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Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 30 (rhodesg30-il)
Reynolds number: 500,000
Max Cl/Cd: 88.74 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg30-il-500000.txt
Download as CSV file: xf-rhodesg30-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 30                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4169   0.10493   0.10261  -0.0252   1.0000   0.0356
 -11.500  -0.4272   0.09804   0.09574  -0.0279   1.0000   0.0299
 -11.250  -0.7658   0.03022   0.02699  -0.0618   1.0000   0.0205
 -11.000  -0.7472   0.03037   0.02713  -0.0595   1.0000   0.0196
 -10.750  -0.7568   0.02721   0.02363  -0.0552   1.0000   0.0187
 -10.500  -0.7295   0.02587   0.02161  -0.0552   0.9984   0.0164
 -10.250  -0.6982   0.02436   0.02000  -0.0565   0.9958   0.0153
 -10.000  -0.6693   0.02234   0.01769  -0.0578   0.9928   0.0148
  -9.750  -0.6396   0.02085   0.01598  -0.0587   0.9893   0.0144
  -9.500  -0.6079   0.01961   0.01456  -0.0599   0.9864   0.0142
  -9.250  -0.5747   0.01848   0.01329  -0.0613   0.9841   0.0142
  -9.000  -0.5445   0.01744   0.01215  -0.0621   0.9802   0.0143
  -8.750  -0.5116   0.01657   0.01119  -0.0632   0.9760   0.0143
  -8.500  -0.4763   0.01570   0.01024  -0.0649   0.9730   0.0147
  -8.250  -0.4395   0.01495   0.00939  -0.0668   0.9709   0.0152
  -8.000  -0.4077   0.01442   0.00877  -0.0675   0.9663   0.0154
  -7.750  -0.3744   0.01394   0.00820  -0.0685   0.9618   0.0156
  -7.500  -0.3388   0.01350   0.00766  -0.0699   0.9579   0.0158
  -7.250  -0.3069   0.01309   0.00717  -0.0705   0.9521   0.0160
  -7.000  -0.2763   0.01263   0.00661  -0.0708   0.9457   0.0167
  -6.750  -0.2447   0.01205   0.00592  -0.0714   0.9402   0.0174
  -6.500  -0.2187   0.01142   0.00517  -0.0709   0.9313   0.0184
  -6.250  -0.1863   0.01202   0.00592  -0.0714   0.9238   0.0230
  -6.000  -0.1615   0.01122   0.00501  -0.0706   0.9143   0.0357
  -5.750  -0.1336   0.01130   0.00503  -0.0702   0.9055   0.0383
  -5.500  -0.1048   0.01156   0.00522  -0.0700   0.8971   0.0401
  -5.250  -0.0781   0.01174   0.00541  -0.0696   0.8873   0.0418
  -5.000  -0.0497   0.01254   0.00626  -0.0694   0.8782   0.0450
  -4.750  -0.0220   0.01353   0.00722  -0.0690   0.8678   0.0483
  -4.500   0.0026   0.01276   0.00637  -0.0684   0.8564   0.0502
  -4.250   0.0281   0.01246   0.00608  -0.0679   0.8449   0.0524
  -4.000   0.0542   0.01239   0.00600  -0.0675   0.8339   0.0549
  -3.750   0.0807   0.01245   0.00601  -0.0670   0.8223   0.0574
  -3.500   0.1068   0.01229   0.00574  -0.0665   0.8099   0.0599
  -3.250   0.1322   0.01148   0.00490  -0.0659   0.7973   0.0613
  -3.000   0.1584   0.01114   0.00450  -0.0653   0.7836   0.0611
  -2.750   0.1846   0.01090   0.00419  -0.0647   0.7687   0.0606
  -2.500   0.2104   0.01061   0.00383  -0.0641   0.7526   0.0605
  -2.250   0.2357   0.01030   0.00347  -0.0634   0.7353   0.0606
  -2.000   0.2608   0.01003   0.00313  -0.0626   0.7169   0.0610
  -1.750   0.2857   0.00980   0.00283  -0.0619   0.6968   0.0617
  -1.500   0.3106   0.00965   0.00261  -0.0612   0.6743   0.0624
  -1.250   0.3352   0.00956   0.00244  -0.0604   0.6489   0.0631
  -1.000   0.3597   0.00953   0.00230  -0.0596   0.6197   0.0639
  -0.750   0.3834   0.00958   0.00220  -0.0586   0.5809   0.0645
  -0.500   0.4058   0.00975   0.00214  -0.0575   0.5200   0.0652
  -0.250   0.4274   0.01005   0.00214  -0.0563   0.4553   0.0659
   0.000   0.4511   0.01025   0.00217  -0.0555   0.4220   0.0667
   0.250   0.4760   0.01038   0.00220  -0.0550   0.4042   0.0684
   0.500   0.5016   0.01048   0.00224  -0.0545   0.3917   0.0698
   0.750   0.5273   0.01058   0.00230  -0.0541   0.3821   0.0708
   1.000   0.5531   0.01067   0.00235  -0.0537   0.3746   0.0737
   1.250   0.5790   0.01074   0.00243  -0.0532   0.3683   0.0815
   1.500   0.5895   0.00906   0.00263  -0.0504   0.3625   0.7546
   1.750   0.6703   0.00889   0.00289  -0.0618   0.3493   1.0000
   2.000   0.6940   0.00907   0.00301  -0.0610   0.3428   1.0000
   2.250   0.7182   0.00922   0.00314  -0.0603   0.3381   1.0000
   2.500   0.7427   0.00935   0.00327  -0.0597   0.3331   1.0000
   2.750   0.7663   0.00955   0.00342  -0.0588   0.3264   1.0000
   3.000   0.7911   0.00965   0.00353  -0.0583   0.3193   1.0000
   3.250   0.8151   0.00982   0.00368  -0.0576   0.3127   1.0000
   3.500   0.8397   0.00995   0.00384  -0.0570   0.3068   1.0000
   3.750   0.8641   0.01009   0.00398  -0.0563   0.2990   1.0000
   4.000   0.8887   0.01023   0.00413  -0.0558   0.2902   1.0000
   4.250   0.9129   0.01039   0.00428  -0.0551   0.2785   1.0000
   4.500   0.9371   0.01056   0.00441  -0.0545   0.2565   1.0000
   4.750   0.9513   0.01158   0.00484  -0.0525   0.1516   1.0000
   5.000   0.9659   0.01269   0.00559  -0.0505   0.0885   1.0000
   5.250   0.9831   0.01356   0.00622  -0.0489   0.0534   1.0000
   5.500   1.0051   0.01397   0.00670  -0.0480   0.0503   1.0000
   5.750   1.0259   0.01448   0.00725  -0.0469   0.0472   1.0000
   6.000   1.0455   0.01509   0.00790  -0.0456   0.0442   1.0000
   6.250   1.0637   0.01578   0.00866  -0.0441   0.0420   1.0000
   6.500   1.0844   0.01622   0.00917  -0.0430   0.0407   1.0000
   6.750   1.1038   0.01676   0.00977  -0.0418   0.0391   1.0000
   7.000   1.1217   0.01737   0.01044  -0.0404   0.0372   1.0000
   7.250   1.1379   0.01807   0.01119  -0.0387   0.0354   1.0000
   7.500   1.1466   0.01925   0.01243  -0.0359   0.0333   1.0000
   7.750   1.1590   0.02010   0.01337  -0.0337   0.0319   1.0000
   8.000   1.1749   0.02060   0.01394  -0.0320   0.0307   1.0000
   8.250   1.1874   0.02123   0.01464  -0.0298   0.0293   1.0000
   8.500   1.1995   0.02189   0.01533  -0.0276   0.0277   1.0000
   8.750   1.2090   0.02272   0.01619  -0.0253   0.0263   1.0000
   9.000   1.2022   0.02481   0.01835  -0.0210   0.0246   1.0000
   9.250   1.2181   0.02528   0.01890  -0.0198   0.0238   1.0000
   9.500   1.2313   0.02598   0.01969  -0.0183   0.0225   1.0000
   9.750   1.2424   0.02686   0.02065  -0.0168   0.0213   1.0000
  10.000   1.2520   0.02789   0.02172  -0.0153   0.0205   1.0000
  10.250   1.2584   0.02920   0.02306  -0.0137   0.0195   1.0000
  10.500   1.2550   0.03157   0.02550  -0.0114   0.0186   1.0000
  10.750   1.2658   0.03263   0.02668  -0.0105   0.0180   1.0000
  11.000   1.2750   0.03390   0.02804  -0.0096   0.0170   1.0000
  11.250   1.2812   0.03553   0.02976  -0.0087   0.0164   1.0000
  11.500   1.2875   0.03719   0.03149  -0.0080   0.0158   1.0000
  11.750   1.2936   0.03892   0.03329  -0.0076   0.0152   1.0000
  12.000   1.2947   0.04128   0.03571  -0.0071   0.0147   1.0000
  12.250   1.2921   0.04414   0.03867  -0.0065   0.0144   1.0000
  12.500   1.2904   0.04704   0.04170  -0.0062   0.0138   1.0000
  12.750   1.2910   0.04979   0.04459  -0.0061   0.0135   1.0000
  13.000   1.2899   0.05278   0.04772  -0.0062   0.0133   1.0000
  13.250   1.2898   0.05578   0.05084  -0.0066   0.0130   1.0000
  13.500   1.2873   0.05918   0.05437  -0.0072   0.0126   1.0000
  13.750   1.2859   0.06255   0.05785  -0.0082   0.0123   1.0000
  14.000   1.2844   0.06609   0.06148  -0.0095   0.0120   1.0000
  14.250   1.2818   0.06990   0.06539  -0.0109   0.0117   1.0000
  14.500   1.2796   0.07377   0.06936  -0.0126   0.0115   1.0000
  14.750   1.2756   0.07799   0.07365  -0.0144   0.0112   1.0000
  15.000   1.2697   0.08255   0.07830  -0.0162   0.0110   1.0000
  15.250   1.2585   0.08795   0.08384  -0.0181   0.0108   1.0000
  15.750   1.2309   0.10037   0.09662  -0.0233   0.0105   1.0000
  16.000   1.2184   0.10661   0.10302  -0.0262   0.0106   1.0000
  16.250   1.2067   0.11307   0.10964  -0.0296   0.0105   1.0000
  16.500   1.1935   0.11993   0.11665  -0.0333   0.0104   1.0000
  16.750   1.1766   0.12773   0.12462  -0.0375   0.0104   1.0000
  17.000   1.1596   0.13589   0.13295  -0.0421   0.0103   1.0000
  17.250   1.1381   0.14529   0.14251  -0.0474   0.0104   1.0000
  17.500   1.1176   0.15503   0.15241  -0.0531   0.0105   1.0000
  17.750   1.0834   0.16928   0.16684  -0.0614   0.0106   1.0000
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