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EPPLER 603 AIRFOIL (e603-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 603 AIRFOIL (e603-il)
Reynolds number: 500,000
Max Cl/Cd: 103.17 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e603-il-500000-n5.txt
Download as CSV file: xf-e603-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 603 AIRFOIL                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.5752   0.10955   0.10668  -0.0639   1.0000   0.0078
 -16.750  -0.6272   0.09473   0.09164  -0.0716   1.0000   0.0077
 -16.500  -0.6532   0.08558   0.08234  -0.0767   1.0000   0.0077
 -16.250  -0.6798   0.07533   0.07188  -0.0834   0.9896   0.0077
 -16.000  -0.6797   0.06639   0.06267  -0.0942   0.9515   0.0077
 -15.750  -0.6638   0.05723   0.05313  -0.1088   0.9153   0.0077
 -15.500  -0.6474   0.05168   0.04697  -0.1177   0.8396   0.0078
 -15.250  -0.6561   0.04843   0.04342  -0.1180   0.8052   0.0078
 -15.000  -0.6606   0.04569   0.04044  -0.1180   0.7845   0.0079
 -14.750  -0.6629   0.04323   0.03776  -0.1179   0.7691   0.0079
 -14.250  -0.6643   0.03886   0.03307  -0.1170   0.7463   0.0080
 -14.000  -0.6645   0.03687   0.03093  -0.1163   0.7375   0.0082
 -13.750  -0.6613   0.03518   0.02911  -0.1155   0.7296   0.0082
 -13.500  -0.6576   0.03359   0.02739  -0.1146   0.7223   0.0083
 -13.250  -0.6505   0.03229   0.02599  -0.1137   0.7160   0.0084
 -13.000  -0.6428   0.03104   0.02464  -0.1128   0.7096   0.0085
 -12.500  -0.6241   0.02885   0.02225  -0.1108   0.6987   0.0088
 -12.250  -0.6134   0.02784   0.02115  -0.1098   0.6935   0.0089
 -12.000  -0.6020   0.02690   0.02011  -0.1088   0.6889   0.0091
 -11.750  -0.5901   0.02600   0.01912  -0.1077   0.6851   0.0092
 -11.500  -0.5772   0.02514   0.01818  -0.1067   0.6814   0.0094
 -11.250  -0.5632   0.02436   0.01732  -0.1057   0.6777   0.0097
 -11.000  -0.5499   0.02356   0.01642  -0.1045   0.6742   0.0098
 -10.750  -0.5362   0.02280   0.01557  -0.1034   0.6710   0.0100
 -10.500  -0.5204   0.02218   0.01487  -0.1024   0.6681   0.0102
 -10.250  -0.5044   0.02154   0.01417  -0.1014   0.6653   0.0103
 -10.000  -0.4907   0.02078   0.01339  -0.1002   0.6624   0.0108
  -9.750  -0.4745   0.02019   0.01275  -0.0991   0.6594   0.0111
  -9.500  -0.4574   0.01968   0.01218  -0.0982   0.6566   0.0115
  -9.250  -0.4402   0.01919   0.01163  -0.0971   0.6539   0.0119
  -9.000  -0.4226   0.01871   0.01108  -0.0961   0.6516   0.0126
  -8.750  -0.4054   0.01819   0.01053  -0.0950   0.6495   0.0129
  -8.500  -0.3885   0.01766   0.00998  -0.0939   0.6474   0.0134
  -8.250  -0.3710   0.01720   0.00950  -0.0928   0.6452   0.0140
  -8.000  -0.3532   0.01677   0.00903  -0.0917   0.6431   0.0147
  -7.750  -0.3353   0.01637   0.00858  -0.0905   0.6410   0.0158
  -7.500  -0.3185   0.01596   0.00815  -0.0892   0.6391   0.0166
  -7.250  -0.3023   0.01561   0.00777  -0.0877   0.6372   0.0179
  -6.750  -0.2703   0.01499   0.00710  -0.0846   0.6336   0.0218
  -6.500  -0.2509   0.01466   0.00677  -0.0837   0.6317   0.0246
  -6.250  -0.2303   0.01436   0.00647  -0.0829   0.6298   0.0280
  -6.000  -0.2093   0.01406   0.00618  -0.0822   0.6281   0.0327
  -5.750  -0.1877   0.01377   0.00590  -0.0816   0.6263   0.0385
  -5.500  -0.1655   0.01350   0.00564  -0.0810   0.6247   0.0465
  -5.250  -0.1432   0.01320   0.00540  -0.0805   0.6231   0.0587
  -5.000  -0.1203   0.01292   0.00516  -0.0801   0.6215   0.0739
  -4.750  -0.0975   0.01261   0.00492  -0.0797   0.6198   0.0952
  -4.500  -0.0746   0.01227   0.00469  -0.0794   0.6181   0.1258
  -4.250  -0.0513   0.01187   0.00446  -0.0792   0.6166   0.1651
  -4.000  -0.0277   0.01143   0.00422  -0.0792   0.6152   0.2158
  -3.750  -0.0038   0.01091   0.00395  -0.0793   0.6137   0.2824
  -3.500   0.0198   0.01011   0.00358  -0.0797   0.6120   0.3908
  -3.250   0.0446   0.00899   0.00323  -0.0805   0.6103   0.5806
  -3.000   0.0731   0.00901   0.00340  -0.0807   0.6085   0.6347
  -2.750   0.1026   0.00910   0.00346  -0.0811   0.6070   0.6524
  -2.500   0.1323   0.00917   0.00347  -0.0816   0.6055   0.6641
  -2.250   0.1619   0.00928   0.00352  -0.0821   0.6039   0.6747
  -2.000   0.1912   0.00945   0.00365  -0.0824   0.6023   0.6843
  -1.750   0.2209   0.00965   0.00380  -0.0828   0.6008   0.6957
  -1.500   0.2490   0.00992   0.00411  -0.0826   0.5994   0.7041
  -1.250   0.2791   0.01004   0.00416  -0.0833   0.5977   0.7106
  -1.000   0.3080   0.01006   0.00417  -0.0836   0.5959   0.7121
  -0.750   0.3371   0.01007   0.00417  -0.0841   0.5942   0.7133
  -0.500   0.3662   0.01010   0.00417  -0.0845   0.5925   0.7144
  -0.250   0.3954   0.01012   0.00416  -0.0850   0.5907   0.7155
   0.000   0.4246   0.01014   0.00415  -0.0855   0.5890   0.7166
   0.250   0.4539   0.01018   0.00416  -0.0860   0.5873   0.7178
   0.500   0.4833   0.01024   0.00417  -0.0865   0.5856   0.7192
   0.750   0.5125   0.01026   0.00419  -0.0870   0.5840   0.7204
   1.000   0.5416   0.01027   0.00420  -0.0876   0.5821   0.7216
   1.250   0.5708   0.01029   0.00422  -0.0881   0.5801   0.7228
   1.500   0.5999   0.01031   0.00424  -0.0886   0.5780   0.7242
   1.750   0.6291   0.01034   0.00426  -0.0892   0.5759   0.7255
   2.000   0.6583   0.01037   0.00426  -0.0897   0.5738   0.7267
   2.250   0.6875   0.01040   0.00427  -0.0903   0.5717   0.7276
   2.500   0.7163   0.01045   0.00430  -0.0908   0.5696   0.7285
   2.750   0.7447   0.01048   0.00436  -0.0911   0.5675   0.7293
   3.000   0.7728   0.01051   0.00444  -0.0915   0.5648   0.7302
   3.250   0.8008   0.01054   0.00451  -0.0918   0.5620   0.7312
   3.500   0.8288   0.01058   0.00457  -0.0920   0.5592   0.7322
   3.750   0.8568   0.01063   0.00463  -0.0923   0.5564   0.7332
   4.000   0.8849   0.01068   0.00467  -0.0927   0.5536   0.7342
   4.250   0.9124   0.01073   0.00477  -0.0929   0.5502   0.7351
   4.500   0.9398   0.01076   0.00485  -0.0931   0.5458   0.7361
   4.750   0.9669   0.01080   0.00491  -0.0933   0.5414   0.7372
   5.000   0.9938   0.01086   0.00495  -0.0934   0.5374   0.7383
   5.250   1.0208   0.01091   0.00508  -0.0935   0.5323   0.7395
   5.500   1.0473   0.01097   0.00516  -0.0936   0.5269   0.7408
   5.750   1.0732   0.01105   0.00524  -0.0935   0.5216   0.7419
   6.000   1.0994   0.01112   0.00536  -0.0936   0.5151   0.7429
   6.250   1.1242   0.01122   0.00546  -0.0933   0.5080   0.7439
   6.500   1.1493   0.01132   0.00560  -0.0931   0.4999   0.7448
   6.750   1.1719   0.01145   0.00573  -0.0925   0.4910   0.7457
   7.000   1.1947   0.01159   0.00590  -0.0919   0.4805   0.7466
   7.250   1.2153   0.01178   0.00609  -0.0909   0.4689   0.7476
   7.500   1.2335   0.01203   0.00633  -0.0894   0.4558   0.7487
   7.750   1.2481   0.01234   0.00661  -0.0873   0.4411   0.7500
   8.000   1.2588   0.01269   0.00693  -0.0845   0.4254   0.7513
   8.250   1.2686   0.01316   0.00736  -0.0817   0.4090   0.7526
   8.500   1.2775   0.01371   0.00787  -0.0789   0.3924   0.7539
   8.750   1.2840   0.01437   0.00849  -0.0758   0.3745   0.7553
   9.000   1.2890   0.01514   0.00921  -0.0727   0.3571   0.7566
   9.250   1.2912   0.01608   0.01010  -0.0694   0.3390   0.7580
   9.500   1.2916   0.01722   0.01118  -0.0661   0.3214   0.7594
  10.250   1.2892   0.02168   0.01551  -0.0579   0.2703   0.7634
  10.500   1.2882   0.02343   0.01724  -0.0556   0.2545   0.7648
  10.750   1.2886   0.02520   0.01898  -0.0537   0.2404   0.7662
  11.000   1.2880   0.02711   0.02086  -0.0518   0.2256   0.7675
  11.250   1.2909   0.02884   0.02258  -0.0504   0.2135   0.7687
  11.500   1.2935   0.03063   0.02437  -0.0490   0.2015   0.7700
  11.750   1.2944   0.03259   0.02630  -0.0476   0.1882   0.7713
  12.000   1.2968   0.03451   0.02820  -0.0464   0.1771   0.7726
  12.250   1.2966   0.03668   0.03032  -0.0451   0.1626   0.7739
  12.500   1.2982   0.03876   0.03236  -0.0441   0.1500   0.7752
  12.750   1.2994   0.04097   0.03453  -0.0431   0.1372   0.7764
  13.000   1.3013   0.04316   0.03668  -0.0423   0.1251   0.7776
  13.250   1.3054   0.04523   0.03873  -0.0417   0.1144   0.7787
  13.500   1.3092   0.04735   0.04083  -0.0411   0.1046   0.7799
  13.750   1.3139   0.04944   0.04294  -0.0407   0.0973   0.7811
  14.000   1.3193   0.05150   0.04501  -0.0403   0.0897   0.7824
  14.250   1.3242   0.05365   0.04719  -0.0400   0.0833   0.7839
  14.500   1.3284   0.05592   0.04946  -0.0397   0.0761   0.7854
  14.750   1.3341   0.05810   0.05168  -0.0395   0.0706   0.7870
  15.000   1.3383   0.06047   0.05405  -0.0394   0.0649   0.7885
  15.250   1.3439   0.06273   0.05636  -0.0394   0.0600   0.7899
  15.500   1.3478   0.06524   0.05887  -0.0394   0.0552   0.7913
  15.750   1.3530   0.06764   0.06132  -0.0396   0.0508   0.7928
  16.000   1.3564   0.07029   0.06399  -0.0398   0.0469   0.7941
  16.500   1.3633   0.07569   0.06948  -0.0403   0.0392   0.7968
  16.750   1.3672   0.07840   0.07224  -0.0407   0.0357   0.7982
  17.000   1.3691   0.08142   0.07531  -0.0412   0.0327   0.7998
  17.250   1.3720   0.08433   0.07828  -0.0417   0.0298   0.8014
  17.500   1.3736   0.08748   0.08149  -0.0424   0.0274   0.8030
  17.750   1.3754   0.09062   0.08469  -0.0431   0.0248   0.8047
  18.000   1.3761   0.09397   0.08811  -0.0439   0.0227   0.8064
  18.250   1.3769   0.09736   0.09156  -0.0448   0.0207   0.8081
  18.500   1.3772   0.10086   0.09512  -0.0459   0.0191   0.8098
  18.750   1.3772   0.10446   0.09879  -0.0470   0.0175   0.8115
  19.000   1.3765   0.10813   0.10254  -0.0482   0.0164   0.8132
  19.250   1.3761   0.11182   0.10632  -0.0495   0.0154   0.8152
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