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GOE 585 AIRFOIL (goe585-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 585 AIRFOIL (goe585-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.48 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe585-il-1000000-n5.txt
Download as CSV file: xf-goe585-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 585 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.9588   0.03279   0.03035  -0.0713   1.0000   0.0068
 -12.250  -0.9643   0.02780   0.02500  -0.0704   1.0000   0.0069
 -12.000  -0.9571   0.02528   0.02226  -0.0689   1.0000   0.0071
 -11.750  -0.9439   0.02344   0.02023  -0.0678   0.9998   0.0073
 -11.500  -0.9183   0.02171   0.01830  -0.0689   0.9985   0.0076
 -11.250  -0.8908   0.02030   0.01669  -0.0701   0.9969   0.0079
 -11.000  -0.8619   0.01910   0.01532  -0.0713   0.9952   0.0081
 -10.750  -0.8342   0.01790   0.01397  -0.0721   0.9933   0.0086
 -10.500  -0.8065   0.01694   0.01290  -0.0728   0.9910   0.0092
 -10.250  -0.7774   0.01611   0.01196  -0.0735   0.9888   0.0098
 -10.000  -0.7473   0.01538   0.01113  -0.0745   0.9870   0.0105
  -9.750  -0.7166   0.01471   0.01036  -0.0754   0.9856   0.0113
  -9.500  -0.6900   0.01426   0.00987  -0.0753   0.9823   0.0122
  -9.250  -0.6613   0.01386   0.00943  -0.0757   0.9797   0.0131
  -9.000  -0.6315   0.01341   0.00891  -0.0762   0.9777   0.0139
  -8.750  -0.6008   0.01301   0.00845  -0.0770   0.9761   0.0147
  -8.500  -0.5711   0.01288   0.00833  -0.0773   0.9735   0.0156
  -8.250  -0.5425   0.01273   0.00817  -0.0774   0.9695   0.0163
  -8.000  -0.5113   0.01256   0.00798  -0.0782   0.9668   0.0173
  -7.750  -0.4789   0.01231   0.00768  -0.0791   0.9646   0.0181
  -7.500  -0.4488   0.01205   0.00736  -0.0796   0.9609   0.0186
  -7.250  -0.4187   0.01178   0.00703  -0.0801   0.9563   0.0189
  -7.000  -0.3874   0.01135   0.00656  -0.0809   0.9523   0.0198
  -6.750  -0.3561   0.01115   0.00634  -0.0817   0.9477   0.0204
  -6.500  -0.3257   0.01095   0.00612  -0.0822   0.9416   0.0210
  -6.250  -0.2943   0.01075   0.00588  -0.0829   0.9362   0.0217
  -6.000  -0.2655   0.01052   0.00560  -0.0830   0.9291   0.0224
  -5.750  -0.2362   0.01027   0.00528  -0.0832   0.9218   0.0231
  -5.500  -0.2084   0.01004   0.00499  -0.0831   0.9146   0.0236
  -5.250  -0.1808   0.00978   0.00466  -0.0830   0.9071   0.0240
  -5.000  -0.1536   0.00958   0.00440  -0.0827   0.8988   0.0243
  -4.750  -0.1266   0.00941   0.00415  -0.0824   0.8871   0.0246
  -4.500  -0.1005   0.00920   0.00385  -0.0818   0.8716   0.0247
  -4.250  -0.0747   0.00901   0.00357  -0.0812   0.8541   0.0248
  -4.000  -0.0499   0.00858   0.00303  -0.0804   0.8367   0.0254
  -3.750  -0.0248   0.00830   0.00263  -0.0797   0.8174   0.0260
  -3.500   0.0002   0.00812   0.00233  -0.0789   0.7934   0.0267
  -3.250   0.0250   0.00802   0.00211  -0.0781   0.7668   0.0276
  -3.000   0.0501   0.00796   0.00193  -0.0773   0.7422   0.0282
  -2.750   0.0758   0.00789   0.00177  -0.0767   0.7238   0.0288
  -2.500   0.1020   0.00783   0.00163  -0.0762   0.7079   0.0294
  -2.250   0.1282   0.00777   0.00151  -0.0757   0.6931   0.0299
  -2.000   0.1546   0.00772   0.00140  -0.0752   0.6782   0.0304
  -1.750   0.1810   0.00769   0.00129  -0.0748   0.6628   0.0309
  -1.500   0.2074   0.00766   0.00121  -0.0743   0.6471   0.0314
  -1.250   0.2337   0.00765   0.00113  -0.0738   0.6284   0.0320
  -1.000   0.2598   0.00768   0.00107  -0.0733   0.6061   0.0325
  -0.750   0.2856   0.00773   0.00102  -0.0728   0.5790   0.0330
  -0.500   0.3111   0.00780   0.00098  -0.0722   0.5482   0.0368
  -0.250   0.3356   0.00785   0.00097  -0.0714   0.5078   0.0579
   0.000   0.3598   0.00798   0.00100  -0.0707   0.4609   0.0847
   0.500   0.4103   0.00819   0.00109  -0.0695   0.4004   0.1233
   0.750   0.4361   0.00825   0.00113  -0.0691   0.3808   0.1441
   1.000   0.4618   0.00825   0.00117  -0.0686   0.3635   0.1844
   1.250   0.4870   0.00820   0.00124  -0.0681   0.3472   0.2562
   1.500   0.5127   0.00821   0.00132  -0.0676   0.3316   0.3052
   1.750   0.5383   0.00818   0.00139  -0.0672   0.3191   0.3621
   2.000   0.5628   0.00799   0.00148  -0.0666   0.3088   0.4812
   2.500   0.6565   0.00713   0.00177  -0.0752   0.2840   1.0000
   2.750   0.6809   0.00727   0.00185  -0.0744   0.2740   1.0000
   3.000   0.7053   0.00740   0.00195  -0.0736   0.2642   1.0000
   3.250   0.7296   0.00755   0.00204  -0.0728   0.2551   1.0000
   3.500   0.7542   0.00768   0.00214  -0.0720   0.2470   1.0000
   3.750   0.7788   0.00782   0.00226  -0.0713   0.2396   1.0000
   4.000   0.8031   0.00798   0.00237  -0.0705   0.2301   1.0000
   4.250   0.8271   0.00818   0.00250  -0.0697   0.2174   1.0000
   4.500   0.8514   0.00835   0.00265  -0.0689   0.2090   1.0000
   4.750   0.8757   0.00853   0.00279  -0.0681   0.2003   1.0000
   5.000   0.8999   0.00871   0.00294  -0.0674   0.1909   1.0000
   5.250   0.9240   0.00892   0.00311  -0.0666   0.1809   1.0000
   5.500   0.9484   0.00911   0.00328  -0.0659   0.1741   1.0000
   5.750   0.9727   0.00931   0.00345  -0.0652   0.1668   1.0000
   6.000   0.9963   0.00956   0.00365  -0.0643   0.1556   1.0000
   6.250   1.0204   0.00978   0.00386  -0.0636   0.1457   1.0000
   6.500   1.0437   0.01007   0.00409  -0.0628   0.1325   1.0000
   6.750   1.0652   0.01052   0.00440  -0.0617   0.1072   1.0000
   7.000   1.0848   0.01117   0.00485  -0.0603   0.0766   1.0000
   7.250   1.1066   0.01160   0.00522  -0.0593   0.0625   1.0000
   7.500   1.1289   0.01199   0.00558  -0.0583   0.0536   1.0000
   7.750   1.1518   0.01233   0.00590  -0.0575   0.0473   1.0000
   8.000   1.1737   0.01275   0.00628  -0.0565   0.0389   1.0000
   8.250   1.1945   0.01326   0.00673  -0.0553   0.0281   1.0000
   8.500   1.2145   0.01385   0.00725  -0.0541   0.0176   1.0000
   8.750   1.2358   0.01430   0.00770  -0.0530   0.0141   1.0000
   9.000   1.2570   0.01474   0.00815  -0.0519   0.0123   1.0000
   9.250   1.2778   0.01520   0.00863  -0.0508   0.0106   1.0000
   9.500   1.2990   0.01560   0.00908  -0.0498   0.0098   1.0000
   9.750   1.3194   0.01605   0.00956  -0.0486   0.0091   1.0000
  10.000   1.3390   0.01656   0.01011  -0.0473   0.0084   1.0000
  10.250   1.3578   0.01711   0.01070  -0.0459   0.0078   1.0000
  10.500   1.3770   0.01758   0.01122  -0.0446   0.0074   1.0000
  10.750   1.3955   0.01807   0.01176  -0.0433   0.0071   1.0000
  11.000   1.4130   0.01861   0.01235  -0.0417   0.0066   1.0000
  11.250   1.4291   0.01919   0.01297  -0.0400   0.0063   1.0000
  11.500   1.4425   0.01979   0.01362  -0.0377   0.0059   1.0000
  11.750   1.4532   0.02052   0.01442  -0.0351   0.0056   1.0000
  12.000   1.4656   0.02113   0.01509  -0.0328   0.0054   1.0000
  12.250   1.4770   0.02182   0.01585  -0.0305   0.0053   1.0000
  12.500   1.4881   0.02254   0.01664  -0.0283   0.0051   1.0000
  12.750   1.4982   0.02334   0.01752  -0.0260   0.0050   1.0000
  13.000   1.5072   0.02422   0.01847  -0.0238   0.0048   1.0000
  13.250   1.5154   0.02519   0.01952  -0.0216   0.0047   1.0000
  13.500   1.5230   0.02624   0.02064  -0.0195   0.0045   1.0000
  13.750   1.5292   0.02742   0.02190  -0.0175   0.0043   1.0000
  14.000   1.5335   0.02882   0.02339  -0.0155   0.0043   1.0000
  14.250   1.5373   0.03032   0.02498  -0.0138   0.0042   1.0000
  14.500   1.5372   0.03225   0.02699  -0.0121   0.0040   1.0000
  14.750   1.5352   0.03448   0.02934  -0.0106   0.0039   1.0000
  15.000   1.5333   0.03689   0.03185  -0.0096   0.0039   1.0000
  15.250   1.5295   0.03969   0.03478  -0.0090   0.0038   1.0000
  15.500   1.5316   0.04201   0.03719  -0.0087   0.0038   1.0000
  15.750   1.5290   0.04500   0.04030  -0.0088   0.0037   1.0000
  16.000   1.5210   0.04888   0.04430  -0.0093   0.0036   1.0000
  16.250   1.5103   0.05335   0.04891  -0.0104   0.0037   1.0000
  16.500   1.5014   0.05786   0.05354  -0.0118   0.0036   1.0000
  16.750   1.4892   0.06319   0.05901  -0.0139   0.0035   1.0000
  17.000   1.4726   0.06951   0.06547  -0.0167   0.0036   1.0000
  17.250   1.4478   0.07762   0.07375  -0.0205   0.0036   1.0000
  17.500   1.4297   0.08464   0.08090  -0.0238   0.0036   1.0000
  17.750   1.4044   0.09308   0.08948  -0.0279   0.0036   1.0000
  18.000   1.3840   0.10071   0.09724  -0.0316   0.0035   1.0000
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