0.03182   0.02697  -0.0098   0.0083   1.0000
  14.000   1.3868   0.03349   0.02873  -0.0091   0.0082   1.0000
  14.250   1.3947   0.03509   0.03041  -0.0085   0.0080   1.0000
  14.500   1.3974   0.03724   0.03267  -0.0079   0.0080   1.0000
  14.750   1.4040   0.03908   0.03460  -0.0076   0.0079   1.0000
  15.000   1.4064   0.04144   0.03705  -0.0074   0.0078   1.0000
  15.250   1.4082   0.04394   0.03965  -0.0074   0.0077   1.0000
  15.500   1.4098   0.04655   0.04236  -0.0076   0.0076   1.0000
  15.750   1.4088   0.04957   0.04549  -0.0080   0.0075   1.0000
  16.000   1.4074   0.05274   0.04878  -0.0087   0.0075   1.0000
  16.250   1.4055   0.05614   0.05229  -0.0095   0.0074   1.0000
  16.500   1.3999   0.06020   0.05647  -0.0108   0.0074   1.0000
  16.750   1.3978   0.06394   0.06031  -0.0122   0.0073   1.0000
  17.000   1.3910   0.06854   0.06504  -0.0141   0.0072   1.0000
  17.250   1.3812   0.07384   0.07047  -0.0164   0.0072   1.0000
  17.500   1.3718   0.07929   0.07604  -0.0191   0.0072   1.0000
  17.750   1.3616   0.08511   0.08199  -0.0221   0.0071   1.0000
  18.000   1.3488   0.09166   0.08867  -0.0256   0.0071   1.0000
  18.250   1.3339   0.09885   0.09600  -0.0296   0.0070   1.0000
  18.500   1.3162   0.10691   0.10420  -0.0343   0.0070   1.0000
  18.750   1.2937   0.11630   0.11375  -0.0399   0.0070   1.0000
  19.000   1.2709   0.12603   0.12363  -0.0458   0.0070   1.0000
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