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Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.94 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eiffel385-il-1000000-n5.txt
Download as CSV file: xf-eiffel385-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.8229   0.08379   0.08083  -0.0732   1.0000   0.0247
 -18.750  -0.8353   0.07892   0.07591  -0.0759   1.0000   0.0249
 -18.500  -0.8459   0.07449   0.07145  -0.0782   1.0000   0.0251
 -18.250  -0.8633   0.06929   0.06620  -0.0812   1.0000   0.0252
 -18.000  -0.8846   0.06400   0.06086  -0.0842   1.0000   0.0253
 -17.750  -0.9230   0.05718   0.05397  -0.0882   1.0000   0.0253
 -17.250  -1.0610   0.02593   0.02200  -0.1218   0.9893   0.0248
 -17.000  -1.0381   0.02411   0.02008  -0.1236   0.9861   0.0252
 -16.750  -1.0124   0.02276   0.01865  -0.1250   0.9839   0.0256
 -16.500  -0.9852   0.02160   0.01739  -0.1262   0.9822   0.0259
 -16.250  -0.9639   0.02071   0.01643  -0.1257   0.9774   0.0262
 -16.000  -0.9375   0.01985   0.01549  -0.1261   0.9738   0.0266
 -15.500  -0.8818   0.01833   0.01382  -0.1270   0.9676   0.0273
 -15.250  -0.8556   0.01767   0.01309  -0.1270   0.9624   0.0275
 -15.000  -0.8237   0.01708   0.01243  -0.1279   0.9592   0.0277
 -14.750  -0.7908   0.01619   0.01146  -0.1294   0.9562   0.0284
 -14.500  -0.7624   0.01552   0.01073  -0.1298   0.9491   0.0288
 -14.250  -0.7297   0.01490   0.01005  -0.1308   0.9436   0.0293
 -14.000  -0.6988   0.01437   0.00946  -0.1314   0.9368   0.0298
 -13.750  -0.6687   0.01390   0.00892  -0.1318   0.9291   0.0303
 -13.500  -0.6397   0.01349   0.00844  -0.1319   0.9216   0.0308
 -13.250  -0.6121   0.01312   0.00800  -0.1316   0.9129   0.0313
 -13.000  -0.5850   0.01278   0.00758  -0.1312   0.9046   0.0317
 -12.750  -0.5587   0.01247   0.00719  -0.1307   0.8949   0.0320
 -12.500  -0.5330   0.01214   0.00679  -0.1300   0.8857   0.0326
 -12.250  -0.5077   0.01180   0.00638  -0.1292   0.8756   0.0333
 -12.000  -0.4823   0.01149   0.00602  -0.1284   0.8665   0.0341
 -11.750  -0.4569   0.01123   0.00568  -0.1276   0.8560   0.0350
 -11.500  -0.4313   0.01098   0.00537  -0.1268   0.8446   0.0359
 -11.250  -0.4058   0.01077   0.00509  -0.1260   0.8322   0.0368
 -11.000  -0.3807   0.01054   0.00478  -0.1251   0.8181   0.0384
 -10.500  -0.3310   0.01012   0.00422  -0.1232   0.7847   0.0432
 -10.250  -0.3067   0.00990   0.00393  -0.1221   0.7636   0.0477
 -10.000  -0.2829   0.00969   0.00365  -0.1210   0.7396   0.0550
  -9.750  -0.2593   0.00946   0.00339  -0.1199   0.7166   0.0667
  -9.500  -0.2346   0.00933   0.00322  -0.1189   0.6955   0.0770
  -9.250  -0.2091   0.00926   0.00309  -0.1181   0.6779   0.0828
  -8.750  -0.1563   0.00914   0.00286  -0.1167   0.6528   0.0904
  -8.500  -0.1296   0.00910   0.00276  -0.1161   0.6433   0.0924
  -8.250  -0.1027   0.00900   0.00264  -0.1155   0.6354   0.0956
  -8.000  -0.0760   0.00893   0.00253  -0.1149   0.6281   0.0982
  -7.750  -0.0486   0.00886   0.00244  -0.1145   0.6225   0.1005
  -7.500  -0.0212   0.00882   0.00235  -0.1140   0.6164   0.1025
  -7.250   0.0060   0.00880   0.00228  -0.1135   0.6107   0.1036
  -7.000   0.0333   0.00870   0.00217  -0.1130   0.6059   0.1069
  -6.750   0.0607   0.00861   0.00208  -0.1126   0.6010   0.1095
  -6.500   0.0877   0.00855   0.00199  -0.1121   0.5948   0.1121
  -6.250   0.1148   0.00851   0.00192  -0.1116   0.5880   0.1147
  -6.000   0.1422   0.00847   0.00185  -0.1112   0.5809   0.1165
  -5.750   0.1692   0.00841   0.00178  -0.1107   0.5752   0.1213
  -5.500   0.1964   0.00833   0.00172  -0.1103   0.5708   0.1272
  -5.250   0.2239   0.00825   0.00166  -0.1100   0.5664   0.1356
  -5.000   0.2510   0.00816   0.00163  -0.1096   0.5616   0.1521
  -4.750   0.2782   0.00814   0.00164  -0.1092   0.5566   0.1665
  -4.500   0.3058   0.00813   0.00163  -0.1089   0.5522   0.1728
  -4.250   0.3335   0.00811   0.00163  -0.1086   0.5474   0.1785
  -4.000   0.3611   0.00812   0.00163  -0.1082   0.5422   0.1824
  -3.750   0.3882   0.00816   0.00163  -0.1078   0.5365   0.1847
  -3.500   0.4160   0.00815   0.00162  -0.1076   0.5314   0.1875
  -3.250   0.4434   0.00815   0.00163  -0.1073   0.5256   0.1907
  -3.000   0.4702   0.00818   0.00164  -0.1069   0.5194   0.1941
  -2.750   0.4978   0.00819   0.00166  -0.1066   0.5129   0.1967
  -2.500   0.5247   0.00823   0.00167  -0.1062   0.5054   0.1983
  -2.250   0.5518   0.00826   0.00169  -0.1059   0.4986   0.1995
  -2.000   0.5787   0.00831   0.00171  -0.1055   0.4898   0.2005
  -1.750   0.6052   0.00836   0.00173  -0.1051   0.4810   0.2018
  -1.500   0.6316   0.00841   0.00176  -0.1047   0.4715   0.2042
  -1.250   0.6580   0.00845   0.00180  -0.1043   0.4630   0.2070
  -0.750   0.7099   0.00862   0.00191  -0.1034   0.4404   0.2108
  -0.500   0.7348   0.00876   0.00199  -0.1027   0.4228   0.2126
  -0.250   0.7592   0.00893   0.00209  -0.1020   0.4042   0.2145
   0.000   0.7844   0.00907   0.00218  -0.1014   0.3903   0.2164
   0.500   0.8341   0.00934   0.00239  -0.1003   0.3660   0.2219
   0.750   0.8585   0.00950   0.00251  -0.0996   0.3524   0.2257
   1.000   0.8828   0.00965   0.00263  -0.0989   0.3393   0.2303
   1.250   0.9072   0.00980   0.00276  -0.0983   0.3279   0.2351
   1.500   0.9305   0.00999   0.00291  -0.0975   0.3138   0.2417
   1.750   0.9539   0.01018   0.00307  -0.0967   0.3015   0.2505
   2.000   0.9779   0.01029   0.00322  -0.0960   0.2920   0.2678
   2.250   1.0007   0.01041   0.00340  -0.0952   0.2828   0.3097
   2.500   1.0239   0.01055   0.00359  -0.0944   0.2724   0.3411
   2.750   1.0466   0.01074   0.00378  -0.0936   0.2616   0.3582
   3.000   1.0687   0.01095   0.00397  -0.0926   0.2510   0.3718
   3.250   1.0911   0.01114   0.00416  -0.0917   0.2405   0.3844
   3.500   1.1123   0.01137   0.00438  -0.0906   0.2287   0.3949
   3.750   1.1321   0.01166   0.00462  -0.0893   0.2139   0.4044
   4.000   1.1481   0.01204   0.00492  -0.0873   0.1922   0.4156
   4.250   1.1610   0.01245   0.00525  -0.0847   0.1694   0.4335
   4.500   1.1683   0.01307   0.00576  -0.0811   0.1355   0.4663
   4.750   1.1642   0.01291   0.00637  -0.0752   0.1121   0.8604
   5.250   1.2452   0.01461   0.00791  -0.0831   0.0594   1.0000
   5.500   1.2623   0.01502   0.00830  -0.0815   0.0560   1.0000
   5.750   1.2800   0.01541   0.00869  -0.0801   0.0534   1.0000
   6.000   1.2982   0.01579   0.00908  -0.0788   0.0522   1.0000
   6.250   1.3163   0.01618   0.00949  -0.0775   0.0511   1.0000
   6.500   1.3332   0.01664   0.00996  -0.0761   0.0496   1.0000
   6.750   1.3498   0.01713   0.01046  -0.0747   0.0484   1.0000
   7.000   1.3658   0.01767   0.01101  -0.0733   0.0472   1.0000
   7.250   1.3814   0.01824   0.01160  -0.0720   0.0461   1.0000
   7.500   1.3985   0.01874   0.01213  -0.0709   0.0456   1.0000
   7.750   1.4150   0.01928   0.01271  -0.0697   0.0448   1.0000
   8.000   1.4310   0.01987   0.01332  -0.0686   0.0437   1.0000
   8.250   1.4456   0.02056   0.01403  -0.0674   0.0425   1.0000
   8.500   1.4592   0.02132   0.01481  -0.0662   0.0413   1.0000
   8.750   1.4719   0.02218   0.01569  -0.0649   0.0401   1.0000
   9.000   1.4841   0.02309   0.01663  -0.0636   0.0394   1.0000
   9.250   1.4985   0.02388   0.01747  -0.0627   0.0389   1.0000
   9.500   1.5118   0.02477   0.01840  -0.0617   0.0384   1.0000
   9.750   1.5244   0.02573   0.01941  -0.0608   0.0378   1.0000
  10.000   1.5361   0.02679   0.02050  -0.0599   0.0370   1.0000
  10.250   1.5469   0.02795   0.02170  -0.0590   0.0361   1.0000
  10.500   1.5568   0.02923   0.02301  -0.0581   0.0353   1.0000
  10.750   1.5654   0.03065   0.02447  -0.0573   0.0345   1.0000
  11.000   1.5731   0.03218   0.02604  -0.0565   0.0337   1.0000
  11.250   1.5829   0.03359   0.02751  -0.0559   0.0331   1.0000
  11.500   1.5915   0.03515   0.02912  -0.0554   0.0324   1.0000
  11.750   1.5990   0.03683   0.03086  -0.0549   0.0316   1.0000
  12.000   1.6055   0.03867   0.03274  -0.0545   0.0307   1.0000
  12.250   1.6108   0.04067   0.03479  -0.0541   0.0299   1.0000
  12.500   1.6149   0.04285   0.03701  -0.0538   0.0291   1.0000
  12.750   1.6194   0.04501   0.03924  -0.0536   0.0285   1.0000
  13.000   1.6235   0.04725   0.04154  -0.0534   0.0275   1.0000
  13.250   1.6262   0.04967   0.04403  -0.0533   0.0269   1.0000
  13.500   1.6282   0.05221   0.04662  -0.0533   0.0258   1.0000
  13.750   1.6281   0.05499   0.04943  -0.0532   0.0245   1.0000
  14.000   1.6284   0.05776   0.05227  -0.0533   0.0238   1.0000
  14.250   1.6272   0.06077   0.05534  -0.0534   0.0225   1.0000
  14.500   1.6250   0.06395   0.05858  -0.0536   0.0218   1.0000
  14.750   1.6213   0.06734   0.06202  -0.0539   0.0208   1.0000
  15.000   1.6180   0.07073   0.06548  -0.0542   0.0198   1.0000
  15.250   1.6128   0.07441   0.06922  -0.0547   0.0188   1.0000
  15.500   1.6068   0.07828   0.07316  -0.0552   0.0181   1.0000
  15.750   1.6005   0.08223   0.07718  -0.0559   0.0175   1.0000
  16.000   1.5933   0.08634   0.08137  -0.0566   0.0167   1.0000
  16.250   1.5861   0.09050   0.08561  -0.0575   0.0162   1.0000
  16.500   1.5783   0.09482   0.09000  -0.0585   0.0157   1.0000
  16.750   1.5692   0.09930   0.09456  -0.0595   0.0151   1.0000
  17.000   1.5605   0.10378   0.09911  -0.0606   0.0147   1.0000
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