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RAE 2822 AIRFOIL (rae2822-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE 2822 AIRFOIL (rae2822-il)
Reynolds number: 1,000,000
Max Cl/Cd: 69.43 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae2822-il-1000000-n5.txt
Download as CSV file: xf-rae2822-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.6753   0.20875   0.20691   0.0137   1.0000   0.0039
 -18.500  -0.8211   0.15006   0.14813  -0.0093   1.0000   0.0051
 -18.250  -0.9366   0.11929   0.11708  -0.0244   1.0000   0.0049
 -18.000  -0.9916   0.10356   0.10114  -0.0323   1.0000   0.0048
 -17.750  -1.0368   0.09036   0.08774  -0.0393   1.0000   0.0047
 -17.500  -1.0690   0.08041   0.07760  -0.0448   1.0000   0.0047
 -17.250  -1.0883   0.07341   0.07045  -0.0485   1.0000   0.0047
 -17.000  -1.1021   0.06763   0.06455  -0.0514   1.0000   0.0047
 -16.750  -1.1126   0.06268   0.05948  -0.0537   1.0000   0.0048
 -16.500  -1.1237   0.05788   0.05455  -0.0558   1.0000   0.0048
 -16.250  -1.1287   0.05414   0.05071  -0.0572   1.0000   0.0048
 -16.000  -1.1367   0.05024   0.04668  -0.0585   1.0000   0.0048
 -15.750  -1.1378   0.04735   0.04370  -0.0593   1.0000   0.0049
 -15.500  -1.1383   0.04464   0.04089  -0.0599   1.0000   0.0050
 -15.250  -1.1395   0.04191   0.03806  -0.0604   1.0000   0.0050
 -15.000  -1.1388   0.03948   0.03553  -0.0606   1.0000   0.0051
 -14.750  -1.1376   0.03716   0.03311  -0.0607   1.0000   0.0052
 -14.500  -1.1333   0.03522   0.03109  -0.0606   1.0000   0.0052
 -14.250  -1.1313   0.03310   0.02886  -0.0604   1.0000   0.0053
 -14.000  -1.1261   0.03139   0.02705  -0.0600   1.0000   0.0054
 -13.750  -1.1192   0.02986   0.02545  -0.0594   1.0000   0.0056
 -13.500  -1.1146   0.02822   0.02372  -0.0587   1.0000   0.0056
 -13.250  -1.1071   0.02691   0.02233  -0.0578   1.0000   0.0058
 -13.000  -1.1017   0.02555   0.02089  -0.0567   1.0000   0.0058
 -12.750  -1.0958   0.02438   0.01964  -0.0552   1.0000   0.0059
 -12.500  -1.0916   0.02329   0.01847  -0.0533   1.0000   0.0060
 -12.250  -1.0900   0.02237   0.01749  -0.0507   1.0000   0.0060
 -12.000  -1.0989   0.02159   0.01665  -0.0459   1.0000   0.0061
 -11.750  -1.0810   0.02049   0.01546  -0.0461   0.9988   0.0063
 -11.500  -1.0554   0.01948   0.01438  -0.0474   0.9967   0.0066
 -11.250  -1.0287   0.01871   0.01356  -0.0486   0.9947   0.0069
 -11.000  -1.0031   0.01805   0.01286  -0.0494   0.9925   0.0072
 -10.750  -0.9774   0.01738   0.01214  -0.0501   0.9899   0.0075
 -10.500  -0.9503   0.01674   0.01144  -0.0511   0.9876   0.0078
 -10.250  -0.9218   0.01615   0.01078  -0.0522   0.9856   0.0082
 -10.000  -0.8926   0.01555   0.01013  -0.0535   0.9841   0.0084
  -9.750  -0.8652   0.01502   0.00954  -0.0542   0.9818   0.0087
  -9.500  -0.8405   0.01437   0.00885  -0.0545   0.9780   0.0093
  -9.250  -0.8122   0.01387   0.00833  -0.0554   0.9754   0.0099
  -9.000  -0.7822   0.01340   0.00782  -0.0565   0.9733   0.0105
  -8.500  -0.7188   0.01256   0.00691  -0.0594   0.9701   0.0117
  -8.250  -0.6941   0.01213   0.00646  -0.0594   0.9648   0.0128
  -8.000  -0.6646   0.01174   0.00606  -0.0603   0.9612   0.0139
  -7.750  -0.6338   0.01139   0.00567  -0.0614   0.9581   0.0150
  -7.500  -0.6041   0.01107   0.00532  -0.0622   0.9544   0.0160
  -7.250  -0.5772   0.01072   0.00496  -0.0625   0.9488   0.0179
  -7.000  -0.5480   0.01041   0.00463  -0.0632   0.9441   0.0199
  -6.750  -0.5199   0.01014   0.00434  -0.0636   0.9390   0.0221
  -6.500  -0.4929   0.00985   0.00405  -0.0638   0.9326   0.0253
  -6.250  -0.4645   0.00962   0.00379  -0.0642   0.9273   0.0281
  -6.000  -0.4382   0.00935   0.00353  -0.0642   0.9207   0.0335
  -5.750  -0.4109   0.00911   0.00329  -0.0643   0.9142   0.0401
  -5.500  -0.3840   0.00890   0.00308  -0.0644   0.9080   0.0469
  -5.000  -0.3304   0.00840   0.00264  -0.0645   0.8950   0.0737
  -4.750  -0.3038   0.00814   0.00244  -0.0645   0.8879   0.0935
  -4.500  -0.2772   0.00785   0.00223  -0.0646   0.8816   0.1220
  -4.250  -0.2509   0.00751   0.00201  -0.0646   0.8748   0.1599
  -3.750  -0.2005   0.00633   0.00142  -0.0647   0.8612   0.3289
  -3.500  -0.1748   0.00582   0.00122  -0.0647   0.8545   0.4216
  -3.250  -0.1472   0.00566   0.00115  -0.0649   0.8483   0.4590
  -3.000  -0.1193   0.00559   0.00110  -0.0650   0.8417   0.4782
  -2.750  -0.0911   0.00555   0.00106  -0.0651   0.8357   0.4931
  -2.500  -0.0629   0.00551   0.00103  -0.0652   0.8292   0.5060
  -2.250  -0.0348   0.00549   0.00101  -0.0653   0.8231   0.5219
  -2.000  -0.0063   0.00548   0.00100  -0.0655   0.8165   0.5318
  -1.500   0.0503   0.00547   0.00095  -0.0657   0.8039   0.5379
  -1.250   0.0786   0.00547   0.00093  -0.0658   0.7972   0.5410
  -1.000   0.1070   0.00548   0.00092  -0.0660   0.7909   0.5437
  -0.750   0.1353   0.00550   0.00091  -0.0661   0.7836   0.5462
  -0.500   0.1633   0.00550   0.00091  -0.0661   0.7754   0.5489
   0.000   0.2189   0.00555   0.00092  -0.0661   0.7535   0.5553
   0.250   0.2465   0.00560   0.00093  -0.0660   0.7401   0.5583
   0.750   0.3008   0.00572   0.00097  -0.0657   0.7072   0.5638
   1.000   0.3271   0.00582   0.00100  -0.0654   0.6807   0.5670
   1.250   0.3509   0.00605   0.00105  -0.0646   0.6290   0.5704
   1.500   0.3733   0.00643   0.00114  -0.0635   0.5530   0.5738
   1.750   0.3944   0.00697   0.00131  -0.0623   0.4576   0.5768
   2.000   0.4161   0.00751   0.00152  -0.0613   0.3667   0.5800
   2.250   0.4387   0.00801   0.00172  -0.0605   0.2860   0.5834
   2.500   0.4615   0.00850   0.00193  -0.0598   0.2119   0.5869
   2.750   0.4856   0.00890   0.00212  -0.0592   0.1584   0.5902
   3.000   0.5097   0.00928   0.00233  -0.0587   0.1108   0.5941
   3.250   0.5348   0.00957   0.00252  -0.0582   0.0811   0.5982
   3.500   0.5603   0.00984   0.00271  -0.0579   0.0611   0.6023
   3.750   0.5862   0.01006   0.00289  -0.0576   0.0491   0.6059
   4.000   0.6120   0.01027   0.00309  -0.0573   0.0404   0.6098
   4.250   0.6380   0.01047   0.00329  -0.0570   0.0349   0.6142
   4.500   0.6639   0.01069   0.00349  -0.0567   0.0303   0.6187
   4.750   0.6898   0.01089   0.00371  -0.0565   0.0272   0.6232
   5.000   0.7152   0.01113   0.00396  -0.0561   0.0237   0.6282
   5.250   0.7411   0.01133   0.00419  -0.0558   0.0219   0.6330
   5.500   0.7664   0.01158   0.00444  -0.0554   0.0198   0.6375
   5.750   0.7914   0.01185   0.00474  -0.0549   0.0179   0.6426
   6.000   0.8167   0.01208   0.00501  -0.0546   0.0169   0.6480
   6.250   0.8417   0.01234   0.00530  -0.0541   0.0157   0.6534
   6.500   0.8662   0.01263   0.00562  -0.0536   0.0143   0.6595
   7.000   0.9150   0.01324   0.00631  -0.0525   0.0126   0.6711
   7.250   0.9391   0.01355   0.00666  -0.0520   0.0120   0.6773
   7.500   0.9630   0.01387   0.00704  -0.0514   0.0113   0.6833
   7.750   0.9863   0.01424   0.00744  -0.0507   0.0107   0.6906
   8.000   1.0087   0.01471   0.00796  -0.0499   0.0099   0.6974
   8.250   1.0318   0.01507   0.00839  -0.0492   0.0097   0.7049
   8.500   1.0548   0.01544   0.00883  -0.0484   0.0093   0.7118
   8.750   1.0774   0.01582   0.00929  -0.0477   0.0089   0.7195
   9.000   1.0998   0.01621   0.00973  -0.0469   0.0085   0.7273
   9.250   1.1217   0.01663   0.01022  -0.0460   0.0081   0.7363
   9.500   1.1427   0.01711   0.01077  -0.0450   0.0078   0.7453
  10.000   1.1815   0.01834   0.01217  -0.0425   0.0071   0.7646
  10.250   1.2015   0.01883   0.01276  -0.0414   0.0070   0.7751
  10.500   1.2206   0.01937   0.01341  -0.0401   0.0069   0.7870
  10.750   1.2383   0.01991   0.01406  -0.0386   0.0067   0.8011
  11.000   1.2539   0.02050   0.01476  -0.0367   0.0065   0.8168
  11.250   1.2686   0.02110   0.01550  -0.0347   0.0064   0.8350
  11.500   1.2821   0.02172   0.01626  -0.0325   0.0062   0.8589
  11.750   1.2938   0.02219   0.01692  -0.0300   0.0061   0.9020
  12.000   1.3072   0.02286   0.01779  -0.0280   0.0060   1.0000
  12.250   1.3213   0.02359   0.01858  -0.0262   0.0058   1.0000
  12.500   1.3336   0.02444   0.01951  -0.0243   0.0057   1.0000
  12.750   1.3456   0.02532   0.02045  -0.0225   0.0055   1.0000
  13.000   1.3562   0.02629   0.02151  -0.0206   0.0054   1.0000
  13.250   1.3649   0.02743   0.02274  -0.0185   0.0053   1.0000
  13.500   1.3719   0.02870   0.02411  -0.0165   0.0052   1.0000
  13.750   1.3751   0.03031   0.02584  -0.0142   0.0051   1.0000
  14.000   1.3772   0.03203   0.02769  -0.0121   0.0050   1.0000
  14.250   1.3780   0.03392   0.02972  -0.0101   0.0049   1.0000
  14.500   1.3822   0.03558   0.03149  -0.0086   0.0049   1.0000
  14.750   1.3853   0.03739   0.03343  -0.0072   0.0048   1.0000
  15.000   1.3851   0.03960   0.03576  -0.0060   0.0048   1.0000
  15.250   1.3836   0.04202   0.03832  -0.0049   0.0048   1.0000
  15.500   1.3828   0.04451   0.04093  -0.0043   0.0047   1.0000
  15.750   1.3759   0.04779   0.04436  -0.0039   0.0047   1.0000
  16.000   1.3678   0.05144   0.04815  -0.0040   0.0047   1.0000
  16.250   1.3627   0.05497   0.05180  -0.0046   0.0046   1.0000
  16.500   1.3467   0.06024   0.05725  -0.0061   0.0046   1.0000
  16.750   1.3327   0.06574   0.06291  -0.0083   0.0045   1.0000
  17.000   1.3124   0.07290   0.07023  -0.0120   0.0046   1.0000
  17.250   1.2860   0.08216   0.07969  -0.0175   0.0045   1.0000
  17.500   1.2442   0.09615   0.09392  -0.0266   0.0046   1.0000
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