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E230 (9.96%) (e230-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E230 (9.96%) (e230-il)
Reynolds number: 1,000,000
Max Cl/Cd: 58.05 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e230-il-1000000-n5.txt
Download as CSV file: xf-e230-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E230  (9.96%)                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.9705   0.14245   0.14073   0.0566   1.0000   0.0035
 -15.750  -1.0100   0.12641   0.12455   0.0476   1.0000   0.0034
 -15.500  -1.0397   0.11375   0.11177   0.0403   1.0000   0.0034
 -15.250  -1.0719   0.10131   0.09920   0.0329   1.0000   0.0034
 -15.000  -1.1011   0.09000   0.08774   0.0260   1.0000   0.0033
 -14.750  -1.1275   0.07973   0.07734   0.0196   1.0000   0.0033
 -14.500  -1.1452   0.07154   0.06900   0.0142   1.0000   0.0033
 -14.250  -1.1652   0.06341   0.06070   0.0089   1.0000   0.0033
 -14.000  -1.1841   0.05627   0.05339   0.0045   1.0000   0.0033
 -13.750  -1.1992   0.05050   0.04745   0.0015   1.0000   0.0033
 -13.500  -1.2086   0.04621   0.04301  -0.0001   1.0000   0.0033
 -13.250  -1.2192   0.04233   0.03898  -0.0007   1.0000   0.0034
 -13.000  -1.2288   0.03905   0.03553  -0.0002   1.0000   0.0034
 -12.750  -1.2358   0.03639   0.03272   0.0012   1.0000   0.0034
 -12.500  -1.2388   0.03434   0.03052   0.0031   1.0000   0.0034
 -12.250  -1.2395   0.03259   0.02862   0.0055   1.0000   0.0035
 -12.000  -1.2400   0.03094   0.02683   0.0084   1.0000   0.0035
 -11.750  -1.2344   0.02980   0.02558   0.0109   1.0000   0.0035
 -11.500  -1.2310   0.02842   0.02407   0.0140   1.0000   0.0035
 -11.250  -1.2213   0.02718   0.02270   0.0161   1.0000   0.0036
 -11.000  -1.2092   0.02595   0.02134   0.0179   1.0000   0.0036
 -10.750  -1.1933   0.02501   0.02029   0.0194   1.0000   0.0036
 -10.500  -1.1781   0.02388   0.01904   0.0209   1.0000   0.0037
 -10.250  -1.1637   0.02255   0.01758   0.0225   1.0000   0.0037
 -10.000  -1.1503   0.02102   0.01589   0.0244   1.0000   0.0038
  -9.750  -1.1336   0.01985   0.01460   0.0258   1.0000   0.0039
  -9.500  -1.1145   0.01890   0.01357   0.0269   1.0000   0.0040
  -9.250  -1.0944   0.01805   0.01264   0.0280   1.0000   0.0040
  -9.000  -1.0729   0.01734   0.01185   0.0288   1.0000   0.0041
  -8.750  -1.0510   0.01664   0.01109   0.0296   1.0000   0.0042
  -8.500  -1.0284   0.01601   0.01039   0.0304   1.0000   0.0043
  -8.250  -1.0055   0.01538   0.00971   0.0310   1.0000   0.0044
  -8.000  -0.9819   0.01483   0.00911   0.0316   1.0000   0.0046
  -7.750  -0.9576   0.01435   0.00859   0.0321   1.0000   0.0048
  -7.500  -0.9334   0.01383   0.00802   0.0327   1.0000   0.0050
  -7.250  -0.9089   0.01333   0.00746   0.0332   1.0000   0.0052
  -7.000  -0.8813   0.01285   0.00693   0.0330   0.9752   0.0054
  -6.750  -0.8554   0.01246   0.00647   0.0333   0.9518   0.0055
  -6.500  -0.8330   0.01215   0.00609   0.0345   0.9346   0.0056
  -6.250  -0.8098   0.01186   0.00573   0.0355   0.9203   0.0058
  -6.000  -0.7869   0.01142   0.00519   0.0365   0.9070   0.0061
  -5.750  -0.7629   0.01108   0.00479   0.0373   0.8943   0.0065
  -5.500  -0.7382   0.01080   0.00444   0.0380   0.8819   0.0068
  -5.250  -0.7131   0.01054   0.00413   0.0386   0.8696   0.0074
  -5.000  -0.6875   0.01032   0.00383   0.0391   0.8572   0.0078
  -4.750  -0.6616   0.01012   0.00357   0.0395   0.8444   0.0084
  -4.500  -0.6357   0.00988   0.00329   0.0400   0.8314   0.0107
  -4.250  -0.6110   0.00946   0.00295   0.0406   0.8182   0.0312
  -4.000  -0.5859   0.00909   0.00266   0.0411   0.8048   0.0577
  -3.750  -0.5605   0.00877   0.00242   0.0415   0.7912   0.0832
  -3.500  -0.5348   0.00848   0.00221   0.0419   0.7774   0.1114
  -3.250  -0.5093   0.00816   0.00201   0.0423   0.7635   0.1482
  -3.000  -0.4839   0.00783   0.00181   0.0427   0.7497   0.1905
  -2.750  -0.4585   0.00751   0.00164   0.0431   0.7352   0.2366
  -2.500  -0.4327   0.00725   0.00150   0.0434   0.7202   0.2780
  -2.250  -0.4065   0.00703   0.00137   0.0437   0.7046   0.3148
  -2.000  -0.3799   0.00687   0.00127   0.0440   0.6882   0.3446
  -1.750  -0.3531   0.00673   0.00118   0.0442   0.6717   0.3720
  -1.500  -0.3264   0.00659   0.00109   0.0444   0.6546   0.4025
  -1.250  -0.2995   0.00648   0.00101   0.0446   0.6372   0.4308
  -1.000  -0.2725   0.00638   0.00095   0.0448   0.6199   0.4576
  -0.750  -0.2456   0.00629   0.00090   0.0450   0.6023   0.4859
  -0.500  -0.2187   0.00620   0.00085   0.0452   0.5843   0.5145
  -0.250  -0.1920   0.00610   0.00081   0.0454   0.5659   0.5460
   0.000  -0.1654   0.00602   0.00078   0.0457   0.5465   0.5777
   0.250  -0.1387   0.00595   0.00076   0.0459   0.5272   0.6086
   0.500  -0.1122   0.00589   0.00075   0.0462   0.5064   0.6399
   0.750  -0.0859   0.00585   0.00075   0.0466   0.4850   0.6710
   1.000  -0.0595   0.00580   0.00076   0.0469   0.4646   0.7006
   1.250  -0.0333   0.00578   0.00077   0.0473   0.4426   0.7309
   1.500  -0.0071   0.00576   0.00080   0.0477   0.4213   0.7601
   1.750   0.0190   0.00576   0.00084   0.0481   0.3988   0.7883
   2.000   0.0451   0.00578   0.00089   0.0485   0.3745   0.8165
   2.250   0.0713   0.00582   0.00095   0.0489   0.3494   0.8443
   2.500   0.0983   0.00585   0.00102   0.0492   0.3290   0.8710
   2.750   0.1265   0.00595   0.00112   0.0491   0.3020   0.8959
   3.000   0.1569   0.00622   0.00126   0.0485   0.2520   0.9173
   3.250   0.1915   0.00655   0.00144   0.0469   0.2043   0.9330
   3.500   0.2272   0.00685   0.00163   0.0450   0.1672   0.9437
   3.750   0.2625   0.00719   0.00183   0.0433   0.1316   0.9506
   4.000   0.2933   0.00752   0.00203   0.0425   0.0992   0.9580
   4.500   0.3559   0.00824   0.00251   0.0406   0.0453   0.9670
   4.750   0.3816   0.00863   0.00278   0.0410   0.0226   0.9729
   5.000   0.4150   0.00901   0.00310   0.0396   0.0120   0.9749
   5.250   0.4477   0.00925   0.00336   0.0385   0.0107   0.9774
   5.500   0.4787   0.00951   0.00363   0.0377   0.0100   0.9804
   5.750   0.5054   0.00978   0.00394   0.0379   0.0095   0.9842
   6.000   0.5382   0.01009   0.00427   0.0367   0.0089   0.9854
   6.250   0.5711   0.01044   0.00465   0.0354   0.0085   0.9866
   6.500   0.6034   0.01090   0.00516   0.0342   0.0080   0.9881
   6.750   0.6350   0.01132   0.00562   0.0331   0.0078   0.9897
   7.000   0.6659   0.01170   0.00606   0.0323   0.0076   0.9914
   7.250   0.6958   0.01213   0.00653   0.0316   0.0074   0.9931
   7.500   0.7247   0.01260   0.00705   0.0310   0.0072   0.9946
   7.750   0.7562   0.01305   0.00755   0.0299   0.0069   0.9955
   8.000   0.7871   0.01356   0.00812   0.0288   0.0067   0.9966
   8.250   0.8175   0.01410   0.00872   0.0279   0.0064   0.9978
   8.500   0.8471   0.01471   0.00940   0.0270   0.0063   0.9989
   8.750   0.8764   0.01533   0.01008   0.0261   0.0061   0.9998
   9.000   0.8991   0.01597   0.01079   0.0266   0.0060   1.0000
   9.250   0.9191   0.01664   0.01152   0.0277   0.0059   1.0000
   9.500   0.9383   0.01735   0.01231   0.0288   0.0058   1.0000
   9.750   0.9570   0.01810   0.01313   0.0300   0.0057   1.0000
  10.000   0.9741   0.01900   0.01411   0.0313   0.0056   1.0000
  10.250   0.9891   0.02009   0.01530   0.0328   0.0055   1.0000
  10.500   1.0003   0.02156   0.01691   0.0347   0.0054   1.0000
  10.750   1.0100   0.02308   0.01858   0.0368   0.0053   1.0000
  11.000   1.0228   0.02411   0.01972   0.0385   0.0053   1.0000
  11.250   1.0356   0.02503   0.02074   0.0401   0.0052   1.0000
  11.500   1.0457   0.02610   0.02192   0.0420   0.0052   1.0000
  11.750   1.0536   0.02722   0.02315   0.0440   0.0052   1.0000
  12.000   1.0547   0.02860   0.02465   0.0468   0.0051   1.0000
  12.250   1.0466   0.03009   0.02626   0.0503   0.0051   1.0000
  12.500   1.0439   0.03184   0.02813   0.0520   0.0051   1.0000
  12.750   1.0414   0.03401   0.03043   0.0526   0.0051   1.0000
  13.000   1.0373   0.03678   0.03333   0.0523   0.0050   1.0000
  13.250   1.0314   0.04020   0.03690   0.0511   0.0050   1.0000
  13.500   1.0263   0.04395   0.04078   0.0491   0.0050   1.0000
  13.750   1.0163   0.04884   0.04581   0.0462   0.0049   1.0000
  14.000   0.9993   0.05517   0.05231   0.0421   0.0050   1.0000
  14.250   0.9863   0.06133   0.05861   0.0380   0.0049   1.0000
  14.500   0.9707   0.06811   0.06551   0.0337   0.0049   1.0000
  14.750   0.9486   0.07628   0.07381   0.0287   0.0049   1.0000
  15.000   0.9166   0.08643   0.08410   0.0229   0.0050   1.0000
  15.250   0.8960   0.09487   0.09264   0.0182   0.0050   1.0000
  15.500   0.8598   0.10688   0.10478   0.0119   0.0051   1.0000
  15.750   0.8233   0.11960   0.11761   0.0056   0.0051   1.0000
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