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GOE 599 AIRFOIL (goe599-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 599 AIRFOIL (goe599-il)
Reynolds number: 1,000,000
Max Cl/Cd: 79.78 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe599-il-1000000.txt
Download as CSV file: xf-goe599-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 599 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.8638   0.07023   0.06833  -0.0356   1.0000   0.0078
 -13.000  -0.9163   0.05300   0.05082  -0.0499   1.0000   0.0076
 -12.750  -0.9429   0.04371   0.04127  -0.0587   1.0000   0.0075
 -12.500  -0.9614   0.03848   0.03582  -0.0619   1.0000   0.0075
 -12.250  -0.9772   0.03544   0.03259  -0.0603   1.0000   0.0076
 -12.000  -0.9859   0.03314   0.03011  -0.0574   1.0000   0.0076
 -11.750  -0.9892   0.03099   0.02777  -0.0546   1.0000   0.0077
 -11.500  -0.9880   0.02913   0.02572  -0.0518   1.0000   0.0079
 -11.250  -0.9840   0.02741   0.02381  -0.0491   1.0000   0.0080
 -11.000  -0.9768   0.02588   0.02209  -0.0466   1.0000   0.0081
 -10.750  -0.9667   0.02453   0.02058  -0.0444   1.0000   0.0083
 -10.500  -0.9540   0.02339   0.01928  -0.0424   1.0000   0.0084
 -10.250  -0.9388   0.02247   0.01822  -0.0406   1.0000   0.0086
 -10.000  -0.9291   0.02050   0.01600  -0.0383   1.0000   0.0088
  -9.750  -0.9169   0.01877   0.01408  -0.0363   1.0000   0.0092
  -9.500  -0.8983   0.01805   0.01330  -0.0350   1.0000   0.0096
  -9.250  -0.8780   0.01756   0.01275  -0.0339   1.0000   0.0099
  -9.000  -0.8574   0.01709   0.01223  -0.0329   1.0000   0.0103
  -8.750  -0.8357   0.01655   0.01162  -0.0320   0.9999   0.0108
  -8.500  -0.8050   0.01589   0.01087  -0.0331   0.9990   0.0112
  -8.250  -0.7737   0.01531   0.01020  -0.0342   0.9979   0.0116
  -8.000  -0.7447   0.01402   0.00876  -0.0351   0.9967   0.0123
  -7.750  -0.7127   0.01341   0.00810  -0.0364   0.9956   0.0131
  -7.500  -0.6795   0.01302   0.00768  -0.0379   0.9947   0.0139
  -7.250  -0.6471   0.01262   0.00723  -0.0392   0.9936   0.0148
  -7.000  -0.6157   0.01233   0.00690  -0.0401   0.9918   0.0155
  -6.750  -0.5849   0.01155   0.00607  -0.0411   0.9900   0.0171
  -6.500  -0.5517   0.01125   0.00577  -0.0425   0.9884   0.0184
  -6.250  -0.5177   0.01097   0.00546  -0.0440   0.9870   0.0198
  -6.000  -0.4837   0.01050   0.00493  -0.0456   0.9858   0.0216
  -5.750  -0.4489   0.01014   0.00459  -0.0473   0.9848   0.0242
  -5.500  -0.4132   0.00993   0.00436  -0.0492   0.9839   0.0264
  -5.250  -0.3807   0.00950   0.00390  -0.0503   0.9821   0.0293
  -5.000  -0.3499   0.00918   0.00357  -0.0511   0.9790   0.0326
  -4.750  -0.3158   0.00896   0.00333  -0.0526   0.9770   0.0351
  -4.500  -0.2818   0.00861   0.00297  -0.0540   0.9750   0.0404
  -4.250  -0.2480   0.00833   0.00269  -0.0554   0.9730   0.0462
  -4.000  -0.2155   0.00785   0.00245  -0.0566   0.9708   0.0947
  -3.750  -0.1888   0.00764   0.00228  -0.0563   0.9648   0.1099
  -3.500  -0.1594   0.00740   0.00208  -0.0566   0.9598   0.1228
  -3.250  -0.1318   0.00704   0.00187  -0.0567   0.9536   0.1615
  -3.000  -0.1060   0.00664   0.00168  -0.0563   0.9435   0.2257
  -2.750  -0.0800   0.00637   0.00152  -0.0558   0.9291   0.2644
  -2.500  -0.0536   0.00615   0.00138  -0.0554   0.9123   0.3008
  -2.250  -0.0266   0.00594   0.00126  -0.0552   0.8960   0.3403
  -2.000   0.0001   0.00570   0.00116  -0.0550   0.8794   0.3981
  -1.750   0.0269   0.00550   0.00109  -0.0548   0.8634   0.4559
  -1.500   0.0540   0.00538   0.00105  -0.0547   0.8492   0.5022
  -1.250   0.0810   0.00529   0.00103  -0.0545   0.8340   0.5489
  -1.000   0.1080   0.00526   0.00101  -0.0543   0.8173   0.5820
  -0.750   0.1355   0.00523   0.00100  -0.0542   0.8034   0.6080
  -0.500   0.1628   0.00519   0.00100  -0.0540   0.7895   0.6393
  -0.250   0.1900   0.00514   0.00101  -0.0538   0.7739   0.6707
   0.000   0.2173   0.00509   0.00101  -0.0537   0.7600   0.7020
   0.250   0.2445   0.00503   0.00103  -0.0535   0.7463   0.7360
   0.500   0.2713   0.00499   0.00105  -0.0532   0.7286   0.7734
   0.750   0.2973   0.00495   0.00108  -0.0527   0.7071   0.8125
   1.000   0.3224   0.00497   0.00112  -0.0520   0.6755   0.8528
   1.250   0.3459   0.00507   0.00117  -0.0509   0.6316   0.8924
   1.500   0.3684   0.00528   0.00126  -0.0495   0.5788   0.9289
   1.750   0.3930   0.00563   0.00138  -0.0488   0.5068   0.9604
   2.000   0.4229   0.00611   0.00153  -0.0494   0.4246   0.9793
   2.250   0.4558   0.00660   0.00170  -0.0509   0.3490   0.9906
   2.500   0.4895   0.00775   0.00207  -0.0530   0.1658   0.9987
   2.750   0.5130   0.00847   0.00236  -0.0524   0.0702   1.0000
   3.000   0.5369   0.00869   0.00253  -0.0517   0.0612   1.0000
   3.250   0.5617   0.00887   0.00270  -0.0510   0.0586   1.0000
   3.500   0.5869   0.00904   0.00288  -0.0505   0.0572   1.0000
   3.750   0.6124   0.00922   0.00307  -0.0501   0.0555   1.0000
   4.000   0.6379   0.00944   0.00330  -0.0496   0.0538   1.0000
   4.250   0.6634   0.00968   0.00354  -0.0492   0.0521   1.0000
   4.500   0.6887   0.00997   0.00384  -0.0487   0.0502   1.0000
   4.750   0.7131   0.01038   0.00429  -0.0481   0.0480   1.0000
   5.000   0.7378   0.01074   0.00469  -0.0476   0.0465   1.0000
   5.250   0.7648   0.01083   0.00477  -0.0475   0.0454   1.0000
   5.500   0.7908   0.01104   0.00500  -0.0472   0.0442   1.0000
   5.750   0.8166   0.01127   0.00525  -0.0469   0.0428   1.0000
   6.000   0.8426   0.01148   0.00546  -0.0467   0.0410   1.0000
   6.250   0.8682   0.01173   0.00571  -0.0464   0.0392   1.0000
   6.500   0.8899   0.01243   0.00645  -0.0454   0.0364   1.0000
   6.750   0.9175   0.01244   0.00647  -0.0454   0.0356   1.0000
   7.000   0.9452   0.01244   0.00647  -0.0455   0.0339   1.0000
   7.250   0.9724   0.01248   0.00647  -0.0455   0.0313   1.0000
   7.500   0.9980   0.01271   0.00666  -0.0452   0.0277   1.0000
   7.750   1.0244   0.01284   0.00675  -0.0451   0.0236   1.0000
   8.000   1.0486   0.01322   0.00709  -0.0446   0.0193   1.0000
   8.250   1.0714   0.01373   0.00759  -0.0438   0.0163   1.0000
   8.500   1.0948   0.01417   0.00806  -0.0431   0.0148   1.0000
   8.750   1.1168   0.01474   0.00865  -0.0423   0.0133   1.0000
   9.000   1.1376   0.01544   0.00943  -0.0412   0.0123   1.0000
   9.250   1.1599   0.01594   0.01000  -0.0403   0.0118   1.0000
   9.500   1.1815   0.01651   0.01062  -0.0394   0.0111   1.0000
   9.750   1.2024   0.01712   0.01128  -0.0384   0.0106   1.0000
  10.000   1.2215   0.01790   0.01212  -0.0371   0.0100   1.0000
  10.250   1.2338   0.01935   0.01371  -0.0348   0.0093   1.0000
  10.500   1.2543   0.01991   0.01436  -0.0338   0.0091   1.0000
  10.750   1.2737   0.02055   0.01507  -0.0326   0.0088   1.0000
  11.000   1.2919   0.02126   0.01587  -0.0313   0.0085   1.0000
  11.250   1.3092   0.02202   0.01670  -0.0299   0.0082   1.0000
  11.500   1.3249   0.02284   0.01761  -0.0283   0.0079   1.0000
  11.750   1.3381   0.02370   0.01855  -0.0262   0.0076   1.0000
  12.000   1.3490   0.02463   0.01956  -0.0239   0.0074   1.0000
  12.250   1.3567   0.02581   0.02083  -0.0212   0.0072   1.0000
  12.500   1.3582   0.02752   0.02270  -0.0179   0.0070   1.0000
  12.750   1.3505   0.03011   0.02552  -0.0140   0.0068   1.0000
  13.000   1.3537   0.03178   0.02734  -0.0116   0.0067   1.0000
  13.250   1.3600   0.03322   0.02889  -0.0098   0.0066   1.0000
  13.500   1.3637   0.03495   0.03076  -0.0080   0.0065   1.0000
  13.750   1.3652   0.03696   0.03291  -0.0064   0.0064   1.0000
  14.000   1.3652   0.03924   0.03534  -0.0051   0.0063   1.0000
  14.250   1.3622   0.04197   0.03823  -0.0041   0.0063   1.0000
  14.500   1.3579   0.04500   0.04141  -0.0035   0.0062   1.0000
  14.750   1.3503   0.04864   0.04520  -0.0034   0.0062   1.0000
  15.000   1.3411   0.05271   0.04944  -0.0039   0.0061   1.0000
  15.250   1.3303   0.05734   0.05423  -0.0051   0.0060   1.0000
  15.500   1.3149   0.06297   0.06003  -0.0071   0.0060   1.0000
  15.750   1.2987   0.06923   0.06646  -0.0100   0.0060   1.0000
  16.000   1.2758   0.07718   0.07459  -0.0142   0.0060   1.0000
  16.250   1.2502   0.08623   0.08381  -0.0192   0.0061   1.0000
  16.500   1.2192   0.09687   0.09464  -0.0253   0.0061   1.0000
  16.750   1.1804   0.10964   0.10758  -0.0324   0.0062   1.0000
  17.000   1.1274   0.12674   0.12489  -0.0416   0.0064   1.0000
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