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E211 (10.96%) (e211-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E211 (10.96%) (e211-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.68 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e211-il-1000000-n5.txt
Download as CSV file: xf-e211-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E211  (10.96%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.5193   0.10606   0.10437  -0.0292   1.0000   0.0063
 -11.500  -0.7561   0.04717   0.04495  -0.0627   0.9996   0.0058
 -11.250  -0.7694   0.03957   0.03709  -0.0723   0.9970   0.0058
 -11.000  -0.7706   0.03517   0.03247  -0.0782   0.9937   0.0058
 -10.750  -0.7697   0.03020   0.02709  -0.0816   0.9894   0.0059
 -10.500  -0.7540   0.02696   0.02355  -0.0840   0.9872   0.0059
 -10.250  -0.7320   0.02429   0.02060  -0.0864   0.9857   0.0060
 -10.000  -0.7043   0.02241   0.01852  -0.0887   0.9847   0.0061
  -9.750  -0.6861   0.02108   0.01704  -0.0881   0.9810   0.0062
  -9.500  -0.6600   0.01998   0.01582  -0.0890   0.9784   0.0063
  -9.250  -0.6315   0.01892   0.01464  -0.0902   0.9767   0.0064
  -9.000  -0.6015   0.01808   0.01371  -0.0915   0.9753   0.0066
  -8.750  -0.5712   0.01719   0.01270  -0.0929   0.9743   0.0067
  -8.500  -0.5403   0.01630   0.01172  -0.0943   0.9735   0.0068
  -8.250  -0.5090   0.01545   0.01076  -0.0957   0.9728   0.0070
  -8.000  -0.4937   0.01478   0.01001  -0.0935   0.9678   0.0071
  -7.750  -0.4669   0.01405   0.00918  -0.0937   0.9653   0.0073
  -7.500  -0.4375   0.01338   0.00843  -0.0945   0.9635   0.0075
  -7.250  -0.4069   0.01273   0.00772  -0.0955   0.9621   0.0077
  -7.000  -0.3753   0.01216   0.00708  -0.0966   0.9609   0.0079
  -6.750  -0.3429   0.01164   0.00650  -0.0979   0.9599   0.0081
  -6.500  -0.3271   0.01129   0.00610  -0.0955   0.9526   0.0083
  -6.250  -0.2979   0.01085   0.00562  -0.0959   0.9496   0.0084
  -6.000  -0.2669   0.01045   0.00518  -0.0968   0.9474   0.0085
  -5.750  -0.2461   0.01006   0.00475  -0.0954   0.9396   0.0087
  -5.500  -0.2153   0.00948   0.00410  -0.0963   0.9353   0.0091
  -5.250  -0.1840   0.00907   0.00365  -0.0971   0.9297   0.0094
  -5.000  -0.1480   0.00871   0.00326  -0.0990   0.9236   0.0100
  -4.750  -0.1088   0.00840   0.00291  -0.1016   0.9165   0.0106
  -4.500  -0.0690   0.00811   0.00255  -0.1043   0.9056   0.0113
  -4.250  -0.0334   0.00790   0.00226  -0.1060   0.8881   0.0119
  -4.000  -0.0023   0.00778   0.00203  -0.1067   0.8668   0.0126
  -3.750   0.0256   0.00770   0.00183  -0.1067   0.8438   0.0144
  -3.500   0.0519   0.00763   0.00168  -0.1064   0.8209   0.0180
  -3.250   0.0774   0.00743   0.00151  -0.1060   0.7995   0.0481
  -3.000   0.1029   0.00727   0.00138  -0.1056   0.7786   0.0793
  -2.750   0.1284   0.00711   0.00128  -0.1052   0.7592   0.1200
  -2.500   0.1543   0.00698   0.00120  -0.1049   0.7408   0.1573
  -2.250   0.1803   0.00682   0.00112  -0.1047   0.7232   0.2057
  -2.000   0.2065   0.00671   0.00106  -0.1045   0.7067   0.2465
  -1.750   0.2326   0.00645   0.00099  -0.1044   0.6910   0.3258
  -1.500   0.2587   0.00610   0.00095  -0.1044   0.6765   0.4425
  -1.250   0.2854   0.00602   0.00095  -0.1042   0.6624   0.4942
  -1.000   0.3125   0.00605   0.00096  -0.1040   0.6494   0.5153
  -0.750   0.3396   0.00607   0.00098  -0.1039   0.6368   0.5351
  -0.500   0.3668   0.00611   0.00100  -0.1037   0.6245   0.5494
   0.000   0.4214   0.00621   0.00105  -0.1035   0.6010   0.5723
   0.250   0.4487   0.00626   0.00108  -0.1033   0.5893   0.5828
   0.500   0.4759   0.00633   0.00112  -0.1032   0.5773   0.5925
   0.750   0.5028   0.00641   0.00117  -0.1030   0.5631   0.6023
   1.000   0.5297   0.00649   0.00122  -0.1028   0.5482   0.6116
   1.250   0.5567   0.00658   0.00128  -0.1026   0.5336   0.6211
   1.500   0.5836   0.00666   0.00134  -0.1024   0.5198   0.6309
   1.750   0.6104   0.00676   0.00141  -0.1022   0.5050   0.6401
   2.000   0.6371   0.00687   0.00150  -0.1020   0.4880   0.6488
   2.250   0.6636   0.00700   0.00158  -0.1017   0.4696   0.6562
   2.500   0.6899   0.00715   0.00168  -0.1015   0.4507   0.6637
   2.750   0.7162   0.00729   0.00179  -0.1012   0.4317   0.6708
   3.000   0.7421   0.00747   0.00190  -0.1008   0.4093   0.6789
   3.250   0.7680   0.00765   0.00204  -0.1005   0.3882   0.6870
   3.750   0.8185   0.00813   0.00236  -0.0996   0.3344   0.7044
   4.000   0.8403   0.00867   0.00264  -0.0986   0.2722   0.7140
   4.500   0.8840   0.00976   0.00327  -0.0967   0.1659   0.7359
   4.750   0.9079   0.01010   0.00354  -0.0961   0.1398   0.7473
   5.000   0.9311   0.01049   0.00383  -0.0953   0.1113   0.7604
   5.250   0.9543   0.01086   0.00413  -0.0946   0.0879   0.7755
   5.500   0.9771   0.01126   0.00446  -0.0937   0.0651   0.7918
   5.750   0.9991   0.01170   0.00483  -0.0927   0.0428   0.8099
   6.000   1.0210   0.01212   0.00522  -0.0917   0.0272   0.8301
   6.250   1.0410   0.01263   0.00569  -0.0903   0.0101   0.8564
   6.500   1.0616   0.01286   0.00603  -0.0889   0.0078   0.8941
   6.750   1.0823   0.01300   0.00632  -0.0874   0.0071   1.0000
   7.000   1.1056   0.01337   0.00671  -0.0867   0.0065   1.0000
   7.250   1.1285   0.01376   0.00714  -0.0858   0.0059   1.0000
   7.500   1.1508   0.01419   0.00759  -0.0849   0.0055   1.0000
   7.750   1.1734   0.01457   0.00801  -0.0841   0.0053   1.0000
   8.000   1.1955   0.01496   0.00844  -0.0832   0.0051   1.0000
   8.250   1.2170   0.01540   0.00892  -0.0822   0.0048   1.0000
   8.500   1.2379   0.01587   0.00943  -0.0811   0.0047   1.0000
   8.750   1.2580   0.01637   0.00997  -0.0798   0.0045   1.0000
   9.000   1.2775   0.01689   0.01054  -0.0785   0.0043   1.0000
   9.250   1.2959   0.01743   0.01113  -0.0770   0.0042   1.0000
   9.500   1.3126   0.01799   0.01174  -0.0752   0.0041   1.0000
   9.750   1.3276   0.01861   0.01242  -0.0731   0.0040   1.0000
  10.000   1.3417   0.01929   0.01316  -0.0709   0.0038   1.0000
  10.250   1.3537   0.02009   0.01403  -0.0684   0.0037   1.0000
  10.500   1.3642   0.02099   0.01500  -0.0658   0.0036   1.0000
  10.750   1.3701   0.02219   0.01632  -0.0626   0.0035   1.0000
  11.000   1.3827   0.02294   0.01713  -0.0605   0.0035   1.0000
  11.250   1.3922   0.02392   0.01819  -0.0580   0.0035   1.0000
  11.500   1.4039   0.02476   0.01911  -0.0560   0.0034   1.0000
  11.750   1.4116   0.02588   0.02033  -0.0536   0.0034   1.0000
  12.000   1.4215   0.02688   0.02140  -0.0516   0.0033   1.0000
  12.250   1.4272   0.02822   0.02284  -0.0492   0.0033   1.0000
  12.500   1.4330   0.02960   0.02431  -0.0471   0.0032   1.0000
  12.750   1.4377   0.03113   0.02594  -0.0451   0.0032   1.0000
  13.000   1.4414   0.03281   0.02773  -0.0432   0.0032   1.0000
  13.250   1.4438   0.03470   0.02972  -0.0415   0.0031   1.0000
  13.500   1.4457   0.03674   0.03187  -0.0401   0.0031   1.0000
  13.750   1.4463   0.03902   0.03426  -0.0389   0.0030   1.0000
  14.000   1.4463   0.04150   0.03687  -0.0380   0.0030   1.0000
  14.250   1.4444   0.04432   0.03981  -0.0373   0.0029   1.0000
  14.500   1.4408   0.04749   0.04311  -0.0369   0.0029   1.0000
  14.750   1.4373   0.05084   0.04658  -0.0370   0.0029   1.0000
  15.000   1.4312   0.05469   0.05057  -0.0373   0.0029   1.0000
  15.250   1.4267   0.05853   0.05453  -0.0380   0.0028   1.0000
  15.500   1.4189   0.06303   0.05916  -0.0391   0.0028   1.0000
  15.750   1.4113   0.06771   0.06398  -0.0406   0.0028   1.0000
  16.000   1.4012   0.07300   0.06941  -0.0425   0.0028   1.0000
  16.250   1.3909   0.07859   0.07513  -0.0448   0.0028   1.0000
  16.500   1.3804   0.08447   0.08115  -0.0474   0.0028   1.0000
  16.750   1.3678   0.09094   0.08776  -0.0505   0.0027   1.0000
  17.000   1.3543   0.09786   0.09481  -0.0540   0.0027   1.0000
  17.250   1.3394   0.10534   0.10244  -0.0580   0.0027   1.0000
  17.500   1.3242   0.11309   0.11032  -0.0622   0.0027   1.0000
  17.750   1.3084   0.12125   0.11862  -0.0669   0.0027   1.0000
  18.000   1.2918   0.12980   0.12731  -0.0719   0.0027   1.0000
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