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Eiffel 428 (Bleriot) (eiffel428-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Eiffel 428 (Bleriot) (eiffel428-il)
Reynolds number: 1,000,000
Max Cl/Cd: 84.03 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eiffel428-il-1000000-n5.txt
Download as CSV file: xf-eiffel428-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.3292   0.09341   0.09087  -0.0648   0.7878   0.0094
 -11.750  -0.3497   0.08434   0.08203  -0.0699   0.8331   0.0105
 -11.250  -0.6926   0.01988   0.01648  -0.0927   0.9555   0.0103
 -11.000  -0.6378   0.01646   0.01260  -0.1010   0.9118   0.0124
 -10.750  -0.6142   0.01557   0.01143  -0.1006   0.8759   0.0136
 -10.500  -0.5921   0.01513   0.01080  -0.0996   0.8445   0.0147
 -10.250  -0.5678   0.01510   0.01069  -0.0989   0.8175   0.0160
 -10.000  -0.5439   0.01488   0.01033  -0.0981   0.7961   0.0172
  -9.750  -0.5217   0.01451   0.00973  -0.0971   0.7642   0.0181
  -9.500  -0.4980   0.01413   0.00917  -0.0964   0.7448   0.0187
  -9.250  -0.4719   0.01420   0.00920  -0.0959   0.7282   0.0195
  -9.000  -0.4451   0.01441   0.00937  -0.0956   0.7141   0.0201
  -8.750  -0.4187   0.01451   0.00942  -0.0952   0.6993   0.0207
  -8.500  -0.3927   0.01456   0.00938  -0.0947   0.6816   0.0213
  -8.250  -0.3668   0.01461   0.00932  -0.0943   0.6608   0.0220
  -8.000  -0.3421   0.01441   0.00895  -0.0937   0.6343   0.0227
  -7.750  -0.3179   0.01409   0.00842  -0.0930   0.6056   0.0232
  -7.500  -0.2940   0.01408   0.00815  -0.0923   0.5511   0.0237
  -7.250  -0.2755   0.01462   0.00799  -0.0907   0.3706   0.0241
  -7.000  -0.2551   0.01514   0.00791  -0.0894   0.1522   0.0243
  -6.750  -0.2292   0.01506   0.00772  -0.0890   0.1130   0.0244
  -6.500  -0.2062   0.01399   0.00645  -0.0883   0.1091   0.0255
  -6.250  -0.1804   0.01367   0.00606  -0.0879   0.1066   0.0260
  -6.000  -0.1543   0.01344   0.00575  -0.0875   0.1050   0.0264
  -5.750  -0.1278   0.01329   0.00556  -0.0872   0.1042   0.0268
  -5.500  -0.1014   0.01315   0.00537  -0.0869   0.1038   0.0274
  -5.250  -0.0752   0.01291   0.00506  -0.0865   0.1034   0.0278
  -5.000  -0.0492   0.01263   0.00472  -0.0861   0.1030   0.0283
  -4.750  -0.0231   0.01239   0.00441  -0.0858   0.1025   0.0287
  -4.500   0.0030   0.01217   0.00414  -0.0854   0.1020   0.0291
  -4.250   0.0291   0.01196   0.00388  -0.0850   0.1016   0.0295
  -4.000   0.0551   0.01175   0.00362  -0.0846   0.1011   0.0298
  -3.750   0.0813   0.01158   0.00340  -0.0842   0.1007   0.0301
  -3.500   0.1074   0.01142   0.00319  -0.0838   0.1003   0.0304
  -3.250   0.1335   0.01128   0.00301  -0.0834   0.0998   0.0307
  -3.000   0.1598   0.01117   0.00287  -0.0831   0.0993   0.0310
  -2.750   0.1860   0.01108   0.00275  -0.0827   0.0990   0.0312
  -2.500   0.2124   0.01104   0.00268  -0.0824   0.0985   0.0315
  -2.250   0.2384   0.01091   0.00251  -0.0820   0.0983   0.0325
  -2.000   0.2645   0.01082   0.00240  -0.0816   0.0979   0.0337
  -1.750   0.2908   0.01080   0.00236  -0.0812   0.0976   0.0347
  -1.500   0.3171   0.01080   0.00236  -0.0809   0.0974   0.0358
  -1.250   0.3435   0.01081   0.00236  -0.0806   0.0970   0.0371
  -1.000   0.3697   0.01084   0.00238  -0.0803   0.0966   0.0384
  -0.750   0.3958   0.01088   0.00241  -0.0799   0.0957   0.0394
  -0.500   0.4214   0.01099   0.00252  -0.0795   0.0940   0.0402
  -0.250   0.4479   0.01098   0.00248  -0.0792   0.0936   0.0422
   0.000   0.4744   0.01096   0.00247  -0.0790   0.0933   0.0452
   0.250   0.5009   0.01097   0.00248  -0.0787   0.0928   0.0478
   0.500   0.5274   0.01100   0.00250  -0.0785   0.0922   0.0502
   0.750   0.5538   0.01104   0.00253  -0.0782   0.0913   0.0530
   1.000   0.5801   0.01105   0.00256  -0.0780   0.0901   0.0606
   1.250   0.6062   0.01103   0.00259  -0.0777   0.0884   0.0905
   1.500   0.6311   0.01082   0.00263  -0.0773   0.0855   0.2263
   1.750   0.6552   0.01059   0.00273  -0.0767   0.0821   0.3665
   2.250   0.7506   0.00976   0.00326  -0.0867   0.0424   1.0000
   2.500   0.7748   0.00996   0.00344  -0.0860   0.0399   1.0000
   2.750   0.7989   0.01016   0.00365  -0.0853   0.0378   1.0000
   3.000   0.8233   0.01033   0.00381  -0.0847   0.0373   1.0000
   3.250   0.8476   0.01052   0.00399  -0.0841   0.0367   1.0000
   3.500   0.8717   0.01071   0.00419  -0.0834   0.0359   1.0000
   3.750   0.8957   0.01091   0.00439  -0.0828   0.0349   1.0000
   4.000   0.9194   0.01112   0.00459  -0.0821   0.0336   1.0000
   4.250   0.9428   0.01136   0.00483  -0.0813   0.0325   1.0000
   4.500   0.9657   0.01163   0.00510  -0.0805   0.0309   1.0000
   4.750   0.9878   0.01195   0.00544  -0.0796   0.0292   1.0000
   5.000   1.0111   0.01217   0.00566  -0.0788   0.0288   1.0000
   5.250   1.0343   0.01240   0.00590  -0.0781   0.0281   1.0000
   5.500   1.0573   0.01263   0.00614  -0.0774   0.0269   1.0000
   5.750   1.0801   0.01286   0.00638  -0.0766   0.0255   1.0000
   6.000   1.1025   0.01312   0.00663  -0.0758   0.0239   1.0000
   6.250   1.1240   0.01344   0.00694  -0.0748   0.0221   1.0000
   6.500   1.1458   0.01372   0.00725  -0.0739   0.0213   1.0000
   6.750   1.1676   0.01399   0.00754  -0.0730   0.0198   1.0000
   7.000   1.1890   0.01428   0.00780  -0.0721   0.0174   1.0000
   7.250   1.2093   0.01462   0.00813  -0.0710   0.0153   1.0000
   7.500   1.2290   0.01498   0.00850  -0.0698   0.0138   1.0000
   7.750   1.2480   0.01538   0.00890  -0.0685   0.0123   1.0000
   8.000   1.2659   0.01582   0.00936  -0.0670   0.0111   1.0000
   8.250   1.2837   0.01624   0.00982  -0.0655   0.0104   1.0000
   8.500   1.2992   0.01669   0.01030  -0.0636   0.0097   1.0000
   8.750   1.3125   0.01718   0.01081  -0.0613   0.0090   1.0000
   9.000   1.3252   0.01772   0.01137  -0.0590   0.0082   1.0000
   9.250   1.3380   0.01830   0.01200  -0.0568   0.0078   1.0000
   9.500   1.3515   0.01888   0.01264  -0.0549   0.0075   1.0000
   9.750   1.3642   0.01952   0.01334  -0.0530   0.0072   1.0000
  10.000   1.3765   0.02023   0.01410  -0.0511   0.0069   1.0000
  10.250   1.3886   0.02099   0.01491  -0.0494   0.0065   1.0000
  10.500   1.3996   0.02186   0.01582  -0.0476   0.0062   1.0000
  10.750   1.4100   0.02283   0.01684  -0.0460   0.0059   1.0000
  11.000   1.4190   0.02396   0.01803  -0.0444   0.0057   1.0000
  11.250   1.4266   0.02526   0.01942  -0.0428   0.0055   1.0000
  11.500   1.4383   0.02628   0.02050  -0.0417   0.0053   1.0000
  11.750   1.4468   0.02760   0.02190  -0.0405   0.0052   1.0000
  12.000   1.4559   0.02893   0.02330  -0.0394   0.0050   1.0000
  12.250   1.4640   0.03038   0.02482  -0.0384   0.0048   1.0000
  12.500   1.4699   0.03208   0.02661  -0.0374   0.0047   1.0000
  12.750   1.4778   0.03363   0.02822  -0.0366   0.0045   1.0000
  13.000   1.4837   0.03540   0.03006  -0.0358   0.0044   1.0000
  13.250   1.4894   0.03721   0.03194  -0.0350   0.0043   1.0000
  13.500   1.4939   0.03917   0.03398  -0.0344   0.0042   1.0000
  13.750   1.4964   0.04138   0.03627  -0.0337   0.0041   1.0000
  14.000   1.4969   0.04381   0.03879  -0.0330   0.0040   1.0000
  14.250   1.4965   0.04640   0.04147  -0.0325   0.0038   1.0000
  14.500   1.4948   0.04921   0.04438  -0.0321   0.0038   1.0000
  14.750   1.4936   0.05203   0.04729  -0.0318   0.0037   1.0000
  15.000   1.4916   0.05503   0.05040  -0.0317   0.0037   1.0000
  15.250   1.4898   0.05810   0.05358  -0.0317   0.0037   1.0000
  15.500   1.4902   0.06095   0.05653  -0.0318   0.0036   1.0000
  15.750   1.4879   0.06420   0.05988  -0.0320   0.0035   1.0000
  16.000   1.4845   0.06772   0.06350  -0.0324   0.0035   1.0000
  16.250   1.4784   0.07167   0.06757  -0.0330   0.0035   1.0000
  16.500   1.4741   0.07543   0.07145  -0.0337   0.0034   1.0000
  16.750   1.4664   0.07980   0.07593  -0.0346   0.0034   1.0000
  17.000   1.4592   0.08418   0.08043  -0.0356   0.0034   1.0000
  17.250   1.4522   0.08863   0.08498  -0.0368   0.0033   1.0000
  17.500   1.4435   0.09339   0.08985  -0.0382   0.0033   1.0000
  17.750   1.4344   0.09833   0.09491  -0.0398   0.0032   1.0000
  18.000   1.4217   0.10403   0.10073  -0.0418   0.0032   1.0000
  18.250   1.4066   0.11024   0.10708  -0.0441   0.0033   1.0000
  18.500   1.3969   0.11563   0.11258  -0.0463   0.0032   1.0000
  18.750   1.3825   0.12209   0.11916  -0.0491   0.0032   1.0000
  19.000   1.3674   0.12892   0.12612  -0.0523   0.0031   1.0000
  19.250   1.3509   0.13630   0.13364  -0.0560   0.0032   1.0000
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