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E205 (10.48%) (e205-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E205 (10.48%) (e205-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.53 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e205-il-1000000-n5.txt
Download as CSV file: xf-e205-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E205  (10.48%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.7236   0.03925   0.03734  -0.0576   1.0000   0.0065
 -10.250  -0.7391   0.03440   0.03219  -0.0565   1.0000   0.0066
 -10.000  -0.7340   0.03199   0.02961  -0.0554   0.9993   0.0066
  -9.750  -0.7140   0.02967   0.02709  -0.0568   0.9918   0.0067
  -9.500  -0.6891   0.02762   0.02484  -0.0586   0.9850   0.0069
  -9.250  -0.6653   0.02560   0.02260  -0.0598   0.9747   0.0071
  -9.000  -0.6408   0.02334   0.02006  -0.0610   0.9575   0.0072
  -8.750  -0.6165   0.02165   0.01808  -0.0615   0.9206   0.0074
  -8.500  -0.5992   0.02045   0.01654  -0.0601   0.8771   0.0076
  -8.250  -0.5808   0.01938   0.01517  -0.0587   0.8435   0.0078
  -8.000  -0.5610   0.01839   0.01390  -0.0576   0.8138   0.0080
  -7.750  -0.5400   0.01740   0.01266  -0.0566   0.7891   0.0081
  -7.500  -0.5177   0.01661   0.01165  -0.0558   0.7675   0.0083
  -7.250  -0.4945   0.01590   0.01075  -0.0551   0.7481   0.0085
  -7.000  -0.4709   0.01523   0.00989  -0.0544   0.7296   0.0086
  -6.750  -0.4469   0.01456   0.00904  -0.0538   0.7135   0.0087
  -6.500  -0.4224   0.01398   0.00830  -0.0532   0.6987   0.0089
  -6.250  -0.3975   0.01347   0.00766  -0.0528   0.6848   0.0090
  -6.000  -0.3723   0.01297   0.00703  -0.0523   0.6726   0.0090
  -5.750  -0.3467   0.01254   0.00649  -0.0519   0.6614   0.0091
  -5.500  -0.3211   0.01212   0.00595  -0.0514   0.6505   0.0092
  -5.000  -0.2713   0.01093   0.00455  -0.0504   0.6309   0.0098
  -4.750  -0.2455   0.01051   0.00403  -0.0500   0.6221   0.0101
  -4.500  -0.2193   0.01019   0.00364  -0.0496   0.6132   0.0105
  -4.250  -0.1926   0.00992   0.00331  -0.0493   0.6057   0.0109
  -4.000  -0.1659   0.00970   0.00301  -0.0491   0.5977   0.0112
  -3.750  -0.1389   0.00949   0.00276  -0.0489   0.5906   0.0118
  -3.500  -0.1118   0.00931   0.00252  -0.0486   0.5834   0.0122
  -3.250  -0.0846   0.00915   0.00230  -0.0484   0.5770   0.0125
  -3.000  -0.0573   0.00901   0.00210  -0.0483   0.5702   0.0129
  -2.750  -0.0299   0.00888   0.00193  -0.0481   0.5643   0.0133
  -2.500  -0.0024   0.00877   0.00178  -0.0480   0.5580   0.0135
  -2.250   0.0250   0.00866   0.00162  -0.0478   0.5521   0.0145
  -2.000   0.0526   0.00854   0.00148  -0.0477   0.5464   0.0167
  -1.750   0.0799   0.00843   0.00136  -0.0475   0.5408   0.0232
  -1.500   0.1068   0.00820   0.00126  -0.0473   0.5356   0.0581
  -1.250   0.1339   0.00804   0.00118  -0.0472   0.5298   0.0878
  -1.000   0.1609   0.00790   0.00112  -0.0470   0.5247   0.1213
  -0.750   0.1881   0.00773   0.00107  -0.0469   0.5196   0.1636
  -0.500   0.2147   0.00753   0.00103  -0.0468   0.5140   0.2232
  -0.250   0.2407   0.00724   0.00101  -0.0465   0.5091   0.3165
   0.000   0.2667   0.00694   0.00100  -0.0463   0.5041   0.4148
   0.250   0.2925   0.00670   0.00100  -0.0459   0.4984   0.5046
   0.500   0.3184   0.00649   0.00101  -0.0456   0.4938   0.5856
   0.750   0.3438   0.00627   0.00103  -0.0451   0.4887   0.6689
   1.000   0.3674   0.00601   0.00106  -0.0442   0.4833   0.7695
   1.250   0.3900   0.00573   0.00111  -0.0428   0.4786   0.8740
   1.500   0.4271   0.00572   0.00123  -0.0445   0.4725   0.9494
   1.750   0.4603   0.00581   0.00129  -0.0456   0.4668   0.9688
   2.000   0.4952   0.00588   0.00134  -0.0471   0.4605   0.9778
   2.250   0.5283   0.00598   0.00139  -0.0483   0.4534   0.9841
   2.500   0.5663   0.00605   0.00144  -0.0505   0.4451   0.9877
   2.750   0.6014   0.00615   0.00150  -0.0522   0.4362   0.9916
   3.000   0.6365   0.00626   0.00156  -0.0538   0.4263   0.9948
   3.250   0.6745   0.00634   0.00160  -0.0561   0.4162   0.9975
   3.500   0.7123   0.00644   0.00167  -0.0584   0.4052   1.0000
   3.750   0.7371   0.00656   0.00176  -0.0578   0.3950   1.0000
   4.000   0.7618   0.00669   0.00185  -0.0572   0.3839   1.0000
   4.250   0.7865   0.00682   0.00195  -0.0566   0.3715   1.0000
   4.500   0.8109   0.00698   0.00208  -0.0559   0.3578   1.0000
   4.750   0.8349   0.00718   0.00221  -0.0552   0.3417   1.0000
   5.000   0.8588   0.00737   0.00236  -0.0545   0.3257   1.0000
   5.250   0.8818   0.00765   0.00254  -0.0537   0.3010   1.0000
   5.500   0.9019   0.00819   0.00285  -0.0524   0.2529   1.0000
   5.750   0.9195   0.00892   0.00327  -0.0508   0.1932   1.0000
   6.000   0.9383   0.00953   0.00366  -0.0493   0.1503   1.0000
   6.250   0.9586   0.01002   0.00401  -0.0481   0.1221   1.0000
   6.500   0.9797   0.01042   0.00432  -0.0470   0.1018   1.0000
   7.000   1.0209   0.01129   0.00503  -0.0446   0.0655   1.0000
   7.250   1.0399   0.01185   0.00546  -0.0432   0.0444   1.0000
   7.500   1.0587   0.01242   0.00593  -0.0418   0.0277   1.0000
   7.750   1.0782   0.01294   0.00638  -0.0405   0.0160   1.0000
   8.000   1.0964   0.01356   0.00694  -0.0390   0.0067   1.0000
   8.250   1.1175   0.01393   0.00736  -0.0380   0.0059   1.0000
   8.500   1.1380   0.01436   0.00781  -0.0369   0.0052   1.0000
   8.750   1.1582   0.01479   0.00828  -0.0357   0.0048   1.0000
   9.000   1.1775   0.01527   0.00882  -0.0345   0.0044   1.0000
   9.250   1.1967   0.01574   0.00933  -0.0332   0.0042   1.0000
   9.500   1.2157   0.01619   0.00982  -0.0320   0.0041   1.0000
   9.750   1.2337   0.01669   0.01038  -0.0306   0.0039   1.0000
  10.000   1.2508   0.01720   0.01094  -0.0291   0.0037   1.0000
  10.250   1.2657   0.01781   0.01160  -0.0273   0.0035   1.0000
  10.500   1.2786   0.01835   0.01219  -0.0250   0.0034   1.0000
  10.750   1.2882   0.01900   0.01290  -0.0223   0.0032   1.0000
  11.000   1.2978   0.01969   0.01365  -0.0198   0.0032   1.0000
  11.250   1.3062   0.02051   0.01454  -0.0174   0.0031   1.0000
  11.500   1.3137   0.02143   0.01552  -0.0151   0.0030   1.0000
  11.750   1.3204   0.02248   0.01666  -0.0129   0.0029   1.0000
  12.000   1.3257   0.02372   0.01798  -0.0110   0.0028   1.0000
  12.250   1.3300   0.02515   0.01949  -0.0092   0.0028   1.0000
  12.500   1.3339   0.02673   0.02116  -0.0078   0.0027   1.0000
  12.750   1.3337   0.02882   0.02335  -0.0064   0.0026   1.0000
  13.000   1.3334   0.03106   0.02570  -0.0055   0.0026   1.0000
  13.250   1.3309   0.03368   0.02844  -0.0047   0.0025   1.0000
  13.500   1.3296   0.03630   0.03117  -0.0043   0.0025   1.0000
  13.750   1.3331   0.03851   0.03346  -0.0041   0.0025   1.0000
  14.000   1.3342   0.04104   0.03608  -0.0040   0.0025   1.0000
  14.250   1.3347   0.04370   0.03883  -0.0041   0.0025   1.0000
  14.500   1.3329   0.04669   0.04192  -0.0042   0.0025   1.0000
  14.750   1.3317   0.04966   0.04498  -0.0045   0.0024   1.0000
  15.000   1.3287   0.05292   0.04834  -0.0050   0.0024   1.0000
  15.250   1.3268   0.05617   0.05169  -0.0056   0.0024   1.0000
  15.500   1.3261   0.05935   0.05497  -0.0063   0.0023   1.0000
  15.750   1.3170   0.06379   0.05952  -0.0074   0.0024   1.0000
  16.000   1.3126   0.06772   0.06356  -0.0085   0.0023   1.0000
  16.250   1.3099   0.07152   0.06744  -0.0098   0.0023   1.0000
  16.500   1.2997   0.07655   0.07260  -0.0115   0.0023   1.0000
  16.750   1.2920   0.08138   0.07754  -0.0133   0.0023   1.0000
  17.000   1.2863   0.08600   0.08226  -0.0151   0.0022   1.0000
  17.250   1.2740   0.09181   0.08819  -0.0175   0.0023   1.0000
  17.500   1.2699   0.09647   0.09295  -0.0196   0.0022   1.0000
  17.750   1.2599   0.10220   0.09879  -0.0222   0.0022   1.0000
  18.000   1.2505   0.10800   0.10470  -0.0249   0.0022   1.0000
  18.250   1.2399   0.11416   0.11097  -0.0279   0.0022   1.0000
  18.500   1.2276   0.12078   0.11770  -0.0313   0.0022   1.0000
  18.750   1.2161   0.12739   0.12442  -0.0347   0.0022   1.0000
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