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Eiffel 428 (Bleriot) (eiffel428-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Eiffel 428 (Bleriot) (eiffel428-il)
Reynolds number: 500,000
Max Cl/Cd: 67.99 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eiffel428-il-500000-n5.txt
Download as CSV file: xf-eiffel428-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Eiffel 428 (Bleriot)                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.3930   0.11826   0.11590  -0.0263   1.0000   0.0093
 -12.000  -0.3938   0.11352   0.11117  -0.0279   1.0000   0.0099
 -11.750  -0.3973   0.10821   0.10587  -0.0298   1.0000   0.0102
 -11.500  -0.3946   0.10486   0.10255  -0.0310   1.0000   0.0106
 -11.250  -0.3899   0.10209   0.09979  -0.0319   1.0000   0.0108
 -11.000  -0.3804   0.10058   0.09830  -0.0324   1.0000   0.0113
 -10.750  -0.3758   0.09726   0.09499  -0.0340   0.9995   0.0118
 -10.500  -0.3673   0.09262   0.09036  -0.0377   0.9609   0.0123
 -10.250  -0.3440   0.08058   0.07824  -0.0548   0.9297   0.0138
 -10.000  -0.2969   0.07524   0.07273  -0.0683   0.9015   0.0146
  -9.750  -0.2760   0.07214   0.06926  -0.0736   0.8210   0.0152
  -9.500  -0.2764   0.06928   0.06637  -0.0747   0.8059   0.0157
  -9.250  -0.2843   0.06631   0.06329  -0.0751   0.7753   0.0163
  -8.750  -0.3288   0.04218   0.03893  -0.0942   0.7719   0.0189
  -8.250  -0.2936   0.03915   0.03558  -0.0947   0.7358   0.0197
  -8.000  -0.2777   0.03631   0.03250  -0.0953   0.7209   0.0206
  -7.750  -0.2858   0.02319   0.01825  -0.0959   0.7228   0.0244
  -7.500  -0.2657   0.02197   0.01677  -0.0953   0.7085   0.0251
  -7.250  -0.2417   0.02183   0.01652  -0.0948   0.6928   0.0256
  -7.000  -0.2183   0.02153   0.01605  -0.0942   0.6741   0.0261
  -6.750  -0.1957   0.02076   0.01506  -0.0935   0.6545   0.0267
  -6.500  -0.1733   0.02006   0.01409  -0.0928   0.6252   0.0275
  -6.250  -0.1514   0.01911   0.01280  -0.0919   0.5910   0.0285
  -6.000  -0.1304   0.01796   0.01120  -0.0908   0.5432   0.0292
  -5.750  -0.1109   0.01733   0.00996  -0.0894   0.4455   0.0298
  -5.500  -0.0947   0.01758   0.00932  -0.0876   0.2206   0.0304
  -5.250  -0.0703   0.01723   0.00871  -0.0870   0.1816   0.0311
  -4.750  -0.0210   0.01612   0.00718  -0.0859   0.1158   0.0318
  -4.500   0.0037   0.01527   0.00620  -0.0854   0.1141   0.0326
  -4.250   0.0293   0.01486   0.00571  -0.0850   0.1128   0.0331
  -4.000   0.0551   0.01452   0.00532  -0.0845   0.1117   0.0335
  -3.750   0.0809   0.01424   0.00499  -0.0841   0.1108   0.0340
  -3.500   0.1067   0.01397   0.00467  -0.0837   0.1100   0.0345
  -3.250   0.1325   0.01373   0.00437  -0.0833   0.1092   0.0350
  -3.000   0.1582   0.01352   0.00413  -0.0828   0.1084   0.0356
  -2.750   0.1841   0.01337   0.00395  -0.0824   0.1078   0.0365
  -2.500   0.2099   0.01322   0.00376  -0.0820   0.1072   0.0374
  -2.250   0.2356   0.01306   0.00357  -0.0815   0.1068   0.0382
  -2.000   0.2613   0.01294   0.00342  -0.0811   0.1062   0.0390
  -1.750   0.2870   0.01285   0.00331  -0.0806   0.1058   0.0397
  -1.500   0.3128   0.01281   0.00324  -0.0802   0.1054   0.0404
  -1.250   0.3380   0.01266   0.00309  -0.0797   0.1050   0.0420
  -1.000   0.3636   0.01262   0.00305  -0.0793   0.1047   0.0438
  -0.750   0.3892   0.01263   0.00305  -0.0788   0.1045   0.0456
  -0.500   0.4149   0.01266   0.00308  -0.0784   0.1043   0.0476
  -0.250   0.4407   0.01268   0.00308  -0.0780   0.1040   0.0498
   0.000   0.4667   0.01271   0.00310  -0.0777   0.1032   0.0518
   0.250   0.4924   0.01271   0.00309  -0.0773   0.1023   0.0576
   0.500   0.5182   0.01274   0.00313  -0.0769   0.1007   0.0628
   0.750   0.5437   0.01277   0.00319  -0.0765   0.0992   0.0765
   1.000   0.5673   0.01251   0.00333  -0.0759   0.0982   0.2389
   1.250   0.5858   0.01176   0.00352  -0.0745   0.0972   0.5914
   1.750   0.6823   0.01137   0.00395  -0.0841   0.0934   1.0000
   2.000   0.7083   0.01140   0.00396  -0.0837   0.0912   1.0000
   2.250   0.7340   0.01146   0.00398  -0.0834   0.0866   1.0000
   2.500   0.7593   0.01155   0.00402  -0.0829   0.0622   1.0000
   2.750   0.7819   0.01188   0.00420  -0.0820   0.0492   1.0000
   3.000   0.8052   0.01214   0.00446  -0.0812   0.0462   1.0000
   3.250   0.8287   0.01238   0.00471  -0.0805   0.0448   1.0000
   3.500   0.8518   0.01265   0.00500  -0.0797   0.0432   1.0000
   3.750   0.8746   0.01293   0.00530  -0.0788   0.0417   1.0000
   4.000   0.8971   0.01325   0.00563  -0.0779   0.0402   1.0000
   4.250   0.9188   0.01361   0.00602  -0.0769   0.0383   1.0000
   4.500   0.9412   0.01391   0.00635  -0.0760   0.0373   1.0000
   4.750   0.9636   0.01420   0.00668  -0.0751   0.0365   1.0000
   5.000   0.9858   0.01450   0.00700  -0.0742   0.0350   1.0000
   5.250   1.0073   0.01484   0.00737  -0.0732   0.0335   1.0000
   5.500   1.0286   0.01519   0.00774  -0.0722   0.0320   1.0000
   5.750   1.0483   0.01563   0.00820  -0.0710   0.0304   1.0000
   6.000   1.0667   0.01615   0.00875  -0.0695   0.0290   1.0000
   6.250   1.0882   0.01643   0.00907  -0.0686   0.0279   1.0000
   6.500   1.1084   0.01679   0.00946  -0.0675   0.0262   1.0000
   6.750   1.1284   0.01714   0.00986  -0.0663   0.0245   1.0000
   7.000   1.1479   0.01750   0.01022  -0.0651   0.0227   1.0000
   7.250   1.1655   0.01796   0.01071  -0.0636   0.0212   1.0000
   7.500   1.1825   0.01838   0.01117  -0.0620   0.0197   1.0000
   7.750   1.1982   0.01881   0.01163  -0.0601   0.0182   1.0000
   8.000   1.2139   0.01923   0.01207  -0.0583   0.0167   1.0000
   8.250   1.2261   0.01986   0.01273  -0.0560   0.0154   1.0000
   8.500   1.2400   0.02042   0.01335  -0.0541   0.0143   1.0000
   8.750   1.2528   0.02108   0.01405  -0.0521   0.0133   1.0000
   9.000   1.2652   0.02178   0.01479  -0.0503   0.0125   1.0000
   9.250   1.2758   0.02265   0.01569  -0.0483   0.0116   1.0000
   9.500   1.2833   0.02377   0.01688  -0.0461   0.0111   1.0000
   9.750   1.2927   0.02482   0.01802  -0.0443   0.0106   1.0000
  10.000   1.3015   0.02598   0.01929  -0.0426   0.0102   1.0000
  10.250   1.3115   0.02710   0.02048  -0.0412   0.0096   1.0000
  10.500   1.3211   0.02829   0.02174  -0.0399   0.0091   1.0000
  10.750   1.3306   0.02954   0.02304  -0.0388   0.0086   1.0000
  11.000   1.3368   0.03113   0.02471  -0.0374   0.0084   1.0000
  11.250   1.3393   0.03312   0.02678  -0.0361   0.0080   1.0000
  11.500   1.3438   0.03498   0.02874  -0.0349   0.0078   1.0000
  11.750   1.3489   0.03685   0.03072  -0.0339   0.0077   1.0000
  12.000   1.3543   0.03871   0.03270  -0.0331   0.0074   1.0000
  12.250   1.3568   0.04090   0.03501  -0.0321   0.0073   1.0000
  12.500   1.3606   0.04300   0.03721  -0.0314   0.0070   1.0000
  12.750   1.3635   0.04523   0.03955  -0.0307   0.0068   1.0000
  13.000   1.3661   0.04753   0.04195  -0.0301   0.0066   1.0000
  13.250   1.3689   0.04983   0.04435  -0.0297   0.0065   1.0000
  13.500   1.3718   0.05218   0.04679  -0.0294   0.0063   1.0000
  13.750   1.3727   0.05483   0.04954  -0.0292   0.0061   1.0000
  14.000   1.3713   0.05783   0.05265  -0.0291   0.0060   1.0000
  14.250   1.3713   0.06075   0.05565  -0.0292   0.0058   1.0000
  14.500   1.3677   0.06418   0.05922  -0.0293   0.0058   1.0000
  14.750   1.3635   0.06785   0.06297  -0.0298   0.0056   1.0000
  15.000   1.3566   0.07194   0.06721  -0.0303   0.0055   1.0000
  15.250   1.3527   0.07576   0.07118  -0.0310   0.0055   1.0000
  15.500   1.3491   0.07965   0.07523  -0.0318   0.0053   1.0000
  15.750   1.3436   0.08393   0.07966  -0.0329   0.0053   1.0000
  16.000   1.3356   0.08872   0.08460  -0.0342   0.0052   1.0000
  16.250   1.3253   0.09403   0.09008  -0.0359   0.0052   1.0000
  16.500   1.3154   0.09946   0.09567  -0.0378   0.0051   1.0000
  16.750   1.3026   0.10554   0.10191  -0.0402   0.0051   1.0000
  17.000   1.2892   0.11195   0.10850  -0.0430   0.0050   1.0000
  17.250   1.2752   0.11874   0.11545  -0.0461   0.0050   1.0000
  17.500   1.2600   0.12606   0.12293  -0.0497   0.0050   1.0000
  17.750   1.2432   0.13406   0.13110  -0.0540   0.0049   1.0000
  18.000   1.2220   0.14355   0.14077  -0.0592   0.0049   1.0000
  18.250   1.1989   0.15404   0.15143  -0.0652   0.0051   1.0000
  18.500   1.1693   0.16702   0.16460  -0.0728   0.0051   1.0000
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