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EPPLER 543 AIRFOIL (e543-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 543 AIRFOIL (e543-il)
Reynolds number: 100,000
Max Cl/Cd: 35.29 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e543-il-100000-n5.txt
Download as CSV file: xf-e543-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 543 AIRFOIL                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.4379   0.10613   0.10099  -0.0587   1.0000   0.0179
 -12.750  -0.4445   0.10000   0.09490  -0.0614   1.0000   0.0177
 -12.500  -0.4602   0.09180   0.08670  -0.0658   1.0000   0.0175
 -12.250  -0.4830   0.08413   0.07898  -0.0699   1.0000   0.0173
 -12.000  -0.5052   0.07825   0.07303  -0.0722   1.0000   0.0170
 -11.750  -0.5290   0.07316   0.06784  -0.0731   1.0000   0.0169
 -11.500  -0.5525   0.06886   0.06343  -0.0728   1.0000   0.0167
 -11.250  -0.5758   0.06512   0.05958  -0.0713   1.0000   0.0167
 -11.000  -0.5985   0.06194   0.05627  -0.0688   1.0000   0.0165
 -10.750  -0.6201   0.05943   0.05366  -0.0654   1.0000   0.0164
 -10.500  -0.6444   0.05754   0.05170  -0.0608   1.0000   0.0165
 -10.250  -0.6564   0.05426   0.04815  -0.0593   0.9929   0.0163
 -10.000  -0.6559   0.05044   0.04394  -0.0596   0.9790   0.0163
  -9.750  -0.6516   0.04702   0.04012  -0.0592   0.9654   0.0164
  -9.500  -0.6394   0.04368   0.03633  -0.0592   0.9555   0.0165
  -9.250  -0.6209   0.04059   0.03281  -0.0594   0.9463   0.0167
  -9.000  -0.5907   0.03752   0.02928  -0.0611   0.9415   0.0170
  -8.750  -0.5571   0.03484   0.02611  -0.0624   0.9351   0.0180
  -8.500  -0.5229   0.03318   0.02438  -0.0647   0.9293   0.0193
  -8.250  -0.4835   0.03143   0.02233  -0.0669   0.9246   0.0215
  -8.000  -0.4489   0.02994   0.02079  -0.0685   0.9174   0.0231
  -7.750  -0.4117   0.02851   0.01924  -0.0705   0.9121   0.0251
  -7.500  -0.3838   0.02734   0.01802  -0.0711   0.9031   0.0276
  -7.250  -0.3546   0.02625   0.01683  -0.0722   0.8955   0.0325
  -7.000  -0.3330   0.02529   0.01579  -0.0717   0.8851   0.0378
  -6.750  -0.3087   0.02430   0.01480  -0.0719   0.8772   0.0469
  -6.500  -0.2902   0.02350   0.01404  -0.0708   0.8670   0.0637
  -6.250  -0.2699   0.02256   0.01336  -0.0701   0.8589   0.1026
  -6.000  -0.2562   0.02163   0.01291  -0.0683   0.8495   0.1825
  -5.750  -0.2587   0.02039   0.01232  -0.0643   0.8394   0.2996
  -5.500  -0.1995   0.02356   0.01702  -0.0628   0.8362   0.6101
  -5.250  -0.1959   0.02346   0.01674  -0.0591   0.8277   0.6459
  -5.000  -0.1944   0.02368   0.01681  -0.0545   0.8179   0.6694
  -4.750  -0.1680   0.02454   0.01745  -0.0531   0.8122   0.6890
  -4.500  -0.1460   0.02537   0.01812  -0.0511   0.8043   0.7050
  -4.250  -0.1084   0.02659   0.01913  -0.0510   0.7991   0.7240
  -4.000  -0.0542   0.02748   0.01978  -0.0542   0.7954   0.7351
  -3.750  -0.0497   0.02744   0.01965  -0.0504   0.7874   0.7452
  -3.500  -0.0113   0.02738   0.01938  -0.0522   0.7825   0.7482
  -3.000   0.0143   0.02710   0.01888  -0.0476   0.7697   0.7611
  -2.750   0.0489   0.02694   0.01856  -0.0490   0.7655   0.7634
  -2.500   0.0739   0.02683   0.01835  -0.0488   0.7603   0.7668
  -2.250   0.0639   0.02658   0.01805  -0.0428   0.7534   0.7757
  -2.000   0.0966   0.02642   0.01775  -0.0439   0.7493   0.7773
  -1.750   0.1234   0.02632   0.01757  -0.0440   0.7444   0.7795
  -1.500   0.1443   0.02623   0.01743  -0.0431   0.7390   0.7825
  -1.250   0.1598   0.02603   0.01714  -0.0414   0.7345   0.7866
  -1.000   0.1642   0.02574   0.01678  -0.0379   0.7299   0.7920
  -0.750   0.1861   0.02571   0.01673  -0.0372   0.7243   0.7938
  -0.500   0.2107   0.02560   0.01657  -0.0369   0.7200   0.7959
  -0.250   0.2351   0.02543   0.01632  -0.0367   0.7165   0.7980
   0.000   0.2473   0.02535   0.01624  -0.0344   0.7114   0.8013
   0.250   0.2474   0.02514   0.01601  -0.0303   0.7058   0.8061
   0.500   0.2688   0.02497   0.01580  -0.0296   0.7020   0.8080
   0.750   0.2980   0.02484   0.01560  -0.0301   0.6991   0.8093
   1.000   0.3098   0.02492   0.01574  -0.0277   0.6929   0.8114
   1.250   0.3288   0.02484   0.01565  -0.0266   0.6884   0.8132
   1.500   0.3519   0.02471   0.01549  -0.0262   0.6850   0.8153
   1.750   0.3670   0.02464   0.01544  -0.0245   0.6806   0.8179
   2.000   0.3740   0.02460   0.01543  -0.0216   0.6747   0.8206
   2.250   0.3927   0.02443   0.01525  -0.0206   0.6706   0.8229
   2.500   0.4227   0.02431   0.01511  -0.0213   0.6676   0.8239
   2.750   0.4331   0.02450   0.01539  -0.0186   0.6612   0.8257
   3.000   0.4538   0.02447   0.01540  -0.0178   0.6562   0.8271
   3.250   0.4821   0.02432   0.01525  -0.0183   0.6526   0.8282
   3.500   0.4958   0.02441   0.01540  -0.0163   0.6466   0.8300
   3.750   0.5133   0.02443   0.01549  -0.0150   0.6408   0.8319
   4.000   0.5424   0.02425   0.01533  -0.0156   0.6368   0.8336
   4.250   0.5554   0.02435   0.01549  -0.0137   0.6303   0.8359
   4.500   0.5755   0.02433   0.01553  -0.0129   0.6242   0.8376
   4.750   0.6086   0.02409   0.01532  -0.0141   0.6200   0.8385
   5.000   0.6170   0.02433   0.01568  -0.0112   0.6120   0.8400
   5.250   0.6440   0.02419   0.01562  -0.0113   0.6063   0.8411
   5.500   0.6657   0.02417   0.01568  -0.0106   0.6000   0.8426
   5.750   0.6825   0.02422   0.01583  -0.0090   0.5922   0.8445
   6.000   0.7145   0.02396   0.01564  -0.0098   0.5864   0.8459
   6.250   0.7229   0.02416   0.01597  -0.0070   0.5769   0.8482
   6.500   0.7526   0.02392   0.01579  -0.0075   0.5698   0.8495
   6.750   0.7648   0.02403   0.01602  -0.0054   0.5599   0.8515
   7.000   0.7831   0.02401   0.01611  -0.0042   0.5503   0.8533
   7.250   0.8087   0.02377   0.01595  -0.0039   0.5409   0.8545
   7.500   0.8104   0.02398   0.01630   0.0001   0.5294   0.8565
   7.750   0.8216   0.02406   0.01649   0.0027   0.5179   0.8588
   8.000   0.8378   0.02408   0.01662   0.0043   0.5057   0.8611
   8.250   0.8522   0.02420   0.01683   0.0061   0.4919   0.8635
   8.500   0.8638   0.02448   0.01720   0.0081   0.4762   0.8660
   8.750   0.8739   0.02489   0.01771   0.0100   0.4585   0.8683
   9.000   0.8843   0.02528   0.01816   0.0120   0.4390   0.8704
   9.250   0.8974   0.02557   0.01844   0.0138   0.4174   0.8725
   9.500   0.9062   0.02617   0.01903   0.0158   0.3934   0.8749
   9.750   0.9161   0.02680   0.01960   0.0176   0.3688   0.8774
  10.000   0.9226   0.02773   0.02049   0.0194   0.3435   0.8803
  10.250   0.9285   0.02881   0.02150   0.0211   0.3191   0.8835
  10.500   0.9318   0.03001   0.02266   0.0231   0.2957   0.8865
  10.750   0.9347   0.03132   0.02393   0.0249   0.2739   0.8898
  11.000   0.9375   0.03277   0.02535   0.0264   0.2521   0.8932
  11.250   0.9403   0.03434   0.02687   0.0277   0.2320   0.8966
  11.500   0.9434   0.03598   0.02851   0.0288   0.2122   0.9000
  11.750   0.9457   0.03764   0.03018   0.0300   0.1940   0.9035
  12.000   0.9480   0.03942   0.03196   0.0309   0.1766   0.9075
  12.250   0.9507   0.04130   0.03384   0.0317   0.1604   0.9119
  12.500   0.9531   0.04324   0.03579   0.0323   0.1454   0.9165
  12.750   0.9556   0.04524   0.03782   0.0329   0.1315   0.9220
  13.000   0.9588   0.04733   0.03995   0.0331   0.1188   0.9288
  13.250   0.9625   0.04954   0.04224   0.0331   0.1069   0.9370
  13.500   0.9670   0.05191   0.04467   0.0325   0.0962   0.9480
  13.750   0.9686   0.05436   0.04715   0.0319   0.0877   0.9742
  14.000   0.9720   0.05679   0.04966   0.0315   0.0796   1.0000
  14.250   0.9748   0.05951   0.05244   0.0309   0.0721   1.0000
  14.500   0.9756   0.06253   0.05546   0.0301   0.0664   1.0000
  14.750   0.9795   0.06527   0.05831   0.0294   0.0607   1.0000
  15.000   0.9790   0.06855   0.06162   0.0285   0.0562   1.0000
  15.250   0.9824   0.07145   0.06465   0.0277   0.0518   1.0000
  15.500   0.9820   0.07487   0.06812   0.0266   0.0480   1.0000
  15.750   0.9834   0.07811   0.07145   0.0256   0.0447   1.0000
  16.000   0.9839   0.08157   0.07502   0.0244   0.0415   1.0000
  16.250   0.9825   0.08523   0.07869   0.0230   0.0393   1.0000
  16.500   0.9832   0.08883   0.08248   0.0217   0.0364   1.0000
  16.750   0.9818   0.09275   0.08650   0.0200   0.0342   1.0000
  17.000   0.9801   0.09667   0.09044   0.0184   0.0325   1.0000
  17.250   0.9789   0.10074   0.09475   0.0167   0.0305   1.0000
  17.500   0.9755   0.10519   0.09932   0.0145   0.0287   1.0000
  17.750   0.9728   0.10950   0.10365   0.0123   0.0274   1.0000
  18.000   0.9694   0.11412   0.10847   0.0101   0.0260   1.0000
  18.250   0.9648   0.11907   0.11360   0.0075   0.0248   1.0000
  18.500   0.9591   0.12428   0.11893   0.0046   0.0236   1.0000
  18.750   0.9566   0.12881   0.12349   0.0019   0.0227   1.0000
  19.000   0.9509   0.13416   0.12899  -0.0012   0.0220   1.0000
  19.250   0.9407   0.14073   0.13579  -0.0050   0.0214   1.0000
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