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GOE 565 AIRFOIL (goe565-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 565 AIRFOIL (goe565-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.08 at α=1.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe565-il-1000000.txt
Download as CSV file: xf-goe565-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 565 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.9191   0.03268   0.03018  -0.0716   1.0000   0.0085
 -11.750  -0.9307   0.02870   0.02589  -0.0698   1.0000   0.0086
 -11.500  -0.9345   0.02576   0.02267  -0.0673   1.0000   0.0088
 -11.250  -0.9288   0.02397   0.02071  -0.0650   1.0000   0.0091
 -11.000  -0.9181   0.02273   0.01935  -0.0630   1.0000   0.0093
 -10.750  -0.8986   0.02174   0.01826  -0.0625   0.9996   0.0096
 -10.500  -0.8693   0.02068   0.01706  -0.0638   0.9983   0.0100
 -10.250  -0.8403   0.01955   0.01578  -0.0651   0.9968   0.0104
 -10.000  -0.8110   0.01842   0.01447  -0.0663   0.9954   0.0107
  -9.750  -0.7806   0.01749   0.01338  -0.0675   0.9943   0.0110
  -9.500  -0.7539   0.01633   0.01203  -0.0681   0.9924   0.0114
  -9.250  -0.7272   0.01496   0.01048  -0.0687   0.9901   0.0122
  -9.000  -0.6971   0.01430   0.00974  -0.0696   0.9884   0.0128
  -8.750  -0.6660   0.01374   0.00911  -0.0706   0.9869   0.0136
  -8.500  -0.6344   0.01321   0.00848  -0.0716   0.9857   0.0143
  -8.250  -0.6030   0.01252   0.00767  -0.0727   0.9846   0.0152
  -8.000  -0.5706   0.01202   0.00715  -0.0739   0.9838   0.0168
  -7.750  -0.5401   0.01169   0.00678  -0.0746   0.9821   0.0181
  -7.500  -0.5121   0.01126   0.00629  -0.0747   0.9791   0.0194
  -7.250  -0.4810   0.01093   0.00597  -0.0755   0.9772   0.0216
  -7.000  -0.4484   0.01078   0.00579  -0.0766   0.9757   0.0235
  -6.750  -0.4158   0.01041   0.00540  -0.0777   0.9745   0.0258
  -6.500  -0.3816   0.01041   0.00544  -0.0790   0.9734   0.0279
  -6.250  -0.3475   0.01041   0.00544  -0.0803   0.9723   0.0298
  -6.000  -0.3144   0.01014   0.00512  -0.0814   0.9709   0.0314
  -5.750  -0.2863   0.00982   0.00480  -0.0816   0.9677   0.0335
  -5.500  -0.2572   0.00974   0.00473  -0.0818   0.9639   0.0352
  -5.250  -0.2263   0.00961   0.00458  -0.0823   0.9605   0.0369
  -5.000  -0.1950   0.00946   0.00440  -0.0829   0.9570   0.0381
  -4.750  -0.1674   0.00945   0.00437  -0.0827   0.9515   0.0388
  -4.500  -0.1425   0.00869   0.00354  -0.0821   0.9456   0.0413
  -4.250  -0.1142   0.00842   0.00325  -0.0821   0.9405   0.0432
  -4.000  -0.0885   0.00822   0.00304  -0.0815   0.9335   0.0449
  -3.750  -0.0609   0.00801   0.00279  -0.0813   0.9279   0.0464
  -3.500  -0.0344   0.00783   0.00257  -0.0809   0.9216   0.0476
  -3.250  -0.0074   0.00767   0.00237  -0.0805   0.9150   0.0486
  -3.000   0.0196   0.00756   0.00224  -0.0802   0.9075   0.0494
  -2.750   0.0458   0.00728   0.00188  -0.0797   0.8979   0.0516
  -2.500   0.0718   0.00707   0.00162  -0.0790   0.8857   0.0546
  -2.250   0.0982   0.00693   0.00145  -0.0786   0.8735   0.0574
  -2.000   0.1252   0.00682   0.00131  -0.0782   0.8628   0.0600
  -1.750   0.1522   0.00674   0.00117  -0.0778   0.8527   0.0630
  -1.500   0.1788   0.00657   0.00109  -0.0775   0.8414   0.0834
  -1.250   0.2053   0.00642   0.00100  -0.0771   0.8289   0.1165
  -1.000   0.2306   0.00610   0.00091  -0.0766   0.8143   0.2006
  -0.750   0.2564   0.00590   0.00088  -0.0761   0.8001   0.2750
  -0.500   0.2827   0.00581   0.00086  -0.0757   0.7858   0.3135
  -0.250   0.3087   0.00570   0.00084  -0.0752   0.7708   0.3606
   0.000   0.3335   0.00548   0.00084  -0.0746   0.7549   0.4589
   0.250   0.3581   0.00527   0.00088  -0.0739   0.7393   0.5630
   0.500   0.3831   0.00517   0.00092  -0.0732   0.7237   0.6322
   0.750   0.4080   0.00507   0.00095  -0.0725   0.7089   0.6952
   1.000   0.4284   0.00472   0.00100  -0.0707   0.6939   0.8305
   1.250   0.4862   0.00459   0.00108  -0.0771   0.6702   0.9852
   1.500   0.5262   0.00478   0.00111  -0.0798   0.6317   1.0000
   1.750   0.5478   0.00505   0.00116  -0.0784   0.5792   1.0000
   2.000   0.5690   0.00538   0.00126  -0.0770   0.5288   1.0000
   2.250   0.5917   0.00565   0.00136  -0.0758   0.4887   1.0000
   2.500   0.6150   0.00589   0.00146  -0.0749   0.4558   1.0000
   2.750   0.6381   0.00616   0.00157  -0.0739   0.4167   1.0000
   3.000   0.6608   0.00648   0.00170  -0.0728   0.3749   1.0000
   3.250   0.6838   0.00679   0.00186  -0.0718   0.3383   1.0000
   3.500   0.7071   0.00710   0.00201  -0.0709   0.3043   1.0000
   3.750   0.7304   0.00741   0.00217  -0.0700   0.2690   1.0000
   4.000   0.7531   0.00779   0.00236  -0.0690   0.2260   1.0000
   4.250   0.7753   0.00823   0.00260  -0.0680   0.1857   1.0000
   4.500   0.7994   0.00851   0.00280  -0.0672   0.1687   1.0000
   4.750   0.8238   0.00877   0.00300  -0.0666   0.1545   1.0000
   5.000   0.8483   0.00901   0.00320  -0.0659   0.1401   1.0000
   5.250   0.8707   0.00947   0.00345  -0.0649   0.1001   1.0000
   5.500   0.8896   0.01030   0.00395  -0.0634   0.0454   1.0000
   5.750   0.9130   0.01068   0.00428  -0.0625   0.0369   1.0000
   6.000   0.9372   0.01097   0.00459  -0.0618   0.0346   1.0000
   6.250   0.9608   0.01133   0.00496  -0.0610   0.0320   1.0000
   6.500   0.9833   0.01181   0.00548  -0.0600   0.0288   1.0000
   6.750   1.0076   0.01208   0.00577  -0.0594   0.0278   1.0000
   7.000   1.0315   0.01238   0.00611  -0.0586   0.0263   1.0000
   7.250   1.0548   0.01274   0.00649  -0.0578   0.0247   1.0000
   7.500   1.0759   0.01333   0.00710  -0.0567   0.0224   1.0000
   7.750   1.0983   0.01375   0.00757  -0.0557   0.0211   1.0000
   8.000   1.1223   0.01402   0.00785  -0.0551   0.0200   1.0000
   8.250   1.1453   0.01435   0.00821  -0.0543   0.0186   1.0000
   8.500   1.1669   0.01483   0.00869  -0.0533   0.0174   1.0000
   8.750   1.1855   0.01558   0.00951  -0.0518   0.0162   1.0000
   9.000   1.2082   0.01590   0.00986  -0.0509   0.0154   1.0000
   9.250   1.2304   0.01625   0.01024  -0.0501   0.0145   1.0000
   9.500   1.2517   0.01667   0.01069  -0.0490   0.0138   1.0000
   9.750   1.2703   0.01730   0.01133  -0.0476   0.0128   1.0000
  10.000   1.2856   0.01819   0.01231  -0.0457   0.0121   1.0000
  10.250   1.3048   0.01871   0.01289  -0.0444   0.0118   1.0000
  10.500   1.3229   0.01928   0.01352  -0.0429   0.0113   1.0000
  10.750   1.3396   0.01992   0.01423  -0.0412   0.0109   1.0000
  11.000   1.3560   0.02047   0.01482  -0.0395   0.0104   1.0000
  11.250   1.3697   0.02108   0.01547  -0.0373   0.0101   1.0000
  11.500   1.3791   0.02192   0.01637  -0.0346   0.0097   1.0000
  11.750   1.3774   0.02352   0.01810  -0.0303   0.0092   1.0000
  12.000   1.3853   0.02453   0.01922  -0.0277   0.0090   1.0000
  12.250   1.3964   0.02534   0.02011  -0.0256   0.0088   1.0000
  12.500   1.4059   0.02626   0.02112  -0.0235   0.0087   1.0000
  12.750   1.4150   0.02725   0.02221  -0.0214   0.0084   1.0000
  13.000   1.4226   0.02838   0.02342  -0.0194   0.0081   1.0000
  13.250   1.4283   0.02968   0.02482  -0.0173   0.0080   1.0000
  13.500   1.4320   0.03121   0.02645  -0.0153   0.0078   1.0000
  13.750   1.4376   0.03263   0.02796  -0.0137   0.0076   1.0000
  14.000   1.4418   0.03424   0.02965  -0.0122   0.0074   1.0000
  14.250   1.4442   0.03610   0.03159  -0.0109   0.0073   1.0000
  14.500   1.4429   0.03842   0.03402  -0.0098   0.0071   1.0000
  14.750   1.4377   0.04134   0.03707  -0.0089   0.0071   1.0000
  15.000   1.4294   0.04477   0.04062  -0.0084   0.0069   1.0000
  15.250   1.4174   0.04893   0.04494  -0.0086   0.0068   1.0000
  15.500   1.4005   0.05405   0.05024  -0.0094   0.0067   1.0000
  15.750   1.3898   0.05877   0.05511  -0.0108   0.0067   1.0000
  16.000   1.3703   0.06514   0.06167  -0.0132   0.0067   1.0000
  16.250   1.3466   0.07273   0.06945  -0.0167   0.0066   1.0000
  16.500   1.3313   0.07934   0.07622  -0.0200   0.0066   1.0000
  16.750   1.3232   0.08506   0.08205  -0.0231   0.0065   1.0000
  17.000   1.3014   0.09346   0.09062  -0.0277   0.0065   1.0000
  17.250   1.2803   0.10209   0.09940  -0.0326   0.0065   1.0000
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