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Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il)
Reynolds number: 500,000
Max Cl/Cd: 106.4 at α=2°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-eiffel385-il-500000.txt
Download as CSV file: xf-eiffel385-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.7168   0.09369   0.09052  -0.0686   1.0000   0.0349
 -18.500  -0.7632   0.08229   0.07893  -0.0769   1.0000   0.0349
 -18.250  -0.7924   0.07449   0.07099  -0.0826   1.0000   0.0349
 -18.000  -0.8159   0.06818   0.06457  -0.0869   1.0000   0.0350
 -17.750  -0.8382   0.06240   0.05868  -0.0906   1.0000   0.0351
 -17.500  -0.8563   0.05756   0.05376  -0.0933   1.0000   0.0352
 -17.250  -0.8717   0.05335   0.04949  -0.0952   1.0000   0.0355
 -17.000  -0.8870   0.04933   0.04543  -0.0968   1.0000   0.0356
 -16.750  -0.9056   0.04523   0.04127  -0.0984   1.0000   0.0357
 -16.500  -0.9317   0.04094   0.03693  -0.0997   1.0000   0.0358
 -16.250  -0.9676   0.03545   0.03128  -0.1027   1.0000   0.0357
 -16.000  -0.9797   0.03322   0.02896  -0.1009   1.0000   0.0359
 -15.750  -0.9848   0.03153   0.02721  -0.0986   1.0000   0.0362
 -15.500  -0.9681   0.02987   0.02548  -0.0994   0.9985   0.0367
 -15.250  -0.9384   0.02828   0.02380  -0.1020   0.9956   0.0375
 -15.000  -0.9067   0.02676   0.02214  -0.1047   0.9932   0.0382
 -14.750  -0.8794   0.02539   0.02065  -0.1061   0.9894   0.0389
 -14.500  -0.8493   0.02419   0.01930  -0.1076   0.9863   0.0395
 -14.250  -0.8173   0.02316   0.01813  -0.1093   0.9839   0.0400
 -14.000  -0.7873   0.02159   0.01651  -0.1111   0.9819   0.0411
 -13.750  -0.7632   0.02062   0.01550  -0.1110   0.9772   0.0420
 -13.500  -0.7335   0.01975   0.01457  -0.1119   0.9739   0.0429
 -13.250  -0.7008   0.01893   0.01366  -0.1131   0.9716   0.0439
 -13.000  -0.6662   0.01814   0.01278  -0.1146   0.9698   0.0449
 -12.750  -0.6367   0.01749   0.01202  -0.1149   0.9662   0.0458
 -12.500  -0.6102   0.01652   0.01103  -0.1150   0.9613   0.0473
 -12.250  -0.5773   0.01580   0.01027  -0.1161   0.9588   0.0491
 -12.000  -0.5422   0.01517   0.00957  -0.1174   0.9569   0.0510
 -11.750  -0.5062   0.01444   0.00878  -0.1190   0.9554   0.0532
 -11.500  -0.4786   0.01382   0.00815  -0.1188   0.9502   0.0563
 -11.250  -0.4468   0.01321   0.00751  -0.1194   0.9459   0.0609
 -11.000  -0.4125   0.01260   0.00694  -0.1205   0.9428   0.0699
 -10.750  -0.3759   0.01223   0.00661  -0.1219   0.9401   0.0838
 -10.500  -0.3474   0.01204   0.00642  -0.1216   0.9332   0.0928
 -10.000  -0.2782   0.01158   0.00586  -0.1234   0.9227   0.1047
  -9.750  -0.2519   0.01137   0.00559  -0.1226   0.9132   0.1085
  -9.500  -0.2184   0.01104   0.00524  -0.1234   0.9065   0.1133
  -9.250  -0.1922   0.01088   0.00502  -0.1226   0.8955   0.1170
  -9.000  -0.1623   0.01070   0.00475  -0.1226   0.8858   0.1202
  -8.750  -0.1352   0.01040   0.00444  -0.1221   0.8741   0.1244
  -8.500  -0.1085   0.01022   0.00421  -0.1214   0.8613   0.1279
  -8.250  -0.0812   0.01007   0.00398  -0.1208   0.8475   0.1310
  -8.000  -0.0545   0.00990   0.00374  -0.1202   0.8323   0.1351
  -7.750  -0.0283   0.00977   0.00358  -0.1194   0.8153   0.1406
  -7.500  -0.0021   0.00970   0.00342  -0.1186   0.7964   0.1455
  -7.250   0.0235   0.00961   0.00329  -0.1178   0.7766   0.1514
  -7.000   0.0495   0.00961   0.00320  -0.1170   0.7574   0.1580
  -6.750   0.0754   0.00961   0.00314  -0.1162   0.7398   0.1650
  -6.500   0.1018   0.00967   0.00311  -0.1155   0.7243   0.1730
  -6.250   0.1280   0.00969   0.00308  -0.1148   0.7112   0.1807
  -6.000   0.1549   0.00980   0.00310  -0.1142   0.6991   0.1887
  -5.750   0.1814   0.00980   0.00306  -0.1136   0.6886   0.1955
  -5.250   0.2352   0.01000   0.00309  -0.1125   0.6684   0.2066
  -5.000   0.2612   0.00994   0.00300  -0.1119   0.6600   0.2124
  -4.750   0.2884   0.00994   0.00300  -0.1115   0.6528   0.2170
  -4.500   0.3154   0.00999   0.00299  -0.1111   0.6460   0.2210
  -4.250   0.3429   0.01007   0.00299  -0.1107   0.6398   0.2238
  -4.000   0.3693   0.00993   0.00289  -0.1102   0.6335   0.2282
  -3.750   0.3962   0.00993   0.00286  -0.1098   0.6274   0.2318
  -3.500   0.4233   0.00995   0.00286  -0.1095   0.6217   0.2351
  -3.250   0.4504   0.00994   0.00285  -0.1091   0.6160   0.2381
  -3.000   0.4774   0.00998   0.00285  -0.1087   0.6101   0.2407
  -2.750   0.5042   0.00997   0.00283  -0.1083   0.6045   0.2445
  -2.500   0.5307   0.00991   0.00282  -0.1079   0.5987   0.2484
  -2.250   0.5574   0.00992   0.00283  -0.1075   0.5929   0.2523
  -2.000   0.5843   0.00998   0.00285  -0.1072   0.5873   0.2559
  -1.750   0.6109   0.00996   0.00286  -0.1067   0.5812   0.2590
  -1.500   0.6372   0.00993   0.00286  -0.1063   0.5752   0.2632
  -1.250   0.6636   0.00997   0.00290  -0.1059   0.5693   0.2677
  -1.000   0.6897   0.00994   0.00293  -0.1054   0.5627   0.2729
  -0.750   0.7157   0.00995   0.00296  -0.1049   0.5559   0.2799
  -0.500   0.7416   0.00996   0.00303  -0.1045   0.5495   0.2913
  -0.250   0.7673   0.00993   0.00310  -0.1040   0.5422   0.3089
   0.000   0.7925   0.00997   0.00319  -0.1034   0.5349   0.3370
   0.250   0.8180   0.00994   0.00329  -0.1029   0.5265   0.3702
   0.500   0.8423   0.01000   0.00335  -0.1021   0.5172   0.3970
   0.750   0.8672   0.00998   0.00342  -0.1015   0.5067   0.4200
   1.000   0.8909   0.00999   0.00350  -0.1007   0.4960   0.4445
   1.250   0.9135   0.00997   0.00359  -0.0997   0.4840   0.4877
   1.500   0.9737   0.00923   0.00391  -0.1071   0.4667   1.0000
   1.750   0.9972   0.00940   0.00403  -0.1062   0.4533   1.0000
   2.000   1.0204   0.00959   0.00417  -0.1053   0.4403   1.0000
   2.250   1.0428   0.00981   0.00433  -0.1043   0.4270   1.0000
   2.500   1.0644   0.01007   0.00450  -0.1032   0.4110   1.0000
   2.750   1.0856   0.01034   0.00470  -0.1020   0.3950   1.0000
   3.000   1.1066   0.01063   0.00491  -0.1008   0.3804   1.0000
   3.250   1.1281   0.01091   0.00513  -0.0997   0.3677   1.0000
   3.500   1.1499   0.01117   0.00536  -0.0987   0.3562   1.0000
   3.750   1.1706   0.01147   0.00561  -0.0975   0.3450   1.0000
   4.000   1.1908   0.01178   0.00587  -0.0963   0.3334   1.0000
   4.250   1.2114   0.01207   0.00613  -0.0951   0.3212   1.0000
   4.500   1.2312   0.01238   0.00641  -0.0938   0.3108   1.0000
   4.750   1.2500   0.01271   0.00670  -0.0923   0.3007   1.0000
   5.000   1.2690   0.01299   0.00698  -0.0909   0.2912   1.0000
   5.250   1.2854   0.01335   0.00730  -0.0890   0.2807   1.0000
   5.500   1.3027   0.01368   0.00762  -0.0873   0.2689   1.0000
   5.750   1.3194   0.01406   0.00797  -0.0856   0.2560   1.0000
   6.000   1.3343   0.01452   0.00837  -0.0836   0.2397   1.0000
   6.250   1.3463   0.01512   0.00887  -0.0812   0.2190   1.0000
   6.500   1.3550   0.01591   0.00950  -0.0784   0.1892   1.0000
   6.750   1.3532   0.01727   0.01055  -0.0743   0.1405   1.0000
   7.000   1.3502   0.01879   0.01182  -0.0703   0.1054   1.0000
   7.250   1.3539   0.02003   0.01295  -0.0674   0.0862   1.0000
   7.500   1.3616   0.02109   0.01396  -0.0651   0.0772   1.0000
   7.750   1.3698   0.02217   0.01503  -0.0631   0.0720   1.0000
   8.000   1.3797   0.02319   0.01608  -0.0614   0.0689   1.0000
   8.250   1.3873   0.02440   0.01730  -0.0597   0.0663   1.0000
   8.500   1.3930   0.02580   0.01873  -0.0579   0.0637   1.0000
   8.750   1.4029   0.02697   0.01997  -0.0566   0.0621   1.0000
   9.000   1.4110   0.02831   0.02137  -0.0554   0.0604   1.0000
   9.250   1.4168   0.02991   0.02301  -0.0541   0.0589   1.0000
   9.500   1.4194   0.03183   0.02499  -0.0528   0.0573   1.0000
   9.750   1.4182   0.03419   0.02741  -0.0515   0.0559   1.0000
  10.000   1.4244   0.03598   0.02928  -0.0508   0.0550   1.0000
  10.250   1.4315   0.03775   0.03113  -0.0502   0.0539   1.0000
  10.500   1.4359   0.03981   0.03326  -0.0496   0.0529   1.0000
  10.750   1.4396   0.04202   0.03554  -0.0492   0.0518   1.0000
  11.000   1.4414   0.04445   0.03805  -0.0488   0.0509   1.0000
  11.250   1.4402   0.04725   0.04089  -0.0484   0.0498   1.0000
  11.500   1.4354   0.05045   0.04415  -0.0480   0.0489   1.0000
  11.750   1.4353   0.05320   0.04697  -0.0477   0.0479   1.0000
  12.000   1.4397   0.05554   0.04941  -0.0477   0.0472   1.0000
  12.250   1.4431   0.05803   0.05198  -0.0477   0.0462   1.0000
  12.500   1.4450   0.06072   0.05474  -0.0478   0.0452   1.0000
  12.750   1.4461   0.06352   0.05761  -0.0479   0.0444   1.0000
  13.000   1.4459   0.06651   0.06064  -0.0482   0.0434   1.0000
  13.250   1.4426   0.06983   0.06400  -0.0483   0.0426   1.0000
  13.500   1.4390   0.07314   0.06736  -0.0483   0.0416   1.0000
  13.750   1.4421   0.07600   0.07034  -0.0489   0.0407   1.0000
  14.000   1.4430   0.07904   0.07347  -0.0494   0.0399   1.0000
  14.250   1.4439   0.08215   0.07666  -0.0501   0.0389   1.0000
  14.500   1.4436   0.08542   0.07999  -0.0507   0.0380   1.0000
  14.750   1.4423   0.08886   0.08348  -0.0515   0.0372   1.0000
  15.000   1.4391   0.09235   0.08697  -0.0520   0.0363   1.0000
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