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NACA 63-210 AIRFOIL (n63210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63-210 AIRFOIL (n63210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 69.02 at α=2°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n63210-il-1000000.txt
Download as CSV file: xf-n63210-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-210 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.8792   0.07479   0.07311  -0.0246   1.0000   0.0059
 -13.500  -0.9188   0.05971   0.05783  -0.0358   1.0000   0.0058
 -13.250  -0.9614   0.04873   0.04662  -0.0441   1.0000   0.0058
 -13.000  -0.9818   0.04295   0.04065  -0.0475   1.0000   0.0058
 -12.750  -0.9952   0.03889   0.03641  -0.0490   1.0000   0.0058
 -12.500  -1.0224   0.03423   0.03149  -0.0487   1.0000   0.0058
 -12.250  -1.0391   0.03137   0.02839  -0.0461   1.0000   0.0058
 -12.000  -1.0394   0.02905   0.02584  -0.0445   1.0000   0.0058
 -11.750  -1.0467   0.02518   0.02152  -0.0424   1.0000   0.0060
 -11.500  -1.0385   0.02288   0.01894  -0.0411   1.0000   0.0063
 -11.250  -1.0221   0.02156   0.01747  -0.0404   1.0000   0.0065
 -11.000  -1.0027   0.02058   0.01639  -0.0397   1.0000   0.0067
 -10.750  -0.9817   0.01981   0.01554  -0.0393   1.0000   0.0069
 -10.500  -0.9595   0.01920   0.01486  -0.0388   1.0000   0.0072
 -10.250  -0.9374   0.01852   0.01409  -0.0384   1.0000   0.0075
 -10.000  -0.9155   0.01775   0.01323  -0.0379   1.0000   0.0078
  -9.750  -0.8935   0.01701   0.01236  -0.0373   1.0000   0.0082
  -9.500  -0.8714   0.01627   0.01156  -0.0368   1.0000   0.0087
  -9.250  -0.8451   0.01643   0.01176  -0.0366   1.0000   0.0092
  -9.000  -0.8195   0.01654   0.01190  -0.0363   1.0000   0.0098
  -8.750  -0.7948   0.01655   0.01190  -0.0359   1.0000   0.0108
  -8.500  -0.7699   0.01674   0.01205  -0.0354   1.0000   0.0115
  -8.250  -0.7497   0.01610   0.01137  -0.0345   1.0000   0.0125
  -8.000  -0.7273   0.01616   0.01146  -0.0337   1.0000   0.0131
  -7.750  -0.7004   0.01612   0.01141  -0.0339   0.9991   0.0141
  -7.500  -0.6649   0.01606   0.01131  -0.0358   0.9964   0.0153
  -7.250  -0.6280   0.01637   0.01156  -0.0379   0.9939   0.0160
  -7.000  -0.5989   0.01417   0.00922  -0.0392   0.9897   0.0175
  -6.750  -0.5648   0.01368   0.00873  -0.0409   0.9856   0.0185
  -6.500  -0.5315   0.01318   0.00819  -0.0424   0.9806   0.0194
  -6.250  -0.5003   0.01278   0.00775  -0.0434   0.9729   0.0204
  -6.000  -0.4715   0.01248   0.00739  -0.0437   0.9628   0.0212
  -5.750  -0.4443   0.01259   0.00745  -0.0435   0.9504   0.0221
  -5.500  -0.4227   0.01133   0.00609  -0.0425   0.9333   0.0228
  -5.250  -0.3993   0.01074   0.00541  -0.0416   0.9118   0.0229
  -5.000  -0.3754   0.01028   0.00483  -0.0408   0.8900   0.0229
  -4.750  -0.3502   0.00988   0.00432  -0.0403   0.8750   0.0229
  -4.500  -0.3241   0.00953   0.00387  -0.0401   0.8635   0.0230
  -4.250  -0.2975   0.00918   0.00343  -0.0399   0.8541   0.0232
  -4.000  -0.2704   0.00888   0.00305  -0.0398   0.8452   0.0234
  -3.750  -0.2428   0.00863   0.00273  -0.0398   0.8370   0.0235
  -3.500  -0.2152   0.00840   0.00243  -0.0398   0.8287   0.0238
  -3.250  -0.1872   0.00818   0.00217  -0.0398   0.8202   0.0243
  -3.000  -0.1593   0.00801   0.00194  -0.0399   0.8120   0.0254
  -2.750  -0.1311   0.00784   0.00175  -0.0399   0.8030   0.0270
  -2.500  -0.1030   0.00771   0.00159  -0.0400   0.7945   0.0291
  -2.250  -0.0749   0.00751   0.00143  -0.0401   0.7857   0.0496
  -2.000  -0.0476   0.00682   0.00119  -0.0405   0.7768   0.1857
  -1.750  -0.0207   0.00595   0.00096  -0.0410   0.7683   0.3812
  -1.500   0.0070   0.00552   0.00088  -0.0413   0.7593   0.4909
  -1.250   0.0352   0.00534   0.00090  -0.0414   0.7507   0.5613
  -1.000   0.0636   0.00534   0.00091  -0.0415   0.7419   0.5956
  -0.750   0.0920   0.00526   0.00088  -0.0416   0.7333   0.6147
  -0.500   0.1203   0.00521   0.00086  -0.0417   0.7250   0.6321
  -0.250   0.1488   0.00517   0.00086  -0.0418   0.7159   0.6469
   0.000   0.1772   0.00516   0.00087  -0.0419   0.7062   0.6605
   0.250   0.2054   0.00517   0.00089  -0.0419   0.6914   0.6798
   0.500   0.2336   0.00519   0.00090  -0.0419   0.6758   0.6971
   0.750   0.2620   0.00522   0.00092  -0.0420   0.6626   0.7080
   1.000   0.2903   0.00525   0.00095  -0.0421   0.6474   0.7188
   1.250   0.3184   0.00530   0.00098  -0.0421   0.6286   0.7299
   1.500   0.3461   0.00541   0.00101  -0.0421   0.5977   0.7413
   1.750   0.3734   0.00557   0.00106  -0.0420   0.5575   0.7529
   2.000   0.4003   0.00580   0.00114  -0.0419   0.5060   0.7645
   2.250   0.4261   0.00622   0.00127  -0.0417   0.4245   0.7760
   2.500   0.4485   0.00729   0.00163  -0.0413   0.2462   0.7877
   2.750   0.4715   0.00831   0.00205  -0.0409   0.0928   0.7996
   3.000   0.4969   0.00884   0.00235  -0.0406   0.0300   0.8113
   3.250   0.5241   0.00902   0.00254  -0.0405   0.0247   0.8225
   3.500   0.5513   0.00917   0.00275  -0.0404   0.0237   0.8336
   3.750   0.5783   0.00935   0.00298  -0.0402   0.0230   0.8450
   4.000   0.6051   0.00956   0.00324  -0.0400   0.0223   0.8566
   4.250   0.6313   0.00978   0.00354  -0.0397   0.0216   0.8685
   4.500   0.6569   0.01004   0.00387  -0.0393   0.0209   0.8814
   4.750   0.6820   0.01034   0.00424  -0.0387   0.0204   0.8949
   5.000   0.7063   0.01067   0.00466  -0.0380   0.0200   0.9096
   5.250   0.7295   0.01103   0.00509  -0.0370   0.0198   0.9261
   5.500   0.7514   0.01141   0.00556  -0.0358   0.0197   0.9441
   5.750   0.7730   0.01179   0.00603  -0.0345   0.0197   0.9689
   6.000   0.8013   0.01234   0.00664  -0.0350   0.0194   1.0000
   6.250   0.8265   0.01294   0.00728  -0.0347   0.0193   1.0000
   6.500   0.8512   0.01361   0.00800  -0.0344   0.0193   1.0000
   6.750   0.8755   0.01433   0.00876  -0.0340   0.0193   1.0000
   7.000   0.8995   0.01511   0.00960  -0.0335   0.0191   1.0000
   7.250   0.9219   0.01624   0.01076  -0.0330   0.0184   1.0000
   7.500   0.9425   0.01848   0.01311  -0.0321   0.0178   1.0000
   7.750   0.9686   0.01837   0.01306  -0.0321   0.0171   1.0000
   8.000   0.9938   0.01872   0.01347  -0.0318   0.0166   1.0000
   8.250   1.0180   0.01934   0.01416  -0.0315   0.0160   1.0000
   8.500   1.0417   0.02002   0.01491  -0.0311   0.0154   1.0000
   8.750   1.0651   0.02062   0.01556  -0.0308   0.0147   1.0000
   9.000   1.0881   0.02116   0.01614  -0.0304   0.0141   1.0000
   9.250   1.1102   0.02182   0.01681  -0.0300   0.0136   1.0000
   9.500   1.1244   0.02495   0.02015  -0.0289   0.0125   1.0000
   9.750   1.1485   0.02457   0.01983  -0.0285   0.0122   1.0000
  10.000   1.1712   0.02472   0.02005  -0.0280   0.0116   1.0000
  10.250   1.1927   0.02509   0.02048  -0.0274   0.0109   1.0000
  10.500   1.2147   0.02515   0.02057  -0.0269   0.0103   1.0000
  10.750   1.2366   0.02518   0.02060  -0.0265   0.0099   1.0000
  11.000   1.2582   0.02520   0.02059  -0.0260   0.0095   1.0000
  11.250   1.2717   0.02641   0.02187  -0.0247   0.0089   1.0000
  11.500   1.2936   0.02641   0.02193  -0.0241   0.0086   1.0000
  11.750   1.3130   0.02673   0.02233  -0.0232   0.0081   1.0000
  12.000   1.3306   0.02695   0.02259  -0.0220   0.0075   1.0000
  12.250   1.3449   0.02738   0.02305  -0.0204   0.0072   1.0000
  12.500   1.3644   0.02734   0.02299  -0.0195   0.0069   1.0000
  12.750   1.3814   0.02760   0.02324  -0.0184   0.0067   1.0000
  13.000   1.3929   0.02837   0.02403  -0.0169   0.0062   1.0000
  13.250   1.3963   0.02993   0.02574  -0.0149   0.0061   1.0000
  13.500   1.4011   0.03145   0.02739  -0.0133   0.0059   1.0000
  13.750   1.4017   0.03346   0.02954  -0.0118   0.0058   1.0000
  14.000   1.4055   0.03526   0.03146  -0.0108   0.0056   1.0000
  14.250   1.4081   0.03727   0.03359  -0.0100   0.0055   1.0000
  14.500   1.4093   0.03955   0.03598  -0.0094   0.0053   1.0000
  14.750   1.4065   0.04239   0.03897  -0.0092   0.0053   1.0000
  15.000   1.4052   0.04522   0.04192  -0.0093   0.0052   1.0000
  15.250   1.4013   0.04854   0.04536  -0.0098   0.0051   1.0000
  15.500   1.3996   0.05175   0.04868  -0.0105   0.0050   1.0000
  15.750   1.3867   0.05669   0.05379  -0.0122   0.0050   1.0000
  16.000   1.3770   0.06151   0.05874  -0.0142   0.0049   1.0000
  16.250   1.3536   0.06888   0.06632  -0.0178   0.0049   1.0000
  16.500   1.3290   0.07724   0.07489  -0.0224   0.0049   1.0000
  16.750   1.3043   0.08640   0.08422  -0.0280   0.0049   1.0000
  17.000   1.2233   0.10969   0.10792  -0.0428   0.0052   1.0000
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