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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 100,000
Max Cl/Cd: 48.26 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-100000-n5.txt
Download as CSV file: xf-rhodesg32-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3714   0.08957   0.08461  -0.0446   1.0000   0.0602
 -10.500  -0.3869   0.08714   0.08227  -0.0432   1.0000   0.0602
 -10.250  -0.4026   0.08527   0.08049  -0.0407   1.0000   0.0600
 -10.000  -0.4134   0.07922   0.07444  -0.0477   0.9926   0.0603
  -9.750  -0.4005   0.07202   0.06714  -0.0565   0.9833   0.0602
  -9.500  -0.3895   0.06585   0.06083  -0.0626   0.9739   0.0600
  -9.250  -0.3809   0.05904   0.05378  -0.0685   0.9638   0.0599
  -9.000  -0.3759   0.05123   0.04547  -0.0741   0.9538   0.0610
  -8.750  -0.3469   0.04977   0.04405  -0.0757   0.9476   0.0621
  -8.500  -0.3291   0.04498   0.03888  -0.0784   0.9395   0.0624
  -8.250  -0.3068   0.04111   0.03464  -0.0805   0.9320   0.0628
  -8.000  -0.2811   0.03849   0.03174  -0.0820   0.9253   0.0640
  -7.750  -0.2578   0.03608   0.02903  -0.0827   0.9171   0.0655
  -7.500  -0.2291   0.03330   0.02580  -0.0842   0.9117   0.0666
  -7.250  -0.2087   0.03118   0.02328  -0.0835   0.9020   0.0672
  -7.000  -0.1775   0.02907   0.02075  -0.0846   0.8965   0.0680
  -6.750  -0.1555   0.02768   0.01901  -0.0837   0.8866   0.0693
  -6.500  -0.1238   0.02632   0.01723  -0.0843   0.8806   0.0709
  -6.250  -0.1007   0.02521   0.01589  -0.0834   0.8708   0.0718
  -6.000  -0.0691   0.02389   0.01443  -0.0840   0.8643   0.0728
  -5.750  -0.0455   0.02301   0.01346  -0.0830   0.8536   0.0738
  -5.500  -0.0157   0.02211   0.01246  -0.0831   0.8456   0.0750
  -5.250   0.0096   0.02142   0.01171  -0.0824   0.8350   0.0770
  -5.000   0.0356   0.02077   0.01096  -0.0817   0.8242   0.0793
  -4.750   0.0650   0.02007   0.01014  -0.0815   0.8146   0.0812
  -4.500   0.0895   0.01951   0.00950  -0.0805   0.8017   0.0824
  -4.250   0.1144   0.01889   0.00887  -0.0795   0.7882   0.0840
  -4.000   0.1397   0.01834   0.00833  -0.0787   0.7750   0.0861
  -3.750   0.1658   0.01789   0.00788  -0.0781   0.7627   0.0896
  -3.500   0.1923   0.01750   0.00742  -0.0774   0.7499   0.0934
  -3.250   0.2170   0.01714   0.00706  -0.0765   0.7351   0.0970
  -3.000   0.2425   0.01682   0.00673  -0.0756   0.7192   0.1016
  -2.750   0.2683   0.01655   0.00642  -0.0748   0.7018   0.1082
  -2.500   0.2938   0.01631   0.00620  -0.0740   0.6826   0.1232
  -2.250   0.3189   0.01608   0.00597  -0.0732   0.6610   0.1539
  -2.000   0.3440   0.01579   0.00574  -0.0724   0.6373   0.1986
  -1.750   0.3685   0.01538   0.00559  -0.0717   0.6108   0.2983
  -1.500   0.3859   0.01439   0.00559  -0.0695   0.5824   0.6049
  -1.250   0.4789   0.01402   0.00559  -0.0814   0.5210   0.9925
  -1.000   0.5023   0.01434   0.00555  -0.0806   0.4854   1.0000
  -0.750   0.5217   0.01465   0.00557  -0.0789   0.4613   1.0000
  -0.500   0.5417   0.01496   0.00563  -0.0774   0.4446   1.0000
  -0.250   0.5625   0.01526   0.00571  -0.0761   0.4325   1.0000
   0.000   0.5838   0.01556   0.00582  -0.0748   0.4232   1.0000
   0.250   0.6060   0.01583   0.00596  -0.0738   0.4155   1.0000
   0.500   0.6284   0.01612   0.00611  -0.0728   0.4094   1.0000
   0.750   0.6513   0.01642   0.00627  -0.0718   0.4044   1.0000
   1.000   0.6749   0.01669   0.00647  -0.0711   0.3998   1.0000
   1.250   0.6987   0.01697   0.00667  -0.0704   0.3960   1.0000
   1.500   0.7228   0.01728   0.00690  -0.0697   0.3927   1.0000
   1.750   0.7475   0.01762   0.00713  -0.0692   0.3899   1.0000
   2.000   0.7724   0.01793   0.00739  -0.0687   0.3873   1.0000
   2.250   0.7974   0.01824   0.00770  -0.0683   0.3848   1.0000
   2.500   0.8224   0.01856   0.00801  -0.0679   0.3823   1.0000
   2.750   0.8474   0.01890   0.00833  -0.0674   0.3795   1.0000
   3.000   0.8721   0.01926   0.00866  -0.0670   0.3760   1.0000
   3.500   0.9209   0.02001   0.00937  -0.0661   0.3685   1.0000
   3.750   0.9445   0.02036   0.00977  -0.0655   0.3644   1.0000
   4.000   0.9688   0.02073   0.01016  -0.0651   0.3610   1.0000
   4.250   0.9938   0.02114   0.01056  -0.0648   0.3583   1.0000
   4.500   1.0194   0.02159   0.01099  -0.0646   0.3556   1.0000
   4.750   1.0429   0.02198   0.01149  -0.0641   0.3528   1.0000
   5.000   1.0662   0.02239   0.01200  -0.0635   0.3499   1.0000
   5.250   1.0901   0.02282   0.01255  -0.0631   0.3475   1.0000
   5.500   1.1140   0.02327   0.01308  -0.0627   0.3449   1.0000
   5.750   1.1379   0.02371   0.01356  -0.0623   0.3416   1.0000
   6.000   1.1623   0.02418   0.01401  -0.0620   0.3375   1.0000
   6.250   1.1799   0.02456   0.01462  -0.0605   0.3319   1.0000
   6.500   1.1999   0.02492   0.01506  -0.0595   0.3260   1.0000
   6.750   1.2223   0.02533   0.01544  -0.0588   0.3206   1.0000
   7.000   1.2377   0.02571   0.01609  -0.0571   0.3145   1.0000
   7.250   1.2559   0.02608   0.01655  -0.0558   0.3084   1.0000
   7.500   1.2748   0.02646   0.01697  -0.0546   0.3027   1.0000
   7.750   1.2877   0.02686   0.01762  -0.0525   0.2957   1.0000
   8.000   1.3035   0.02721   0.01809  -0.0508   0.2894   1.0000
   8.250   1.3167   0.02764   0.01870  -0.0489   0.2829   1.0000
   8.500   1.3273   0.02805   0.01929  -0.0465   0.2749   1.0000
   8.750   1.3349   0.02847   0.01989  -0.0436   0.2662   1.0000
   9.000   1.3410   0.02891   0.02046  -0.0406   0.2560   1.0000
   9.250   1.3473   0.02953   0.02133  -0.0379   0.2425   1.0000
   9.500   1.3536   0.03027   0.02227  -0.0355   0.2181   1.0000
   9.750   1.3503   0.03116   0.02298  -0.0322   0.1881   1.0000
  10.000   1.3411   0.03285   0.02442  -0.0288   0.1710   1.0000
  10.250   1.3327   0.03499   0.02648  -0.0261   0.1589   1.0000
  10.500   1.3230   0.03750   0.02896  -0.0238   0.1498   1.0000
  10.750   1.3175   0.03994   0.03150  -0.0222   0.1410   1.0000
  11.000   1.3067   0.04300   0.03460  -0.0207   0.1342   1.0000
  11.250   1.2995   0.04601   0.03777  -0.0198   0.1260   1.0000
  11.500   1.2853   0.04990   0.04174  -0.0193   0.1200   1.0000
  11.750   1.2753   0.05372   0.04574  -0.0192   0.1124   1.0000
  12.000   1.2591   0.05850   0.05060  -0.0197   0.1069   1.0000
  12.250   1.2458   0.06329   0.05555  -0.0206   0.1007   1.0000
  12.500   1.2302   0.06866   0.06101  -0.0219   0.0948   1.0000
  12.750   1.2175   0.07383   0.06628  -0.0233   0.0891   1.0000
  13.000   1.2057   0.07902   0.07154  -0.0248   0.0834   1.0000
  13.250   1.1962   0.08389   0.07645  -0.0263   0.0788   1.0000
  13.500   1.1879   0.08862   0.08120  -0.0277   0.0744   1.0000
  13.750   1.1807   0.09317   0.08572  -0.0291   0.0711   1.0000
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