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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 500,000
Max Cl/Cd: 92.12 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-500000.txt
Download as CSV file: xf-rhodesg32-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 32                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.3313   0.10072   0.09834  -0.0391   1.0000   0.0390
 -11.750  -0.3312   0.09772   0.09537  -0.0397   1.0000   0.0404
 -11.500  -0.3696   0.08916   0.08688  -0.0471   1.0000   0.0424
 -11.250  -0.2441   0.07826   0.07609  -0.0518   0.9871   0.0438
 -11.000  -0.3629   0.08201   0.07978  -0.0490   0.9972   0.0431
 -10.750  -0.3421   0.07977   0.07753  -0.0511   0.9923   0.0436
 -10.500  -0.2606   0.05441   0.05222  -0.0777   0.9700   0.0492
 -10.250  -0.3018   0.03799   0.03553  -0.0932   0.9559   0.0498
 -10.000  -0.2720   0.03846   0.03608  -0.0921   0.9488   0.0503
  -9.750  -0.2523   0.03639   0.03397  -0.0935   0.9406   0.0508
  -9.500  -0.3121   0.03626   0.03297  -0.1005   0.9408   0.0481
  -9.250  -0.3076   0.03138   0.02770  -0.1001   0.9289   0.0476
  -9.000  -0.2995   0.02737   0.02321  -0.0989   0.9187   0.0473
  -8.750  -0.2844   0.02478   0.02022  -0.0976   0.9098   0.0477
  -8.500  -0.2664   0.02345   0.01854  -0.0961   0.9008   0.0487
  -8.250  -0.2451   0.02273   0.01747  -0.0948   0.8929   0.0494
  -8.000  -0.2284   0.02015   0.01461  -0.0934   0.8846   0.0498
  -7.750  -0.2061   0.01865   0.01296  -0.0926   0.8771   0.0505
  -7.500  -0.1821   0.01803   0.01235  -0.0919   0.8685   0.0515
  -7.250  -0.1573   0.01739   0.01162  -0.0912   0.8601   0.0524
  -7.000  -0.1335   0.01664   0.01076  -0.0903   0.8508   0.0531
  -6.750  -0.1085   0.01589   0.00985  -0.0895   0.8425   0.0537
  -6.500  -0.0839   0.01523   0.00908  -0.0887   0.8321   0.0545
  -6.250  -0.0585   0.01466   0.00837  -0.0879   0.8223   0.0553
  -6.000  -0.0328   0.01427   0.00787  -0.0872   0.8117   0.0562
  -5.750  -0.0071   0.01393   0.00741  -0.0865   0.8002   0.0569
  -5.500   0.0188   0.01367   0.00704  -0.0857   0.7876   0.0574
  -5.250   0.0433   0.01253   0.00581  -0.0850   0.7740   0.0584
  -5.000   0.0680   0.01196   0.00519  -0.0842   0.7579   0.0594
  -4.750   0.0930   0.01161   0.00478  -0.0834   0.7409   0.0605
  -4.500   0.1181   0.01136   0.00448  -0.0826   0.7237   0.0620
  -4.250   0.1430   0.01113   0.00417  -0.0818   0.7051   0.0633
  -4.000   0.1676   0.01094   0.00388  -0.0809   0.6847   0.0643
  -3.500   0.2159   0.01071   0.00343  -0.0790   0.6362   0.0664
  -3.250   0.2389   0.01065   0.00321  -0.0778   0.6040   0.0673
  -3.000   0.2594   0.01051   0.00288  -0.0763   0.5557   0.0696
  -2.750   0.2758   0.01086   0.00280  -0.0740   0.4556   0.0717
  -2.500   0.2960   0.01113   0.00280  -0.0725   0.4026   0.0736
  -2.250   0.3196   0.01122   0.00276  -0.0716   0.3839   0.0757
  -2.000   0.3445   0.01125   0.00271  -0.0710   0.3738   0.0778
  -1.750   0.3690   0.01125   0.00266  -0.0702   0.3664   0.0822
  -1.500   0.3944   0.01121   0.00263  -0.0697   0.3614   0.0891
  -1.250   0.4189   0.01110   0.00270  -0.0690   0.3570   0.1454
  -1.000   0.4431   0.01105   0.00276  -0.0683   0.3531   0.1906
  -0.750   0.4650   0.01073   0.00285  -0.0673   0.3499   0.3372
  -0.500   0.4816   0.00993   0.00295  -0.0653   0.3475   0.6282
  -0.250   0.5391   0.00936   0.00326  -0.0712   0.3433   0.9585
   0.000   0.6002   0.00961   0.00341  -0.0784   0.3389   0.9923
   0.250   0.6436   0.00986   0.00355  -0.0819   0.3352   1.0000
   0.500   0.6655   0.01002   0.00367  -0.0807   0.3331   1.0000
   0.750   0.6884   0.01013   0.00376  -0.0797   0.3318   1.0000
   1.000   0.7114   0.01024   0.00386  -0.0787   0.3299   1.0000
   1.250   0.7344   0.01037   0.00396  -0.0777   0.3276   1.0000
   1.500   0.7573   0.01051   0.00408  -0.0768   0.3256   1.0000
   1.750   0.7804   0.01066   0.00421  -0.0758   0.3239   1.0000
   2.000   0.8033   0.01083   0.00435  -0.0749   0.3220   1.0000
   2.250   0.8263   0.01103   0.00452  -0.0740   0.3204   1.0000
   2.500   0.8492   0.01127   0.00472  -0.0731   0.3184   1.0000
   2.750   0.8726   0.01150   0.00493  -0.0723   0.3165   1.0000
   3.000   0.8965   0.01163   0.00508  -0.0716   0.3153   1.0000
   3.250   0.9202   0.01175   0.00523  -0.0708   0.3137   1.0000
   3.500   0.9437   0.01186   0.00535  -0.0701   0.3110   1.0000
   3.750   0.9670   0.01198   0.00549  -0.0693   0.3080   1.0000
   4.000   0.9902   0.01213   0.00564  -0.0685   0.3053   1.0000
   4.250   1.0132   0.01236   0.00584  -0.0677   0.3027   1.0000
   4.500   1.0365   0.01265   0.00611  -0.0670   0.2999   1.0000
   4.750   1.0599   0.01272   0.00625  -0.0663   0.2981   1.0000
   5.000   1.0831   0.01281   0.00639  -0.0655   0.2952   1.0000
   5.250   1.1061   0.01291   0.00653  -0.0647   0.2919   1.0000
   5.500   1.1286   0.01304   0.00667  -0.0639   0.2884   1.0000
   5.750   1.1502   0.01330   0.00690  -0.0630   0.2842   1.0000
   6.000   1.1732   0.01333   0.00703  -0.0622   0.2807   1.0000
   6.250   1.1959   0.01341   0.00717  -0.0614   0.2765   1.0000
   6.500   1.2173   0.01354   0.00731  -0.0604   0.2714   1.0000
   6.750   1.2387   0.01367   0.00748  -0.0594   0.2657   1.0000
   7.000   1.2605   0.01376   0.00763  -0.0585   0.2577   1.0000
   7.250   1.2804   0.01390   0.00778  -0.0573   0.2467   1.0000
   7.500   1.2955   0.01418   0.00793  -0.0552   0.2123   1.0000
   7.750   1.2942   0.01542   0.00877  -0.0508   0.1584   1.0000
   8.000   1.3035   0.01624   0.00952  -0.0481   0.1442   1.0000
   8.250   1.3167   0.01686   0.01013  -0.0461   0.1346   1.0000
   8.500   1.3299   0.01750   0.01077  -0.0442   0.1244   1.0000
   8.750   1.3422   0.01820   0.01144  -0.0423   0.1130   1.0000
   9.000   1.3524   0.01905   0.01221  -0.0401   0.0933   1.0000
   9.250   1.3540   0.02042   0.01334  -0.0371   0.0648   1.0000
   9.500   1.3602   0.02153   0.01444  -0.0348   0.0581   1.0000
   9.750   1.3653   0.02275   0.01568  -0.0325   0.0543   1.0000
  10.000   1.3719   0.02393   0.01692  -0.0305   0.0515   1.0000
  10.250   1.3798   0.02506   0.01813  -0.0288   0.0495   1.0000
  10.500   1.3845   0.02646   0.01960  -0.0270   0.0475   1.0000
  10.750   1.3841   0.02830   0.02149  -0.0250   0.0455   1.0000
  11.000   1.3861   0.03007   0.02335  -0.0234   0.0439   1.0000
  11.250   1.3934   0.03151   0.02488  -0.0224   0.0424   1.0000
  11.500   1.3974   0.03329   0.02673  -0.0213   0.0408   1.0000
  11.750   1.3975   0.03549   0.02901  -0.0203   0.0395   1.0000
  12.000   1.3919   0.03836   0.03196  -0.0194   0.0384   1.0000
  12.250   1.3861   0.04143   0.03513  -0.0188   0.0372   1.0000
  12.500   1.3911   0.04354   0.03734  -0.0186   0.0361   1.0000
  12.750   1.3917   0.04618   0.04007  -0.0185   0.0349   1.0000
  13.000   1.3893   0.04926   0.04324  -0.0186   0.0340   1.0000
  13.250   1.3847   0.05274   0.04678  -0.0189   0.0329   1.0000
  13.500   1.3736   0.05712   0.05124  -0.0194   0.0321   1.0000
  13.750   1.3659   0.06123   0.05545  -0.0201   0.0313   1.0000
  14.000   1.3646   0.06466   0.05899  -0.0209   0.0304   1.0000
  14.250   1.3608   0.06847   0.06291  -0.0218   0.0295   1.0000
  14.500   1.3552   0.07258   0.06710  -0.0228   0.0288   1.0000
  14.750   1.3501   0.07670   0.07129  -0.0239   0.0282   1.0000
  15.000   1.3434   0.08105   0.07571  -0.0251   0.0276   1.0000
  15.250   1.3331   0.08579   0.08049  -0.0263   0.0269   1.0000
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