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EPPLER 603 AIRFOIL (e603-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: EPPLER 603 AIRFOIL (e603-il)
Reynolds number: 200,000
Max Cl/Cd: 56.49 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e603-il-200000.txt
Download as CSV file: xf-e603-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2318   0.09212   0.08844  -0.1087   0.8689   0.0685
 -12.000  -0.2024   0.09163   0.08778  -0.1076   0.8512   0.0697
 -11.750  -0.3101   0.05194   0.04760  -0.1181   0.8186   0.0402
 -11.500  -0.3208   0.04782   0.04337  -0.1182   0.8125   0.0393
 -11.250  -0.4038   0.05422   0.04936  -0.1223   0.8232   0.0422
 -11.000  -0.4613   0.04705   0.04146  -0.1171   0.8138   0.0341
 -10.750  -0.4667   0.04433   0.03852  -0.1150   0.8068   0.0338
 -10.500  -0.4732   0.04182   0.03580  -0.1122   0.7995   0.0334
 -10.250  -0.4782   0.03963   0.03331  -0.1092   0.7936   0.0330
 -10.000  -0.4794   0.03758   0.03094  -0.1064   0.7879   0.0332
  -9.750  -0.4736   0.03547   0.02854  -0.1042   0.7825   0.0332
  -9.500  -0.4648   0.03362   0.02634  -0.1022   0.7780   0.0337
  -9.250  -0.4527   0.03205   0.02436  -0.1005   0.7743   0.0342
  -9.000  -0.4355   0.03040   0.02244  -0.0993   0.7701   0.0345
  -8.750  -0.4062   0.02815   0.02002  -0.0998   0.7664   0.0352
  -8.500  -0.3755   0.02670   0.01853  -0.1005   0.7630   0.0363
  -8.250  -0.3464   0.02563   0.01736  -0.1008   0.7598   0.0378
  -8.000  -0.3158   0.02471   0.01630  -0.1013   0.7568   0.0398
  -7.750  -0.2842   0.02364   0.01526  -0.1020   0.7534   0.0429
  -7.500  -0.2601   0.02300   0.01464  -0.1016   0.7498   0.0459
  -7.250  -0.2351   0.02223   0.01381  -0.1012   0.7468   0.0494
  -7.000  -0.2165   0.02158   0.01322  -0.1001   0.7441   0.0537
  -6.750  -0.2003   0.02098   0.01261  -0.0987   0.7416   0.0604
  -6.500  -0.1859   0.02054   0.01216  -0.0969   0.7390   0.0684
  -6.250  -0.1769   0.02003   0.01174  -0.0944   0.7359   0.0789
  -6.000  -0.1701   0.01941   0.01125  -0.0917   0.7326   0.0951
  -5.750  -0.1614   0.01874   0.01076  -0.0893   0.7296   0.1241
  -5.500  -0.1541   0.01795   0.01030  -0.0869   0.7271   0.1771
  -5.250  -0.1492   0.01697   0.00982  -0.0844   0.7249   0.2751
  -5.000  -0.1466   0.01572   0.00937  -0.0817   0.7227   0.4335
  -4.750  -0.1308   0.01646   0.01110  -0.0776   0.7201   0.6153
  -4.500  -0.1057   0.01723   0.01179  -0.0767   0.7171   0.6604
  -4.250  -0.0789   0.01826   0.01272  -0.0755   0.7143   0.6824
  -4.000  -0.0511   0.01944   0.01382  -0.0740   0.7120   0.6979
  -3.750  -0.0238   0.02039   0.01466  -0.0729   0.7100   0.7113
  -3.500   0.0088   0.02160   0.01579  -0.0715   0.7081   0.7162
  -3.250   0.0336   0.02208   0.01613  -0.0709   0.7061   0.7288
  -3.000   0.0628   0.02316   0.01723  -0.0691   0.7033   0.7322
  -2.750   0.0921   0.02411   0.01814  -0.0679   0.7008   0.7403
  -2.500   0.1214   0.02486   0.01885  -0.0669   0.6983   0.7497
  -2.250   0.1413   0.02525   0.01918  -0.0654   0.6957   0.7628
  -2.000   0.1856   0.02580   0.01964  -0.0665   0.6936   0.7667
  -1.750   0.1974   0.02587   0.01964  -0.0645   0.6915   0.7784
  -1.500   0.2385   0.02606   0.01974  -0.0658   0.6899   0.7815
  -1.250   0.2692   0.02632   0.01999  -0.0661   0.6874   0.7860
  -1.000   0.2629   0.02644   0.02015  -0.0613   0.6836   0.7961
  -0.750   0.2936   0.02651   0.02020  -0.0616   0.6809   0.7989
  -0.500   0.3208   0.02652   0.02018  -0.0616   0.6784   0.8027
  -0.250   0.3224   0.02643   0.02004  -0.0583   0.6759   0.8107
   0.000   0.3521   0.02625   0.01979  -0.0587   0.6740   0.8132
   0.250   0.3846   0.02623   0.01970  -0.0595   0.6723   0.8155
   0.500   0.3818   0.02665   0.02025  -0.0550   0.6674   0.8196
   0.750   0.3859   0.02674   0.02036  -0.0519   0.6635   0.8242
   1.000   0.4006   0.02661   0.02019  -0.0509   0.6607   0.8280
   1.250   0.4289   0.02644   0.01998  -0.0510   0.6587   0.8296
   1.500   0.4580   0.02626   0.01975  -0.0515   0.6569   0.8311
   1.750   0.4666   0.02660   0.02013  -0.0489   0.6530   0.8339
   2.000   0.4626   0.02711   0.02074  -0.0447   0.6470   0.8370
   2.250   0.4870   0.02700   0.02060  -0.0450   0.6441   0.8388
   2.500   0.5190   0.02678   0.02034  -0.0464   0.6422   0.8410
   2.750   0.5537   0.02659   0.02009  -0.0485   0.6404   0.8427
   3.000   0.5880   0.02640   0.01985  -0.0500   0.6388   0.8438
   3.250   0.5576   0.02768   0.02133  -0.0418   0.6288   0.8463
   3.500   0.5890   0.02744   0.02108  -0.0426   0.6266   0.8479
   3.750   0.6259   0.02709   0.02070  -0.0444   0.6250   0.8492
   4.000   0.6644   0.02674   0.02032  -0.0464   0.6234   0.8502
   4.250   0.6388   0.02835   0.02210  -0.0399   0.6130   0.8528
   4.500   0.6757   0.02802   0.02175  -0.0418   0.6107   0.8541
   4.750   0.7176   0.02756   0.02127  -0.0444   0.6091   0.8555
   5.000   0.7607   0.02708   0.02078  -0.0472   0.6075   0.8567
   5.250   0.8057   0.02661   0.02028  -0.0504   0.6061   0.8575
   5.500   0.7833   0.02816   0.02200  -0.0444   0.5951   0.8596
   5.750   0.8255   0.02745   0.02130  -0.0466   0.5933   0.8603
   6.000   0.8689   0.02672   0.02057  -0.0490   0.5915   0.8612
   6.250   0.9139   0.02600   0.01983  -0.0516   0.5899   0.8624
   6.500   0.8919   0.02728   0.02128  -0.0450   0.5795   0.8651
   6.750   0.9363   0.02652   0.02054  -0.0476   0.5771   0.8660
   7.000   0.9845   0.02566   0.01968  -0.0509   0.5751   0.8669
   7.250   1.0327   0.02490   0.01891  -0.0542   0.5728   0.8678
   7.500   1.0206   0.02581   0.02000  -0.0491   0.5630   0.8700
   7.750   1.0697   0.02486   0.01905  -0.0524   0.5601   0.8710
   8.000   1.1230   0.02389   0.01806  -0.0565   0.5575   0.8722
   8.250   1.1138   0.02462   0.01896  -0.0517   0.5478   0.8746
   8.500   1.1587   0.02362   0.01798  -0.0542   0.5439   0.8756
   8.750   1.1665   0.02363   0.01810  -0.0513   0.5368   0.8773
   9.000   1.1879   0.02322   0.01776  -0.0503   0.5302   0.8789
   9.250   1.2192   0.02262   0.01720  -0.0509   0.5239   0.8804
   9.500   1.2254   0.02276   0.01744  -0.0480   0.5150   0.8826
   9.750   1.2431   0.02266   0.01740  -0.0468   0.5065   0.8850
  10.000   1.2660   0.02241   0.01719  -0.0464   0.4972   0.8873
  10.250   1.2708   0.02299   0.01787  -0.0441   0.4855   0.8896
  10.500   1.2809   0.02323   0.01817  -0.0421   0.4740   0.8916
  10.750   1.2937   0.02348   0.01843  -0.0405   0.4613   0.8938
  11.000   1.3039   0.02399   0.01894  -0.0389   0.4472   0.8961
  11.250   1.3101   0.02484   0.01981  -0.0371   0.4314   0.8987
  11.500   1.3144   0.02596   0.02093  -0.0354   0.4144   0.9014
  11.750   1.3175   0.02733   0.02227  -0.0339   0.3964   0.9043
  12.000   1.3167   0.02871   0.02363  -0.0317   0.3789   0.9074
  12.250   1.3159   0.03031   0.02519  -0.0297   0.3608   0.9106
  12.500   1.3153   0.03208   0.02690  -0.0282   0.3426   0.9138
  12.750   1.3143   0.03405   0.02879  -0.0269   0.3244   0.9169
  13.000   1.3118   0.03619   0.03092  -0.0256   0.3067   0.9200
  13.250   1.3084   0.03836   0.03305  -0.0242   0.2896   0.9236
  13.500   1.3060   0.04063   0.03529  -0.0232   0.2731   0.9275
  13.750   1.3041   0.04303   0.03766  -0.0224   0.2568   0.9316
  14.000   1.3011   0.04548   0.04008  -0.0215   0.2413   0.9362
  14.250   1.2981   0.04800   0.04258  -0.0207   0.2263   0.9421
  14.500   1.2958   0.05061   0.04517  -0.0202   0.2117   0.9497
  14.750   1.2940   0.05337   0.04793  -0.0201   0.1972   0.9616
  15.000   1.2916   0.05613   0.05067  -0.0201   0.1839   1.0000
  15.250   1.2917   0.05925   0.05376  -0.0207   0.1707   1.0000
  15.500   1.2921   0.06244   0.05692  -0.0214   0.1585   1.0000
  15.750   1.2940   0.06557   0.06007  -0.0223   0.1468   1.0000
  16.000   1.2960   0.06871   0.06323  -0.0231   0.1361   1.0000
  16.250   1.2962   0.07207   0.06657  -0.0240   0.1267   1.0000
  16.500   1.2961   0.07555   0.07002  -0.0250   0.1176   1.0000
  16.750   1.2979   0.07890   0.07344  -0.0260   0.1085   1.0000
  17.000   1.2974   0.08249   0.07702  -0.0271   0.1010   1.0000
  17.250   1.2972   0.08613   0.08069  -0.0283   0.0935   1.0000
  17.500   1.2973   0.08977   0.08439  -0.0295   0.0863   1.0000
  17.750   1.2944   0.09380   0.08836  -0.0308   0.0800   1.0000
  18.000   1.2950   0.09750   0.09218  -0.0322   0.0735   1.0000
  18.250   1.2913   0.10165   0.09627  -0.0337   0.0679   1.0000
  18.500   1.2903   0.10568   0.10041  -0.0353   0.0622   1.0000
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