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RAE 2822 AIRFOIL (rae2822-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RAE 2822 AIRFOIL (rae2822-il)
Reynolds number: 1,000,000
Max Cl/Cd: 79.03 at α=2.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rae2822-il-1000000.txt
Download as CSV file: xf-rae2822-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 2822 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.8978   0.08724   0.08500  -0.0420   1.0000   0.0075
 -15.750  -0.9227   0.07820   0.07580  -0.0473   1.0000   0.0075
 -15.500  -0.9398   0.07135   0.06882  -0.0513   1.0000   0.0076
 -15.250  -0.9585   0.06479   0.06210  -0.0547   1.0000   0.0076
 -15.000  -0.9756   0.05901   0.05616  -0.0574   1.0000   0.0076
 -14.750  -0.9941   0.05358   0.05054  -0.0595   1.0000   0.0075
 -14.500  -0.9968   0.05044   0.04731  -0.0606   1.0000   0.0076
 -14.250  -1.0103   0.04610   0.04280  -0.0616   1.0000   0.0076
 -14.000  -1.0130   0.04322   0.03979  -0.0621   1.0000   0.0077
 -13.750  -1.0167   0.04033   0.03677  -0.0624   1.0000   0.0079
 -13.500  -1.0214   0.03742   0.03371  -0.0622   1.0000   0.0078
 -13.250  -1.0220   0.03506   0.03122  -0.0619   1.0000   0.0081
 -13.000  -1.0205   0.03302   0.02906  -0.0613   1.0000   0.0081
 -12.750  -1.0193   0.03104   0.02696  -0.0604   1.0000   0.0082
 -12.500  -1.0161   0.02940   0.02519  -0.0592   1.0000   0.0083
 -12.250  -1.0120   0.02799   0.02368  -0.0579   1.0000   0.0084
 -12.000  -1.0088   0.02668   0.02228  -0.0561   1.0000   0.0085
 -11.750  -1.0042   0.02580   0.02132  -0.0540   1.0000   0.0086
 -11.500  -1.0158   0.02430   0.01970  -0.0496   1.0000   0.0087
 -11.250  -1.0318   0.02297   0.01827  -0.0438   1.0000   0.0088
 -11.000  -1.0358   0.02170   0.01689  -0.0396   1.0000   0.0091
 -10.750  -1.0254   0.02067   0.01581  -0.0379   0.9996   0.0094
 -10.500  -0.9961   0.01985   0.01494  -0.0396   0.9981   0.0098
 -10.250  -0.9658   0.01923   0.01428  -0.0413   0.9965   0.0103
 -10.000  -0.9354   0.01848   0.01345  -0.0430   0.9951   0.0108
  -9.750  -0.9054   0.01775   0.01265  -0.0445   0.9936   0.0113
  -9.500  -0.8773   0.01709   0.01193  -0.0454   0.9913   0.0116
  -9.250  -0.8503   0.01597   0.01070  -0.0465   0.9887   0.0122
  -9.000  -0.8212   0.01497   0.00964  -0.0480   0.9867   0.0130
  -8.750  -0.7892   0.01442   0.00906  -0.0497   0.9853   0.0138
  -8.500  -0.7564   0.01393   0.00854  -0.0514   0.9842   0.0148
  -8.250  -0.7229   0.01349   0.00805  -0.0533   0.9833   0.0155
  -8.000  -0.6985   0.01277   0.00728  -0.0533   0.9791   0.0168
  -7.750  -0.6681   0.01224   0.00672  -0.0545   0.9767   0.0184
  -7.500  -0.6357   0.01185   0.00632  -0.0559   0.9750   0.0200
  -7.250  -0.6024   0.01147   0.00590  -0.0576   0.9737   0.0213
  -7.000  -0.5690   0.01087   0.00529  -0.0594   0.9725   0.0248
  -6.750  -0.5347   0.01057   0.00497  -0.0611   0.9714   0.0274
  -6.500  -0.5040   0.01008   0.00450  -0.0622   0.9689   0.0330
  -6.250  -0.4766   0.00977   0.00418  -0.0624   0.9644   0.0380
  -6.000  -0.4459   0.00941   0.00385  -0.0634   0.9611   0.0468
  -5.750  -0.4149   0.00900   0.00351  -0.0645   0.9582   0.0636
  -5.500  -0.3852   0.00864   0.00323  -0.0653   0.9544   0.0846
  -5.250  -0.3596   0.00821   0.00294  -0.0652   0.9485   0.1175
  -5.000  -0.3317   0.00765   0.00260  -0.0658   0.9438   0.1742
  -4.750  -0.3068   0.00691   0.00221  -0.0659   0.9379   0.2664
  -4.500  -0.2837   0.00590   0.00179  -0.0659   0.9313   0.4204
  -4.250  -0.2547   0.00570   0.00167  -0.0663   0.9266   0.4636
  -4.000  -0.2275   0.00561   0.00161  -0.0662   0.9201   0.4861
  -3.750  -0.1986   0.00555   0.00154  -0.0665   0.9146   0.5009
  -3.500  -0.1702   0.00551   0.00149  -0.0666   0.9088   0.5121
  -3.250  -0.1421   0.00547   0.00144  -0.0667   0.9025   0.5224
  -2.750  -0.0852   0.00544   0.00137  -0.0669   0.8902   0.5394
  -2.500  -0.0564   0.00545   0.00133  -0.0671   0.8843   0.5474
  -2.250  -0.0283   0.00547   0.00135  -0.0672   0.8778   0.5581
  -2.000   0.0000   0.00546   0.00133  -0.0672   0.8714   0.5652
  -1.750   0.0284   0.00545   0.00130  -0.0674   0.8653   0.5684
  -1.500   0.0567   0.00544   0.00128  -0.0675   0.8584   0.5714
  -1.250   0.0853   0.00546   0.00125  -0.0676   0.8523   0.5744
  -1.000   0.1134   0.00543   0.00122  -0.0677   0.8453   0.5775
  -0.750   0.1418   0.00543   0.00121  -0.0678   0.8387   0.5806
  -0.500   0.1697   0.00542   0.00120  -0.0678   0.8306   0.5837
  -0.250   0.1979   0.00544   0.00119  -0.0679   0.8224   0.5869
   0.000   0.2258   0.00546   0.00119  -0.0679   0.8128   0.5900
   0.250   0.2535   0.00545   0.00119  -0.0678   0.8027   0.5936
   0.500   0.2810   0.00546   0.00119  -0.0677   0.7917   0.5970
   1.000   0.3356   0.00555   0.00121  -0.0674   0.7637   0.6039
   1.250   0.3618   0.00560   0.00122  -0.0669   0.7398   0.6075
   1.500   0.3882   0.00566   0.00125  -0.0666   0.7199   0.6114
   1.750   0.4150   0.00574   0.00130  -0.0664   0.6997   0.6154
   2.000   0.4412   0.00586   0.00135  -0.0660   0.6763   0.6192
   2.250   0.4667   0.00598   0.00141  -0.0655   0.6437   0.6232
   2.500   0.4908   0.00621   0.00150  -0.0647   0.5948   0.6273
   2.750   0.5102   0.00680   0.00169  -0.0632   0.4904   0.6315
   3.000   0.5276   0.00766   0.00199  -0.0614   0.3569   0.6357
   3.250   0.5469   0.00840   0.00230  -0.0601   0.2466   0.6403
   3.500   0.5676   0.00907   0.00261  -0.0590   0.1558   0.6452
   3.750   0.5903   0.00959   0.00288  -0.0582   0.0986   0.6498
   4.000   0.6141   0.00997   0.00314  -0.0576   0.0663   0.6546
   4.250   0.6391   0.01027   0.00339  -0.0571   0.0500   0.6599
   4.500   0.6641   0.01059   0.00366  -0.0566   0.0403   0.6652
   4.750   0.6898   0.01079   0.00390  -0.0563   0.0359   0.6709
   5.000   0.7144   0.01113   0.00425  -0.0557   0.0307   0.6769
   5.250   0.7402   0.01133   0.00449  -0.0554   0.0282   0.6828
   5.500   0.7643   0.01169   0.00486  -0.0548   0.0249   0.6890
   5.750   0.7888   0.01204   0.00525  -0.0542   0.0230   0.6953
   6.000   0.8137   0.01229   0.00557  -0.0537   0.0215   0.7018
   6.250   0.8383   0.01259   0.00588  -0.0532   0.0198   0.7091
   6.500   0.8595   0.01322   0.00659  -0.0521   0.0179   0.7162
   6.750   0.8844   0.01348   0.00690  -0.0516   0.0172   0.7240
   7.000   0.9082   0.01381   0.00730  -0.0509   0.0163   0.7317
   7.500   0.9547   0.01459   0.00818  -0.0495   0.0146   0.7483
   7.750   0.9712   0.01571   0.00941  -0.0476   0.0135   0.7573
   8.000   0.9951   0.01599   0.00977  -0.0470   0.0131   0.7673
   8.250   1.0179   0.01637   0.01023  -0.0462   0.0126   0.7776
   8.500   1.0400   0.01681   0.01075  -0.0454   0.0121   0.7884
   8.750   1.0617   0.01726   0.01129  -0.0445   0.0115   0.8004
   9.000   1.0829   0.01774   0.01184  -0.0435   0.0111   0.8137
   9.250   1.1024   0.01833   0.01252  -0.0422   0.0107   0.8290
   9.500   1.1156   0.01973   0.01410  -0.0400   0.0101   0.8471
   9.750   1.1313   0.02076   0.01532  -0.0381   0.0099   0.8701
  10.000   1.1467   0.02129   0.01606  -0.0360   0.0097   0.9076
  10.250   1.1650   0.02191   0.01687  -0.0346   0.0095   1.0000
  10.500   1.1817   0.02280   0.01787  -0.0331   0.0092   1.0000
  10.750   1.1964   0.02372   0.01889  -0.0312   0.0090   1.0000
  11.000   1.2090   0.02482   0.02010  -0.0291   0.0088   1.0000
  11.250   1.2206   0.02589   0.02129  -0.0269   0.0086   1.0000
  11.500   1.2306   0.02705   0.02257  -0.0246   0.0085   1.0000
  11.750   1.2427   0.02774   0.02332  -0.0227   0.0082   1.0000
  12.000   1.2495   0.02912   0.02483  -0.0202   0.0081   1.0000
  12.250   1.2593   0.02995   0.02571  -0.0182   0.0079   1.0000
  12.500   1.2648   0.03132   0.02720  -0.0159   0.0078   1.0000
  12.750   1.2684   0.03281   0.02878  -0.0137   0.0076   1.0000
  13.000   1.2644   0.03513   0.03128  -0.0111   0.0075   1.0000
  13.250   1.2473   0.03885   0.03527  -0.0080   0.0073   1.0000
  13.500   1.2193   0.04389   0.04063  -0.0054   0.0072   1.0000
  13.750   1.2049   0.04768   0.04464  -0.0043   0.0071   1.0000
  14.000   1.1956   0.05117   0.04828  -0.0039   0.0071   1.0000
  14.250   1.1885   0.05465   0.05191  -0.0042   0.0071   1.0000
  14.500   1.1750   0.05929   0.05671  -0.0053   0.0071   1.0000
  14.750   1.1558   0.06529   0.06289  -0.0076   0.0070   1.0000
  15.000   1.1184   0.07537   0.07320  -0.0130   0.0071   1.0000
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