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GOE 534 AIRFOIL (goe534-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 534 AIRFOIL (goe534-il)
Reynolds number: 500,000
Max Cl/Cd: 91 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe534-il-500000-n5.txt
Download as CSV file: xf-goe534-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 534 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.6662   0.09539   0.09208  -0.0435   1.0000   0.0274
 -15.000  -0.7080   0.08432   0.08082  -0.0507   1.0000   0.0277
 -14.750  -0.7330   0.07660   0.07297  -0.0558   1.0000   0.0278
 -14.500  -0.7516   0.07022   0.06648  -0.0600   1.0000   0.0279
 -14.250  -0.7700   0.06420   0.06037  -0.0641   1.0000   0.0280
 -14.000  -0.7834   0.05950   0.05561  -0.0670   1.0000   0.0281
 -13.750  -0.7977   0.05502   0.05111  -0.0696   1.0000   0.0283
 -13.500  -0.8188   0.05003   0.04606  -0.0724   1.0000   0.0283
 -13.250  -0.8541   0.04478   0.04075  -0.0742   1.0000   0.0283
 -13.000  -0.8742   0.03925   0.03513  -0.0785   1.0000   0.0283
 -12.750  -0.8793   0.03420   0.02997  -0.0833   1.0000   0.0285
 -12.500  -0.8722   0.03002   0.02566  -0.0875   1.0000   0.0287
 -12.250  -0.8577   0.02698   0.02248  -0.0903   1.0000   0.0290
 -12.000  -0.8233   0.02495   0.02032  -0.0945   0.9963   0.0293
 -11.750  -0.7894   0.02339   0.01866  -0.0977   0.9907   0.0297
 -11.500  -0.7572   0.02210   0.01727  -0.1000   0.9840   0.0300
 -11.250  -0.7260   0.02100   0.01607  -0.1017   0.9758   0.0304
 -11.000  -0.6915   0.01999   0.01497  -0.1038   0.9671   0.0309
 -10.750  -0.6564   0.01910   0.01397  -0.1058   0.9550   0.0314
 -10.500  -0.6189   0.01828   0.01304  -0.1081   0.9408   0.0318
 -10.250  -0.5794   0.01727   0.01195  -0.1110   0.9220   0.0323
 -10.000  -0.5427   0.01649   0.01105  -0.1131   0.8943   0.0328
  -9.500  -0.4880   0.01549   0.00973  -0.1128   0.8368   0.0338
  -9.250  -0.4630   0.01509   0.00918  -0.1121   0.8160   0.0344
  -9.000  -0.4377   0.01473   0.00868  -0.1114   0.7990   0.0349
  -8.750  -0.4121   0.01438   0.00820  -0.1108   0.7846   0.0355
  -8.500  -0.3864   0.01398   0.00772  -0.1102   0.7723   0.0363
  -8.000  -0.3343   0.01327   0.00684  -0.1090   0.7492   0.0385
  -7.750  -0.3080   0.01299   0.00646  -0.1084   0.7392   0.0397
  -7.500  -0.2812   0.01265   0.00609  -0.1079   0.7292   0.0416
  -7.000  -0.2275   0.01216   0.00557  -0.1069   0.7086   0.0503
  -6.750  -0.2000   0.01209   0.00548  -0.1063   0.6986   0.0577
  -6.500  -0.1720   0.01200   0.00535  -0.1059   0.6878   0.0621
  -6.250  -0.1444   0.01196   0.00520  -0.1053   0.6760   0.0656
  -6.000  -0.1166   0.01188   0.00508  -0.1048   0.6633   0.0679
  -5.750  -0.0888   0.01184   0.00497  -0.1043   0.6505   0.0702
  -5.500  -0.0613   0.01180   0.00483  -0.1038   0.6350   0.0722
  -5.250  -0.0340   0.01174   0.00466  -0.1032   0.6169   0.0737
  -5.000  -0.0071   0.01163   0.00449  -0.1026   0.5980   0.0752
  -4.750   0.0199   0.01160   0.00436  -0.1020   0.5788   0.0769
  -4.500   0.0469   0.01156   0.00422  -0.1014   0.5603   0.0782
  -4.250   0.0741   0.01152   0.00408  -0.1009   0.5443   0.0793
  -4.000   0.1015   0.01150   0.00396  -0.1003   0.5307   0.0806
  -3.750   0.1287   0.01146   0.00384  -0.0998   0.5184   0.0817
  -3.500   0.1558   0.01134   0.00367  -0.0993   0.5068   0.0830
  -3.250   0.1831   0.01127   0.00355  -0.0988   0.4955   0.0841
  -2.750   0.2380   0.01119   0.00335  -0.0978   0.4728   0.0864
  -2.500   0.2653   0.01116   0.00327  -0.0973   0.4638   0.0876
  -2.250   0.2933   0.01112   0.00319  -0.0969   0.4563   0.0890
  -2.000   0.3209   0.01112   0.00313  -0.0965   0.4478   0.0902
  -1.750   0.3484   0.01104   0.00303  -0.0960   0.4403   0.0919
  -1.500   0.3762   0.01098   0.00296  -0.0956   0.4333   0.0930
  -1.250   0.4036   0.01097   0.00290  -0.0951   0.4259   0.0942
  -1.000   0.4314   0.01095   0.00286  -0.0947   0.4189   0.0956
  -0.750   0.4590   0.01094   0.00283  -0.0943   0.4108   0.0972
  -0.500   0.4864   0.01097   0.00281  -0.0938   0.4037   0.0989
  -0.250   0.5142   0.01096   0.00279  -0.0934   0.3972   0.1013
   0.000   0.5416   0.01096   0.00279  -0.0929   0.3899   0.1056
   0.250   0.5689   0.01097   0.00279  -0.0925   0.3830   0.1130
   0.750   0.6227   0.01085   0.00284  -0.0916   0.3671   0.1843
   1.000   0.6500   0.01082   0.00290  -0.0912   0.3601   0.2189
   1.250   0.6768   0.01084   0.00298  -0.0907   0.3523   0.2489
   1.500   0.7037   0.01088   0.00306  -0.0902   0.3448   0.2753
   1.750   0.7305   0.01096   0.00315  -0.0897   0.3359   0.2955
   2.000   0.7572   0.01105   0.00326  -0.0892   0.3276   0.3135
   2.250   0.7838   0.01114   0.00337  -0.0886   0.3194   0.3323
   2.500   0.8102   0.01127   0.00349  -0.0881   0.3115   0.3470
   2.750   0.8366   0.01139   0.00361  -0.0875   0.3024   0.3612
   3.250   0.8889   0.01168   0.00390  -0.0864   0.2857   0.3898
   3.500   0.9145   0.01185   0.00407  -0.0857   0.2778   0.4063
   3.750   0.9404   0.01200   0.00423  -0.0851   0.2699   0.4211
   4.000   0.9656   0.01221   0.00441  -0.0845   0.2622   0.4340
   4.250   0.9914   0.01236   0.00458  -0.0838   0.2554   0.4464
   4.500   1.0164   0.01257   0.00478  -0.0831   0.2484   0.4605
   4.750   1.0415   0.01275   0.00498  -0.0825   0.2425   0.4764
   5.000   1.0666   0.01292   0.00518  -0.0818   0.2367   0.4952
   5.500   1.1155   0.01331   0.00563  -0.0802   0.2267   0.5296
   6.000   1.1635   0.01365   0.00609  -0.0786   0.2173   0.5821
   6.250   1.1831   0.01359   0.00636  -0.0770   0.2133   0.7131
   6.750   1.2558   0.01380   0.00693  -0.0805   0.2047   1.0000
   7.000   1.2788   0.01411   0.00720  -0.0796   0.2005   1.0000
   7.250   1.3012   0.01444   0.00751  -0.0786   0.1968   1.0000
   7.500   1.3249   0.01468   0.00777  -0.0777   0.1939   1.0000
   7.750   1.3478   0.01496   0.00804  -0.0768   0.1902   1.0000
   8.000   1.3696   0.01529   0.00836  -0.0757   0.1863   1.0000
   8.250   1.3903   0.01567   0.00871  -0.0745   0.1825   1.0000
   8.500   1.4122   0.01596   0.00902  -0.0734   0.1794   1.0000
   8.750   1.4333   0.01628   0.00935  -0.0723   0.1753   1.0000
   9.000   1.4527   0.01667   0.00972  -0.0709   0.1708   1.0000
   9.250   1.4707   0.01708   0.01012  -0.0693   0.1668   1.0000
   9.500   1.4889   0.01742   0.01048  -0.0677   0.1633   1.0000
   9.750   1.5052   0.01781   0.01088  -0.0658   0.1594   1.0000
  10.000   1.5196   0.01829   0.01136  -0.0637   0.1558   1.0000
  10.250   1.5348   0.01876   0.01184  -0.0618   0.1527   1.0000
  10.500   1.5505   0.01922   0.01233  -0.0600   0.1495   1.0000
  10.750   1.5649   0.01975   0.01288  -0.0582   0.1461   1.0000
  11.000   1.5771   0.02042   0.01355  -0.0562   0.1425   1.0000
  11.250   1.5904   0.02106   0.01422  -0.0544   0.1394   1.0000
  11.500   1.6036   0.02174   0.01493  -0.0527   0.1363   1.0000
  11.750   1.6149   0.02256   0.01578  -0.0510   0.1329   1.0000
  12.000   1.6244   0.02354   0.01677  -0.0493   0.1300   1.0000
  12.250   1.6355   0.02448   0.01776  -0.0479   0.1276   1.0000
  12.500   1.6462   0.02550   0.01883  -0.0466   0.1249   1.0000
  12.750   1.6553   0.02670   0.02007  -0.0454   0.1222   1.0000
  13.000   1.6624   0.02812   0.02152  -0.0442   0.1196   1.0000
  13.250   1.6690   0.02966   0.02311  -0.0432   0.1172   1.0000
  13.500   1.6775   0.03110   0.02461  -0.0423   0.1151   1.0000
  13.750   1.6841   0.03276   0.02633  -0.0415   0.1127   1.0000
  14.000   1.6886   0.03467   0.02829  -0.0409   0.1103   1.0000
  14.250   1.6901   0.03691   0.03058  -0.0403   0.1080   1.0000
  14.500   1.6926   0.03914   0.03287  -0.0398   0.1061   1.0000
  14.750   1.6960   0.04132   0.03514  -0.0395   0.1042   1.0000
  15.000   1.6972   0.04377   0.03766  -0.0392   0.1024   1.0000
  15.250   1.6961   0.04655   0.04051  -0.0391   0.1005   1.0000
  15.500   1.6925   0.04970   0.04373  -0.0392   0.0987   1.0000
  15.750   1.6863   0.05326   0.04735  -0.0395   0.0971   1.0000
  16.000   1.6843   0.05640   0.05059  -0.0398   0.0957   1.0000
  16.250   1.6817   0.05968   0.05395  -0.0403   0.0940   1.0000
  16.500   1.6773   0.06323   0.05759  -0.0408   0.0926   1.0000
  16.750   1.6698   0.06723   0.06167  -0.0416   0.0907   1.0000
  17.000   1.6597   0.07167   0.06617  -0.0426   0.0889   1.0000
  17.250   1.6482   0.07635   0.07092  -0.0438   0.0873   1.0000
  17.500   1.6436   0.08013   0.07480  -0.0446   0.0858   1.0000
  17.750   1.6359   0.08443   0.07919  -0.0458   0.0841   1.0000
  18.000   1.6263   0.08905   0.08388  -0.0472   0.0824   1.0000
  18.250   1.6150   0.09399   0.08890  -0.0488   0.0808   1.0000
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