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E10(08%) (e228-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E10(08%) (e228-il)
Reynolds number: 1,000,000
Max Cl/Cd: 71.59 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e228-il-1000000-n5.txt
Download as CSV file: xf-e228-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E10(08%)                                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9647   0.12487   0.12292   0.0236   1.0000   0.0024
 -16.250  -1.0211   0.10749   0.10538   0.0136   1.0000   0.0024
 -16.000  -1.0665   0.09355   0.09130   0.0056   1.0000   0.0023
 -15.750  -1.0844   0.08554   0.08323   0.0010   1.0000   0.0024
 -15.500  -1.1444   0.06936   0.06680  -0.0090   1.0000   0.0023
 -15.250  -1.1860   0.05745   0.05466  -0.0170   1.0000   0.0022
 -15.000  -1.2038   0.05062   0.04767  -0.0214   1.0000   0.0023
 -14.750  -1.2166   0.04529   0.04220  -0.0245   1.0000   0.0023
 -14.500  -1.2291   0.04076   0.03751  -0.0264   1.0000   0.0023
 -14.250  -1.2391   0.03718   0.03378  -0.0271   1.0000   0.0023
 -14.000  -1.2433   0.03464   0.03111  -0.0266   1.0000   0.0023
 -13.750  -1.2502   0.03221   0.02854  -0.0252   1.0000   0.0023
 -13.500  -1.2518   0.03044   0.02664  -0.0233   1.0000   0.0023
 -13.250  -1.2522   0.02891   0.02499  -0.0209   1.0000   0.0023
 -13.000  -1.2511   0.02756   0.02350  -0.0180   1.0000   0.0024
 -12.750  -1.2454   0.02653   0.02236  -0.0154   1.0000   0.0024
 -12.500  -1.2369   0.02536   0.02107  -0.0132   1.0000   0.0024
 -12.250  -1.2285   0.02393   0.01948  -0.0111   1.0000   0.0025
 -12.000  -1.2176   0.02257   0.01796  -0.0092   1.0000   0.0026
 -11.750  -1.2032   0.02142   0.01669  -0.0077   1.0000   0.0028
 -11.500  -1.1860   0.02050   0.01567  -0.0065   1.0000   0.0029
 -11.250  -1.1670   0.01971   0.01480  -0.0055   1.0000   0.0031
 -11.000  -1.1467   0.01903   0.01406  -0.0046   1.0000   0.0033
 -10.750  -1.1259   0.01837   0.01333  -0.0038   1.0000   0.0034
 -10.500  -1.1045   0.01774   0.01262  -0.0030   1.0000   0.0036
 -10.250  -1.0823   0.01719   0.01200  -0.0024   1.0000   0.0039
 -10.000  -1.0602   0.01659   0.01134  -0.0017   1.0000   0.0041
  -9.750  -1.0374   0.01606   0.01074  -0.0010   1.0000   0.0043
  -9.500  -1.0143   0.01555   0.01016  -0.0004   1.0000   0.0044
  -9.250  -0.9924   0.01483   0.00936   0.0004   1.0000   0.0049
  -9.000  -0.9690   0.01432   0.00882   0.0010   1.0000   0.0055
  -8.750  -0.9448   0.01390   0.00839   0.0015   1.0000   0.0060
  -8.500  -0.9204   0.01350   0.00795   0.0019   1.0000   0.0066
  -8.250  -0.8957   0.01313   0.00754   0.0024   1.0000   0.0072
  -8.000  -0.8707   0.01281   0.00718   0.0028   1.0000   0.0076
  -7.750  -0.8464   0.01240   0.00672   0.0033   1.0000   0.0082
  -7.500  -0.8188   0.01198   0.00629   0.0031   0.9913   0.0092
  -7.250  -0.7865   0.01165   0.00595   0.0019   0.9791   0.0102
  -7.000  -0.7560   0.01134   0.00559   0.0012   0.9665   0.0111
  -6.750  -0.7289   0.01107   0.00527   0.0013   0.9527   0.0117
  -6.500  -0.7040   0.01085   0.00499   0.0019   0.9390   0.0121
  -6.250  -0.6796   0.01062   0.00470   0.0027   0.9260   0.0124
  -6.000  -0.6556   0.01030   0.00430   0.0035   0.9132   0.0142
  -5.750  -0.6308   0.01003   0.00400   0.0041   0.9010   0.0157
  -5.500  -0.6054   0.00981   0.00371   0.0046   0.8888   0.0168
  -5.250  -0.5795   0.00962   0.00346   0.0051   0.8767   0.0178
  -5.000  -0.5535   0.00943   0.00321   0.0055   0.8645   0.0197
  -4.750  -0.5277   0.00920   0.00297   0.0060   0.8522   0.0252
  -4.500  -0.5023   0.00888   0.00270   0.0064   0.8398   0.0431
  -4.250  -0.4764   0.00863   0.00248   0.0068   0.8272   0.0597
  -4.000  -0.4506   0.00836   0.00225   0.0072   0.8144   0.0818
  -3.750  -0.4247   0.00811   0.00206   0.0075   0.8012   0.1070
  -3.500  -0.3987   0.00784   0.00188   0.0078   0.7877   0.1375
  -3.250  -0.3722   0.00765   0.00172   0.0081   0.7737   0.1602
  -3.000  -0.3456   0.00747   0.00158   0.0083   0.7594   0.1851
  -2.500  -0.2924   0.00712   0.00133   0.0088   0.7301   0.2415
  -2.250  -0.2665   0.00685   0.00121   0.0091   0.7154   0.2926
  -2.000  -0.2401   0.00665   0.00112   0.0093   0.7002   0.3348
  -1.750  -0.2131   0.00654   0.00103   0.0095   0.6846   0.3614
  -1.500  -0.1861   0.00643   0.00097   0.0097   0.6686   0.3890
  -1.250  -0.1590   0.00634   0.00091   0.0098   0.6517   0.4155
  -1.000  -0.1320   0.00626   0.00086   0.0100   0.6343   0.4432
  -0.750  -0.1049   0.00619   0.00082   0.0102   0.6169   0.4709
  -0.500  -0.0778   0.00612   0.00079   0.0103   0.5991   0.5000
  -0.250  -0.0509   0.00606   0.00076   0.0105   0.5801   0.5306
   0.250   0.0029   0.00596   0.00074   0.0109   0.5425   0.5907
   0.500   0.0298   0.00592   0.00075   0.0111   0.5232   0.6215
   0.750   0.0565   0.00590   0.00076   0.0113   0.5034   0.6509
   1.000   0.0832   0.00588   0.00078   0.0116   0.4829   0.6808
   1.250   0.1098   0.00589   0.00081   0.0119   0.4620   0.7088
   1.500   0.1364   0.00590   0.00085   0.0122   0.4406   0.7363
   1.750   0.1628   0.00593   0.00090   0.0125   0.4188   0.7634
   2.000   0.1891   0.00598   0.00096   0.0128   0.3945   0.7899
   2.250   0.2154   0.00604   0.00104   0.0132   0.3707   0.8160
   2.500   0.2415   0.00610   0.00112   0.0136   0.3483   0.8420
   2.750   0.2674   0.00619   0.00121   0.0141   0.3232   0.8680
   3.000   0.2938   0.00629   0.00131   0.0144   0.2998   0.8927
   3.250   0.3212   0.00643   0.00144   0.0146   0.2765   0.9150
   3.500   0.3510   0.00662   0.00159   0.0142   0.2514   0.9342
   3.750   0.3832   0.00686   0.00175   0.0132   0.2240   0.9482
   4.000   0.4156   0.00710   0.00192   0.0121   0.1992   0.9584
   4.250   0.4466   0.00739   0.00211   0.0113   0.1708   0.9670
   4.500   0.4785   0.00771   0.00231   0.0102   0.1427   0.9727
   4.750   0.5094   0.00802   0.00251   0.0094   0.1178   0.9783
   5.000   0.5389   0.00832   0.00273   0.0089   0.0970   0.9830
   5.250   0.5721   0.00867   0.00298   0.0075   0.0747   0.9853
   5.500   0.6045   0.00897   0.00323   0.0063   0.0606   0.9879
   5.750   0.6358   0.00930   0.00349   0.0053   0.0465   0.9907
   6.000   0.6659   0.00967   0.00379   0.0046   0.0331   0.9935
   6.250   0.6984   0.00998   0.00407   0.0034   0.0254   0.9952
   6.500   0.7309   0.01032   0.00437   0.0021   0.0191   0.9970
   6.750   0.7629   0.01069   0.00471   0.0009   0.0138   0.9987
   7.000   0.7939   0.01109   0.00510  -0.0001   0.0089   1.0000
   7.250   0.8161   0.01145   0.00547   0.0009   0.0068   1.0000
   7.500   0.8384   0.01183   0.00587   0.0019   0.0055   1.0000
   7.750   0.8607   0.01218   0.00626   0.0028   0.0051   1.0000
   8.000   0.8828   0.01255   0.00667   0.0038   0.0047   1.0000
   8.250   0.9046   0.01295   0.00711   0.0048   0.0042   1.0000
   8.500   0.9261   0.01340   0.00760   0.0058   0.0039   1.0000
   8.750   0.9468   0.01393   0.00820   0.0070   0.0035   1.0000
   9.000   0.9665   0.01458   0.00893   0.0082   0.0032   1.0000
   9.250   0.9862   0.01522   0.00965   0.0095   0.0031   1.0000
   9.500   1.0067   0.01573   0.01022   0.0106   0.0030   1.0000
   9.750   1.0268   0.01627   0.01083   0.0117   0.0030   1.0000
  10.000   1.0456   0.01693   0.01157   0.0130   0.0029   1.0000
  10.250   1.0645   0.01757   0.01228   0.0142   0.0029   1.0000
  10.500   1.0831   0.01820   0.01301   0.0155   0.0028   1.0000
  10.750   1.1005   0.01895   0.01384   0.0169   0.0027   1.0000
  11.000   1.1174   0.01969   0.01467   0.0182   0.0026   1.0000
  11.250   1.1326   0.02057   0.01565   0.0198   0.0025   1.0000
  11.500   1.1468   0.02147   0.01665   0.0214   0.0025   1.0000
  11.750   1.1611   0.02231   0.01757   0.0230   0.0024   1.0000
  12.000   1.1717   0.02335   0.01873   0.0249   0.0024   1.0000
  12.250   1.1811   0.02426   0.01972   0.0271   0.0022   1.0000
  12.500   1.1853   0.02524   0.02080   0.0299   0.0022   1.0000
  12.750   1.1886   0.02642   0.02207   0.0323   0.0022   1.0000
  13.000   1.1911   0.02782   0.02358   0.0343   0.0021   1.0000
  13.250   1.1950   0.02927   0.02514   0.0357   0.0020   1.0000
  13.500   1.1859   0.03203   0.02810   0.0370   0.0022   1.0000
  13.750   1.1900   0.03388   0.03001   0.0373   0.0020   1.0000
  14.000   1.1855   0.03681   0.03309   0.0371   0.0020   1.0000
  14.250   1.1876   0.03929   0.03564   0.0365   0.0019   1.0000
  14.500   1.1791   0.04332   0.03983   0.0349   0.0019   1.0000
  14.750   1.1649   0.04857   0.04525   0.0323   0.0020   1.0000
  15.000   1.1544   0.05367   0.05049   0.0295   0.0020   1.0000
  15.250   1.1339   0.06072   0.05771   0.0254   0.0020   1.0000
  15.500   1.1099   0.06871   0.06588   0.0207   0.0020   1.0000
  15.750   1.0951   0.07537   0.07262   0.0169   0.0019   1.0000
  16.000   1.0677   0.08450   0.08188   0.0119   0.0019   1.0000
  16.250   1.0277   0.09625   0.09383   0.0056   0.0021   1.0000
  16.500   0.9998   0.10613   0.10382   0.0005   0.0021   1.0000
  16.750   0.9694   0.11692   0.11471  -0.0051   0.0021   1.0000
  17.000   0.9345   0.12918   0.12710  -0.0114   0.0021   1.0000
  17.250   0.9095   0.13982   0.13782  -0.0168   0.0022   1.0000
  17.500   0.8750   0.15352   0.15165  -0.0237   0.0022   1.0000
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