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Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il)
Reynolds number: 100,000
Max Cl/Cd: 55.24 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eiffel385-il-100000-n5.txt
Download as CSV file: xf-eiffel385-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Eiffel 385 (S.T. Ae)                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.4169   0.09142   0.08571  -0.0536   1.0000   0.0636
 -13.500  -0.4174   0.08899   0.08333  -0.0534   1.0000   0.0642
 -13.000  -0.7212   0.04427   0.03844  -0.0785   1.0000   0.0644
 -12.750  -0.7172   0.04181   0.03588  -0.0789   0.9989   0.0654
 -12.500  -0.6913   0.03879   0.03263  -0.0835   0.9927   0.0674
 -12.250  -0.6678   0.03546   0.02892  -0.0874   0.9857   0.0699
 -12.000  -0.6403   0.03324   0.02644  -0.0901   0.9798   0.0728
 -11.750  -0.6100   0.03224   0.02539  -0.0918   0.9734   0.0759
 -11.500  -0.5816   0.03016   0.02292  -0.0940   0.9671   0.0808
 -11.250  -0.5510   0.02943   0.02220  -0.0951   0.9602   0.0846
 -11.000  -0.5199   0.02790   0.02031  -0.0969   0.9545   0.0909
 -10.750  -0.4913   0.02720   0.01962  -0.0975   0.9467   0.0960
 -10.500  -0.4564   0.02600   0.01806  -0.0996   0.9418   0.1041
 -10.250  -0.4294   0.02556   0.01767  -0.0995   0.9329   0.1097
 -10.000  -0.3946   0.02458   0.01639  -0.1012   0.9273   0.1174
  -9.750  -0.3648   0.02429   0.01617  -0.1014   0.9194   0.1229
  -9.500  -0.3316   0.02357   0.01520  -0.1025   0.9127   0.1303
  -9.250  -0.2921   0.02346   0.01519  -0.1044   0.9085   0.1367
  -9.000  -0.2658   0.02301   0.01452  -0.1041   0.8977   0.1444
  -8.750  -0.2274   0.02321   0.01483  -0.1055   0.8923   0.1509
  -8.500  -0.1999   0.02276   0.01414  -0.1053   0.8817   0.1580
  -8.250  -0.1638   0.02259   0.01399  -0.1064   0.8752   0.1624
  -8.000  -0.1357   0.02216   0.01341  -0.1062   0.8644   0.1676
  -7.750  -0.1006   0.02155   0.01262  -0.1073   0.8571   0.1727
  -7.500  -0.0730   0.02126   0.01230  -0.1069   0.8457   0.1765
  -7.000  -0.0108   0.02038   0.01114  -0.1075   0.8260   0.1878
  -6.750   0.0208   0.02003   0.01073  -0.1079   0.8166   0.1932
  -6.500   0.0508   0.01963   0.01010  -0.1080   0.8061   0.2003
  -6.250   0.0797   0.01933   0.00983  -0.1079   0.7956   0.2057
  -6.000   0.1113   0.01905   0.00943  -0.1082   0.7865   0.2136
  -5.750   0.1387   0.01880   0.00909  -0.1079   0.7755   0.2204
  -5.500   0.1701   0.01854   0.00879  -0.1082   0.7672   0.2272
  -5.250   0.1971   0.01837   0.00848  -0.1078   0.7564   0.2344
  -5.000   0.2268   0.01813   0.00823  -0.1079   0.7481   0.2403
  -4.750   0.2542   0.01800   0.00807  -0.1075   0.7383   0.2468
  -4.500   0.2834   0.01788   0.00781  -0.1075   0.7300   0.2542
  -4.250   0.3104   0.01776   0.00773  -0.1071   0.7208   0.2602
  -4.000   0.3389   0.01767   0.00759  -0.1069   0.7126   0.2671
  -3.750   0.3660   0.01760   0.00746  -0.1066   0.7034   0.2733
  -3.500   0.3938   0.01754   0.00741  -0.1063   0.6949   0.2801
  -3.250   0.4206   0.01754   0.00735  -0.1058   0.6856   0.2894
  -3.000   0.4478   0.01753   0.00738  -0.1055   0.6771   0.2976
  -2.750   0.4744   0.01754   0.00735  -0.1050   0.6681   0.3061
  -2.500   0.5021   0.01753   0.00735  -0.1048   0.6605   0.3126
  -2.250   0.5281   0.01756   0.00738  -0.1043   0.6518   0.3201
  -2.000   0.5570   0.01756   0.00735  -0.1042   0.6448   0.3280
  -1.750   0.5817   0.01762   0.00747  -0.1035   0.6361   0.3368
  -1.500   0.6095   0.01764   0.00749  -0.1033   0.6287   0.3464
  -1.250   0.6348   0.01771   0.00760  -0.1027   0.6204   0.3581
  -1.000   0.6618   0.01776   0.00766  -0.1024   0.6125   0.3724
  -0.750   0.6885   0.01782   0.00776  -0.1021   0.6048   0.3891
  -0.500   0.7141   0.01787   0.00788  -0.1016   0.5961   0.4080
  -0.250   0.7413   0.01788   0.00795  -0.1014   0.5887   0.4316
   0.000   0.7653   0.01789   0.00815  -0.1007   0.5794   0.4617
   0.250   0.7919   0.01776   0.00824  -0.1004   0.5719   0.5198
   0.750   0.8612   0.01724   0.00863  -0.1030   0.5529   1.0000
   1.000   0.8837   0.01747   0.00886  -0.1020   0.5428   1.0000
   1.250   0.9082   0.01769   0.00902  -0.1013   0.5341   1.0000
   1.500   0.9309   0.01792   0.00925  -0.1003   0.5240   1.0000
   1.750   0.9540   0.01816   0.00946  -0.0995   0.5142   1.0000
   2.000   0.9773   0.01838   0.00967  -0.0986   0.5045   1.0000
   2.250   0.9994   0.01866   0.00996  -0.0976   0.4942   1.0000
   2.500   1.0230   0.01889   0.01013  -0.0968   0.4851   1.0000
   2.750   1.0441   0.01920   0.01048  -0.0957   0.4738   1.0000
   3.000   1.0661   0.01948   0.01075  -0.0947   0.4636   1.0000
   3.250   1.0879   0.01978   0.01101  -0.0936   0.4534   1.0000
   3.500   1.1080   0.02012   0.01138  -0.0924   0.4416   1.0000
   3.750   1.1282   0.02045   0.01168  -0.0911   0.4300   1.0000
   4.000   1.1479   0.02078   0.01195  -0.0898   0.4182   1.0000
   4.250   1.1659   0.02118   0.01238  -0.0882   0.4058   1.0000
   4.500   1.1845   0.02160   0.01282  -0.0868   0.3947   1.0000
   4.750   1.2029   0.02203   0.01318  -0.0854   0.3843   1.0000
   5.000   1.2188   0.02250   0.01368  -0.0836   0.3718   1.0000
   5.250   1.2334   0.02299   0.01417  -0.0816   0.3590   1.0000
   5.500   1.2462   0.02350   0.01467  -0.0793   0.3457   1.0000
   5.750   1.2573   0.02405   0.01516  -0.0768   0.3334   1.0000
   6.000   1.2680   0.02464   0.01580  -0.0744   0.3213   1.0000
   6.250   1.2786   0.02528   0.01647  -0.0720   0.3098   1.0000
   6.500   1.2889   0.02598   0.01716  -0.0697   0.2991   1.0000
   6.750   1.2991   0.02671   0.01797  -0.0675   0.2882   1.0000
   7.000   1.3084   0.02751   0.01883  -0.0653   0.2771   1.0000
   7.250   1.3155   0.02843   0.01977  -0.0629   0.2651   1.0000
   7.500   1.3209   0.02948   0.02085  -0.0606   0.2515   1.0000
   7.750   1.3252   0.03067   0.02210  -0.0583   0.2363   1.0000
   8.000   1.3272   0.03208   0.02351  -0.0560   0.2194   1.0000
   8.250   1.3276   0.03372   0.02516  -0.0539   0.1992   1.0000
   8.500   1.3243   0.03574   0.02713  -0.0518   0.1772   1.0000
   8.750   1.3175   0.03823   0.02951  -0.0498   0.1549   1.0000
   9.000   1.3091   0.04107   0.03225  -0.0482   0.1372   1.0000
   9.250   1.3011   0.04410   0.03522  -0.0469   0.1245   1.0000
   9.500   1.2934   0.04729   0.03839  -0.0460   0.1153   1.0000
   9.750   1.2869   0.05051   0.04164  -0.0453   0.1083   1.0000
  10.000   1.2809   0.05382   0.04499  -0.0449   0.1029   1.0000
  10.250   1.2768   0.05702   0.04826  -0.0446   0.0981   1.0000
  10.500   1.2713   0.06048   0.05176  -0.0445   0.0946   1.0000
  10.750   1.2672   0.06384   0.05516  -0.0444   0.0917   1.0000
  11.000   1.2667   0.06685   0.05828  -0.0444   0.0887   1.0000
  11.250   1.2654   0.07001   0.06152  -0.0446   0.0859   1.0000
  11.500   1.2637   0.07325   0.06481  -0.0448   0.0836   1.0000
  11.750   1.2628   0.07636   0.06791  -0.0449   0.0815   1.0000
  12.000   1.2663   0.07901   0.07069  -0.0451   0.0793   1.0000
  12.250   1.2693   0.08174   0.07351  -0.0453   0.0771   1.0000
  12.500   1.2722   0.08449   0.07633  -0.0456   0.0751   1.0000
  12.750   1.2755   0.08718   0.07904  -0.0458   0.0732   1.0000
  13.000   1.2813   0.08938   0.08120  -0.0459   0.0713   1.0000
  13.250   1.2851   0.09216   0.08415  -0.0463   0.0695   1.0000
  13.500   1.2888   0.09495   0.08705  -0.0468   0.0676   1.0000
  13.750   1.2920   0.09778   0.08996  -0.0473   0.0657   1.0000
  14.000   1.2967   0.10033   0.09252  -0.0478   0.0638   1.0000
  14.250   1.3055   0.10208   0.09422  -0.0478   0.0620   1.0000
  14.500   1.3041   0.10589   0.09824  -0.0490   0.0605   1.0000
  14.750   1.3038   0.10949   0.10200  -0.0502   0.0589   1.0000
  15.000   1.3048   0.11283   0.10547  -0.0513   0.0573   1.0000
  15.250   1.3077   0.11578   0.10847  -0.0523   0.0557   1.0000
  15.500   1.3191   0.11706   0.10966  -0.0523   0.0540   1.0000
  15.750   1.3143   0.12156   0.11436  -0.0542   0.0529   1.0000
  16.000   1.3050   0.12704   0.12009  -0.0567   0.0517   1.0000
  16.250   1.2972   0.13228   0.12554  -0.0593   0.0505   1.0000
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