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GOE 564 AIRFOIL (goe564-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 564 AIRFOIL (goe564-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.23 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe564-il-1000000-n5.txt
Download as CSV file: xf-goe564-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 564 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -1.0313   0.03237   0.02963  -0.0664   1.0000   0.0047
 -12.500  -1.0185   0.02841   0.02538  -0.0680   0.9985   0.0048
 -12.250  -0.9993   0.02589   0.02265  -0.0691   0.9969   0.0049
 -12.000  -0.9769   0.02410   0.02068  -0.0699   0.9955   0.0051
 -11.750  -0.9535   0.02257   0.01898  -0.0706   0.9943   0.0053
 -11.500  -0.9311   0.02129   0.01754  -0.0707   0.9926   0.0055
 -11.250  -0.9069   0.02017   0.01627  -0.0710   0.9908   0.0058
 -11.000  -0.8813   0.01910   0.01506  -0.0715   0.9893   0.0059
 -10.750  -0.8543   0.01820   0.01402  -0.0721   0.9879   0.0061
 -10.500  -0.8272   0.01713   0.01280  -0.0727   0.9868   0.0064
 -10.250  -0.7993   0.01619   0.01174  -0.0735   0.9859   0.0069
 -10.000  -0.7754   0.01548   0.01094  -0.0731   0.9834   0.0072
  -9.750  -0.7494   0.01483   0.01019  -0.0732   0.9813   0.0076
  -9.500  -0.7216   0.01423   0.00949  -0.0735   0.9796   0.0080
  -9.250  -0.6925   0.01369   0.00886  -0.0741   0.9782   0.0085
  -9.000  -0.6625   0.01309   0.00818  -0.0749   0.9770   0.0092
  -8.750  -0.6314   0.01254   0.00758  -0.0758   0.9759   0.0101
  -8.500  -0.6058   0.01210   0.00710  -0.0755   0.9724   0.0112
  -8.250  -0.5777   0.01169   0.00662  -0.0757   0.9695   0.0121
  -8.000  -0.5476   0.01131   0.00623  -0.0764   0.9675   0.0139
  -7.750  -0.5165   0.01100   0.00590  -0.0772   0.9659   0.0155
  -7.500  -0.4849   0.01068   0.00555  -0.0781   0.9644   0.0168
  -7.250  -0.4584   0.01045   0.00533  -0.0779   0.9602   0.0184
  -7.000  -0.4298   0.01028   0.00516  -0.0781   0.9565   0.0201
  -6.750  -0.3988   0.01008   0.00492  -0.0788   0.9537   0.0214
  -6.500  -0.3668   0.00989   0.00469  -0.0797   0.9512   0.0222
  -6.250  -0.3393   0.00976   0.00453  -0.0796   0.9458   0.0226
  -6.000  -0.3104   0.00938   0.00410  -0.0799   0.9406   0.0238
  -5.750  -0.2799   0.00905   0.00372  -0.0805   0.9365   0.0251
  -5.500  -0.2528   0.00883   0.00348  -0.0804   0.9300   0.0263
  -5.250  -0.2236   0.00862   0.00324  -0.0806   0.9239   0.0273
  -5.000  -0.1953   0.00843   0.00301  -0.0807   0.9176   0.0281
  -4.750  -0.1671   0.00825   0.00277  -0.0807   0.9097   0.0289
  -4.500  -0.1394   0.00807   0.00254  -0.0806   0.9017   0.0294
  -4.250  -0.1118   0.00791   0.00232  -0.0805   0.8934   0.0299
  -4.000  -0.0847   0.00776   0.00212  -0.0802   0.8855   0.0303
  -3.500  -0.0305   0.00752   0.00179  -0.0797   0.8709   0.0312
  -3.000   0.0231   0.00725   0.00146  -0.0791   0.8562   0.0361
  -2.750   0.0496   0.00715   0.00134  -0.0787   0.8467   0.0390
  -2.500   0.0756   0.00707   0.00123  -0.0782   0.8339   0.0463
  -2.250   0.1008   0.00694   0.00113  -0.0775   0.8183   0.0668
  -2.000   0.1263   0.00689   0.00107  -0.0769   0.8013   0.0798
  -1.750   0.1521   0.00686   0.00102  -0.0763   0.7854   0.0891
  -1.500   0.1780   0.00683   0.00096  -0.0758   0.7685   0.0967
  -1.250   0.2024   0.00687   0.00091  -0.0749   0.7370   0.1026
  -1.000   0.2238   0.00707   0.00088  -0.0734   0.6766   0.1065
  -0.750   0.2462   0.00724   0.00088  -0.0722   0.6319   0.1131
  -0.500   0.2709   0.00735   0.00089  -0.0715   0.6051   0.1193
  -0.250   0.2957   0.00743   0.00090  -0.0708   0.5787   0.1282
   0.000   0.3203   0.00749   0.00092  -0.0701   0.5481   0.1483
   0.250   0.3442   0.00753   0.00094  -0.0693   0.5112   0.1856
   0.500   0.3674   0.00758   0.00098  -0.0684   0.4677   0.2387
   0.750   0.3901   0.00761   0.00105  -0.0675   0.4252   0.3137
   1.000   0.4125   0.00762   0.00113  -0.0665   0.3841   0.4044
   1.250   0.4344   0.00759   0.00122  -0.0654   0.3445   0.5059
   1.500   0.4558   0.00758   0.00134  -0.0642   0.3026   0.6092
   1.750   0.4753   0.00747   0.00146  -0.0625   0.2673   0.7366
   2.000   0.5250   0.00726   0.00172  -0.0673   0.2320   0.9728
   2.250   0.5717   0.00750   0.00185  -0.0716   0.2125   0.9917
   2.500   0.6093   0.00768   0.00196  -0.0739   0.1997   0.9987
   3.000   0.6610   0.00803   0.00217  -0.0731   0.1729   1.0000
   3.250   0.6846   0.00816   0.00227  -0.0722   0.1671   1.0000
   3.500   0.7079   0.00832   0.00239  -0.0712   0.1584   1.0000
   3.750   0.7315   0.00846   0.00251  -0.0703   0.1522   1.0000
   4.000   0.7549   0.00862   0.00264  -0.0693   0.1434   1.0000
   4.250   0.7784   0.00879   0.00278  -0.0684   0.1341   1.0000
   4.500   0.8010   0.00903   0.00294  -0.0674   0.1171   1.0000
   4.750   0.8224   0.00936   0.00315  -0.0661   0.0954   1.0000
   5.000   0.8449   0.00962   0.00336  -0.0650   0.0858   1.0000
   5.250   0.8674   0.00988   0.00359  -0.0640   0.0787   1.0000
   5.500   0.8910   0.01006   0.00378  -0.0631   0.0755   1.0000
   5.750   0.9146   0.01025   0.00398  -0.0622   0.0713   1.0000
   6.000   0.9372   0.01053   0.00422  -0.0612   0.0641   1.0000
   6.250   0.9575   0.01099   0.00454  -0.0598   0.0395   1.0000
   6.500   0.9793   0.01134   0.00486  -0.0587   0.0312   1.0000
   6.750   1.0015   0.01167   0.00518  -0.0576   0.0271   1.0000
   7.000   1.0242   0.01196   0.00547  -0.0567   0.0239   1.0000
   7.250   1.0467   0.01226   0.00578  -0.0557   0.0206   1.0000
   7.500   1.0684   0.01263   0.00615  -0.0546   0.0169   1.0000
   7.750   1.0903   0.01298   0.00650  -0.0535   0.0146   1.0000
   8.000   1.1116   0.01339   0.00690  -0.0524   0.0122   1.0000
   8.250   1.1336   0.01372   0.00726  -0.0514   0.0111   1.0000
   8.500   1.1548   0.01411   0.00767  -0.0502   0.0100   1.0000
   8.750   1.1754   0.01456   0.00815  -0.0490   0.0089   1.0000
   9.000   1.1962   0.01498   0.00860  -0.0478   0.0084   1.0000
   9.250   1.2169   0.01538   0.00904  -0.0466   0.0079   1.0000
   9.500   1.2372   0.01580   0.00951  -0.0454   0.0074   1.0000
   9.750   1.2566   0.01629   0.01002  -0.0441   0.0069   1.0000
  10.000   1.2753   0.01682   0.01059  -0.0426   0.0065   1.0000
  10.250   1.2933   0.01736   0.01118  -0.0410   0.0060   1.0000
  10.500   1.3116   0.01786   0.01175  -0.0395   0.0058   1.0000
  10.750   1.3283   0.01840   0.01235  -0.0378   0.0056   1.0000
  11.000   1.3436   0.01892   0.01293  -0.0357   0.0053   1.0000
  11.250   1.3582   0.01947   0.01354  -0.0336   0.0051   1.0000
  11.500   1.3718   0.02009   0.01420  -0.0314   0.0049   1.0000
  11.750   1.3852   0.02071   0.01489  -0.0292   0.0047   1.0000
  12.000   1.3968   0.02147   0.01570  -0.0269   0.0045   1.0000
  12.250   1.4058   0.02239   0.01672  -0.0242   0.0043   1.0000
  12.500   1.4159   0.02325   0.01767  -0.0219   0.0042   1.0000
  12.750   1.4262   0.02410   0.01860  -0.0196   0.0041   1.0000
  13.000   1.4350   0.02505   0.01964  -0.0173   0.0041   1.0000
  13.250   1.4428   0.02609   0.02078  -0.0151   0.0040   1.0000
  13.500   1.4514   0.02710   0.02188  -0.0130   0.0038   1.0000
  13.750   1.4572   0.02834   0.02322  -0.0109   0.0038   1.0000
  14.000   1.4634   0.02959   0.02456  -0.0089   0.0037   1.0000
  14.250   1.4698   0.03088   0.02593  -0.0072   0.0036   1.0000
  14.500   1.4734   0.03245   0.02760  -0.0055   0.0035   1.0000
  14.750   1.4748   0.03429   0.02955  -0.0038   0.0034   1.0000
  15.000   1.4787   0.03600   0.03134  -0.0026   0.0033   1.0000
  15.250   1.4745   0.03857   0.03406  -0.0013   0.0033   1.0000
  15.500   1.4742   0.04091   0.03650  -0.0005   0.0032   1.0000
  15.750   1.4735   0.04344   0.03913  -0.0001   0.0032   1.0000
  16.000   1.4684   0.04667   0.04247   0.0000   0.0031   1.0000
  16.250   1.4607   0.05044   0.04638  -0.0005   0.0031   1.0000
  16.500   1.4497   0.05498   0.05105  -0.0016   0.0030   1.0000
  16.750   1.4357   0.06028   0.05649  -0.0035   0.0029   1.0000
  17.000   1.4228   0.06571   0.06206  -0.0057   0.0030   1.0000
  17.250   1.4005   0.07314   0.06967  -0.0092   0.0030   1.0000
  17.500   1.3781   0.08109   0.07777  -0.0132   0.0030   1.0000
  17.750   1.3544   0.08965   0.08649  -0.0177   0.0030   1.0000
  18.000   1.3230   0.10003   0.09704  -0.0232   0.0031   1.0000
  18.250   1.2862   0.11167   0.10885  -0.0293   0.0031   1.0000
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