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Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il)
Reynolds number: 500,000
Max Cl/Cd: 93.49 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eiffel385-il-500000-n5.txt
Download as CSV file: xf-eiffel385-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.7628   0.08803   0.08445  -0.0704   1.0000   0.0290
 -18.500  -0.7686   0.08396   0.08035  -0.0725   1.0000   0.0293
 -18.250  -0.7761   0.07970   0.07604  -0.0747   1.0000   0.0296
 -18.000  -0.7841   0.07557   0.07187  -0.0768   1.0000   0.0298
 -17.750  -0.7924   0.07156   0.06782  -0.0787   1.0000   0.0300
 -17.500  -0.8045   0.06720   0.06341  -0.0810   1.0000   0.0302
 -17.250  -0.8179   0.06305   0.05921  -0.0829   1.0000   0.0303
 -17.000  -0.8367   0.05849   0.05460  -0.0851   1.0000   0.0304
 -16.750  -0.8614   0.05364   0.04971  -0.0871   1.0000   0.0305
 -16.500  -0.8987   0.04835   0.04438  -0.0886   1.0000   0.0305
 -16.250  -0.9486   0.03945   0.03536  -0.0965   0.9964   0.0303
 -16.000  -0.9389   0.03067   0.02626  -0.1100   0.9899   0.0306
 -15.750  -0.9161   0.02791   0.02332  -0.1136   0.9857   0.0310
 -15.500  -0.8895   0.02607   0.02133  -0.1162   0.9828   0.0315
 -15.250  -0.8671   0.02466   0.01979  -0.1170   0.9780   0.0319
 -15.000  -0.8414   0.02342   0.01842  -0.1181   0.9739   0.0323
 -14.750  -0.8140   0.02198   0.01691  -0.1196   0.9707   0.0329
 -14.500  -0.7909   0.02089   0.01573  -0.1197   0.9649   0.0333
 -14.250  -0.7640   0.01991   0.01467  -0.1203   0.9602   0.0339
 -14.000  -0.7337   0.01905   0.01373  -0.1213   0.9573   0.0346
 -13.750  -0.7072   0.01832   0.01292  -0.1214   0.9527   0.0353
 -13.500  -0.6793   0.01764   0.01215  -0.1216   0.9478   0.0360
 -13.250  -0.6477   0.01698   0.01140  -0.1225   0.9443   0.0366
 -13.000  -0.6150   0.01638   0.01070  -0.1235   0.9408   0.0372
 -12.750  -0.5886   0.01569   0.00996  -0.1234   0.9339   0.0381
 -12.500  -0.5576   0.01505   0.00926  -0.1241   0.9288   0.0392
 -12.250  -0.5263   0.01451   0.00865  -0.1247   0.9237   0.0403
 -12.000  -0.4980   0.01406   0.00813  -0.1247   0.9163   0.0416
 -11.750  -0.4665   0.01361   0.00760  -0.1252   0.9097   0.0432
 -11.500  -0.4395   0.01314   0.00708  -0.1249   0.9010   0.0456
 -11.250  -0.4103   0.01273   0.00661  -0.1250   0.8926   0.0485
 -11.000  -0.3840   0.01232   0.00616  -0.1245   0.8835   0.0529
 -10.750  -0.3565   0.01191   0.00573  -0.1242   0.8741   0.0602
 -10.500  -0.3306   0.01159   0.00541  -0.1235   0.8631   0.0699
 -10.250  -0.3034   0.01136   0.00516  -0.1231   0.8519   0.0792
 -10.000  -0.2764   0.01118   0.00494  -0.1225   0.8393   0.0853
  -9.750  -0.2496   0.01106   0.00474  -0.1219   0.8261   0.0901
  -9.500  -0.2231   0.01092   0.00452  -0.1212   0.8113   0.0937
  -9.250  -0.1970   0.01078   0.00431  -0.1204   0.7941   0.0974
  -9.000  -0.1710   0.01070   0.00412  -0.1196   0.7757   0.1006
  -8.750  -0.1451   0.01064   0.00394  -0.1188   0.7566   0.1027
  -8.500  -0.1198   0.01057   0.00375  -0.1179   0.7366   0.1047
  -8.250  -0.0949   0.01047   0.00355  -0.1169   0.7176   0.1076
  -8.000  -0.0696   0.01038   0.00338  -0.1161   0.7009   0.1110
  -7.750  -0.0438   0.01032   0.00324  -0.1153   0.6867   0.1142
  -7.500  -0.0177   0.01028   0.00311  -0.1146   0.6746   0.1168
  -7.000   0.0344   0.01008   0.00283  -0.1133   0.6553   0.1252
  -6.750   0.0607   0.01003   0.00273  -0.1126   0.6471   0.1293
  -6.500   0.0874   0.00995   0.00263  -0.1121   0.6400   0.1345
  -6.250   0.1141   0.00987   0.00256  -0.1116   0.6332   0.1426
  -6.000   0.1406   0.00985   0.00254  -0.1110   0.6268   0.1542
  -5.750   0.1680   0.00982   0.00253  -0.1106   0.6206   0.1649
  -5.500   0.1949   0.00984   0.00250  -0.1101   0.6129   0.1726
  -5.250   0.2218   0.00986   0.00250  -0.1096   0.6056   0.1792
  -5.000   0.2491   0.00987   0.00247  -0.1092   0.5986   0.1842
  -4.750   0.2760   0.00988   0.00245  -0.1087   0.5930   0.1881
  -4.500   0.3032   0.00988   0.00244  -0.1083   0.5881   0.1920
  -4.250   0.3307   0.00988   0.00243  -0.1080   0.5830   0.1957
  -4.000   0.3579   0.00990   0.00242  -0.1076   0.5776   0.1989
  -3.500   0.4121   0.00989   0.00239  -0.1068   0.5674   0.2046
  -3.250   0.4391   0.00988   0.00239  -0.1065   0.5621   0.2075
  -3.000   0.4658   0.00990   0.00239  -0.1060   0.5566   0.2105
  -2.750   0.4928   0.00991   0.00240  -0.1057   0.5511   0.2132
  -2.500   0.5199   0.00992   0.00240  -0.1053   0.5452   0.2151
  -2.250   0.5464   0.00995   0.00241  -0.1049   0.5393   0.2168
  -2.000   0.5732   0.00997   0.00243  -0.1045   0.5333   0.2184
  -1.750   0.5997   0.00996   0.00244  -0.1041   0.5261   0.2215
  -1.500   0.6255   0.01000   0.00247  -0.1036   0.5194   0.2246
  -1.250   0.6522   0.01000   0.00251  -0.1032   0.5121   0.2273
  -1.000   0.6779   0.01005   0.00255  -0.1027   0.5037   0.2304
  -0.750   0.7041   0.01010   0.00259  -0.1023   0.4950   0.2337
  -0.500   0.7294   0.01017   0.00265  -0.1017   0.4862   0.2370
  -0.250   0.7552   0.01021   0.00271  -0.1012   0.4771   0.2411
   0.000   0.7799   0.01028   0.00279  -0.1006   0.4667   0.2468
   0.250   0.8043   0.01039   0.00287  -0.0998   0.4534   0.2529
   0.500   0.8279   0.01050   0.00298  -0.0990   0.4375   0.2635
   0.750   0.8514   0.01063   0.00311  -0.0982   0.4222   0.2768
   1.000   0.8747   0.01075   0.00327  -0.0974   0.4083   0.3036
   1.250   0.8981   0.01088   0.00345  -0.0965   0.3960   0.3369
   1.500   0.9210   0.01106   0.00362  -0.0957   0.3838   0.3576
   1.750   0.9439   0.01124   0.00380  -0.0948   0.3700   0.3735
   2.000   0.9658   0.01147   0.00399  -0.0937   0.3543   0.3871
   2.250   0.9882   0.01166   0.00419  -0.0928   0.3426   0.3997
   2.500   1.0100   0.01187   0.00439  -0.0918   0.3317   0.4121
   2.750   1.0315   0.01208   0.00461  -0.0907   0.3199   0.4273
   3.000   1.0528   0.01225   0.00483  -0.0896   0.3092   0.4519
   3.250   1.0658   0.01192   0.00516  -0.0870   0.3001   0.7266
   3.750   1.1509   0.01231   0.00588  -0.0942   0.2722   1.0000
   4.000   1.1709   0.01263   0.00615  -0.0930   0.2601   1.0000
   4.250   1.1896   0.01297   0.00644  -0.0915   0.2479   1.0000
   4.500   1.2065   0.01334   0.00675  -0.0897   0.2348   1.0000
   4.750   1.2235   0.01371   0.00706  -0.0879   0.2213   1.0000
   5.000   1.2378   0.01419   0.00745  -0.0857   0.2035   1.0000
   5.250   1.2510   0.01475   0.00791  -0.0834   0.1815   1.0000
   5.500   1.2577   0.01563   0.00858  -0.0802   0.1468   1.0000
   5.750   1.2632   0.01661   0.00937  -0.0769   0.1164   1.0000
   6.000   1.2721   0.01746   0.01011  -0.0743   0.0965   1.0000
   6.250   1.2811   0.01834   0.01090  -0.0718   0.0785   1.0000
   6.500   1.2910   0.01919   0.01168  -0.0696   0.0674   1.0000
   6.750   1.3031   0.01996   0.01243  -0.0678   0.0623   1.0000
   7.000   1.3168   0.02065   0.01314  -0.0662   0.0600   1.0000
   7.250   1.3299   0.02140   0.01392  -0.0647   0.0581   1.0000
   7.500   1.3418   0.02225   0.01480  -0.0631   0.0562   1.0000
   7.750   1.3527   0.02321   0.01578  -0.0616   0.0544   1.0000
   8.000   1.3647   0.02413   0.01675  -0.0602   0.0532   1.0000
   8.250   1.3768   0.02507   0.01775  -0.0590   0.0524   1.0000
   8.500   1.3883   0.02609   0.01883  -0.0578   0.0516   1.0000
   8.750   1.3986   0.02724   0.02004  -0.0566   0.0506   1.0000
   9.000   1.4079   0.02850   0.02135  -0.0555   0.0495   1.0000
   9.250   1.4153   0.02996   0.02285  -0.0544   0.0480   1.0000
   9.500   1.4204   0.03169   0.02462  -0.0533   0.0467   1.0000
   9.750   1.4275   0.03331   0.02629  -0.0524   0.0458   1.0000
  10.000   1.4368   0.03479   0.02785  -0.0518   0.0450   1.0000
  10.250   1.4449   0.03641   0.02955  -0.0512   0.0441   1.0000
  10.500   1.4523   0.03815   0.03136  -0.0507   0.0433   1.0000
  10.750   1.4580   0.04011   0.03338  -0.0503   0.0425   1.0000
  11.000   1.4628   0.04220   0.03554  -0.0499   0.0417   1.0000
  11.250   1.4661   0.04452   0.03792  -0.0496   0.0410   1.0000
  11.500   1.4680   0.04701   0.04047  -0.0493   0.0403   1.0000
  11.750   1.4672   0.04984   0.04337  -0.0491   0.0396   1.0000
  12.000   1.4720   0.05210   0.04571  -0.0491   0.0390   1.0000
  12.250   1.4755   0.05453   0.04823  -0.0490   0.0384   1.0000
  12.500   1.4784   0.05705   0.05083  -0.0491   0.0376   1.0000
  12.750   1.4806   0.05970   0.05356  -0.0492   0.0369   1.0000
  13.000   1.4820   0.06247   0.05640  -0.0494   0.0362   1.0000
  13.250   1.4822   0.06543   0.05943  -0.0496   0.0354   1.0000
  13.500   1.4812   0.06858   0.06265  -0.0499   0.0347   1.0000
  13.750   1.4781   0.07205   0.06618  -0.0504   0.0341   1.0000
  14.000   1.4766   0.07537   0.06958  -0.0508   0.0335   1.0000
  14.250   1.4766   0.07853   0.07284  -0.0513   0.0329   1.0000
  14.500   1.4765   0.08172   0.07612  -0.0519   0.0319   1.0000
  14.750   1.4740   0.08528   0.07976  -0.0526   0.0313   1.0000
  15.000   1.4724   0.08876   0.08331  -0.0534   0.0304   1.0000
  15.250   1.4692   0.09250   0.08712  -0.0542   0.0296   1.0000
  15.500   1.4646   0.09649   0.09116  -0.0552   0.0289   1.0000
  15.750   1.4616   0.10023   0.09500  -0.0562   0.0283   1.0000
  16.000   1.4598   0.10383   0.09869  -0.0572   0.0273   1.0000
  16.250   1.4564   0.10771   0.10265  -0.0584   0.0266   1.0000
  16.500   1.4524   0.11175   0.10676  -0.0597   0.0258   1.0000
  16.750   1.4478   0.11588   0.11095  -0.0611   0.0250   1.0000
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