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Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il)
Reynolds number: 200,000
Max Cl/Cd: 76.02 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-eiffel385-il-200000.txt
Download as CSV file: xf-eiffel385-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7876   0.04595   0.04148  -0.0923   1.0000   0.0587
 -14.250  -0.8138   0.04213   0.03741  -0.0914   1.0000   0.0588
 -14.000  -0.8269   0.03886   0.03391  -0.0900   1.0000   0.0592
 -13.750  -0.8264   0.03661   0.03154  -0.0883   1.0000   0.0597
 -13.500  -0.8190   0.03516   0.03006  -0.0865   1.0000   0.0605
 -13.250  -0.8108   0.03368   0.02849  -0.0849   1.0000   0.0613
 -13.000  -0.8016   0.03218   0.02685  -0.0833   1.0000   0.0623
 -12.750  -0.7908   0.03076   0.02525  -0.0819   1.0000   0.0636
 -12.500  -0.7580   0.02880   0.02294  -0.0847   0.9958   0.0655
 -12.250  -0.7250   0.02695   0.02081  -0.0870   0.9914   0.0674
 -12.000  -0.6903   0.02604   0.01994  -0.0887   0.9864   0.0694
 -11.750  -0.6519   0.02507   0.01883  -0.0912   0.9823   0.0720
 -11.500  -0.6193   0.02392   0.01737  -0.0926   0.9760   0.0752
 -11.250  -0.5814   0.02324   0.01680  -0.0946   0.9713   0.0788
 -11.000  -0.5449   0.02249   0.01584  -0.0964   0.9662   0.0838
 -10.750  -0.5114   0.02175   0.01514  -0.0975   0.9597   0.0887
 -10.500  -0.4710   0.02097   0.01422  -0.0999   0.9558   0.0973
 -10.250  -0.4387   0.02056   0.01365  -0.1006   0.9480   0.1065
 -10.000  -0.4005   0.01990   0.01308  -0.1025   0.9429   0.1171
  -9.750  -0.3577   0.01938   0.01260  -0.1052   0.9398   0.1267
  -9.500  -0.3284   0.01892   0.01199  -0.1052   0.9305   0.1339
  -9.250  -0.2858   0.01877   0.01192  -0.1076   0.9265   0.1414
  -9.000  -0.2403   0.01835   0.01140  -0.1105   0.9239   0.1486
  -8.750  -0.2083   0.01829   0.01139  -0.1108   0.9145   0.1538
  -8.500  -0.1662   0.01790   0.01077  -0.1130   0.9099   0.1604
  -8.250  -0.1214   0.01784   0.01087  -0.1157   0.9064   0.1666
  -8.000  -0.0922   0.01783   0.01071  -0.1153   0.8945   0.1736
  -7.750  -0.0503   0.01747   0.01040  -0.1175   0.8892   0.1793
  -7.500  -0.0219   0.01722   0.01009  -0.1171   0.8762   0.1839
  -7.250   0.0100   0.01680   0.00947  -0.1174   0.8650   0.1890
  -7.000   0.0437   0.01624   0.00886  -0.1181   0.8550   0.1939
  -6.750   0.0713   0.01600   0.00861  -0.1176   0.8413   0.1990
  -6.500   0.1004   0.01575   0.00816  -0.1173   0.8289   0.2055
  -6.250   0.1315   0.01526   0.00764  -0.1176   0.8187   0.2119
  -6.000   0.1573   0.01511   0.00743  -0.1168   0.8054   0.2198
  -5.750   0.1846   0.01481   0.00706  -0.1164   0.7940   0.2282
  -5.500   0.2138   0.01465   0.00683  -0.1163   0.7843   0.2372
  -5.250   0.2393   0.01443   0.00655  -0.1156   0.7727   0.2453
  -5.000   0.2676   0.01432   0.00640  -0.1153   0.7635   0.2532
  -4.750   0.2941   0.01422   0.00619  -0.1148   0.7531   0.2605
  -4.500   0.3210   0.01407   0.00607  -0.1143   0.7434   0.2671
  -4.250   0.3483   0.01404   0.00594  -0.1139   0.7337   0.2742
  -4.000   0.3747   0.01394   0.00581  -0.1134   0.7241   0.2803
  -3.750   0.4021   0.01389   0.00575  -0.1130   0.7156   0.2864
  -3.500   0.4286   0.01390   0.00570  -0.1125   0.7071   0.2922
  -3.250   0.4559   0.01384   0.00560  -0.1122   0.6990   0.2972
  -3.000   0.4827   0.01384   0.00562  -0.1118   0.6913   0.3026
  -2.750   0.5093   0.01386   0.00562  -0.1113   0.6832   0.3090
  -2.500   0.5369   0.01389   0.00562  -0.1111   0.6760   0.3157
  -2.250   0.5624   0.01393   0.00572  -0.1104   0.6676   0.3236
  -2.000   0.5909   0.01401   0.00571  -0.1103   0.6607   0.3317
  -1.750   0.6155   0.01403   0.00583  -0.1096   0.6524   0.3392
  -1.500   0.6429   0.01409   0.00584  -0.1093   0.6448   0.3485
  -1.250   0.6684   0.01411   0.00595  -0.1087   0.6370   0.3574
  -1.000   0.6946   0.01412   0.00599  -0.1083   0.6290   0.3697
  -0.750   0.7210   0.01416   0.00607  -0.1079   0.6215   0.3866
  -0.500   0.7452   0.01410   0.00615  -0.1071   0.6128   0.4096
  -0.250   0.7717   0.01404   0.00618  -0.1067   0.6055   0.4438
   0.000   0.7932   0.01384   0.00630  -0.1055   0.5965   0.4931
   0.250   0.8540   0.01293   0.00642  -0.1122   0.5870   1.0000
   0.500   0.8771   0.01307   0.00654  -0.1112   0.5771   1.0000
   0.750   0.9036   0.01326   0.00661  -0.1108   0.5691   1.0000
   1.000   0.9262   0.01339   0.00676  -0.1097   0.5589   1.0000
   1.250   0.9514   0.01356   0.00685  -0.1091   0.5499   1.0000
   1.500   0.9743   0.01368   0.00697  -0.1081   0.5392   1.0000
   1.750   0.9976   0.01383   0.00710  -0.1072   0.5286   1.0000
   2.000   1.0217   0.01396   0.00713  -0.1064   0.5178   1.0000
   2.250   1.0427   0.01408   0.00728  -0.1050   0.5048   1.0000
   2.500   1.0647   0.01424   0.00741  -0.1039   0.4923   1.0000
   2.750   1.0871   0.01443   0.00753  -0.1028   0.4804   1.0000
   3.000   1.1087   0.01463   0.00769  -0.1017   0.4679   1.0000
   3.250   1.1297   0.01486   0.00793  -0.1004   0.4550   1.0000
   3.500   1.1510   0.01514   0.00816  -0.0993   0.4431   1.0000
   3.750   1.1723   0.01544   0.00838  -0.0982   0.4314   1.0000
   4.000   1.1920   0.01573   0.00866  -0.0968   0.4185   1.0000
   4.250   1.2114   0.01604   0.00897  -0.0954   0.4058   1.0000
   4.500   1.2300   0.01637   0.00926  -0.0939   0.3931   1.0000
   4.750   1.2485   0.01676   0.00956  -0.0924   0.3812   1.0000
   5.000   1.2667   0.01710   0.00995  -0.0908   0.3698   1.0000
   5.250   1.2846   0.01749   0.01034  -0.0893   0.3590   1.0000
   5.750   1.3174   0.01829   0.01116  -0.0857   0.3376   1.0000
   6.000   1.3315   0.01872   0.01159  -0.0835   0.3273   1.0000
   6.250   1.3437   0.01918   0.01203  -0.0811   0.3167   1.0000
   6.500   1.3560   0.01961   0.01253  -0.0787   0.3056   1.0000
   6.750   1.3667   0.02012   0.01307  -0.0761   0.2939   1.0000
   7.000   1.3753   0.02072   0.01366  -0.0733   0.2806   1.0000
   7.250   1.3825   0.02138   0.01434  -0.0705   0.2644   1.0000
   7.500   1.3878   0.02219   0.01515  -0.0676   0.2426   1.0000
   7.750   1.3863   0.02342   0.01627  -0.0641   0.2111   1.0000
   8.000   1.3757   0.02538   0.01797  -0.0600   0.1678   1.0000
   8.250   1.3626   0.02784   0.02016  -0.0562   0.1355   1.0000
   8.500   1.3531   0.03032   0.02251  -0.0533   0.1196   1.0000
   8.750   1.3485   0.03263   0.02479  -0.0511   0.1099   1.0000
   9.000   1.3453   0.03497   0.02713  -0.0493   0.1039   1.0000
   9.250   1.3452   0.03718   0.02939  -0.0480   0.0989   1.0000
   9.500   1.3415   0.03979   0.03199  -0.0467   0.0953   1.0000
   9.750   1.3430   0.04204   0.03429  -0.0457   0.0922   1.0000
  10.000   1.3461   0.04419   0.03652  -0.0449   0.0890   1.0000
  10.250   1.3476   0.04654   0.03891  -0.0442   0.0862   1.0000
  10.500   1.3471   0.04908   0.04141  -0.0434   0.0837   1.0000
  10.750   1.3517   0.05122   0.04363  -0.0429   0.0813   1.0000
  11.000   1.3563   0.05338   0.04587  -0.0424   0.0789   1.0000
  11.250   1.3604   0.05561   0.04814  -0.0421   0.0767   1.0000
  11.500   1.3643   0.05784   0.05036  -0.0416   0.0746   1.0000
  11.750   1.3715   0.05965   0.05215  -0.0409   0.0725   1.0000
  12.000   1.3764   0.06191   0.05454  -0.0407   0.0706   1.0000
  12.250   1.3815   0.06416   0.05687  -0.0405   0.0686   1.0000
  12.500   1.3872   0.06631   0.05903  -0.0403   0.0666   1.0000
  12.750   1.3987   0.06767   0.06031  -0.0396   0.0645   1.0000
  13.000   1.4048   0.06984   0.06259  -0.0393   0.0628   1.0000
  13.250   1.4072   0.07253   0.06543  -0.0394   0.0611   1.0000
  13.500   1.4112   0.07502   0.06800  -0.0395   0.0594   1.0000
  13.750   1.4184   0.07707   0.07005  -0.0395   0.0575   1.0000
  14.000   1.4345   0.07808   0.07100  -0.0385   0.0553   1.0000
  14.250   1.4304   0.08167   0.07481  -0.0392   0.0542   1.0000
  14.500   1.4290   0.08499   0.07829  -0.0398   0.0528   1.0000
  14.750   1.4292   0.08811   0.08152  -0.0404   0.0513   1.0000
  15.000   1.4358   0.09033   0.08376  -0.0406   0.0499   1.0000
  15.250   1.4509   0.09161   0.08498  -0.0399   0.0480   1.0000
  15.500   1.4388   0.09645   0.09008  -0.0415   0.0473   1.0000
  15.750   1.4292   0.10114   0.09500  -0.0430   0.0464   1.0000
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