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GOE 599 AIRFOIL (goe599-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 599 AIRFOIL (goe599-il)
Reynolds number: 500,000
Max Cl/Cd: 65.47 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe599-il-500000-n5.txt
Download as CSV file: xf-goe599-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.8520   0.07313   0.07055  -0.0339   1.0000   0.0056
 -13.000  -0.9066   0.05575   0.05283  -0.0469   1.0000   0.0054
 -12.750  -0.9277   0.04682   0.04366  -0.0552   1.0000   0.0054
 -12.500  -0.9426   0.04111   0.03773  -0.0598   1.0000   0.0054
 -12.250  -0.9556   0.03753   0.03396  -0.0602   1.0000   0.0054
 -12.000  -0.9663   0.03518   0.03144  -0.0578   1.0000   0.0055
 -11.750  -0.9677   0.03313   0.02923  -0.0557   1.0000   0.0056
 -11.500  -0.9646   0.03143   0.02737  -0.0535   1.0000   0.0057
 -11.250  -0.9586   0.02989   0.02568  -0.0514   1.0000   0.0058
 -11.000  -0.9504   0.02846   0.02410  -0.0494   1.0000   0.0059
 -10.750  -0.9405   0.02710   0.02257  -0.0474   1.0000   0.0060
 -10.500  -0.9291   0.02581   0.02112  -0.0455   1.0000   0.0062
 -10.250  -0.9164   0.02455   0.01969  -0.0436   1.0000   0.0064
 -10.000  -0.9025   0.02335   0.01831  -0.0419   1.0000   0.0066
  -9.750  -0.8873   0.02223   0.01702  -0.0402   1.0000   0.0069
  -9.500  -0.8706   0.02127   0.01590  -0.0387   1.0000   0.0071
  -9.250  -0.8525   0.02044   0.01492  -0.0374   1.0000   0.0074
  -9.000  -0.8334   0.01926   0.01360  -0.0364   0.9997   0.0078
  -8.750  -0.8057   0.01833   0.01257  -0.0372   0.9983   0.0083
  -8.500  -0.7767   0.01757   0.01172  -0.0380   0.9969   0.0087
  -8.250  -0.7470   0.01683   0.01085  -0.0390   0.9955   0.0092
  -8.000  -0.7172   0.01610   0.01002  -0.0399   0.9942   0.0098
  -7.750  -0.6884   0.01545   0.00925  -0.0405   0.9923   0.0104
  -7.500  -0.6591   0.01470   0.00841  -0.0413   0.9903   0.0113
  -7.250  -0.6283   0.01416   0.00784  -0.0423   0.9885   0.0126
  -7.000  -0.5965   0.01372   0.00734  -0.0435   0.9870   0.0139
  -6.750  -0.5640   0.01327   0.00679  -0.0448   0.9858   0.0152
  -6.500  -0.5353   0.01273   0.00623  -0.0453   0.9829   0.0174
  -6.250  -0.5043   0.01239   0.00588  -0.0462   0.9804   0.0203
  -6.000  -0.4716   0.01211   0.00555  -0.0475   0.9784   0.0226
  -5.750  -0.4387   0.01165   0.00509  -0.0488   0.9768   0.0265
  -5.500  -0.4045   0.01136   0.00475  -0.0504   0.9754   0.0301
  -5.250  -0.3761   0.01112   0.00446  -0.0506   0.9711   0.0323
  -5.000  -0.3452   0.01073   0.00406  -0.0515   0.9677   0.0369
  -4.750  -0.3128   0.01044   0.00375  -0.0526   0.9650   0.0411
  -4.500  -0.2830   0.01014   0.00344  -0.0531   0.9609   0.0481
  -4.250  -0.2549   0.00976   0.00317  -0.0533   0.9554   0.0698
  -4.000  -0.2239   0.00946   0.00296  -0.0542   0.9513   0.0981
  -3.750  -0.1959   0.00929   0.00277  -0.0542   0.9446   0.1083
  -3.500  -0.1663   0.00907   0.00256  -0.0546   0.9382   0.1177
  -3.250  -0.1379   0.00883   0.00237  -0.0548   0.9305   0.1318
  -3.000  -0.1094   0.00847   0.00216  -0.0551   0.9222   0.1770
  -2.750  -0.0820   0.00813   0.00201  -0.0552   0.9116   0.2333
  -2.500  -0.0536   0.00787   0.00187  -0.0553   0.8997   0.2723
  -2.250  -0.0250   0.00766   0.00169  -0.0554   0.8816   0.3016
  -2.000   0.0025   0.00750   0.00153  -0.0552   0.8563   0.3354
  -1.750   0.0289   0.00731   0.00142  -0.0549   0.8344   0.3882
  -1.500   0.0557   0.00713   0.00136  -0.0548   0.8215   0.4439
  -1.250   0.0830   0.00701   0.00133  -0.0547   0.8113   0.4829
  -1.000   0.1105   0.00694   0.00132  -0.0546   0.8017   0.5166
  -0.750   0.1380   0.00689   0.00131  -0.0546   0.7926   0.5464
  -0.500   0.1653   0.00685   0.00131  -0.0544   0.7787   0.5740
  -0.250   0.1918   0.00683   0.00130  -0.0541   0.7559   0.6020
   0.000   0.2177   0.00686   0.00128  -0.0536   0.7240   0.6261
   0.250   0.2441   0.00687   0.00128  -0.0532   0.6967   0.6523
   0.500   0.2701   0.00688   0.00129  -0.0528   0.6685   0.6802
   0.750   0.2955   0.00695   0.00133  -0.0522   0.6325   0.7103
   1.000   0.3200   0.00708   0.00138  -0.0515   0.5879   0.7432
   1.250   0.3429   0.00728   0.00149  -0.0505   0.5268   0.7860
   1.500   0.3640   0.00754   0.00164  -0.0490   0.4570   0.8407
   1.750   0.3846   0.00778   0.00182  -0.0472   0.3987   0.9070
   2.000   0.4159   0.00811   0.00200  -0.0479   0.3456   0.9633
   2.250   0.4526   0.00864   0.00220  -0.0503   0.2686   0.9888
   2.500   0.4837   0.00959   0.00256  -0.0517   0.1336   1.0000
   2.750   0.5052   0.01012   0.00281  -0.0507   0.0682   1.0000
   3.000   0.5299   0.01033   0.00298  -0.0501   0.0625   1.0000
   3.250   0.5549   0.01054   0.00317  -0.0496   0.0589   1.0000
   3.500   0.5801   0.01076   0.00339  -0.0491   0.0560   1.0000
   3.750   0.6052   0.01101   0.00365  -0.0486   0.0536   1.0000
   4.000   0.6307   0.01123   0.00388  -0.0482   0.0524   1.0000
   4.250   0.6563   0.01145   0.00412  -0.0479   0.0514   1.0000
   4.500   0.6817   0.01169   0.00440  -0.0475   0.0504   1.0000
   4.750   0.7069   0.01197   0.00470  -0.0470   0.0494   1.0000
   5.000   0.7320   0.01226   0.00503  -0.0466   0.0485   1.0000
   5.250   0.7569   0.01258   0.00539  -0.0461   0.0475   1.0000
   5.500   0.7817   0.01291   0.00576  -0.0456   0.0465   1.0000
   5.750   0.8064   0.01324   0.00610  -0.0452   0.0446   1.0000
   6.000   0.8296   0.01373   0.00660  -0.0445   0.0417   1.0000
   6.250   0.8544   0.01404   0.00694  -0.0440   0.0403   1.0000
   6.500   0.8801   0.01423   0.00719  -0.0438   0.0390   1.0000
   6.750   0.9058   0.01442   0.00741  -0.0435   0.0368   1.0000
   7.000   0.9314   0.01462   0.00763  -0.0432   0.0344   1.0000
   7.250   0.9560   0.01493   0.00791  -0.0428   0.0318   1.0000
   7.500   0.9815   0.01511   0.00816  -0.0425   0.0284   1.0000
   7.750   1.0063   0.01537   0.00839  -0.0422   0.0216   1.0000
   8.000   1.0290   0.01586   0.00882  -0.0415   0.0158   1.0000
   8.250   1.0504   0.01649   0.00945  -0.0405   0.0130   1.0000
   8.500   1.0720   0.01709   0.01012  -0.0395   0.0116   1.0000
   8.750   1.0933   0.01769   0.01081  -0.0386   0.0105   1.0000
   9.000   1.1138   0.01837   0.01155  -0.0375   0.0096   1.0000
   9.250   1.1330   0.01918   0.01242  -0.0363   0.0087   1.0000
   9.500   1.1520   0.01998   0.01333  -0.0350   0.0081   1.0000
   9.750   1.1714   0.02070   0.01418  -0.0339   0.0078   1.0000
  10.000   1.1898   0.02149   0.01508  -0.0326   0.0074   1.0000
  10.250   1.2074   0.02233   0.01602  -0.0312   0.0070   1.0000
  10.500   1.2241   0.02322   0.01701  -0.0297   0.0067   1.0000
  10.750   1.2398   0.02414   0.01803  -0.0281   0.0065   1.0000
  11.000   1.2536   0.02513   0.01912  -0.0263   0.0062   1.0000
  11.250   1.2628   0.02631   0.02040  -0.0237   0.0059   1.0000
  11.500   1.2688   0.02774   0.02196  -0.0209   0.0057   1.0000
  11.750   1.2793   0.02882   0.02318  -0.0188   0.0055   1.0000
  12.000   1.2885   0.03002   0.02455  -0.0167   0.0053   1.0000
  12.250   1.2954   0.03142   0.02609  -0.0145   0.0052   1.0000
  12.500   1.3006   0.03298   0.02781  -0.0123   0.0050   1.0000
  12.750   1.3042   0.03473   0.02971  -0.0103   0.0049   1.0000
  13.000   1.3062   0.03667   0.03181  -0.0084   0.0048   1.0000
  13.250   1.3065   0.03886   0.03417  -0.0068   0.0047   1.0000
  13.500   1.3057   0.04129   0.03676  -0.0055   0.0046   1.0000
  13.750   1.3030   0.04403   0.03967  -0.0046   0.0045   1.0000
  14.000   1.2986   0.04716   0.04296  -0.0042   0.0045   1.0000
  14.250   1.2920   0.05072   0.04669  -0.0042   0.0044   1.0000
  14.500   1.2836   0.05479   0.05093  -0.0049   0.0044   1.0000
  14.750   1.2725   0.05954   0.05585  -0.0062   0.0043   1.0000
  15.000   1.2586   0.06512   0.06161  -0.0085   0.0043   1.0000
  15.250   1.2411   0.07180   0.06848  -0.0117   0.0043   1.0000
  15.500   1.2200   0.07968   0.07655  -0.0160   0.0043   1.0000
  15.750   1.1936   0.08925   0.08632  -0.0214   0.0044   1.0000
  16.000   1.1589   0.10114   0.09843  -0.0282   0.0044   1.0000
  16.250   1.1106   0.11714   0.11466  -0.0369   0.0046   1.0000
  16.500   1.0250   0.14400   0.14176  -0.0502   0.0050   1.0000
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