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E226 (10.19%) (e226-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E226 (10.19%) (e226-il)
Reynolds number: 1,000,000
Max Cl/Cd: 73.41 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e226-il-1000000-n5.txt
Download as CSV file: xf-e226-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E226  (10.19%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.8343   0.08845   0.08649  -0.0142   1.0000   0.0048
 -13.750  -0.8810   0.07398   0.07183  -0.0230   1.0000   0.0047
 -13.500  -0.9242   0.06070   0.05833  -0.0322   1.0000   0.0046
 -13.250  -0.9376   0.05382   0.05132  -0.0374   1.0000   0.0046
 -13.000  -0.9564   0.04674   0.04406  -0.0429   1.0000   0.0046
 -12.750  -0.9763   0.04082   0.03793  -0.0467   1.0000   0.0046
 -12.500  -0.9797   0.03795   0.03496  -0.0478   1.0000   0.0047
 -12.250  -0.9912   0.03483   0.03167  -0.0475   1.0000   0.0047
 -12.000  -1.0033   0.03224   0.02890  -0.0454   1.0000   0.0047
 -11.750  -1.0048   0.03079   0.02734  -0.0427   1.0000   0.0047
 -11.500  -1.0032   0.02904   0.02543  -0.0405   1.0000   0.0048
 -11.250  -0.9939   0.02765   0.02391  -0.0389   1.0000   0.0048
 -11.000  -0.9829   0.02626   0.02237  -0.0374   1.0000   0.0049
 -10.750  -0.9700   0.02495   0.02093  -0.0360   1.0000   0.0049
 -10.500  -0.9542   0.02389   0.01974  -0.0348   1.0000   0.0050
 -10.250  -0.9388   0.02267   0.01838  -0.0335   1.0000   0.0051
 -10.000  -0.9223   0.02155   0.01713  -0.0323   1.0000   0.0052
  -9.750  -0.9053   0.02045   0.01590  -0.0310   1.0000   0.0053
  -9.500  -0.8877   0.01942   0.01475  -0.0297   1.0000   0.0054
  -9.250  -0.8701   0.01845   0.01367  -0.0283   1.0000   0.0054
  -9.000  -0.8518   0.01763   0.01276  -0.0269   1.0000   0.0055
  -8.750  -0.8334   0.01687   0.01191  -0.0255   1.0000   0.0057
  -8.500  -0.8075   0.01609   0.01103  -0.0256   0.9977   0.0058
  -8.250  -0.7783   0.01527   0.01012  -0.0264   0.9936   0.0059
  -8.000  -0.7486   0.01461   0.00939  -0.0272   0.9894   0.0060
  -7.750  -0.7171   0.01407   0.00878  -0.0284   0.9857   0.0062
  -7.500  -0.6875   0.01351   0.00815  -0.0291   0.9802   0.0062
  -7.250  -0.6584   0.01268   0.00723  -0.0298   0.9737   0.0065
  -7.000  -0.6303   0.01201   0.00649  -0.0301   0.9654   0.0067
  -6.750  -0.6017   0.01150   0.00593  -0.0305   0.9568   0.0069
  -6.500  -0.5750   0.01108   0.00545  -0.0304   0.9458   0.0071
  -6.250  -0.5491   0.01073   0.00504  -0.0300   0.9343   0.0073
  -6.000  -0.5237   0.01040   0.00465  -0.0296   0.9228   0.0075
  -5.750  -0.4983   0.01011   0.00429  -0.0290   0.9111   0.0078
  -5.500  -0.4727   0.00986   0.00397  -0.0286   0.8990   0.0082
  -5.250  -0.4468   0.00963   0.00368  -0.0281   0.8866   0.0086
  -5.000  -0.4207   0.00941   0.00340  -0.0277   0.8745   0.0089
  -4.750  -0.3946   0.00918   0.00310  -0.0273   0.8622   0.0093
  -4.500  -0.3683   0.00896   0.00280  -0.0270   0.8500   0.0100
  -4.250  -0.3418   0.00879   0.00256  -0.0266   0.8370   0.0107
  -4.000  -0.3151   0.00863   0.00235  -0.0264   0.8239   0.0118
  -3.750  -0.2883   0.00848   0.00215  -0.0261   0.8108   0.0148
  -3.500  -0.2625   0.00812   0.00190  -0.0257   0.7977   0.0452
  -3.250  -0.2369   0.00777   0.00168  -0.0254   0.7840   0.0866
  -3.000  -0.2109   0.00747   0.00150  -0.0251   0.7702   0.1283
  -2.750  -0.1843   0.00728   0.00137  -0.0249   0.7559   0.1590
  -2.500  -0.1576   0.00711   0.00126  -0.0247   0.7414   0.1891
  -2.250  -0.1313   0.00689   0.00115  -0.0245   0.7262   0.2334
  -2.000  -0.1057   0.00656   0.00104  -0.0242   0.7110   0.3054
  -1.750  -0.0791   0.00640   0.00097  -0.0240   0.6955   0.3476
  -1.500  -0.0519   0.00632   0.00091  -0.0238   0.6796   0.3736
  -1.250  -0.0249   0.00624   0.00086  -0.0237   0.6636   0.4034
  -1.000   0.0022   0.00618   0.00083  -0.0235   0.6468   0.4319
  -0.750   0.0294   0.00612   0.00080  -0.0234   0.6300   0.4602
  -0.500   0.0565   0.00608   0.00078  -0.0232   0.6130   0.4880
  -0.250   0.0836   0.00604   0.00077  -0.0231   0.5957   0.5159
   0.000   0.1108   0.00601   0.00077  -0.0229   0.5776   0.5442
   0.250   0.1378   0.00599   0.00077  -0.0227   0.5587   0.5732
   0.500   0.1647   0.00599   0.00079  -0.0225   0.5391   0.6011
   0.750   0.1917   0.00600   0.00081  -0.0224   0.5193   0.6287
   1.000   0.2186   0.00601   0.00085  -0.0222   0.4988   0.6567
   1.250   0.2454   0.00604   0.00089  -0.0219   0.4782   0.6841
   1.500   0.2721   0.00607   0.00094  -0.0217   0.4575   0.7112
   1.750   0.2986   0.00612   0.00101  -0.0214   0.4363   0.7383
   2.000   0.3251   0.00619   0.00108  -0.0211   0.4139   0.7637
   2.500   0.3775   0.00636   0.00125  -0.0204   0.3666   0.8126
   2.750   0.4035   0.00647   0.00136  -0.0200   0.3441   0.8362
   3.000   0.4292   0.00658   0.00147  -0.0195   0.3208   0.8595
   3.250   0.4548   0.00670   0.00159  -0.0190   0.3003   0.8833
   3.500   0.4801   0.00683   0.00172  -0.0184   0.2785   0.9071
   3.750   0.5045   0.00717   0.00190  -0.0177   0.2310   0.9305
   4.000   0.5313   0.00760   0.00213  -0.0177   0.1765   0.9514
   4.250   0.5628   0.00791   0.00233  -0.0186   0.1484   0.9667
   4.500   0.5951   0.00822   0.00253  -0.0198   0.1231   0.9774
   4.750   0.6266   0.00856   0.00276  -0.0208   0.0982   0.9857
   5.000   0.6592   0.00898   0.00303  -0.0221   0.0690   0.9913
   5.250   0.6905   0.00944   0.00335  -0.0232   0.0428   0.9968
   5.500   0.7196   0.00989   0.00368  -0.0237   0.0228   1.0000
   5.750   0.7412   0.01034   0.00405  -0.0226   0.0102   1.0000
   6.000   0.7648   0.01061   0.00434  -0.0218   0.0087   1.0000
   6.250   0.7885   0.01089   0.00463  -0.0211   0.0080   1.0000
   6.500   0.8123   0.01118   0.00495  -0.0204   0.0075   1.0000
   6.750   0.8361   0.01151   0.00530  -0.0196   0.0071   1.0000
   7.000   0.8596   0.01189   0.00572  -0.0189   0.0067   1.0000
   7.250   0.8830   0.01229   0.00616  -0.0182   0.0063   1.0000
   7.500   0.9069   0.01263   0.00652  -0.0176   0.0060   1.0000
   7.750   0.9304   0.01302   0.00696  -0.0169   0.0058   1.0000
   8.000   0.9537   0.01345   0.00742  -0.0162   0.0056   1.0000
   8.250   0.9767   0.01389   0.00792  -0.0155   0.0054   1.0000
   8.500   0.9994   0.01436   0.00843  -0.0147   0.0053   1.0000
   8.750   1.0217   0.01488   0.00899  -0.0139   0.0051   1.0000
   9.000   1.0434   0.01542   0.00959  -0.0131   0.0049   1.0000
   9.250   1.0648   0.01599   0.01021  -0.0122   0.0048   1.0000
   9.500   1.0856   0.01660   0.01088  -0.0113   0.0047   1.0000
   9.750   1.1054   0.01727   0.01162  -0.0102   0.0046   1.0000
  10.000   1.1230   0.01813   0.01255  -0.0089   0.0044   1.0000
  10.250   1.1384   0.01914   0.01365  -0.0073   0.0043   1.0000
  10.500   1.1528   0.02019   0.01480  -0.0056   0.0043   1.0000
  10.750   1.1702   0.02089   0.01558  -0.0043   0.0042   1.0000
  11.000   1.1848   0.02178   0.01656  -0.0027   0.0041   1.0000
  11.250   1.1997   0.02256   0.01743  -0.0011   0.0041   1.0000
  11.500   1.2102   0.02344   0.01839   0.0011   0.0040   1.0000
  11.750   1.2165   0.02445   0.01950   0.0039   0.0040   1.0000
  12.000   1.2232   0.02549   0.02063   0.0063   0.0039   1.0000
  12.250   1.2291   0.02663   0.02187   0.0085   0.0039   1.0000
  12.500   1.2345   0.02789   0.02323   0.0105   0.0038   1.0000
  12.750   1.2352   0.02960   0.02506   0.0125   0.0038   1.0000
  13.000   1.2352   0.03150   0.02708   0.0141   0.0038   1.0000
  13.250   1.2363   0.03347   0.02917   0.0152   0.0037   1.0000
  13.500   1.2356   0.03576   0.03159   0.0159   0.0037   1.0000
  13.750   1.2335   0.03840   0.03435   0.0162   0.0036   1.0000
  14.000   1.2271   0.04174   0.03783   0.0160   0.0036   1.0000
  14.250   1.2253   0.04478   0.04099   0.0153   0.0036   1.0000
  14.500   1.2173   0.04885   0.04520   0.0141   0.0036   1.0000
  14.750   1.2078   0.05344   0.04994   0.0122   0.0035   1.0000
  15.000   1.1976   0.05840   0.05503   0.0099   0.0036   1.0000
  15.250   1.1929   0.06282   0.05955   0.0075   0.0035   1.0000
  15.500   1.1711   0.07026   0.06717   0.0036   0.0035   1.0000
  15.750   1.1534   0.07742   0.07447  -0.0004   0.0035   1.0000
  16.000   1.1385   0.08440   0.08158  -0.0044   0.0035   1.0000
  16.250   1.1173   0.09283   0.09015  -0.0092   0.0035   1.0000
  16.500   1.1002   0.10080   0.09823  -0.0138   0.0035   1.0000
  16.750   1.0838   0.10893   0.10647  -0.0184   0.0035   1.0000
  17.000   1.0551   0.11993   0.11763  -0.0246   0.0036   1.0000
  17.250   1.0329   0.13003   0.12785  -0.0304   0.0036   1.0000
  17.500   1.0116   0.14025   0.13818  -0.0361   0.0036   1.0000
  17.750   0.9956   0.14953   0.14756  -0.0413   0.0036   1.0000
  18.000   0.9676   0.16252   0.16066  -0.0485   0.0037   1.0000
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