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NACA 63012A AIRFOIL (n63012a-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63012A AIRFOIL (n63012a-il)
Reynolds number: 500,000
Max Cl/Cd: 54.25 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63012a-il-500000-n5.txt
Download as CSV file: xf-n63012a-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -1.0050   0.09854   0.09567  -0.0009   1.0000   0.0092
 -15.750  -1.0336   0.08807   0.08503  -0.0071   1.0000   0.0092
 -15.500  -1.0574   0.07935   0.07613  -0.0123   1.0000   0.0091
 -15.250  -1.0766   0.07205   0.06865  -0.0166   1.0000   0.0092
 -15.000  -1.0931   0.06575   0.06216  -0.0199   1.0000   0.0092
 -14.750  -1.1057   0.06040   0.05663  -0.0225   1.0000   0.0092
 -14.500  -1.1170   0.05554   0.05159  -0.0246   1.0000   0.0093
 -14.250  -1.1307   0.05066   0.04652  -0.0262   1.0000   0.0094
 -14.000  -1.1389   0.04674   0.04244  -0.0271   1.0000   0.0095
 -13.750  -1.1423   0.04357   0.03914  -0.0276   1.0000   0.0096
 -13.500  -1.1423   0.04097   0.03640  -0.0277   1.0000   0.0098
 -13.250  -1.1397   0.03875   0.03407  -0.0275   1.0000   0.0099
 -13.000  -1.1357   0.03677   0.03198  -0.0271   1.0000   0.0101
 -12.750  -1.1305   0.03498   0.03008  -0.0265   1.0000   0.0102
 -12.500  -1.1246   0.03332   0.02831  -0.0255   1.0000   0.0104
 -12.250  -1.1179   0.03176   0.02662  -0.0244   1.0000   0.0106
 -12.000  -1.1102   0.03030   0.02502  -0.0230   1.0000   0.0108
 -11.750  -1.1014   0.02894   0.02354  -0.0215   1.0000   0.0110
 -11.500  -1.0914   0.02769   0.02216  -0.0199   1.0000   0.0112
 -11.250  -1.0801   0.02654   0.02088  -0.0182   1.0000   0.0114
 -11.000  -1.0674   0.02546   0.01966  -0.0166   1.0000   0.0116
 -10.750  -1.0522   0.02444   0.01851  -0.0153   1.0000   0.0119
 -10.500  -1.0353   0.02355   0.01751  -0.0142   1.0000   0.0121
 -10.250  -1.0172   0.02276   0.01661  -0.0131   1.0000   0.0123
 -10.000  -1.0013   0.02165   0.01541  -0.0118   1.0000   0.0126
  -9.750  -0.9848   0.02062   0.01432  -0.0106   1.0000   0.0130
  -9.500  -0.9665   0.01980   0.01343  -0.0095   1.0000   0.0133
  -9.250  -0.9472   0.01909   0.01266  -0.0084   1.0000   0.0136
  -9.000  -0.9275   0.01841   0.01193  -0.0074   1.0000   0.0139
  -8.750  -0.9075   0.01777   0.01124  -0.0064   1.0000   0.0142
  -8.500  -0.8874   0.01716   0.01058  -0.0054   1.0000   0.0146
  -8.250  -0.8672   0.01660   0.00996  -0.0043   1.0000   0.0151
  -8.000  -0.8469   0.01608   0.00938  -0.0032   1.0000   0.0156
  -7.750  -0.8268   0.01560   0.00885  -0.0020   1.0000   0.0161
  -7.500  -0.8073   0.01513   0.00833  -0.0007   1.0000   0.0164
  -7.250  -0.7856   0.01448   0.00765   0.0001   0.9981   0.0173
  -7.000  -0.7539   0.01394   0.00708  -0.0012   0.9921   0.0182
  -6.750  -0.7218   0.01348   0.00659  -0.0025   0.9852   0.0194
  -6.500  -0.6904   0.01307   0.00613  -0.0036   0.9764   0.0208
  -6.250  -0.6594   0.01263   0.00566  -0.0046   0.9664   0.0228
  -6.000  -0.6285   0.01223   0.00526  -0.0056   0.9549   0.0259
  -5.750  -0.5985   0.01189   0.00489  -0.0062   0.9417   0.0299
  -5.500  -0.5705   0.01156   0.00456  -0.0065   0.9264   0.0358
  -5.250  -0.5443   0.01125   0.00423  -0.0062   0.9100   0.0445
  -5.000  -0.5189   0.01096   0.00394  -0.0058   0.8934   0.0555
  -4.750  -0.4939   0.01067   0.00366  -0.0054   0.8777   0.0707
  -4.500  -0.4693   0.01033   0.00338  -0.0049   0.8626   0.0955
  -4.250  -0.4457   0.00986   0.00306  -0.0043   0.8485   0.1415
  -4.000  -0.4232   0.00923   0.00272  -0.0037   0.8354   0.2176
  -3.750  -0.4006   0.00862   0.00241  -0.0030   0.8230   0.3005
  -3.500  -0.3773   0.00813   0.00218  -0.0024   0.8115   0.3769
  -3.250  -0.3525   0.00781   0.00201  -0.0020   0.8004   0.4328
  -3.000  -0.3271   0.00757   0.00190  -0.0016   0.7903   0.4789
  -2.500  -0.2749   0.00727   0.00173  -0.0009   0.7708   0.5462
  -2.250  -0.2482   0.00718   0.00167  -0.0007   0.7619   0.5709
  -2.000  -0.2212   0.00711   0.00163  -0.0005   0.7526   0.5919
  -1.750  -0.1940   0.00706   0.00158  -0.0003   0.7439   0.6092
  -1.500  -0.1667   0.00702   0.00154  -0.0002   0.7351   0.6244
  -1.250  -0.1390   0.00699   0.00151  -0.0001   0.7261   0.6364
  -1.000  -0.1113   0.00698   0.00147  -0.0001   0.7176   0.6458
  -0.750  -0.0834   0.00696   0.00145  -0.0001   0.7084   0.6551
  -0.500  -0.0557   0.00695   0.00143   0.0000   0.6997   0.6637
  -0.250  -0.0278   0.00695   0.00141   0.0000   0.6906   0.6730
   0.000   0.0000   0.00694   0.00141   0.0000   0.6817   0.6816
   0.250   0.0278   0.00695   0.00141   0.0000   0.6730   0.6906
   0.500   0.0557   0.00695   0.00143   0.0000   0.6637   0.6997
   0.750   0.0835   0.00696   0.00145   0.0001   0.6551   0.7084
   1.000   0.1113   0.00698   0.00147   0.0001   0.6458   0.7176
   1.250   0.1390   0.00699   0.00151   0.0001   0.6364   0.7262
   1.500   0.1667   0.00702   0.00154   0.0002   0.6244   0.7351
   1.750   0.1940   0.00706   0.00158   0.0003   0.6092   0.7439
   2.000   0.2212   0.00711   0.00163   0.0005   0.5918   0.7526
   2.250   0.2481   0.00718   0.00167   0.0007   0.5709   0.7619
   2.500   0.2749   0.00727   0.00173   0.0009   0.5462   0.7708
   3.000   0.3270   0.00758   0.00190   0.0016   0.4786   0.7904
   3.250   0.3524   0.00781   0.00201   0.0020   0.4331   0.8005
   3.500   0.3773   0.00813   0.00218   0.0024   0.3772   0.8115
   3.750   0.4006   0.00862   0.00241   0.0030   0.3008   0.8231
   4.000   0.4232   0.00923   0.00272   0.0037   0.2183   0.8354
   4.250   0.4456   0.00986   0.00306   0.0043   0.1418   0.8485
   4.500   0.4693   0.01033   0.00338   0.0049   0.0955   0.8627
   4.750   0.4938   0.01067   0.00366   0.0054   0.0707   0.8777
   5.000   0.5188   0.01096   0.00394   0.0059   0.0555   0.8935
   5.250   0.5442   0.01125   0.00423   0.0063   0.0445   0.9101
   5.500   0.5704   0.01156   0.00455   0.0065   0.0358   0.9264
   5.750   0.5984   0.01189   0.00489   0.0063   0.0299   0.9417
   6.000   0.6285   0.01223   0.00526   0.0056   0.0259   0.9549
   6.250   0.6593   0.01263   0.00567   0.0046   0.0228   0.9664
   6.500   0.6904   0.01307   0.00613   0.0036   0.0208   0.9764
   6.750   0.7218   0.01348   0.00659   0.0025   0.0194   0.9851
   7.000   0.7538   0.01394   0.00708   0.0012   0.0182   0.9921
   7.250   0.7855   0.01448   0.00765  -0.0001   0.0172   0.9981
   7.500   0.8073   0.01513   0.00833   0.0007   0.0164   1.0000
   7.750   0.8268   0.01560   0.00885   0.0020   0.0161   1.0000
   8.000   0.8469   0.01608   0.00938   0.0032   0.0156   1.0000
   8.250   0.8672   0.01660   0.00996   0.0043   0.0151   1.0000
   8.500   0.8874   0.01716   0.01057   0.0054   0.0146   1.0000
   8.750   0.9075   0.01777   0.01124   0.0064   0.0142   1.0000
   9.000   0.9275   0.01841   0.01193   0.0074   0.0139   1.0000
   9.250   0.9472   0.01908   0.01266   0.0084   0.0136   1.0000
   9.500   0.9665   0.01980   0.01343   0.0095   0.0133   1.0000
   9.750   0.9849   0.02062   0.01432   0.0105   0.0130   1.0000
  10.000   1.0013   0.02165   0.01541   0.0118   0.0126   1.0000
  10.250   1.0172   0.02276   0.01662   0.0131   0.0123   1.0000
  10.500   1.0354   0.02355   0.01751   0.0142   0.0121   1.0000
  10.750   1.0523   0.02444   0.01851   0.0153   0.0119   1.0000
  11.000   1.0675   0.02546   0.01966   0.0166   0.0116   1.0000
  11.250   1.0802   0.02654   0.02087   0.0182   0.0114   1.0000
  11.500   1.0915   0.02769   0.02216   0.0199   0.0112   1.0000
  11.750   1.1016   0.02894   0.02354   0.0215   0.0110   1.0000
  12.000   1.1104   0.03029   0.02502   0.0230   0.0108   1.0000
  12.250   1.1182   0.03175   0.02661   0.0243   0.0106   1.0000
  12.500   1.1249   0.03331   0.02829   0.0255   0.0104   1.0000
  12.750   1.1309   0.03497   0.03007   0.0264   0.0102   1.0000
  13.000   1.1362   0.03674   0.03195   0.0271   0.0101   1.0000
  13.250   1.1404   0.03870   0.03402   0.0275   0.0099   1.0000
  13.500   1.1428   0.04095   0.03638   0.0276   0.0098   1.0000
  13.750   1.1430   0.04354   0.03911   0.0275   0.0096   1.0000
  14.000   1.1395   0.04671   0.04242   0.0270   0.0095   1.0000
  14.250   1.1313   0.05063   0.04650   0.0261   0.0094   1.0000
  14.500   1.1177   0.05552   0.05157   0.0245   0.0093   1.0000
  14.750   1.1065   0.06038   0.05661   0.0224   0.0092   1.0000
  15.000   1.0940   0.06574   0.06216   0.0198   0.0092   1.0000
  15.250   1.0776   0.07202   0.06862   0.0164   0.0092   1.0000
  15.500   1.0580   0.07942   0.07620   0.0121   0.0091   1.0000
  15.750   1.0347   0.08807   0.08503   0.0069   0.0092   1.0000
  16.000   1.0060   0.09858   0.09572   0.0006   0.0092   1.0000
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